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 | 98.967° |
| Eccentricity | 0.00152 |
| RA ascending node | 4.063 hr |
| Argument perigee | 217.038° |
| Mean anomaly | 142.974° |
| Orbital period | 102.623 min |
| Epoch of osculation | 20 Mar 2026, 11:57 |
Derived Quantities
| Min Altitude | 878.9 km |
| Mean Altitude | 889.9 km |
| Peak Altitude | 900.9 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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