FENGYUN 1C DEB, 31565
Orbit data source: Space-Track
FENGYUN 1C DEB, 31565 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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31565 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: 3 days ago
TLE from 3 days ago
0 FENGYUN 1C DEB
1 31565U 99025BZG 25306.87476335 .00008195 00000-0 26916-2 0 9993
2 31565 100.7169 169.1982 0052540 133.2888 227.2691 14.37846356637801Epoch: 2025-11-02T20:59Z
TLE epoch observation values (Epoch: 2025-11-02T20:59:39.553Z)
Latitude
-0.00006°
Longitude
171.89918°
Altitude
794.069 km
Speed
7.443 km/s
True Right ascension
11h 16m 47s
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
09:40:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
800.384 km
Perigee altitude
725.346 km
Semi-major axis
7,141.002 km
Eccentricity
0.00525
Inclination
100.7169°
RAAN
169.1982°
Arg. of periapsis
133.2888°
True anomaly
226.82882°
Mean anomaly
227.2691°
Eccentric anomaly
227.04876°
Mean motion
3.5967 °/min
Orbital period
100.09 mins
BSTAR
0.0026916
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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 | 2025-11-05 14:15:34.807Z | 133.513° SE | 2025-11-05 14:19:34.807Z | 65.327° ENE | 33.858° | 2025-11-05 14:23:34.807Z | 0.8° NNE |
| 6 mins | 2025-11-05 15:55:34.807Z | 222.326° SW | 2025-11-05 15:58:34.807Z | 266.526° W | 20.405° | 2025-11-05 16:01:34.807Z | 307.778° NW |
| 7 mins | 2025-11-06 04:04:34.807Z | 16.239° NNE | 2025-11-06 04:07:34.807Z | 11.614° NNE | 44.941° | 2025-11-06 04:11:34.807Z | 197.649° 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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