FENGYUN 1C DEB, 37060
Orbit data source: Space-Track
FENGYUN 1C DEB, 37060 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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37060 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: 6 months ago
TLE from 6 months ago
0 FENGYUN 1C DEB
1 37060U 99025EEU 25264.42451371 .00000533 00000-0 37875-3 0 9991
2 37060 99.1060 322.2229 0079367 215.7472 143.8364 14.00491559615543Epoch: 2025-09-21T10:11Z
TLE epoch observation values (Epoch: 2025-09-21T10:11:17.984Z)
Latitude
-0.00003°
Longitude
168.85472°
Altitude
941.72 km
Speed
7.357 km/s
True Right ascension
21h 28m 53s
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
07:48:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
946.977 km
Perigee altitude
831.618 km
Semi-major axis
7,267.434 km
Eccentricity
0.00794
Inclination
99.106°
RAAN
322.2229°
Arg. of periapsis
215.7472°
True anomaly
144.3688°
Mean anomaly
143.8364°
Eccentric anomaly
144.10303°
Mean motion
3.50325 °/min
Orbital period
102.76 mins
BSTAR
0.00037875
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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 | 2026-03-10 03:57:31.242Z | 163.631° S | 2026-03-10 04:02:31.242Z | 90.73° ESE | 44.988° | 2026-03-10 04:07:31.242Z | 346.409° N |
| 8 mins | 2026-03-10 16:27:31.242Z | 37.188° NE | 2026-03-10 16:30:31.242Z | 89.298° E | 34.716° | 2026-03-10 16:35:31.242Z | 169.562° S |
| 6 mins | 2026-03-10 18:09:31.242Z | 332.847° NNW | 2026-03-10 18:12:31.242Z | 288.092° WNW | 21.795° | 2026-03-10 18:15:31.242Z | 250.103° W |
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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