FENGYUN 1C DEB, 32418
Orbit data source: Space-Track
FENGYUN 1C DEB, 32418 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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32418 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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 FENGYUN 1C DEB
1 32418U 99025DAE 26204.81560373 .00005820 00000-0 29732-2 0 9990
2 32418 98.1903 58.9635 0222022 124.3631 237.8759 14.03987670661184Epoch: 2026-07-23T19:34Z
TLE epoch observation values (Epoch: 2026-07-23T19:34:28.162Z)
Latitude
-0°
Longitude
-176.20501°
Altitude
971.16 km
Speed
7.321 km/s
True Right ascension
03h 55m 51s
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
23:18:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,038.257 km
Perigee altitude
716.089 km
Semi-major axis
7,255.31 km
Eccentricity
0.0222
Inclination
98.1903°
RAAN
58.9635°
Arg. of periapsis
124.3631°
True anomaly
235.75307°
Mean anomaly
237.8759°
Eccentric anomaly
236.81132°
Mean motion
3.51204 °/min
Orbital period
102.5 mins
BSTAR
0.0029732
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-08-26 14:17:50.078Z | 175.449° S | 2026-08-26 14:21:50.078Z | 294.464° NW | 42.763° | 2026-08-26 14:25:50.078Z | 342.183° N |
| 9 mins | 2026-08-27 02:43:50.078Z | 24.598° NE | 2026-08-27 02:47:50.078Z | 108.804° ESE | 41.908° | 2026-08-27 02:52:50.078Z | 180.712° SSW |
| 6 mins | 2026-08-27 04:25:50.078Z | 329.512° NNW | 2026-08-27 04:28:50.078Z | 292.478° WNW | 18.573° | 2026-08-27 04:31:50.078Z | 258.877° W |
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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