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 |