ZX-9A (ChinaSat-9A) |
China |
Int. spacecraft nº: |
Chinese spacecraft nº: 338 |
| Designation | 42763 / 17035A |
| Launch date | 18 June 2017 - 16:11 UT |
| Launch site | Xichang, LC-2 |
| Launch vehicle | CZ-3B/G2 |
| Mission | Communications |
| Earth orbit: | |
| Perigee / Apogee | 193 x 16357 km |
| Eccentricity | |
| Inclination | 25.7° |
| Period | min |
| Prime manufacturer | China Academy of Space Technology (CAST) |
| Platform | DFH-4 bus |
| Operator | Sino Satellite Communications ? China Satcom |
| Mass at launch | 5100 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | 24 Ku-band transponders |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | 15 yrs |
| Ref.: #7(JR739,740), #228 - update: 19.12.17 | Home |