Designation | 23105 / 94029A |
Launch date | 19 May 1994 |
Country of origin | United States |
Mission | Military: technology |
Perigee/Apogee | 604/818 km |
Inclination | 81.9° |
Period | 99 min |
Launch vehicle | Pegasus #5 |
Prime contractor | TRW |
Platform | STEP |
Mass at launch | |
Mass in orbit | |
Dimension | |
Solar array | |
Stabilization | 3-axis |
DC power | 95 W |
Design lifetime | 1 year |