| AmbaSat-1 Sprite Satellite Platform |
AmbaSat
|
0.01 |
— |
— |
35 |
— |
— |
| CubeSat 0.5U Electronics Package |
Tiger Innovations, Inc.
|
0.02 |
0.05 |
5 |
— |
— |
PDF
|
| SD-SAT |
Space Kidz India
|
0.033 |
— |
— |
— |
— |
— |
| OzQube-1 |
Picosat Systems
|
0.1 |
— |
— |
50 |
— |
— |
| VERSE-02 2U Cubesat Structure |
2NDSpace Srl
|
0.195 |
— |
— |
— |
2U |
PDF
|
| RW40 |
Comat
|
0.23 |
0.9 |
— |
— |
— |
— |
| PocketQube Satellite Platform |
Delta Space Leonis
|
0.25 |
— |
— |
50 |
— |
— |
| XavSat PocketQubes (1P to 3P) |
Xavier Space Solutions (XavSat)
|
0.25 |
1 |
— |
— |
— |
— |
| MINIATURE SATELLITES (PocketQubes) |
Xavier Space Solutions (XavSat)
|
0.25 |
1 |
— |
— |
— |
— |
| VERSE-03 3U Cubesat Structure |
2NDSpace Srl
|
0.29 |
— |
— |
— |
3U |
PDF
|
| CubeSat Kit GEN1 |
Hex-Star Universe
|
0.3 |
— |
— |
100 |
— |
— |
| Hydra Space PocketQube IoT Satellite Platform |
Hydra Space
|
0.4 |
— |
— |
100 |
— |
— |
| Structure 3U CubeSat with Separation System |
SPUTNIX
|
0.455 |
— |
— |
340.5 |
— |
— |
| VERSE-06 6U Cubesat Structure |
2NDSpace Srl
|
0.69 |
— |
— |
— |
6U |
PDF
|
| Thybolt Mission |
Dhruva Space
|
0.75 |
— |
— |
— |
Near circular polar sun-synchronous orbi |
— |
| TubeSat 3.0 Personal Satellite Kit |
Interorbital Systems
|
0.75 |
— |
— |
— |
Hexadecagonal (16-sided) prism |
— |
| IOS TubeSat Kit |
Interorbital Systems
|
0.75 |
— |
— |
— |
— |
— |
| VERSE-08 8U Cubesat Structure |
2NDSpace Srl
|
0.89 |
— |
— |
— |
8U |
PDF
|
| ONDOSAT-OWL CubeSat |
ONDO Space
|
0.9 |
— |
— |
— |
0.5U CubeSat |
— |
| OrbiCraft-Pro 1U Experimental (SXC1) |
SPUTNIX
|
0.9 |
— |
— |
113.5 |
— |
PDF
|
| 8U CubeSat Structure |
EnduroSat
|
0.973 |
— |
— |
454 |
— |
— |
| ExseedSat-1 Amateur Radio CubeSat (VO-96) |
Satellize
|
1 |
2.8 |
— |
— |
1U CubeSat (10 × 10 × 10 cm) |
— |
| ESAT Educational Nanosatellite |
Theia Space
|
1 |
— |
— |
100 |
1U CubeSat |
PDF
|
| ROBUSTA-1A |
ISAE-SUPAERO — Club CubeSat
|
1 |
— |
— |
— |
LEO 800 km SSO |
— |
| BEESAT-2 |
TU Berlin — Chair of Space Technology
|
1 |
— |
— |
— |
LEO |
— |
| BEESAT-1 |
TU Berlin — Chair of Space Technology
|
1 |
— |
— |
— |
LEO |
— |
| Seiren CubeSat Bus Systems and SAR Satellite Antennas |
SEIREN Co., Ltd. (Space Division)
|
1 |
— |
— |
— |
— |
— |
| MicroOrbiter-1 (MO-1) CubeSat |
MicroOrbiter
|
1 |
— |
— |
— |
1U CubeSat (10 cm cube) |
— |
| Satellite Platforms (P-DoT, P-30, P-Nu, LEAP series) |
Dhruva Space
|
1 |
50 |
— |
— |
— |
— |
| P-DoT CubeSat Satellite Platform |
Dhruva Space
|
1 |
— |
— |
— |
0.5U to 12U CubeSat |
— |
| PEGASUS |
FH Wiener Neustadt
|
1 |
— |
— |
— |
1U CubeSat |
— |
| Tailored Small Satellite Systems |
S4 – Smart Small Satellite Systems GmbH
|
1 |
— |
— |
— |
— |
PDF
|
| 3U platform |
Orbital Systems
|
1 |
— |
— |
340 |
— |
— |
| OrbiCraft-Pro Educational CubeSat Kit |
SPUTNIX
|
1 |
2 |
— |
— |
1U / 3U |
PDF
|
| VERSE-12 12U Cubesat Structure |
2NDSpace Srl
|
1.19 |
— |
— |
— |
12U |
PDF
|
| UoBSat-1 CubeSat Research Platform |
University of Bristol
|
1.33 |
— |
— |
— |
10 x 10 x 10 cm |
— |
| CubeSat 3.0 Personal Satellite Kit |
Interorbital Systems
|
1.33 |
— |
— |
— |
— |
— |
| OrbiCraft-Pro 3U Flight (SXC3-GA) |
SPUTNIX
|
1.45 |
— |
— |
— |
— |
PDF
|
| 3U Cubesat Platform |
Orbital Systems
|
1.5 |
50 |
— |
— |
— |
— |
| VERSE-16 16U Cubesat Structure |
2NDSpace Srl
|
1.52 |
— |
— |
— |
16U |
PDF
|
| FIREBIRD-II CubeSat |
Montana State University
|
2 |
— |
— |
150 |
1.5U CubeSat (pair) |
— |
| PanelSat™ |
Blink Astro
|
2 |
— |
— |
— |
— |
— |
| PanelSat |
Blink Astro
|
2 |
— |
— |
— |
— |
— |
| UNSW-EC0 |
UNSW Sydney (ACSER)
|
2 |
— |
— |
— |
2U CubeSat |
— |
| Kuva Space Hyperspectral Microsatellites (Hyperfield Constellation) |
Kuva Space
|
2 |
— |
— |
— |
— |
— |
| OrbiCraft 3D nanosatellite functional kit |
SPUTNIX
|
2 |
— |
6.6–8.4 |
— |
— |
— |
| Geoscan 1U CubeSat Platform |
Geoscan
|
2 |
— |
— |
100 |
1U CubeSat |
PDF
|
| XO-BUS CubeSat Buses |
Exobotics
|
2.2 |
25 |
— |
— |
— |
— |
| MOVE-II |
TU Munich — WARR / MOVE
|
2.4 |
— |
— |
— |
LEO 575 km SSO |
— |
| GS-1 Nanosatellite |
Yuzhnoye Design Bureau
|
2.987 |
— |
— |
370 |
— |
— |
| SALSAT |
TU Braunschweig — ERIG e.V.
|
3 |
— |
— |
— |
LEO 584 km SSO |
— |
| 3U-16U Platforms |
C3S LLC
|
3.3 |
4.5 |
— |
340.5 |
— |
PDF
|
| Cosmoworks Satellite Bus with EO-Telescope |
Cosmoworks
|
3.7 |
— |
— |
340 |
— |
— |
| BEVO-2 |
University of Texas at Austin
|
4.2 |
— |
— |
— |
3U CubeSat |
— |
| SABHASAT |
Nebula Space Organisation
|
5 |
— |
— |
— |
97.41 deg, 505 km |
— |
| Astrocast Nanosatellite |
Astrocast
|
5 |
— |
— |
— |
3U CubeSat |
— |
| 6U Platform Kit |
GomSpace
|
6 |
100 |
— |
— |
— |
PDF
|
| nSight-2 3U nano-satellite |
SCS Space
|
6 |
— |
— |
— |
3U nano-satellite |
— |
| CubeSat 3U Platform |
IMT (Ingegneria Marketing Technologies)
|
6 |
— |
— |
— |
— |
— |
| 8U Platform Kit |
GomSpace
|
6.5 |
100 |
— |
— |
— |
— |
| Generic Nanosatellite Bus (GNB) |
SFL Missions (Space Flight Laboratory)
|
6.5 |
— |
— |
200 |
— |
— |
| HORYU-2 |
Kyushu Institute of Technology (Kyutech)
|
7.1 |
— |
— |
— |
Nanosatellite, 350x310x315 mm |
— |
| 6U CubeSat Platform |
Orbital Systems
|
7.5 |
— |
— |
340 |
— |
— |
| CORVUS — 6U CubeSat Platform with Synthetic Aperture Radar |
RoInSpace (RISE, Romanian InSpace Engineering)
|
8 |
20 |
— |
— |
6U CubeSat (30 × 20 × 10 cm) |
— |
| 12U Platform Kit |
GomSpace
|
8 |
100 |
— |
— |
— |
— |
| RapidCube-6 |
Rapid Cubes GmbH
|
8 |
10 |
— |
360 |
— |
— |
| RapidCube-10 |
Rapid Cubes GmbH
|
10 |
— |
— |
— |
— |
— |
| 8U Platform |
EnduroSat
|
11.2 |
— |
— |
— |
— |
— |
| R2D3 CubeSat Bus |
Gran Systems
|
12 |
50 |
— |
— |
— |
— |
| 6U CubeSat Platform SXC6 VOL AS TF |
SPUTNIX
|
12 |
35 |
— |
366 |
6U CubeSat |
— |
| 6U CubeSat Platform SXC6 ADC AS TFF |
SPUTNIX
|
12 |
35 |
— |
366 |
6U CubeSat |
— |
| Satellite platform SXC6 modification "ADC" |
SPUTNIX
|
12 |
35 |
— |
— |
— |
PDF
|
| Satellite platform SXC6 modification "Basic" |
SPUTNIX
|
12 |
15 |
5 |
— |
— |
PDF
|
| VCUB1 Nanosatellite Platform |
Visiona Tecnologia Espacial
|
12 |
— |
— |
— |
Scalable 3U to 27U+ |
— |
| CubeSat 6U Lunar |
Yuzhnoye Design Bureau
|
14 |
60 |
— |
— |
— |
— |
| Triumph |
Terran Orbital
|
14 |
100 |
— |
— |
— |
PDF
|
| RapidCube-20 |
Rapid Cubes GmbH
|
15 |
17 |
12–24 |
440 |
12U/16U CubeSat |
— |
| M8P 8U CubeSat Nanosatellite |
NanoAvionics
|
16 |
26.5 |
— |
— |
8U CubeSat |
PDF
|
| M6P Nanosatellite Bus |
NanoAvionics
|
16 |
14.5 |
— |
— |
6U CubeSat |
PDF
|
| 12U/16U CubeSat Platform |
Orbital Systems
|
16 |
— |
— |
322 |
— |
— |
| CubeSat 12U Lunar |
Yuzhnoye Design Bureau
|
20 |
80 |
— |
— |
— |
— |
| PHI-1 SAT |
MBRSC
|
20 |
— |
— |
300 |
Low Earth Orbit (~500 km altitude) |
— |
| P-30 NanoSat Satellite Platform |
Dhruva Space
|
20 |
50 |
— |
— |
LEO-optimized |
— |
| DEFIANT Small Satellite Bus |
SFL Missions (Space Flight Laboratory)
|
20 |
50 |
— |
450 |
— |
PDF
|
| Geoscan 16U |
Geoscan
|
20 |
45 |
10.5–12.6 |
454 |
— |
— |
| Satellite platform SXC12 |
SPUTNIX
|
24 |
— |
— |
— |
— |
PDF
|
| Satellite Systems (General Offering) |
ST Engineering Satellite Systems
|
24.5 |
4000 |
— |
— |
— |
PDF
|
| Renegade |
Terran Orbital
|
25 |
100 |
— |
— |
— |
PDF
|
| GNOMES — GNSS Radio Occultation Weather Data Constellation |
PlanetiQ
|
30 |
— |
— |
— |
Sun-synchronous LEO, 525–645 km |
— |
| YuzhSat Universal Spacecraft Bus |
Yuzhnoye Design Bureau
|
30 |
80 |
— |
— |
— |
— |
| Creotech Instruments Space Products and Services |
Creotech Instruments S.A.
|
30 |
80 |
28 |
— |
— |
— |
| Voyager |
Terran Orbital
|
30 |
100 |
— |
— |
— |
PDF
|
| SSTL-MICRO |
SSTL (Surrey Satellite Technology)
|
30 |
63 |
— |
— |
— |
PDF
|
| M12P 12U CubeSat Nanosatellite |
NanoAvionics
|
32 |
29.5 |
— |
— |
12U CubeSat |
PDF
|
| M16P 16U CubeSat Nanosatellite |
NanoAvionics
|
36 |
21.5 |
— |
— |
16U CubeSat |
PDF
|
| YuzhSat-1 |
Yuzhnoye Design Bureau
|
38.4 |
80 |
— |
— |
— |
— |
| NewSat |
Satellogic
|
38.5 |
— |
— |
820 |
Sun-synchronous LEO, ~440-600 km altitud |
— |
| Satellogic EO Constellation |
Satellogic
|
45 |
— |
— |
— |
— |
— |
| Skywalker IoT & AIS Constellation |
HEAD Aerospace
|
45 |
— |
— |
— |
— |
— |
| MS-VR |
Yuzhnoye Design Bureau
|
50 |
— |
— |
— |
— |
— |
| VSP-50 Versatile Satellite Platform |
Aerospacelab
|
50 |
— |
— |
— |
LEO / SSO |
PDF
|
| DFHSAT-1 Small Satellite Platform |
Shenzhen Aerospace Dongfanghong Satellite
|
50 |
— |
— |
— |
LEO |
— |
| Azista BST Aerospace Satellite Manufacturing Services |
Azista BST Aerospace
|
50 |
— |
— |
— |
— |
— |
| ABLean Satellite Manufacturing Platform |
Azista BST Aerospace
|
50 |
— |
— |
— |
— |
— |
| ABLean Manufacturing Platform |
Azista BST Aerospace
|
50 |
— |
— |
— |
— |
— |
| BIG CAT 100 |
Space Inventor ApS
|
50 |
130 |
— |
— |
— |
— |
| Firefly Hyperspectral Satellite Constellation |
Pixxel
|
50 |
— |
— |
— |
Sun-synchronous LEO |
— |
| TY-33 50kg-Class Satellite Platform |
Spacety
|
50 |
— |
— |
— |
— |
— |
| Honghu 50kg-Class Satellite Platform |
Spacety
|
50 |
— |
— |
— |
— |
— |
| CE-SAT |
Canon Electronics – Space
|
50 |
— |
— |
— |
— |
— |
| ηDragonfly |
Dragonfly Aerospace
|
50 |
71 |
24.3–32.4 |
— |
— |
PDF
|
| Photon Spacecraft Bus Platform |
Rocket Lab – Photon
|
50 |
3000 |
— |
— |
— |
— |
| HiakaSat |
University of Hawai’i at Manoa
|
55 |
— |
— |
— |
— |
— |
| General-purpose Hyperspectral Satellite Series Product |
Zhongke Xingchen
|
55 |
— |
— |
— |
— |
— |
| Orbita OHS Hyperspectral Satellite |
Zhuhai Orbita Aerospace
|
67 |
— |
— |
— |
— |
— |
| HEO (Hawk for Earth Observation) |
Argotec Srl
|
70 |
— |
— |
— |
— |
— |
| Meridian Space LEO Satcom Constellation & Microsatellite Bus |
SpinLaunch
|
70 |
— |
— |
— |
Proliferated LEO, repeating ground track |
— |
| Umbra SAR Satellite |
Umbra Lab Inc.
|
70 |
300 |
— |
— |
Sun-synchronous LEO, ~560 km altitude, 9 |
— |
| SITAEL S-75 — All-Electric Microsatellite Platform |
STRIVING
|
75 |
30 |
— |
— |
— |
PDF
|
| MP42H Microsatellite Bus |
NanoAvionics
|
75 |
98 |
— |
— |
— |
— |
| Small Satellite Platforms (S-75 to S-350) |
SITAEL S.p.A.
|
75 |
— |
— |
— |
— |
— |
| OmniFlex Satellite Platform Family |
Reflex Aerospace
|
75 |
— |
— |
— |
Full range of LEO |
— |
| Methane Integrated Satellite Series |
Zhongke Xingchen
|
75 |
— |
— |
— |
— |
— |
| Rassvet LEO Broadband Constellation |
Bureau 1440
|
80 |
— |
— |
— |
— |
— |
| GRUS |
Axelspace
|
80 |
— |
— |
— |
585-600 km altitude, sun-synchronous sub |
— |
| YAM Platform |
Loft Orbital
|
80 |
— |
— |
— |
— |
— |
| Corvus-XL |
Astro Digital
|
81 |
— |
— |
— |
— |
PDF
|
| ICEYE Gen4 SAR Satellite |
ICEYE
|
85 |
— |
— |
— |
Sun-synchronous LEO, ~500-620 km altitud |
— |
| GHOSt |
Orbital Sidekick
|
91.4 |
— |
— |
— |
— |
— |
| iQPS SAR Microsatellite Constellation |
iQPS (Institute for Q-shu Pioneers of Space)
|
100 |
— |
— |
— |
— |
— |
| ICEYE SAR Satellite Constellation |
ICEYE
|
100 |
— |
— |
— |
— |
— |
| CAST Small Satellite Platforms |
China Academy of Space Technology (CAST)
|
100 |
— |
— |
— |
— |
— |
| RapidCube-100 |
Rapid Cubes GmbH
|
100 |
100 |
— |
860 |
— |
— |
| Condor |
Muon Space
|
100 |
20000 |
— |
— |
— |
— |
| Acadia SAR Satellite Constellation |
Capella Space
|
100 |
— |
— |
— |
525 km SSO |
— |
| Ocean monitoring hyperspectral satellite |
Zhongke Xingchen
|
100 |
— |
— |
— |
— |
— |
| SIGI Satellite Mission |
Reflex Aerospace
|
109 |
330 |
— |
— |
510 km Sun Synchronous Orbit (~97,4° inc |
— |
| METEORITE Satellite Bus |
Moog Space Defense Group
|
120 |
150 |
28 |
711.2 |
— |
PDF
|
| Pallada Microsatellite Platform |
SPUTNIX
|
120 |
500 |
27 |
— |
LEO, 500–800 |
PDF
|
| Excelsior |
Terran Orbital
|
125 |
500 |
— |
— |
— |
PDF
|
| Mineral Monitoring Satellite Series |
Zhongke Xingchen
|
130 |
— |
— |
— |
— |
— |
| High-resolution agricultural and forestry monitoring satellite series |
Zhongke Xingchen
|
130 |
— |
— |
— |
— |
— |
| VSP-150 Versatile Satellite Platform |
Aerospacelab
|
136 |
— |
— |
1140 |
LEO / SSO, ~525 km |
PDF
|
| Orbital Test Bed (OTB) Satellite |
General Atomics Electromagnetic Systems
|
139 |
150 |
— |
2462 |
720 km circular altitude, 24° inclinatio |
PDF
|
| MIRI Earth Observation Satellite |
Reflex Aerospace
|
145 |
600 |
— |
— |
500 km Sun Synchronous Orbit |
— |
| Multipurpose Satellite Platform |
Beyond Gravity (ex-RUAG Space)
|
150 |
1000 |
— |
— |
— |
PDF
|
| OneWeb Satellite (Gen 1) |
Airbus OneWeb Satellites
|
150 |
— |
— |
— |
LEO, ~1,200 km altitude |
— |
| MP42 Microsatellite Bus |
NanoAvionics
|
150 |
— |
— |
— |
— |
— |
| Wide-field methane series satellites |
Zhongke Xingchen
|
150 |
— |
— |
— |
— |
— |
| Carbon dioxide series satellites |
Zhongke Xingchen
|
150 |
— |
— |
— |
— |
— |
| Sich-2-1 (Sich-2-30) |
Yuzhnoye Design Bureau
|
155 |
— |
— |
— |
— |
— |
| NeuSAR SAR Microsatellite |
SSTL (Singapore Space and Technology Ltd / DSO National Laboratories)
|
160 |
— |
— |
— |
— |
— |
| BIG CAT 300 |
Space Inventor ApS
|
170 |
500 |
— |
— |
— |
— |
| Mini4EO |
Indra Sistemas
|
190 |
400 |
— |
1550 |
— |
— |
| Mini4EO Satellite Platform |
Deimos Space (Indra)
|
190 |
400 |
— |
1550 |
— |
— |
| MicroSat-M |
Yuzhnoye Design Bureau
|
195 |
— |
— |
— |
— |
— |
| DEEPSPACE-2 |
AstroForge
|
200 |
2000 |
— |
— |
— |
— |
| DeepSpace bus |
AstroForge
|
200 |
2000 |
— |
— |
— |
— |
| HAWK HEAVY |
Argotec Srl
|
200 |
— |
— |
— |
— |
— |
| SITAEL S-200 — All-Electric Minisatellite Platform |
STRIVING
|
200 |
— |
— |
— |
— |
PDF
|
| CAST 2000 Satellite Platform |
Shenzhen Aerospace Dongfanghong Satellite
|
200 |
1000 |
— |
— |
— |
— |
| Gaofen series satellites |
Zhongke Xingchen
|
200 |
— |
— |
— |
— |
— |
| Standard Small Satellite Buses (6U, 8U, 12U, 16U CubeSats and Microsatellites) |
NanoAvionics
|
200 |
— |
— |
— |
— |
— |
| BIG CAT 600 |
Space Inventor ApS
|
230 |
750 |
— |
— |
— |
— |
| Taijing-3/01 satellite |
MinoSpace
|
240 |
— |
— |
— |
— |
— |
| Viewpoint imaging satellite |
SpaceFab.US, Inc.
|
250 |
— |
— |
— |
320 km |
— |
| Nebula |
Terran Orbital
|
250 |
1000 |
— |
820 |
— |
PDF
|
| Sich-3-O |
Yuzhnoye Design Bureau
|
290 |
— |
— |
— |
— |
— |
| GeoMicroSat (GMS) Satellite Platform |
Princeton Satellite Systems
|
292 |
4400 |
— |
— |
— |
PDF
|
| VSP-300 Versatile Satellite Platform |
Aerospacelab
|
300 |
— |
— |
— |
LEO / SSO |
PDF
|
| Astranis UtilitySat |
Astranis Space Technologies
|
300 |
— |
— |
— |
Geostationary (GEO) |
— |
| Astranis Prime (MicroGEO) |
Astranis Space Technologies
|
300 |
— |
— |
— |
Geostationary (GEO) |
— |
| Taijing-3/04 satellite |
MinoSpace
|
310 |
— |
— |
— |
— |
— |
| Taijing-4/01 satellite |
MinoSpace
|
350 |
— |
— |
— |
— |
— |
| Twinspector Earth Observation Constellation |
Reflex Aerospace
|
350 |
715 |
— |
— |
500 km Sun Synchronous Orbit |
— |
| MicroGEO Satellite |
Astranis Space Technologies
|
400 |
— |
— |
— |
Geostationary (GEO, 35,786 km) |
— |
| Griffin Lunar Lander |
Astrobotic Technology
|
430 |
— |
— |
— |
— |
— |
| ESPAStar |
Northrop Grumman Space Systems
|
430 |
3000 |
— |
— |
— |
PDF
|
| SpaceEye-X Commercial EO Satellites |
Satrec Initiative
|
500 |
— |
— |
— |
SSO at 500 km |
— |
| CAS500 (Compact Advanced Satellite 500) |
KAI (Korea Aerospace Industries)
|
500 |
— |
— |
— |
— |
— |
| NEXTAR |
NEC Space Technologies
|
500 |
— |
— |
— |
— |
— |
| HummingSat |
SWISSto12
|
500 |
3500 |
— |
— |
Geostationary (GEO) |
PDF
|
| Enterprise |
Terran Orbital
|
500 |
2000 |
— |
— |
— |
PDF
|
| Ambassador |
Terran Orbital
|
500 |
1500 |
— |
— |
— |
PDF
|
| Kuiper Satellite |
Amazon (Project Kuiper)
|
537 |
— |
— |
— |
— |
— |
| Astranis Omega |
Astranis Space Technologies
|
650 |
— |
— |
— |
Geostationary (GEO) |
— |
| Telesat Lightspeed LEO Satellite |
Thales Alenia Space
|
700 |
— |
— |
— |
— |
— |
| Galileo Navigation Satellite Manufacturing |
OHB SE
|
733 |
— |
— |
— |
— |
— |
| SmartMEO |
OHB System AG
|
733 |
— |
— |
— |
Medium Earth Orbit (MEO), ~23,616 km, 56 |
PDF
|
| SEOSat-Ingenio |
INTA — Instituto Nacional de Tecnica Aeroespacial
|
750 |
— |
— |
— |
— |
— |
| SmartLEO |
OHB System AG
|
770 |
— |
— |
— |
Low Earth Orbit (LEO), including Sun-Syn |
PDF
|
| ULTRA Lunar Lander |
ispace
|
1000 |
— |
— |
— |
— |
— |
| RESILIENCE Lunar Lander (Series 1) |
ispace
|
1000 |
— |
— |
— |
— |
PDF
|
| SAOCOM SAR Satellite |
INVAP
|
1600 |
— |
— |
— |
Sun-synchronous LEO (~620 km) |
— |
| Sich-3-R |
Yuzhnoye Design Bureau
|
1800 |
— |
— |
— |
— |
— |
| SmartLEO Agile (SARah) |
OHB System AG
|
1900 |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| Nova-C Lunar Lander |
Intuitive Machines
|
1900 |
— |
— |
— |
— |
— |
| COSMO-SkyMed Satellite Manufacturing |
OHB Italia S.p.A.
|
2200 |
— |
— |
— |
— |
— |
| Optus (satellite) series |
Optus
|
2350 |
— |
— |
— |
— |
— |
| Observation Satellites (ALOS-4, ALOS-3, ALOS-2, GOSAT-GW, GOSAT-2, GOSAT, Himawari-8, Himawari-9, MTSAT-2/Himawari-7, AD |
Mitsubishi Electric (Space Division)
|
3000 |
5300 |
— |
— |
— |
— |
| Satellite Platform DS2000 |
Mitsubishi Electric (Space Division)
|
3000 |
15000 |
— |
— |
— |
— |
| SmallGEO |
OHB System AG
|
3200 |
3000 |
— |
— |
Geostationary Earth Orbit (GEO) |
PDF
|
| Heinrich Hertz (H2Sat) Platform |
OHB System AG
|
3408 |
— |
— |
— |
Geostationary Earth Orbit (GEO) |
— |
| DFH-4E Commercial GEO Satellite Platform |
DFH Satellite Co., Ltd.
|
4600 |
6000 |
— |
— |
— |
— |
| DFH-4 GEO Communications Satellite Bus |
China Academy of Space Technology (CAST)
|
5200 |
8000 |
— |
— |
— |
— |
| DFH-4 Geostationary Satellite Platform |
China Academy of Space Technology (CAST)
|
5200 |
10500 |
— |
— |
Geostationary |
— |
| Spacebus NEO |
Thales Alenia Space
|
7600 |
20000 |
— |
— |
Geostationary orbit |
— |
| 0.3U Satellite |
Apogeo Space
|
— |
6 |
— |
— |
— |
— |
| 12U Cubesat Platform |
Orbital Systems
|
— |
100 |
— |
— |
— |
— |
| 12U SUPERNOVA CubeSat Bus |
Pumpkin, Inc.
|
— |
105 |
3.3–30 |
— |
12U CubeSat |
PDF
|
| 16U CubeSat Platform |
U-Space
|
— |
200 |
— |
— |
16U CubeSat |
PDF
|
| 16U Satellite Bus Platform |
Nara Space
|
— |
— |
— |
— |
16U |
PDF
|
| 1U, 3U, 6U CubeSat Platform |
Apogeo Space
|
— |
3 |
— |
— |
1U, 3U, 6U (CubeSat Specification) |
— |
| 3U CubeSat Platform |
Kairo Space
|
— |
— |
— |
— |
3U CubeSat |
PDF
|
| 3U PLATFORM |
Alén Space
|
— |
180 |
— |
— |
— |
PDF
|
| 6U PLATFORM |
Alén Space
|
— |
180 |
— |
— |
— |
PDF
|
| 6U SUPERNOVA CubeSat Bus |
Pumpkin, Inc.
|
— |
68 |
3.3–30 |
— |
6U CubeSat |
PDF
|
| 6U–8U CubeSat Platform |
Spacemanic s.r.o.
|
— |
— |
— |
— |
6U or 8U CubeSat |
PDF
|
| 8U Bio-Platform |
Kairo Space
|
— |
— |
— |
— |
8U CubeSat |
PDF
|
| A16 — 16U CubeSat Platform |
Akula Tech
|
— |
144 |
— |
— |
16U CubeSat (expandable to 30U) |
— |
| Aalto-2 |
Aalto University
|
— |
— |
— |
— |
2U CubeSat |
— |
| ADRAS-J Debris Assessment Mission |
Astroscale US
|
— |
— |
— |
— |
Low Earth Orbit (same orbit as target de |
— |
| AI-MotherBox-1 |
Phemotron Systems
|
— |
— |
— |
— |
12U CubeSat |
— |
| ALEASAT |
UBC Orbit (University of British Columbia)
|
— |
— |
— |
— |
1U CubeSat |
— |
| ALEASAT |
Simon Fraser University
|
— |
— |
— |
— |
1U CubeSat |
— |
| Alén Space Platforms |
Alén Space
|
— |
0.8 |
— |
— |
— |
PDF
|
| Aquarius 1U CubeSat |
Skyline Celestial
|
— |
— |
— |
— |
1U CubeSat |
— |
| ARROW 150 Satellite Bus |
Airbus OneWeb Satellites
|
— |
250 |
— |
— |
— |
PDF
|
| Astrocast IoT Satellite Network |
Astrocast
|
— |
— |
— |
— |
3U–6U CubeSats |
— |
| AX Satellite Platform Family (AX-03/06/12) |
HEX20
|
— |
48 |
— |
— |
— |
— |
| AX-03 |
HEX20
|
— |
48 |
— |
— |
— |
— |
| AX-06 |
HEX20
|
— |
48 |
— |
— |
— |
— |
| AX-12 |
HEX20
|
— |
48 |
— |
— |
— |
— |
| BJ3N3 Satellite |
Twenty First Century Aerospace Technology
|
— |
— |
— |
— |
Sun-synchronous, 97.942° |
— |
| Black Kite-1 |
Rapidtek Technologies
|
— |
— |
— |
— |
SSO |
— |
| BRO Nanosatellite Constellation |
Unseenlabs
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| Cleon I |
NPK Barl
|
— |
4 |
3.3–5 |
— |
— |
— |
| Comet Mini |
Apex
|
— |
6000 |
— |
— |
— |
— |
| Condor-Ultra |
Muon Space
|
— |
20000 |
— |
— |
— |
— |
| CubeSat 6U Platform |
IMT (Ingegneria Marketing Technologies)
|
— |
10 |
— |
— |
— |
— |
| CUBIC-16 |
Modularity Space
|
— |
— |
— |
— |
16U CubeSat bus |
— |
| DFH-4 / DFH-4E GEO Satellite Platform |
China Academy of Space Technology (CAST)
|
— |
8000 |
— |
— |
GEO (geostationary) |
— |
| DINK-N MicroSat Series |
HEX20
|
— |
100 |
— |
— |
— |
— |
| Dove Satellite |
Planet Labs PBC
|
— |
— |
— |
— |
3U CubeSat (~4 kg) |
— |
| Dragonfly Bus |
Dragonfly Aerospace
|
— |
800 |
28–48 |
— |
— |
PDF
|
| E-Space LEO Satellite Constellation |
E-Space
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| ElaraSat Platform |
Gilmour Space Technologies
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| Elevation Spacecraft Product Line |
BAE Systems
|
— |
850 |
— |
— |
— |
PDF
|
| EROS Earth Observation Satellites |
Elbit Systems Space
|
— |
— |
— |
— |
SSO at ~500 km |
— |
| ESTCube-2 |
University of Tartu
|
— |
— |
— |
— |
3U CubeSat |
— |
| EXA KRATOS 1U CubeSat Platform |
EXA (Ecuadorian Space Agency)
|
— |
100 |
— |
— |
— |
PDF
|
| Faraday Phoenix Hosted Payload Satellite |
In Space Missions
|
— |
1 |
— |
— |
— |
— |
| FAST 1U Nanosatellite |
Cervos Space
|
— |
— |
— |
— |
CubeSat |
— |
| FAST 2U Nanosatellite |
Cervos Space
|
— |
— |
— |
— |
CubeSat |
— |
| FAST 3U Nanosatellite |
Cervos Space
|
— |
— |
— |
— |
CubeSat |
— |
| FAST 6U Nanosatellite |
Cervos Space
|
— |
— |
— |
— |
CubeSat |
— |
| Flamingo Satellite Constellation |
Vyoma GmbH
|
— |
— |
— |
— |
SSO 10:30 AM |
— |
| FOSSASat |
Fossa Systems
|
— |
30 |
— |
— |
— |
— |
| FRAME Max |
EnduroSat
|
— |
10000 |
— |
— |
— |
— |
| FreeForm Microsatellite Platform |
U-Space
|
— |
250 |
— |
— |
— |
PDF
|
| GEN-1P Reentry Capsule & PocketQube Satellite |
Genesis SFL (Genesis Space Flight Laboratories)
|
— |
0.43 |
— |
67 |
— |
— |
| Gen-3 |
BlackSky
|
— |
— |
— |
— |
Mid-inclined orbit, collecting between 6 |
— |
| Geoscan 16U CubeSat Platform (InnoSat16) |
Geoscan
|
— |
45 |
10.5–12.6 |
454 |
— |
— |
| Geoscan 3U |
Geoscan
|
— |
2 |
— |
340.5 |
— |
PDF
|
| Geoscan Educational CubeSat Kit |
Geoscan
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
PDF
|
| German Orbital Systems Satellite Platforms |
German Orbital Systems
|
— |
24 |
— |
— |
— |
— |
| GOKTURK-Y Earth Observation Satellite Development Program |
Turkish Aerospace Industries (TUSAS/TAI)
|
— |
— |
— |
— |
Sun Synchronous Orbit at ~700 km |
— |
| GomSpace 6U Platform Kit |
GomSpace
|
— |
— |
— |
— |
6U CubeSat |
PDF
|
| GPS III Satellite |
Lockheed Martin Space
|
— |
— |
— |
— |
MEO (~20,200 km) |
— |
| GRail Space Laser Art and Advertising |
Avant Space
|
— |
100 |
— |
— |
— |
— |
| Heimdallr 6U CubeSat |
Ragnarok Industries
|
— |
— |
— |
— |
6U CubeSat |
— |
| Hello Space Istanbul PocketQube Satellite |
Hello Space
|
— |
— |
— |
— |
PocketQube (5 × 5 × 5 cm) |
— |
| Hosted Payload Satellite Service |
Loft Orbital
|
— |
— |
— |
— |
LEO sun-synchronous |
— |
| HYPSO-1 |
Orbit NTNU
|
— |
— |
— |
— |
6U CubeSat |
— |
| Inovor 6U Small Satellite Platform |
Inovor Technologies
|
— |
— |
— |
— |
6U CubeSat class |
PDF
|
| IOS CubeSat 3.0 Kit |
Interorbital Systems
|
— |
4 |
— |
— |
1U to 6U |
— |
| JiLin-1 Commercial EO Constellation |
Changguang Satellite (CGST)
|
— |
— |
— |
— |
SSO at 500–535 km |
— |
| Jilin-1 Earth Observation Satellite Constellation |
Changguang Satellite (CGST)
|
— |
— |
— |
— |
LEO |
— |
| K2 Large GEO Satellite Bus |
K2 Space
|
— |
15000 |
— |
— |
— |
— |
| Kineis Satellite IoT Network |
Kineis
|
— |
0.1 |
— |
— |
— |
— |
| KSF Space CubeSat Kit V2.0 |
KSF Space Foundation
|
— |
— |
— |
— |
1U CubeSat |
PDF
|
| Lantern |
Basalt Technologies
|
— |
— |
— |
— |
16U |
— |
| Lantern Custom |
Basalt Technologies
|
— |
— |
— |
— |
16U |
— |
| LEMUR |
Spire Global
|
— |
25.5 |
— |
— |
Low Earth orbit, approximately 400-650 k |
— |
| LEO Aries |
Apex
|
— |
175 |
— |
— |
— |
— |
| LEOS-100 |
Berlin Space Technologies
|
— |
154 |
— |
— |
— |
PDF
|
| LEOS-50 |
Berlin Space Technologies
|
— |
160 |
— |
— |
— |
PDF
|
| Lunar Pathfinder |
SSTL (Surrey Satellite Technology)
|
— |
— |
— |
— |
Elliptical Lunar Frozen Orbit (ELFO) |
PDF
|
| M-1000 Satellite Bus |
Momentus Space
|
— |
3000 |
— |
— |
— |
PDF
|
| MAC-150 Microsatellite Bus Platform |
Magellan Aerospace
|
— |
— |
— |
— |
LEO |
PDF
|
| Mega Class Satellite Platform |
K2 Space
|
— |
10000 |
— |
— |
— |
— |
| MicroOrbiter-1 |
MicroOrbiter
|
— |
— |
— |
— |
Low Earth Orbit (LEO), approximately 400 |
PDF
|
| Millennium Space Systems Small Satellite Systems |
Millennium Space Systems
|
— |
500 |
— |
— |
— |
PDF
|
| MoI Satellite (Multispectral on-board Intelligence) |
TakeMe2Space
|
— |
120 |
— |
— |
— |
— |
| MuSat XL |
Muon Space
|
— |
1000 |
— |
— |
— |
— |
| Nano Satellite |
Data Patterns (India) Ltd.
|
— |
— |
— |
— |
PC104 |
— |
| Nanosatellite Platform of CubeSat 3U Format |
Samara University
|
— |
— |
3.3–14 |
— |
— |
— |
| NaraSpace Satellite Platforms |
Nara Space
|
— |
— |
— |
— |
6U |
PDF
|
| NarSha — Hyperspectral & Methane Detection Satellite (16U) |
Nara Space
|
— |
— |
— |
— |
16U |
PDF
|
| NEMO-HD Microsatellite |
SPACE-SI (Slovenian Centre of Excellence for Space Sciences and Technologies)
|
— |
770.9 |
— |
— |
— |
— |
| NEO — Near Earth Orbiter VLEO Earth Observation Constellation |
Skeyeon
|
— |
— |
— |
— |
VLEO (Very Low Earth Orbit), ~250 km alt |
PDF
|
| NEO-1 |
NewOrbit Space
|
— |
200 |
— |
— |
— |
— |
| Next-Generation LEO Broadband Communication Satellite |
Hongqing Technology (鸿擎科技)
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| Nightjar |
Rapidtek Technologies
|
— |
— |
— |
— |
SSO |
— |
| NUTS (NTNU Test Satellite) |
NTNU SmallSat Lab
|
— |
— |
— |
— |
2U CubeSat |
— |
| NX-50 |
HEX20
|
— |
100 |
— |
— |
— |
— |
| Observer |
Basalt Technologies
|
— |
— |
— |
— |
3U |
— |
| Observer — Multispectral Earth Observation Satellite (16U) |
Nara Space
|
— |
— |
— |
— |
16U |
PDF
|
| ODALISS |
Emxys
|
— |
8 |
— |
— |
— |
PDF
|
| Odyssey 1U CubeSat |
Skyline Celestial
|
— |
— |
— |
— |
1U CubeSat |
— |
| Ofeq Reconnaissance Satellite Series |
Israel Aerospace Industries (IAI)
|
— |
— |
— |
— |
Retrograde LEO (westward launch) |
— |
| OPTSAT-3000 Earth Observation Satellite |
Israel Aerospace Industries (IAI)
|
— |
— |
— |
— |
Sun-synchronous LEO (~600 km) |
— |
| OPTSAT-3000 Electro-Optical Satellite |
Elbit Systems Space
|
— |
— |
— |
— |
Sun-synchronous LEO |
— |
| ORB-3 — 3U CubeSat Satellite Platform |
OrbAstro
|
— |
160 |
— |
— |
3U CubeSat |
— |
| ORB-6 — 6U CubeSat Satellite Platform |
OrbAstro
|
— |
400 |
— |
— |
6U CubeSat |
— |
| ORB-8 / ORB-16 — Mid-size Nanosatellite Platform |
OrbAstro
|
— |
14 |
— |
— |
LEO (12+ yr), MEO (5 yr), GEO (10+ yr) |
— |
| OrbAstro Technologies |
OrbAstro
|
— |
2000 |
— |
— |
— |
— |
| OrbiCraft-Pro 1U CubeSat Platform |
SPUTNIX
|
— |
— |
7.4 |
113.5 |
1U CubeSat |
PDF
|
| OrbiCraft-Pro 3U CubeSat Platform |
SPUTNIX
|
— |
0.6 |
7.4 |
340.5 |
3U CubeSat |
PDF
|
| OrbiCraft-Pro 3U Experimental (SXC3) |
SPUTNIX
|
— |
— |
— |
— |
3U CubeSat |
PDF
|
| Orbot-1 & Orbot-2 |
Rogue Space Systems Corp.
|
— |
— |
— |
— |
200 kg bus / up to 100 kg payload |
— |
| Orbot™-3 / Waypoint™-1 |
Rogue Space Systems Corp.
|
— |
— |
— |
— |
SSO |
— |
| OreSat0 |
OreSat (Portland State Aerospace Society)
|
— |
— |
7.2 |
— |
1U CubeSat |
— |
| OreSat0.5 |
OreSat (Portland State Aerospace Society)
|
— |
— |
— |
— |
2U CubeSat |
— |
| OTP-2 |
Rogue Space Systems Corp.
|
— |
— |
— |
— |
8U CubeSat |
— |
| OTP-2B |
Rogue Space Systems Corp.
|
— |
— |
— |
— |
8U / 16 kg |
— |
| Phantom |
Deployable Space Systems (DSS) — now Redwire
|
— |
25 |
— |
1800 |
— |
— |
| PHOENIX 2 |
ATMOS Space Cargo
|
— |
50 |
— |
— |
— |
— |
| QPS-SAR |
iQPS (Institute for Q-shu Pioneers of Space)
|
— |
2000 |
— |
— |
— |
— |
| RapidCube-20 CubeSat Bus |
Rapid Cubes GmbH
|
— |
15 |
— |
440 |
400–500 km SSO |
— |
| RapidCube-50 |
Rapid Cubes GmbH
|
— |
30 |
— |
— |
— |
— |
| RapidCube-6 CubeSat Bus |
Rapid Cubes GmbH
|
— |
10 |
— |
450 |
— |
— |
| RTU — Remote Terminal Unit |
Terma
|
— |
15 |
20–100 |
— |
— |
— |
| S-CORE Ultra-Small Satellite Bus |
ArkEdge Space
|
— |
— |
— |
— |
1U–3U CubeSat |
— |
| SabreSat |
Deployable Space Systems (DSS) — now Redwire
|
— |
5000 |
— |
— |
— |
— |
| SASSI2 (Student Aerothermal Spectrometer Satellite of Illinois and Indiana) |
Purdue University
|
— |
— |
— |
— |
CubeSat (Purdue CubeSat Lab standard bus |
— |
| Satellite Platform CubeSat 1U |
SPUTNIX
|
— |
0.25 |
— |
113 |
— |
— |
| Satellite Platform CubeSat 3U |
SPUTNIX
|
— |
1 |
— |
340.5 |
— |
— |
| Satellite Platform CubeSat 3U for Complex Missions |
SPUTNIX
|
— |
2 |
— |
340.5 |
— |
— |
| Satellite Platform CubeSat 6U |
SPUTNIX
|
— |
4 |
— |
340.5 |
— |
— |
| Satellite platform OrbiCraft-Pro 3U modification "Experimental" |
SPUTNIX
|
— |
0.6 |
5 |
340.5 |
— |
PDF
|
| Satellite platform OrbiCraft-Pro 3U modification "Flight" |
SPUTNIX
|
— |
1.5 |
5 |
340.5 |
— |
PDF
|
| Satellite platform OrbiCraft-Pro 3U modification "Profi" |
SPUTNIX
|
— |
1.5 |
5 |
340.5 |
— |
PDF
|
| Satellite Platform SXC6 ADC (SXC6-ADC) |
SPUTNIX
|
— |
— |
— |
— |
6U |
— |
| Satellite Platform SXC6 Basic (SXC6-VOL) |
SPUTNIX
|
— |
— |
— |
— |
6U |
PDF
|
| Satellite Platform SXC6 RS (OrbiCraft-Pro 6U) |
SPUTNIX
|
— |
— |
— |
— |
6U |
PDF
|
| SatFab 3U CubeSat with Novel Phase Change Material Thermal Control System |
University of Maryland
|
— |
— |
— |
— |
Lower Earth Orbit (via ISS deployment) |
— |
| Scientific Experimental Satellite |
Hongqing Technology (鸿擎科技)
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| SCOT |
Digantara
|
— |
— |
— |
— |
Sun-synchronous LEO |
— |
| SG3 CubeSat Platform (4U / 16U) |
SPUTNIX
|
— |
— |
— |
454 |
CubeSat 4U / 16U |
PDF
|
| Silta |
ReOrbit
|
— |
— |
— |
— |
Geostationary (GEO), small-class |
— |
| SITRO-AIS Maritime Monitoring Constellation |
SITRONICS Space
|
— |
— |
— |
— |
3U CubeSat (4 kg each) |
— |
| Skykraft Block 2 ATM Satellite |
Skykraft
|
— |
— |
— |
— |
LEO |
— |
| SkySat Satellite |
Planet Labs PBC
|
— |
— |
— |
— |
~450 km, mixed inclinations |
— |
| Small Geostationary Satellites |
AscendArc
|
— |
— |
— |
— |
Geostationary (GEO) |
— |
| Small Size GEO Satellite Platform (Full-Electric HTS) |
Turkish Aerospace Industries (TUSAS/TAI)
|
— |
— |
— |
— |
GEO |
PDF
|
| Space INSPIRE |
Thales Alenia Space
|
— |
— |
— |
— |
Geostationary orbit |
— |
| Space-Based Solar Power Demonstration Satellite |
Cowboy Space Corporation (formerly Aetherflux)
|
— |
1000 |
— |
— |
— |
— |
| SpaceSail LEO Broadband Satellite |
Shanghai Spacecom (SSST / SpaceSail)
|
— |
— |
— |
— |
LEO (various altitudes) |
— |
| SpaceSight-X Optical Earth Observation Satellite |
Satrec Initiative
|
— |
— |
— |
— |
Sun-synchronous (SSO) |
— |
| SSTL-CUBE |
SSTL (Surrey Satellite Technology)
|
— |
— |
— |
— |
12U (Cube-Vista EO) / 8U (Cube-Signal co |
PDF
|
| SSTL-MINI |
SSTL (Surrey Satellite Technology)
|
— |
2000 |
— |
— |
Low Earth Orbit |
PDF
|
| Standard CubeSat and Microsatellite Buses |
NanoAvionics
|
— |
— |
— |
— |
12U CubeSat |
— |
| Standard CubeSat Satellite Bus |
NanoAvionics
|
— |
— |
— |
— |
6U CubeSat |
— |
| Standard CubeSat Satellite Bus (6U, 8U, 12U, 16U) |
NanoAvionics
|
— |
— |
— |
— |
16U CubeSat |
— |
| Stara Relay Constellation |
Stara Space
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| Stingray Satellite Constellation |
EOI Space (Earth Observant)
|
— |
— |
— |
— |
Very Low Earth Orbit (VLEO) |
— |
| STRaND-2 CubeSat Rendezvous Demonstrator |
University of Strathclyde
|
— |
— |
— |
— |
10 x 10 x 34 cm |
— |
| SUCHAI-3 |
Universidad de Chile – SPEL (Space and Planetary Exploration Laboratory)
|
— |
— |
— |
— |
3U CubeSat |
— |
| SXC12 12U CubeSat Platform |
SPUTNIX
|
— |
50 |
6–8.4 |
366 |
12U CubeSat |
— |
| SXC6 6U CubeSat Platform |
SPUTNIX
|
— |
15 |
6–8.4 |
366 |
6U CubeSat |
PDF
|
| TabletSat Platform |
SPUTNIX
|
— |
— |
— |
— |
1U CubeSat |
— |
| Taurus 3U — CubeSat Satellite Platform |
Satoro
|
— |
18 |
— |
— |
3U CubeSat |
— |
| TechnoSat |
TU Berlin — Chair of Space Technology
|
— |
— |
— |
— |
LEO 500 km SSO |
— |
| TEPHRA-TESSEL |
NPC Spacemind
|
— |
135 |
— |
— |
— |
— |
| TET Satellite Family (TET-X / TET-XL) |
OHB System AG
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
PDF
|
| TheOrbiter — LEO Inspection Nanosatellite |
SpaceAble
|
— |
— |
— |
— |
Low Earth Orbit (LEO) |
— |
| Triton-X — Modular Smallsat Bus (40–250 kg) |
LuxSpace
|
— |
9 |
— |
— |
— |
— |
| ULTRA300 RH — 300K LUT Radiation-Hardened FPGA |
NanoXplore
|
— |
— |
1.2–3.3 |
— |
— |
— |
| UMsat CubeSat |
University of Massachusetts Amherst
|
— |
— |
— |
— |
1U (10 cm x 10 cm x 10 cm modular unit) |
— |
| UNSW-EC0 (Australia's First CubeSat) |
UNSW Canberra Space
|
— |
— |
— |
— |
1U CubeSat |
— |
| Ut ProSat-1 |
Virginia Tech
|
— |
— |
— |
— |
3U CubeSat |
— |
| Vast Satellite (15 kW-class satellite bus) |
Vast Space
|
— |
— |
— |
3600 |
— |
PDF
|
| ViaSat-3 GEO Broadband Constellation |
Viasat, Inc.
|
— |
— |
— |
— |
Geostationary (GEO) |
— |
| WISeSat — Post-Quantum Secure LEO IoT Satellite Constellation |
SEALSQ / WISeSat
|
— |
— |
— |
— |
LEO, 450–600 km, near-polar SSO (~97.4° |
— |
| WorldView Legion Constellation |
Vantor
|
— |
— |
— |
— |
SSO |
— |
| X-Sat Mercury Class Microsat Platform |
Blue Canyon Technologies
|
— |
108 |
— |
— |
— |
PDF
|
| Zorkiy-2M Earth Observation Constellation |
SITRONICS Space
|
— |
— |
— |
— |
12U CubeSat (24 kg) |
— |
| μDragonfly Bus |
Dragonfly Aerospace
|
— |
140 |
24.3–32.4 |
— |
— |
PDF
|