FENGYUN 1C DEB, 30926
Orbit data source: Space-Track
FENGYUN 1C DEB, 30926 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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30926 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, 0.076 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 30926U 99025AZQ 26300.43053825 .00002500 00000-0 19849-3 0 9997
2 30926 98.8398 283.6354 0158660 75.3172 286.5570 14.92230295 55166Epoch: 2026-10-27T10:19Z
TLE epoch observation values (Epoch: 2026-10-27T10:19:58.504Z)
Latitude
-0.00011°
Longitude
92.84787°
Altitude
564.099 km
Speed
7.595 km/s
True Right ascension
18h 54m 32s
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
08:54:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
698.577 km
Perigee altitude
477.526 km
Semi-major axis
6,966.188 km
Eccentricity
0.01587
Inclination
98.8398°
RAAN
283.6354°
Arg. of periapsis
75.3172°
True anomaly
284.80465°
Mean anomaly
286.557°
Eccentric anomaly
285.68178°
Mean motion
3.73293 °/min
Orbital period
96.44 mins
BSTAR
0.00019849
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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 | 2026-10-29 22:01:56.155Z | 104.026° ESE | 2026-10-29 22:03:56.155Z | 69.794° E | 15.855° | 2026-10-29 22:05:56.155Z | 32.969° NE |
| 4 mins | 2026-10-29 23:37:56.155Z | 222.32° SW | 2026-10-29 23:38:56.155Z | 248.128° W | 28.176° | 2026-10-29 23:41:56.155Z | 317.828° NNW |
| 5 mins | 2026-10-30 11:19:56.155Z | 53.388° ENE | 2026-10-30 11:21:56.155Z | 97.981° ESE | 27.887° | 2026-10-30 11:24:56.155Z | 154.055° SSE |
| 4 mins | 2026-10-30 12:55:56.155Z | 319.084° NNW | 2026-10-30 12:56:56.155Z | 298.903° NW | 20.589° | 2026-10-30 12:59:56.155Z | 246.657° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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