FENGYUN 1C DEB, 30936
Orbit data source: Space-Track
FENGYUN 1C DEB, 30936 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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30936 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 FENGYUN 1C DEB
1 30936U 99025BAA 26169.34431869 .00000739 00000-0 33767-3 0 9996
2 30936 98.5595 200.3465 0048112 104.5767 274.7838 14.23778288998027Epoch: 2026-06-18T08:15Z
TLE epoch observation values (Epoch: 2026-06-18T08:15:49.134Z)
Latitude
18.58944°
Longitude
166.9165°
Altitude
812.286 km
Speed
7.45 km/s
True Right ascension
13h 09m 50s
True Declination
18° 29' 12"
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
08:53:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
844.332 km
Perigee altitude
775.167 km
Semi-major axis
7,187.886 km
Eccentricity
0.00481
Inclination
98.5595°
RAAN
200.3465°
Arg. of periapsis
104.5767°
True anomaly
274.23413°
Mean anomaly
274.7838°
Eccentric anomaly
274.50899°
Mean motion
3.56157 °/min
Orbital period
101.08 mins
BSTAR
0.00033767
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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 | 2026-06-19 01:11:13.163Z | 120.533° SE | 2026-06-19 01:14:13.163Z | 78.34° E | 26.306° | 2026-06-19 01:18:13.163Z | 14.422° NNE |
| 7 mins | 2026-06-19 02:51:13.163Z | 209.432° SW | 2026-06-19 02:54:13.163Z | 255.136° W | 27.605° | 2026-06-19 02:58:13.163Z | 319.593° NNW |
| 8 mins | 2026-06-19 15:07:13.163Z | 9.39° NNE | 2026-06-19 15:11:13.163Z | 247.949° W | 44.127° | 2026-06-19 15:15:13.163Z | 200.339° SSW |
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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