Spacecraft data:
| Prime contractor | Polyot (Russia) |
| Platform | |
| Operator | Russian Space Agency |
| Mass at launch | 171 kg |
| Dry Mass | 55 kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| DC power | 330 W |
| Design lifetime | 5 yrs |
|
Decay:
| Out of service: | Dec 2011 |
| Cause: | |
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