Spacecraft data:
Prime contractor | Soka University |
Platform | Cubesat |
Operator | Soka University in Tokyo |
Mass at launch | 1 kg |
Dry Mass | kg |
Basic shape | Cube |
Dimension (m) | 0.1 side |
Solar array | |
Stabilization | |
Propulsion | none |
DC power | |
|
Decay:
Descent date: | 26 Jun 2010 |
Lifetime: | 37 days |
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