FENGYUN 1C DEB, 29967
Orbit data source: Space-Track
FENGYUN 1C DEB, 29967 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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29967 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: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 29967U 99025KR 26254.18537325 .00002031 00000-0 85842-3 0 9997
2 29967 98.8545 338.0815 0074779 225.1025 164.5921 14.25184656 10699Epoch: 2026-09-11T04:26Z
TLE epoch observation values (Epoch: 2026-09-11T04:26:56.248Z)
Latitude
29.5776°
Longitude
-83.91097°
Altitude
863.397 km
Speed
7.397 km/s
True Right ascension
22h 12m 08s
True Declination
29° 25' 56"
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
11:41:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
858.745 km
Perigee altitude
751.315 km
Semi-major axis
7,183.167 km
Eccentricity
0.00748
Inclination
98.8545°
RAAN
338.0815°
Arg. of periapsis
225.1025°
True anomaly
164.81774°
Mean anomaly
164.5921°
Eccentric anomaly
164.70512°
Mean motion
3.56508 °/min
Orbital period
100.98 mins
BSTAR
0.00085842
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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 | 2026-09-12 19:38:08.248Z | 347.351° N | 2026-09-12 19:42:08.248Z | 295.052° NW | 26.008° | 2026-09-12 19:46:08.248Z | 241.778° WSW |
| 9 mins | 2026-09-13 05:18:08.248Z | 146.659° SSE | 2026-09-13 05:22:08.248Z | 67.642° E | 60.521° | 2026-09-13 05:27:08.248Z | 354.543° N |
| 5 mins | 2026-09-13 07:00:08.248Z | 241.811° WSW | 2026-09-13 07:02:08.248Z | 267.074° W | 17.782° | 2026-09-13 07:05:08.248Z | 303.041° NW |
| 6 mins | 2026-09-13 17:35:08.248Z | 52.824° ENE | 2026-09-13 17:38:08.248Z | 95.709° ESE | 22.81° | 2026-09-13 17:41:08.248Z | 137.684° SSE |
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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