FENGYUN 1C DEB, 36267
Orbit data source: Space-Track
FENGYUN 1C DEB, 36267 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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36267 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: 12 hours ago
TLE from 12 hours ago
0 FENGYUN 1C DEB
1 36267U 99025DWU 26213.32707801 .00001102 00000-0 60364-3 0 9997
2 36267 98.5716 154.6294 0124930 272.2376 241.2867 14.09997478897924Epoch: 2026-08-01T07:50Z
TLE epoch observation values (Epoch: 2026-08-01T07:50:59.540Z)
Latitude
27.42586°
Longitude
-88.59663°
Altitude
907.036 km
Speed
7.378 km/s
True Right ascension
22h 36m 22s
True Declination
27° 17' 18"
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
09:04:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
946.928 km
Perigee altitude
766.162 km
Semi-major axis
7,234.682 km
Eccentricity
0.01249
Inclination
98.5716°
RAAN
154.6294°
Arg. of periapsis
272.2376°
True anomaly
240.04059°
Mean anomaly
241.2867°
Eccentric anomaly
240.6627°
Mean motion
3.52707 °/min
Orbital period
102.07 mins
BSTAR
0.00060364
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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 | 2026-08-01 20:50:57.178Z | 199.393° SSW | 2026-08-01 20:55:57.178Z | 271.118° WNW | 31.031° | 2026-08-01 21:00:57.178Z | 329.759° NNW |
| 4 mins | 2026-08-02 07:36:57.178Z | 71.641° E | 2026-08-02 07:38:57.178Z | 94.929° ESE | 14.801° | 2026-08-02 07:40:57.178Z | 117.041° SE |
| 9 mins | 2026-08-02 09:15:57.178Z | 6.55° NNE | 2026-08-02 09:19:57.178Z | 285.005° WNW | 43.663° | 2026-08-02 09:24:57.178Z | 203.87° SW |
| 7 mins | 2026-08-02 19:02:57.178Z | 104.289° ESE | 2026-08-02 19:05:57.178Z | 60.412° ENE | 24.484° | 2026-08-02 19:09:57.178Z | 13.178° NNE |
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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