FENGYUN 1C DEB, 37906
Orbit data source: Space-Track
FENGYUN 1C DEB, 37906 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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37906 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: 5 days ago
TLE from 5 days ago
0 FENGYUN 1C DEB
1 37906U 99025ENF 25302.88839998 .00000740 00000-0 67549-3 0 9999
2 37906 99.6074 343.0357 0163461 143.7019 37.2791 13.80702267588504Epoch: 2025-10-29T21:19Z
TLE epoch observation values (Epoch: 2025-10-29T21:19:17.758Z)
Latitude
-2.23217°
Longitude
164.38059°
Altitude
869.8 km
Speed
7.465 km/s
True Right ascension
10h 50m 38s
True Declination
-2° 13' 09"
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
19:32:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.579 km
Perigee altitude
838.724 km
Semi-major axis
7,336.789 km
Eccentricity
0.01635
Inclination
99.6074°
RAAN
343.0357°
Arg. of periapsis
143.7019°
True anomaly
38.43231°
Mean anomaly
37.2791°
Eccentric anomaly
37.85382°
Mean motion
3.4537 °/min
Orbital period
104.24 mins
BSTAR
0.00067549
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-04 01:47:57.457Z | 128.252° SE | 2025-11-04 01:52:57.457Z | 73.235° E | 29.06° | 2025-11-04 01:57:57.457Z | 6.584° NNE |
| 9 mins | 2025-11-04 03:31:57.457Z | 203.798° SW | 2025-11-04 03:35:57.457Z | 258.916° W | 30.462° | 2025-11-04 03:40:57.457Z | 324.84° NNW |
| 4 mins | 2025-11-04 14:29:57.457Z | 73.213° E | 2025-11-04 14:31:57.457Z | 99.739° ESE | 16.224° | 2025-11-04 14:33:57.457Z | 124.007° SE |
| 9 mins | 2025-11-04 16:10:57.457Z | 1.662° NNE | 2025-11-04 16:14:57.457Z | 278.532° WNW | 39.876° | 2025-11-04 16:19:57.457Z | 212.094° SW |
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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