FENGYUN 1C DEB, 31715
Orbit data source: Space-Track
FENGYUN 1C DEB, 31715 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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31715 intel report (Beta)
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Edit Public Description
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: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 1C DEB
1 31715U 99025CDN 25341.79382745 .00008571 00000-0 16938-2 0 9992
2 31715 99.2933 170.0847 0187127 134.2132 227.4603 14.52094814616457Epoch: 2025-12-07T19:03Z
TLE epoch observation values (Epoch: 2025-12-07T19:03:06.691Z)
Latitude
-0.00005°
Longitude
167.50472°
Altitude
812.887 km
Speed
7.399 km/s
True Right ascension
11h 20m 20s
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
02:27:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
848.708 km
Perigee altitude
583.209 km
Semi-major axis
7,094.095 km
Eccentricity
0.01871
Inclination
99.2933°
RAAN
170.0847°
Arg. of periapsis
134.2132°
True anomaly
225.90515°
Mean anomaly
227.4603°
Eccentric anomaly
226.68027°
Mean motion
3.63243 °/min
Orbital period
99.11 mins
BSTAR
0.0016938
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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 | 2025-12-08 11:43:46.264Z | 120.664° SE | 2025-12-08 11:47:46.264Z | 62.812° ENE | 23.522° | 2025-12-08 11:50:46.264Z | 16.693° NNE |
| 6 mins | 2025-12-08 13:22:46.264Z | 211.094° SW | 2025-12-08 13:25:46.264Z | 270.874° WNW | 28.266° | 2025-12-08 13:28:46.264Z | 319.222° NNW |
| 6 mins | 2025-12-09 01:24:46.264Z | 31.877° NE | 2025-12-09 01:26:46.264Z | 75.506° E | 37.678° | 2025-12-09 01:30:46.264Z | 178.41° S |
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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