Spacecraft information: CZ-4 DEB
| Launched | 2 September 1990 |
| Flight ended | 6 September 2025 |
| Status | Decayed |
| Launch site | Taiyuan Space Center, PRC |
| Owner | People's Republic of China |
| NORAD ID | 20865 |
| COSPAR ID | 1990-081AD |
| Observing |
Current orbital elements
| Inclination | 98.150° |
| Eccentricity | 0.00140 |
| RA ascending node | 18.225 hr |
| Argument perigee | 219.059° |
| Mean anomaly | 140.969° |
| Orbital period | 89.588 min |
| Epoch of osculation | 06 Sep 2025, 19:48 |
Derived Quantities
| Min Altitude | 252.0 km |
| Mean Altitude | 261.3 km |
| Peak Altitude | 270.5 km |
Launched alongside
FENGYUN 1B 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 DEBOrbital History
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