FENGYUN 1C DEB *, 47041
Orbit data source: Space-Track
FENGYUN 1C DEB *, 47041 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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47041 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 47041U 99025FBT 26228.40235186 .00043800 00000-0 15447-2 0 9998
2 47041 98.2282 281.5295 0010059 86.7901 285.7764 15.29080345749306Epoch: 2026-08-16T09:39Z
TLE epoch observation values (Epoch: 2026-08-16T09:39:23.200Z)
Latitude
12.28238°
Longitude
170.08932°
Altitude
479.004 km
Speed
7.628 km/s
True Right ascension
18h 38m 56s
True Declination
12° 12' 30"
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
04:58:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.445 km
Perigee altitude
468.657 km
Semi-major axis
6,853.688 km
Eccentricity
0.00101
Inclination
98.2282°
RAAN
281.5295°
Arg. of periapsis
86.7901°
True anomaly
285.66544°
Mean anomaly
285.7764°
Eccentric anomaly
285.72092°
Mean motion
3.82522 °/min
Orbital period
94.11 mins
BSTAR
0.0015447
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-24 16:01:28.229Z | 47.55° ENE | 2026-08-24 16:03:28.229Z | 95.321° ESE | 25.134° | 2026-08-24 16:06:28.229Z | 157.745° S |
| 5 mins | 2026-08-25 04:08:28.229Z | 202.478° SSW | 2026-08-25 04:10:28.229Z | 257.506° W | 30.61° | 2026-08-25 04:13:28.229Z | 327.317° 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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