FENGYUN 1C DEB, 30325
Orbit data source: Space-Track
FENGYUN 1C DEB, 30325 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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30325 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
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 30325U 99025AAL 25259.00018915 .00000177 00000-0 12650-3 0 9997
2 30325 98.7426 281.0088 0016975 139.5488 220.6948 14.09060712957804Epoch: 2025-09-16T00:00Z
TLE epoch observation values (Epoch: 2025-09-16T00:00:16.342Z)
Latitude
0°
Longitude
-74.25607°
Altitude
874.816 km
Speed
7.41 km/s
True Right ascension
18h 44m 02s
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
05:36:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
872.049 km
Perigee altitude
847.476 km
Semi-major axis
7,237.9 km
Eccentricity
0.0017
Inclination
98.7426°
RAAN
281.0088°
Arg. of periapsis
139.5488°
True anomaly
220.56817°
Mean anomaly
220.6948°
Eccentric anomaly
220.63147°
Mean motion
3.52472 °/min
Orbital period
102.14 mins
BSTAR
0.0001265
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-17 14:04:52.685Z | 24.082° NE | 2025-09-17 14:09:52.685Z | 110.51° ESE | 39.519° | 2025-09-17 14:14:52.685Z | 178.506° S |
| 6 mins | 2025-09-17 15:47:52.685Z | 327.63° NNW | 2025-09-17 15:49:52.685Z | 301.3° NW | 18.72° | 2025-09-17 15:53:52.685Z | 253.266° W |
| 9 mins | 2025-09-18 01:32:52.685Z | 167.518° S | 2025-09-18 01:36:52.685Z | 209.168° SW | 44.799° | 2025-09-18 01:41:52.685Z | 345.089° N |
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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