FENGYUN 1C DEB, 30243
Orbit data source: Space-Track
FENGYUN 1C DEB, 30243 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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30243 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 30243U 99025XC 26155.01093448 .00000533 00000-0 30703-3 0 9992
2 30243 98.6861 166.4367 0011867 354.1017 60.4992 14.13270853997266Epoch: 2026-06-04T00:15Z
TLE epoch observation values (Epoch: 2026-06-04T00:15:44.739Z)
Latitude
53.90131°
Longitude
-101.99016°
Altitude
852.805 km
Speed
7.434 km/s
True Right ascension
10h 17m 37s
True Declination
53° 44' 22"
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
04:03:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
853.939 km
Perigee altitude
836.795 km
Semi-major axis
7,223.504 km
Eccentricity
0.00119
Inclination
98.6861°
RAAN
166.4367°
Arg. of periapsis
354.1017°
True anomaly
60.61764°
Mean anomaly
60.4992°
Eccentric anomaly
60.55841°
Mean motion
3.53526 °/min
Orbital period
101.83 mins
BSTAR
0.00030703
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-11 00:20:35.967Z | 147.132° SSE | 2026-06-11 00:24:35.967Z | 87.05° E | 40.084° | 2026-06-11 00:29:35.967Z | 356.185° N |
| 5 mins | 2026-06-11 02:03:35.967Z | 238.908° WSW | 2026-06-11 02:05:35.967Z | 263.859° W | 16.671° | 2026-06-11 02:08:35.967Z | 301.214° NW |
| 7 mins | 2026-06-11 12:43:35.967Z | 48.384° ENE | 2026-06-11 12:46:35.967Z | 90.96° ESE | 24.593° | 2026-06-11 12:50:35.967Z | 146.642° SSE |
| 8 mins | 2026-06-11 14:23:35.967Z | 351.995° N | 2026-06-11 14:27:35.967Z | 289.435° WNW | 31.962° | 2026-06-11 14:31:35.967Z | 229.523° 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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