Spacecraft data:
| Prime contractor | CAST |
| Operator | |
| Platform | |
| Mass at launch | 3800? kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension | |
| Solar array | |
| Stabilization | |
| Propulsion | FG-23A retro-motor ? |
|
Decay:
| Out of service: | 28 Sep 2005 - ~23:31 UT |
| Cause: | Recovery descent module |
Descent date equipment module: | 16 Oct 2005 |
| Lifetime: | |
|