FENGYUN 1C DEB, 38158
Orbit data source: Space-Track
FENGYUN 1C DEB, 38158 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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38158 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: 2 months ago
TLE from 2 months ago
0 FENGYUN 1C DEB
1 38158U 99025ERF 25364.29425831 .00001459 00000-0 14106-2 0 9997
2 38158 99.2857 30.6402 0213269 40.8229 320.8678 13.71813552571238Epoch: 2025-12-30T07:03Z
TLE epoch observation values (Epoch: 2025-12-30T07:03:43.917Z)
Latitude
-0.00003°
Longitude
-174.27238°
Altitude
875.301 km
Speed
7.475 km/s
True Right ascension
02h 02m 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
16:32:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,147.463 km
Perigee altitude
833.17 km
Semi-major axis
7,368.454 km
Eccentricity
0.02133
Inclination
99.2857°
RAAN
30.6402°
Arg. of periapsis
40.8229°
True anomaly
319.2931°
Mean anomaly
320.8678°
Eccentric anomaly
320.08372°
Mean motion
3.43146 °/min
Orbital period
104.91 mins
BSTAR
0.0014106
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-10 13:14:52.348Z | 61.112° ENE | 2026-03-10 13:17:52.348Z | 92.189° ESE | 13.64° | 2026-03-10 13:19:52.348Z | 113.443° SE |
| 10 mins | 2026-03-10 14:56:52.348Z | 10.744° NNE | 2026-03-10 15:01:52.348Z | 284.51° WNW | 44.407° | 2026-03-10 15:06:52.348Z | 201.979° SSW |
| 10 mins | 2026-03-11 00:58:52.348Z | 127.362° SE | 2026-03-11 01:03:52.348Z | 58.146° ENE | 34.003° | 2026-03-11 01:08:52.348Z | 2.803° NNE |
| 11 mins | 2026-03-11 02:41:52.348Z | 204.198° SW | 2026-03-11 02:46:52.348Z | 262.11° W | 30.572° | 2026-03-11 02:52:52.348Z | 326.953° 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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