FENGYUN 1C DEB, 31054
Orbit data source: Space-Track
FENGYUN 1C DEB, 31054 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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31054 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: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 31054U 99025BEY 26206.28627971 .00000174 00000-0 11754-3 0 9999
2 31054 98.6829 217.4075 0009322 197.1973 176.3661 14.12295885999334Epoch: 2026-07-25T06:52Z
TLE epoch observation values (Epoch: 2026-07-25T06:52:14.566Z)
Latitude
13.37766°
Longitude
169.27565°
Altitude
860.412 km
Speed
7.42 km/s
True Right ascension
14h 21m 20s
True Declination
13° 18' 06"
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
00:10:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
855.43 km
Perigee altitude
841.957 km
Semi-major axis
7,226.83 km
Eccentricity
0.00093
Inclination
98.6829°
RAAN
217.4075°
Arg. of periapsis
197.1973°
True anomaly
176.37286°
Mean anomaly
176.3661°
Eccentric anomaly
176.36948°
Mean motion
3.53282 °/min
Orbital period
101.9 mins
BSTAR
0.00011754
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-26 12:19:57.975Z | 57.235° ENE | 2026-07-26 12:22:57.975Z | 91.902° ESE | 15.139° | 2026-07-26 12:25:57.975Z | 126.132° SE |
| 9 mins | 2026-07-26 13:59:57.975Z | 4.478° NNE | 2026-07-26 14:03:57.975Z | 292.786° NW | 42.094° | 2026-07-26 14:08:57.975Z | 207.52° SW |
| 7 mins | 2026-07-26 23:45:57.975Z | 114.44° SE | 2026-07-26 23:48:57.975Z | 73.903° E | 24.883° | 2026-07-26 23:52:57.975Z | 16.253° NNE |
| 9 mins | 2026-07-27 01:25:57.975Z | 200.176° SSW | 2026-07-27 01:29:57.975Z | 263.422° W | 32.018° | 2026-07-27 01:34:57.975Z | 330.081° NNW |
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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