FENGYUN 1C DEB, 31281
Orbit data source: Space-Track
FENGYUN 1C DEB, 31281 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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31281 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: 21 hours ago
TLE from 21 hours ago
0 FENGYUN 1C DEB
1 31281U 99025BNP 26039.34230273 .00046878 00000-0 17792-2 0 9995
2 31281 98.3861 185.7949 0105301 255.9585 102.9925 15.21582491 5746Epoch: 2026-02-08T08:12Z
TLE epoch observation values (Epoch: 2026-02-08T08:12:54.955Z)
Latitude
0.00003°
Longitude
-75.88693°
Altitude
521.141 km
Speed
7.593 km/s
True Right ascension
12h 23m 10s
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
07:23:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.482 km
Perigee altitude
425.667 km
Semi-major axis
6,876.212 km
Eccentricity
0.01053
Inclination
98.3861°
RAAN
185.7949°
Arg. of periapsis
255.9585°
True anomaly
104.16472°
Mean anomaly
102.9925°
Eccentric anomaly
103.57897°
Mean motion
3.80644 °/min
Orbital period
94.58 mins
BSTAR
0.0017792
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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 | 2026-02-09 09:35:14.722Z | 162.556° S | 2026-02-09 09:39:14.722Z | 6.423° NNE | 43.066° | 2026-02-09 09:42:14.722Z | 348.961° N |
| 6 mins | 2026-02-09 22:40:14.722Z | 9.713° NNE | 2026-02-09 22:43:14.722Z | 216.469° SW | 42.398° | 2026-02-09 22:46:14.722Z | 197.958° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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