Designation | 26546 / 00057B |
Launch date | 26 Sep 2000 |
Country of origin | Italy |
Mission | Technology |
Perigee/Apogee | 631/649 km |
Inclination | 64.6° |
Period | |
Launch vehicle | Dnepr #2 |
Launch site | Tyuratam |
Out of service | |
Cause | |
Decay | 4 Nov 2003 |
Prime contractor | Megsat |
Platform | |
Mass at launch | 56 kg |
Mass in orbit | |
Dimension | |
Solar array | |
Stabilization | |
DC power | |
Design lifetime |