FENGYUN 1C DEB, 38809
Orbit data source: Space-Track
FENGYUN 1C DEB, 38809 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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38809 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: 17 hours ago
TLE from 17 hours ago
0 FENGYUN 1C DEB
1 38809U 99025EUZ 26121.21358039 .00000960 00000-0 38280-3 0 9995
2 38809 98.5846 132.0563 0220399 285.3379 72.3539 14.18562050711833Epoch: 2026-05-01T05:07Z
TLE epoch observation values (Epoch: 2026-05-01T05:07:33.345Z)
Latitude
-0.00007°
Longitude
-163.98169°
Altitude
788.181 km
Speed
7.483 km/s
True Right ascension
08h 48m 13s
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
05:16:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
986.181 km
Perigee altitude
668.564 km
Semi-major axis
7,205.509 km
Eccentricity
0.02204
Inclination
98.5846°
RAAN
132.0563°
Arg. of periapsis
285.3379°
True anomaly
74.78019°
Mean anomaly
72.3539°
Eccentric anomaly
73.5651°
Mean motion
3.54851 °/min
Orbital period
101.45 mins
BSTAR
0.0003828
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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 | 2026-05-01 23:52:04.824Z | 132.4° SE | 2026-05-01 23:57:04.824Z | 66.948° ENE | 31.279° | 2026-05-02 00:02:04.824Z | 4.011° NNE |
| 8 mins | 2026-05-02 01:34:04.824Z | 215.751° SW | 2026-05-02 01:37:04.824Z | 260.189° W | 27.074° | 2026-05-02 01:42:04.824Z | 324.086° NNW |
| 6 mins | 2026-05-02 12:14:04.824Z | 59.195° ENE | 2026-05-02 12:17:04.824Z | 93.479° ESE | 17.26° | 2026-05-02 12:20:04.824Z | 126.622° SE |
| 10 mins | 2026-05-02 13:53:04.824Z | 5.146° NNE | 2026-05-02 13:57:04.824Z | 315.735° NNW | 42.022° | 2026-05-02 14:03:04.824Z | 206.588° SW |
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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