FENGYUN 1C DEB, 29751
Orbit data source: Space-Track
FENGYUN 1C DEB, 29751 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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29751 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: 12 hours ago
TLE from 12 hours ago
0 FENGYUN 1C DEB
1 29751U 99025AR 25353.58052490 .00000251 00000-0 12320-3 0 9999
2 29751 98.5407 21.2550 0090096 119.4971 42.7764 14.23634421981705Epoch: 2025-12-19T13:55Z
TLE epoch observation values (Epoch: 2025-12-19T13:55:57.351Z)
Latitude
16.81118°
Longitude
-93.56691°
Altitude
768.09 km
Speed
7.496 km/s
True Right ascension
13h 35m 22s
True Declination
16° 42' 59"
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
01:18:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
874.997 km
Perigee altitude
745.469 km
Semi-major axis
7,188.37 km
Eccentricity
0.00901
Inclination
98.5407°
RAAN
21.255°
Arg. of periapsis
119.4971°
True anomaly
43.48338°
Mean anomaly
42.7764°
Eccentric anomaly
43.12931°
Mean motion
3.56121 °/min
Orbital period
101.09 mins
BSTAR
0.0001232
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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 | 2025-12-20 02:46:47.654Z | 202.325° SSW | 2025-12-20 02:50:47.654Z | 254.737° W | 27.571° | 2025-12-20 02:54:47.654Z | 319.355° NNW |
| 8 mins | 2025-12-20 15:03:47.654Z | 9.143° NNE | 2025-12-20 15:07:47.654Z | 242.488° WSW | 43.819° | 2025-12-20 15:11:47.654Z | 200.399° SSW |
| 5 mins | 2025-12-21 00:46:47.654Z | 90.907° ESE | 2025-12-21 00:48:47.654Z | 62.31° ENE | 18.314° | 2025-12-21 00:51:47.654Z | 23.713° NE |
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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