FENGYUN 1C DEB, 36162
Orbit data source: Space-Track
FENGYUN 1C DEB, 36162 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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36162 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: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 36162U 99025DSK 26296.09179013 .00004651 00000-0 21908-2 0 9996
2 36162 97.6236 49.6675 0244129 292.0503 65.4905 14.05839656749346Epoch: 2026-10-23T02:12Z
TLE epoch observation values (Epoch: 2026-10-23T02:12:10.667Z)
Latitude
0.00005°
Longitude
-14.89426°
Altitude
806.749 km
Speed
7.486 km/s
True Right ascension
03h 18m 40s
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
01:28:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,047.737 km
Perigee altitude
693.803 km
Semi-major axis
7,248.907 km
Eccentricity
0.02441
Inclination
97.6236°
RAAN
49.6675°
Arg. of periapsis
292.0503°
True anomaly
68.06768°
Mean anomaly
65.4905°
Eccentric anomaly
66.77591°
Mean motion
3.51669 °/min
Orbital period
102.37 mins
BSTAR
0.0021908
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-10-30 06:50:46.272Z | 131.331° SE | 2026-10-30 06:55:46.272Z | 65.479° ENE | 38.393° | 2026-10-30 07:00:46.272Z | 5.841° NNE |
| 9 mins | 2026-10-30 08:32:46.272Z | 210.176° SW | 2026-10-30 08:36:46.272Z | 264.024° W | 33.549° | 2026-10-30 08:41:46.272Z | 325.666° NNW |
| 8 mins | 2026-10-30 19:18:46.272Z | 49.523° ENE | 2026-10-30 19:21:46.272Z | 84.23° E | 23.653° | 2026-10-30 19:26:46.272Z | 141.524° SSE |
| 10 mins | 2026-10-30 20:58:46.272Z | 359.691° N | 2026-10-30 21:03:46.272Z | 289.102° WNW | 53.348° | 2026-10-30 21:08:46.272Z | 215.855° 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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