KSAT 2 [Kagoshima University]
KSAT 2 (Kagoshima Satellite 2, also named Hayato 2) is a small 1U CubeSat mission developed by the Kagoshima University. It is a modified reflight of the failed KSAT (Hayato) satellite.
The objectives of the mission are:
Nation: | Japan |
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Type / Application: | Technology |
Operator: | Kagoshima University |
Contractors: | Kagoshima University |
Equipment: | |
Configuration: | CubeSat (1U) |
Propulsion: | None |
Power: | 2 deployable fixed solar arrays, solar cells, batteries |
Lifetime: | ? |
Mass: | 1.5 kg |
Orbit: | 382 km × 388 km, 65.01° |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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KSAT 2 (Hayato 2) | 2014-009G | 27.02.2014 | Ta YLP-1 | H-2A-202 | with GPM-Core, STARS 2, ShindaiSat, TeikyoSat 3, OPUSAT, INVADER, ITF 1 |