FENGYUN 1C DEB, 36203
Orbit data source: Space-Track
FENGYUN 1C DEB, 36203 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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36203 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: 3 weeks ago
TLE from 3 weeks ago
0 FENGYUN 1C DEB
1 36203U 99025DUC 26022.59052217 .00016324 00000-0 20720-2 0 9991
2 36203 99.1016 336.6696 0083067 22.6407 337.8431 14.79342117640330Epoch: 2026-01-22T14:10Z
TLE epoch observation values (Epoch: 2026-01-22T14:10:21.115Z)
Latitude
-0.00004°
Longitude
2.14013°
Altitude
580.516 km
Speed
7.599 km/s
True Right ascension
22h 26m 40s
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
07:06:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
686.703 km
Perigee altitude
570.299 km
Semi-major axis
7,006.638 km
Eccentricity
0.00831
Inclination
99.1016°
RAAN
336.6696°
Arg. of periapsis
22.6407°
True anomaly
337.48062°
Mean anomaly
337.8431°
Eccentric anomaly
337.66221°
Mean motion
3.70066 °/min
Orbital period
97.28 mins
BSTAR
0.002072
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-11 08:40:31.249Z | 66.284° ENE | 2026-02-11 08:42:31.249Z | 92.794° ESE | 13.196° | 2026-02-11 08:44:31.249Z | 119.182° SE |
| 8 mins | 2026-02-11 10:15:31.249Z | 2.964° NNE | 2026-02-11 10:18:31.249Z | 314.476° NW | 39.829° | 2026-02-11 10:23:31.249Z | 208.77° SW |
| 7 mins | 2026-02-11 21:10:31.249Z | 178.959° S | 2026-02-11 21:13:31.249Z | 256.171° W | 41.938° | 2026-02-11 21:17:31.249Z | 338.827° N |
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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