Designation | 27848 / 03031J |
Launch date | 30 Jun 2003 |
Country of origin | Japan |
Mission | Technology |
Perigee/Apogee | 817/832 km, sunsynchronous |
Inclination | 98.72° |
Period | 101 min |
Launch vehicle | Rokot #9 |
Prime contractor | |
Platform | |
Mass at launch | 1 kg |
Mass in orbit | |
Dimension | 10 x 10 x 10 cm |
Solar array | |
Stabilization | |
DC power | |
Design lifetime |