FENGYUN 1C DEB, 30036
Orbit data source: Space-Track
FENGYUN 1C DEB, 30036 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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30036 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, 0.050 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 1C DEB
1 30036U 99025NM 26297.06311006 .00001132 00000-0 26076-3 0 9991
2 30036 98.2243 320.7779 0186877 325.9116 56.5363 14.47211357 37330Epoch: 2026-10-24T01:30Z
TLE epoch observation values (Epoch: 2026-10-24T01:30:52.709Z)
Latitude
24.01731°
Longitude
-98.089°
Altitude
666.168 km
Speed
7.564 km/s
True Right ascension
21h 08m 25s
True Declination
23° 53' 17"
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
06:10:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
864.739 km
Perigee altitude
598.999 km
Semi-major axis
7,110.006 km
Eccentricity
0.01869
Inclination
98.2243°
RAAN
320.7779°
Arg. of periapsis
325.9116°
True anomaly
58.34577°
Mean anomaly
56.5363°
Eccentric anomaly
57.43873°
Mean motion
3.62025 °/min
Orbital period
99.44 mins
BSTAR
0.00026076
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-10-24 13:36:01.815Z | 37.959° NE | 2026-10-24 13:41:01.815Z | 100.142° ESE | 26.342° | 2026-10-24 13:45:01.815Z | 148.405° SSE |
| 9 mins | 2026-10-24 15:15:01.815Z | 353.791° N | 2026-10-24 15:19:01.815Z | 292.651° NW | 42.508° | 2026-10-24 15:24:01.815Z | 222.071° SW |
| 6 mins | 2026-10-25 00:48:01.815Z | 102.521° ESE | 2026-10-25 00:50:01.815Z | 66.763° ENE | 25.227° | 2026-10-25 00:54:01.815Z | 12.089° NNE |
| 6 mins | 2026-10-25 02:26:01.815Z | 216.982° SW | 2026-10-25 02:28:01.815Z | 257.306° W | 32.451° | 2026-10-25 02:32:01.815Z | 323.942° NNW |
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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