FENGYUN 1C DEB, 32153
Orbit data source: Space-Track
FENGYUN 1C DEB, 32153 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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32153 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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 32153U 99025CSX 25309.34725795 .00001144 00000-0 24377-3 0 9996
2 32153 98.7735 150.8010 0208193 334.5114 24.5923 14.48555422966820Epoch: 2025-11-05T08:20Z
TLE epoch observation values (Epoch: 2025-11-05T08:20:03.086Z)
Latitude
-0.00012°
Longitude
-19.03307°
Altitude
599.276 km
Speed
7.631 km/s
True Right ascension
10h 03m 12s
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
11:13:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
875.427 km
Perigee altitude
579.558 km
Semi-major axis
7,105.629 km
Eccentricity
0.02082
Inclination
98.7735°
RAAN
150.801°
Arg. of periapsis
334.5114°
True anomaly
25.60912°
Mean anomaly
24.5923°
Eccentric anomaly
25.09828°
Mean motion
3.62359 °/min
Orbital period
99.35 mins
BSTAR
0.00024377
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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 | 2025-11-07 02:20:08.083Z | 17.014° NNE | 2025-11-07 02:25:08.083Z | 64.119° ENE | 43.67° | 2025-11-07 02:31:08.083Z | 189.256° SSW |
| 5 mins | 2025-11-07 04:01:08.083Z | 322.462° NNW | 2025-11-07 04:03:08.083Z | 298.273° NW | 15.761° | 2025-11-07 04:06:08.083Z | 264.82° W |
| 7 mins | 2025-11-07 13:31:08.083Z | 163.46° S | 2025-11-07 13:34:08.083Z | 358.293° N | 44.318° | 2025-11-07 13:38:08.083Z | 347.109° 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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