FENGYUN 1C DEB, 32314
Orbit data source: Space-Track
FENGYUN 1C DEB, 32314 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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32314 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 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 32314U 99025CXF 25343.55282576 .00020854 00000-0 23179-2 0 9998
2 32314 98.8627 88.2704 0149391 167.7932 192.6962 14.79358552973830Epoch: 2025-12-09T13:16Z
TLE epoch observation values (Epoch: 2025-12-09T13:16:04.145Z)
Latitude
0.00001°
Longitude
170.71727°
Altitude
736.591 km
Speed
7.432 km/s
True Right ascension
05h 53m 04s
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
20:58:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
733.108 km
Perigee altitude
523.764 km
Semi-major axis
7,006.573 km
Eccentricity
0.01494
Inclination
98.8627°
RAAN
88.2704°
Arg. of periapsis
167.7932°
True anomaly
192.3267°
Mean anomaly
192.6962°
Eccentric anomaly
192.51078°
Mean motion
3.70071 °/min
Orbital period
97.28 mins
BSTAR
0.0023179
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-17 06:26:33.049Z | 127.532° SE | 2025-12-17 06:30:33.049Z | 56.686° ENE | 26.59° | 2025-12-17 06:33:33.049Z | 10.247° NNE |
| 6 mins | 2025-12-17 08:03:33.049Z | 218.1° SW | 2025-12-17 08:06:33.049Z | 269.39° W | 21.882° | 2025-12-17 08:09:33.049Z | 314.973° NW |
| 6 mins | 2025-12-17 19:52:33.049Z | 31.286° NE | 2025-12-17 19:54:33.049Z | 76.573° E | 36.727° | 2025-12-17 19:58:33.049Z | 178.267° S |
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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