FENGYUN 1C DEB, 31511
Orbit data source: Space-Track
FENGYUN 1C DEB, 31511 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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31511 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: 16 hours ago
TLE from 16 hours ago
0 FENGYUN 1C DEB
1 31511U 99025BXA 26081.24846103 .00001443 00000-0 55841-3 0 9999
2 31511 99.0741 258.8006 0106164 298.1287 60.9197 14.28674106972219Epoch: 2026-03-22T05:57Z
TLE epoch observation values (Epoch: 2026-03-22T05:57:47.032Z)
Latitude
-0.00001°
Longitude
-10.40291°
Altitude
762.677 km
Speed
7.492 km/s
True Right ascension
17h 15m 12s
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
02:42:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
869.466 km
Perigee altitude
717.195 km
Semi-major axis
7,171.468 km
Eccentricity
0.01062
Inclination
99.0741°
RAAN
258.8006°
Arg. of periapsis
298.1287°
True anomaly
61.98973°
Mean anomaly
60.9197°
Eccentric anomaly
61.45403°
Mean motion
3.57381 °/min
Orbital period
100.73 mins
BSTAR
0.00055841
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-22 23:23:05.979Z | 54.02° ENE | 2026-03-22 23:26:05.979Z | 87.968° E | 16.552° | 2026-03-22 23:29:05.979Z | 124.497° SE |
| 9 mins | 2026-03-23 01:02:05.979Z | 4.207° NNE | 2026-03-23 01:06:05.979Z | 299.951° NW | 41.424° | 2026-03-23 01:11:05.979Z | 209.917° SW |
| 6 mins | 2026-03-23 10:42:05.979Z | 104.281° ESE | 2026-03-23 10:45:05.979Z | 56.767° ENE | 23.328° | 2026-03-23 10:48:05.979Z | 17.157° NNE |
| 7 mins | 2026-03-23 12:21:05.979Z | 205.316° SW | 2026-03-23 12:24:05.979Z | 265.632° W | 32.87° | 2026-03-23 12:28:05.979Z | 326.59° NNW |
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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