Zhongxing-2D (ZX-2D, ChinaSat-2D) |
China (PRC) |
Int. spacecraft nº: |
Chinese spacecraft nº: 457 |
| Designation | 43920 / 19001A |
| Launch date | 10 Jan 2019 - 17:11 UT |
| Launch site | Xichang, LC-2 |
| Launch vehicle | CZ-3B/G3 |
| Mission | Military Communication |
| Geostationary orbit: | |
| Perigee / Apogee | 35788 x 35799 km |
| Eccentricity | |
| Inclination | 0.0° |
| Period | 1436.1 min |
| Prime manufacturer | CAST |
| Platform | DFH-4 bus |
| Operator | People's Liberation Army (PLA) |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Date | Position | Remarks |
| 22 Jan 2019 | 130.0° E |
| Ref.: #7(JR760,766), #14, #228 - update: 14.03.19 | Home |