Spacecraft information: FENGYUN 1B
| Launched | 2 September 1990 |
| Flight ended | – |
| Status | Non-operational |
| Launch site | Taiyuan Space Center, PRC |
| Owner | People's Republic of China |
| NORAD ID | 20788 |
| COSPAR ID | 1990-081A |
| Alternative names |
FY-1B |
| Observing |
Current orbital elements
| Inclination | 98.959° |
| Eccentricity | 0.00157 |
| RA ascending node | 1.039 hr |
| Argument perigee | 351.498° |
| Mean anomaly | 8.591° |
| Orbital period | 102.624 min |
| Epoch of osculation | 02 Feb 2026, 10:25 |
Derived Quantities
| Min Altitude | 878.5 km |
| Mean Altitude | 889.9 km |
| Peak Altitude | 901.4 km |
Launched alongside
QQW-1 QQW-2 CZ-4 R/B CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEB CZ-4 DEBOrbital History
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