Designation | 26064 / 00004D |
Launch date | 27 Jan 2000 |
Country of origin | United States |
Mission | Technology |
Perigee/Apogee | 773 km |
Inclination | 100.2° |
Period | 100.4 min |
Launch vehicle | Minotaur #1 |
Out of service | Feb 2000 |
Cause | Power system failure |
Decay |
Prime contractor | |
Platform | |
Mass at launch | 52 kg |
Mass in orbit | |
Dimension | |
Solar array | |
Stabilization | |
DC power | |
Design lifetime |