FENGYUN 1C DEB, 38172
Orbit data source: Space-Track
FENGYUN 1C DEB, 38172 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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38172 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, 0.050 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FENGYUN 1C DEB
1 38172U 99025ERV 26268.10535628 .00000425 00000-0 53823-3 0 9995
2 38172 100.4282 20.3571 0279593 348.1747 11.2912 13.55007695655505Epoch: 2026-09-25T02:31Z
TLE epoch observation values (Epoch: 2026-09-25T02:31:42.782Z)
Latitude
-0.00006°
Longitude
-21.5037°
Altitude
853.084 km
Speed
7.527 km/s
True Right ascension
01h 21m 25s
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
06:45:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,258.941 km
Perigee altitude
843.502 km
Semi-major axis
7,429.358 km
Eccentricity
0.02796
Inclination
100.4282°
RAAN
20.3571°
Arg. of periapsis
348.1747°
True anomaly
11.94072°
Mean anomaly
11.2912°
Eccentric anomaly
11.61369°
Mean motion
3.38935 °/min
Orbital period
106.22 mins
BSTAR
0.00053823
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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 | 2026-09-25 19:06:07.258Z | 52.124° ENE | 2026-09-25 19:10:07.258Z | 89.037° E | 21.469° | 2026-09-25 19:15:07.258Z | 135.351° SSE |
| 12 mins | 2026-09-25 20:50:07.258Z | 10.184° NNE | 2026-09-25 20:55:07.258Z | 319.875° NNW | 71.909° | 2026-09-25 21:02:07.258Z | 206.638° SW |
| 5 mins | 2026-09-25 22:37:07.258Z | 324.479° NNW | 2026-09-25 22:39:07.258Z | 306.223° NW | 15.53° | 2026-09-25 22:42:07.258Z | 280.226° WNW |
| 9 mins | 2026-09-26 07:01:07.258Z | 138.406° SSE | 2026-09-26 07:05:07.258Z | 55.34° ENE | 54.953° | 2026-09-26 07:10:07.258Z | 354.128° N |
| 7 mins | 2026-09-26 08:47:07.258Z | 231.873° WSW | 2026-09-26 08:50:07.258Z | 269.389° W | 19.905° | 2026-09-26 08:54:07.258Z | 312.23° NW |
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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