FENGYUN 1C DEB, 29767
Orbit data source: Space-Track
FENGYUN 1C DEB, 29767 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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29767 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: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 29767U 99025BH 26152.34719898 .00003365 00000-0 13173-2 0 9995
2 29767 98.2118 109.9882 0324722 294.8298 221.7213 14.05045033979942Epoch: 2026-06-01T08:19Z
TLE epoch observation values (Epoch: 2026-06-01T08:19:57.991Z)
Latitude
25.59721°
Longitude
-80.89531°
Altitude
1,058.605 km
Speed
7.234 km/s
True Right ascension
19h 35m 43s
True Declination
25° 28' 08"
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
00:25:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,109.006 km
Perigee altitude
638.051 km
Semi-major axis
7,251.665 km
Eccentricity
0.03247
Inclination
98.2118°
RAAN
109.9882°
Arg. of periapsis
294.8298°
True anomaly
219.31852°
Mean anomaly
221.7213°
Eccentric anomaly
220.51268°
Mean motion
3.51469 °/min
Orbital period
102.43 mins
BSTAR
0.0013173
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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 | 2026-06-10 20:43:04.064Z | 145.369° SSE | 2026-06-10 20:47:04.064Z | 81.107° E | 41.096° | 2026-06-10 20:53:04.064Z | 355.398° N |
| 7 mins | 2026-06-10 22:26:04.064Z | 235.407° WSW | 2026-06-10 22:29:04.064Z | 271.415° WNW | 20.565° | 2026-06-10 22:33:04.064Z | 313.386° NW |
| 10 mins | 2026-06-11 09:10:04.064Z | 33.894° NE | 2026-06-11 09:15:04.064Z | 95.551° ESE | 30.533° | 2026-06-11 09:20:04.064Z | 158.111° S |
| 9 mins | 2026-06-11 10:52:04.064Z | 348.751° N | 2026-06-11 10:56:04.064Z | 295.863° NW | 31.247° | 2026-06-11 11:01:04.064Z | 231.381° WSW |
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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