FENGYUN 1C DEB, 38801
Orbit data source: Space-Track
FENGYUN 1C DEB, 38801 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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38801 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: 5 days ago
TLE from 5 days ago
0 FENGYUN 1C DEB
1 38801U 99025EUR 26066.40393816 .00003651 00000-0 83362-3 0 9999
2 38801 98.3608 118.3108 0346532 102.8707 325.6511 14.25341338655661Epoch: 2026-03-07T09:41Z
TLE epoch observation values (Epoch: 2026-03-07T09:41:40.257Z)
Latitude
64.94593°
Longitude
149.54618°
Altitude
615.772 km
Speed
7.663 km/s
True Right ascension
06h 40m 21s
True Declination
64° 48' 40"
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
00:17:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,053.376 km
Perigee altitude
555.575 km
Semi-major axis
7,182.612 km
Eccentricity
0.03465
Inclination
98.3608°
RAAN
118.3108°
Arg. of periapsis
102.8707°
True anomaly
323.32823°
Mean anomaly
325.6511°
Eccentric anomaly
324.49807°
Mean motion
3.56549 °/min
Orbital period
100.97 mins
BSTAR
0.00083362
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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 | 2026-03-13 03:40:04.825Z | 184.968° SSW | 2026-03-13 03:43:04.825Z | 245.212° WSW | 38.913° | 2026-03-13 03:47:04.825Z | 336.031° NNW |
| 7 mins | 2026-03-13 15:55:04.825Z | 35.212° NE | 2026-03-13 15:57:04.825Z | 79.9° E | 36.58° | 2026-03-13 16:02:04.825Z | 176.732° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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