FENGYUN 1C DEB *, 47102
Orbit data source: Space-Track
FENGYUN 1C DEB *, 47102 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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47102 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: 3 days ago
TLE from 3 days ago
0 FENGYUN 1C DEB *
1 47102U 99025FCA 26096.28856897 .00002670 00000-0 12411-2 0 9991
2 47102 98.4447 34.2002 0118517 80.9934 71.4762 14.17724097635631Epoch: 2026-04-06T06:55Z
TLE epoch observation values (Epoch: 2026-04-06T06:55:32.359Z)
Latitude
25.96504°
Longitude
-80.14242°
Altitude
809.974 km
Speed
7.464 km/s
True Right ascension
14h 33m 17s
True Declination
25° 49' 51"
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
12:52:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
915.64 km
Perigee altitude
744.777 km
Semi-major axis
7,208.346 km
Eccentricity
0.01185
Inclination
98.4447°
RAAN
34.2002°
Arg. of periapsis
80.9934°
True anomaly
72.76992°
Mean anomaly
71.4762°
Eccentric anomaly
72.12246°
Mean motion
3.54642 °/min
Orbital period
101.51 mins
BSTAR
0.0012411
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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 | 2026-04-09 07:39:04.972Z | 51.616° ENE | 2026-04-09 07:42:04.972Z | 93.536° ESE | 20.885° | 2026-04-09 07:46:04.972Z | 144.228° SSE |
| 8 mins | 2026-04-09 09:19:04.972Z | 352.398° N | 2026-04-09 09:23:04.972Z | 275.838° WNW | 33.378° | 2026-04-09 09:27:04.972Z | 222.194° SW |
| 7 mins | 2026-04-09 19:03:04.972Z | 123.66° SE | 2026-04-09 19:06:04.972Z | 72.28° E | 29.329° | 2026-04-09 19:10:04.972Z | 8.697° NNE |
| 6 mins | 2026-04-09 20:44:04.972Z | 223.451° SW | 2026-04-09 20:47:04.972Z | 273.495° WNW | 22.918° | 2026-04-09 20:50:04.972Z | 315.268° 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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