FENGYUN 1C DEB, 30453
Orbit data source: Space-Track
FENGYUN 1C DEB, 30453 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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30453 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: 16 hours ago
TLE from 16 hours ago
0 FENGYUN 1C DEB
1 30453U 99025AFQ 26263.94216172 .00001601 00000-0 63955-3 0 9990
2 30453 98.7955 341.8298 0114409 128.4680 287.8403 14.26298784 12560Epoch: 2026-09-20T22:36Z
TLE epoch observation values (Epoch: 2026-09-20T22:36:42.772Z)
Latitude
54.20347°
Longitude
-9.50042°
Altitude
788.697 km
Speed
7.477 km/s
True Right ascension
21h 58m 01s
True Declination
54° 02' 27"
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
08:08:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
883.422 km
Perigee altitude
719.144 km
Semi-major axis
7,179.42 km
Eccentricity
0.01144
Inclination
98.7955°
RAAN
341.8298°
Arg. of periapsis
128.468°
True anomaly
286.58692°
Mean anomaly
287.8403°
Eccentric anomaly
287.21415°
Mean motion
3.56787 °/min
Orbital period
100.9 mins
BSTAR
0.00063955
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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 | 2026-09-21 17:27:32.124Z | 36.134° NE | 2026-09-21 17:31:32.124Z | 94.287° ESE | 30.528° | 2026-09-21 17:35:32.124Z | 156.437° SSE |
| 6 mins | 2026-09-21 19:08:32.124Z | 339.444° N | 2026-09-21 19:11:32.124Z | 288.255° WNW | 27.17° | 2026-09-21 19:14:32.124Z | 242.422° WSW |
| 8 mins | 2026-09-22 04:47:32.124Z | 140.493° SSE | 2026-09-22 04:51:32.124Z | 63.988° ENE | 49.783° | 2026-09-22 04:55:32.124Z | 0.159° NNE |
| 5 mins | 2026-09-22 06:29:32.124Z | 241.153° WSW | 2026-09-22 06:31:32.124Z | 269.684° W | 19.087° | 2026-09-22 06:34:32.124Z | 307.589° NW |
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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