Spacecraft n°: |
US spacecraft n°: |
DUMMY MASS 2
Launch data:
| Designation | 24926 / 97048B |
| Launch date | 01 Sept 1997 |
| Launch site | Taiyuan |
| Launch vehicle |
CZ-2C/SD (#F15) |
| Mission | |
| Perigee / Apogee | 619 x 629 km |
| Eccentricity | |
| Inclination | 86.3 deg |
| Period | 97.0 min |
Spacecraft data:
| Prime contractor | |
| Platform | |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | |
Mission details:
- Dummy satellite to test Long March 2 (China) as rocket for launching Iridium satellites.
Ref.: #228 - update: 31.03.12