FENGYUN 1C DEB, 31083
Orbit data source: Space-Track
FENGYUN 1C DEB, 31083 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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31083 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 31083U 99025BGD 26301.35007013 .00006396 00000-0 10778-2 0 9990
2 31083 98.6639 81.0763 0026856 35.5096 354.5535 14.69657535 23868Epoch: 2026-10-28T08:24Z
TLE epoch observation values (Epoch: 2026-10-28T08:24:06.059Z)
Latitude
29.70857°
Longitude
-86.60983°
Altitude
647.091 km
Speed
7.547 km/s
True Right ascension
05h 04m 27s
True Declination
29° 33' 30"
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
06:27:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
678.151 km
Perigee altitude
640.352 km
Semi-major axis
7,037.389 km
Eccentricity
0.00269
Inclination
98.6639°
RAAN
81.0763°
Arg. of periapsis
35.5096°
True anomaly
354.52419°
Mean anomaly
354.5535°
Eccentric anomaly
354.53886°
Mean motion
3.67643 °/min
Orbital period
97.92 mins
BSTAR
0.0010778
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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 | 2026-10-29 22:24:56.513Z | 12.862° NNE | 2026-10-29 22:28:56.513Z | 210.943° SW | 82.039° | 2026-10-29 22:32:56.513Z | 195.783° SSW |
| 7 mins | 2026-10-30 09:24:56.513Z | 163.882° S | 2026-10-30 09:27:56.513Z | 139.626° SSE | 83.634° | 2026-10-30 09:31:56.513Z | 347.272° N |
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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