Designation | 28941 / 06005C |
Launch date | 21 Feb 2006 |
Country of origin | Japan |
Mission | Technology |
Perigee/Apogee | 300 x 711 km |
Inclination | 98.2° |
Period | 94.7 min |
Launch vehicle | Mu 5 #29 |
Out of service | |
Cause | |
Decay | planned in Oct 2009 |
Prime contractor | |
Platform | |
Mass at launch | 10 kg |
Dry mass | |
Dimension | 10 x 10 x 20 cm |
Solar array | |
Stabilization | |
DC power | |
Design lifetime |