FENGYUN 1C DEB, 38795
Orbit data source: Space-Track
FENGYUN 1C DEB, 38795 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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38795 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 month ago
TLE from 1 month ago
0 FENGYUN 1C DEB
1 38795U 99025EUK 26080.27427205 .00002670 00000-0 28970-2 0 9995
2 38795 98.6882 93.2380 0497762 11.4880 349.7130 13.30320054798223Epoch: 2026-03-21T06:34Z
TLE epoch observation values (Epoch: 2026-03-21T06:34:57.105Z)
Latitude
-0.00001°
Longitude
175.70273°
Altitude
780.446 km
Speed
7.644 km/s
True Right ascension
06h 12m 57s
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
08:17:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,517.19 km
Perigee altitude
768.46 km
Semi-major axis
7,520.962 km
Eccentricity
0.04978
Inclination
98.6882°
RAAN
93.238°
Arg. of periapsis
11.488°
True anomaly
348.62823°
Mean anomaly
349.713°
Eccentric anomaly
349.17749°
Mean motion
3.32762 °/min
Orbital period
108.19 mins
BSTAR
0.002897
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-04-18 12:02:17.913Z | 40.358° NE | 2026-04-18 12:08:17.913Z | 90.752° ESE | 25.718° | 2026-04-18 12:14:17.913Z | 142.517° SSE |
| 15 mins | 2026-04-18 13:48:17.913Z | 6.56° NNE | 2026-04-18 13:55:17.913Z | 295.872° NW | 42.747° | 2026-04-18 14:03:17.913Z | 209.331° SW |
| 8 mins | 2026-04-18 15:37:17.913Z | 332.112° NNW | 2026-04-18 15:40:17.913Z | 309.892° NW | 15.844° | 2026-04-18 15:45:17.913Z | 274.074° WNW |
| 5 mins | 2026-04-18 22:27:17.913Z | 63.671° ENE | 2026-04-18 22:29:17.913Z | 46.404° ENE | 13.373° | 2026-04-18 22:32:17.913Z | 23.461° NE |
| 12 mins | 2026-04-19 00:09:17.913Z | 149.012° SSE | 2026-04-19 00:14:17.913Z | 52.121° ENE | 42.641° | 2026-04-19 00:21:17.913Z | 351.621° 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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