FENGYUN 1C DEB, 38168
Orbit data source: Space-Track
FENGYUN 1C DEB, 38168 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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38168 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, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 FENGYUN 1C DEB
1 38168U 99025ERR 26253.09004879 .00002851 00000-0 96968-3 0 9993
2 38168 98.7899 355.8776 0038912 33.9069 326.4593 14.36942783683592Epoch: 2026-09-10T02:09Z
TLE epoch observation values (Epoch: 2026-09-10T02:09:40.215Z)
Latitude
0.00002°
Longitude
-25.67272°
Altitude
748.402 km
Speed
7.493 km/s
True Right ascension
23h 43m 30s
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
16:57:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
793.556 km
Perigee altitude
737.959 km
Semi-major axis
7,143.894 km
Eccentricity
0.00389
Inclination
98.7899°
RAAN
355.8776°
Arg. of periapsis
33.9069°
True anomaly
326.21193°
Mean anomaly
326.4593°
Eccentric anomaly
326.33571°
Mean motion
3.59452 °/min
Orbital period
100.15 mins
BSTAR
0.00096968
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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 | 2026-09-14 06:32:45.924Z | 148.328° SSE | 2026-09-14 06:36:45.924Z | 96.006° ESE | 53.421° | 2026-09-14 06:41:45.924Z | 356.101° N |
| 4 mins | 2026-09-14 08:14:45.924Z | 243.252° WSW | 2026-09-14 08:16:45.924Z | 270.239° WNW | 15.425° | 2026-09-14 08:18:45.924Z | 296.336° NW |
| 5 mins | 2026-09-14 18:44:45.924Z | 62.389° ENE | 2026-09-14 18:46:45.924Z | 90.315° ESE | 19.386° | 2026-09-14 18:49:45.924Z | 130.978° SE |
| 8 mins | 2026-09-14 20:22:45.924Z | 355.694° N | 2026-09-14 20:25:45.924Z | 305.447° NW | 47.419° | 2026-09-14 20:30:45.924Z | 216.99° SW |
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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