Yaogan 30-06-01, 02 & 03 (CX-5 16/18) |
China (PRC) |
Spacecraft nº: |
Chinese spacecraft nº: 542 / 44 |
| Type | Yaogan 30-06-01 | Yaogan 30-06-02 | Yaogan 30-06-03 |
| Other name | Chuangxin-5 16 | Chuangxin-5 17 | Chuangxin-5 18 |
| NORAD ID | 45460 | 45461 | 45462 |
| Designation | 20021A | 20021B | 20021C |
| Launch date | 24 Mar 2020 - 03:43 UTC | ||
| Launch site | Xichang, LC-3 | ||
| Launch vehicle | CZ-2C | ||
| Mission | Mil: Sigint | ||
| Earth orbit: | |||
| Perigee / Apogee | 591 x 602 km | 591 x 602 km | 591 x 602 km |
| Inclination | 35.0° | ||
| Period | 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(JR777) - update: 01.05.20 | Home |