FENGYUN 1C DEB, 31388
Orbit data source: Space-Track
FENGYUN 1C DEB, 31388 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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31388 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: 20 hours ago
TLE from 20 hours ago
0 FENGYUN 1C DEB
1 31388U 99025BSU 26165.77977030 .00000293 00000-0 19754-3 0 9991
2 31388 98.8193 154.2596 0047831 45.2686 77.6086 14.07523939990307Epoch: 2026-06-14T18:42Z
TLE epoch observation values (Epoch: 2026-06-14T18:42:52.153Z)
Latitude
55.67331°
Longitude
163.52966°
Altitude
869.792 km
Speed
7.427 km/s
True Right ascension
23h 09m 17s
True Declination
55° 30' 56"
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
01:13:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
899.682 km
Perigee altitude
830.393 km
Semi-major axis
7,243.175 km
Eccentricity
0.00478
Inclination
98.8193°
RAAN
154.2596°
Arg. of periapsis
45.2686°
True anomaly
78.14461°
Mean anomaly
77.6086°
Eccentric anomaly
77.87654°
Mean motion
3.52087 °/min
Orbital period
102.25 mins
BSTAR
0.00019754
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-15 21:37:39.490Z | 77.976° E | 2026-06-15 21:39:39.490Z | 54.526° ENE | 12.849° | 2026-06-15 21:41:39.490Z | 32.425° NE |
| 9 mins | 2026-06-15 23:15:39.490Z | 168.708° S | 2026-06-15 23:19:39.490Z | 275.449° WNW | 44.774° | 2026-06-15 23:24:39.490Z | 344.659° N |
| 9 mins | 2026-06-16 11:40:39.490Z | 31.457° NE | 2026-06-16 11:44:39.490Z | 104.187° ESE | 37.022° | 2026-06-16 11:49:39.490Z | 173.463° S |
| 6 mins | 2026-06-16 13:22:39.490Z | 331.744° NNW | 2026-06-16 13:25:39.490Z | 289.113° WNW | 21.274° | 2026-06-16 13:28:39.490Z | 252.182° 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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