Spacecraft data:
| Prime contractor | Polyot/Moscow State University |
| Platform | |
| Operator | Moscow State University (MSU) |
| Mass at launch | 120 kg |
| Dry Mass | 98 kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | Solar cells |
| Stabilization | |
| DC power | |
| Design lifetime | 1-3 yrs |
|
Decay:
| Out of service: | Dec 2011 |
| Cause: | |
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