FENGYUN 1C DEB, 29762
Orbit data source: Space-Track
FENGYUN 1C DEB, 29762 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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29762 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 29762U 99025BC 26206.42368861 .00000758 00000-0 28833-3 0 9992
2 29762 98.6000 188.8770 0204554 42.5997 108.4831 14.22892822 11384Epoch: 2026-07-25T10:10Z
TLE epoch observation values (Epoch: 2026-07-25T10:10:06.695Z)
Latitude
26.42448°
Longitude
-82.49967°
Altitude
868.147 km
Speed
7.395 km/s
True Right ascension
00h 52m 39s
True Declination
26° 17' 23"
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
00:10:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
959.826 km
Perigee altitude
665.642 km
Semi-major axis
7,190.871 km
Eccentricity
0.02046
Inclination
98.6°
RAAN
188.877°
Arg. of periapsis
42.5997°
True anomaly
110.68778°
Mean anomaly
108.4831°
Eccentric anomaly
109.58729°
Mean motion
3.55935 °/min
Orbital period
101.14 mins
BSTAR
0.00028833
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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 | 2026-07-26 11:20:44.080Z | 25.687° NE | 2026-07-26 11:25:44.080Z | 112.523° SE | 37.85° | 2026-07-26 11:30:44.080Z | 176.097° S |
| 6 mins | 2026-07-26 13:02:44.080Z | 328.159° NNW | 2026-07-26 13:04:44.080Z | 300.53° NW | 19.558° | 2026-07-26 13:08:44.080Z | 250.766° W |
| 7 mins | 2026-07-26 22:43:44.080Z | 157.204° SSE | 2026-07-26 22:46:44.080Z | 81.831° E | 44.027° | 2026-07-26 22:50:44.080Z | 350.759° N |
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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