Yaogan 30-04-01, 02 & 03 (CX-5 10/12) |
China (PRC) |
Spacecraft nº: |
Chinese spacecraft nº: 370/372 |
| Type | Yaogan 30-04-01 | Yaogan 30-04-02 | Yaogan 30-04-03 |
| Other name | Chuangxin-5 10 | Chuangxin-5 11 | Chuangxin-5 12 |
| NORAD ID | 43170 | 43171 | 43172 |
| Designation | 18011B | 18011C | 18011D |
| Launch date | 25 Jan 2018 - 05:39 UTC | ||
| Launch site | Xichang, LC-3 | ||
| Launch vehicle | CZ-2C | ||
| Mission | Mil: Sigint? | ||
| Earth orbit: | |||
| Perigee / Apogee | 591 x 602 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(JR745), #228 - update: 08.02.18 | Home |