FENGYUN 1C DEB, 29869
Orbit data source: Space-Track
FENGYUN 1C DEB, 29869 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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29869 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: 15 hours ago
TLE from 15 hours ago
0 FENGYUN 1C DEB
1 29869U 99025FP 26150.63811433 .00000799 00000-0 27272-3 0 9990
2 29869 98.8873 91.3198 0085521 232.1819 253.4847 14.37263756 12412Epoch: 2026-05-30T15:18Z
TLE epoch observation values (Epoch: 2026-05-30T15:18:53.078Z)
Latitude
54.391°
Longitude
165.99091°
Altitude
794.343 km
Speed
7.452 km/s
True Right ascension
18h 55m 27s
True Declination
54° 13' 44"
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
15:34:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.783 km
Perigee altitude
703.611 km
Semi-major axis
7,142.834 km
Eccentricity
0.00855
Inclination
98.8873°
RAAN
91.3198°
Arg. of periapsis
232.1819°
True anomaly
252.54802°
Mean anomaly
253.4847°
Eccentric anomaly
253.01607°
Mean motion
3.59532 °/min
Orbital period
100.13 mins
BSTAR
0.00027272
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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 | 2026-05-31 08:02:00.947Z | 41.283° NE | 2026-05-31 08:06:00.947Z | 95.469° ESE | 23.112° | 2026-05-31 08:10:00.947Z | 149.912° SSE |
| 7 mins | 2026-05-31 09:42:00.947Z | 346.219° N | 2026-05-31 09:45:00.947Z | 292.115° WNW | 30.596° | 2026-05-31 09:49:00.947Z | 229.383° WSW |
| 7 mins | 2026-05-31 19:17:00.947Z | 122.147° SE | 2026-05-31 19:20:00.947Z | 69.66° E | 31.054° | 2026-05-31 19:24:00.947Z | 7.934° NNE |
| 7 mins | 2026-05-31 20:56:00.947Z | 217.732° SW | 2026-05-31 20:59:00.947Z | 263.585° W | 25.175° | 2026-05-31 21:03:00.947Z | 318.513° NNW |
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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