FENGYUN 1C DEB, 31387
Orbit data source: Space-Track
FENGYUN 1C DEB, 31387 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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31387 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, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 FENGYUN 1C DEB
1 31387U 99025BST 26081.61924950 .00000480 00000-0 21355-3 0 9991
2 31387 99.1575 327.6425 0240403 250.2731 107.2367 14.13708100977084Epoch: 2026-03-22T14:51Z
TLE epoch observation values (Epoch: 2026-03-22T14:51:43.156Z)
Latitude
0.00001°
Longitude
-75.41033°
Altitude
904.847 km
Speed
7.371 km/s
True Right ascension
21h 50m 34s
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
14:29:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,017.517 km
Perigee altitude
670.277 km
Semi-major axis
7,222.034 km
Eccentricity
0.02404
Inclination
99.1575°
RAAN
327.6425°
Arg. of periapsis
250.2731°
True anomaly
109.84366°
Mean anomaly
107.2367°
Eccentric anomaly
108.5426°
Mean motion
3.53634 °/min
Orbital period
101.8 mins
BSTAR
0.00021355
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-03-23 14:48:22.935Z | 100.864° ESE | 2026-03-23 14:52:22.935Z | 58.65° ENE | 18.815° | 2026-03-23 14:56:22.935Z | 17.916° NNE |
| 11 mins | 2026-03-23 16:27:22.935Z | 174.091° S | 2026-03-23 16:32:22.935Z | 278.389° WNW | 43.577° | 2026-03-23 16:38:22.935Z | 342.051° N |
| 10 mins | 2026-03-24 04:50:22.935Z | 26.375° NE | 2026-03-24 04:55:22.935Z | 110.498° ESE | 38.619° | 2026-03-24 05:00:22.935Z | 176.951° S |
| 6 mins | 2026-03-24 06:32:22.935Z | 334.665° NNW | 2026-03-24 06:35:22.935Z | 295.554° NW | 21.125° | 2026-03-24 06:38:22.935Z | 257.453° W |
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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