FENGYUN 1C DEB, 32093
Orbit data source: Space-Track
FENGYUN 1C DEB, 32093 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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32093 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: 20 hours ago
TLE from 20 hours ago
0 FENGYUN 1C DEB
1 32093U 99025CQK 26093.07699122 .00001541 00000-0 50704-3 0 9998
2 32093 98.9105 315.0676 0079451 25.3974 335.1084 14.37939460981171Epoch: 2026-04-03T01:50Z
TLE epoch observation values (Epoch: 2026-04-03T01:50:52.041Z)
Latitude
0.00001°
Longitude
95.93446°
Altitude
716.834 km
Speed
7.524 km/s
True Right ascension
21h 00m 16s
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
03:51:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
819.192 km
Perigee altitude
705.726 km
Semi-major axis
7,140.596 km
Eccentricity
0.00795
Inclination
98.9105°
RAAN
315.0676°
Arg. of periapsis
25.3974°
True anomaly
334.72171°
Mean anomaly
335.1084°
Eccentric anomaly
334.91541°
Mean motion
3.59701 °/min
Orbital period
100.08 mins
BSTAR
0.00050704
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-04-04 03:27:31.108Z | 19.157° NNE | 2026-04-04 03:32:31.108Z | 104.629° ESE | 43.001° | 2026-04-04 03:37:31.108Z | 185.898° SSW |
| 4 mins | 2026-04-04 05:09:31.108Z | 316.208° NNW | 2026-04-04 05:10:31.108Z | 303.178° NW | 14.759° | 2026-04-04 05:13:31.108Z | 266.448° W |
| 8 mins | 2026-04-04 14:42:31.108Z | 165.799° S | 2026-04-04 14:46:31.108Z | 332.215° NNW | 44.723° | 2026-04-04 14:50:31.108Z | 345.667° N |
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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