FENGYUN 1C DEB, 30125
Orbit data source: Space-Track
FENGYUN 1C DEB, 30125 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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30125 intel report (Beta)
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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 30125U 99025SE 26011.25305537 .00003810 00000-0 94398-3 0 9994
2 30125 98.7211 114.8378 0341289 258.3903 126.2231 14.22849811973411Epoch: 2026-01-11T06:04Z
TLE epoch observation values (Epoch: 2026-01-11T06:04:23.983Z)
Latitude
27.3808°
Longitude
-91.56215°
Altitude
969.483 km
Speed
7.292 km/s
True Right ascension
07h 21m 13s
True Declination
27° 14' 41"
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
06:41:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,058.303 km
Perigee altitude
567.46 km
Semi-major axis
7,191.018 km
Eccentricity
0.03413
Inclination
98.7211°
RAAN
114.8378°
Arg. of periapsis
258.3903°
True anomaly
129.29897°
Mean anomaly
126.2231°
Eccentric anomaly
127.76885°
Mean motion
3.55924 °/min
Orbital period
101.15 mins
BSTAR
0.00094398
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-01-12 07:21:50.329Z | 194.466° SSW | 2026-01-12 07:26:50.329Z | 265.03° W | 35.065° | 2026-01-12 07:32:50.329Z | 333.627° NNW |
| 10 mins | 2026-01-12 19:40:50.329Z | 14.013° NNE | 2026-01-12 19:45:50.329Z | 187.728° SSW | 44.631° | 2026-01-12 19:50:50.329Z | 194.676° SSW |
| 4 mins | 2026-01-12 21:22:50.329Z | 320.982° NNW | 2026-01-12 21:24:50.329Z | 298.995° NW | 14.305° | 2026-01-12 21:26:50.329Z | 277.436° WNW |
| 8 mins | 2026-01-13 05:21:50.329Z | 100.598° ESE | 2026-01-13 05:25:50.329Z | 54.858° ENE | 20.673° | 2026-01-13 05:29:50.329Z | 15.488° NNE |
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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