Designation | 22561 / 93014A |
Launch date | 25 Mar 1993 |
Country of origin | CIS |
Mission | Test |
Perigee/Apogee | 680/968 km |
Inclination | 75.8° |
Period | 101.4 min |
Launch vehicle | Start #1 |
Prime contractor | |
Platform | |
Mass at launch | |
Dry mass | 260 kg |
Dimension | two cylinders < 1.5 m diameter |
Solar array | |
Stabilization | gravity-gradient |
DC power | |
Design lifetime |