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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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: 16 hours ago
TLE from 16 hours ago
0 FENGYUN 1C DEB
1 30113U 99025RS 26038.57155723 .00007924 00000-0 22028-2 0 9995
2 30113 99.0380 259.4488 0037738 192.8408 221.5575 14.46299459987306Epoch: 2026-02-07T13:43Z
TLE epoch observation values (Epoch: 2026-02-07T13:43:02.544Z)
Latitude
53.24252°
Longitude
-96.23401°
Altitude
766.577 km
Speed
7.465 km/s
True Right ascension
16h 28m 52s
True Declination
53° 04' 40"
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
07:31:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
761.743 km
Perigee altitude
708.057 km
Semi-major axis
7,113.037 km
Eccentricity
0.00377
Inclination
99.038°
RAAN
259.4488°
Arg. of periapsis
192.8408°
True anomaly
221.27164°
Mean anomaly
221.5575°
Eccentric anomaly
221.41447°
Mean motion
3.61793 °/min
Orbital period
99.5 mins
BSTAR
0.0022028
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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 | 2026-02-08 14:29:50.102Z | 161.279° S | 2026-02-08 14:33:50.102Z | 27.086° NE | 44.601° | 2026-02-08 14:37:50.102Z | 347.915° N |
| 6 mins | 2026-02-09 02:35:50.102Z | 49.992° ENE | 2026-02-09 02:38:50.102Z | 94.515° ESE | 21.015° | 2026-02-09 02:41:50.102Z | 139.901° SSE |
| 6 mins | 2026-02-09 04:14:50.102Z | 342.812° N | 2026-02-09 04:16:50.102Z | 304.96° NW | 30.386° | 2026-02-09 04:20:50.102Z | 230.025° 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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