FENGYUN 1C DEB, 29841
Orbit data source: Space-Track
FENGYUN 1C DEB, 29841 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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29841 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: 21 hours ago
TLE from 21 hours ago
0 FENGYUN 1C DEB
1 29841U 99025EK 26207.38774712 .00002114 00000-0 46387-3 0 9994
2 29841 98.8440 169.3572 0199459 16.5638 133.1495 14.47165994 25832Epoch: 2026-07-26T09:18Z
TLE epoch observation values (Epoch: 2026-07-26T09:18:21.351Z)
Latitude
28.32015°
Longitude
-89.53368°
Altitude
836.957 km
Speed
7.385 km/s
True Right ascension
23h 36m 34s
True Declination
28° 10' 42"
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
20:05:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
873.866 km
Perigee altitude
590.228 km
Semi-major axis
7,110.184 km
Eccentricity
0.01995
Inclination
98.844°
RAAN
169.3572°
Arg. of periapsis
16.5638°
True anomaly
134.78883°
Mean anomaly
133.1495°
Eccentric anomaly
133.97196°
Mean motion
3.62011 °/min
Orbital period
99.44 mins
BSTAR
0.00046387
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-07-27 10:04:31.903Z | 25.999° NE | 2026-07-27 10:08:31.903Z | 91.976° ESE | 39.436° | 2026-07-27 10:13:31.903Z | 177.811° S |
| 5 mins | 2026-07-27 11:44:31.903Z | 325.501° NNW | 2026-07-27 11:46:31.903Z | 297.628° NW | 18.51° | 2026-07-27 11:49:31.903Z | 258.858° W |
| 7 mins | 2026-07-27 21:15:31.903Z | 149.96° SSE | 2026-07-27 21:18:31.903Z | 62.612° ENE | 41.514° | 2026-07-27 21:22:31.903Z | 353.226° 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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