FENGYUN 1C DEB, 37069
Orbit data source: Space-Track
FENGYUN 1C DEB, 37069 is space debris in LEO 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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37069 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: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 37069U 99025EFD 26128.48884219 .00001442 00000-0 16461-2 0 9994
2 37069 95.8491 42.0721 0418860 220.7912 136.1165 13.38681528896718Epoch: 2026-05-08T11:43Z
TLE epoch observation values (Epoch: 2026-05-08T11:43:55.965Z)
Latitude
-0.00006°
Longitude
-0.23098°
Altitude
1,349.342 km
Speed
7.071 km/s
True Right ascension
02h 48m 17s
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
19:03:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,425.049 km
Perigee altitude
797.641 km
Semi-major axis
7,489.482 km
Eccentricity
0.04189
Inclination
95.8491°
RAAN
42.0721°
Arg. of periapsis
220.7912°
True anomaly
139.32086°
Mean anomaly
136.1165°
Eccentric anomaly
137.73071°
Mean motion
3.34862 °/min
Orbital period
107.51 mins
BSTAR
0.0016461
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-15 16:07:41.969Z | 92.791° ESE | 2026-05-15 16:11:41.969Z | 63.527° ENE | 15.48° | 2026-05-15 16:15:41.969Z | 31.58° NE |
| 14 mins | 2026-05-15 17:50:41.969Z | 158.446° S | 2026-05-15 17:57:41.969Z | 60.607° ENE | 43.916° | 2026-05-15 18:04:41.969Z | 354.468° N |
| 10 mins | 2026-05-15 19:39:41.969Z | 232.037° WSW | 2026-05-15 19:44:41.969Z | 275.614° WNW | 21.864° | 2026-05-15 19:49:41.969Z | 317.855° NNW |
| 4 mins | 2026-05-16 05:11:41.969Z | 62.681° ENE | 2026-05-16 05:13:41.969Z | 83.748° E | 13.325° | 2026-05-16 05:15:41.969Z | 105.334° ESE |
| 10 mins | 2026-05-16 06:55:41.969Z | 5.533° NNE | 2026-05-16 07:00:41.969Z | 314.736° NW | 43.581° | 2026-05-16 07:05:41.969Z | 199.84° SSW |
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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