Fengyun 2-08 (FY 2G) |
China |
Spacecraft nº: |
Chinese spacecraft nº: 243 |
| Designation | 40367 / 14090A |
| Launch date | 31 Dec 2014 - 01:02 UT |
| Launch site | Xichang, LC-2 |
| Launch vehicle | CZ-3A |
| Mission | Weather |
| Geostationary orbit: | |
| Perigee / Apogee | 35770 x 35800 km |
| Eccentricity | |
| Inclination | 2.3° |
| Period | min |
| Prime manufacturer | |
| Platform | |
| Operator | China's National Satellite Monitoring Centre |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Date | Position | Remarks |
| Jan 2015 | 100° E |
| Ref.: #7(JR707-708), #228 - update: 02.04.15 | Home |