Designation | 28221 / 04012B |
Launch date | 18 Apr 2004 |
Country of origin | China |
Mission | Technology |
Perigee/Apogee | 599/615 km |
Inclination | 97.7° |
Period | 97 min |
Launch vehicle | Long March 2C |
Prime contractor | Tsinghua University |
Platform | |
Mass at launch | < 25 kg |
Mass in orbit | |
Dimension | |
Solar array | |
Stabilization | |
DC power | |
Design lifetime |