FENGYUN 1C DEB, 32212
Orbit data source: Space-Track
FENGYUN 1C DEB, 32212 is space debris in SSO originally from a launch on Mon, 10 May 1999 UTC launched from the Taiyaun Space Center, China (TSC). Fengyun 1C debris stems from the Chinese weather satellite Fengyun-1C, which was intentionally destroyed by a Chinese anti-satellite missile in 2007. This event dramatically increased the amount of space debris, with thousands of trackable fragments posing hazards to satellites and human spaceflight. The Fengyun 1C debris cloud has become a focal point in discussions about space sustainability and the need for international regulations to prevent the creation of new debris.
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32212 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 FENGYUN 1C DEB
1 32212U 99025CVJ 25297.52264895 .00002884 00000-0 83504-3 0 9996
2 32212 99.5740 28.4269 0137830 220.7237 154.4259 14.40018857953535Epoch: 2025-10-24T12:32Z
TLE epoch observation values (Epoch: 2025-10-24T12:32:36.869Z)
Latitude
15.5738°
Longitude
164.42663°
Altitude
849.654 km
Speed
7.383 km/s
True Right ascension
01h 42m 59s
True Declination
15° 29' 10"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:17:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
853.935 km
Perigee altitude
657.287 km
Semi-major axis
7,133.748 km
Eccentricity
0.01378
Inclination
99.574°
RAAN
28.4269°
Arg. of periapsis
220.7237°
True anomaly
155.09724°
Mean anomaly
154.4259°
Eccentric anomaly
154.76261°
Mean motion
3.60219 °/min
Orbital period
99.94 mins
BSTAR
0.00083504
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Other satellites on launch #25 in the year 1999 (1999-05-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FENGYUN 1C DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-30 05:20:34.456Z | 128.369° SE | 2025-10-30 05:24:34.456Z | 77.834° E | 29.612° | 2025-10-30 05:29:34.456Z | 5.037° NNE |
| 7 mins | 2025-10-30 07:00:34.456Z | 213.293° SW | 2025-10-30 07:03:34.456Z | 260.241° W | 27.495° | 2025-10-30 07:07:34.456Z | 318.34° NNW |
| 8 mins | 2025-10-30 19:08:34.456Z | 17.585° NNE | 2025-10-30 19:12:34.456Z | 139.71° SSE | 44.488° | 2025-10-30 19:16:34.456Z | 192.004° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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