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Cubesat
e-st@r
e-st@r
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American low-cost nanosatellite bus. Used in dozens of launches.

AKA: See list. Status: Operational 2003. First Launch: 2003-06-30. Last Launch: 2015-11-04. Number: 346 . Gross mass: 1.00 kg (2.20 lb). Height: 0.0100 m (0.0320 ft). Span: 0.0100 m (0.0320 ft).

Employing ultra-small satellite technology invented by Stanford University, CubeSats provided a satellite that could be placed into Earth orbit for under $ 100,000. The Cubesat bus measured 10 centimeters on a side, and weighed less than one kilogram. The CubeSat microsatellite was a perfect cube, holding its experiments inside like shelves in a cupboard. A CubeSat microsatellite could hold anything, from microgravity experiments to the ashes of a loved one. One Stop Satellite Solutions was one company marketing the technology. They combined the CubeSat technology with their Multi-Payload Adaptor, effectively creating a launch pad in space. Scores of satellites could be launched at once.

Cubesats could be used for scientific missions (microgravity, biomedical, component testing, amateur radio) or personal (burial, photography). Users could buy the bare-bones structure, or satellites equipped with computer, communications, and the power systems to meet mission requirements.

Family: Astronomy, Biology, Communications, Earth, MX, Navigation, Science, Surveillance, Technology, Technology satellite. Country: USA. Spacecraft: ISS Japanese Experiment Module. Launch Vehicles: Antares 130, Chang Zheng 11, Chang Zheng 6, Thor, R-7, Minuteman, R-14, Proton, Antares, Kosmos 3, Proton-K, Space Shuttle, Kosmos 11K65M, Strypi, R-36M 15A14, UR-100N, Rokot, Chang Zheng 2D, PSLV, Taurus, Ariane 5, Delta 7920-10C, Dnepr, Minotaur 1, Atlas V, CZ-NGLV, H-IIA 202, Atlas V 401, Ariane 5ECA, Soyuz-2-1A, Delta 7320-10C, Falcon 1, Soyuz-2-1B, Atlas V 421, Falcon 9 v1.1, Atlas V 501, Minotaur IV, Falcon 9, Proton-M/DM-3, Taurus 3110, PSLV-XL, Vega, Antares 110. Launch Sites: Taiyuan LC16, Cape Canaveral, Baikonur, Plesetsk, Vandenberg SLC2W, Baikonur LC31, Vandenberg SLC3E, Vandenberg 576E, Vandenberg SLC4E, Cape Canaveral LC40, Cape Canaveral LC41, Cape Canaveral LC39A, Plesetsk LC132/1, Baikonur LC109, Plesetsk LC133/3, Sriharikota PSLV, Tanegashima Y, Wallops Island LA0A, Jiuquan SLS-2, Sriharikota SLP, Kwajalein OM, Wallops Island LA0B, Kourou ELV, Wallops Island LP0A. Agency: Stanford. More at: 6438. Bibliography: 2.


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Aalto 1Aalto 1
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AAU CubesatAAU Cubesat
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ADAMASatADAMASat
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PTecSatPTecSat
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Aerocube 2Aerocube 2
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Aerocube 4Aerocube 4
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Aerocube 5aAerocube 5a
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Aerocube 6aAerocube 6a
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OCSD AOCSD A
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Aerocube-8aAerocube-8a
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AggieSat 2AggieSat 2
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ALICEALICE
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ANDESITEANDESITE
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AOSATAOSAT
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ARAPAIMAARAPAIMA
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ARC 1ARC 1
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Ardusat-2Ardusat-2
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Ardusat-1Ardusat-1
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ArgusArgus
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Arkyd-6Arkyd-6
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Black Knight 1Black Knight 1
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BRICSat-PBRICSat-P
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CADRECADRE
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Mayflower-CaerusMayflower-Caerus
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Cal Poly 1UCal Poly 1U
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CanX-1CanX-1
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CanX-2CanX-2
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CanX 7CanX 7
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CANYVAL-X 1CANYVAL-X 1
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CAPE 1CAPE 1
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CAPE 2CAPE 2
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Centennial 1Centennial 1
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CeREsCeREs
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Chasqui 1Chasqui 1
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ChargerSat 1ChargerSat 1
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CHIRPCHIRP
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CHOMPTTCHOMPTT
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CinemaCinema
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CNUSail 1CNUSail 1
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Compass 1Compass 1
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COMPASS 2COMPASS 2
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ConSat 1ConSat 1
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COPPERCOPPER
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CP 1CP 1
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CP 4CP 4
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CP 3CP 3
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CP5CP5
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CP 9CP 9
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Cross in SpaceCross in Space
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CryoCube 1CryoCube 1
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CSSWECSSWE
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CSTB 1CSTB 1
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CubeBug-1CubeBug-1
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CubeSailCubeSail
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CubETHCubETH
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CUNYSAT 1CUNYSAT 1
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Cute-1.7-APD-IICute-1.7-APD-II
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Cute-1Cute-1
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Cute 1.7Cute 1.7
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CXBNCXBN
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DelFFi DeltaDelFFi Delta
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Delfi-C3Delfi-C3
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Delfi-3nXtDelfi-3nXt
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DellingrDellingr
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DeorbitSailDeorbitSail
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DICE-XDICE-X
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DISCOSAT 1DISCOSAT 1
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Dove-1Dove-1
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Dove-2Dove-2
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Dove-3Dove-3
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DragonsatDragonsat
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DTUSATDTUSAT
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Dtusat 2Dtusat 2
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Duchifat 1Duchifat 1
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E1PE1P
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EcAMSatEcAMSat
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EDSNEDSN
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ELFINELFIN
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EQUiSatEQUiSat
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ESCAPEESCAPE
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ESTCube-1ESTCube-1
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Ex-Alta 1Ex-Alta 1
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ExoCube CP10ExoCube CP10
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ExoplanetSatExoplanetSat
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F-1F-1
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FalconSat 7FalconSat 7
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FIREBIRD FU1FIREBIRD FU1
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FireflyFirefly
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First-MoveFirst-Move
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NiwakaNiwaka
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Flock 1b-10Flock 1b-10
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Fox 1EFox 1E
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FUNcube-1FUNcube-1
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GalassiaGalassia
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GASPACSGASPACS
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GEARRSatGEARRSat
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GeneSat-1GeneSat-1
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GLADOSGLADOS
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GoliatGoliat
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GOMX-1GOMX-1
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GOMX 3GOMX 3
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GOSTE 1GOSTE 1
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GRIFEXGRIFEX
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HARPHARP
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HAUSAT 1HAUSAT 1
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Hawksat 1Hawksat 1
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HeidelSatHeidelSat
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HermesHermes
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HiNCubeHiNCube
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Hoĉoponopono 2Hoĉoponopono 2
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Horyu 1Horyu 1
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Horyu 3Horyu 3
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HUMSAT-DHUMSAT-D
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IceCubeIceCube
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ICECube 1ICECube 1
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ICUBE-1ICUBE-1
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YuiYui
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CubeSatCubeSat
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INSPIRE AINSPIRE A
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InvaderInvader
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IONION
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IPEXIPEX
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ISARAISARA
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ITASAT 1ITASAT 1
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IT_-pSat 1IT_-pSat 1
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JUGNUJUGNU
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KAUSAT 5KAUSAT 5
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KickSat 1KickSat 1
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KN-Sat 1KN-Sat 1
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HayatoHayato
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KSAT 2KSAT 2
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Kumu AĈoKumu AĈo
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KUTESat PathfinderKUTESat Pathfinder
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KySat-1KySat-1
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KySat-2KySat-2
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LAICELAICE
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LambdaSatLambdaSat
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Lemur 1Lemur 1
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Libertad 1Libertad 1
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LightSail ALightSail A
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LINKLINK
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LituanicaSat-1LituanicaSat-1
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LituanicaSAT 2LituanicaSAT 2
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Litsat 1Litsat 1
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LMRSTSatLMRSTSat
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Lunar-IceCubeLunar-IceCube
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NEA-ScoutNEA-Scout
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MarCOMarCO
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MaSat-1MaSat-1
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MASTMAST
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M-CubedM-Cubed
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MEROPEMEROPE
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MicroMASMicroMAS
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MinXSSMinXSS
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MiRaTAMiRaTA
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Nanosail-DNanosail-D
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NanoSatC-Br 1NanoSatC-Br 1
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Ncube 1Ncube 1
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NEE 01 PegasoNEE 01 Pegaso
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NEE 02 KrysaorNEE 02 Krysaor
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Negai✰Negai✰
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NEUTRON 1NEUTRON 1
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NMTSatNMTSat
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Nodes 1Nodes 1
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NPS-SCATNPS-SCAT
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NUTSNUTS
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OGMS-SAOGMS-SA
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USA 219USA 219
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OPTOSOPTOS
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OPUSatOPUSat
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ORS Tech 1ORS Tech 1
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ORS-SquaredORS-Squared
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OSIRIS-3UOSIRIS-3U
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OSSI-1OSSI-1
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OUFTI 1OUFTI 1
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Outernet 1Outernet 1
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PacePace
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PATRIOTPATRIOT
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Perseus-M 1Perseus-M 1
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Perseus 000Perseus 000
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Perseus-O 1Perseus-O 1
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PharmaSat 1PharmaSat 1
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PhoneSat 1.0PhoneSat 1.0
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PhoneSat 2.0PhoneSat 2.0
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PICASSOPICASSO
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PicoDragonPicoDragon
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PlanetiQ 1PlanetiQ 1
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PolarCubePolarCube
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Politech.1Politech.1
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Polyitan 1Polyitan 1
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CPOD ACPOD A
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POPACSPOPACS
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Popsat Hip 1Popsat Hip 1
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PrintSatPrintSat
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PropSatPropSat
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ProiteresProiteres
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PrometheusPrometheus
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PSat APSat A
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PTLSPTLS
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PUCP-Sat 1PUCP-Sat 1
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PW-Sat 1PW-Sat 1
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PW-Sat 2PW-Sat 2
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QARMANQARMAN
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Qb50P1Qb50P1
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Qb50p2Qb50p2
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QBITOQBITO
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QbX 1QbX 1
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QuakeSat 1QuakeSat 1
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Quest 1Quest 1
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RAIKORAIKO
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RAMPARTRAMPART
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RAVANRAVAN
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RAX 1RAX 1
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Rincon 1Rincon 1
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RoBiSAT 1RoBiSAT 1
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ROBUSTAROBUSTA
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SACREDSACRED
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SAMSON 1SAMSON 1
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SEEDS 2SEEDS 2
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SENSE-ASENSE-A
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SERPENSSERPENS
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SIGMASIGMA
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SkyCubeSkyCube
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SkyFireSkyFire
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SMARTSatSMARTSat
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SMDC-TechSatSMDC-TechSat
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ORSESORSES
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SNAPSSNAPS
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SNUSAT 1SNUSAT 1
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SOMPSOMP
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SOMP 2SOMP 2
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SpaceBuoySpaceBuoy
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SporeSatSporeSat
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StangSatStangSat
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STEP Cube LabSTEP Cube Lab
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STF 1STF 1
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STMSat 1STMSat 1
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STRaND-1STRaND-1
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STRaND 2STRaND 2
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StudsatStudsat
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Supernova-BetaSupernova-Beta
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SwampSatSwampSat
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SwayamSwayam
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SwissCubeSwissCube
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TechEdSatTechEdSat
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TechEdSat 3pTechEdSat 3p
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TechCube 1TechCube 1
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TigrisatTigrisat
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TINYSCOPETINYSCOPE
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Tisat 1Tisat 1
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ORS-3ORS-3
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Trailblazer 1Trailblazer 1
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Triton 1Triton 1
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TSatTSat
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Turksat-3USATTurksat-3USAT
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UAPSat 1UAPSat 1
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Ukube 1Ukube 1
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AlmasatAlmasat
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USS LangleyUSS Langley
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UWE-1UWE-1
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Velox 1Velox 1
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VELOX 2VELOX 2
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VELOX P1VELOX P1
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Vermont Lunar CubesaVermont Lunar Cubesa
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Waseda-SAT2Waseda-SAT2
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We WishWe Wish
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WRENWREN
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XaTcobeoXaTcobeo
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XI 4XI 4
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YamSat 1AYamSat 1A
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ZACUBE 1ZACUBE 1
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Rax-2Rax-2
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MastMast
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HiakaSatHiakaSat
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BeakerSat-1BeakerSat-1
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Nanosail-DNanosail-D
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2003 June 30 - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/3. LV Family: UR-100N. Launch Vehicle: Rokot.
  • CubeSat XI-IV - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Tokyo. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 27848 . COSPAR: 2003-031J. Apogee: 833 km (517 mi). Perigee: 818 km (508 mi). Inclination: 98.7000 deg. Period: 101.40 min. Cubesat XI carried technology tests for the University of Tokyo..
  • CanX-1 - . Mass: 1.00 kg (2.20 lb). Nation: Canada. Agency: Toronto. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 27847 . COSPAR: 2003-031H. Apogee: 831 km (516 mi). Perigee: 817 km (507 mi). Inclination: 98.7000 deg. Period: 101.40 min. 1U cubesat from the University of Toronto, carried a camera for attitude determination. Failed. No signal from spacecraft..
  • AAU Cubesat - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Agency: Aalborg. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 27846 . COSPAR: 2003-031G. Apogee: 831 km (516 mi). Perigee: 816 km (507 mi). Inclination: 98.7000 deg. Period: 101.40 min. Aalborg University successfully contacted its AAU-Cubesat nanosatellite after it was separated. It carried a 100-meter-resolution Earth imaging camera..
  • Quakesat - . Mass: 3.00 kg (6.60 lb). Nation: USA. Agency: QuakeFinder. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 27845 . COSPAR: 2003-031F. Apogee: 834 km (518 mi). Perigee: 820 km (500 mi). Inclination: 98.7000 deg. Period: 101.40 min. 3U cubesat for Stanford University/Quakesat LLC Quakesat was to be used for detection of ELF radio emissions from seismic activity. Successful..
  • Cute-1 - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: TIT. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 27844 . COSPAR: 2003-031E. Apogee: 833 km (517 mi). Perigee: 817 km (507 mi). Inclination: 98.7000 deg. Period: 101.40 min. CUTE-I carried engineering test equipment and was built by the Tokyo Institute of Technology..
  • DTUSAT - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Agency: Danish Technical University. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 27842 . COSPAR: 2003-031C. Apogee: 831 km (516 mi). Perigee: 816 km (507 mi). Inclination: 98.7000 deg. Period: 101.40 min. Danish 1U cubesat DTUSat remained silent after release despite several attempts to contact it. Carried a 450-meter copper wire tether for lowering the satellite orbit..

2005 October 27 - . 06:52 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: R-14. Launch Vehicle: Kosmos 11K65M.
  • UWE-1 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Agency: BJMU. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 28892 . COSPAR: 2005-043C. Apogee: 708 km (439 mi). Perigee: 683 km (424 mi). Inclination: 98.2000 deg. Period: 98.70 min. University of Wurzburg 1U cubesat. Released from SSETI Express. Mission: Technology / Communications. Failed. Contact lost on 17 November.
  • NCube-2 - . Mass: 1.00 kg (2.20 lb). Nation: Norway. Agency: Norsk Romsenter. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 28898 . COSPAR: 2005-043G. Apogee: 712 km (442 mi). Perigee: 684 km (425 mi). Inclination: 98.2000 deg. Period: 98.70 min. Norwegian 1U cubesat for ARR/NSC. Evidently was released from SSETI Express but no signal received..
  • Cubesat XI-V - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Tokyo. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 28895 . COSPAR: 2005-043F. Apogee: 708 km (439 mi). Perigee: 682 km (423 mi). Inclination: 98.2000 deg. Period: 98.70 min. University of Tokyo cubesat. Released from SSETI Express..

2006 December 16 - . 12:00 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA0B. LV Family: Minuteman. Launch Vehicle: Minotaur 1.
  • GeneSat-1 - . Mass: 7.00 kg (15.40 lb). Nation: USA. Agency: NASA. Manufacturer: NASA Ames. Class: Biology. Type: Biology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-04-02 . USAF Sat Cat: 29654 . COSPAR: 2006-058B. Apogee: 426 km (264 mi). Perigee: 410 km (250 mi). Inclination: 40.0100 deg. Period: 92.93 min.

    3U cubesat launched as a secondary payload. A collaboration of NASA, industry, and local universities resulted in this fully-automated, miniaturized spaceflight system that provided life support, nutrient delivery, and performed assays to monitor genetic changes of E. coli bacteria in space conditions.


2007 March 9 - . 03:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 401.
  • MEPSI Picosat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: DARPA. Manufacturer: Aerospace. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. COSPAR: 2007-006x. Apogee: 563 km (349 mi). Perigee: 558 km (346 mi). Inclination: 35.4000 deg. Released from STPSat..
  • MEPSI Picosat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: DARPA. Manufacturer: Aerospace. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. COSPAR: 2007-006x. Apogee: 563 km (349 mi). Perigee: 558 km (346 mi). Inclination: 35.4000 deg. Period: 1,436.10 min. Released from STPSat..

2007 April 17 - . 06:46 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.
  • CAPE 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: Makeyev Design Bureau. Manufacturer: Louisiana. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 31130 . COSPAR: 2007-012P. Apogee: 793 km (492 mi). Perigee: 646 km (401 mi). Inclination: 98.1000 deg. Period: 99.20 min. Cajun Advanced Picosatellite Experiment by the University of Louisiana at Lafayette..
  • Aerocube 2 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: Makeyev Design Bureau. Manufacturer: Aerospace. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 31122 . COSPAR: 2007-012F. Apogee: 771 km (479 mi). Perigee: 648 km (402 mi). Inclination: 98.1000 deg. Period: 99.00 min. 1U cubesat for Aerospace Corporation. Failed. Solar converter malfunction on 18 April 2007..
  • CSTB 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: Makeyev Design Bureau. Manufacturer: Boeing. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 31133 . COSPAR: 2007-012R. Apogee: 771 km (479 mi). Perigee: 648 km (402 mi). Inclination: 98.1000 deg. Period: 99.00 min. CubeSat TestBed for Boeing IDS/Advanced Systems, Huntington Beach, California..
  • CP 3 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: Makeyev Design Bureau. Manufacturer: Cal Poly. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 31128 . COSPAR: 2007-012M. Apogee: 793 km (492 mi). Perigee: 646 km (401 mi). Inclination: 98.1000 deg. Period: 99.20 min. California Polytechnic University cubesat, the backup for CP2 lost in a Dnepr launch failure in 2006..
  • CP 4 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: Makeyev Design Bureau. Manufacturer: Cal Poly. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 31132 . COSPAR: 2007-012Q. Apogee: 771 km (479 mi). Perigee: 648 km (402 mi). Inclination: 98.1000 deg. Period: 99.00 min. California Polytechnic University cubesat..
  • Libertad - . Mass: 1.00 kg (2.20 lb). Nation: Colombia. Agency: Makeyev Design Bureau. Manufacturer: Arboleda. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 31129 . COSPAR: 2007-012N. Apogee: 793 km (492 mi). Perigee: 646 km (401 mi). Inclination: 98.1000 deg. Period: 99.20 min. Picosat built and operated by the Universidad Sergio Arboleda, Bogota, Colombia..
  • MAST - . Mass: 3.00 kg (6.60 lb). Nation: USA. Agency: Tethers. Manufacturer: Stanford. Class: Technology. Type: Tether technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 31126 . COSPAR: 2007-012K. Apogee: 783 km (486 mi). Perigee: 647 km (402 mi). Inclination: 98.1000 deg. Period: 99.10 min.

    Multi Application Survivable Tether experiment, built by Tethers Unlimited Inc and Stanford University. MAST consisted of the TED (Tether Deployer) satellite, with a 1 km deployable multi-strand Hoytether; RALPH, a small end mass satellite; and between them, GADGET, an inspector 1U cubesat which could move along the tether. Before deployment the MAST package fit into a 0.3 m x 0.1 m module. Failed to deploy, but radio contact made.


2008 April 28 - . 03:53 GMT - . Launch Site: Sriharikota. LV Family: PSLV. Launch Vehicle: PSLV.
  • Cute-1.7-APD-II - . Mass: 4.00 kg (8.80 lb). Nation: Japan. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 32785 . COSPAR: 2008-021C. Apogee: 635 km (394 mi). Perigee: 615 km (382 mi). Inclination: 98.0000 deg. Period: 97.20 min. 2U cubesat for Tokyo Institute of Technology. Separation system demonstration and Avalanche Photo Diode sensor experiment. Successful..
  • Compass 1 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 32787 . COSPAR: 2008-021E. Apogee: 636 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.0000 deg. Period: 97.20 min. 1U cubesat for Fachhochschule Aachen nanosat. Demonstration of commercial off-the-shelf components and taking photos. Successful..
  • AAUSat-II - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Agency: ISRO. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 32788 . COSPAR: 2008-021F. Apogee: 636 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.0000 deg. Period: 97.20 min. University of Aalborg 1U cubesat; carried a gamma ray burst detector for the Danish National Space Center. Successful..
  • Delfi-C3 - . Mass: 5.00 kg (11.00 lb). Nation: Netherlands. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 32789 . COSPAR: 2008-021G. Apogee: 636 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.0000 deg. Period: 97.20 min. Technical University of Delft 3U cubesat. On-orbit testing of thin film solar cells (TFSC) and autonomous wireless sun sensor (AWSS). Demonstrated the world's first linear amateur radio transponder on a CubeSat..
  • Can X-2 - . Mass: 2.00 kg (4.40 lb). Nation: Canada. Agency: ISRO. Class: Communications. Type: Military communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 32790 . COSPAR: 2008-021H. Apogee: 635 km (394 mi). Perigee: 615 km (382 mi). Inclination: 98.0000 deg. Period: 97.20 min. 3U cubesat for University of Toronto, Canada. Mission: Technology demonstrator for formation flying. Successful..
  • SEEDS 2 - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: ISRO. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 32791 . COSPAR: 2008-021J. Apogee: 637 km (395 mi). Perigee: 614 km (381 mi). Inclination: 98.0000 deg. Period: 97.20 min. 1U cubesat for Nihon University, Japan. Amateur radio experiments and preprogrammed message sending. Successful..

2008 August 3 - . 03:34 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein OM. LV Family: Falcon. Launch Vehicle: Falcon 1. FAILURE: The new Merlin 1C first stage engine completed its burn, but the thrust took longer to decay than expected. It was still thrusting when stage 2 tried to separate, and the two stages collided, setting the second stage tumbling..
  • Nanosail-D - . Mass: 4.00 kg (8.80 lb). Nation: USA. Agency: SpaceX. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. 3U cubesat for NASA. Technology mission..
  • PreSat - . Mass: 4.00 kg (8.80 lb). Nation: USA. Agency: SpaceX. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. 3U cubesat for NASA. Technology mission..

2009 May 18 - . 23:55 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA0B. LV Family: Minuteman. Launch Vehicle: Minotaur 1.
  • Aerocube 3 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-08-11 . USAF Sat Cat: 35005 . COSPAR: 2009-028E. Apogee: 464 km (288 mi). Perigee: 427 km (265 mi). Inclination: 40.5000 deg. Period: 93.50 min. 10-cm 1U cubesat for Aerospace Corporation..
  • Pharmasat - . Mass: 3.00 kg (6.60 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2012-08-14 . USAF Sat Cat: 35002 . COSPAR: 2009-028B. Apogee: 465 km (288 mi). Perigee: 429 km (266 mi). Inclination: 40.5000 deg. Period: 93.50 min. 3U cubesat for NASA Ames Research Center, Santa Clara University, UTMB. Measured the effect of antifungal countermeasures on yeast strains in microgravity. 96 hour experiment was successful..
  • Hawksat 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-10-06 . USAF Sat Cat: 35003 . COSPAR: 2009-028C. Apogee: 464 km (288 mi). Perigee: 428 km (265 mi). Inclination: 40.5000 deg. Period: 93.50 min. 10-cm 1U cubesat for Hawk Institute for Space Sciences..
  • CP6 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-09-04 . USAF Sat Cat: 35004 . COSPAR: 2009-028D. Apogee: 463 km (287 mi). Perigee: 427 km (265 mi). Inclination: 40.5000 deg. Period: 93.50 min. 10-cm 1U cubesat for California Polytechnic..

2009 July 15 - . 22:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Space Shuttle.
  • Dragonsat - . Mass: 3.00 kg (6.60 lb). Nation: USA. Agency: Clemson. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-03-17 . USAF Sat Cat: 35690 . COSPAR: 2009-038B. Apogee: 332 km (206 mi). Perigee: 326 km (202 mi). Inclination: 51.6000 deg. Period: 91.10 min.

    Ejected from the Endeavour on 30 July at 12:34 GMT. Dragonsat consisted of two 1.5 kg cubesats, BEVO-1 from the University of Texas at Austin and Aggiesat 2 from Texas A&M University. The two satellites were ejected attached to each other, but failed to separate as planned.


2009 September 23 - . 06:21 GMT - . Launch Site: Sriharikota. LV Family: PSLV. Launch Vehicle: PSLV.
  • SwissCube - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 35932 . COSPAR: 2009-051B. Apogee: 712 km (442 mi). Perigee: 702 km (436 mi). Inclination: 98.4300 deg. Period: 98.93 min. Cubesat from Ecole Polytechnique Federale de Lausanne, Switzerland.
  • BEESAT - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 35933 . COSPAR: 2009-051C. Apogee: 710 km (440 mi). Perigee: 703 km (436 mi). Inclination: 98.4300 deg. Period: 98.92 min. Cubesat from Technische Universitat Berlin, Germany..
  • UWE-2 - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 35934 . COSPAR: 2009-051D. Apogee: 712 km (442 mi). Perigee: 704 km (437 mi). Inclination: 98.4200 deg. Period: 98.95 min. 1U cubesat from Julius-Maximilians-Universitat Wurzburg, Germany. ADCS technology demonstrator. Successful..
  • ITU-p-SAT 1 - . Mass: 1.00 kg (2.20 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 35935 . COSPAR: 2009-051E. Apogee: 715 km (444 mi). Perigee: 704 km (437 mi). Inclination: 98.4400 deg. Period: 98.97 min. Cubesat from Istanbul Teknik Universitesi..

2010 May 20 - . 21:58 GMT - . Launch Site: Tanegashima. LV Family: H-2. Launch Vehicle: H-IIA 202.
  • Hayato - . Payload: K-SAT. Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Mitsubishi. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-06-28 . USAF Sat Cat: 36573 . COSPAR: 2010-020A. Apogee: 172 km (106 mi). Perigee: 166 km (103 mi). Inclination: 30.0000 deg. Period: 87.90 min. 1U cubesat for Kagoshima University, released in parking orbit. Failed..
  • Waseda-SAT2 - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Mitsubishi. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-07-12 . USAF Sat Cat: 36574 . COSPAR: 2010-020B. Apogee: 183 km (113 mi). Perigee: 177 km (109 mi). Inclination: 30.0000 deg. Period: 88.10 min. 1U cubesat for Waseda University, Tokyo, released in parking orbit. Status unclear..
  • Negai - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Agency: Mitsubishi. Class: Earth. Type: Earth resources satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-06-26 . USAF Sat Cat: 36575 . COSPAR: 2010-020C. Apogee: 190 km (110 mi). Perigee: 176 km (109 mi). Inclination: 30.0000 deg. Period: 88.20 min. 1U cubesat for Soka University, Tokyo, released in parking orbit. Successful,.

2010 July 12 - . 03:52 GMT - . Launch Site: Sriharikota. LV Family: PSLV. Launch Vehicle: PSLV.
  • Studsat - . Mass: 1.00 kg (2.20 lb). Nation: India. Agency: ISRO. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 36796 . COSPAR: 2010-035B. Apogee: 640 km (390 mi). Perigee: 621 km (385 mi). Inclination: 98.2000 deg. Period: 97.30 min. ISRO-sponsored Indian student-designed 1U cubesat. First Indian picosatellite..
  • Tisat 1 - . Mass: 1.00 kg (2.20 lb). Nation: Switzerland. Agency: ISRO. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 36799 . COSPAR: 2010-035E. Apogee: 639 km (397 mi). Perigee: 619 km (384 mi). Inclination: 98.2000 deg. Period: 97.30 min. Swiss student 1U cubesat for SUPSI. Successful..

2010 November 20 - . 01:25 GMT - . Launch Site: Kodiak. LV Family: Peacekeeper. Launch Vehicle: Minotaur IV.
  • USA 218 - . Payload: RAX. Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37223 . COSPAR: 2010-062B. Radio Aurora Explorer, a National Science Foundation 3U cubesat, built by the University of Michigan, to study the aurora by picking up ground-based radar signals..
  • USA 219 - . Payload: O/OREOS. Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Biology. Type: Biology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37224 . COSPAR: 2010-062C. 3U cubesat by NASA-Ames with life science experiments to study microbes in free fall and the effects of ultraviolet light on organic materials..
  • Nanosail-D - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37361 . COSPAR: 2010-062L. 3U cubesat for NASA with 3-m span solar sail; ejected from USA 220 on 18 January 2011 unexpectedly after earlier ejection efforts failed..

2010 December 8 - . 15:43 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.
  • QBX2 - . Payload: QbX-2. Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-12-31 . USAF Sat Cat: 37245 . COSPAR: 2010-066B. Apogee: 187 km (116 mi). Perigee: 173 km (107 mi). Inclination: 34.5000 deg. Period: 88.10 min. 3U cubesat built by Pumpkin Inc of San Francisco for the National Reconaissance Office's Colony-1 technology development project. Successful..
  • SMDC One - . Payload: SMDC-One. Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-12-31 . USAF Sat Cat: 37246 . COSPAR: 2010-066C. Apogee: 184 km (114 mi). Perigee: 173 km (107 mi). Inclination: 34.5000 deg. Period: 88.10 min. Operational Nanosatellite Experiment for the US Army Space and Missile Defense Center.
  • Perseus 003 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-01-06 . USAF Sat Cat: 37247 . COSPAR: 2010-066D. Apogee: 190 km (110 mi). Perigee: 179 km (111 mi). Inclination: 34.5000 deg. Period: 88.20 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..
  • Perseus 001 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-12-30 . USAF Sat Cat: 37248 . COSPAR: 2010-066E. Apogee: 183 km (113 mi). Perigee: 176 km (109 mi). Inclination: 34.5000 deg. Period: 88.10 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..
  • QBX1 - . Payload: QbX-1. Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-12-30 . USAF Sat Cat: 37249 . COSPAR: 2010-066F. Apogee: 197 km (122 mi). Perigee: 185 km (114 mi). Inclination: 34.5000 deg. Period: 88.30 min. 3U cubesat satellite built by Pumpkin Inc of San Francisco for the National Reconaissance Office's Colony-1 technology development project. Successful..
  • Perseus 002 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-12-22 . USAF Sat Cat: 37250 . COSPAR: 2010-066G. Apogee: 193 km (119 mi). Perigee: 183 km (113 mi). Inclination: 34.5000 deg. Period: 88.20 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..
  • Perseus 000 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-12-30 . USAF Sat Cat: 37251 . COSPAR: 2010-066H. Apogee: 190 km (110 mi). Perigee: 180 km (110 mi). Inclination: 34.5000 deg. Period: 88.20 min. Los Alamos National Laboratory cubesat, perhaps for ionospheric monitoring..
  • Mayflower - . Payload: Caerus/Mayflower. Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2010-12-22 . USAF Sat Cat: 37252 . COSPAR: 2010-066J. Apogee: 194 km (120 mi). Perigee: 179 km (111 mi). Inclination: 34.5000 deg. Period: 88.20 min.

    Experiment for Northrop Grumman NovaWorks and the University of Southern California. 3U cubesat with deployable solar panels composed of a Northrop Grumman's 2-unit Mayflower Next Generation Technology Nanosat and University of Southern California's 1-unit cubesat.


2011 March 4 - . 10:09 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576E. LV Family: Taurus. Launch Vehicle: Taurus 3110. FAILURE: Fairing failed to separate..
  • E1P - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Explorer 1 Prime, Montana State University Cubesat. Was to have duplicated Explorer 1's discovery of the van Allen radiation belts in 1958 using a geiger counter..
  • Hermes - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. 1U cubesat for University of Colorado at Boulder..
  • KySat-1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. University of Kentucky Cubesat..

2011 October 12 - . 05:31 GMT - . Launch Site: Sriharikota. LV Family: PSLV. Launch Vehicle: PSLV.
  • JUGNU - . Mass: 10 kg (22 lb). Nation: India. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37839 . COSPAR: 2011-058B. Apogee: 866 km (538 mi). Perigee: 839 km (521 mi). Inclination: 20.0000 deg. Period: 102.00 min. 3U cubesat for the Indian Institute of Technology in Kanpur. Micro-imaging system, near infrared camera to observe vegetation, and GPS Receiver to aid tracking. Successful..

2011 October 28 - . 09:48 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Thor. Launch Vehicle: Delta 7920-10C.
  • AubieSat-1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37854 . COSPAR: 2011-061E. Apogee: 817 km (507 mi). Perigee: 457 km (283 mi). Inclination: 101.7000 deg. Period: 97.50 min. Auburn University, Alabama 1U cubesat. First CubeSat from Auburn University. Successful..
  • DICE-X - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37851 . COSPAR: 2011-061B. Apogee: 816 km (507 mi). Perigee: 458 km (284 mi). Inclination: 101.7000 deg. Period: 97.50 min. Utah State University 1.5U cubesat. Deployed 10-m span electric field antennae to study magnetosphere..
  • DICE-Y - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37852 . COSPAR: 2011-061C. Apogee: 816 km (507 mi). Perigee: 458 km (284 mi). Inclination: 101.7000 deg. Period: 97.50 min. Utah State University 1.5U cubesat. Deployed 10-m span electric field antennae to study magnetosphere..
  • Explorer-1 PRIME Flight Unit 2 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-11-29 . USAF Sat Cat: 37856 . COSPAR: 2011-061G. Apogee: 815 km (506 mi). Perigee: 458 km (284 mi). Inclination: 101.7000 deg. Period: 97.50 min. Montana State University 1U cubesat. Carried one of Van Allen's original Geiger tubes..
  • M-Cubed - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 37855 . COSPAR: 2011-061F. Apogee: 815 km (506 mi). Perigee: 457 km (283 mi). Inclination: 101.7000 deg. Period: 97.40 min. University of Michigan 1U cubesat. Michigan Multipurpose Mission. Objective was to obtain a mid-resolution image of the earth covering at least 60% land mass and a maximum of 20% cloud coverage from a single CubeSat platform..
  • RAX-2 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2011-11-29 . USAF Sat Cat: 37853 . COSPAR: 2011-061D. Apogee: 817 km (507 mi). Perigee: 456 km (283 mi). Inclination: 101.7000 deg. Period: 97.50 min. University of Michigan 3U cubesat. National Science Foundation funded Radio Aurora Explorer..

2012 February 13 - . 10:00 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELV. LV Family: Vega. Launch Vehicle: Vega.
  • UNICubeSat-GG - . Mass: 1.00 kg (2.20 lb). Nation: Italy. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38078 . COSPAR: 2012-006B. Apogee: 1,415 km (879 mi). Perigee: 312 km (193 mi). Inclination: 69.5000 deg. Period: 102.20 min. Student 1U cubesat from the GAUSS team-Universita Roma La Sapienza with a gravity gradient experiment. First Italian CubeSat..
  • MaSat-1 - . Mass: 1.00 kg (2.20 lb). Nation: Hungary. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-01-16 . USAF Sat Cat: 38079 . COSPAR: 2012-006C. Apogee: 1,385 km (860 mi). Perigee: 305 km (189 mi). Inclination: 69.5000 deg. Period: 101.80 min. Student 1U cubesat from the Budapest University of Technology and Economics. Technological demonstration. Successful. First Hungarian satellite.
  • PWSat-1 - . Mass: 1.00 kg (2.20 lb). Nation: Poland. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-12-31 . USAF Sat Cat: 38080 . COSPAR: 2012-006D. Apogee: 1,384 km (859 mi). Perigee: 306 km (190 mi). Inclination: 69.5000 deg. Period: 101.80 min. 1U cubesat student satellite from the Warsaw Institute of Technology..
  • Goliat - . Mass: 1.00 kg (2.20 lb). Nation: Romania. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-01-09 . USAF Sat Cat: 38081 . COSPAR: 2012-006E. Apogee: 1,386 km (861 mi). Perigee: 305 km (189 mi). Inclination: 69.5000 deg. Period: 101.80 min. Student 1U cubesat from the University of Bucharest. Earth imaging and space environment measuring. First Romanian satellite..
  • e-st@r - . Mass: 1.00 kg (2.20 lb). Nation: Italy. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-08-31 . USAF Sat Cat: 38082 . COSPAR: 2012-006F. Apogee: 1,376 km (855 mi). Perigee: 305 km (189 mi). Inclination: 69.5000 deg. Period: 101.70 min. Student satellite from the Politecnico di Torino..
  • ROBUSTA - . Mass: 1.00 kg (2.20 lb). Nation: France. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-10-28 . USAF Sat Cat: 38083 . COSPAR: 2012-006G. Apogee: 1,379 km (856 mi). Perigee: 306 km (190 mi). Inclination: 69.5000 deg. Period: 101.80 min. Student 1U cubesat from the Universite' de Montpellier. Mission: Radiation effects on bipolar-transistor-based circuits. Status: Failed. First French CubeSat.
  • XaTcobeo - . Mass: 1.00 kg (2.20 lb). Nation: Spain. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-01-28 . USAF Sat Cat: 38084 . COSPAR: 2012-006H. Apogee: 1,390 km (860 mi). Perigee: 305 km (189 mi). Inclination: 69.5000 deg. Period: 101.90 min. Student satellite from the University of Vigo..

2012 September 9 - . 04:23 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. Launch Pad: LP1. LV Family: PSLV. Launch Vehicle: PSLV.
  • Proiteres - . Mass: 15 kg (33 lb). Nation: Japan. Class: Technology. Type: Ion engine technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38756 . COSPAR: 2012-047B. Apogee: 657 km (408 mi). Perigee: 640 km (390 mi). Inclination: 98.3000 deg. Period: 97.70 min. 15 kg pulsed plasma thruster experiment: 'Project of Osaka Institute of Technology Electric Rocket Engine aboard small Spaceship'..

2012 September 13 - . 21:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas V. Launch Vehicle: Atlas V 401.
  • SMDC One 1.2 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Climate technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38759 . COSPAR: 2012-048B. 3U cubesat operational Nanosatellite Effect communications experiment for US Army Space and Missile Defence Command, Huntsville, Alabama..
  • Aeneas - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38760 . COSPAR: 2012-048C. Cubesat with a cargo container tracking experiment by the University of Southern California, Los Angeles for the Department of Homeland Security.
  • CSSWE - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38761 . COSPAR: 2012-048D. University of Colorado, Boulder Colorado Student 3U cubesat with a Space Weather Experiment. Studied radiation belt electrons and protons. Extended mission was completed..
  • CXBN - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38762 . COSPAR: 2012-048E. Morehead State University, Kentucky cosmic hard X-ray background radiation experiment..
  • CP5 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Solar sail technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38763 . COSPAR: 2012-048F. California Polytechnic State University San Luis Obispo solar sail deorbit technology experiment..
  • Cinema - . Payload: CINEMA 1. Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38764 . COSPAR: 2012-048G. University of California Berkeley magnetospheric experiment..
  • RE - . Payload: Re/STARE. Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Surveillance. Type: Orbital object tracking satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38765 . COSPAR: 2012-048H. Lawrence Livermore Natlional Laboratory space debris tracking experiment..
  • SMDC One 1.1 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38766 . COSPAR: 2012-048J. 3U cubesat operational Nanosatellite Effect communications experiment for US Army Space and Missile Defence Command, Huntsville, Alabama..
  • Aerocube 4.5A - . Payload: Aerocube-4.5A. Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38767 . COSPAR: 2012-048K. Cubesat for Aerospace Corporation, El Segundo, California..
  • Aerocube 4.5B - . Payload: Aerocube-4.5B. Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38768 . COSPAR: 2012-048L. Cubesat for Aerospace Corporation, El Segundo, California..
  • Aerocube 4 - . Payload: Aerocube-4. Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 38769 . COSPAR: 2012-048M. Cubesat for Aerospace Corporation, El Segundo, California..

2012 October 4 - . 14:37 GMT - . Launch Site: ISS. LV Family: Proton. Launch Vehicle: Proton-K.
  • RAIKO - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-08-06 . USAF Sat Cat: 38852 . COSPAR: 1998-067CN. Apogee: 414 km (257 mi). Perigee: 390 km (240 mi). Inclination: 51.6000 deg. Period: 92.60 min. Released from the J-SSOD cubesat deployer outside the ISS Kibo module's equipment airlock by the JEM-RMS robot arm..
  • We Wish - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-03-11 . USAF Sat Cat: 38856 . COSPAR: 1998-067CS. Apogee: 400 km (240 mi). Perigee: 375 km (233 mi). Inclination: 51.6000 deg. Period: 92.30 min. Released from ISS Kibo module..
  • Niwaka - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-07-04 . USAF Sat Cat: 38853 . COSPAR: 1998-067CP. Apogee: 410 km (250 mi). Perigee: 390 km (240 mi). Inclination: 51.6000 deg. Period: 92.60 min. Released from ISS Kibo module..
  • TechEdSat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-05-05 . USAF Sat Cat: 38854 . COSPAR: 1998-067CQ. Apogee: 406 km (252 mi). Perigee: 385 km (239 mi). Inclination: 51.6000 deg. Period: 92.50 min. Released from ISS Kibo module. 1U cubesat for San Jose State University. Mission: SPA hardware and software, inter-satellite communication link analysis ..
  • F-1 - . Mass: 1.00 kg (2.20 lb). Nation: Vietnam. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-05-09 . USAF Sat Cat: 38855 . COSPAR: 1998-067CR. Apogee: 407 km (252 mi). Perigee: 386 km (239 mi). Inclination: 51.6000 deg. Period: 92.50 min. Released from ISS Kibo module..

2013 February 25 - . 12:31 GMT - . Launch Site: Sriharikota. LV Family: PSLV. Launch Vehicle: PSLV.
  • AAUSAT3 - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Class: Navigation. Type: Navigation satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39087 . COSPAR: 2013-009B. Apogee: 787 km (489 mi). Perigee: 770 km (470 mi). Inclination: 98.6300 deg. Period: 100.41 min. 2U cubesat built by Aalborg University in Denmark; carried a double AIS ship tracking receiver and a GPS receiver for tracking ships in Arctic regions. Successful..
  • STRaND-1 - . Mass: 4.00 kg (8.80 lb). Nation: UK. Agency: Surrey. Manufacturer: Surrey. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39090 . COSPAR: 2013-009E. Apogee: 783 km (486 mi). Perigee: 771 km (479 mi). Inclination: 98.6300 deg. Period: 100.40 min. 3U cubesat, a technical test project of Surrey Satellite and the Surrey Space Centre. Carried a Google Nexus One smartphone as its main avionics, and featured plasma thrusters and a water-alcohol thruster. Successful; first in STRaND Program..

2013 April 19 - . 10:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. Launch Pad: LC31/6. LV Family: R-7. Launch Vehicle: Soyuz-2-1A.
  • OSSI-1 - . Mass: 1.00 kg (2.20 lb). Nation: Korea South. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-07-08 . USAF Sat Cat: 39131 . COSPAR: 2013-015B. Apogee: 348 km (216 mi). Perigee: 218 km (135 mi). Inclination: 64.8600 deg. Period: 90.17 min. Cubesat developed by a Korean artist..
  • Dove-2 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39132 . COSPAR: 2013-015C. Apogee: 575 km (357 mi). Perigee: 564 km (350 mi). Inclination: 64.8700 deg. Period: 96.06 min. 3U cubesat, a demonstration satellite for Cosmogia, designed to return on-board system health data and validate the design for future Dove satellites, which will carry remote sensing payloads..
  • BEESAT-3 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39134 . COSPAR: 2013-015E. Apogee: 574 km (356 mi). Perigee: 558 km (346 mi). Inclination: 64.8800 deg. Period: 95.97 min. 1U cubesat from the Technical University of Berlin. Reaction wheel technology qualification. Successful..
  • SOMP - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39135 . COSPAR: 2013-015F. Apogee: 574 km (356 mi). Perigee: 558 km (346 mi). Inclination: 64.8800 deg. Period: 95.98 min. Student Oxygen Measurement 1U cubesat from Technical University of Dresden. Mission: Education, testing software defined radio, measuring atomic oxygen concentration, demonstrating TFSC ..
  • BEESAT-2 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39136 . COSPAR: 2013-015G. Apogee: 574 km (356 mi). Perigee: 558 km (346 mi). Inclination: 64.8800 deg. Period: 95.98 min. 1U cubesat from the Technical University of Berlin. Mission: Reaction wheel technology qualification. Successful..

2013 April 21 - . 21:00 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LP0A. LV Family: Antares LV. Launch Vehicle: Antares 110.
  • Dove-1 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-04-27 . USAF Sat Cat: 39143 . COSPAR: 2013-016B. Apogee: 169 km (105 mi). Perigee: 160 km (90 mi). Inclination: 51.6200 deg. Period: 87.78 min. 3U cubesat, a demonstration satellite for Cosmogia, designed to return on-board system health data and validate the design for future Dove satellites, which will carry remote sensing payloads..
  • Alexander - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-04-27 . USAF Sat Cat: 39144 . COSPAR: 2013-016C. Apogee: 152 km (94 mi). Perigee: 134 km (83 mi). Inclination: 51.6000 deg. Period: 87.35 min. 1U cubesat from NASA's Ames Research Center, designed to demonstrate use of a commercial Nexus S mobile phone as a spacecraft avionics/computer system, together with an S-band radio, solar panels, GPS receiver, magnetorquers and reaction wheels..
  • Bell - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-05-10 . USAF Sat Cat: 39145 . COSPAR: 2013-016D. Apogee: 150 km (90 mi). Perigee: 144 km (89 mi). Inclination: 51.6100 deg. Period: 87.42 min. 1U cubesat from NASA's Ames Research Center, designed to demonstrate use of a commercial Nexus One Android-based mobile phone as a spacecraft avionics/computer system..
  • Graham - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2013-04-26 . USAF Sat Cat: 39146 . COSPAR: 2013-016E. Apogee: 175 km (108 mi). Perigee: 161 km (100 mi). Inclination: 51.6200 deg. Period: 87.85 min. 1U cubesat from NASA's Ames Research Center, designed to demonstrate use of a commercial Nexus One Android-based mobile phone as a spacecraft avionics/computer system..

2013 April 26 - . 04:13 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: Chang Zheng 2D.
  • NEE-01 Pegaso - . Mass: 1.00 kg (2.20 lb). Nation: Ecuador. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39151 . COSPAR: 2013-018B. Apogee: 654 km (406 mi). Perigee: 627 km (389 mi). Inclination: 98.0700 deg. Period: 97.53 min. 1U cubesat for the Ecuadorian space agency EXA..
  • Turksat-3USAT - . Mass: 3.00 kg (6.60 lb). Nation: Turkey. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39152 . COSPAR: 2013-018C. Apogee: 654 km (406 mi). Perigee: 628 km (390 mi). Inclination: 98.0500 deg. Period: 97.54 min. 3U cubesat from Istanbul Technical University..
  • CubeBug-1 - . Mass: 2.00 kg (4.40 lb). Nation: Argentina. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39153 . COSPAR: 2013-018D. Apogee: 654 km (406 mi). Perigee: 627 km (389 mi). Inclination: 98.0700 deg. Period: 97.53 min. 2U cubesat from Argentina..

2013 May 7 - . 02:06 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELV. LV Family: Vega. Launch Vehicle: Vega.
  • ESTCube-1 - . Mass: 1.00 kg (2.20 lb). Nation: Estonia. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39161 . COSPAR: 2013-021C. Apogee: 672 km (417 mi). Perigee: 656 km (407 mi). Inclination: 98.1300 deg. Period: 98.03 min. 1U cubesat by the Estonian Student Satellite Program led by the University of Tartu. Space test of the electric solar wind sail. Successful. First Estonian satellite.

2013 September 29 - . 16:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Falcon. Launch Vehicle: Falcon 9.
  • POPACS 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39268 . COSPAR: 2013-055D. Apogee: 1,419 km (881 mi). Perigee: 323 km (200 mi). Inclination: 81.0000 deg. Period: 102.37 min. 3U cubesat which split after deployment into four spacer sections that released three 0.10 m diameter aluminium spheres used as passive atmospheric density calibration probes..
  • POPACS 2 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39269 . COSPAR: 2013-055E. Apogee: 1,440 km (890 mi). Perigee: 323 km (200 mi). Inclination: 81.0000 deg. Period: 102.60 min.
  • POPACS 3 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39270 . COSPAR: 2013-055F. Apogee: 1,451 km (901 mi). Perigee: 324 km (201 mi). Inclination: 81.0000 deg. Period: 102.73 min.

2013 November 19 - . 12:18 GMT - . Launch Site: ISS. LV Family: Proton. Launch Vehicle: Proton-K.
  • PicoDragon - . Mass: 1.00 kg (2.20 lb). Nation: Vietnam. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-04-16 . USAF Sat Cat: 39412 . COSPAR: 1998-067DA. Apogee: 188 km (116 mi). Perigee: 180 km (110 mi). Inclination: 51.6300 deg. Period: 88.17 min. On 19 November a J-SSOD cubesat deployer was retrieved from the Kibo module airlock by the JEM RMS arm and moved to a deployment position; at 12:18 GMT it ejected three 1U cubesats, including PicoDragon for Vietnam..
  • Ardusat-1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-02-28 . USAF Sat Cat: 39413 . COSPAR: 1998-067DB. Apogee: 165 km (102 mi). Perigee: 121 km (75 mi). Inclination: 51.7300 deg. Period: 87.35 min.

    On 19 November a J-SSOD cubesat deployer was retrieved from the Kibo module airlock by the JEM RMS arm and moved to a deployment position; at 12:18 GMT it ejected three 1U cubesats, including two Ardusats for a demonstration of spaceborne Arduino processors for the US company NanoSatisfi.

  • Ardusat-Xh - . Mass: 1.00 kg (2.20 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-04-15 . USAF Sat Cat: 39414 . COSPAR: 1998-067DC. Apogee: 178 km (110 mi). Perigee: 173 km (107 mi). Inclination: 51.6200 deg. Period: 88.00 min.

    On 19 November a J-SSOD cubesat deployer was retrieved from the Kibo module airlock by the JEM RMS arm and moved to a deployment position; at 12:18 GMT it ejected three 1U cubesats, including two Ardusats for a demonstration of spaceborne Arduino processors for the US company NanoSatisfi.


2013 November 20 - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA0B. LV Family: Minuteman. Launch Vehicle: Minotaur 1.
  • Prometheus 1-1 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39406 . COSPAR: 2013-064AC. Apogee: 482 km (299 mi). Perigee: 473 km (293 mi). Inclination: 40.5100 deg. Period: 94.15 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • Prometheus 1-1 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39406 . COSPAR: 2013-064AC. Apogee: 482 km (299 mi). Perigee: 473 km (293 mi). Inclination: 40.5100 deg. Period: 94.15 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • Prometheus 1-3 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39408 . COSPAR: 2013-064AE. Apogee: 482 km (299 mi). Perigee: 473 km (293 mi). Inclination: 40.5100 deg. Period: 94.16 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • ORSES - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39386 . COSPAR: 2013-064G. Apogee: 483 km (300 mi). Perigee: 474 km (294 mi). Inclination: 40.5000 deg. Period: 94.17 min. 3U ORS Enabler Satellite, a tactical communications satellite for the USAF Operationally Responsive Space office and the US Space and Missile Defense Command..
  • ORS Tech 1 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-03-23 . USAF Sat Cat: 39387 . COSPAR: 2013-064H. Apogee: 473 km (293 mi). Perigee: 457 km (283 mi). Inclination: 40.5200 deg. Period: 93.90 min. Cubesat; 3U technology demonstration satellites for USAF Operationally Responsive Space office developed by APL..
  • Prometheus 1-4 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39390 . COSPAR: 2013-064L. Apogee: 482 km (299 mi). Perigee: 474 km (294 mi). Inclination: 40.5000 deg. Period: 94.16 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • Prometheus 1-2 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39391 . COSPAR: 2013-064M. Apogee: 482 km (299 mi). Perigee: 474 km (294 mi). Inclination: 40.5000 deg. Period: 94.16 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • Prometheus 1-5 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39393 . COSPAR: 2013-064P. Apogee: 482 km (299 mi). Perigee: 472 km (293 mi). Inclination: 40.5200 deg. Period: 94.14 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • Prometheus 1-6 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39394 . COSPAR: 2013-064Q. Apogee: 482 km (299 mi). Perigee: 473 km (293 mi). Inclination: 40.5200 deg. Period: 94.16 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • ORS Tech 2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-04-03 . USAF Sat Cat: 39396 . COSPAR: 2013-064S. Apogee: 474 km (294 mi). Perigee: 458 km (284 mi). Inclination: 40.5200 deg. Period: 93.92 min. Cubesat; 3U technology demonstration satellites for USAF Operationally Responsive Space office developed by APL..
  • Prometheus 1-8 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39401 . COSPAR: 2013-064X. Apogee: 481 km (298 mi). Perigee: 473 km (293 mi). Inclination: 40.5200 deg. Period: 94.15 min. 1.5 U Cubesat; part of a constellation of low orbit military tactical communications satellites for the US Southern Command (SOCOM); developed by Los Alamos..
  • Firefly - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39404 . COSPAR: 2013-064AA. Apogee: 487 km (302 mi). Perigee: 482 km (299 mi). Inclination: 40.5200 deg. Period: 94.30 min. Cubesat; a 3U science sat for the National Science Foundation built by the Hawk Institute for Space Sciences in Maryland in collaboration with Siena College, that studied terrestrial gamma-ray flashes..
  • ChargerSat 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39405 . COSPAR: 2013-064AB. Apogee: 484 km (300 mi). Perigee: 476 km (295 mi). Inclination: 40.5000 deg. Period: 94.21 min. Cubesat from University of Alabama-Huntsville..
  • PhoneSat-2.4 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39381 . COSPAR: 2013-064B. Apogee: 487 km (302 mi). Perigee: 480 km (290 mi). Inclination: 40.5000 deg. Period: 94.28 min. Cubesat from NASA-Ames, with systems based on a Nexus/Android cellphone..
  • CAPE 2 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-10-23 . USAF Sat Cat: 39382 . COSPAR: 2013-064C. Apogee: 445 km (276 mi). Perigee: 417 km (259 mi). Inclination: 40.4900 deg. Period: 93.20 min. Cubesat from University of Louisiana-Lafayette..
  • Vermont Lunar Cubesat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39407 . COSPAR: 2013-064AD. Apogee: 482 km (299 mi). Perigee: 473 km (293 mi). Inclination: 40.5300 deg. Period: 94.15 min. 1U cubesat from Vermont Technical College, testing equipment for a proposed future lunar mission. Testing navigation components to be used in a follow up 3U ion drive CubeSat to the Moon. Successful. First university satellite from New England..
  • DragonSat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39383 . COSPAR: 2013-064D. Apogee: 487 km (302 mi). Perigee: 478 km (297 mi). Inclination: 40.5100 deg. Period: 94.26 min. Cubesat from Drexel University, Penn. and the US Naval Academy, Annapolis..
  • KySat-2 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-02-12 . USAF Sat Cat: 39384 . COSPAR: 2013-064E. Apogee: 470 km (290 mi). Perigee: 452 km (280 mi). Inclination: 40.5000 deg. Period: 93.81 min. Cubesat from Kentucky Space, Lexington, Kentucky..
  • TJ3Sat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-09-17 . USAF Sat Cat: 39385 . COSPAR: 2013-064F. Apogee: 481 km (298 mi). Perigee: 469 km (291 mi). Inclination: 40.5300 deg. Period: 94.10 min. Cubesat from Thomas Jefferson High School, Virginia..
  • SENSE-A - . Payload: SENSE SV1. Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-03-21 . USAF Sat Cat: 39388 . COSPAR: 2013-064J. Apogee: 473 km (293 mi). Perigee: 459 km (285 mi). Inclination: 40.5200 deg. Period: 93.91 min. 3U Cubesat ionospheric monitoring satellite for the USAF Space and Missile Center..
  • NPS-SCAT - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-10-28 . USAF Sat Cat: 39389 . COSPAR: 2013-064K. Apogee: 482 km (299 mi). Perigee: 471 km (292 mi). Inclination: 40.5000 deg. Period: 94.13 min. Cubesat for the US Navy Postgraduate School, with a solar cell exposure experiment..
  • SENSE-B - . Payload: SENSE SV2. Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Earth. Type: Ionosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39392 . COSPAR: 2013-064N. Apogee: 491 km (305 mi). Perigee: 483 km (300 mi). Inclination: 40.5100 deg. Period: 94.35 min. 3U Cubesat ionospheric monitoring satellite for the USAF Space and Missile Center..
  • COPPER - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39395 . COSPAR: 2013-064R. Apogee: 484 km (300 mi). Perigee: 475 km (295 mi). Inclination: 40.5000 deg. Period: 94.19 min. Cubesat from Saint Louis University, Missouri..
  • Horus/STARE-B - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Surveillance. Type: Orbital object tracking satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39397 . COSPAR: 2013-064T. Apogee: 489 km (303 mi). Perigee: 482 km (299 mi). Inclination: 40.5100 deg. Period: 94.32 min. Cubesat; a 3U Lawrence Livermore experiment for space debris monitoring..
  • Black Knight 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-07-16 . USAF Sat Cat: 39398 . COSPAR: 2013-064U. Apogee: 479 km (297 mi). Perigee: 467 km (290 mi). Inclination: 40.5300 deg. Period: 94.06 min. Cubesat for the US Military Academy at West Point, New York..
  • Trailblazer - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39400 . COSPAR: 2013-064W. Apogee: 485 km (301 mi). Perigee: 477 km (296 mi). Inclination: 40.5100 deg. Period: 94.23 min. Cubesat from University of New Mexico-Albequerque..
  • SwampSat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39402 . COSPAR: 2013-064Y. Apogee: 483 km (300 mi). Perigee: 473 km (293 mi). Inclination: 40.5000 deg. Period: 94.17 min. Cubesat from University of Florida-Gainesville..
  • Ho oponopono 2 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Surveillance. Type: Radar calibration target. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39403 . COSPAR: 2013-064Z. Apogee: 492 km (305 mi). Perigee: 485 km (301 mi). Inclination: 40.5300 deg. Period: 94.38 min. 3U Cubesat for radar calibration, from University of Hawaii-Manoa..

2013 November 20 - . 07:58 GMT - . Launch Site: ISS. LV Family: Proton. Launch Vehicle: Proton-K.
  • TechEdSat-3p - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-01-16 . USAF Sat Cat: 39415 . COSPAR: 1998-067DD. Apogee: 227 km (141 mi). Perigee: 205 km (127 mi). Inclination: 51.6200 deg. Period: 88.81 min.

    On 19 November a J-SSOD cubesat deployer was retrieved from the Kibo module airlock by the JEM RMS arm and moved to a deployment position. On 20 November it released this 3U cubesat from NASA-Ames and San Jose State University, which deployed an 0.6m `Exobrake' sail to test a way to increase the cubesat's drag and make it reenter quickly.


2013 November 21 - . 07:10 GMT - . Launch Site: Dombarovskiy. Launch Pad: xxx. LV Family: R-36M. Launch Vehicle: Dnepr.
  • HINCube-1 - . Mass: 1.00 kg (2.20 lb). Nation: South Africa. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39417 . COSPAR: 2013-066B. Apogee: 678 km (421 mi). Perigee: 592 km (367 mi). Inclination: 97.7800 deg. Period: 97.42 min. 1U cubesat from French South African Institute of Technology at the Cape Peninsula University of Technology. Mission: Space weather, technology demonstration, education and human capital development.. Successful. First South African CubeSat..
  • OPTOS - . Mass: 4.00 kg (8.80 lb). Nation: Spain. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39420 . COSPAR: 2013-066E. Apogee: 793 km (492 mi). Perigee: 594 km (369 mi). Inclination: 97.7600 deg. Period: 98.63 min. 3U cubesat from INTA of Spain..
  • KHUSAT-1 - . Payload: CINEMA 2. Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39424 . COSPAR: 2013-066J. Apogee: 727 km (451 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.94 min. 3U cubesat from Kyung Hee University, Seoul, to join the CINEMA constellation..
  • KHUSAT-2 - . Payload: CINEMA 3. Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39426 . COSPAR: 2013-066L. Apogee: 743 km (461 mi). Perigee: 594 km (369 mi). Inclination: 97.7700 deg. Period: 98.11 min. 3U cubesat from Kyung Hee University, Seoul, to join the CINEMA constellation..
  • Triton 1 - . Mass: 4.00 kg (8.80 lb). Nation: UK. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39427 . COSPAR: 2013-066M. Apogee: 758 km (470 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.27 min. 3U cubesat test of an AIS receiver from ISIS b.v., Netherlands..
  • Delfi-3nXt - . Mass: 5.00 kg (11.00 lb). Nation: Netherlands. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39428 . COSPAR: 2013-066N. Apogee: 773 km (480 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.41 min. 3U cubesat from Delft University of Technology..
  • Dove-3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39429 . COSPAR: 2013-066P. Apogee: 809 km (502 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.80 min. 3U imaging satellite from PlanetLabs, San Francisco..
  • GOMX-1 - . Mass: 6.00 kg (13.20 lb). Nation: Denmark. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39430 . COSPAR: 2013-066Q. Apogee: 813 km (505 mi). Perigee: 593 km (368 mi). Inclination: 97.7600 deg. Period: 98.84 min. 2U cubesat test an ADS-B air traffic control receiver, for GOMSpace, Aalborg, Denmark..
  • ICUBE-1 - . Mass: 2.00 kg (4.40 lb). Nation: Pakistan. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39432 . COSPAR: 2013-066S. Apogee: 634 km (393 mi). Perigee: 587 km (364 mi). Inclination: 97.7800 deg. Period: 96.90 min. 2U cubesat from Unisat-5 for Institute of Space Technology, Islamabad. Successful. First Pakistani cubesat..
  • HUMSAT-D - . Mass: 1.00 kg (2.20 lb). Nation: Spain. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39433 . COSPAR: 2013-066T. Apogee: 632 km (392 mi). Perigee: 586 km (364 mi). Inclination: 97.7800 deg. Period: 96.88 min. Deployed from Unisat-5 for University of Vigo, Spain..
  • Dove-4 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39434 . COSPAR: 2013-066U. Apogee: 624 km (387 mi). Perigee: 581 km (361 mi). Inclination: 97.7800 deg. Period: 96.75 min. 3U Earth imaging satellite, deployed from Unisat-5 for PlanetLabs..
  • WREN - . Mass: 0 kg (0 lb). Nation: Germany. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39435 . COSPAR: 2013-066V. Apogee: 638 km (396 mi). Perigee: 594 km (369 mi). Inclination: 97.8000 deg. Period: 97.02 min. PocketQube cubesat from StaDoKo (spinoff company of the University of Aachen)..
  • 50SAT - . Mass: 0 kg (0 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39436 . COSPAR: 2013-066W. Apogee: 615 km (382 mi). Perigee: 580 km (360 mi). Inclination: 97.7800 deg. Period: 96.63 min. AKA Eagle-2, 50DollarSat; from Morehead State University. First PocketQube cubesat; 1P size was 0.15 kg, 5 x 5 x 5cm cubes.
  • BeakerSat-1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39437 . COSPAR: 2013-066X. Apogee: 619 km (384 mi). Perigee: 583 km (362 mi). Inclination: 97.7900 deg. Period: 96.71 min. 2.5P PocketQube, AKA Eagle-1, from Morehead State University..
  • VELOX-P2 - . Mass: 1.00 kg (2.20 lb). Nation: Singapore. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39438 . COSPAR: 2013-066Y. Apogee: 695 km (431 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.60 min. Cubesat from Nanyang Tech University..
  • First-Move - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39439 . COSPAR: 2013-066Z. Apogee: 691 km (429 mi). Perigee: 591 km (367 mi). Inclination: 97.7700 deg. Period: 97.54 min. Cubesat from Technical University of Munich..
  • Manolito - . Payload: CUBEBUG 2. Mass: 2.00 kg (4.40 lb). Nation: Argentina. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39440 . COSPAR: 2013-066AA. Apogee: 710 km (440 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.76 min. 2U cubesat from Argentina..
  • Krysaor - . Payload: NEE-2. Mass: 1.00 kg (2.20 lb). Nation: Ecuador. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39441 . COSPAR: 2013-066AB. Apogee: 711 km (441 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.77 min. Cubesat from Ecuadorian Space Agency..
  • PUCPSat-1 - . Mass: 1.00 kg (2.20 lb). Nation: Peru. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39442 . COSPAR: 2013-066AC. Apogee: 633 km (393 mi). Perigee: 587 km (364 mi). Inclination: 97.7800 deg. Period: 96.90 min. 1U cubesat deployed from Unisat-5 for Pontifica Universidad Catolica del Peru, Lima..
  • QBScout-1 - . Mass: 0 kg (0 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39443 . COSPAR: 2013-066AD. Apogee: 630 km (390 mi). Perigee: 591 km (367 mi). Inclination: 97.7800 deg. Period: 96.90 min. 2.5P PocketQube from University of Maryland/Baltimore County..
  • FUNcube-1 - . Mass: 1.00 kg (2.20 lb). Nation: UK. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39444 . COSPAR: 2013-066AE. Apogee: 677 km (420 mi). Perigee: 592 km (367 mi). Inclination: 97.7700 deg. Period: 97.41 min. Cubesat for AMSAT-UK..
  • Tshepiso - . Payload: ZACUBE. Mass: 1.00 kg (2.20 lb). Nation: Norway. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39445 . COSPAR: 2013-066AF. Apogee: 677 km (420 mi). Perigee: 592 km (367 mi). Inclination: 97.7700 deg. Period: 97.41 min. Cubesat from South Africa's Cape Peninsula University of Tech (CPUT)..
  • UWE-3 - . Mass: 1.00 kg (2.20 lb). Nation: Germany. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39446 . COSPAR: 2013-066AG. Apogee: 694 km (431 mi). Perigee: 593 km (368 mi). Inclination: 97.7700 deg. Period: 97.59 min. Cubesat from University of Wurzburg..
  • Pocket-PUCP - . Mass: 0 kg (0 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. COSPAR: 2013-066x. Apogee: 616 km (382 mi). Perigee: 579 km (359 mi). Inclination: 97.7800 deg. Period: 96.64 min. PocketQube cubesat ejected from PUCPSat-1..

2013 December 6 - . 07:14 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas V. Launch Vehicle: Atlas V 501.
  • FIREBIRD A - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39463 . COSPAR: 2013-072B. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg.

    1.5U cubesat from the Montana Space Grant Consortium to study electron microbursts in the magnetosphere. The Centaur AV-042 upper stage, after deploying the main payload, made two orbit lowering burns to a 467 x 883 km x 120.5 deg orbit. Attached to AV-042 was GEMSAT, the second NPSCuL cubesat launcher, which ejected 12 cubesats between around 10:22 and 10:38 GMT.

  • FIREBIRD B - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39464 . COSPAR: 2013-072C. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 1.5U cubesat from the Montana Space Grant Consortium to study electron microbursts in the magnetosphere..
  • Aerocube 5a - . Mass: 10 kg (22 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39465 . COSPAR: 2013-072D. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 5U technology cubesat for the Aerospace Corporation..
  • Aerocube 5b - . Mass: 10 kg (22 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39466 . COSPAR: 2013-072E. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 5U technology cubesat for the Aerospace Corporation..
  • ALICE - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39467 . COSPAR: 2013-072F. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 1U cubesat from the Air Force Institute of Technology carrying technology experiments..
  • SNAP-3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39468 . COSPAR: 2013-072G. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 3U cubesat for the SMDC Nanosatellite Program, with an unknown mission..
  • MCubed-2 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39469 . COSPAR: 2013-072H. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 1U cubesat from the University of Michigan with technology experiments, including a low resolution imager..
  • CUNYSAT 1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39470 . COSPAR: 2013-072J. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 1U cubesat from the City University of New York's Medgar Evers College, with a GPS ionospheric receiver..
  • IPEX - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39471 . COSPAR: 2013-072K. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 1U cubesat built by Cal Poly to test systems and algorithms for JPL..
  • SMDC One 2.4 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39472 . COSPAR: 2013-072L. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 3U cubesat communications satellite for the US Army Space and Missile Defense Command..
  • Tacsat 6 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39473 . COSPAR: 2013-072M. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 3U cubesat for SMDC with an unknown mission, probably tactical communications or imaging..
  • SMDC One 2.3 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 39474 . COSPAR: 2013-072N. Apogee: 883 km (548 mi). Perigee: 467 km (290 mi). Inclination: 120.5000 deg. 3U cubesat communications satellite for the US Army Space and Missile Defense Command..

2014 February 11 - . 08:31 GMT - . Launch Site: ISS. LV Family: Proton. Launch Vehicle: Proton-K.
  • Flock1-1 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-15 . USAF Sat Cat: 39512 . COSPAR: 1998-067DG. Apogee: 195 km (121 mi). Perigee: 181 km (112 mi). Inclination: 51.6200 deg. Period: 88.26 min.

    Flock-1 satellites, 3U Dove-class Earth imaging cubesats, for the San Francisco based company PlanetLabs, were deployed by the ISS JEM RMS at about 08:31 GMT on February 11. By February 15 all 16 satellites from the first Nanoracks bag had been ejected; by 19 February all of the Flock-1 satellites had been ejected.

  • Flock1-2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-09 . USAF Sat Cat: 39513 . COSPAR: 1998-067DH. Apogee: 162 km (100 mi). Perigee: 155 km (96 mi). Inclination: 51.6000 deg. Period: 87.65 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-25 . USAF Sat Cat: 39514 . COSPAR: 1998-067DJ. Apogee: 170 km (100 mi). Perigee: 162 km (100 mi). Inclination: 51.6300 deg. Period: 87.81 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-4 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-18 . USAF Sat Cat: 39515 . COSPAR: 1998-067DK. Apogee: 185 km (114 mi). Perigee: 169 km (105 mi). Inclination: 51.6200 deg. Period: 88.03 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-5 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-02 . USAF Sat Cat: 39518 . COSPAR: 1998-067DL. Apogee: 154 km (95 mi). Perigee: 148 km (91 mi). Inclination: 51.6100 deg. Period: 87.51 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-6 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-15 . USAF Sat Cat: 39519 . COSPAR: 1998-067DM. Apogee: 169 km (105 mi). Perigee: 156 km (96 mi). Inclination: 51.6200 deg. Period: 87.73 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-11 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-06 . USAF Sat Cat: 39520 . COSPAR: 1998-067DN. Apogee: 175 km (108 mi). Perigee: 133 km (82 mi). Inclination: 51.5800 deg. Period: 87.57 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-12 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-25 . USAF Sat Cat: 39521 . COSPAR: 1998-067DP. Apogee: 159 km (98 mi). Perigee: 153 km (95 mi). Inclination: 51.6200 deg. Period: 87.61 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-13 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-07-06 . USAF Sat Cat: 39525 . COSPAR: 1998-067DQ. Apogee: 291 km (180 mi). Perigee: 287 km (178 mi). Inclination: 51.6300 deg. Period: 90.30 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-14 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-14 . USAF Sat Cat: 39526 . COSPAR: 1998-067DR. Apogee: 165 km (102 mi). Perigee: 157 km (97 mi). Inclination: 51.6100 deg. Period: 87.70 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-15 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-13 . USAF Sat Cat: 39527 . COSPAR: 1998-067DS. Apogee: 172 km (106 mi). Perigee: 165 km (102 mi). Inclination: 51.6200 deg. Period: 87.86 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-16 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-10-26 . USAF Sat Cat: 39528 . COSPAR: 1998-067DT. Apogee: 370 km (220 mi). Perigee: 368 km (228 mi). Inclination: 51.6400 deg. Period: 91.93 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-7 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-07-02 . USAF Sat Cat: 39529 . COSPAR: 1998-067DU. Apogee: 288 km (178 mi). Perigee: 279 km (173 mi). Inclination: 51.6400 deg. Period: 90.19 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-8 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-20 . USAF Sat Cat: 39530 . COSPAR: 1998-067DV. Apogee: 177 km (109 mi). Perigee: 162 km (100 mi). Inclination: 51.6100 deg. Period: 87.88 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-9 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-21 . USAF Sat Cat: 39531 . COSPAR: 1998-067DW. Apogee: 181 km (112 mi). Perigee: 166 km (103 mi). Inclination: 51.6000 deg. Period: 87.96 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-10 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-20 . USAF Sat Cat: 39532 . COSPAR: 1998-067DX. Apogee: 171 km (106 mi). Perigee: 157 km (97 mi). Inclination: 51.6200 deg. Period: 87.77 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-17 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-19 . USAF Sat Cat: 39555 . COSPAR: 1998-067DY. Apogee: 187 km (116 mi). Perigee: 177 km (109 mi). Inclination: 51.6400 deg. Period: 88.14 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-18 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-10-29 . USAF Sat Cat: 39556 . COSPAR: 1998-067DZ. Apogee: 374 km (232 mi). Perigee: 370 km (220 mi). Inclination: 51.6400 deg. Period: 92.00 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-21 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-25 . USAF Sat Cat: 39557 . COSPAR: 1998-067EA. Apogee: 161 km (100 mi). Perigee: 150 km (90 mi). Inclination: 51.6100 deg. Period: 87.59 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-22 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-05 . USAF Sat Cat: 39558 . COSPAR: 1998-067EB. Apogee: 178 km (110 mi). Perigee: 165 km (102 mi). Inclination: 51.6400 deg. Period: 87.92 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-19 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-03 . USAF Sat Cat: 39559 . COSPAR: 1998-067EC. Apogee: 190 km (110 mi). Perigee: 186 km (115 mi). Inclination: 51.6300 deg. Period: 88.26 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-20 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-10-09 . USAF Sat Cat: 39560 . COSPAR: 1998-067ED. Apogee: 367 km (228 mi). Perigee: 363 km (225 mi). Inclination: 51.6500 deg. Period: 91.85 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-23 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-07-10 . USAF Sat Cat: 39561 . COSPAR: 1998-067EE. Apogee: 321 km (199 mi). Perigee: 315 km (195 mi). Inclination: 51.6400 deg. Period: 90.89 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-24 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-16 . USAF Sat Cat: 39562 . COSPAR: 1998-067EF. Apogee: 183 km (113 mi). Perigee: 172 km (106 mi). Inclination: 51.6200 deg. Period: 88.04 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-25 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-24 . USAF Sat Cat: 39563 . COSPAR: 1998-067EG. Apogee: 245 km (152 mi). Perigee: 236 km (146 mi). Inclination: 51.6300 deg. Period: 89.31 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-26 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-10 . USAF Sat Cat: 39564 . COSPAR: 1998-067EH. Apogee: 183 km (113 mi). Perigee: 177 km (109 mi). Inclination: 51.6100 deg. Period: 88.09 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..

2014 February 27 - . 18:37 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 202.
  • Hayato-2 - . Payload: ITF 1. Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-29 . USAF Sat Cat: 39573 . COSPAR: 2014-009B. Apogee: 256 km (159 mi). Perigee: 233 km (144 mi). Inclination: 65.0000 deg. Period: 89.40 min. Cubesat from Tsukuba University..
  • OPUSat - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-07-24 . USAF Sat Cat: 39575 . COSPAR: 2014-009D. Apogee: 310 km (190 mi). Perigee: 288 km (178 mi). Inclination: 65.0000 deg. Period: 90.50 min. 1U cubesat from Osaka Prefectural University. Technology mission..
  • Invader - . Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-09-02 . USAF Sat Cat: 39577 . COSPAR: 2014-009F. Apogee: 336 km (208 mi). Perigee: 315 km (195 mi). Inclination: 65.0100 deg. Period: 91.04 min. Cubesat from Tama Art University..
  • Yui - . Payload: K-SAT2. Mass: 1.00 kg (2.20 lb). Nation: Japan. Class: Technology. Type: Education satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-04-26 . USAF Sat Cat: 39579 . COSPAR: 2014-009H. Apogee: 162 km (100 mi). Perigee: 145 km (90 mi). Inclination: 64.9900 deg. Period: 87.56 min. Cubesat from Kagoshima University..

2014 February 28 - . 04:20 GMT - . Launch Site: ISS. LV Family: Proton. Launch Vehicle: Proton-K.
  • Flock1-27 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-03 . USAF Sat Cat: 39565 . COSPAR: 1998-067EJ. Apogee: 193 km (119 mi). Perigee: 174 km (108 mi). Inclination: 51.6200 deg. Period: 88.17 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock1-28 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-03 . USAF Sat Cat: 39566 . COSPAR: 1998-067EK. Apogee: 152 km (94 mi). Perigee: 146 km (90 mi). Inclination: 51.6100 deg. Period: 87.47 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Ardusat-2 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-11-08 . USAF Sat Cat: 39567 . COSPAR: 1998-067EL. Apogee: 376 km (233 mi). Perigee: 373 km (231 mi). Inclination: 51.6400 deg. Period: 92.04 min. Cubesat from Nanosatisfi Inc., San Francisco, with an Arduino processor..
  • UAP-SAT - . Mass: 2.00 kg (4.40 lb). Nation: Peru. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-22 . USAF Sat Cat: 39568 . COSPAR: 1998-067EM. Apogee: 196 km (121 mi). Perigee: 183 km (113 mi). Inclination: 51.6200 deg. Period: 88.28 min. Cubesat from Universidad Alas Peruanas, Lima..
  • SkyCube 1 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-07-28 . USAF Sat Cat: 39569 . COSPAR: 1998-067EN. Apogee: 325 km (201 mi). Perigee: 320 km (190 mi). Inclination: 51.6400 deg. Period: 90.98 min. Cubesat from Southern Stars Group LLC, San Francisco, with an Earth imager..
  • Litsat 1 - . Mass: 2.00 kg (4.40 lb). Nation: Lithuania. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-23 . USAF Sat Cat: 39570 . COSPAR: 1998-067EP. Apogee: 180 km (110 mi). Perigee: 168 km (104 mi). Inclination: 51.5900 deg. Period: 87.97 min. Cubesat from the Lithuanian Space Association, Vilnius, Lithuania..
  • LituanicaSat-1 - . Mass: 2.00 kg (4.40 lb). Nation: Lithuania. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-07-01 . USAF Sat Cat: 39571 . COSPAR: 1998-067EQ. Apogee: 291 km (180 mi). Perigee: 281 km (174 mi). Inclination: 51.6400 deg. Period: 90.23 min. Cubesat from Kaunas Tech Univ. in Kaunas, Lithuania..

2014 April 18 - . 19:25 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: SLC40. LV Family: Falcon. Launch Vehicle: Falcon 9.
  • SporeSat - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Biology. Type: Biology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-06-04 . USAF Sat Cat: 39681 . COSPAR: 2014-022B. Apogee: 153 km (95 mi). Perigee: 151 km (93 mi). Inclination: 51.6200 deg. Period: 87.54 min. Cubesat for NASA Ames. Released from Falcon second stage..
  • TSat - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-28 . USAF Sat Cat: 39682 . COSPAR: 2014-022C. Apogee: 167 km (103 mi). Perigee: 153 km (95 mi). Inclination: 51.6100 deg. Period: 87.68 min. Cubesat for Taylor University. Released from Falcon second stage..
  • All-Star - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-26 . USAF Sat Cat: 39683 . COSPAR: 2014-022D. Apogee: 156 km (96 mi). Perigee: 154 km (95 mi). Inclination: 51.6400 deg. Period: 87.59 min. Cubesat for the Colorado Space Grant consortium. Released from Falcon second stage..
  • PhoneSat-2.5 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-15 . USAF Sat Cat: 39684 . COSPAR: 2014-022E. Apogee: 119 km (73 mi). Perigee: 109 km (67 mi). Inclination: 51.5400 deg. Period: 86.76 min. Cubesat for NASA Ames. Released from Falcon second stage..
  • Kicksat - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2014-05-14 . USAF Sat Cat: 39685 . COSPAR: 2014-022F. Apogee: 175 km (108 mi). Perigee: 160 km (90 mi). Inclination: 51.6500 deg. Period: 87.83 min.

    Cubesat for Cornell University's Space Systems Design Stuido. The satellite had a mass of 2.68 kg, of which 0.52 kg was to have been ejected on May 4 in the form of 104 tiny 5-gram Sprites, circuit boards which acted as independent satellites with small transmitters able to send a simple message to ground stations. A timer problem on Kicksat meant that the deployment of the Sprite subsatellites was reset to May 16. However, Kicksat, and its undeployed Sprites, were destroyed when it reentered on May 14.


2014 June 19 - . 19:11 GMT - . Launch Site: Dombarovskiy. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Duchifat 1 - . Mass: 1.00 kg (2.20 lb). Nation: Israel. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40021 . COSPAR: 2014-033M. Apogee: 623 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9700 deg. Period: 96.94 min. 1U cubesat by the Herzliya Science Center..
  • Pace - . Mass: 3.00 kg (6.60 lb). Nation: Taiwan. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40022 . COSPAR: 2014-033N. Apogee: 623 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.94 min. 2U cubesat for the National Cheng Kung University..
  • Flock 1C 10 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40023 . COSPAR: 2014-033P. Apogee: 623 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.94 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Nanosat C BR1 - . Mass: 1.00 kg (2.20 lb). Nation: Brazil. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40024 . COSPAR: 2014-033Q. Apogee: 623 km (387 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.94 min. 1U cubesat for the Southern Regional Space Research Center..
  • Qb50P1 - . Mass: 2.00 kg (4.40 lb). Nation: Belgium. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40025 . COSPAR: 2014-033R. Apogee: 623 km (387 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.95 min. 2U cubesat; part of a constellation of 50 CubeSats built by university teams to study the llower thermosphere..
  • Flock 1C 7 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40026 . COSPAR: 2014-033S. Apogee: 622 km (386 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.94 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1C 1 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40027 . COSPAR: 2014-033T. Apogee: 623 km (387 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.95 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Popsat Hip 1 - . Mass: 3.00 kg (6.60 lb). Nation: Singapore. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40028 . COSPAR: 2014-033U. Apogee: 625 km (388 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.96 min. 3U cubesat by Microspace Rapid..
  • Flock 1C 2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40029 . COSPAR: 2014-033V. Apogee: 625 km (388 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.97 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Dtusat 2 - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40030 . COSPAR: 2014-033W. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9700 deg. Period: 96.97 min. 1U cubesat by the Danish Technical University..
  • Flock 1C 4 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40031 . COSPAR: 2014-033X. Apogee: 624 km (387 mi). Perigee: 601 km (373 mi). Inclination: 97.9800 deg. Period: 96.95 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Qb50p2 - . Mass: 2.00 kg (4.40 lb). Nation: Belgium. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40032 . COSPAR: 2014-033Y. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 96.97 min. 2U cubesat; part of a constellation of 50 CubeSats built by university teams to study the llower thermosphere..
  • Flock 1C 11 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40033 . COSPAR: 2014-033Z. Apogee: 624 km (387 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.97 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Antelsat - . Mass: 3.00 kg (6.60 lb). Nation: Uruguay. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40034 . COSPAR: 2014-033AA. Apogee: 700 km (430 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.87 min. 2U cubesat by Uruguayan State Faculty of engineering; carried infrared imager and amateur radio payloads..
  • Flock 1C 9 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40035 . COSPAR: 2014-033AB. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 96.97 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1C 6 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40036 . COSPAR: 2014-033AC. Apogee: 624 km (387 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 96.98 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Perseus M2 - . Mass: 7.00 kg (15.40 lb). Nation: Russia. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40037 . COSPAR: 2014-033AD. Apogee: 626 km (388 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.99 min. 6U Cubesat by by Canopus Systems with an Automatic Identification System (AIS) receiver for tracking shipping..
  • Flock 1C 5 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40038 . COSPAR: 2014-033AE. Apogee: 626 km (388 mi). Perigee: 602 km (374 mi). Inclination: 97.9800 deg. Period: 96.98 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Perseus M1 - . Mass: 7.00 kg (15.40 lb). Nation: Russia. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40039 . COSPAR: 2014-033AF. Apogee: 627 km (389 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 97.01 min. 6U Cubesat by by Canopus Systems with an Automatic Identification System (AIS) receiver for tracking shipping..
  • Flock 1C 8 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40040 . COSPAR: 2014-033AG. Apogee: 626 km (388 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.99 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1C 3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40041 . COSPAR: 2014-033AH. Apogee: 625 km (388 mi). Perigee: 603 km (374 mi). Inclination: 97.9800 deg. Period: 96.98 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Polyitan 1 - . Mass: 1.00 kg (2.20 lb). Nation: Ukraine. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40042 . COSPAR: 2014-033AJ. Apogee: 628 km (390 mi). Perigee: 604 km (375 mi). Inclination: 97.9800 deg. Period: 97.01 min. 1U cubesat by National Technical University of Ukraine..
  • Tigrisat - . Mass: 3.00 kg (6.60 lb). Nation: Iraq. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40043 . COSPAR: 2014-033AK. Apogee: 698 km (433 mi). Perigee: 610 km (370 mi). Inclination: 97.9700 deg. Period: 97.81 min. 3U cubesat built by Iraqi students at the La Sapienza University of Rome..
  • Lemur 1 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40044 . COSPAR: 2014-033AL. Apogee: 697 km (433 mi). Perigee: 611 km (379 mi). Inclination: 97.9700 deg. Period: 97.82 min. 3U cubesat by NanoSatisfi Inc..
  • Aerocube 6a - . Mass: 10 kg (22 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40045 . COSPAR: 2014-033AM. Apogee: 700 km (430 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.87 min.
  • Aerocube 6b - . Mass: 10 kg (22 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40046 . COSPAR: 2014-033AN. Apogee: 700 km (430 mi). Perigee: 613 km (380 mi). Inclination: 97.9700 deg. Period: 97.87 min.

2014 June 30 - . 04:22 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota PSLV. LV Family: PSLV. Launch Vehicle: PSLV.
  • Velox 1 - . Mass: 4.00 kg (8.80 lb). Nation: Singapore. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40057 . COSPAR: 2014-034E. Apogee: 658 km (408 mi). Perigee: 639 km (397 mi). Inclination: 98.2500 deg. Period: 97.69 min. 3u cubesat by Singapore National Technical University; to have deployed the Velox P3 subsatellite..

2014 July 8 - . 15:58 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-2-1B.
  • Ukube 1 - . Mass: 3.00 kg (6.60 lb). Nation: UK. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40074 . COSPAR: 2014-037F. Apogee: 633 km (393 mi). Perigee: 623 km (387 mi). Inclination: 98.4000 deg. Period: 97.27 min. 3U cubesat sponsored by the UK Space Agency; first of a series to be launched annually to promote space technology in the UK..

2014 September 5 - . 09:29 GMT - . Launch Site: ISS.
  • Flock 1b-17 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. COSPAR: 1998-067FF. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-18 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. COSPAR: 1998-067FE. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..

2014 October 28 - . 22:20 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA0A. Launch Pad: Wallops MARS 0A. LV Family: Antares LV. Launch Vehicle: Antares 130.
  • RACE - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Apogee: 0.10 km (0.06 mi). Perigee: -6,378 km (-6,378 mi). Inclination: 51.6000 deg. JPL/U-Texas 3U cubesat. Lost in explosion of booster..
  • Arkyd-3 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Apogee: 0.10 km (0.06 mi). Perigee: -6,378 km (-6,378 mi). Inclination: 51.6000 deg. 3U cubesat from Planetary Resources. Lost in explosion of booster..
  • GOMX-2 - . Mass: 3.00 kg (6.60 lb). Nation: Denmark. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Apogee: 0.10 km (0.06 mi). Perigee: -6,378 km (-6,378 mi). Inclination: 51.6000 deg. Ship tracking 2U cubesat from GOMX of Aalborg, Denmark. Lost in explosion of booster..
  • Flock-1d 1 to 26 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. 26 PlanetLabs Flock-1d 3U cubesats. Lost in explosion of booster. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..

2015 January 31 - . 14:22 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Thor. Launch Vehicle: Delta 7320-10C.
  • FIREBIRD IIA - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Space science. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40377 . COSPAR: 2015-003B. Apogee: 643 km (399 mi). Perigee: 431 km (267 mi). Inclination: 99.1000 deg. Period: 95.38 min. 1.5U cubesat by NSF/Montana State/U. New Hampshire space science satellite. Sun synchronous orbit; 0600 GMT local time of the descending node..
  • FIREBIRD IIB - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Space science. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40378 . COSPAR: 2015-003C. Apogee: 643 km (399 mi). Perigee: 431 km (267 mi). Inclination: 99.1000 deg. Period: 95.38 min. 1.5U cubesat by NSF/Montana State/U. New Hampshire space science satellite. Sun synchronous orbit; 0600 GMT local time of the descending node..
  • GRIFEX - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40379 . COSPAR: 2015-003D. Apogee: 648 km (402 mi). Perigee: 433 km (269 mi). Inclination: 99.1000 deg. Period: 95.45 min. 3U cubesat by Michigan/JPL; technology satellite. Sun synchronous orbit; 0600 GMT local time of the descending node..
  • ExoCube CP10 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Earth. Type: Atmosphere satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40380 . COSPAR: 2015-003E. Apogee: 652 km (405 mi). Perigee: 434 km (269 mi). Inclination: 99.1000 deg. Period: 95.51 min. 3U cubesat by California Polytechnic. Sun synchronous orbit; 0600 GMT local time of the descending node..

2015 February 5 - . 12:50 GMT - . Launch Site: ISS. Launch Complex: ISS Japanese Experiment Module. Launch Pad: ISS Kibo RMS.
  • AESP-14 - . Mass: 1.00 kg (2.20 lb). Nation: Brazil. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-05-11 . USAF Sat Cat: 40389 . COSPAR: 1998-067FM. Apogee: 405 km (251 mi). Perigee: 397 km (246 mi). Inclination: 51.6000 deg. ISS cubesat deploys resumed after a five-month hiatus following deployer problems. Brazil's AESP-14 cubesat was ejected but appeared not to be transmitting..
  • Flock 1b-27 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-10-14 . USAF Sat Cat: 40422 . COSPAR: 1998-067FN. Apogee: 404 km (251 mi). Perigee: 396 km (246 mi). Inclination: 51.7000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-28 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-08-07 . USAF Sat Cat: 40423 . COSPAR: 1998-067FP. Apogee: 404 km (251 mi). Perigee: 396 km (246 mi). Inclination: 51.7000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-21 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-10-12 . USAF Sat Cat: 40427 . COSPAR: 1998-067FQ. Apogee: 402 km (249 mi). Perigee: 395 km (245 mi). Inclination: 51.7000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-22 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-10-03 . USAF Sat Cat: 40428 . COSPAR: 1998-067FR. Apogee: 402 km (249 mi). Perigee: 395 km (245 mi). Inclination: 51.7000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-9 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-08-23 . USAF Sat Cat: 40429 . COSPAR: 1998-067FS. Apogee: 407 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.6000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-10 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-06-28 . USAF Sat Cat: 40430 . COSPAR: 1998-067FT. Apogee: 413 km (256 mi). Perigee: 398 km (247 mi). Inclination: 51.6000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1d'-1 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-10-13 . USAF Sat Cat: 40451 . COSPAR: 1998-067FU. Apogee: 405 km (251 mi). Perigee: 393 km (244 mi). Inclination: 51.6000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1d'-2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40452 . COSPAR: 1998-067FV. Apogee: 313 km (194 mi). Perigee: 301 km (187 mi). Inclination: 51.6300 deg. Period: 90.67 min. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-5 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-08-17 . USAF Sat Cat: 40453 . COSPAR: 1998-067FW. Apogee: 407 km (252 mi). Perigee: 394 km (244 mi). Inclination: 51.6000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-6 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-10-16 . USAF Sat Cat: 40454 . COSPAR: 1998-067FX. Apogee: 407 km (252 mi). Perigee: 392 km (243 mi). Inclination: 51.6000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • TechEdSat-4 - . Mass: 4.00 kg (8.80 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-04-03 . USAF Sat Cat: 40455 . COSPAR: 1998-067FY. Apogee: 402 km (249 mi). Perigee: 393 km (244 mi). Inclination: 51.6000 deg. 3U cubesat of San Jose State University, the University of Idaho, and NASA Ames. Tested Exo-Brake passive de-orbit system..
  • GEARRSat - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-11-08 . USAF Sat Cat: 40456 . COSPAR: 1998-067FZ. Apogee: 404 km (251 mi). Perigee: 395 km (245 mi). Inclination: 51.6000 deg. First 3U Globalstar Risk Reduction satellite from startup Near Space Launch (a Taylor University spinoff), with AFRL, to demo cubesat data relay via the Globalstar system..
  • MicroMAS - . Mass: 6.00 kg (13.20 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-08-01 . USAF Sat Cat: 40457 . COSPAR: 1998-067GA. Apogee: 406 km (252 mi). Perigee: 393 km (244 mi). Inclination: 51.6000 deg. Three-axis stabilized 3U cubesat by the Space Systems Laboratory. Carried an MIT Lincoln Laboratory microwave radiometer payload..
  • LambdaSat - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Communications technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-05-16 . USAF Sat Cat: 40458 . COSPAR: 1998-067GB. Apogee: 405 km (251 mi). Perigee: 393 km (244 mi). Inclination: 51.6000 deg. 1U cubesat built by the Lambda Team of San Jose, California..
  • Flock 1b-11 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-09-07 . USAF Sat Cat: 40459 . COSPAR: 1998-067GC. Apogee: 405 km (251 mi). Perigee: 395 km (245 mi). Inclination: 51.6000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..
  • Flock 1b-12 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Decay Date: 2015-09-29 . USAF Sat Cat: 40460 . COSPAR: 1998-067GD. Apogee: 405 km (251 mi). Perigee: 395 km (245 mi). Inclination: 51.6000 deg. Part of a Planetary Labs constellation of over 100 3U cubesats to provide continuous optical surveillance of the earth..

2015 May 20 - . 15:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. Launch Pad: Cape Canaveral SLC40. LV Family: Atlas V. Launch Vehicle: Atlas V 501.
  • USS Langley - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40652 . COSPAR: 2015-025B. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. 3U cubesat from the US Naval Academy (UNSA) testing out an IP link to the satellite's computer which hosts a Unix webserver..
  • PSat-1 - . Payload: PARKINSONSAT (PSAT). Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40654 . COSPAR: 2015-025D. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. 1.5U cubesat from the US Naval Academy (UNSA) hosting the USN SCP/ODTML buoy communications payload and an amateur radio payload..
  • BRICSat-P - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40655 . COSPAR: 2015-025E. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. 1.5U cubesat from the US Naval Academy (UNSA), built in collaboration with George Washington University, testing an electric micropropulsion system..
  • GEARRS-2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40657 . COSPAR: 2015-025G. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. Second 3U Globalstar Risk Reduction satellite from startup Near Space Launch (a Taylor University spinoff), with AFRL, to demo cubesat data relay via the Globalstar system..
  • Aerocube-8a - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40659 . COSPAR: 2015-025J. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. Aerospace Corporation 1.5U cubesat testing an ion-electrospray propulsion system..
  • Aerocube-8b - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40660 . COSPAR: 2015-025K. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. Aerospace Corporation 1.5U cubesat testing carbon nanotube materials..
  • O/C-1 - . Payload: OPTICUBE 01. Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Surveillance. Type: Radar calibration target. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40653 . COSPAR: 2015-025C. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. 3U Optical Cubesat sponsored by NRO and built by Cal Poly as targets for space surveillance calibration..
  • O/C-2 - . Payload: OPTICUBE 02. Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Radar calibration target. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40656 . COSPAR: 2015-025F. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. 3U Optical Cubesat sponsored by NRO and built by Cal Poly as targets for space surveillance calibration..
  • O/C-3 - . Payload: OPTICUBE 03. Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Radar calibration target. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40658 . COSPAR: 2015-025H. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg. 3U Optical Cubesat sponsored by NRO and built by Cal Poly as targets for space surveillance calibration..
  • LightSail-A - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40661 . COSPAR: 2015-025L. Apogee: 700 km (430 mi). Perigee: 350 km (210 mi). Inclination: 55.0000 deg.

    Planetary Society's 3U cubesat with a solar sail deployment experiment. The cubesat went into safe mode a few days after launch but rebooted on May 30. Its solar panels were deployed on June 3 and the solar sail was unfurled on June 7 at 19:47 GMT. The satellite reentered on June 14.


2015 July 10 - . 16:28 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Pad: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
  • DeOrbitSail - . Mass: 3.00 kg (6.60 lb). Nation: UK. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: CubeSat. USAF Sat Cat: 40719 . COSPAR: 2015-032E. Apogee: 657 km (408 mi). Perigee: 634 km (393 mi). Inclination: 98.0400 deg. Period: 97.63 min. 3U cubesat. 22:10 local time longitude of descending node sun synchronous orbit..

2015 July 13 - . 16:40 GMT - . Launch Site: ISS. LV Family: PSLV. Launch Vehicle: PSLV-XL.
  • Flock 1e-1 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40722 . COSPAR: 1998-067GE. Apogee: 370 km (220 mi). Perigee: 361 km (224 mi). Inclination: 51.6400 deg. Period: 91.86 min.
  • Flock 1e-2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40723 . COSPAR: 1998-067GF. Apogee: 381 km (236 mi). Perigee: 373 km (231 mi). Inclination: 51.6400 deg. Period: 92.08 min.
  • Flock 1e-4 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40724 . COSPAR: 1998-067GG. Apogee: 379 km (235 mi). Perigee: 375 km (233 mi). Inclination: 51.6400 deg. Period: 92.09 min.
  • Flock 1e-3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40725 . COSPAR: 1998-067GH. Apogee: 374 km (232 mi). Perigee: 368 km (228 mi). Inclination: 51.6400 deg. Period: 91.97 min.
  • Flock 1e-5 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40728 . COSPAR: 1998-067GL. Apogee: 381 km (236 mi). Perigee: 373 km (231 mi). Inclination: 51.6400 deg. Period: 92.09 min.
  • Flock 1e-6 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40729 . COSPAR: 1998-067GM. Apogee: 380 km (230 mi). Perigee: 372 km (231 mi). Inclination: 51.6400 deg. Period: 92.07 min.
  • Flock 1e-7 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40726 . COSPAR: 1998-067GJ. Apogee: 381 km (236 mi). Perigee: 375 km (233 mi). Inclination: 51.6400 deg. Period: 92.11 min.
  • Flock 1e-8 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40727 . COSPAR: 1998-067GK. Apogee: 379 km (235 mi). Perigee: 371 km (230 mi). Inclination: 51.6400 deg. Period: 92.05 min.
  • Flock 1e-9 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40736 . COSPAR: 1998-067GN. Apogee: 381 km (236 mi). Perigee: 377 km (234 mi). Inclination: 51.6400 deg. Period: 92.13 min.
  • Flock 1e-10 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40737 . COSPAR: 1998-067GP. Apogee: 381 km (236 mi). Perigee: 375 km (233 mi). Inclination: 51.6400 deg. Period: 92.11 min.
  • Flock 1e-11 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40738 . COSPAR: 1998-067GQ. Apogee: 377 km (234 mi). Perigee: 371 km (230 mi). Inclination: 51.6400 deg. Period: 92.02 min.
  • Flock 1e-12 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40739 . COSPAR: 1998-067GR. Apogee: 382 km (237 mi). Perigee: 374 km (232 mi). Inclination: 51.6400 deg. Period: 92.12 min.
  • Flock 1e-13 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40740 . COSPAR: 1998-067GS. Apogee: 380 km (230 mi). Perigee: 374 km (232 mi). Inclination: 51.6400 deg. Period: 92.09 min.
  • Flock 1e-14 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40741 . COSPAR: 1998-067GT. Apogee: 380 km (230 mi). Perigee: 374 km (232 mi). Inclination: 51.6400 deg. Period: 92.08 min.
  • Centennial-1 - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Surveillance. Type: Radar calibration target. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40742 . COSPAR: 1998-067GU. Apogee: 337 km (209 mi). Perigee: 328 km (203 mi). Inclination: 51.6400 deg. Period: 91.18 min. 1U cubesat by Booz Allen, used as a space surveillance target by the USAF..
  • Arkyd-3R - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40743 . COSPAR: 1998-067GV. Apogee: 354 km (219 mi). Perigee: 345 km (214 mi). Inclination: 51.6400 deg. Period: 91.53 min. 3U cubesat from Planetary Resources, testing software and systems for future Arkyd satellites..
  • S-CUBE - . Mass: 3.00 kg (6.60 lb). Nation: Japan. Class: Astronomy. Type: Astronomy satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40898 . COSPAR: 1998-067GY. Apogee: 397 km (246 mi). Perigee: 388 km (241 mi). Inclination: 51.6400 deg. Period: 92.40 min. S-CUBE meteor-observation cubesat from Chiba Institute of Technology; ejected from the J-SSOD deployer on the Kibo robot arm on 17 September..
  • SERPENS - . Mass: 4.00 kg (8.80 lb). Nation: Brazil. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: CubeSat. USAF Sat Cat: 40897 . COSPAR: 1998-067GX. Apogee: 384 km (238 mi). Perigee: 380 km (230 mi). Inclination: 51.6400 deg. Period: 92.19 min. SERPENS 3U cubesat from the University of Brasilia; ejected from the J-SSOD deployer on the Kibo robot arm on 17 September..

2015 September 19 - . 23:01 GMT - . Launch Site: Taiyuan. Launch Complex: Taiyuan LC16. LV Family: CZ-NGLV. Launch Vehicle: Chang Zheng 6.
  • DCBB - . Payload: KAITUO 1B. Mass: 2.00 kg (4.40 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40912 . COSPAR: 2015-049P. Apogee: 536 km (333 mi). Perigee: 510 km (310 mi). Inclination: 97.4600 deg. Period: 95.10 min. 2U cubesat with an amateur radio payload..

2015 September 25 - . 01:41 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan SLS-2. Launch Pad: Jiuquan SLS-E. LV Family: CZ-NGLV. Launch Vehicle: Chang Zheng 11.
  • Shangkeda-2 - . Payload: TIANWANG 1C (TW-1C). Mass: 3.00 kg (6.60 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40926 . COSPAR: 2015-051B. Apogee: 485 km (301 mi). Perigee: 460 km (280 mi). Inclination: 97.3000 deg. Period: 94.04 min.

    Part of the Tianwang constallation of three CubeSats for space networking experiments. Codeveloped by the Shanghai Engineering Center for Microsatellites (SECM), the Nanjing University of Science and Technology (NJUST), GomSpace Denmark, Tekever Space Portugal and NanoSpace Sweden.

  • NJUST-2 - . Payload: TIANWANG 1B (TW-1B). Mass: 3.00 kg (6.60 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40927 . COSPAR: 2015-051C. Apogee: 485 km (301 mi). Perigee: 462 km (287 mi). Inclination: 97.3100 deg. Period: 94.07 min.
  • NJFA-1 - . Payload: TIANWANG 1A (TW-1A). Mass: 3.00 kg (6.60 lb). Nation: China. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40928 . COSPAR: 2015-051D. Apogee: 485 km (301 mi). Perigee: 463 km (287 mi). Inclination: 97.2900 deg. Period: 94.08 min.

2015 September 28 - . 04:30 GMT - . Launch Site: Sriharikota. Launch Complex: Sriharikota SLP. Launch Pad: Sriharikota FLP. LV Family: PSLV. Launch Vehicle: PSLV-XL.
  • Lemur-2-Joel - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40933 . COSPAR: 2015-052D. Apogee: 650 km (400 mi). Perigee: 629 km (390 mi). Inclination: 6.0100 deg. Period: 97.50 min.

    3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.

  • Lemur-2-Peter - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40934 . COSPAR: 2015-052E. Apogee: 650 km (400 mi). Perigee: 634 km (393 mi). Inclination: 6.0100 deg. Period: 97.55 min.

    3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.

  • Lemur-2-Jeroen - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40935 . COSPAR: 2015-052F. Apogee: 650 km (400 mi). Perigee: 634 km (393 mi). Inclination: 6.0100 deg. Period: 97.56 min.

    3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.

  • Lemur-2-Chris - . Mass: 5.00 kg (11.00 lb). Nation: Canada. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40936 . COSPAR: 2015-052G. Apogee: 650 km (400 mi). Perigee: 635 km (394 mi). Inclination: 6.0000 deg. Period: 97.57 min.

    3U cubesat by San Francisco-based Spire Global, built in Glasgow, Scotland. 3U cubesat, carried an AIS payload and GPS radio occultation equipment, which used the bending of GPS radio signals by the atmosphere to derive atmospheric temperature and pressure.


2015 October 5 - . 14:05 GMT - . Launch Site: ISS. LV Family: Atlas V. Launch Vehicle: Atlas V 421.
  • AAUSAT-5 - . Mass: 1.00 kg (2.20 lb). Nation: Denmark. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40949 . COSPAR: 1998-067HA. Apogee: 393 km (244 mi). Perigee: 385 km (239 mi). Inclination: 51.6400 deg. Period: 92.33 min. Aalborg University 1U cubesat for tests of AIS ship tracking receivers.
  • GOMX-3 - . Mass: 5.00 kg (11.00 lb). Nation: Denmark. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40948 . COSPAR: 1998-067GZ. Apogee: 387 km (240 mi). Perigee: 381 km (236 mi). Inclination: 51.6400 deg. Period: 92.24 min. GOMSpace 3U cubesat for tests of ADS-B aircraft data relay.
  • Flock 2b-1 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40950 . COSPAR: 1998-067HB. Apogee: 391 km (242 mi). Perigee: 387 km (240 mi). Inclination: 51.6400 deg. Period: 92.34 min.
  • Flock 2b-2 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40951 . COSPAR: 1998-067HC. Apogee: 391 km (242 mi). Perigee: 387 km (240 mi). Inclination: 51.6400 deg. Period: 92.33 min.
  • Flock 2b-3 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40952 . COSPAR: 1998-067HD. Apogee: 391 km (242 mi). Perigee: 389 km (241 mi). Inclination: 51.6400 deg. Period: 92.35 min.
  • Flock 2b-4 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40953 . COSPAR: 1998-067HE. Apogee: 392 km (243 mi). Perigee: 389 km (241 mi). Inclination: 51.6400 deg. Period: 92.36 min.
  • Flock 2b-5 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40954 . COSPAR: 1998-067HF. Apogee: 394 km (244 mi). Perigee: 385 km (239 mi). Inclination: 51.6400 deg. Period: 92.34 min.
  • Flock 2b-6 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40955 . COSPAR: 1998-067HG. Apogee: 397 km (246 mi). Perigee: 389 km (241 mi). Inclination: 51.6400 deg. Period: 92.41 min.
  • Flock 2b-7 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40956 . COSPAR: 1998-067HH. Apogee: 392 km (243 mi). Perigee: 384 km (238 mi). Inclination: 51.6400 deg. Period: 92.32 min.
  • Flock 2b-8 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40957 . COSPAR: 1998-067HJ. Apogee: 387 km (240 mi). Perigee: 382 km (237 mi). Inclination: 51.6400 deg. Period: 92.24 min.
  • Flock 2b-9 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40962 . COSPAR: 1998-067HK. Apogee: 394 km (244 mi). Perigee: 385 km (239 mi). Inclination: 51.6400 deg. Period: 92.34 min.
  • Flock 2b-10 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40963 . COSPAR: 1998-067HL. Apogee: 394 km (244 mi). Perigee: 386 km (239 mi). Inclination: 51.6400 deg. Period: 92.36 min.
  • Flock 2b-13 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40979 . COSPAR: 1998-067HM. Apogee: 394 km (244 mi). Perigee: 385 km (239 mi). Inclination: 51.6400 deg. Period: 92.35 min.
  • Flock 2b-14 - . Mass: 5.00 kg (11.00 lb). Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40980 . COSPAR: 1998-067HN. Apogee: 391 km (242 mi). Perigee: 384 km (238 mi). Inclination: 51.6400 deg. Period: 92.31 min.

2015 October 8 - . 12:49 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas V. Launch Vehicle: Atlas V 401.
  • Aerocube-5C - . Mass: 10 kg (22 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40965 . COSPAR: 2015-058B. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. Aerospace Corporation cubesat..
  • Aerocube-7 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40966 . COSPAR: 2015-058C. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. Aerospace Corporation cubesat..
  • AMSAT-OSCAR-85 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Communications technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40967 . COSPAR: 2015-058D. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. Also called Fox-1A; amateur radio cubesat from AMSAT-North America..
  • Bisonsat - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40968 . COSPAR: 2015-058E. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. Cubesat from Salish Kootenai College in Montana..
  • ARC-1 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40969 . COSPAR: 2015-058F. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. Alaska Research Cubesat 1 from University of Alaska, Fairbanks..
  • SNAP-3 ALICE - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40970 . COSPAR: 2015-058G. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. One of three SMDC Nanosatellite Program (SNAP-3) communications cubesats for the US Army Strategica Missile Defence Command..
  • LMRST - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40971 . COSPAR: 2015-058H. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. Low Mass Radio Science Transponder experiment cubesat from JPL..
  • SNAP-3 EDDIE - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40972 . COSPAR: 2015-058J. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. One of three SMDC Nanosatellite Program (SNAP-3) communications cubesats for the US Army Strategica Missile Defence Command..
  • PropCube-3 Merryweather - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40973 . COSPAR: 2015-058K. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. One of two PropCube ionospheric-propagation-study cubesats from Tyvak Nanosystems and the US Navy Postgraduate School..
  • SINOD-D 1 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40974 . COSPAR: 2015-058L. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. One of two SINOD-D cubesats with software-defined radio demonstrations from SRI International..
  • SNAP-3 JIMI - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40975 . COSPAR: 2015-058M. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. One of three SMDC Nanosatellite Program (SNAP-3) communications cubesats for the US Army Strategica Missile Defence Command..
  • PropCube-1 Flora - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Science. Type: Science satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40976 . COSPAR: 2015-058N. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. One of two PropCube ionospheric-propagation-study cubesats from Tyvak Nanosystems and the US Navy Postgraduate School..
  • SINOD-D 3 - . Mass: 2.00 kg (4.40 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. USAF Sat Cat: 40977 . COSPAR: 2015-058P. Apogee: 802 km (498 mi). Perigee: 500 km (310 mi). Inclination: 64.8000 deg. One of two SINOD-D cubesats with software-defined radio demonstrations from SRI International..

2015 November 4 - . 03:45 GMT - . Launch Site: Barking Sands. LV Family: Strypi. Launch Vehicle: Super Strypi. FAILURE: Went out of control during first stage burn and was destroyed.
  • Hiakasat - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat.

    Launched from the Kauai Test Facility's Kokole Point pad; went out of control during first stage burn and was destroyed. The University of Hawaii's Hiakasat and 12 cubesats were aboard. The vehicle had three solid stages (LEO-46, LEO-7 and LEO-1) developed by Aerojet.

  • STACEM - . Nation: USA. Class: Surveillance. Type: Surveillance satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • PrintSat - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • Techsat-1 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 1 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 2 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 3 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 4 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 5 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 6 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 7 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • EDSN 8 - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..
  • Argus - . Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft Bus: Cubesat. Spacecraft: Cubesat. Cubesat; lost when first stage failed..


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