FENGYUN 1C DEB, 31269
Orbit data source: Space-Track
FENGYUN 1C DEB, 31269 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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31269 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 1C DEB
1 31269U 99025BNB 26213.14579611 .00003927 00000-0 78946-3 0 9992
2 31269 98.1565 87.8146 0230511 289.3564 225.2763 14.46735205998291Epoch: 2026-08-01T03:29Z
TLE epoch observation values (Epoch: 2026-08-01T03:29:56.783Z)
Latitude
26.94627°
Longitude
-90.27753°
Altitude
856.95 km
Speed
7.365 km/s
True Right ascension
18h 07m 53s
True Declination
26° 48' 34"
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
02:02:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
897.356 km
Perigee altitude
569.497 km
Semi-major axis
7,111.563 km
Eccentricity
0.02305
Inclination
98.1565°
RAAN
87.8146°
Arg. of periapsis
289.3564°
True anomaly
223.43716°
Mean anomaly
225.2763°
Eccentric anomaly
224.35301°
Mean motion
3.61906 °/min
Orbital period
99.47 mins
BSTAR
0.00078946
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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 | 2026-08-01 14:33:09.500Z | 104.604° ESE | 2026-08-01 14:36:09.500Z | 63.21° ENE | 20.378° | 2026-08-01 14:40:09.500Z | 15.476° NNE |
| 8 mins | 2026-08-01 16:11:09.500Z | 197.605° SSW | 2026-08-01 16:14:09.500Z | 263.051° W | 36.582° | 2026-08-01 16:19:09.500Z | 335.326° NNW |
| 9 mins | 2026-08-02 04:16:09.500Z | 24.04° NE | 2026-08-02 04:20:09.500Z | 92.288° ESE | 41.116° | 2026-08-02 04:25:09.500Z | 179.278° S |
| 6 mins | 2026-08-02 05:55:09.500Z | 333.754° NNW | 2026-08-02 05:58:09.500Z | 297.19° NW | 18.951° | 2026-08-02 06:01:09.500Z | 260.156° 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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