RocketChang Zheng 11variant H
SpaceportYellow Sea (sea launch)pad LP2
OutcomeSuccess
Launch agencyCALTChina
Flight
- Date and time (UTC)
- September 15, 2020, 01:23
- Launch designation
- 2020-065
- Mission
- Jilin-1
- Flight name
- Jilin-1 03B/03C
- Vehicle flight ID
- Y2
- Year
- Launches in 2020
Orbit and payload
- Initial perigee
- 531 km
- Initial apogee
- 547 km
- Inclination
- 97.5°
- Payload mass to orbit
- 0.378 t
- Payloads
- 9
- GCAT launch code
- OS
Payloads
| Payload | Designation | Owner | Mission type | Mass | Fate |
|---|---|---|---|---|---|
| Jilin-1 GaoFen 03B 01 xing | 2020-065ANORAD 46454 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | Reentered (orbital decay) · Apr 27, 2026 |
| Jilin-1 GaoFen 03B 02 xing | 2020-065BNORAD 46455 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | Reentered (orbital decay) · Feb 11, 2026 |
| Jilin-1 GaoFen 03B 03 xing | 2020-065CNORAD 46456 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | Reentered (orbital decay) · Jan 2, 2026 |
| Jilin-1 GaoFen 03B 04 xing | 2020-065DNORAD 46457 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | In orbit |
| Jilin-1 GaoFen 03B 05 xing | 2020-065ENORAD 46458 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | In orbit |
| Jilin-1 GaoFen 03B 06 xing | 2020-065FNORAD 46459 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | Reentered (orbital decay) · Sep 25, 2026 |
| Jilin-1 GaoFen 03C 01 xing | 2020-065GNORAD 46460 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | Reentered (orbital decay) · Oct 19, 2026 |
| Jilin-1 GaoFen 03C 02 xing | 2020-065HNORAD 46461 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | Reentered (orbital decay) · Jun 9, 2026 |
| Jilin-1 GaoFen 03C 03 xing | 2020-065JNORAD 46462 | Chang Guang Satellite Technology Ltd | Optical imaging | 42 kg | Reentered (orbital decay) · May 11, 2026 |
Source: GCAT launch list and payload catalogs, Jonathan C. McDowell (CC BY 4.0). Orbit values are the initial orbit reported for the launch.