FENGYUN 1C DEB, 31440
Orbit data source: Space-Track
FENGYUN 1C DEB, 31440 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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31440 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 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 31440U 99025BUC 26033.72339626 .00005231 00000-0 17491-2 0 9994
2 31440 98.7417 127.5555 0039769 187.8078 172.2494 14.37387598970722Epoch: 2026-02-02T17:21Z
TLE epoch observation values (Epoch: 2026-02-02T17:21:41.436Z)
Latitude
-0.00001°
Longitude
94.21826°
Altitude
798.244 km
Speed
7.44 km/s
True Right ascension
08h 30m 13s
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
07:04:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
792.684 km
Perigee altitude
735.875 km
Semi-major axis
7,142.417 km
Eccentricity
0.00398
Inclination
98.7417°
RAAN
127.5555°
Arg. of periapsis
187.8078°
True anomaly
172.31056°
Mean anomaly
172.2494°
Eccentric anomaly
172.28001°
Mean motion
3.59563 °/min
Orbital period
100.12 mins
BSTAR
0.0017491
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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 | 2026-02-11 05:18:20.334Z | 128.389° SE | 2026-02-11 05:22:20.334Z | 75.017° E | 27.916° | 2026-02-11 05:26:20.334Z | 11.239° NNE |
| 7 mins | 2026-02-11 06:58:20.334Z | 212.395° SW | 2026-02-11 07:01:20.334Z | 258.459° W | 26.087° | 2026-02-11 07:05:20.334Z | 319.177° NNW |
| 8 mins | 2026-02-11 19:07:20.334Z | 12.771° NNE | 2026-02-11 19:11:20.334Z | 223.839° SW | 44.855° | 2026-02-11 19:15:20.334Z | 196.285° SSW |
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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