Ziyuan-3 02 (ZY-3 02) |
China |
Int. spacecraft nº: |
Chinese spacecraft nº: 293 |
| Designation | 41556 / 16033A |
| Launch date | 30 May 2016 - 03:17 UT |
| Launch site | Taiyuan, LC-9 |
| Launch vehicle | CZ-4B |
| Mission | Governm.: Earth observation, Imaging |
| LEO, Sun-Synchronous Earth orbit: | |
| Perigee / Apogee | 484 x 499 km |
| Eccentricity | 947E-04 |
| Inclination | 97.5 ° |
| Period | 94.49 min |
| Prime manufacturer | China Academy of Space Technology (CAST) |
| Platform | |
| Operator | China Centre for Resources Satellite Data and Application (CRESDA) |
| Mass at launch | 2630 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | 4 yrs |
| Ref.: #7(JR726), #226 - update: 23.04.17 | Home |