FENGYUN 1C DEB, 31471
Orbit data source: Space-Track
FENGYUN 1C DEB, 31471 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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31471 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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 31471U 99025BVK 26163.43993272 .00002819 00000-0 12955-2 0 9992
2 31471 97.9668 33.1860 0144360 185.4558 174.5053 14.16498271665485Epoch: 2026-06-12T10:33Z
TLE epoch observation values (Epoch: 2026-06-12T10:33:30.187Z)
Latitude
-0.00007°
Longitude
-25.95912°
Altitude
943.869 km
Speed
7.327 km/s
True Right ascension
02h 12m 44s
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
10:29:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
938.468 km
Perigee altitude
730.229 km
Semi-major axis
7,212.485 km
Eccentricity
0.01444
Inclination
97.9668°
RAAN
33.186°
Arg. of periapsis
185.4558°
True anomaly
174.6609°
Mean anomaly
174.5053°
Eccentric anomaly
174.58338°
Mean motion
3.54336 °/min
Orbital period
101.6 mins
BSTAR
0.0012955
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-19 04:12:01.493Z | 11.751° NNE | 2026-06-19 04:16:01.493Z | 344.67° N | 44.84° | 2026-06-19 04:21:01.493Z | 195.238° SSW |
| 5 mins | 2026-06-19 13:58:01.493Z | 90.426° ESE | 2026-06-19 14:00:01.493Z | 64.947° ENE | 18.279° | 2026-06-19 14:03:01.493Z | 28.19° NE |
| 9 mins | 2026-06-19 15:36:01.493Z | 183.06° SSW | 2026-06-19 15:40:01.493Z | 254.077° W | 41.434° | 2026-06-19 15:45:01.493Z | 338.78° 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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