FENGYUN 1C DEB, 30552
Orbit data source: Space-Track
FENGYUN 1C DEB, 30552 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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30552 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: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 30552U 99025AKS 26296.38992556 .00010464 00000-0 20871-2 0 9997
2 30552 98.8456 93.1795 0011486 14.5395 345.6132 14.62127885 22392Epoch: 2026-10-23T09:21Z
TLE epoch observation values (Epoch: 2026-10-23T09:21:29.568Z)
Latitude
-0.00007°
Longitude
-79.00485°
Altitude
681.418 km
Speed
7.52 km/s
True Right ascension
06h 12m 43s
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
14:10:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
691.532 km
Perigee altitude
675.31 km
Semi-major axis
7,061.558 km
Eccentricity
0.00115
Inclination
98.8456°
RAAN
93.1795°
Arg. of periapsis
14.5395°
True anomaly
345.58045°
Mean anomaly
345.6132°
Eccentric anomaly
345.59683°
Mean motion
3.65757 °/min
Orbital period
98.43 mins
BSTAR
0.0020871
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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 | 2026-10-24 23:43:10.745Z | 5.642° NNE | 2026-10-24 23:46:10.745Z | 264.877° W | 70.735° | 2026-10-24 23:50:10.745Z | 203.19° SW |
| 8 mins | 2026-10-25 10:45:10.745Z | 176.605° S | 2026-10-25 10:48:10.745Z | 220.57° SW | 63.214° | 2026-10-25 10:53:10.745Z | 340.9° N |
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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