FENGYUN 1C DEB, 35167
Orbit data source: Space-Track
FENGYUN 1C DEB, 35167 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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35167 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 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 35167U 99025DMX 26253.19969384 .00000844 00000-0 24875-3 0 9999
2 35167 98.4663 244.7331 0228454 120.3952 242.0029 14.32074132739040Epoch: 2026-09-10T04:47Z
TLE epoch observation values (Epoch: 2026-09-10T04:47:33.547Z)
Latitude
0.00003°
Longitude
-176.39751°
Altitude
867.45 km
Speed
7.377 km/s
True Right ascension
16h 18m 55s
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
01:31:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
945.51 km
Perigee altitude
618.36 km
Semi-major axis
7,160.072 km
Eccentricity
0.02285
Inclination
98.4663°
RAAN
244.7331°
Arg. of periapsis
120.3952°
True anomaly
239.72257°
Mean anomaly
242.0029°
Eccentric anomaly
240.85963°
Mean motion
3.58234 °/min
Orbital period
100.49 mins
BSTAR
0.00024875
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-12 12:42:59.014Z | 0.141° NNE | 2026-09-12 12:45:59.014Z | 256.708° W | 58.335° | 2026-09-12 12:49:59.014Z | 206.095° SW |
| 5 mins | 2026-09-12 22:21:59.014Z | 93.93° ESE | 2026-09-12 22:23:59.014Z | 63.706° ENE | 19.11° | 2026-09-12 22:26:59.014Z | 22.861° NE |
| 7 mins | 2026-09-12 23:59:59.014Z | 196.605° SSW | 2026-09-13 00:02:59.014Z | 260.376° W | 45.818° | 2026-09-13 00:06:59.014Z | 331.082° 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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