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 |
|