FENGYUN 1C DEB, 30080
Orbit data source: Space-Track
FENGYUN 1C DEB, 30080 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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30080 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, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 FENGYUN 1C DEB
1 30080U 99025QH 26263.44245112 .00000199 00000-0 12449-3 0 9990
2 30080 98.7295 240.6701 0132486 341.1969 149.6921 14.11013504 12106Epoch: 2026-09-20T10:37Z
TLE epoch observation values (Epoch: 2026-09-20T10:37:07.776Z)
Latitude
47.71095°
Longitude
-88.28115°
Altitude
946.372 km
Speed
7.341 km/s
True Right ascension
04h 41m 21s
True Declination
47° 32' 39"
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
16:37:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
948.88 km
Perigee altitude
757.273 km
Semi-major axis
7,231.213 km
Eccentricity
0.01325
Inclination
98.7295°
RAAN
240.6701°
Arg. of periapsis
341.1969°
True anomaly
150.44742°
Mean anomaly
149.6921°
Eccentric anomaly
150.07083°
Mean motion
3.52961 °/min
Orbital period
101.99 mins
BSTAR
0.00012449
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-20 23:44:26.939Z | 227.804° WSW | 2026-09-20 23:47:26.939Z | 267.673° W | 19.917° | 2026-09-20 23:50:26.939Z | 306.725° NW |
| 8 mins | 2026-09-21 10:26:26.939Z | 51.98° ENE | 2026-09-21 10:29:26.939Z | 91.49° ESE | 26.106° | 2026-09-21 10:34:26.939Z | 149.044° SSE |
| 9 mins | 2026-09-21 12:06:26.939Z | 355.276° N | 2026-09-21 12:10:26.939Z | 293.074° NW | 46.955° | 2026-09-21 12:15:26.939Z | 221.347° SW |
| 8 mins | 2026-09-21 21:52:26.939Z | 129.455° SE | 2026-09-21 21:56:26.939Z | 58.789° ENE | 38.562° | 2026-09-21 22:00:26.939Z | 4.583° NNE |
| 4 mins | 2026-09-21 23:34:26.939Z | 226.168° WSW | 2026-09-21 23:37:26.939Z | 273.563° WNW | 24.638° | 2026-09-21 23:38:26.939Z | 290.043° WNW |
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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