FENGYUN 1C DEB, 38827
Orbit data source: Space-Track
FENGYUN 1C DEB, 38827 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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38827 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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 38827U 99025EVT 26090.32529270 .00004060 00000-0 11468-2 0 9992
2 38827 98.3755 114.8902 0214662 350.1598 9.5414 14.33572633626154Epoch: 2026-03-31T07:48Z
TLE epoch observation values (Epoch: 2026-03-31T07:48:25.289Z)
Latitude
-0.00003°
Longitude
169.08074°
Altitude
631.294 km
Speed
7.622 km/s
True Right ascension
07h 39m 33s
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
15:55:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
930.529 km
Perigee altitude
623.344 km
Semi-major axis
7,155.073 km
Eccentricity
0.02147
Inclination
98.3755°
RAAN
114.8902°
Arg. of periapsis
350.1598°
True anomaly
9.96021°
Mean anomaly
9.5414°
Eccentric anomaly
9.74968°
Mean motion
3.5861 °/min
Orbital period
100.39 mins
BSTAR
0.0011468
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-04-09 13:30:05.060Z | 39.858° NE | 2026-04-09 13:34:05.060Z | 88.31° E | 26.015° | 2026-04-09 13:39:05.060Z | 151.576° SSE |
| 9 mins | 2026-04-09 15:10:05.060Z | 349.715° N | 2026-04-09 15:14:05.060Z | 281.548° WNW | 33.529° | 2026-04-09 15:19:05.060Z | 222.819° SW |
| 7 mins | 2026-04-10 00:47:05.060Z | 118.373° SE | 2026-04-10 00:50:05.060Z | 63.05° ENE | 28.04° | 2026-04-10 00:54:05.060Z | 7.809° NNE |
| 6 mins | 2026-04-10 02:27:05.060Z | 227.229° WSW | 2026-04-10 02:29:05.060Z | 263.394° W | 24.423° | 2026-04-10 02:33:05.060Z | 320.561° 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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