FENGYUN 1C DEB, 31367
Orbit data source: Space-Track
FENGYUN 1C DEB, 31367 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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31367 intel report (Beta)
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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, 0.056 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 FENGYUN 1C DEB
1 31367U 99025BRX 26314.23903517 .00001651 00000-0 42603-3 0 9992
2 31367 98.7254 224.6116 0098096 93.4294 57.7124 14.48569698 32586Epoch: 2026-11-10T05:44Z
TLE epoch observation values (Epoch: 2026-11-10T05:44:12.638Z)
Latitude
27.59368°
Longitude
-86.26915°
Altitude
696.968 km
Speed
7.53 km/s
True Right ascension
03h 16m 45s
True Declination
27° 27' 06"
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
17:46:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
797.148 km
Perigee altitude
657.742 km
Semi-major axis
7,105.582 km
Eccentricity
0.00981
Inclination
98.7254°
RAAN
224.6116°
Arg. of periapsis
93.4294°
True anomaly
58.66891°
Mean anomaly
57.7124°
Eccentric anomaly
58.19003°
Mean motion
3.62363 °/min
Orbital period
99.35 mins
BSTAR
0.00042603
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-11 06:29:37.628Z | 36.028° NE | 2026-11-11 06:33:37.628Z | 111.83° ESE | 34.997° | 2026-11-11 06:36:37.628Z | 160.04° S |
| 5 mins | 2026-11-11 08:09:37.628Z | 322.125° NNW | 2026-11-11 08:11:37.628Z | 286.077° WNW | 21.917° | 2026-11-11 08:14:37.628Z | 245.068° WSW |
| 7 mins | 2026-11-11 17:39:37.628Z | 133.68° SE | 2026-11-11 17:42:37.628Z | 67.411° ENE | 43.762° | 2026-11-11 17:46:37.628Z | 1.161° NNE |
| 4 mins | 2026-11-11 19:19:37.628Z | 245.142° WSW | 2026-11-11 19:20:37.628Z | 260.531° W | 17.389° | 2026-11-11 19:23:37.628Z | 303.828° NW |
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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