FENGYUN 1C DEB, 30245
Orbit data source: Space-Track
FENGYUN 1C DEB, 30245 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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30245 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: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 30245U 99025XE 26253.17119905 .00000661 00000-0 59397-3 0 9999
2 30245 98.9101 229.6695 0190382 243.8681 114.2777 13.79691342984362Epoch: 2026-09-10T04:06Z
TLE epoch observation values (Epoch: 2026-09-10T04:06:31.597Z)
Latitude
-0.00007°
Longitude
178.82512°
Altitude
1,027.511 km
Speed
7.308 km/s
True Right ascension
15h 18m 40s
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
07:33:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,101.949 km
Perigee altitude
822.456 km
Semi-major axis
7,340.339 km
Eccentricity
0.01904
Inclination
98.9101°
RAAN
229.6695°
Arg. of periapsis
243.8681°
True anomaly
116.24672°
Mean anomaly
114.2777°
Eccentric anomaly
115.26417°
Mean motion
3.45119 °/min
Orbital period
104.31 mins
BSTAR
0.00059397
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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 | 2026-09-11 22:00:35.303Z | 143.277° SSE | 2026-09-11 22:05:35.303Z | 59.521° ENE | 58.336° | 2026-09-11 22:11:35.303Z | 354.653° N |
| 9 mins | 2026-09-11 23:44:35.303Z | 223.33° SW | 2026-09-11 23:48:35.303Z | 267.199° W | 24.428° | 2026-09-11 23:53:35.303Z | 317.772° NNW |
| 9 mins | 2026-09-12 10:41:35.303Z | 36.542° NE | 2026-09-12 10:45:35.303Z | 89.798° E | 38.524° | 2026-09-12 10:50:35.303Z | 160.564° S |
| 9 mins | 2026-09-12 12:24:35.303Z | 348.442° N | 2026-09-12 12:28:35.303Z | 298.067° NW | 33.018° | 2026-09-12 12:33:35.303Z | 235.835° WSW |
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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