FENGYUN 1C DEB, 31441
Orbit data source: Space-Track
FENGYUN 1C DEB, 31441 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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31441 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, 0.050 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 31441U 99025BUD 26300.52271975 .00078949 00000-0 47417-2 0 9999
2 31441 99.2813 224.7326 0056888 46.8614 313.7346 15.09186337688414Epoch: 2026-10-27T12:32Z
TLE epoch observation values (Epoch: 2026-10-27T12:32:42.986Z)
Latitude
0.00001°
Longitude
0.66885°
Altitude
514.61 km
Speed
7.621 km/s
True Right ascension
14h 58m 55s
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
09:59:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.087 km
Perigee altitude
496.423 km
Semi-major axis
6,913.892 km
Eccentricity
0.00569
Inclination
99.2813°
RAAN
224.7326°
Arg. of periapsis
46.8614°
True anomaly
313.26126°
Mean anomaly
313.7346°
Eccentric anomaly
313.49816°
Mean motion
3.77537 °/min
Orbital period
95.35 mins
BSTAR
0.0047417
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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 | 2026-10-29 18:45:44.245Z | 148.53° SSE | 2026-10-29 18:48:44.245Z | 102.682° ESE | 47.237° | 2026-10-29 18:52:44.245Z | 356.169° N |
| 6 mins | 2026-10-30 07:56:44.245Z | 27.349° NE | 2026-10-30 07:58:44.245Z | 96.197° ESE | 65.541° | 2026-10-30 08:02:44.245Z | 186.201° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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