FENGYUN 1C DEB, 30993
Orbit data source: Space-Track
FENGYUN 1C DEB, 30993 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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30993 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, 0.050 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 FENGYUN 1C DEB
1 30993U 99025BCK 26300.23036918 .00002637 00000-0 87949-3 0 9990
2 30993 98.8482 46.4942 0018179 156.0004 233.4885 14.38325645 14959Epoch: 2026-10-27T05:31Z
TLE epoch observation values (Epoch: 2026-10-27T05:31:43.897Z)
Latitude
28.98739°
Longitude
-76.95636°
Altitude
775.381 km
Speed
7.465 km/s
True Right ascension
02h 46m 17s
True Declination
28° 50' 32"
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
07:50:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
774.155 km
Perigee altitude
748.198 km
Semi-major axis
7,139.314 km
Eccentricity
0.00182
Inclination
98.8482°
RAAN
46.4942°
Arg. of periapsis
156.0004°
True anomaly
233.32129°
Mean anomaly
233.4885°
Eccentric anomaly
233.40487°
Mean motion
3.59798 °/min
Orbital period
100.06 mins
BSTAR
0.00087949
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-30 19:07:59.139Z | 44.598° NE | 2026-10-30 19:11:59.139Z | 98.759° ESE | 22.056° | 2026-10-30 19:14:59.139Z | 140.151° SSE |
| 7 mins | 2026-10-30 20:47:59.139Z | 346.9° N | 2026-10-30 20:50:59.139Z | 284.227° WNW | 39.953° | 2026-10-30 20:54:59.139Z | 224.109° SW |
| 7 mins | 2026-10-31 06:22:59.139Z | 114.734° SE | 2026-10-31 06:25:59.139Z | 60.666° ENE | 30.809° | 2026-10-31 06:29:59.139Z | 7.619° NNE |
| 6 mins | 2026-10-31 08:01:59.139Z | 218.204° SW | 2026-10-31 08:04:59.139Z | 273.213° WNW | 29.528° | 2026-10-31 08:07:59.139Z | 317.261° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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