Yaogan 30-05-01, 02 & 03 (CX-5 13/15) |
China (PRC) |
Spacecraft nº: |
Chinese spacecraft nº: 480/82 |
| Type | Yaogan 30-05-01 | Yaogan 30-05-02 | Yaogan 30-05-03 |
| - | Yaogan-30N | Yaogan-30P | Yaogan-30Q |
| Other name | Chuangxin-5 13 | Chuangxin-5 14 | Chuangxin-5 15 |
| NORAD ID | 44449 | 44450 | 44451 |
| Designation | 19045A | 19045B | 19045C |
| Launch date | 26 July 2019 - 03:57 UTC | ||
| Launch site | Xichang, LC-3 | ||
| Launch vehicle | CZ-2C | ||
| Mission | Mil: Sigint? | ||
| Earth orbit: | |||
| Perigee / Apogee | 603x608 km | 598x614 km | 605x607 km |
| Inclination | 35.0° | ||
| Period | 96.7 min | ||
| Decay | |||
| Prime manufacturer | Chinese Academy of Sciences' (CAS) Small Satellite Center |
| Platform | |
| Operator | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime |
| Ref.: #7(JR767), #228 - update: 11.11.19 | Home |