FENGYUN 1C DEB, 30113
Orbit data source: Space-Track
FENGYUN 1C DEB, 30113 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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30113 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 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 30113U 99025RS 26154.60460784 .00005145 00000-0 14001-2 0 9999
2 30113 99.0310 23.1996 0036409 205.3433 209.2470 14.47542272 4066Epoch: 2026-06-03T14:30Z
TLE epoch observation values (Epoch: 2026-06-03T14:30:38.117Z)
Latitude
53.5092°
Longitude
-98.86056°
Altitude
765.041 km
Speed
7.465 km/s
True Right ascension
00h 43m 26s
True Declination
53° 20' 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
01:59:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
756.708 km
Perigee altitude
704.942 km
Semi-major axis
7,108.962 km
Eccentricity
0.00364
Inclination
99.031°
RAAN
23.1996°
Arg. of periapsis
205.3433°
True anomaly
209.04397°
Mean anomaly
209.247°
Eccentric anomaly
209.1454°
Mean motion
3.62104 °/min
Orbital period
99.42 mins
BSTAR
0.0014001
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-11 03:39:24.996Z | 30.646° NE | 2026-06-11 03:43:24.996Z | 90.594° ESE | 32.441° | 2026-06-11 03:47:24.996Z | 164.941° S |
| 5 mins | 2026-06-11 05:19:24.996Z | 331.104° NNW | 2026-06-11 05:21:24.996Z | 300.241° NW | 20.169° | 2026-06-11 05:24:24.996Z | 254.27° W |
| 8 mins | 2026-06-11 14:49:24.996Z | 142.326° SSE | 2026-06-11 14:53:24.996Z | 53.751° ENE | 37.926° | 2026-06-11 14:57:24.996Z | 357.411° 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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