FENGYUN 1C DEB, 30413
Orbit data source: Space-Track
FENGYUN 1C DEB, 30413 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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30413 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 30413U 99025AEC 26010.97112412 .00005187 00000-0 19025-2 0 9992
2 30413 102.0633 260.1875 0044035 136.9679 235.4781 14.32926221975580Epoch: 2026-01-10T23:18Z
TLE epoch observation values (Epoch: 2026-01-10T23:18:25.123Z)
Latitude
11.72002°
Longitude
157.56638°
Altitude
801.976 km
Speed
7.444 km/s
True Right ascension
17h 10m 38s
True Declination
11° 39' 08"
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
00:15:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
810.817 km
Perigee altitude
747.781 km
Semi-major axis
7,157.436 km
Eccentricity
0.0044
Inclination
102.0633°
RAAN
260.1875°
Arg. of periapsis
136.9679°
True anomaly
235.06365°
Mean anomaly
235.4781°
Eccentric anomaly
235.27074°
Mean motion
3.58432 °/min
Orbital period
100.44 mins
BSTAR
0.0019025
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-01-12 04:21:43.678Z | 67.642° E | 2026-01-12 04:23:43.678Z | 93.906° ESE | 15.165° | 2026-01-12 04:26:43.678Z | 132.186° SE |
| 8 mins | 2026-01-12 05:59:43.678Z | 4.908° NNE | 2026-01-12 06:02:43.678Z | 314.493° NW | 39.362° | 2026-01-12 06:07:43.678Z | 215.015° SW |
| 8 mins | 2026-01-12 15:36:43.678Z | 125.972° SE | 2026-01-12 15:40:43.678Z | 55.322° ENE | 31.547° | 2026-01-12 15:44:43.678Z | 359.721° N |
| 6 mins | 2026-01-12 17:16:43.678Z | 218.719° SW | 2026-01-12 17:19:43.678Z | 267.406° W | 23.165° | 2026-01-12 17:22:43.678Z | 309.405° NW |
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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