FENGYUN 1C DEB, 32192
Orbit data source: Space-Track
FENGYUN 1C DEB, 32192 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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32192 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: 4 days ago
TLE from 4 days ago
0 FENGYUN 1C DEB
1 32192U 99025CUN 25299.38793296 .00000477 00000-0 42162-3 0 9992
2 32192 98.6557 174.0661 0181294 291.4156 66.7745 13.82461771920586Epoch: 2025-10-26T09:18Z
TLE epoch observation values (Epoch: 2025-10-26T09:18:37.407Z)
Latitude
-0.00007°
Longitude
-0.5946°
Altitude
907.653 km
Speed
7.424 km/s
True Right ascension
11h 36m 15s
True Declination
0° 00' 00"
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
10:20:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,085.271 km
Perigee altitude
819.475 km
Semi-major axis
7,330.51 km
Eccentricity
0.01813
Inclination
98.6557°
RAAN
174.0661°
Arg. of periapsis
291.4156°
True anomaly
68.70046°
Mean anomaly
66.7745°
Eccentric anomaly
67.7358°
Mean motion
3.45813 °/min
Orbital period
104.1 mins
BSTAR
0.00042162
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-30 15:53:15.288Z | 173.302° S | 2025-10-30 15:59:15.288Z | 272.029° WNW | 43.645° | 2025-10-30 16:05:15.288Z | 342.458° N |
| 11 mins | 2025-10-31 04:33:15.288Z | 16.252° NNE | 2025-10-31 04:38:15.288Z | 73.257° E | 44.609° | 2025-10-31 04:44:15.288Z | 191.048° SSW |
| 7 mins | 2025-10-31 06:17:15.288Z | 333.59° NNW | 2025-10-31 06:20:15.288Z | 303.381° NW | 17.329° | 2025-10-31 06:24:15.288Z | 263.52° W |
| 8 mins | 2025-10-31 14:32:15.288Z | 104.802° ESE | 2025-10-31 14:35:15.288Z | 67.331° ENE | 24.382° | 2025-10-31 14:40:15.288Z | 11.917° NNE |
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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