FENGYUN 1C DEB, 29982
Orbit data source: Space-Track
FENGYUN 1C DEB, 29982 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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29982 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 29982U 99025LG 26164.15491541 .00003280 00000-0 52038-3 0 9998
2 29982 99.3959 17.2700 0120759 92.1738 35.9403 14.68229030 29591Epoch: 2026-06-13T03:43Z
TLE epoch observation values (Epoch: 2026-06-13T03:43:04.691Z)
Latitude
50.22593°
Longitude
-108.57061°
Altitude
606.173 km
Speed
7.598 km/s
True Right ascension
13h 54m 41s
True Declination
50° 03' 11"
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
00:05:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
748.894 km
Perigee altitude
578.818 km
Semi-major axis
7,041.993 km
Eccentricity
0.01208
Inclination
99.3959°
RAAN
17.27°
Arg. of periapsis
92.1738°
True anomaly
36.76252°
Mean anomaly
35.9403°
Eccentric anomaly
36.3504°
Mean motion
3.67282 °/min
Orbital period
98.02 mins
BSTAR
0.00052038
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-13 14:42:52.053Z | 197.474° SSW | 2026-06-13 14:45:52.053Z | 253.666° W | 30.446° | 2026-06-13 14:49:52.053Z | 327.197° NNW |
| 6 mins | 2026-06-14 02:37:52.053Z | 47.343° ENE | 2026-06-14 02:39:52.053Z | 90.787° ESE | 29.17° | 2026-06-14 02:43:52.053Z | 164.582° S |
| 4 mins | 2026-06-14 04:15:52.053Z | 312.928° NW | 2026-06-14 04:16:52.053Z | 293.931° NW | 18.467° | 2026-06-14 04:19:52.053Z | 248.741° W |
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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