FENGYUN 1C DEB, 31313
Orbit data source: Space-Track
FENGYUN 1C DEB, 31313 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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31313 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
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 31313U 99025BPR 26151.19253076 .00000723 00000-0 34127-3 0 9996
2 31313 99.0093 63.8419 0046057 57.0681 303.4913 14.22505103994719Epoch: 2026-05-31T04:37Z
TLE epoch observation values (Epoch: 2026-05-31T04:37:14.657Z)
Latitude
-0.00005°
Longitude
105.83311°
Altitude
801.618 km
Speed
7.462 km/s
True Right ascension
04h 15m 22s
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
01:00:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.188 km
Perigee altitude
780.938 km
Semi-major axis
7,192.2 km
Eccentricity
0.00461
Inclination
99.0093°
RAAN
63.8419°
Arg. of periapsis
57.0681°
True anomaly
303.04975°
Mean anomaly
303.4913°
Eccentric anomaly
303.27067°
Mean motion
3.55837 °/min
Orbital period
101.17 mins
BSTAR
0.00034127
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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 | 2026-06-01 17:52:45.722Z | 153.182° SSE | 2026-06-01 17:56:45.722Z | 93.062° ESE | 42.433° | 2026-06-01 18:01:45.722Z | 352.196° N |
| 7 mins | 2026-06-02 06:10:45.722Z | 47.741° ENE | 2026-06-02 06:13:45.722Z | 90.366° ESE | 23.987° | 2026-06-02 06:17:45.722Z | 147.314° SSE |
| 8 mins | 2026-06-02 07:50:45.722Z | 348.315° N | 2026-06-02 07:53:45.722Z | 299.563° NW | 31.057° | 2026-06-02 07:58:45.722Z | 226.351° WSW |
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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