FENGYUN 1C DEB, 37044
Orbit data source: Space-Track
FENGYUN 1C DEB, 37044 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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37044 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 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 37044U 99025EEC 26092.54273684 .00010751 00000-0 47410-2 0 9993
2 37044 98.9595 196.8179 0503168 227.1237 128.6616 13.72221089853778Epoch: 2026-04-02T13:01Z
TLE epoch observation values (Epoch: 2026-04-02T13:01:32.462Z)
Latitude
-0.00006°
Longitude
170.54293°
Altitude
1,237.006 km
Speed
7.116 km/s
True Right ascension
13h 07m 16s
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
19:07:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,359.514 km
Perigee altitude
618.15 km
Semi-major axis
7,366.969 km
Eccentricity
0.05032
Inclination
98.9595°
RAAN
196.8179°
Arg. of periapsis
227.1237°
True anomaly
132.98933°
Mean anomaly
128.6616°
Eccentric anomaly
130.84257°
Mean motion
3.43249 °/min
Orbital period
104.88 mins
BSTAR
0.004741
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-04-03 19:24:20.598Z | 21.809° NNE | 2026-04-03 19:30:20.598Z | 101.924° ESE | 40.176° | 2026-04-03 19:35:20.598Z | 177.979° S |
| 7 mins | 2026-04-03 21:10:20.598Z | 334.851° NNW | 2026-04-03 21:13:20.598Z | 299.111° NW | 20.579° | 2026-04-03 21:17:20.598Z | 253.593° W |
| 11 mins | 2026-04-04 05:26:20.598Z | 107.951° ESE | 2026-04-04 05:31:20.598Z | 60.494° ENE | 25.749° | 2026-04-04 05:37:20.598Z | 8.56° NNE |
| 14 mins | 2026-04-04 07:07:20.598Z | 177.034° S | 2026-04-04 07:14:20.598Z | 269.635° W | 42.904° | 2026-04-04 07:21:20.598Z | 340.268° N |
| 4 mins | 2026-04-04 08:57:20.598Z | 264.437° W | 2026-04-04 08:58:20.598Z | 272.134° WNW | 12.226° | 2026-04-04 09:01:20.598Z | 294.787° NW |
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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