FENGYUN 1C DEB, 30235
Orbit data source: Space-Track
FENGYUN 1C DEB, 30235 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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30235 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: 4 hours ago
TLE from 4 hours ago
0 FENGYUN 1C DEB
1 30235U 99025WU 26299.29087001 .00000238 00000-0 14410-3 0 9999
2 30235 98.7336 313.0830 0154528 60.9810 313.0609 14.09157055 13641Epoch: 2026-10-26T06:58Z
TLE epoch observation values (Epoch: 2026-10-26T06:58:51.168Z)
Latitude
12.54203°
Longitude
171.75129°
Altitude
788.932 km
Speed
7.499 km/s
True Right ascension
20h 44m 32s
True Declination
12° 28' 11"
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
06:28:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.272 km
Perigee altitude
747.59 km
Semi-major axis
7,237.568 km
Eccentricity
0.01545
Inclination
98.7336°
RAAN
313.083°
Arg. of periapsis
60.981°
True anomaly
311.74997°
Mean anomaly
313.0609°
Eccentric anomaly
312.40716°
Mean motion
3.52496 °/min
Orbital period
102.13 mins
BSTAR
0.0001441
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-26 12:38:16.103Z | 55.205° ENE | 2026-10-26 12:41:16.103Z | 90.02° ESE | 16.498° | 2026-10-26 12:44:16.103Z | 125.591° SE |
| 8 mins | 2026-10-26 14:19:16.103Z | 0.964° NNE | 2026-10-26 14:22:16.103Z | 311.616° NW | 58.896° | 2026-10-26 14:27:16.103Z | 210.282° SW |
| 6 mins | 2026-10-27 00:07:16.103Z | 110.427° ESE | 2026-10-27 00:10:16.103Z | 58.798° ENE | 27.059° | 2026-10-27 00:13:16.103Z | 15.69° NNE |
| 7 mins | 2026-10-27 01:47:16.103Z | 206.543° SW | 2026-10-27 01:50:16.103Z | 251.648° W | 31.39° | 2026-10-27 01:54:16.103Z | 319.744° 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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