Space Data Centers Database
Search and compare space data center projects and related orbital computing demonstrations, including developers, technical specifications, suppliers, agreements and milestones. Follow each commitment to its original announcement.
Catalog: 95 projects. 13 proposal / study · 33 development · 13 launched · 20 demonstrated · 4 operating · 9 historical · 3 uncertain. These are project classifications, not spacecraft counts or verified commercial capacity.
37 projects classified as launched, demonstrated or operating: 29 reviewed, 8 with review limits or awaiting review. Each project appears in one classification.
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1–25 of 95 projects shown
| Project / developer | Intended use | Development status | Configuration / scope | Representative compute capability / hardware | IT electrical power | Linked coverage |
|---|---|---|---|---|---|---|
Project Suncatcher →Google / Planet · United StatesLatest development 30 Oct 2026 ↗Manual review 30 Oct 2026Stage detail: Operator-reported onboard AI inference Compared Google October30 response report with the recorded prototype. Onboard Gemma4 inference and Svalbard response downlink are reported demonstrations. Thermal/radiation reliability and the separate 2027 interconnect test remain future work. Last full profile review: 20 Oct 2026. Sources collected: 20 Oct 2026. Source collection and substantive profile review are separate checks. | TPU hardware and optical interconnect validation | Demonstrated Operator-reported onboard AI inference Next project milestoneContinue in-orbit TPU thermal-stress and radiation tests, followed by the separate twin-satellite interconnect experiment planned for 2027. | 2 satellitesInterconnect experimentReported specificationPlanned specification · 2027 Evidence & qualificationsSeparate from the initial Transporter-18 TPU hardware-survival test. Planned specification · 2027 Source / observation date: . Supporting source ↗1 more configurations / specifications1 prototype satellite2026 TPU survival-test prototypeReported specificationofficial operator launch account Evidence & qualificationsOne prototype launched October 1, 2026. Google's October30 report establishes an operator-reported onboard Gemma4 workload response, not a commercial fleet or measured throughput. official operator launch account Source / observation date: . Supporting source ↗ | Google Trillium TPUs2026 TPU survival-test prototypeReported specificationofficial prelaunch hardware account Evidence & qualificationsGoogle identifies Trillium TPUs in the prototype test context. The official pages do not disclose chip count, installed throughput or numerical precision. official prelaunch hardware account Source / observation date: . Supporting source ↗1 more configurations / specificationsTPU test prototype in commissioning; generation and numerical performance not capturedExisting project descriptionRecorded descriptionExisting catalog prose, not a new measurement Evidence & qualificationsHardware description only, not a throughput benchmark. Preserve the named mission/generation. Recorded source links are in the supporting evidence below. Existing catalog prose, not a new measurement Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThe September 24 and October 1 Google accounts do not disclose project-specific IT electrical power. | 2 suppliers / hosts2 relationship records |
EDGX STERNA orbital-computing demonstrations →EDGX · EuropeLatest development 28 Oct 2026 ↗Manual review 31 Oct 2026Stage detail: First payload operational data reported Compared the October28 flight release with ESA's undated Sterna/Morus development record and existing configurations. Retained product ratings, interfaces and TRL claims as held references. March operational-data receipt, planned 2027 hardware and unresolved product lifetime targets remain separate. No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Onboard AI and third-party software hosting | Launched First payload operational data reported Next project milestoneVerify published orbital test results and progress of the booked 2027 missions. | Two March 2026 hosted demonstrationsMarch 2026 STERNA demonstrationsRecorded descriptionExisting catalog prose, not a new measurement Evidence & qualificationsOne payload returned operational data within two weeks. The second still awaits satellite commissioning. Later 2027 bookings are separate. Existing catalog prose, not a new measurement Source / observation date: . Supporting source ↗ | STERNA with NVIDIA Jetson Orin NX in Super ModeOut of Tern planned for February 2027Reported specificationofficial project specification Evidence & qualificationsThe operator explicitly maps this hardware and mode to the booked Gracious Gloria demonstration. It does not establish the March 2026 payload mode, numerical performance or sustained flight power. The October28 release describes over50percent more AI performance in Super Mode. Relative design claim only, with workload and arithmetic format unspecified. official project specification Source / observation date: . Supporting source ↗2 more configurations / specificationsHyperspectral camera, STERNA, Morus based on NVIDIA Jetson Thor, and relay linkWingman planned for October 2027Reported specificationofficial project specification Evidence & qualificationsThe booked D-Orbit ION mission is described as the first complete EDGX payload and first Morus flight. Component models, count, workload throughput and mission power are not disclosed here. Product-wide Morus ratings are not assigned to this mission. The October 28 release identifies Morus as based on Jetson Thor. This is planned hardware, not flown performance. official project specification Source / observation date: . Supporting source ↗STERNA built on NVIDIA JetsonMarch 2026 STERNA demonstrationsReported specificationofficial reported specification Evidence & qualificationsExact Jetson variant, installed count and achieved AI throughput are not disclosed for the March payloads. Do not assign planned 2027 Orin NX Super Mode to these flights. The Sterna platform is designed to adapt processing to power and thermal conditions, without a disclosed flight operating envelope. official reported specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 3 suppliers / hosts4 relationship records |
Starcloud →Starcloud · United StatesLatest development 28 Oct 2026 ↗Manual review with evidence gaps 30 Oct 2026Stage detail: Demonstration program Operator pages retain Starcloud-1 launch/model reports and planned Starcloud-2 GPU cluster, persistent storage and sun-synchronous orbit. Quindar software plan and supplier link reconciled. Earlier launch forecasts, investor mission mapping and power definition remain unresolved, without blocking supported facts. Last full profile review: 20 Oct 2026. Sources collected: 20 Oct 2026. Source collection and substantive profile review are separate checks. | Orbital AI experiments and planned cloud services | Demonstrated Demonstration program Next project milestoneStarcloud-2 commercial follow-on: late-2026/October launch targets in partner and executive announcements, with limited customer access and full operation targeted by 2027. | 1 satelliteStarcloud-1 prototypeReported specificationLaunched hardware specification Evidence & qualificationsLaunched November 2025; this records the disclosed demonstration, not a current total of all company spacecraft. Launched hardware specification Source / observation date: . Supporting source ↗ | 1 NVIDIA H100 GPUStarcloud-1 prototypeReported specificationReported demonstration Evidence & qualificationsCompany reports onboard model execution and training. Hardware count is not a measured FLOPS figure. Reported demonstration Source / observation date: . Supporting source ↗1 more configurations / specificationsPlanned GPU cluster, models and quantities undisclosedStarcloud-2 planned commercial missionReported specificationoperator planned configuration Evidence & qualificationsOperator's current undated product page describes the planned commercial mission. This does not establish installed processor models, GPU counts or arithmetic throughput and is separate from Starcloud-1's H100. operator planned configuration Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThe reviewed material does not establish a current project-specific IT load. Proposed later spacecraft figures are retained separately and are not assigned to Starcloud-1. | 8 suppliers / hosts8 relationship records |
Stampede →Cowboy Space · United StatesLatest development 27 Oct 2026 ↗Manual review 27 Oct 2026Stage detail: In development Compared Cowboy homepage, the October 27 Big Iron announcement and existing Stampede records. Big Iron specifications are planned; no operating compute fleet or flight result is established. Last full profile review: 21 Oct 2026. Sources collected: 21 Oct 2026. Source collection and substantive profile review are separate checks. | Integrated launch, power and orbital data-center system | Development In development Next project milestoneFirst Big Iron flight, targeted for 2028 | Compute constellationDetailed configuration not available in reviewed material. | Five NVIDIA Vera Rubin GPU compute racksPlanned Big Iron computing upper stage for StampedeReported specificationplanned specification Evidence & qualificationsAnnounced carrying configuration, not installed hardware or a throughput benchmark. planned specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThe megawatt-class Big Iron statement does not establish IT load, operating duty or delivered performance. It remains an unresolved-boundary electrical design claim. | 1 suppliers / hosts1 relationship records |
Orbit Keeper 01 →Graviron Aerospace · United StatesLatest development 25 Oct 2026 ↗Manual review 29 Oct 2026Stage detail: In development Compared service, launch selection and Vector Phase A pages. Reused eight accepted technical observations, reconciled their single Vector configuration, and added separate payload-envelope concepts. Hosted budgets remain distinct from IT capacity. Generic reusable-drone specifications are not assigned to non-reusable Vector. No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Shared orbital computing and hosted payload services | Development In development Next project milestoneDevelop and qualify Orbit Keeper 01 Vector for a targeted Q2 2028 first commercial mission. | 10 hosted positions plus Graviron onboard computing demonstrationVector Phase A preliminary designReported specificationoperator preliminary phase a design Evidence & qualificationsPreliminary accommodation budget, not ten processors, ten computers or an installed fleet. The dedicated onboard-computing hardware is not identified. operator preliminary phase a design Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteVector Phase A page does not disclose installed processor/GPU, arithmetic throughput, compute RAM, IT-compute power or a quantified thermal design. Hosted position allocations do not fill these fields. | Not disclosed in reviewed sources Coverage noteVector Phase A page does not disclose installed processor/GPU, arithmetic throughput, compute RAM, IT-compute power or a quantified thermal design. Hosted position allocations do not fill these fields. | 0 suppliers / hosts0 relationship records |
MESEO distributed EO processing framework →GMV Aerospace and Defence-led consortium · Europe · Spain-ledLatest development 23 Oct 2026 ↗Manual review 29 Oct 2026Stage detail: In development Compared the CORDIS fact sheet and results, consortium directory and technical contributions. Verified the EU grant, added consortium links and orchestration architecture, and kept ground benchmarks separate from orbital capability No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Distributed Earth-observation processing and orchestration | Development In development Next project milestoneComplete the funded research period by November 30, 2026 and pursue further validation and adoption. | Orbital and ground software research programDetailed configuration not available in reviewed material. | SATLANTIS payload Electronics Control System with planned FPGA-based data writingOnboard ECS research and prototypingReported specificationconsortium reported development architecture Evidence & qualificationsThe SATLANTIS contribution describes customizing the ECS and FPGA-based disk writing for onboard processing. Processor/FPGA model, installed quantity, compute throughput and a named flight deployment are not disclosed. Generic iSIM product performance is not assigned to this project. consortium reported development architecture Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 0 suppliers / hosts8 relationship records |
ORCHIDE onboard orchestration platform →Thales Alenia Space-led consortium · Europe · France-ledLatest development 23 Oct 2026 ↗Manual review 28 Oct 2026Stage detail: Research program completed Compared the CORDIS fact sheet and October 2026 results article. Completion, consortium roles, EU contribution and the software/simulation results are supported; no launched ORCHIDE payload or operating commercial service is established. No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | AI application SDK and satellite orchestration research | Historical Research program completed Next project milestoneFurther development of the results under the separate ORION program and future adoption or flight validation. | Orbital software research programDetailed configuration not available in reviewed material. | KP Labs Leopard single-node testbed: Zynq UltraScale+ SoC, four Cortex-A53 cores, two Cortex-R5 cores and FPGALeopard single-node ground research testbedReported specificationpublished ground research testbench Evidence & qualificationsThe project paper identifies this exact test configuration. Intuition-1 heritage of the Leopard product does not establish an ORCHIDE flight. No sustained orbital throughput is demonstrated. published ground research testbench Source / observation date: . Supporting source ↗2 more configurations / specificationsFive Raspberry Pi 5 boards with quad-core Arm Cortex-A76 processorsFive-node Raspberry Pi 5 ground research clusterReported specificationpublished ground research testbench Evidence & qualificationsSection 10.4 and the results tables identify the evaluated five-board cluster. An earlier development paragraph mentions one controller and three workers. The configurations are not combined, and none is flight hardware. published ground research testbench Source / observation date: . Supporting source ↗Kalray-equipped AMD64 host, NXP LX2160 16-core Arm node and Versal VCK190 nodeThree-node heterogeneous ground research clusterReported specificationpublished ground research testbench Evidence & qualificationsMixed-architecture ground testbench identified in section 10.6. Its lab-network links, CPU counts and memory are not a deployed orbital constellation or a spacecraft link specification. published ground research testbench Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 0 suppliers / hosts4 relationship records |
ORION orbital orchestration framework →Planetek Hellas-led Horizon Europe consortium · Europe · Greece-ledLatest development 23 Oct 2026 ↗Manual review 30 Oct 2026Stage detail: Funded development Compared current CORDIS objectives, grant and participant records. Expanded the documented software architecture. Planetek announcement unavailable, but CORDIS supports the accepted research scope and funding. Last full profile review: 15 Oct 2026. Sources collected: 23 Oct 2026. Source collection and substantive profile review are separate checks. | Collaborative satellite and edge-processing orchestration | Development Funded development Next project milestoneDevelop and validate the orbital orchestration framework; specific flight assets and demonstration dates are not disclosed. | Orbital software platformDetailed configuration not available in reviewed material. | Not disclosed in reviewed sources Coverage noteInspected official project and technical material on October 30 does not provide configuration-specific arithmetic throughput and precision. No value is borrowed from generic components or a different mission. | Not disclosed in reviewed sources Coverage noteInspected official project and technical material on October 30 does not provide configuration-specific IT electrical load. No value is borrowed from generic components or a different mission. | 0 suppliers / hosts4 relationship records |
SOPHOS onboard processing and memory program →DSI Aerospace-led consortium · Europe · Germany-ledLatest development 23 Oct 2026 ↗Manual review 31 Oct 2026Stage detail: Ground demonstrator completed Compared CORDIS results with the project, partner and EU grant records. Added processing/memory modules, Ethernet routing, SAR algorithms and ground-validation scope. Derived flight technologies remain unnamed, and no operating data-center capacity or numerical compute benchmark is established. No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Payload processing, mass memory and SAR research | Historical Ground demonstrator completed Next project milestonePartners continue technology development and mission adoption following the research program, which ended in February 2026. | Integrated hardware/software tested in a ground demonstratorSOPHOS ground research demonstratorReported specificationofficial ground research result Evidence & qualificationsGround research result, not an operating data center or named new flight. Coordinator separately reports derived technologies already in orbit without naming missions. official ground research result Source / observation date: . Supporting source ↗ | Unibap Payload Processing ModuleSOPHOS ground research demonstratorReported specificationofficial ground research result Evidence & qualificationsHigh-performance processing module developed under SOPHOS. Processor model, accelerator count and arithmetic throughput are not stated. official ground research result Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 0 suppliers / hosts4 relationship records |
HPE Spaceborne Computer-4 →Hewlett Packard Enterprise · United StatesLatest development 20 Oct 2026 ↗Manual review 27 Oct 2026Stage detail: Launch planned Compared current HPE announcement and integration timeline. Hardware and planned workloads are supported; launch, lunar operation and benchmark results remain future. No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Lunar rover AI, LiDAR processing and HPC testing | Development Launch planned Next project milestonePlanned late-2026 launch on the Griffin-1 mission, followed by deployment near the lunar south pole if the mission lands successfully. | Lunar computing payloadDetailed configuration not available in reviewed material. | Fanless, low-power CPU and GPU module with KIOXIA SSD flash storageHPE Spaceborne Computer-4 on Astrolab FLIPReported specificationofficial issuer description Evidence & qualificationsHPE describes the planned lunar hardware. Processor models, storage capacity and numeric electrical power are not disclosed. This is not a lunar performance result. official issuer description Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 2 suppliers / hosts4 relationship records |
Reason-2 →Cowboy Space Corporation · United StatesLatest development 20 Oct 2026 ↗Manual review 29 Oct 2026Stage detail: In development Direct review of Cowboy Space and NOAA releases confirmed the planned 2027 Reason-2 NOAA demonstration, NVIDIA GPU processing, CSPP LEO and MiRS workloads, and a planned 25 Gbps optical downlink. Exact GPU model, quantity, IT power, orbit and launch booking remain undisclosed optional facts. No completed full profile review is recorded. Sources collected: 20 Oct 2026. Source collection and substantive profile review are separate checks. | NOAA environmental-data processing and optical downlink | Development In development Next project milestoneLaunch Reason-2 in 2027 and execute the NOAA in-orbit data-processing demonstration. | Orbital compute demonstrationDetailed configuration not available in reviewed material. | Planned NVIDIA GPU-based NOAA CSPP LEO / MiRS demonstration; model/count undisclosedExisting project descriptionRecorded descriptionExisting catalog prose, not a new measurement Evidence & qualificationsHardware description only, not a throughput benchmark. Preserve the named mission/generation. Recorded source links are in the supporting evidence below. Existing catalog prose, not a new measurement Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 0 suppliers / hosts1 relationship records |
Three-Body Computing Constellation →Zhejiang Lab / ADA Space / partners · ChinaLatest development 20 Oct 2026 ↗Manual review with evidence gaps 30 Oct 2026Stage detail: Satellites launched October 9 operator recap adds planned IAC compute-pair storage, model, throughput and optical-link specifications, plus a distinct new Oman-pair design. October 8 flight wording conflicts with the later Q4 launch plan. Existing launched batches and shared assets remain separate. Last full profile review: 15 Oct 2026. Sources collected: 15 Oct 2026. Source collection and substantive profile review are separate checks. | Distributed computing, networking and AI research | Launched Satellites launched Next project milestonePublish group-02 commissioning and onboard computing results. No dated result is established. | 12 satellitesFirst constellation batchReported specificationLaunched hardware specification Evidence & qualificationsLaunch count for the first batch, not a claim that all satellites remain operational. Launched hardware specification Source / observation date: . Supporting source ↗2 more configurations / specifications2 planned satellitesMarco Polo / Ibn Battuta planned pairReported specificationoperator planned configuration Evidence & qualificationsOctober 9 recap targets Q4 2026 launch. No launcher, exact date, completed deployment or commissioning is established. Parent ecosystem membership does not establish a current active-satellite total. operator planned configuration Source / observation date: . Supporting source ↗2 planned satellitesNew Oman Lens / STAR.VISION pairReported specificationoperator planned configuration Evidence & qualificationsSource announces two new AI remote-sensing satellites. It does not establish launch date or operation. The new pair and prior OL-1 must not be combined into an asserted active fleet count. operator planned configuration Source / observation date: . Supporting source ↗ | 1,000 POPS · Arithmetic precision not specifiedFull constellation roadmapReported specificationPlanned specification Evidence & qualificationsPeta operations per second as stated by the source. Numerical precision and realized utilization are not disclosed; not converted to FLOPS. Planned specification Source / observation date: . Supporting source ↗3 more configurations / specifications5 POPS · Arithmetic precision not specifiedReported aggregate capability of the twelve May 2025 satellitesReported specificationLaunched hardware specification Evidence & qualificationsWIC/CCTV reports 5 POPS. This is an attributed capability rating for launched hardware, not an independent sustained benchmark. Precision is unspecified; an early 4 POPS report differs, so no PFLOPS conversion or reconciliation is assumed. Launched hardware specification Source / observation date: . Supporting source ↗Up to 744 TOPS · Arithmetic precision not specifiedHighest stated single-satellite capability in the initial batchReported specificationLaunched hardware specification Evidence & qualificationsSource states a maximum, not a uniform rating for each of twelve satellites. Precision and independent measured throughput are unspecified; do not multiply by twelve. Launched hardware specification Source / observation date: . Supporting source ↗10 POPSIbn Battuta planned satelliteReported specificationoperator planned configuration Evidence & qualificationsOperator-reported planned capability in the native POPS unit. Arithmetic precision, operation type and sustained performance are unspecified. No FLOPS conversion or measured orbital performance is established. operator planned configuration Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 7 suppliers / hosts11 relationship records |
Mingzhu Constellation Plan →Shanghai Oriental Tiansuan · ChinaLatest development 16 Oct 2026 ↗Manual review 31 Oct 2026Stage detail: Precursor launched Compared the Shanghai launch account with existing shared-batch records. Added per-payload peak2PFLOPS and16TB storage, functions, conduction design and orbit type. Arithmetic precision, numerical power and measured orbital results remain unspecified. Last full profile review: 14 Oct 2026. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Shared orbital computing infrastructure | Launched Precursor launched Next project milestoneObtain dated commissioning and onboard test results for the launched precursor. Wider network deployment remains planned. | 6 computing payloadsSix Oriental Tiansuan payloads in shared Xingsuan group02Reported specificationofficial reported launched inventory Evidence & qualificationsOne named precursor is Star Era-44. Six payload hosts are part of the shared eight-satellite batch, not six additional spacecraft. official reported launched inventory Source / observation date: . Supporting source ↗ | About 2 PFLOPSPer Oriental Tiansuan group02 computing payloadReported specificationofficial source specification Evidence & qualificationsPeak computing-core hardware rating per payload. Arithmetic precision and operating workload are unspecified. Not measured orbital throughput or an aggregate constellation benchmark. official source specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteNo applicable numerical value in official material inspected on2026-10-31. A dated review finding, not universal nondisclosure. | 0 suppliers / hosts9 relationship records |
Solafune–Tohoku onboard-AI satellite →Solafune / Tohoku University · JapanLatest development 15 Oct 2026 ↗Manual review 29 Oct 2026Stage detail: Planned development and in-orbit demonstration The October 15 official issuer release confirms the institute, onboard analysis-and-planning loop and planned satellite demonstration. Hardware, schedule, financing and measured performance are undisclosed. No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Mission-serving onboard AI for Earth-observation data analysis and observation planning | Development Planned development and in-orbit demonstration Next project milestoneDefine the spacecraft configuration, launch schedule and success criteria for the planned in-orbit demonstration. | Onboard AI research satelliteDetailed configuration not available in reviewed material. | Not disclosed in reviewed sources Coverage noteThe official release gives no arithmetic throughput or application timing. | Not disclosed in reviewed sources Coverage noteThe official release gives no IT electrical load. | 0 suppliers / hosts1 relationship records |
Pazhou Intelligent Computing Constellation →Yusuan Xinghe (宇算星河) · ChinaLatest development 14 Oct 2026 ↗Manual review 30 Oct 2026Stage detail: Launched — first two satellites, broader validation outstanding Compared the October 14 issuer release with the roadmap and suppliers. Saved the first two satellites and intended data workflow. Numerical compute, IT power and sustained orbital service remain unverified. Last full profile review: 20 Oct 2026. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Distributed orbital AI computing | Launched Launched — first two satellites, broader validation outstanding Next project milestoneCheck official results of the A-group orbital model validation and announcements for subsequent groups. No verified date is available. | About 24 satellitesPlanned Pazhou constellation across four deployment groupsReported specificationPlanned specification Evidence & qualificationsCompany roadmap, not launched or operating assets. The later October 14 issuer release identifies two first-group spacecraft, Xing Shidai-47 and -48. Do not infer six satellites in every group. Later evidence: https://m.sohu.com/a/1087797879_121613636 Planned specification Source / observation date: . Supporting source ↗1 more configurations / specifications2 satellitesPazhou A-group, October 14 2026Reported specificationissuer reported launch Evidence & qualificationsIssuer-distributed PCI release identifies Xing Shidai-47 and -48, built by ADA Space. Count is part of the planned 24-satellite system, not additional to it and not evidence of sustained compute service. issuer reported launch Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteInspected official project and technical material on October 30 does not provide configuration-specific arithmetic throughput and precision. No value is borrowed from generic components or a different mission. | Not disclosed in reviewed sources Coverage noteInspected official project and technical material on October 30 does not provide configuration-specific IT electrical load. No value is borrowed from generic components or a different mission. | 2 suppliers / hosts2 relationship records |
TakeMe2Space MOI program →TakeMe2Space · IndiaLatest development 14 Oct 2026 ↗Manual review with evidence gaps 29 Oct 2026Stage detail: MOI-1A reported lost. MOI-1B planned. Current operator records support successful MOI-TD AI-lab operation. The older undated data sheet is retained as superseded historical evidence. Separate MOI-1A loss details and network schedule conflicts remain limited-profile questions. Last full profile review: 14 Oct 2026. Sources collected: 23 Oct 2026. Source collection and substantive profile review are separate checks. | Onboard AI, imagery processing and hosted applications | Development MOI-1A reported lost. MOI-1B planned. Next project milestoneOperator targets MOI-1B for November 2026. Launch and results remain unconfirmed. The exact date and cause of the MOI-1A loss remain undisclosed. | 6 satellitesTotal planned MOI constellationReported specificationPlanned specification Evidence & qualificationsRIDE!'s September 10 release describes a total six-satellite constellation and says its contracted pair forms part of that total, with the pair targeted for Q3 2028. The operator homepage's older Q4 2027 network target conflicts with this schedule; overall constellation completion remains unresolved. The pair is not additional to the six, and no deployed count is established. Planned specification Source / observation date: . Supporting source ↗1 more configurations / specifications6 UMOI-1B current operator-page designReported specificationofficial reported specification Evidence & qualificationsCurrent page names MOI-1B and a November 2026 launch target. This is a planned configuration and must not overwrite MOI-1A or resolve historical MOI-TD claims. official reported specification Source / observation date: . Supporting source ↗ | 117 TOPS · Arithmetic precision not specifiedMOI-1A replacement satellite GPU specificationReported specificationPlanned specification · October 2026 Evidence & qualificationsObserved on an undated operator page on September 26. Numerical precision is unspecified; this is not a demonstrated benchmark or failed MOI-1 capacity. Planned specification · October 2026 Source / observation date: . Supporting source ↗2 more configurations / specifications4 TOPS · Arithmetic precision not specifiedHistorical MOI-TD Edge TPU advertised hardware capabilityReported specificationLaunched hardware specification Evidence & qualificationsOperator technical account of the launched demonstrator with unspecified arithmetic precision. Current operator mission history and technical article report successful AI-lab protocol execution and in-orbit inference. The 4 TOPS value is an advertised hardware specification, not measured orbital throughput. An older undated data sheet is retained as superseded historical evidence. This is separate from the planned MOI-1A 117 TOPS specification. Launched hardware specification Source / observation date: . Supporting source ↗117 TOPSMOI-1B current operator-page designReported specificationofficial reported specification Evidence & qualificationsAdvertised rating with undisclosed arithmetic precision. Not a measured orbital benchmark. official reported specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThe operator reports a 120 W payload or peak figure and a separate 10 to 55 W AI-Cube product range. Neither establishes the strict mission IT load for the displayed project configuration. | 7 suppliers / hosts9 relationship records |
Merlin constellation →Satellogic · United States / ArgentinaLatest development 13 Oct 2026 ↗Manual review 29 Oct 2026Stage detail: First satellite in early operations Compared Satellogic’s October 2 launch release and October 13 health update. One Merlin.01 spacecraft launched, contacted ground, updated software and showed deployed arrays. Onboard AI, 30-minute alerts and inter-satellite cueing remain design claims until payload commissioning and results are reported. No completed full profile review is recorded. Sources collected: Date unavailable. Source collection and substantive profile review are separate checks. | Mission-serving onboard AI for Earth-observation detection, alerting and satellite cueing | Launched First satellite in early operations Next project milestoneComplete Merlin.01 payload testing and commissioning; Satellogic targets full service in the second half of 2027. | First-pass contact; onboard software updated within two days; solar arrays deployed; payload commissioning pendingMerlin.01 launched spacecraftReported specificationSatellogic early-operations update Evidence & qualificationsThis supports spacecraft health and software-update capability, not commissioned onboard-AI performance. Satellogic early-operations update Source / observation date: . Supporting source ↗ | Onboard AI processes imagery and recognizes changeMerlin constellation designReported specificationSatellogic design description Evidence & qualificationsQualitative workload description; processor, precision, throughput and commissioned results are undisclosed. Satellogic design description Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThe reviewed releases give no IT electrical load. | 1 suppliers / hosts2 relationship records |
Altair-Next Gen →Marlan Space / Loft Orbital · France / United Arab EmiratesLatest development 12 Oct 2026 ↗Manual review 31 Oct 2026Stage detail: Operator-reported onboard AI workload Compared Loft's October12 installed-hardware disclosure with Unibap's October1 flight account and current project/relationship records. Added the iX10 identity while preserving the separate two Jetson AGX Orin modules, future hardware evaluations and overlapping ten/50-satellite scopes. Their internal hardware mapping remains unspecified. Last full profile review: 18 Oct 2026. Sources collected: 18 Oct 2026. Source collection and substantive profile review are separate checks. | Onboard AI and hosted applications | Demonstrated Operator-reported onboard AI workload Next project milestoneFurther commissioning and measured application-service results for Altair1, plus delivery dates for subsequent satellites. | 50 satellitesInitial program phaseReported specificationPlanned specification Evidence & qualificationsThe first ten were in production; the 50-satellite program is not an operational fleet. Planned specification Source / observation date: . Supporting source ↗1 more configurations / specificationsShared onboard applications generate alerts and georeferenced outputs from sensor dataAltair-1 launched October 1 2026Reported specificationofficial mission design specification Evidence & qualificationsLoft describes a shared multi-application platform. User-facing seconds/minutes claims do not provide a defined latency benchmark. First spacecraft, not completion of the50-satellite program. official mission design specification Source / observation date: . Supporting source ↗ | 2 NVIDIA Jetson AGX Orin modulesAltair-1 launched October 1 2026Reported specificationofficial launched hardware account Evidence & qualificationsLoft October 12 and NVIDIA accounts identify the first satellite's installed model. Not a fleet-wide count or generic product benchmark. official launched hardware account Source / observation date: . Supporting source ↗1 more configurations / specificationsUnibap iX10 onboard computing hardwareAltair-1 launched October 1 2026Reported specificationofficial project specification Evidence & qualificationsSupplier's October1 account associates an iX10 with the launched Altair mission. Operator's two Jetson AGX Orin modules remain separate disclosed hardware. Sources do not define their interconnection or establish that those modules are inside the iX10. No generic iX10 product ratings are assigned. official project specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 15 suppliers / hosts18 relationship records |
Loft YAM Orbital Computing Platform →Loft Orbital · United States / FranceLatest development 12 Oct 2026 ↗Manual review with evidence gaps 29 Oct 2026Stage detail: On-orbit computing demonstrated Compared operator articles and the NAVI-Orbital primary paper. Saved YAM-9 cluster layout, qualified GPU ratings, quantized model and separate ground timing. YAM-6 launch year differs between official articles. RAM and power remain unspecified. No completed full profile review is recorded. Sources collected: 10 Oct 2026. Source collection and substantive profile review are separate checks. | Shared software and AI application hosting | Demonstrated On-orbit computing demonstrated Next project milestoneFurther application deployments and disclosed service capacity. No exact next YAM deployment date is established. | Shared orbital application-hosting platformDetailed configuration not available in reviewed material. | GPU1: 248 TOPS. GPU2: 248 TOPSYAM-9 JPL demonstrationReported specificationofficial reported specification Evidence & qualificationsTable I reported hardware ratings, arithmetic precision unspecified. Do not sum into measured mission throughput. Engineering models were benchmarked, and only Comp2 provided working GPU acceleration in that test. official reported specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteMission paper, anniversary account and October 12 release inspected. Installed RAM/storage and mission power not established. Paper's 8 GB minimum VRAM is a model requirement, not installed capacity. | 1 suppliers / hosts1 relationship records |
Tiansuan / BUPT Orbital Computing Research Platform →Beijing University of Posts and Telecommunications / Spacety · ChinaLatest development 10 Oct 2026 ↗Manual review 30 Oct 2026Stage detail: Research satellites launched Compared the university's BUPT-4 launch account and supplier solar-wing report. Added spacecraft mass class and substrate construction. Per-node compute, memory and IT power remain undisclosed in those sources. Last full profile review: 18 Oct 2026. Sources collected: 18 Oct 2026. Source collection and substantive profile review are separate checks. | Open satellite computing and network-security experiments | Launched Research satellites launched Next project milestonePublish further phase-two launches and current experiment/server availability; no exact next launch date is established | 24 satellitesTiansuan second-phase deployment planReported specificationPlanned specification Evidence & qualificationsPlanned phase-two total. Do not infer that 24 satellites have launched or add earlier repository phase figures as deployed capacity. Planned specification Source / observation date: . Supporting source ↗1 more configurations / specifications16 satellitesResearch network reported September 7, 2026Reported specificationofficial reported specification Evidence & qualificationsBeijing Haidian Commerce Bureau reports a network of sixteen LEO satellites. This is an attributed program snapshot, not sixteen dedicated compute satellites, an audited live count, or an amount additional to historical launch batches. official reported specification Source / observation date: . Supporting source ↗ | Satellite-computing module and satellite-network security moduleBUPT-4 / TY49 spacecraftReported specificationofficial launch hardware description Evidence & qualificationsUniversity launch account identifies these modules and a small remote-sensing camera. Processor models, memory and computing throughput are not specified. Launch telemetry is not a sustained compute benchmark. The university-authored July 23 launch account on Beijing Daily's author platform confirms the same modules and camera at https://peking.bjd.com.cn/content/s6a622584e4b0e45f3fd517fc.html. official launch hardware description Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteUniversity-authored BUPT-4 launch account and supplier solar-wing mission account do not give installed processor ratings, RAM, storage capacity or IT-only electrical power. The separately reported token-per-joule claim lacks an identified configuration and benchmark. | 5 suppliers / hosts9 relationship records |
Oman OL-1 Intelligent Computing Satellite →STAR.VISION / Oman · Oman / ChinaLatest development 8 Oct 2026 ↗Manual review 30 Oct 2026Stage detail: Operator-reported on-orbit operation STAR.VISION reports more than 5,000 hours of OL-1 platform operation in its October 8 account. Earlier launch, Zhejiang Lab software and delivered ground segment are reconciled. No independent processor benchmark, completed model validation or paid compute service established. Last full profile review: 15 Oct 2026. Sources collected: 23 Oct 2026. Source collection and substantive profile review are separate checks. | Remote-sensing AI and distributed operating-system validation | Operating Operator-reported on-orbit operation Next project milestoneOperational commissioning and current service status have not been publicly verified | 1 satelliteOL-1 missionReported specificationLaunched hardware specification Evidence & qualificationsThe source establishes launch; current commissioning and commercial service status are not established. Launched hardware specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThe inspected mission-specific launch/delivery account does not identify arithmetic throughput or numerical precision. Generic STAR.VISION product ratings are not assigned to OL-1. | Not disclosed in reviewed sources Coverage noteThe inspected mission-specific launch/delivery account does not identify an IT-only electrical load. Generic STAR.VISION product ratings are not assigned to OL-1. | 1 suppliers / hosts2 relationship records |
NarSha / GYEONGGISat-2 methane-monitoring program →Nara Space Technology · South KoreaLatest development 7 Oct 2026 ↗Manual review 31 Oct 2026Stage detail: First mission launched, commissioning reported Compared the computing supplier, operator platform and media accounts, and Scanway mission and contract disclosures. Published source-specific platform specifications separately from flight evidence. Full computing benchmarks and per-spacecraft hardware mapping remain unspecified. No completed full profile review is recorded. Sources collected: 10 Oct 2026. Source collection and substantive profile review are separate checks. | Onboard processing for methane-monitoring optical missions | Launched First mission launched, commissioning reported Next project milestonePublish full instrument and onboard-processing validation results. Additional Scanway instruments are due in Q3 2027 for a planned early-2028 mission. | 16U CubeSat standard platformNarSha standard-platform design, not final flight inventoryReported specificationofficial project specification Evidence & qualificationsOperator standard-platform description. Not a count of launched spacecraft. official project specification Source / observation date: . Supporting source ↗1 more configurations / specificationsAt least twelve microsatellites in the supplier's program roadmapNarSha constellation roadmapReported specificationofficial project specification Evidence & qualificationsJune25 supplier account states at least12, while earlier report wording and later possibilities vary. Not contracted spacecraft count, completed hardware or an additive total across aliases. official project specification Source / observation date: . Supporting source ↗ | Unibap iX5 onboard computerNarSha compute mission on Transporter-18Reported specificationofficial project specification Evidence & qualificationsSupplier associates iX5 with the NarSha mission on October1. Exact iX5 variant, installed processor components, node count and flight benchmark are not identified. Not the D-Orbit iX20 or Altair iX10. official project specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteNo project-specific value in the official sources inspected on2026-10-31. This does not establish universal nondisclosure. | 4 suppliers / hosts6 relationship records |
Axiom Orbital Data Centers →Axiom Space · United StatesLatest development 6 Oct 2026 ↗Manual review with evidence gaps 30 Oct 2026Stage detail: ARC communications validated Compared current program page and dated ISS-node announcement. Added per-drive SSD capacity and source-backed LiSS hardware. Corrected the planned optical link to satellite-to-ISS. Launched ARC bits-versus-bytes conflict remains unresolved. Last full profile review: 20 Oct 2026. Sources collected: 20 Oct 2026. Source collection and substantive profile review are separate checks. | Orbital data storage and computing services | Demonstrated ARC communications validated Next project milestoneDevelop the separate ISS data-center node targeted for 2027 and expand interoperability with the two dedicated nodes. | 2 dedicated nodesJanuary 2026 deploymentReported specificationLaunched hardware specification Evidence & qualificationsExcludes the separate ISS prototype; launched nodes do not establish commercial utilization. Launched hardware specification Source / observation date: . Supporting source ↗ | Microchip PIC64-HPSC controller/workload CPU, PCIe Gen5 switch and PolarFire SoC in Spacebilt LiSSSeparate ISS node planned for 2027Reported specificationofficial mission specific description Evidence & qualificationsSeptember 16, 2025 mission-specific architecture. Replaces the catalog-only description under the same ID. Not hardware assigned to the launched ARC nodes or a measured compute benchmark. official mission specific description Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 7 suppliers / hosts10 relationship records |
Kepler Tranche 1 →Kepler Communications · CanadaLatest development 6 Oct 2026 ↗Manual review with evidence gaps 30 Oct 2026Stage detail: Commercial services operating Compared dated commissioning release and current Compute page. Added distributed/failover architecture and CUDA framework support. Product-page100Gbps is not assigned to Tranche1. Existing optical-link unit conflict remains. Last full profile review: 15 Oct 2026. Sources collected: 23 Oct 2026. Source collection and substantive profile review are separate checks. | Optical relay, distributed compute and hosted nodes | Operating Commercial services operating Next project milestoneFurther customer deployment and service-performance disclosure; no exact next event date announced. | 10 satellitesFirst Kepler optical-relay trancheReported specificationLaunched hardware specification Evidence & qualificationsCounts spacecraft, including those carrying hosted services. Do not add Axiom node counts to this asset total. Launched hardware specification Source / observation date: . Supporting source ↗1 more configurations / specificationsSingle-node and clustered distributed workloads, with reassignment when a node is unavailableFirst tranche: ten-satellite compute networkReported specificationofficial attributed description Evidence & qualificationsMarch16 2026 operator commissioning announcement describes the architecture. No measured failover time, uptime or workload scaling benchmark is disclosed. Existing forty-module and ten-spacecraft metrics are reused. official attributed description Source / observation date: . Supporting source ↗ | 40 Jetson Orin modulesDistributed computing across ten Tranche 1 satellitesReported specificationReported demonstration Evidence & qualificationsCommissioned hardware modules, not forty satellites or measured throughput. No conversion to FLOPS or IT power. Reported demonstration Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteThis is a coverage gap in the inspected published data. It does not prove that no disclosure exists elsewhere. | 3 suppliers / hosts3 relationship records |
Aethero Titan →Aethero · United StatesLatest development 5 Oct 2026 ↗Manual review with evidence gaps 30 Oct 2026Stage detail: Launch planned Compared current Aethero mission pages and both partnership accounts. Added the planned mid-inclination LEO route and named distribution modules. IT load is undisclosed. Launch remains planned and arithmetic precision and throughput qualifiers remain unresolved. Last full profile review: 20 Oct 2026. Sources collected: 23 Oct 2026. Source collection and substantive profile review are separate checks. | High-performance orbital computing demonstration | Development Launch planned Next project milestoneAethero's current platform and company pages and explicit partnership-release update target SpaceX Bandwagon-6 no earlier than Q2 2027. This supersedes its October 2026 and Transporter-19 targets. Launch and commissioning remain unconfirmed. | COTS compute with checkpointing, error correction, scrubbing and filesystem resilienceTitan / FRAME-15 planned spacecraftReported specificationofficial design description Evidence & qualificationsMission-announcement reliability design. Does not establish a radiation dose limit, qualification result or demonstrated orbital availability. official design description Source / observation date: . Supporting source ↗ | NxA-ECM and NxN-ECM cluster with Thor-based NxA modules, integrated through Aethero PCDM, PDM and DDMTitan / FRAME-15 planned spacecraftReported specificationoperator mission design specification Evidence & qualificationsPlanned Titan architecture and named power/data distribution modules on the current operator platform page. Module counts, arithmetic precision and sustained throughput are not established. Generic NxA product storage, size and thermal ratings are not assigned to the installed Titan payload. operator mission design specification Source / observation date: . Supporting source ↗ | Not disclosed in reviewed sources Coverage noteNeither the current mission page nor the partnership releases disclose a dedicated IT load. The 3.4 kW solar peak rating must not be used as compute consumption. | 2 suppliers / hosts2 relationship records |
Technical specifications retain the source’s original units and evidence status. Hardware counts, compute rates and power are not equivalent; launched hardware does not establish demonstrated performance. Supplier counts include suppliers and hosts only, reflect current filters and cover this directory, not the entire market. “No record” means no disclosure captured; it does not mean the work is unawarded. Latest developments use source dates, not routine review or collection dates.