FENGYUN 1C DEB, 30414
Orbit data source: Space-Track
FENGYUN 1C DEB, 30414 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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30414 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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FENGYUN 1C DEB
1 30414U 99025AED 26123.91476370 .00005762 00000-0 19577-2 0 9999
2 30414 99.0923 293.5935 0057850 132.4813 228.1281 14.36065531991264Epoch: 2026-05-03T21:57Z
TLE epoch observation values (Epoch: 2026-05-03T21:57:15.583Z)
Latitude
-0.00003°
Longitude
102.4671°
Altitude
802.196 km
Speed
7.438 km/s
True Right ascension
19h 34m 22s
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
15:48:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
810.028 km
Perigee altitude
727.339 km
Semi-major axis
7,146.82 km
Eccentricity
0.00579
Inclination
99.0923°
RAAN
293.5935°
Arg. of periapsis
132.4813°
True anomaly
227.63685°
Mean anomaly
228.1281°
Eccentric anomaly
227.88224°
Mean motion
3.59231 °/min
Orbital period
100.21 mins
BSTAR
0.0019577
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-04 09:50:40.846Z | 85.407° E | 2026-05-04 09:52:40.846Z | 59.396° ENE | 14.739° | 2026-05-04 09:54:40.846Z | 33.949° NE |
| 8 mins | 2026-05-04 11:27:40.846Z | 178.932° S | 2026-05-04 11:30:40.846Z | 231.311° WSW | 42.046° | 2026-05-04 11:35:40.846Z | 339.548° N |
| 7 mins | 2026-05-04 23:38:40.846Z | 44.79° NE | 2026-05-04 23:41:40.846Z | 110.475° ESE | 31.101° | 2026-05-04 23:45:40.846Z | 166.414° S |
| 6 mins | 2026-05-05 01:17:40.846Z | 333.497° NNW | 2026-05-05 01:19:40.846Z | 302.91° NW | 21.214° | 2026-05-05 01:23:40.846Z | 245.24° 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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