FENGYUN 1C DEB, 30081
Orbit data source: Space-Track
FENGYUN 1C DEB, 30081 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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30081 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: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 30081U 99025QJ 26296.95228749 -.00000032 00000-0 72529-5 0 9994
2 30081 98.9412 290.0033 0075786 187.3878 201.8126 13.98539570 7567Epoch: 2026-10-23T22:51Z
TLE epoch observation values (Epoch: 2026-10-23T22:51:17.639Z)
Latitude
28.54187°
Longitude
-90.06905°
Altitude
953.614 km
Speed
7.351 km/s
True Right ascension
19h 00m 28s
True Declination
28° 24' 06"
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
21:49:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
951.183 km
Perigee altitude
840.927 km
Semi-major axis
7,274.192 km
Eccentricity
0.00758
Inclination
98.9412°
RAAN
290.0033°
Arg. of periapsis
187.3878°
True anomaly
201.49273°
Mean anomaly
201.8126°
Eccentric anomaly
201.65238°
Mean motion
3.49837 °/min
Orbital period
102.9 mins
BSTAR
0.0000072529
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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 | 2026-10-25 11:23:11.665Z | 47.112° ENE | 2026-10-25 11:27:11.665Z | 94.203° ESE | 20.025° | 2026-10-25 11:30:11.665Z | 131.88° SE |
| 9 mins | 2026-10-25 13:05:11.665Z | 358.275° N | 2026-10-25 13:09:11.665Z | 284.327° WNW | 51.579° | 2026-10-25 13:14:11.665Z | 215.217° SW |
| 9 mins | 2026-10-25 22:56:11.665Z | 128.715° SE | 2026-10-25 23:00:11.665Z | 62.3° ENE | 42.163° | 2026-10-25 23:05:11.665Z | 1.184° NNE |
| 8 mins | 2026-10-26 00:38:11.665Z | 217.451° SW | 2026-10-26 00:41:11.665Z | 256.357° W | 28.14° | 2026-10-26 00:46:11.665Z | 319.847° 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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