FENGYUN 1C DEB, 29918
Orbit data source: Space-Track
FENGYUN 1C DEB, 29918 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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29918 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 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 29918U 99025HQ 26296.23400292 .00003205 00000-0 11239-2 0 9999
2 29918 98.8470 31.2711 0014509 118.4784 270.5594 14.35704522 23048Epoch: 2026-10-23T05:36Z
TLE epoch observation values (Epoch: 2026-10-23T05:36:57.852Z)
Latitude
28.54241°
Longitude
-89.45794°
Altitude
776.171 km
Speed
7.469 km/s
True Right ascension
01h 45m 45s
True Declination
28° 23' 55"
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
00:22:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
780.241 km
Perigee altitude
759.499 km
Semi-major axis
7,148.007 km
Eccentricity
0.00145
Inclination
98.847°
RAAN
31.2711°
Arg. of periapsis
118.4784°
True anomaly
270.39314°
Mean anomaly
270.5594°
Eccentric anomaly
270.47627°
Mean motion
3.59142 °/min
Orbital period
100.24 mins
BSTAR
0.0011239
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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 | 2026-10-24 06:40:29.652Z | 176.827° S | 2026-10-24 06:45:29.652Z | 269.587° W | 63.267° | 2026-10-24 06:49:29.652Z | 337.674° N |
| 8 mins | 2026-10-24 18:52:29.652Z | 34.855° NE | 2026-10-24 18:55:29.652Z | 84.156° E | 41.867° | 2026-10-24 19:00:29.652Z | 169.688° S |
| 6 mins | 2026-10-24 20:32:29.652Z | 329.859° NNW | 2026-10-24 20:34:29.652Z | 299.873° NW | 22.146° | 2026-10-24 20:38:29.652Z | 246.522° 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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