FENGYUN 1C DEB, 31082
Orbit data source: Space-Track
FENGYUN 1C DEB, 31082 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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31082 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: 1 month ago
TLE from 1 month ago
0 FENGYUN 1C DEB
1 31082U 99025BGC 26115.76687546 .00000993 00000-0 53617-3 0 9999
2 31082 98.6711 124.1474 0069040 176.8047 183.3581 14.13660194982039Epoch: 2026-04-25T18:24Z
TLE epoch observation values (Epoch: 2026-04-25T18:24:18.039Z)
Latitude
-0.00002°
Longitude
-5.70829°
Altitude
899.588 km
Speed
7.377 km/s
True Right ascension
08h 16m 35s
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
18:20:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
893.901 km
Perigee altitude
794.177 km
Semi-major axis
7,222.176 km
Eccentricity
0.0069
Inclination
98.6711°
RAAN
124.1474°
Arg. of periapsis
176.8047°
True anomaly
183.31215°
Mean anomaly
183.3581°
Eccentric anomaly
183.33509°
Mean motion
3.53623 °/min
Orbital period
101.8 mins
BSTAR
0.00053617
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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 | 2026-05-26 12:13:22.213Z | 51.717° ENE | 2026-05-26 12:16:22.213Z | 89.05° E | 18.327° | 2026-05-26 12:20:22.213Z | 138.231° SSE |
| 8 mins | 2026-05-26 13:54:22.213Z | 353.807° N | 2026-05-26 13:57:22.213Z | 294.658° NW | 37.32° | 2026-05-26 14:02:22.213Z | 215.8° SW |
| 7 mins | 2026-05-26 23:39:22.213Z | 120.183° SE | 2026-05-26 23:42:22.213Z | 72.028° E | 28.566° | 2026-05-26 23:46:22.213Z | 10.581° NNE |
| 7 mins | 2026-05-27 01:20:22.213Z | 218.119° SW | 2026-05-27 01:23:22.213Z | 268.412° W | 26.13° | 2026-05-27 01:27:22.213Z | 321.901° NNW |
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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