FENGYUN 1C DEB, 31049
Orbit data source: Space-Track
FENGYUN 1C DEB, 31049 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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31049 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: 5 months ago
TLE from 5 months ago
0 FENGYUN 1C DEB
1 31049U 99025BET 25160.26080283 .00000572 00000-0 38429-3 0 9998
2 31049 98.7847 176.5158 0049142 295.4773 64.1315 14.04057506584988Epoch: 2025-06-09T06:15Z
TLE epoch observation values (Epoch: 2025-06-09T06:15:33.364Z)
Latitude
-0.00006°
Longitude
-175.24777°
Altitude
867.246 km
Speed
7.427 km/s
True Right ascension
11h 46m 03s
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
07:43:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
912.615 km
Perigee altitude
841.309 km
Semi-major axis
7,255.099 km
Eccentricity
0.00491
Inclination
98.7847°
RAAN
176.5158°
Arg. of periapsis
295.4773°
True anomaly
64.63955°
Mean anomaly
64.1315°
Eccentric anomaly
64.38539°
Mean motion
3.51219 °/min
Orbital period
102.5 mins
BSTAR
0.00038429
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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 | 2025-11-09 13:24:09.710Z | 22.29° NNE | 2025-11-09 13:29:09.710Z | 79.721° E | 39.234° | 2025-11-09 13:34:09.710Z | 176.335° S |
| 6 mins | 2025-11-09 15:08:09.710Z | 327.707° NNW | 2025-11-09 15:10:09.710Z | 301.674° NW | 19.282° | 2025-11-09 15:14:09.710Z | 253.801° W |
| 4 mins | 2025-11-09 23:17:09.710Z | 75.982° E | 2025-11-09 23:18:09.710Z | 64.525° ENE | 14.683° | 2025-11-09 23:21:09.710Z | 31.212° NE |
| 9 mins | 2025-11-10 00:55:09.710Z | 169.736° S | 2025-11-10 00:59:09.710Z | 265.88° W | 44.72° | 2025-11-10 01:04:09.710Z | 344.087° 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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