FENGYUN 1C DEB, 29966
Orbit data source: Space-Track
FENGYUN 1C DEB, 29966 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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29966 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: 10 hours ago
TLE from 10 hours ago
0 FENGYUN 1C DEB
1 29966U 99025KQ 26256.45336357 .00000442 00000-0 20453-3 0 9991
2 29966 99.4596 130.6977 0038470 285.0643 74.6279 14.26164846 19589Epoch: 2026-09-13T10:52Z
TLE epoch observation values (Epoch: 2026-09-13T10:52:50.612Z)
Latitude
-0.00003°
Longitude
-24.96097°
Altitude
800.249 km
Speed
7.457 km/s
True Right ascension
08h 42m 47s
True Declination
0° 00' 00"
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
13:35:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
829.388 km
Perigee altitude
774.146 km
Semi-major axis
7,179.904 km
Eccentricity
0.00385
Inclination
99.4596°
RAAN
130.6977°
Arg. of periapsis
285.0643°
True anomaly
75.0535°
Mean anomaly
74.6279°
Eccentric anomaly
74.84065°
Mean motion
3.56751 °/min
Orbital period
100.91 mins
BSTAR
0.00020453
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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 | 2026-09-14 04:18:04.713Z | 25.227° NE | 2026-09-14 04:23:04.713Z | 118.961° SE | 54.836° | 2026-09-14 04:27:04.713Z | 177.291° S |
| 5 mins | 2026-09-14 06:00:04.713Z | 323.681° NNW | 2026-09-14 06:02:04.713Z | 295.574° NW | 19.857° | 2026-09-14 06:05:04.713Z | 258.275° W |
| 8 mins | 2026-09-14 15:38:04.713Z | 163.742° S | 2026-09-14 15:42:04.713Z | 347.397° N | 76.2° | 2026-09-14 15:46:04.713Z | 345.65° 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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