Designation | n/a |
Launch date | 29 Nov 2003 |
Country of origin | Japan |
Mission | Military: reconnaissance |
Perigee/Apogee | 500 km, near-polar |
Inclination | 97.3° |
Period | (4-day revisit) |
Launch vehicle | H2A #13 Failed |
Prime contractor | Mitsubishi Electric |
Platform | |
Mass at launch | 850 kg |
Mass in orbit | |
Dimension | |
Solar array | |
Stabilization | |
DC power | |
Design lifetime | 5 years |