Low Earth Orbit (LEO) SATCOM Cybersecurity Assessment
EUROPEAN UNION AGENCY FOR CYBERSECURITY
LEO SATCOM CYBERSECURITY ASSESSMENT
February 2024 0 LEO Satcom Cybersecurity Assessment
February 2024
ABOUT ENISA
The European Union Agency for Cybersecurity, ENISA, is the Union’s agency dedicated to achieving a high common level of cybersecurity across Europe. Established in 2004 and strengthened by the EU Cybersecurity Act, the European Union Agency for Cybersecurity contributes to EU cyber policy, enhances the trustworthiness of ICT products, services and processes with cybersecurity certification schemes, cooperates with Member States and EU bodies, and helps Europe prepare for the cyber challenges of tomorrow. Through knowledge sharing, capacity building and awareness raising, the Agency works together with its key stakeholders to strengthen trust in the connected economy, to boost resilience of the Union’s infrastructure, and, ultimately, to keep Europe’s society and citizens digitally secure. More information about ENISA and its work can be found here: www.enisa.europa.eu. CONTACT For contacting the authors please use info@enisa.europa.eu For media enquiries about this paper, please use press@enisa.europa.eu. AUTHORS Laurent Franck, Satconsult EDITORS Monika Adamczyk, Georgia Bafoutsou, ENISA LEGAL NOTICE This publication represents the views and interpretations of ENISA, unless stated otherwise. It does not endorse a regulatory obligation of ENISA or of ENISA bodies pursuant to the Regulation (EU) No 2019/881. ENISA has the right to alter, update or remove the publication or any of its contents. It is intended for information purposes only and it must be accessible free of charge. All references to it or its use as a whole or partially must contain ENISA as its source. Third-party sources are quoted as appropriate. ENISA is not responsible or liable for the content of the external sources, including external websites, referenced in this publication. Neither ENISA nor any person acting on its behalf is responsible for the use that might be made of the information contained in this publication. ENISA maintains its intellectual property rights in relation to this publication. COPYRIGHT NOTICE © European Union Agency for Cybersecurity (ENISA), 2024 This publication is licenced under CC-BY 4.0 ‘Unless otherwise noted, the reuse of this document is authorised under the Creative Commons Attribution 4.0 International (CC BY 4.0) licence (). This means that reuse is allowed, provided that appropriate credit is given and any changes are indicated”. 1 LEO Satcom Cybersecurity Assessment
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For any use or reproduction of photos or other material that is not under the ENISA copyright, permission must be sought directly from the copyright holders. ISBN 978-92-9204-649-1 doi:10.2824/317096 TP-09-23-475-EN-N 2 LEO Satcom Cybersecurity Assessment
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TABLE OF CONTENTS
LIST OF ABREVIATIONS 5 1. INTRODUCTION 7 1.1 BACKGROUND 7 1.2 SCOPE AND OBJECTIVES 7 1.3 TARGET AUDIENCE 7 1.4 STRUCTURE OF THE REPORT 7 2. LEO SATCOM OVERVIEW 9 2.1 INVENTORY OF LEO SATELLITES COMMUNICATIONS SERVICES 11 2.2 THE FINANCIAL DIMENSION OF LEO CONSTELLATIONS 13 2.3 COMPARISON TO GEOSTATIONARY SATELLITE COMMUNICATION SYSTEMS 14 3. LEO SATCOM ASSETS AND INFRASTRUCTURES 16 3.1 LEO SATCOM SYSTEM ARCHITECTURE 16 3.2 ORGANISATION OF SPACE PROJECTS 18 3.3 TECHNOLOGY AND SUPPLY CHAIN 19 4. SECURITY CHALLENGES FOR LEO SATCOM SYSTEMS AND SERVICES 22 4.1 TECHNICAL RISKS 22 4.2 FINANCIAL AND COMMERCIAL RISKS 23 4.3 MALICIOUS THREATS 23 4.4 NON-MALICIOUS THREATS 27 4.5 CYBER INCIDENTS ON LEO SATCOM SYSTEMS 29 5. STANDARDS AND RECOMMENDATIONS FOR SATCOM CYBERSECURITY 33 5.1 EUROPEAN COOPERATION FOR SPACE STANDARDIZATION 34 3 LEO Satcom Cybersecurity Assessment
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5.2 CONSULTATIVE COMMITTEE FOR SPACE DATA SYSTEMS 35 5.3 EUROPEAN TELECOMMUNICATION STANDARDs INSTITUTE 37 5.4 NATIONAL INSTITUTE OF STANDARDS AND TECHNOLOGY 38 5.5 EUROPEAN SPACE AGENCY AND AEROSPACE CORPORATION THREAT FRAMEWORKS 39 5.6 OTHER INITIATIES 40 5.7 OUTLOOK ON FORTHCOMING INITIATIVES 40 6. CYBERSECURITY STRENGTHS AND WEAKNESSES OF SATCOM IN COMPARISO TERRESTRIAL NETWORKS 42 7. CONCLUSIONS 48 4 LEO Satcom Cybersecurity Assessment
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LIST OF ABREVIATIONS
ADC Analogue-to-Digital Converter AIAA American Institute of Aeronautics and Astronautics AOCS Attitude and Orbit Control System API Application Programming Interface BSI German Federal Office for Information Security (Bundesamt für Sicherheit in der Informationstechnik) CAPEX Capital expenditures CCSDS Consultative Committee for Space Data Systems CERT Computer Emergency Response Team CRM Customer Relationship Manager DVB Digital Video Broadcasting ECSS European Cooperation for Space Standardization ETSI European Telecommunication Standard Institute FDIR Fault Detection, Isolation and Recovery FOP Flight Operation Procedure GMR GEO Mobile Radio GNC Guidance, Navigation and Control GNSS Global Navigation Satellite System GSaaS Ground Segment as a Service GSO Geostationary HEO Highly Elliptical Orbit HTS High Throughput Satellite ICT Information and Communications Technology IOT Internet of things ISL Inter-satellite Link IRIS Infrastructure for Resilience, Interconnectivity and Security by Satellite LEO Low-Earth Orbit LEOP Launch and Early Orbit Phase MAIT Manufacturing, Assembly, Integration and Testing MEO Medium-Earth Orbit M2M Machine-to-machine NRA National Regulatory Authority NOC Network Operation Centre PCB Printed Circuit Board RF Radio frequency RPO Rendezvous and Proximity Operations SATCOM Satellites communication SCC Satellite Control Centre TC Telecommand TM Telemetry TT&C Telemetry, Tracking & Command 5 LEO Satcom Cybersecurity Assessment
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EXECUTIVE SUMMARY
This report covers the topic of cybersecurity of Low Earth Orbit (LEO) constellations delivering telecommunications services (LEO satcom in short). The key specifics of an LEO satcom system may be summed up as (a) many assets forming the space and ground segments and (b) a worldwide distribution of the services delivered by those assets. These two aspects usually differentiate satcom systems from terrestrial and other space systems (such as geostationary satellites), where the service coverage under the responsibility of a single organisation/system is smaller. The global nature of LEO satcom also calls for tailored cybersecurity treatment. When looking at different threats and incurred risks (whether technical, financial or commercial), the landscape of possible attacks is rich. It includes classic cyber threats as found in terrestrial systems that target the user and control segments (terminals, gateways, telemetry tracking and command stations, and interconnection networks). But it also extends to attacks focusing specifically on the satellites forming the space segment. For these reasons, LEO satcom systems deserve a tailored approach when it comes to their security. This situation is acknowledged by actors in the sector and has resulted in several initiatives, among them the European Space Agency (ESA) Space Attacks and Countermeasures Engineering Shield (SPACE-SHIELD). The survey on past cyber incidents shows that most attacks fall roughly into two categories: data theft through reverse engineering of user link transmission techniques; and denial of service, targeting either the ground or space segments, possibly resulting in a service degradation or outage. The first category of incidents calls for the use of common encryption techniques. The second calls for standards and recommendations in cyber protection, which are applicable to all segments of space systems. The report also includes a comparison of LEO satcom and broadband terrestrial cellular networks based on cyber threat exposure and impact severity. The case of cellular networks is believed to be a representative case of more generic terrestrial networks. Based on technical considerations only, the comparison reveals that the cyber risk is higher for space systems. Concluding, the report shows that the cyber protection needs of LEO satcom systems extend beyond what exists for terrestrial systems. The advent of commercial mega-constellations is a clear call for a coordinated approach in space systems security by means of standards, recommendations, information sharing and training. 6 LEO Satcom Cybersecurity Assessment
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1. INTRODUCTION
1.1 BACKGROUND Use of satellite communication for commercial purposes has been rapidly increasing in recent years, with many private companies and entrepreneurs taking advantage of this technology to support their business operations. For that reason, the rapidly growing satellite sector, particularly relying on LEO satellite infrastructure, is becoming an increasingly important part of the overall EU electronics communications market and is a focus of attention for the telecommunications National Regulatory Authorities (NRAs). Under the European Electronic Communications Code (EECC) directive , the NRAs have the obligation to supervise the security of electronic communication networks and services. Satellite operators providing electronic communications services for a fee are within the scope of the EECC supervision. The NIS2 directive includes the providers of public electronic communications networks and services as one of the critical sectors for which uniform security measures must be applied . ENISA has identified lack of analysis and control of space-based infrastructure and objects as one of the top cybersecurity threats that are likely to emerge by 2030 . 1.2 SCOPE AND OBJECTIVES With this study, ENISA wants to provide a better understanding of the LEO satcom sector from the cybersecurity perspective. However, while the report focuses on LEO satellites used for communications services, we need to acknowledge that geostationary satellites have shaped the satcom market for decades generating more than 90 % of satcom revenues. It is only recently that there has been a renewed interest and commercial activity around LEO systems. For that reason, this report will make several references to geostationary satellites to better highlights the specifics of LEO systems and their heritage as far as cybersecurity is concerned. 1.3 TARGET AUDIENCE This document is aimed at national authorities supervising the implementation of Article 40 of the EECC and in general at national authorities that are responsible for telecom security. It may also be useful for policy experts in the European Commission, cybersecurity agencies, experts working in the telecom or satcom sectors, industry associations and other bodies with roles in standardisation and telecom security. 1.4 STRUCTURE OF THE REPORT After the introduction, the report is structured as follows. • Chapter 2 discusses the purpose of LEO satellite for communications services: what services they provide and what the known present and forthcoming systems are. Financial considerations are also addressed.
Directive (EU) 2018/1972 of the European Parliament and of the Council of 11 December 2018 establishing the European Electronic Communications Code (Recast) (OJ L 321, 17.12.2018, p. 36), https://eur-lex.europa.eu/legalcontent/EN/TXT/?uri=CELEX %3A02018L1972-20181217. Directive (EU) 2022/2555 of the European Parliament and of the Council of 14 December 2022 on measures for a high common level of cybersecurity across the Union, amending Regulation (EU) No 910/2014 and Directive (EU) 2018/1972, and repealing Directive (EU) 2016/1148 (NIS 2 Directive) (OJ L 333, 27.12.2022, p. 80), https://eur-lex.europa.eu/eli/dir/2022/2555. As stated in Article 43 of the NIS2 directive, Articles 40 and 41 of the EECC will be deleted in October 2024. Instead, the security measures defined in Article 21 of the NIS2 directive will apply to the telecommunication sector. Cybersecurity Threats Fast-Forward 2030: Fasten your Security-Belt Before the Ride!, https://www.enisa.europa.eu/news/cybersecurity-threats-fast-forward-2030.
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• Chapter 3 gives insights into how LEO systems are designed and the key engineering concepts. • Chapter 4 provides an inventory of threats to which LEO telecommunications are exposed and identifies past cyber incidents affecting these systems using publicly available sources. It also includes a sample (proof of concept) attack made on an experimental satellite to illustrate how spacecraft vulnerabilities can be exploited. • Chapter 5 describes current standardisation and recommendation initiatives published in the field of space systems security. • Chapter 6 compares space and terrestrial systems from a cybersecurity standpoint on grounds of threat exposure and impact severity. • Chapter 7 concludes by issuing some recommendations in the light of prior chapters. 8 LEO Satcom Cybersecurity Assessment
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2. LEO SATCOM OVERVIEW
Low Earth Orbit (LEO) satellites are orbiting the Earth at altitudes of several hundreds of km and provide communications services to users mostly located in remote places with no or weak connection to terrestrial infrastructures. LEO satellites are located at an altitude below 2 000 km but are generally in range from 500 km to 1 400 km above the Earth’s surface, the orbital plane being often inclined with respect to the equatorial plane. Medium Earth Orbit (MEO) systems have a circular or elliptical orbit, their farthest point on orbit being located at an altitude ranging from 8 000 to 40 000 km (this is the case of Highly Elliptical Orbit (HEO)). As far as this report is concerned, no difference is made between LEO and MEO /HEO. Finally, this report also makes references to geostationary (GSO) satellites. These satellites have an altitude of around 36 000 km, their orbital plane being aligned to the Earth’s equatorial plane. From the viewpoint of an on-Earth observer, they appear fixed in the sky. An LEO satellite sweeps the Earth’s surface with a given revisit period due to the combined effect of satellite motion and the Earth’s rotation. By arranging several (10+) satellites in a pattern called a constellation, it is possible to ensure that any place within the service delivery area on Earth will be covered by at least one satellite at any time. Some systems may even be composed of ‘layers’ of satellites arranged at different altitudes. The dynamics of a constellation make the end-to-end communication system more complex to engineer compared to a satellite located on the geostationary orbit. In consequence, the operating costs for large LEO satellite constellations are higher when compared with GSO satellites. However, the cost of bringing LEO satellites into orbit is significantly lower than that of launching GSO satellites. On the other hand, the smaller distance from Earth favours shorter (about 20 to 80 times smaller) radiofrequency propagation delays to the benefit of interactive communications services. Section 2.3 will cover the differences between geostationary systems in more detail. An electronic communications service based on an LEO satellite system can follow several basic scenarios (see also Figure 1). • Scenario 1. A remote person/device (called the remote terminal) uses the satellite as a relay to establish a communication link to/from an Earth station that provides interconnection to the terrestrial backbone networks. This setup can be extended if several satellites are interconnected through inter-satellite links (ISLs), relieving the need to hop to/from intermediate ground infrastructures to reach the destination. • Scenario 2. Two remote terminals use a satellite as a relay to communicate with each other (possibly by going through several satellites if ISLs are present). • Scenario 3. A remote terminal posts/receives messages to/from a passing satellite, these messages being transferred to/from the terrestrial backbone network when the spacecraft passes over an Earth station. This scheme is called store-and-forward operations. 9 LEO Satcom Cybersecurity Assessment
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Figure 1: Different scenarios of terminal–satellite–Earth station communications The following is a summary of the key points of LEO satellite communications systems. • LEO satellites sweep the surface of Earth on a periodic basis. • The communication service offered is global (truly worldwide if the orbit inclination is highly aligned to North–South) thanks to Earth–spacecraft relative motion. • The delivery of the service relies on the capability to communicate via radiofrequency and in the future via optical links to/from the satellite by means of remote terminals and ground facilities (e.g. Earth stations). • While a remote terminal requires limited infrastructures (power-supply or none for battery-operated terminals), ground infrastructures are needed for the Earth stations that provide inter-connection to the terrestrial networks and the systems that ensure spacecraft monitoring and control. • The combination of satellite coverage and radio frequency also enables the communication of messages from one peer to many using a single transmission. 10 LEO Satcom Cybersecurity Assessment
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2.1 INVENTORY OF LEO SATELLITES COMMUNICATIONS SERVICES Table 1 lists services that are typical to LEO satcom constellations by summarising the elements examined in the previous sections. Table 1: Types of services provided by LEO satcom systems
Service type Service description Applications
Internet of things (IOT), machine-to- Uni- or bidirectional exchange of short machine (M2M), emergency alerting
Short message
(less than 200 bytes) messages (when combined with satellite-based localisation)
Bidirectional exchange of generic data at M2M, basic internet access (email, Narrowband data throughput less than 100 kilobits per frugal web browsing) second (kbit/s)
Bidirectional exchange of generic data at Internet access (email, web browsing), Broadband data throughput ranging from 100 kbit/s to audio/video conferencing, video several megabits per second (Mbit/s) streaming, Voice over IP
Bidirectional interconnection of networks at Network interconnection, extension of
Trunking
high throughput (several tens of Mbit/s) cellular networks
Bidirectional, real-time voice Voice Telephony communication
Table 3 provides examples of how these applications can be implemented. Each example is linked to the critical sectors identified in Annex 2 and 3 of the NIS2 directive. Table 2: Satcom applications and their relation to NIS2 directive critical sectors
Application Example of implementation Sector from NIS2 Annex 1
Location tracking of a container and alerting in IOT Transport / rail case of anomaly (e.g. door opening)
Network Backup trans-national network for the monitoring Energy / electricity interconnection of European power grids
Satellite-enabled telephony for assessment teams during a disaster with potential Telephony Public administration destruction/saturation of the terrestrial cell phone networks
Monitoring and remote operation of hydroelectric M2M Energy / electricity plants in remote areas
Backup of terrestrial-based internet access for the Internet access Health / healthcare providers logistics department of a hospital
These applications can be deployed in terrestrial, maritime and aeronautical environments, categorising the terminals either as fixed or mobile (with communication on the move or in one place). LEO satellites are also sometimes used to deliver services such as remote sensing or Earth observation (e.g. images, infrared, radar) and location and navigation services. These services are not categorised as satellite communications services and are therefore outside the scope of this report. 11 LEO Satcom Cybersecurity Assessment
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Table 3 lists the main and future LEO/MEO constellations, with key characteristics and associated service types, that were on the market at the time when the study was conducted ( ). The future constellations listed are those that have secured funding. The number of satellites does not include ground or in-orbit spares. For the definition of the narrowband/broadband data throughputs (in bit/s), a distinction has been made between the uplink throughput (from the user to the spacecraft) and the downlink throughput (from the spacecraft to the user). The actual performance is subject to the number of users sharing the uplink and the environmental conditions (snow and heavy rain may degrade performance). Table 3: Key characteristics of current and future LEO/MEO constellations
% of No of spacecrafts Owner satellites launched to Name Service types Coverage (country) for full achieve deployment operational status
Selected Short message areas below Globalstar Narrowband data northern polar Globalstar (United 24 100 % (10 kbit/s bidirectional) and above States) Voice southern polar regions.
Short message Narrowband data Gonets/Leosat Gonets 36 Unknown (9.6 kbit/s uplink, Russia (Russia) 20 kbit/s downlink) Voice
Short message Narrowband data (20 kbit/s uplink, 90 kbit/s Iridium (United downlink) Iridium 66 100 % Global States) Broadband data (350 kbit/s uplink, 700 kbit/s downlink) Voice
Area below Amazon Broadband from northern Kuiper (United 3 236 0 % 100 Mbit/s to 1 gigabit Europe and States) per second (Gbit/s) above Patagonia
OneWeb Broadband (up to OneWeb (United 648 100 % 32 Mbit/s uplink, Global Kingdom) 195 Mbit/s downlink)
Selected areas below SpaceX Broadband (up to Northern polar Starlink (United 4 408 > 74 % 250 Mbit/s bidirectional) and above States) Southern polar regions.
Area below northern O3b SES Broadband (up to 11 (MEO) 18 % Europe and mPOWER (Luxembourg) 400 Mbit/s bidirectional) above Patagonia
Satellite company’s websites in April 2023 and Euroconsult, Quarterly briefing, NGSO constellations, Q4 2022.
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Looking at Table 3, it should be noted that not all constellations provide global (i.e. truly worldwide) coverage. A constellation operator devises its business model according to considerations such as (a) covering locations where the market demand is expected to be high and (b) covering locations where the market demand is low, but users are ready to pay premium prices because access to communication capabilities is critical. The service provisioning by a satellite constellation also depends on the landing rights obtained from NRAs. Some constellations provide services to residential end-user terminals while others target commercialisation of capacity towards enterprises only. In addition to the operators listed above, there are others that deploy constellations targeting message exchange services. Because these low-price services are based on non-real-time low bit rate communications, spacecrafts can be smaller (from several kilogrammes to several tens of kilogrammes), reducing manufacturing and launching costs . It should be noted that while these operators do not have the media coverage of the ones listed above, they are also very likely to be the target of cyberattacks. Finally, it should be noted that the constellations listed in Table 3 are all commercial systems. However, some of them are also used for military applications, making them de facto dual-use systems. 2.2 THE FINANCIAL DIMENSION OF LEO CONSTELLATIONS This section covers the financial aspects of building, launching and operating satellite constellations. This information helps to assess the value of the assets in the event of a cybersecurity incident. The cost breakdown of building and running a satcom constellation is as follows. • Design and manufacturing cost of the satellites. • Launching costs. • Ground facilities (Earth stations, infrastructures, data centres, high data rate links). • Recurring operations costs and maintenance costs on the ground infrastructures. The quantitative breakdown varies a lot among all constellations as it depends on the strategy chosen: a lot of small satellites offering little individual capacity or more capacitive and powerful satellites. The total manufacturing and launching costs can exceed EUR 10 billion in case of mega-constellations with several thousands of satellites. From a business standpoint, these costs are then to be balanced by the revenues from selling the services either directly to end users and enterprises or to resellers (e.g. selling bulk communication capacity). In the case of a cybersecurity incident, the potential impact encompasses the loss of the asset and the loss of the revenues associated with the asset. Taking this perspective, Table 4 gives examples of service prices for some of the constellations listed in the previous section.
Monteiro, J. B. et al., ‘A review of SmallSat constellations for IoT connectivity’, Proceedings of the 73rd International Astronautical Congress, Paris, 18–22 September 2022, 2022. Satellite company’s websites in April 2023 and Euroconsult, Quarterly briefing, NGSO constellations, Q4 2022.
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Table 4: Estimates of service price for several satcom constellations
Name Services prices
EUR 99/month for a 150-minute call plan Globalstar EUR 14.95/month for 20 custom messages sent, unlimited predefined messages transmission, unlimited message reception
EUR 153 for a 75-minute call plan per month Iridium EUR 300/month for a 300 megabyte data plan (Certus service) EUR 35.10/month for 17 kilobytes of short messages
EUR 200/month per connectivity data rate of 1 Mbit/s (trunking service not meant for
OneWeb
residential users)
USD 5000/month for 100–350 Mbit/s, unlimited data (maritime service and prosumers) Starlink Around EUR 70/month (pricing depending on country) for basic service (50–100 Mbit/s best effort, about 250 gigabytes of data volume)
O3b mPOWER From EUR 100 to EUR 450/month per Mbit/s
To get access to the service, the end user must also procure a terminal. Depending on the form factor and capabilities (possible throughput, antenna technology), the price ranges from several hundreds of euros to tens of thousands. Looking at the trends, it is expected that by 2031, the market value of the capacity provided by LEO satcom systems will double compared to 2021, while the market value of capacity available from geostationary High-Throughput Systems (HTS) will increase by a margin. 2.3 COMPARISON TO GEOSTATIONARY SATELLITE COMMUNICATION SYSTEMS What differentiates LEO and GSO telecommunications systems is summarised below. • Lower latency. Compared to the geostationary orbit, a lower altitude yields shortest propagation delay therefore easing the delivery of services where interactivity is key. • Stronger signal. Similarly, the signal transmitted from the spacecrafts suffers less from free space loss (as a rule of thumb, doubling the travel distance cuts the signal power by four). It can either favour larger throughput or more integrated terminals. • More satellite diversity. A lower altitude leads to a tighter instantaneous service coverage for single spacecraft. It calls for multiple spacecrafts and therefore a more complex space segment. However, the potential coverage of the constellation is then broader than the one of a single geostationary satellite (three geostationary satellites are needed to provide a global coverage between latitudes 80° North and South). • More ground infrastructure. For a similar reason, LEO satcom systems require up to 10 times more earth stations for the ground infrastructure compared to geostationary satellite systems. • Smaller antennae and terminals. When a high throughput (> 50 kbit/s) is required, the relative motion of the spacecraft calls for complex antenna designs (compared to a fixed antenna dish); on the other hand, the lower altitude of the orbit enables smaller antennae and therefore smaller terminals. • Lower single spacecraft capacity. The communication capacity (in bit/s) of a single LEO spacecraft is lower than that of a geostationary satellite, therefore challenging from a financial standpoint throughput-hungry services such as multimedia
Euroconsult, Satellite Connectivity and Video Market, 29th edition, 2022.
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broadcasting. In addition to that, the larger coverage of geostationary satellites favours broadcasting. • Higher system capacity. Because multiple satellites are used, the overall capacity (in bit/s) of the constellation is usually higher than the one of a single high-throughput geostationary satellite (several terabits per second vs several tens of Gbit/s) • Shorter lifetime. The lifetime of a geostationary satellite is often rated for 15 years of service. A LEO satellite lifetime can be as low as 5 years, especially if the industrial strategy favours low-cost, low-lifetime spacecrafts over more costly ones. • More redundancy. LEO satcom systems often accommodate for in-orbit spares. This is one of the reasons that achieving high reliability is less costly. Redundancy in geostationary satellite networks can only be achieved through the deployment of several GSO satellites over close (or similar) orbital positions. 15 LEO Satcom Cybersecurity Assessment
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3. LEO SATCOM ASSETS AND INFRASTRUCTURES
This chapter covers how a LEO satcom system is organised into different segments, each segment being assigned a role in the delivery of the mission and the control of the system. The discussion will also serve as a foundation for highlighting the engineering and industrial processes supporting the development of such systems and finally highlighting the core technological blocks and the associated supply chain. 3.1 LEO SATCOM SYSTEM ARCHITECTURE A LEO satcom system is split into three segments. • The space segment includes the satellites forming the constellation. Each satellite comprises a platform and a payload. The payload is the subsystem supporting the mission, the platforms provide all services for spacecraft to behave as expected (e.g. thermal control, power supply, attitude control, etc.). • The user ground segment covers all entities contributing to the delivery of the communications services: fixed and mobile terminals, and the Earth stations called gateways or hubs. • The control ground segment hosts entities contributing to: (a) command and control of the space segment: the Telemetry, Tracking and Command (TT&C) station and the Satellite Control Centre (SCC) and (b) control, configuration, and monitoring of the user ground segment: the Network Operation Centre (NOC). The ground segment makes sure that the mission is conducted within the expected service level objectives. The launch segment is also present, being extensively active at the very start of the system' operational lifetime. While the launch segment is not part of the LEO satcom system, its importance should not be neglected as – in addition to the initial constellation deployment – it also plays a role in placing in-orbit spare spacecrafts. For the sake of completeness, the list of technological domains provided at the end of this chapter also covers the launch segment. Figure 2 depicts how the space, ground and user segments constitute an end-to-end system. • The satellites serve the associated terminals under their coverage, acting as relay with the gateway that is visible from the satellite. If inter-satellite links (ISLs) are present, mutual visibility between the terminal and the gateway is not required and ISLs are used to reach a distant gateway. • User service requests (e.g., a new terminal logged in the network, a terminal issuing a call or data requests) are mapped to the satellite network resources by the NOC. The NOC instructs the gateways and the satellite control centre (SCC) (see below) accordingly. • The SCC commands and monitors the fleet of satellites by means of several TT&C stations. These stations, on behalf of the SCC, receive telemetry (health information) and send telecommand (configuration and operation orders) to the satellites that are visible. They can also collect information contributing to the accurate localisation of the satellites. Later in this chapter, the various technologies supporting all these entities will be covered. 16 LEO Satcom Cybersecurity Assessment
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Figure 2: Organisation in segments of an LEO satcom system Figure 3 shows how this translates from a geometrical standpoint with examples of radio frequency (RF) links between the satellites and their respective TT&C station (circles), gateways (squares) and terminals (triangles) under visibility (grey discs). The constellation depicted below is the first generation of the Iridium system: 66 satellites distributed over 6 orbital planes in a close-to-polar layout. In addition to the geometrical aspects, the figure helps with understanding the dynamics of the ground-to-space connectivity: the satellites are moving in a North–South pattern and the Earth rotation makes them also sweep East–West. From the perspective of a cyber attacker on the ground, a satellite is only visible for a fraction of time (up to 10 minutes for the Iridium system depicted here). 17 LEO Satcom Cybersecurity Assessment
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Figure 3: Example of RF communication links involving TT&C stations Geostationary satcom systems are also organised in three segments (space, user and control) and the roles of the different entities are similar. The difference lies in the number of satellites and user/control ground entities and in their distribution over the Earth. LEO satcom systems call for a high number of gateways (e.g. as of Q4 2022 the Starlink constellation features around 160 active gateway sites, each site hosting between 8 and 32 antennae). By comparison, a high-throughput geostationary satcom system may require up to 10 gateways. The same rule applies to the TT&C stations. A typical geostationary satcom will provision for two TT&C stations in active-passive configuration. A LEO satcom constellation should account for a larger number, finding the adequate trade-off between the cost of the ground system and the operability of the constellation. Therefore, it is not uncommon for an LEO satcom constellation to have about 50 % of the Capital Expenditures (CAPEX) dedicated to the ground system. For remote sensing LEO systems, there is an emerging trend around the concept of Ground Segment as a Service (GSaaS). This approach makes sense when the ground segment is not permanently used (e.g. because of low density of the space segment). For LEO satcom systems that provide ‘anywhere, anytime’ communications services, the GSaaS concept can be revisited. Indeed, while a gateway antenna cannot be shared among different satellite operators, the upstream devices (modems, computing capabilities, storage) can be. 3.2 ORGANISATION OF SPACE PROJECTS This section covers the engineering and industrial processes that are involved in the design, development and operations of LEO satcom systems. Because of their human and financial stakes, complexity and often non-recurring schemes, space projects are backed by wellestablished methodological frameworks. See for example the European Cooperation for Space Standardization (ECSS) ECSS-M-ST-10C standard . Overall, a project is split into several phases that span the major stages of the system life cycle: (a) early definition and feasibility studies, (b) definition and design, (c) production and testing and (d) utilisation and disposal. The three segments can be considered as different projects
ECSS, ‘ECSS-M-ST-10C Rev.1 – Project planning and implementation (6 March 2009)’, 2009.
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since they are addressed by different manufacturers. This report will focus on the space segment because it is arguably the most challenging. Moreover, compared to project management for the manufacturing of consumer goods (cars, smartphones, etc.) there are major differences, as listed below. • From the early design to the beginning of utilisation, up to 10 years can pass. • A spacecraft is made of thousands of parts, most of these parts coming from suppliers. • Several thousands of documents are produced during the project lifetime and stored in a document management system. • The processes for design, production, testing and utilisation are now supported by digital tools forming a consistent and comprehensive suite relying heavily on data management and processing. For example, all satellite telemetry received from the early tests to the Launch and Early Orbit Phase (LEOP) operations and onwards is stored in a data lake. • Today’s satellite manufacturers rely heavily on subcontractors, especially for the production and testing phases. • Customers (i.e. the operators buying the satellites) participate in most phases of the project. They are based on-premises in dedicated offices, and have access to documentation and to clean rooms hosting the manufacturing, assembly, integration and testing (MAIT) facilities. These clean rooms can also host other projects at the same time. 3.3 TECHNOLOGY AND SUPPLY CHAIN Table 5 provides a list of technology domains that are used in LEO satcom systems (including the launch segment). The taxonomy refers to the ESA Technology Tree and is also used in Table 6 for the definition for each technology domain. This report only addresses the technology domains pertaining to the scope of telecommunications as defined in the Article 2 of the EECC . The ESA technology tree also includes two technology domains that are transverse to all segments: (a) system design and verification and (b) quality, dependability and safety. The latter includes aspects such as commercial off-the-shelf components and subsystems. Table 5: ICT-related technology domains used in LEO satcom systems
Entity/segment Technology domains
On-board data subsystem / space system software / space system Launch segment / launch vehicle control / RF subsystems, payloads and technologies / electromagnetic technologies and techniques.
Space system software / mission operation and ground data
Launch segment / control centre &
systems / ground station systems and networks / electromagnetic
tracking stations
technologies and techniques.
On-board data subsystem / space system software / space system control / RF subsystems, payloads and technologies /
Space segment / spacecraft
electromagnetic technologies and techniques / flight dynamics and global navigation satellite system (GNSS) / optics.
Space system software / space system control / mission operation Ground segment / TT&C station and ground data systems / ground station systems and networks / electromagnetic technologies and techniques / optics.
Ground segment / gateway Space system software / space system control / ground station systems and networks / electromagnetic technologies and Ground segment / user terminal techniques / optics.
ESA, ESA Technology Tree – Version 4.0, STM-277 3rd edition, ESA Communications, 2020. See Directive (EU) 2018/1972.
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Space system software / mission operation and ground data
Ground segment / network operation
systems / RF systems, payloads and technologies / ground station
centre
systems and networks.
Space system software / mission operation and ground data
Ground segment / Satellite control
systems / ground station systems and networks / flight dynamics and
centre
GNSS.
Table 6: Definition of the technology domains (reproduced from the ESA technology tree taxonomy document).
Technology domain Definition (from the ESA Technology Tree)
Spacecraft data management; payload data processing; hardware and software required for data acquisition, data processing, storage
On-board data subsystem
for both payload and spacecraft data, on-board networking and the space-link network layer and above.
All basic techniques and technologies in the fields of software and Space system software information technology (IT) with respect to their application to space missions, for both space and ground segment.
Design and implementation of control subsystems for space applications. Includes attitude and orbit control system (AOCS) for Space system control satellites; guidance, navigation and control (GNC) for space vehicles and launchers; and pointing acquisition and tracking systems for antennae, laser terminals, and line-of-sight stabilisation equipment.
All technologies and techniques operating in the RF domain related to satellite systems and networks, spacecraft payloads, instruments and specific ground equipment, for telecommunication, TT&C, RF subsystems, payloads and navigation, Earth observation and space science, including security technologies aspects. (Technologies for control centres, TT&C and Earth Observation Payload Data Transmission Ground Stations and Ground Station Networks are covered in ‘Ground station systems and networks”)
Electromagnetic technologies and Antennas and related technologies, wave interaction and techniques propagation, and electromagnetic compatibility.
Aspects related to the control and operations of space system Mission operation and ground data elements (satellites, transfer vehicles, orbiters, landers, probes, systems rovers, etc.) and related ground segment, addressing the technologies associated with supporting subsystems and tools.
All elements and know-how required for the engineering of the Ground station systems and facilities that connect the space segment with control centres. The networks application range covers everything from high-performance deepspace stations to networks of small ground stations.
Activities related to the analysis and definition of trajectory aspects of space projects, known as mission analysis. All operational ground activities related to the measurement and control of spacecraft orbit
Flight dynamics and GNSS
and attitude. Provision of precise navigation services to both groundand space-based users and also the provision of the geodetic reference frame.
Technologies and techniques for subsystems, instruments and Optics components, as well as design, engineering and verification methods, in the field of optics.
The supply chain also plays an important role in the design, development, and operation of space systems. Here, the supply chain encompasses suppliers of hardware parts (e.g. ground 20 LEO Satcom Cybersecurity Assessment
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segment network appliances), subcontract workers (e.g. at the spacecraft assembly, integration, and test facilities) and service providers (e.g. leased line operators for the ground segment). The supply chain for the space domain faces several challenges. • As already mentioned, suppliers are extensively involved in all segments. • Components can be highly specialised, not only because of their role, but also because of the manufacturing constraints regarding the space environment. This negatively impacts the price and reduces the number of suppliers. • For the space segment, security risk detection or mitigation can only be consolidated while the components are on the ground. These characteristics call for common and agreed quality and security practices among all stakeholders of the supply chain. They also raise the question of sovereignty and trust for critical components. Finally, they call for automated late testing/auditing when the components are in a controlled environment. 21 LEO Satcom Cybersecurity Assessment
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4. SECURITY CHALLENGES FOR LEO SATCOM SYSTEMS AND SERVICES
As described in the prior chapters, LEO satcom systems are complex and associated with high financial risks. The most dominant feature of the investment is that there is almost no exit strategy: once deployment has commenced, the complete constellation configuration needed in order to start services must be brought into use. This chapter deals with threats (malicious and non-malicious) and risks (technical and nontechnical) to LEO satcom systems. Threats and risks are both related to vulnerabilities. The chapter focuses on cybersecurity related threats and ends with an inventory of past cyber incidents that affected LEO satcom systems. 4.1 TECHNICAL RISKS Table 7 lists possible technical risks to which an LEO satcom system can be exposed. Risks can be multiple and linked in a causal relationship (e.g. a spacecraft being hijacked can lead to its destruction). Table 7: Technical risks affecting LEO satcom systems
Risk Details
Degradation of the user service quality (e.g. the offered User service degradation/outage throughput) or, in the worst-case scenario, interruption of the service.
Degradation or interruption of the capability to monitor/control
Monitoring and control
the user service, the ground segment or the space segment
degradation/outage
(e.g. loss of commanding capability on a spacecraft).
Damage to or destruction of ground segment equipment or spacecraft, or a subsystem of the spacecraft (e.g. overdriving
Asset damage/destruction
an on-board Analogue to Digital Converter (ADC) by inputting a very strong RF signal).
Disclosure of sensitive information (e.g. leak of the spacecraft
Data theft, data leak
engineering blueprints).
Damage to / destruction or theft of assets or services
Extraneous asset or service
belonging to an external organisation (e.g. interference to a
damage/theft
neighbouring satellite damaging the service quality).
Use-without-right of the satellite’s capability (e.g. Capability hijacking communications capability hijacking or rogue spacecraft manoeuvre).
Information forgery Forgery of information.
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4.2 FINANCIAL AND COMMERCIAL RISKS These risks are related to the non-tangible assets of the organisation, such as reputation or commercial profitability. Investments in satellite communications are high yield / high risk. Securing proper and reliable debt financing is therefore challenging. Table 8: Financial and commercial risks
Financial and commercial risk Details Main associated technical risks
Satcom services are often considered as ‘premium services’ User service degradation/outage either because of their price or Monitoring and control because of their positioning on the market. Satellite operations degradation/outage Harm to the company require careful coordination Data theft, data leak reputation between all space stakeholders (orbits, frequency). Extraneous asset or service damage/destruction/outage Having a reputation for being serious in business often helps the Capability hijacking business itself run smoothly.
Chapter 2 indicates that, to offer a User service degradation/outage global service, a constellation of satellites is required as well as a Capability hijacking Loss of commercial set of earth stations. Any capabilities impairment to these elements can Monitoring and control compromise the delivery of the degradation/outage communication service, leading to Asset damage/destruction financial loss, among other things.
The provision of satellite communications services is often associated with service-level agreements (SLA). This is User service degradation/outage Financial loss because of especially enforced if the satellite penalties communication service is Extraneous asset or service established as a backup of a damage/destruction/outage terrestrial service. Non-compliance with SLA leads to financial penalties.
The recent developments in New Space have led to an increase in competition between LEO satcom operators. The competition spans Data theft, data leak Loss/degradation of from the technical to commercial Asset damage/destruction competitive advantage fields. Therefore, any delay in the time to market or leak of industrial Capability hijacking property may lead to the degradation of competitive advantage.
4.3 MALICIOUS THREATS All systems are exposed to threats. A threat will resolve into a successful attack when an existing vulnerability is exploited. It is therefore important to know the threats targeting LEO satcom systems and to devise adequate prevention and recovery plans. Table 9 shows a list of malicious threats, which are associated with the technology domains described in an earlier chapter. This list is inspired by attack matrices such as the European Space Agency (ESA) space attacks and countermeasures engineering shield (SPACE-SHIELD) , space attack research
ESA, ‘SPACE-SHIELD’, ESA website, retrieved May 2023, https://spaceshield.esa.int/.
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and tactic analysis (SPARTA) and MITRE ATT&CK . Work on the threat landscape has been conducted by various organisations, including academics and the Center for Strategic and International Studies (CSIS) . According to the published findings, attack campaigns use the weakest spot as an entry point in the system and exploit (e.g. through lateral movements) a sequence of threats to achieve their goal. Therefore, several threats can be involved in a single attack. Table 9: Threats of malicious origin
Technology Threats Short definition and example domains
Signal/information level threats
RF subsystems, payloads and technologies, Transmission of a stronger signal to degrade the space system Signal jamming/interference quality of a legitimate signal and disrupt its effect 17 control, ground (e.g. jamming the telecommand TC uplink) . station systems and networks, optics.
RF subsystems, payloads and Forgery of a signal bearing wrong information technologies, Signal spoofing (e.g. spoofing of GNSS signals to misroute a 18 ground station spacecraft) . systems and networks.
RF subsystems, payloads and Replay of a previous valid signal to trick the technologies, Signal replay receiving entity (e.g. replay of a 19 ground station telecommand) . systems and networks.
RF subsystems, payloads and Study of signal characteristics to derive technologies, Signal intelligence additional knowledge (e.g. reverse engineering 20 ground station of the user downlink signal) . systems and networks.
On-board data subsystems, Illegitimate interception of information to gain space system knowledge (e.g. capture of login/passwords software, ground
Information eavesdropping
when using unsecured remote-access/web 21 station systems protocols) . and networks, mission operation and
The Aerospace Corporation, ‘SPARTA: Space Attack Research and Tactics Analysis’, Aerospace website, retrieved May 2023, https://aerospace.org/sparta. MITRE, ‘MITRE ATT&CK’, MITRE website, retrieved May 2023, https://attack.mitre.org/. Pavur, J., ‘Securing New Space: On Satellite Cyber-Security, A thesis submitted for the degree of Doctor of Philosophy, University of Oxford, 2021; Plotnek, J., ‘A threat-driven resilience assessment framework and security ontology for space systems’, thesis submitted for the degree of Doctor of Philosophy, The University of South Australia, 2022. CSIS, Bingen, K. A., Johnson, K. and Young, M., Space Threat Assessment 2023, Center for Strategic and International Studies, Washington DC, 2023. Some states have army corps dedicated to electronic warfare including mobile transmitting stations for jamming satellites. Some LEO satellites rely on GNSS signals for orbit determination. Signal replay can be used to fool a system protected with authentication if no anti-replay protection is embedded. A TC can then be issued twice (the first time being legitimate), with expected harmful consequences. Characterising an unknown signal (frequency, modulation, and coding schemes) is the first step in gathering intelligence from its source or developing a signal spoofing strategy. Information eavesdropping is the first technique used on clear (not encrypted) communication channels to capture sensitive information (e.g. passwords).
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ground data systems.
On-board data subsystems, Forgery of fake information to fool a user or space system system (e.g. forgery of an illegitimate command software, ground packet to gain access to a spacecraft station systems
Information spoofing
subsystem). This threat can be part of the and networks, subsequent stages of an attack based on an mission initial threat. operation and ground data systems.
System/subsystem level threats
On-board data subsystems, space system software, space system control, Illegitimate use of the satellite RF subsystems, Payload hijacking 22 (communication) . payloads and technologies, mission operation and ground data systems.
On-board data subsystems, space system software, space system control, RF subsystems, Illegitimate control of the spacecraft platform payloads and Platform hijacking (e.g. modifying the spacecraft attitude to create technologies, service outage) ground station systems and networks, mission operation and ground data systems.
Interaction with a system/subsystem to create
System/subsystem
disruption (e.g. blinding of spacecraft star All impairment 23 tracker with a laser during a manoeuvre) .
Hardware-/software-level threats
Physical interaction with a component to gain an advantage (e.g. physical connection to a spacecraft bus probe point to collect information). This is an example of insider threat. However, physical tampering is not Physical tampering restricted to phases where the spacecraft is on All the ground (e.g. in clean room). Some states have developed spacecrafts meant for illegitimate interaction with / inspection of other spacecrafts called rendezvous and proximity operations (RPO)
Hardware backdoor Modification of a hardware component to All add/modify functionalities (e.g. a modified
Some satellites work as transparent RF relays, taking the signal that comes in, amplifying it and sending it back to Earth. With that respect, there is no check as to whether or not the signal is legitimate. In the most extreme form, it includes the use of anti-satellite kinetic weapons such as missiles. Such destruction will generate additional space debris. The Kessler syndrome depicts a phenomenon where a sudden increase of debris on an orbit may damage other spacecrafts, triggering a chain reaction of destruction.
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chipset in a computer to bypass memory read protection). This is an example of insider threat.
On-board data subsystems, space system software, space Modification of a software component to system control, add/modify functionalities (e.g. a network server ground station Software backdoor that receives a specific illegitimate packet will systems and trigger the execution of unwanted code). This is networks, an example of insider threat. mission operation and ground data systems.
On-board data subsystems, space system software, ground Injection of rogue software to conduct station systems Malware injection illegitimate activities (e.g. injecting a key logger and networks, on a control centre computer). mission operation and ground data systems.
On-board data subsystems, space system software, ground Exploit of a software/hardware weakness to gain station systems Privilege escalation undue privileges (e.g. hacking of a modem to 24 and networks, bypass transmit power limitations) . mission operation and ground data systems.
User-level threats
Ground station systems and Taking advantage of human networks, space weakness/credulity/fears to gain information system software,
Social engineering
knowledge (e.g. phishing to gain access to mission remote access credentials). operation and ground data systems.
Taking advantage of security protections being Weak cybersecurity impaired by users not applying best security All. practices by users practices (weak passwords, sensitive information written out on post-its, etc.).
These threats cover a whole spectrum of attacks that can be conducted against the user/control ground or space segments. Additionally, depending on the threat or the entry point in the asset that is targeted, the level of sophistication required for conducting the attack varies. It also depends on whether best practices of cyber protection have been applied. Some general trends can be identified. For example, it is easier to attack a ground asset connected to the internet than to get physical access to a spacecraft bus in space. Figure 4 depicts these coarse-grained relations.
Privilege escalation (i.e. undue granting of software execution rights) is a threat that also applies to on-board software such as a spacecraft real-time operating system.
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Figure 4: Sophistication level of an attack versus entry point As mentioned in the introduction of this chapter, risks relate to threats through vulnerabilities. There is also a link between the risk exposure and engineering practices, especially in relation to system reliability. For example, if the power supply of a ground system is not guaranteed by means of an Uninterruptible Power Supply (UPS), basic attacks to the power distribution network are likely to result in a denial of service. This is also true in the case of failure of the power grid, showing how reliability engineering and cybersecurity protection share common grounds. These aspects cover all phases of the space project: from design to operations and decommissioning. Finally, physical security was also not addressed here but has a direct relation to the mitigation of cybersecurity risks. For example, manufacturing facilities with poor physical security are exposed to threats from outsiders and insiders. Launchpads are exposed to sabotage if not physically secured. 4.4 NON-MALICIOUS THREATS The following figure describes non-malicious threats from the harshness of the space environment, system failures or human error. Such errors can be either operators’ mistakes or misconfiguration/bugs in the spacecraft/ground control software, especially for situations that do not happen often or software execution branches that are special or uncommon (e.g. during anomalies). Regardless of their unintentional nature, they yield similar risks as malicious threats. 27 LEO Satcom Cybersecurity Assessment
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Table 10: Threats of non-malicious origin
Non-malicious
Details Technology domains
threats
During high-energy periods of Sun cycles, on- On-board data subsystem, RF board electronics may get damaged or disrupted. subsystems, payloads and Satellite lifetime may decrease because the Earth technologies, electromagnetic atmosphere envelope ‘swells’ causing unwanted technologies and techniques,
Solar radiation
drag on the spacecraft (in some extreme cases, space system control, mission the spacecraft burns in the atmosphere). operation and ground data systems, ground station systems and networks.
Debris is the result of former activities in space (launches, collisions, or intentional destruction of satellites). Considering the travel speed of debris Space system control, flight
Collisions with
and orbiting objects, even the smallest object dynamics and GNSS, mission
debris and other
(e.g. a bolt) has enough kinetic energy to pierce operation and ground data
space bodies
through the wall of a satellite and cause damage. systems. Debris is tracked by several governmental agencies.
Unintentional collision between two spacecrafts can occur (and has occurred) either because one of the spacecrafts is not under control or simply as the result of a human mistake. In addition to Space system control, flight Collisions with the damage it causes, it creates additional debris. dynamics and GNSS, mission other satellites The European Space Surveillance and Tracking operation and ground data (EU-SST) cooperation implements a collision systems. warning service dedicated to operators of spacecrafts. Collision avoidance manoeuvres can then be conducted.
Manoeuvres are meant to maintain the spacecraft on its intended orbit. The associated Space system control, flight parameters (e.g. thruster activation) are Miscomputed dynamics and GNSS, mission computed on ground before being uploaded on manoeuvre operation and ground data board. A miscomputed manoeuvre (e.g. because systems. it is unusual) may for example cause a service outage because of payload antenna de-pointing.
The spacecraft is ‘driven’ through TCs and flight operation procedures (FOPs). The satellite user manual provides guidance regarding what sort of TCs is allowed based on the current operating On-board data subsystem, state of the satellite. Executing a flight operation space system software, RF Misconfiguration procedure that is not compatible with the satellite subsystems, payloads and of the platform state may trigger a Fault Detection, Isolation and technologies, space system Recovery (FDIR) mechanism that will control, mission operation and autonomously put the spacecraft in safe mode. ground data systems. This often corresponds to a temporary interruption of the current mission and therefore to a service outage.
Like the platform, the payload is configured On-board data subsystem, through TCs and flight operations procedures. space system software, RF Misconfiguration Payloads with on-board processing are complex subsystems, payloads and of the payload (as often found in LEO satcom systems), a technologies, space system misconfiguration can translate into service control, mission operation and outage. ground data systems.
Space systems rely a lot on wireless RF subsystems, payloads and transmissions (often RF). For that reason, technologies, electromagnetic Non-compliance international radio regulations enforce a fair technologies and techniques, with radio share and use of the RF spectrum among all mission operation and ground regulations users. Although signal jamming is an example of data systems, ground station malicious non-compliance, there are also cases systems and networks. of non-malevolent infringements, such as a
See https://www.eusst.eu/
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malfunctioning device or an incorrect understanding of the radio regulations.
Launch failures translate either to the destruction of the spacecraft or to a wrong injection into orbit. In the latter case, the outcome depends on how far the injection orbit is from the planned one. If Space system control, mission Launcher the difference is too significant, the spacecraft operation and ground data failures must be decommissioned, otherwise the systems. spacecraft uses its own propulsion subsystem to reach the intended orbit, at the expense of a reduced lifetime (due to reduced propellant available for conducting the mission).
Spacecrafts are also subject to unexpected failures. The spacecraft design is resilient to some failures using redundant units. In some cases, redundancy cannot help (so-called single Unspecified point failures without any redundancy), and the All. failures failure translates to degraded performance of the platform or the payload (e.g. parts of a solar panel may fail, impairing the overall power budget available to the payload) or a total loss of the spacecraft.
4.5 CYBER INCIDENTS ON LEO SATCOM SYSTEMS This section describes known cyber incidents that affected LEO satcom constellations. It should be noted that the list of incidents is not long. Because of the very nature of these incidents, not all of them were reported publicly. Providers of public electronic communications networks or of publicly available electronic communications services have the obligation to report cyber incidents to national or European authorities (see the Article 40 of the EECC ). ENISA runs the Cybersecurity Incident Reporting and Analysis System platform (CIRAS) , where competent authorities submit annual incident reports. This chapter ends with the description of an attack made on an experimental satellite operated by ESA. The attack – although real – was legitimate and conducted within the frame of research work. For that reason, it is extensively documented and constitutes a good reference for how (illegitimate) attacks could be conducted. Table 11lists cyber incidents disclosed publicly that target LEO satcom constellations. Regarding the term ‘incident’, some of these incidents cover actual attacks, while others are public disclosures of weaknesses or engineering details that may be exploited by a malicious third party.
As of October 2024, security requirements from ECCC will be replaced by security requirements from the NIS2 directive, which also include mandatory incident reporting. ENISA, ‘Incident reporting – CIRAS’, ENISA website, retrieved June 2023, https://ciras.enisa.europa.eu/.
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Table 11: Cyber incidents affecting LEO satcom systems, gathered from public sources
Affected Year Threat and risk Description system
2014 Iridium Software backdoor, privilege Terminal contains hardcoded and escalation undocumented credentials for accessing the terminal management interface.
No known attack, could be used to render terminal useless (service outage) or for illicit terminal usage (capacity hijacking).
2015 Globalstar Signal spoofing, information Reverse engineering of the uplink spoofing waveform to spoof the signal.
No known attack, demonstrated application for spoofing an asset tracking signal, obfuscating the ongoing asset theft (extraneous asset theft).
2015 Iridium Information eavesdropping Reverse engineering of the clear pager leading to data theft channel leading to the ability to eavesdrop on customer messages.
2022 Starlink Signal jamming leading to Repeated jamming of Starlink downlink service outage signals and GNSS signals used by the terminal during set-up.
2022 Starlink Subsystem denial of service Denial-of-service attack on an leading to service outage application programming interface (API) taking part in service delivery and leading to service outage.
2022 Starlink Privilege escalation Injection of hardware fault on the terminal printed circuit board to gain privileged access to the terminal software.
No known attack, could be used to render terminal useless (service outage) or for illicit terminal usage (capability hijacking).
2022 Gonets-M Privilege escalation, leading to Privilege escalation exploit on the subsystem denial of service ground CRM system, enabling the leading to service outage deletion of a key database used for service delivery.
Santamarta, R., ‘SATCOM terminals: Hacking by air, sea, and land’, Proceedings of the BlackHat US 2014 conference, retrieved June 2023, https://www.blackhat.com/docs/us-14/materials/us-14-Santamarta-SATCOM-Terminals-Hacking-By-Air-Sea-And- Land-WP.pdf. Moore, C., ‘Spread spectrum satcom hacking: Attacking the Globalstar simplex data service’, Proceedings of the Blackhat US 2015 conference, retrieved June 2023, https://www.blackhat.com/docs/us-15/materials/us-15-Moore-Spread-Spectrum-Satcom- Hacking-Attacking-The-GlobalStar-Simplex-Data-Service-wp.pdf. Sec and Schneider, ‘Iridium hacking – Please don’t sue us’, Proceedings of the 2015 Chaos Communication Camp, retrieved June 2023, https://www.youtube.com/watch?v=ahZOGhV8qnc. Laursen, L., ‘Satellite signal jamming reaches new lows’, IEEE Spectrum website, May 2023, retrieved June 2023, https://spectrum.ieee.org/satellite-jamming. Trustwave, SpiderLabs blog, ‘Killnet claims attacks against Starlink, Whitehouse.gov, and United Kingdom websites’, Trustwave website, November 2022, retrieved June 2023, https://www.trustwave.com/en-us/resources/blogs/spiderlabs-blog/killnetclaims-attacks-against-starlink-whitehousegov-and-united-kingdom-websites/. Wouters, L., ‘Glitched on Earth by humans: A black-box security evaluation of the SpaceX Starlink user terminal’, Proceedings of the Blackhat US 2022 conference, retrieved June 2023, https://i.blackhat.com/USA-22/Wednesday/US-22-Wouters-Glitched- On-Earth.pdf. Bussoletti, F., ‘Cyber warfare, Team OneFist hits Russia in space again’, Difesa & Sicurezza website, October 2022, retrieved June 2023, https://www.difesaesicurezza.com/en/defence-and-security/cyber-warfare-team-onefist-hits-russia-in-space-again/;
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2023 OPS-SAT Privilege escalation, leading to Demonstration from a research team of hijacking of capabilities taking control of the spacecraft by exploiting a bug in the data handler through the sending of specially craft TCs.
The war in Ukraine has caused a surge of attacks on satellite communication systems. Readers interested in space electronic warfare may refer to these sources .They cover topics such as: destruction of space assets by means of kinetic or non-kinetic weapons and use of spacecrafts to inspect or malevolently interact with other spacecrafts (RPO: rendezvous and proximity operations). Case study: an attack on the OPS-SAT experimental satellite This case study is based on the work from Willbold et al. on on-board software security. One of the case studies addresses the OPS-SAT experimental satellite. OPS-SAT is a satellite demonstrator based on a 3U-CubSat platform developed by Graz University of Technology under the auspices of ESA. It was launched in 2019 on low-earth orbit. It takes on board various payloads for Earth observation, RF and optical communications meant to host experiments. Its on-board software is open source and based on commercial off-theshelf products. In that respect, it is representative of the majority of CubeSats that are launched either by academic institutions or by New Space companies as part of their product development roadmap. As such, OPS-SAT does not match the scope of this report (i.e., LEO constellations offering communications services). However, its experimental and scientific purpose yields welldocumented studies that are illustrative and relevant to the topic of satellite cybersecurity. By combining experiments and study of the on-board software source code, Willbold et al. followed the steps listed below to take over control of the spacecraft. 1. Search for an entry point in the commanding subsystem of the spacecraft. It turned out that one of the TC channels was configured in clear mode, i.e. not implementing encryption and authentication. The other TC channels were protected. 2. Search for specific TCs that give access to critical functions, such as updating the onboard software or modifying the internal file structure. A weakness was found that combines two elements: (a) such critical TCs bear a special flag, however no extra protection is implemented; and (b) protected and unprotected TC channels ended in the same on-board computer, the latter not checking against the origin of the TC (e.g. protected, or unprotected TC channels). 3. Search for weaknesses in on-board functions that can be invoked from TC. Several weaknesses were found, one of them allowing arbitrary code execution. Such weaknesses are often linked to the lack of protection for memory write operations (e.g. buffer overflow attacks).
This entry is not a malicious attack. It is a demonstration from a team of academics. OPS-SAT is a single satellite, not a constellation. CSIS, Bingen, K. A., Johnson, K. and Young, M., Space Threat Assessment 2023, Center for Strategic and International Studies, Washington DC, 2023; European Space Policy Institute, ESPI Short Report 1 – The war in Ukraine from a space cybersecurity perspective, European Space Policy Institute, Vienna, 2022; Grossman, T., Kaminska, M., Shires, J. et al., Workshop report: the Cyber Dimensions of the Russia-Ukraine War, European Cyber Conflict Research Initiative, 2023; Secure World Foundation, Global counterspace capabilities – An Open Source Assessment, Secure World Foundation, 2023. Willbold, J., Schloegel, M., Vögel, M. et al., ‘Space odyssey: An experimental software security analysis of satellites’, Proceedings of the 44th IEEE Symposium on Security and Privacy, May 2023.
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4. Craft special TC packets that exploit the weaknesses exposed in the previous points and allow the execution of a piece of code that takes control of the spacecraft. Having a clear TC channel may seem non-representative of real (i.e. commercial) spacecrafts. Surprisingly, it is still common practice for some satellite manufacturers to enable TC channel encryption and authentication only at the end of launch and early orbit phase (LEOP) operations. For geostationary satellites with electrical propulsion, these operations may last for up to 6 months. One may also object that having open-source software is a major weakness. It triggers the traditional debate about the effectiveness of ‘security through obscurity’, where not publishing the software sources is thought to increase the product’s inherent security. Considering that satellite manufacturing (a) relies on a network of suppliers and sub-contractors and (b) tends to increase the use of off-the-shelf (i.e. not space specific) components, it can be stated that the so-called ‘obscurity’ is not guaranteed. A safe approach is therefore to not rely on ‘security through obscurity’ and to implement all required safeguards and best practices. This is the subject of the next chapter. 32 LEO Satcom Cybersecurity Assessment
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5. STANDARDS AND RECOMMENDATIONS FOR SATCOM CYBERSECURITY
This chapter discusses published standards and existing recommendations for securing satellite systems. Some of these initiatives deal with threat landscape, while others describe best practices for securing a satellite link by means of cryptography. In order to illustrate these different scopes, this report adopts a conceptual view of ‘cybersecurity engineering’ loosely inspired by the well-known ‘V-model’ development life cycle, augmented with operations (Figure 5). The left part of the V shape depicts the requirements–specification–design trilogy while the right part addresses all the equivalent verification and validation activities. Standards and recommendations identified in the following sections of the chapter are positioned on the figure with respect to their scope. The chapter ends with an outlook on forthcoming initiatives. 33 LEO Satcom Cybersecurity Assessment
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Figure 5: Framework for cybersecurity development and operations 5.1 EUROPEAN COOPERATION FOR SPACE STANDARDIZATION ECCS standards and handbooks, when applied to commercial satcom systems, mostly refer to project management, manufacturing, testing, launch activities and communications for the control segment. The ECSS documents do not address cybersecurity in a dedicated standard or recommendation, however the topic is mentioned in several documents (see Table 13). Furthermore, for communications engineering, ECSS relies on the suite of Consultative Committee for Space Data Systems (CCSDS) standards (see the CCSDS section later in this chapter), sometimes further detailing adaptations of a CCSDS standard through an Adoption Notice. See for example ECSS-E-AS-50-25 covering the adoption of the CCSDS TC Space Data Link Protocol, including the use of SDLS (Space Data Link Security) for providing confidentiality, authentication, and integrity. 34 LEO Satcom Cybersecurity Assessment
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Table 13: ECCS documents covering security aspects
Positioning on system Document Document Asset and risk addressed development and operations type framework
ECSS-E-ST-10 Standard All assets, no specific impact Development (testing is cited in ‘System addressed. the document).
engineering general requirements’
ECSS-E-ST-40 Standard All assets, no specific impact Development (requirement, ‘Software’ addressed. specifications, testing).
Operations (from security monitoring to security requirements update).
Documentation.
ECSS-E-ST-50 Standard Assets: control and user Development (requirement, ‘Communications’ segments (links). design).
Risk: capability hijacking and data theft (loss of link confidentiality, integrity and authentication).
ECSS-E-AS-50-25 Adoption Asset: control segment Development (design). ‘Adoption Notice of notice (links).
CCSDS 232.0-B-4,
Risk: capability hijacking and
TC Space Data Link
41 data theft (loss of link
Protocol’
confidentiality, integrity and authentication).
5.2 CONSULTATIVE COMMITTEE FOR SPACE DATA SYSTEMS The CCSDS is an international forum publishing various documents, including recommended standards (‘blue books’), recommended practices (‘magenta books’) and informational reports (‘green books’). Books are identified by a series number, a volume number, a letter code depending on the colour of the book and a version number. Books in the 350, 351, 352, 355, 356 and 357 series cover various aspects of space system security: from threat assessment through security architecture to management of keys for securing data links (Table 14). CCSDS standards have been implemented on hundreds of missions ranging from space probes to experimental CubeSats. Because of this, there are several commercial off-the-shelf products supporting the CCSDS protocols, for both the space segment and the ground segment. While most commercial satcom system use CCSDS protocols for the command-and-control part of the spacecraft, the user segment often relies on proprietary solutions, and is therefore outside of the scope of standardisation.
ECSS, ‘ECSS-E-ST-10C Rev.1 – System engineering general requirements (15 February 2017)’, 2017. ECSS, ‘ECSS-E-ST-40C – Software (6 March 2009)’, 2009. ECSS, ‘ECSS-E-ST-50C Rev.1 – Communications (1 March 2021)’, 2021. ECSS, ‘ECSS-E-AS-50-25C Rev.1 – Adoption Notice of CCSDS 232.0-B-4, TC Space Data Link Protocol (13 January 2023)’, January 2023.
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Table 14: CCSDS documents related to security
Positioning on system Document Asset and threat Document development & operations type addressed framework
CCSDS 350.0-G-3 Informational Assets: control and user Development (design). ‘The application of report segment (communication security to CCSDS links).
protocols’
Risk: capability hijacking, information forgery and data theft (loss of link confidentiality, integrity, and authentication).
CCSDS 350.1-G-3 Informational All assets. Development (threat analysis). ‘Security threats report All risks, mostly coming
against space
43 from threats with malicious
missions’
origin.
CCSDS 350.4-G-2 Informational Assets: control and user Development (requirements, ‘CCSDS guide for report ground segments (IT specifications, design and secure system network interconnections). testing).
interconnection’
All risks. Operations (all phases).
CCSDS 350.5-G-1 Informational Assets: control and user Development (design). ‘Space data link report segment (communication security protocol– links).
summary of concept
45 Risk: capability hijacking,
and rationale’
information forgery and data theft (loss of link confidentiality, integrity, and authentication).
CCSDS 350.6-G-1 Informational Assets: all segments. Development (requirements, ‘Space missions key report specifications, design). Risks: all risks protected
management
46 by crypto systems (data
concept’
theft, capability hijacking and information forgery).
CCSDS 350.7-G-2 Informational Assets: all segments. Development (requirements, ‘Security guide for report threat analysis). 47 Risks: all risks.
mission planners’
CCSDS 350.8-M-2 Recommended Not applicable. Not applicable. ‘Information security practice
glossary of terms’
CCSDS 350.9-G-1 Informational Assets: all segments. Development (design). ‘CCSDS report Risks: all risks protected
cryptographic
49 by crypto systems (data
algorithms’
theft, capability hijacking and information forgery).
CCSDS 351.0-M-1 Recommended Assets: all segments Development (design). ‘Security practice (communication links).
architecture for
CCSDS, ‘The application of security to CCSDS protocols’, Informational Report, No 3, CCSDS 350.0-G-3, 2019. CCSDS, ‘Security threats against space missions’, Informational Report, No 3, CCSDS 350.1-G-3, 2022. CCSDS, ‘CCSDS guide for secure system interconnection’, Informational Report, No 2, CCSDS 350.4-G-2, 2019. CCSDS, ‘Space data link security protocol–Summary of concept and rationale’, Informational Report, No 1, CCSDS 350.5-G-1, 2018. CCSDS, ‘Space missions key management concept’, Informational Report, No 1, CCSDS 350.6-G-1, 2011. CCSDS, ‘Security guide for mission planners’, Informational Report, No 2, CCSDS 350.7-G-2, 2019. CCSDS, ‘Information security glossary of terms’, Recommended Practice, No 2, CCSDS 350.8-M-2, 2020. CCSDS, ‘CCSDS cryptographic algorithms’, Recommended Standard, No 1, CCSDS 350.9-G-1, 2014. Companion document of CCSDS 352.0-B-2.
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space data Risk: capability hijacking, systems’ information forgery and data theft (loss of link confidentiality, integrity, and authentication).
CCSDS 352.0-B-2 Recommended Assets: all segments. Development (design). ‘CCSDS standard Risks: all risks protected
cryptographic
52 by crypto systems (data
algorithms’
theft, capability hijacking and information forgery).
CCSDS 355.0-B-2 Recommended Assets: control and user Development (design). ‘Space data link standard segment (links).
security protocol’
Risk: capability hijacking, information forgery and data theft (loss of link confidentiality, integrity, and authentication).
CCSDS 355.1-B-1 Recommended Assets: control and user Development (design). ‘Space data link standard segment (links).
security protocol–
Risk: capability hijacking,
Extended
54 information forgery and
procedures’
data theft (loss of link confidentiality, integrity, and authentication).
CCSDS 356.0-B-1 Recommended Assets: control and user Development (design). ‘Network layer standard segment (links).
security adaptation
55 Risk: capability hijacking,
profile’
information forgery and data theft (loss of link confidentiality, integrity, and authentication).
CCSDS 357.0-B-1 Recommended Assets: all segments. Development (design). ‘CCSDS standard Risks: capability hijacking,
authentication
56 information forgery and
credentials’
data theft (breach of authentication).
5.3 EUROPEAN TELECOMMUNICATION STANDARDs INSTITUTE The European Telecommunication Standards Institute (ETSI) hosts a technical committee, called Satellite Earth Station, addressing standardisation for space communication systems. ETSI Satellite Earth Station has issued a set of standards for satellite phones (phone handhelds communicating by means of satellites) under the common denomination of GEO-mobile radio interface (GMR). The GMR standards (they are called GMR-1 and GMR-2, but are different standards addressing different systems) are used by some geostationary system operators and include provision for encryption at the air interface (i.e. the transmission scheme that is used between the user terminal and the satellite). However, the standards do not specify what encryption algorithm or what authentication scheme to use, leaving it up to vendors. By applying reverse engineering on the firmware of two satellite phones, in 2012 researchers were able to
CCSDS, ‘Security architecture for space data systems’, Recommended Practice, No 1, CCSDS 351.0-M-1, 2012. CCSDS, ‘CCSDS cryptographic algorithms’, Recommended Standard, No 2, CCSDS 352.0-B-2, 2019. CCSDS, ‘Space data link security protocol’, Recommended Standard, No 2, CCSDS 355.0-B-2, 2022. CCSDS, ‘Space data link security protocol–Extended procedures’, Recommended Standard, No 1, CCSDS 355.1-B-1, 2020. CCSDS, ‘Network layer security adaptation profile’, Recommended Standard, No 1, CCSDS 356.0-B-1, 2018. CCSDS, ‘CCSDS authentication credentials’, Recommended Standard, No 1, CCSDS 357.0-B-1, 2019.
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reveal weaknesses in the implemented encryption algorithms , potentially compromising the confidentiality of voice calls. Table 15: ETSI GMR-1 and GMR-2 documents related to the security of user data traffic
Positioning on system Document Document Asset and threat addressed development and type operations framework
GMR-1 (ETSI TS 101 Standard Asset: user segment (links). Development 376-3-9 V1.1.1) (requirement). Risks: capability hijacking,
‘GEO-Mobile Radio
information forgery and data theft.
Interface Specifications; Part 3: Network specifications; Subpart 9: Security related Network Functions; GMR-1 03.020’
GMR-2 (ETSI TS 101 Standard Asset: user segment (links). Development 377-2-3 V1.1.1) (implementation). Risks: capability hijacking,
‘GEO-Mobile Radio
information forgery and data theft.
Interface
Specifications; Part 2:
Service specifications; Subpart 3: Security Aspects; GMR-2 02.009’
ETSI also hosts standardisation activities related to the digital video broadcasting (DVB) project. DVB standards (such as DVB/S2) are popular transmission schemes used in commercial satcom systems. Despite the name, DVB standards are also applicable to data-based satcom systems. However, these standards do not specify security mechanisms (e.g. encryption schemes). They are left to the higher layers of the communication stack (e.g. at IP or application level). 5.4 NATIONAL INSTITUTE OF STANDARDS AND TECHNOLOGY The National Institute of Standards and Technology (NIST) is a US agency, originally founded to provide accurate time reference. Nowadays, NIST is involved in standard publications and is the home of the Cybersecurity Framework : ‘a methodology to protect individual privacy and civil liberties when critical infrastructure organizations conduct cybersecurity activities’. Using this framework as a baseline, NIST has developed a few cybersecurity guidelines for satellite systems.
Driessen, B., Hund, R., Willems, C. et al., ‘Don’t trust satellite phones: A security analysis of two satphone standards’, 2012 IEEE Symposium on Security and Privacy, 2012, pp. 128–142. ETSI, ‘ETSI TS 101 376-3-9 V1.1.1 – GMR-1 GEO-Mobile Radio Interface Specifications; Part 3: Network specifications; Sub-part 9: Security related Network Functions; GMR-1 03.020’, 2001. ETSI, ‘ETSI TS 101 377-2-3 V1.1.1 – GMR-2 GEO-Mobile Radio Interface Specifications; Part 2: Service specifications; Sub-part 3: Security Aspects; GMR-2 02.009’, 2001. NIST, Barrett, M. P., Framework for Improving Critical Infrastructure Cybersecurity, 2018.
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Table 16: NIST reports addressing security in satellites
Positioning on system Asset and threat Document Document type development and addressed operations framework
NIST IR 8401 NIST Asset: ground segment. Development (from Satellite Ground Interagency requirements to Risks: all risks. Segment Applying report specifications) and the Cybersecurity operations covered by five Framework, to ‘functions’: identify (assets, Satellite Command threats), protect, detect and Control (attacks), respond, and recover.
NIST IR 8270 Draft of NIST Asset: space segment. Development (from Introduction to Interagency requirements to Risks: all risks. Cybersecurity for report specifications) and Commercial operations covered by five Satellite Operations ‘functions’: identify (assets, (2nd Draft threats), protect, detect (attacks), respond, and recover.
NIST IR 8441 Draft of NIST Assets: all segments. Development (from Cybersecurity interagency requirements to Risks: all risks. Framework Profile report specifications) and for Hybrid Satellite NB: hybrid satellite operations covered by five Networks (HSN) – networks cover spacecraft ‘functions’: identify (assets, Initial public draft that hosts different threats), protect, detect payload for different (attacks), respond, and missions and virtualised recover.
(e.g. cloud-based) ground
segments.
5.5 EUROPEAN SPACE AGENCY AND AEROSPACE CORPORATION THREAT FRAMEWORKS Threat and attack frameworks have already been referenced in Chapter 4 when listing risks and threats. They are recapped in Table 17 and are both derived from the MITRE ATT&CK framework with elements focusing specifically on space systems. Table 17: Threat and attack frameworks for space systems
Framework Comments
Aerospace Applicable to all space segments. Covers attacks and countermeasures. Has corporation a similar structure to ESA SPACE-SHIELD. Attacks are categorised according 65 to techniques (e.g. reconnaissance, initial access, defence evasion).and the
SPARTA
framework also covers risks such as data manipulation, jamming and loss of spacecraft commanding. Initially released in 2022.
ESA SPACE- Applicable to all space segments. Covers attacks and countermeasures. Has SHIELD strong links with the work of the Aerospace corporation with SPARTA. Initially released in 2023.
NIST, ‘Satellite ground segment – Applying the cybersecurity framework to satellite command and control’, NIST Interagency Report, NIST IR 8401, 2022. NIST, ‘Introduction to cybersecurity for commercial satellite operations, NIST Interagency Report Draft (2nd), NIST IR 8270, 2022. NIST, ‘Cybersecurity framework profile for hybrid satellite networks (HSN)’, NIST IR 8441 (initial public draft), 2023. MITRE, ‘MITRE ATT&CK’, MITRE website, retrieved May 2023, https://attack.mitre.org/. The Aerospace Corporation, ‘SPARTA: Space attack research and tactic analysis’, Aerospace website, retrieved May 2023, https://aerospace.org/sparta. ESA, ‘SPACE-SHIELD’, ESA website, retrieved May 2023, https://spaceshield.esa.int/.
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The primary use of these frameworks is to make a systematic inventory of possible threats and attacks during a threat analysis (as shown in Figure 5). However, thanks to the rich underlying information model of these frameworks, they reveal their full power when navigating downstream (from threats to mitigation techniques), upstream or sideways (e.g. among threats sharing a common mitigation). They are fully applicable to commercial satcom systems. 5.6 OTHER INITIATIES The German Federal Office for Information Security (Bundesamt für Sicherheit in der Informationstechnik (BSI)) has published two documents that address cybersecurity in satellite systems. Table 18: BSI guidelines on satellite security
Document Comments
IT-Grundschutz Profile for The IT-Grundschutz is a methodology for information security Space Infrastructures – management systems. It is compatible with ISO/IEC 27001. This Minimum Protection for document aims at easing the listing of security requirements Satellites Covering their Entire during all phases of satellite design, manufacturing and Life Cycle operations (including decommissioning).
Technical Guideline BSI TR- This document is focused on the space segment. It provides a 03184 Information Security for mapping between business processes (e.g. manufacturing, Space Systems, Part 1: Space launch), applications (e.g. software and hardware tools, transport 68 containers), threats and security measures.
segment
5.7 OUTLOOK ON FORTHCOMING INITIATIVES EU Space Strategy for Security and Defence In March 2023, the European Commission published the EU Space Strategy for Security and Defence. The topic of resilience and protection of EU space systems and services is addressed notably through the intention to ‘set up an Information Sharing and Analysis Centre (ISAC) to raise awareness and facilitate exchange of best practices among commercial and relevant public entities on resilience measures for space capabilities’ . The implementation of an EU Space ISAC will be backed by the ‘ISAC in Box’ initiative developed by ENISA, aiming to provide ‘as a kit’ all tools, documents and processes needed to set up an ISAC . US-based Space ISAC, founded in 2019 to establish a forum ‘to enhance our ability to prepare for and respond to vulnerabilities, incidents, and threats; to disseminate timely and actionable information among member entities’ , is also used as an example for the creation of the EU Space ISAC. The strategy also states that the Commission will consider proposing the creation of an EU Space Law. The EU recognises space as a critical sector in its existing legislation on cybersecurity (NIS2 directive), covering ground-based infrastructure of Member States, including in the EU outermost regions, and of private operators as well as satellites used for delivering telecommunication services. The implementation of the NIS2 directive and the
BSI, IT-Grundschutz Profile for Space Infrastructures – Minimum protection for satellites covering their entire life cycle, 2022. BSI, Technical Guideline BSI TR-03184 Information Security for Space Systems – Part 1: Space segment, 2023. European Commission, ‘EU space strategy for security and defence ‘, European Commission website, retrieved September 2023, https://defence-industry-space.ec.europa.eu/eu-space-policy/eu-space-strategy-security-and-defence_en. ENISA, ‘ISAC in a box’, ENISA website, retrieved September 2023, https://www.enisa.europa.eu/topics/national-cyber-securitystrategies/information-sharing/isacs-toolkit/view. Space ISAC, retrieved September 2023, https://s-isac.org/.
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upcoming Cyber Resilience Act, as well as other existing cybersecurity frameworks, will incentivise the uptake of cybersecurity requirements for critical digital products that are used in space. Specific cybersecurity standards and procedures in the space domain could be considered as part of the EU Space Law where relevant. A call for space security standardisation In 2022, a group of space professionals (academics and members of the industry) took the opportunity of the American Institute of Aeronautics and Astronautics Ascend conference to publish a call to action for the standardisation of cybersecurity practices for commercial space systems (‘An International Technical Standard for Commercial Space System Cybersecurity – A Call to Action’ ). The authors anticipate a move to mass production, driven by a growing demand for space missions, not always from companies that are well established or well acquainted with the space environment. For that reason, the scope of the foreseen technical standard targets modular and commercial off-the-shelf space systems (whatever the segment), including the supply chain. In February 2023, the Institute of Electrical and Electronics Engineers’ (IEEE) Space System Cybersecurity Working Group was created with the following project scope: ‘This standard defines cybersecurity controls for space systems including subcommittees for the space/ground/user/link segments and the integration layer.’
Falco, G., Henry, W., Aliberti, M. et al., ‘An international technical standard for commercial space system cybersecurity – A call to action’, American Institute of Aeronautics and Astronautics Ascend conference, 24–26 October 2022, 2022. IEEE, ‘P3349 – Standard for space system cybersecurity’, IEEE website, retrieved September 2023, https://standards.ieee.org/ieee/3349/11182/.
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6. CYBERSECURITY STRENGTHS AND WEAKNESSES OF SATCOM IN COMPARISON TO TERRESTRIAL NETWORKS
This chapter elaborates on the commonalities and differences between LEO satcom and terrestrial networks as far as cybersecurity is concerned. It is important to state that – as mentioned later – the comparison is based on a high level of comparable architecture threat and impact analysis and does not consider the actual cyber protection put in place in concrete implementation scenarios. Therefore, this chapter should not be considered as a definitive assessment as to whether one or the other sector is more or less secure. Before focusing further on cyber aspects, Table 19 describes key differences between space systems and terrestrial systems. Table 19: Key characteristics of LEO satcom systems compared to terrestrial systems
Key characteristics Description
A single satellite at an altitude of 500 km sweeps an area of 2 372 000 km (assuming it is visible at least 25 degrees above the horizon). In similar conditions, a telecommunication device placed at an Large service coverage altitude of 100 m ‘sees’ 4 000 km . This has two consequences: (a) terrestrial communication systems require denser infrastructures; and (b) terrestrial communication systems are more dependent on the geopolitical context.
Because of the large service coverage and the use of RF transmission, the broadcasting of information is easily affordable. While LEO satcom systems are not the best choice for multimedia broadcasting, other use Direct information broadcasting cases exist, such as distribution of network management information. In terrestrial networks, such information broadcasting either requires complex routing strategies or is inefficient from a resource usage standpoint.
LEO satcom systems can provide the service throughput they were designed for on every part of the service area at any time. A single High throughput transmission satellite has a capacity of at least several Gbit/s, often several tens of Gbit/s that directly connect the service area to the corresponding Earth station. This combination of ubiquity and very high throughput is unique.
Satcom systems display a high level of resilience for three reasons: spacecrafts are less exposed to terrestrial incidents or catastrophes; they High system resilience are designed to survive failures (see the next paragraphs); and the ground infrastructure is less complex and less distributed. This helps reliability engineering.
These key characteristics are essential in order to tackle the challenges of launching and operating assets in space. These challenges are listed in Table 20. 42 LEO Satcom Cybersecurity Assessment
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Table 20: Challenges that satcom systems face
Challenge Description
Satellites rely on launching capabilities to put spacecrafts in orbit. Currently, the most visible New Space developments are related to launcher technology, showcasing a decrease in price per mass to launch, Launching capabilities reusability of launcher elements, new propulsion systems and new structure material. The Russian war of aggression against Ukraine and the associated ban on some launch services providers has also raised the case of access to space sovereignty.
Once launched, servicing a spacecraft is (currently) not possible. This has a lot of implications: space-proven technology is usually more costly than the terrestrial equivalent or the performance/price ratio is less No servicing possible favourable. Designs often make use of redundant components, impairing the weight and power consumption. Finally, assembly, integration and testing activities are costly to ensure the required quality. Taking these into account, cost-effective mass production is a challenge.
Vacuum, cosmic radiations, 300+ °Celsius thermal variations, vibrations during launch and limited power supply make the space environment
Harsh space environment
hard to reach and harsh to stay in. Spacecraft must be designed accordingly.
Systems using RF rely on the right to transmit on given frequency bands, also known as ‘spectrum’. There is a direct link between the throughput that can be achieved and the available spectrum (in hertz). Access to the spectrum is subject to international regulations because if two co-located systems use the same spectrum, they can interfere mutually, impairing the throughput achievable during transmission. Considering that usable
Dependency on RF spectrum
spectrum is a finite resource and that LEO satcom systems are global,
resources
spectrum management is complex.
For that reason, there is currently a growing interest in the use of optical transmission for ground-to-space links as well as ISLs. While optical technology is sensitive to weather conditions, it may alleviate some of the limitations of RF transmission.
Because of the distance between Earth and the spacecraft and the Line of sight transmissions transmission/received power involved, satellite communications require line of sight. As a corollary, the antenna must be located outside.
To support the comparison between LEO satcom constellations and terrestrial networks from a cybersecurity standpoint, it is helpful to select an example of terrestrial network technology, which uses comparable systems for similar functionality. Broadband cellular networks (e.g. 4G) are chosen for this purpose because both type of networks offer large-coverage commercial communications services and they are used for transferring voice, data and multimedia content. They also rely on a mix of wired and wireless communication techniques to deliver their services. In this context, Figure 6 illustrates how the architecture of LEO satcom and cellular networks compare at a high level. Solid lines correspond to wired communications (fibre, copper, etc.) while dotted lines are wireless. This distinction makes sense since, as detailed later, wireless communications are more prone to cyberattacks.
The New Space can be defined as recent (in the past 10 years) developments combining a surge of private funding, the development of new businesses and innovation. An oversimplifying summary would be ‘privatisation of space activities’.
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Figure 6: Components making the architectures of LEO and cellular networks Table 21 details the correspondence between components of the LEO and cellular network architectures. The mapping is based on the coarse-grain functions of each component. Table 21: Mapping of LEO and cellular networks components based on their function
LEO satcom system Cellular networks Coarse-grain function
Provisioning of the service to Satellite terminal Mobile terminal (e.g. cell phone) the user
Cell tower (e.g. eNodeB in the 4G Relay between the terminal Satellite architecture) and operator’s network
User traffic manager (e.g. the Evolved Management of the user Satellite Gateway traffic within the operator’s Packet Core in the 4G architecture) network and interconnection
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with the internet or other backbones
Monitoring and control of the SCC and TT&C stations Network management system network components
The cybersecurity comparison will be built on the concepts of threat and impact. Note that this chapter is not meant to provide an extensive comparison. Rather, the objective is to identify general strengths and weaknesses applicable to LEO satcom systems, keeping in mind the generalisation towards terrestrial systems. For this reason, the following considerations apply when referring to threats and impacts. • The exposure to threats: is a LEO satcom system more exposed to threats than a cellular broadband network? • The severity of the impacts: if a threat turns into a successful attack, is a LEO satcom system likely to be more severely impacted than a cellular broadband network? These elements are covered in Table 22 and Table 23. Table 22: Comparison of the exposure to threats for components of LEO satcom systems vs cellular broadband networks
Component Exposure to threats
Both a satellite terminal and a mobile phone are exposed to threats coming from their carrier network (satellite or cellular) or the terrestrial connectivity they are using/offering (e.g. Wi-Fi, Bluetooth or wired LAN).
However, compared to a satellite terminal, a mobile phone also hosts thirdparty applications and offers email and web browsing directly from the phone. For that reason, the surface of exposure to threats is larger. Another consideration is the fierce competition in the phone consumer market leading to frequent product lines renewal. This often impairs the availability of security updates (firmware, operating systems or even the applications) for the older versions of mobile phones. Satellite terminal vs mobile phone Finally, because of their carry-everywhere nature, phones are much more exposed to risks deriving from crowded places (airports, hotels, train stations), such as physical theft, data theft and capability hijacking. At a more basic level, smartphone users may not follow basic cybersecurity hygiene practices.
Satellite terminals, on the other hand, only serve as communication bridges between a local network and the satellite network. End users have few – if any – interactions with terminals apart from the physical connection of cables. The exposed surface is therefore smaller. Software updates for satellite terminals are often pushed ‘over the air’ from the system operator’s facilities.
A satellite, because of its location in space, is less exposed to ‘cheap’ attacks (such a destruction through brute force). On the other hand, its design is more complex, increasing the threat surface for attackers that can afford access to satcom transmission technology. Satellite vs cell tower Unlike a cell tower, LEO satellites are exposed to a fixed ground attacker for a limited amount of time, during the pass. Attacks requiring longer times (i.e. more than 10 minutes) are therefore less straightforward to conduct or require coordination among multiple attackers.
Both entities serve the same role: connecting the terminals to backbone networks such as internet (see Figure 6) indirectly through the satellite or the cell tower. For that reason, the surface of exposure is almost similar. Satellite gateway vs user traffic manager There is a disadvantage to the satellite gateway. Satellite links are wireless, so all threats based on signal jamming/spoofing or eavesdropping apply. User traffic managers, on the other hand, are connected to cell towers by means of wired technology.
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Both entities implement monitoring and control of the system. They are therefore exposed to similar threats, especially those targeting software systems, networks and human operators, all of these being core elements of such systems. It should be noted that, in both cases, the software update policy should be considered as early as during the system design. The SCC and TT&C vs objective is to balance the difficulty of software maintenance on missionnetwork management critical systems and the need to have up-to-date software. system
In addition, because monitoring and controlling the satellite is done through TM/TC wireless links, it opens the door to additional signal threats (jamming, spoofing, eavesdropping), like the ones of the satellite gateway.
Table 23: Comparison of the impact severity for components of LEO satcom systems vs cellular broadband networks
Component Severity of the impacts
In the case of a successful attack on a satellite terminal, the impact is likely to be more severe than for a mobile phone for two reasons:
Satellite terminal vs • satellite communications are often used for critical missions mobile phone requiring a high availability figure;
• satellite terminals are deployed in remote areas, possibly making servicing or replacement more complicated.
If a satellite is compromised (vs a cell tower), the impact will be much higher. The two major reasons are:
Satellite vs cell tower • the value of the asset (millions of euros);
• the inherent difficulty of diagnosing and fixing a satellite located thousands of kilometres away.
As with the prior element, the disadvantage is on the space system side. Having a failed gateway decreases – at least temporarily – the overall system capacity. There are several reasons for this.
• The redundancy factor (how many spares for a working unit) of gateways is less than the cellular broadband networks, mostly for cost reasons. Less redundancy means less resilience to outages. Satellite gateway vs user traffic manager • Recovery operations on the space system are more complex and possibly not automated. They may require reconfiguration of the satellites’ payload and processing strategy.
On the other hand, satcom systems that feature ISLs can rely on the ISL to divert the traffic from the failed gateway to another one. While this improves failure resiliency, it also increases the load on the ISLs, possibly at the expense of low-priority users.
Both components for space and terrestrial networks are based on software, IT and communication networks. They also share commonalities in terms of location, implementation, and resilience strategies.
An SCC also relies on TT&C stations for transmitting commands and SCC and TT&C vs receiving telemetry to/from the satellites. It raises the question of what the network management impact of losing a TT&C station is. Contrary to gateway antennae, bringing system down a TT&C station has less impact on the overall command and control capabilities. Other TT&C stations can take over without compromising the global command and control capabilities.
For this reason, there is no significant difference in terms of impact on the SCC and the network management system.
Summarising these two tables, one can say the following. 46 LEO Satcom Cybersecurity Assessment
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• Since LEO satcom systems rely heavily on wireless links (terminal to spacecraft, spacecraft to gateway and uplink and downlink of command and control), their threat exposure is generally higher than that of cellular broadcast networks. Regarding the terminal, mobile phones also run third-party applications, e.g. web browsing or email services; therefore, their surface exposure to attacks is expected to be higher. • The impact of a successful attack on a LEO satcom system is more severe than what can be observed on a cellular broadcast network. This statement relies on two facts: first, the price of a satcom assets is higher; second, spacecrafts or remote terminals, because of their isolated location, are more difficult to diagnose or fix. Note that the presented analysis does not infer the actual security of a specific real-world system, space or terrestrial. The actual security of each system depends on a wide range of aspects, including but not limited to the risk factors and implemented cyber protection measures. Therefore, this report is not making a judgment as to whether one type of system is more secure than another, but only points out where possible larger security issues exist in satcom in comparison to terrestrial networks. 47 LEO Satcom Cybersecurity Assessment
February 2024
7. CONCLUSIONS
This report addresses the topic of cybersecurity for constellations of LEO satellites delivering publicly available electronic communications services. To some extent, it also covers space communications systems in general. The in-depth and extensive study of cyber protection for space systems is a recent concern despite decades of computer crime and countermeasures having been observed on terrestrial systems. One of the reasons for this is the assumption that space is less exposed to cybersecurity threats because it is demanding to reach (both technically and financially) and usually reserved to governments and specialised companies. Several trends prove that this assumption is wrong, the following among them. • Access to space is now easier and cheaper than before, with the strong development of new and more affordable launch services. • The strong development of the New Space transforms space into a business market for private companies (including startups) delivering new and innovative services. • Commercial off-the-shelf components are now favoured – when possible – over custom or specifically developed components for space. Retro-engineering and indepth technical analysis is then easier to conduct. • The development of some large space systems calls for extensive supply chains: the wider the supply chain, the more difficult it is to secure. • Industrial engineering and operations must be optimised to sustain the pressure of competition: time and cost to market work against long engineering cycles (including extensive testing). • Cybercriminals now have easy access to advanced technology (e.g. software defined radio) and information: this increases the number of potential threat actors and attack vectors. • Rendezvous and proximity operations (RPO) ( ) are now a reality, compromising the simple belief that space is a safe place. The need for a coordinated approach in space systems security is clear and calls for standards, recommendations, information sharing and training. • When devising space systems, security requirements must be integrated into the early phase of the project and be subject to the same processing as other requirements, assessing the cost vs benefit of cyber protection. It calls for a comprehensive risk analysis also covering the potential impact on other, neighbouring systems. • From an industrialisation perspective, the former point would benefit from the organisation of integrated (manufacturer and customer) teams to handle the topic of cybersecurity. Because devising cybersecurity is a matter of trade-off and lacks a truly integrated approach, this will lead to over-specification of the cybersecurity features, severely impairing the cost-effectiveness and operability of the system. The actual implementation of such integrated teams could be the subject of standard and recommended practices.
A spacecraft approaches another spacecraft for inspection or more aggressive behaviour.
48 LEO Satcom Cybersecurity Assessment
February 2024