FENGYUN 1C DEB, 41006
Orbit data source: Space-Track
FENGYUN 1C DEB, 41006 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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41006 intel report (Beta)
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Edit Public Description
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
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 41006U 99025EXL 25253.27963773 .00002823 00000-0 22479-2 0 9998
2 41006 102.3707 94.6652 0187285 231.5035 126.9183 13.84578394561953Epoch: 2025-09-10T06:42Z
TLE epoch observation values (Epoch: 2025-09-10T06:42:40.699Z)
Latitude
-0.00001°
Longitude
4.43729°
Altitude
1,034.464 km
Speed
7.292 km/s
True Right ascension
06h 18m 39s
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
21:59:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,082.258 km
Perigee altitude
807.951 km
Semi-major axis
7,323.241 km
Eccentricity
0.01873
Inclination
102.3707°
RAAN
94.6652°
Arg. of periapsis
231.5035°
True anomaly
128.61006°
Mean anomaly
126.9183°
Eccentric anomaly
127.76657°
Mean motion
3.46328 °/min
Orbital period
103.95 mins
BSTAR
0.0022479
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-18 12:32:20.264Z | 126.898° SE | 2025-09-18 12:38:20.264Z | 55.691° ENE | 32.254° | 2025-09-18 12:43:20.264Z | 359.334° N |
| 10 mins | 2025-09-18 14:15:20.264Z | 197.481° SSW | 2025-09-18 14:20:20.264Z | 263.003° W | 31.932° | 2025-09-18 14:25:20.264Z | 321.93° NNW |
| 10 mins | 2025-09-19 02:53:20.264Z | 16.841° NNE | 2025-09-19 02:58:20.264Z | 223.072° SW | 44.359° | 2025-09-19 03:03:20.264Z | 202.13° SSW |
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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