FENGYUN 1C DEB *, 47104
Orbit data source: Space-Track
FENGYUN 1C DEB *, 47104 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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47104 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: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB *
1 47104U 99025FCC 26255.32224893 .00000214 00000-0 12193-3 0 9990
2 47104 98.8805 291.0216 0039606 272.4937 87.1705 14.19650908662549Epoch: 2026-09-12T07:44Z
TLE epoch observation values (Epoch: 2026-09-12T07:44:02.307Z)
Latitude
-0.00001°
Longitude
-176.32093°
Altitude
828.146 km
Speed
7.44 km/s
True Right ascension
19h 24m 05s
True Declination
0° 00' 00"
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
16:22:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
852.224 km
Perigee altitude
795.177 km
Semi-major axis
7,201.838 km
Eccentricity
0.00396
Inclination
98.8805°
RAAN
291.0216°
Arg. of periapsis
272.4937°
True anomaly
87.6239°
Mean anomaly
87.1705°
Eccentric anomaly
87.39719°
Mean motion
3.55122 °/min
Orbital period
101.37 mins
BSTAR
0.00012193
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-19 02:14:25.029Z | 155.369° SSE | 2026-09-19 02:18:25.029Z | 97.214° ESE | 71.3° | 2026-09-19 02:23:25.029Z | 351.298° N |
| 7 mins | 2026-09-19 14:34:25.029Z | 46.611° ENE | 2026-09-19 14:37:25.029Z | 92.535° ESE | 30.527° | 2026-09-19 14:41:25.029Z | 151.548° SSE |
| 8 mins | 2026-09-19 16:14:25.029Z | 345.75° N | 2026-09-19 16:17:25.029Z | 300.036° NW | 33.848° | 2026-09-19 16:22:25.029Z | 230.234° WSW |
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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