FENGYUN 1C DEB, 29893
Orbit data source: Space-Track
FENGYUN 1C DEB, 29893 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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29893 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 29893U 99025GP 26260.48193046 .00000101 00000-0 11881-3 0 9991
2 29893 98.5394 334.6470 0173941 119.0089 256.2753 13.79570428989834Epoch: 2026-09-17T11:33Z
TLE epoch observation values (Epoch: 2026-09-17T11:33:58.791Z)
Latitude
13.17255°
Longitude
162.73°
Altitude
999.926 km
Speed
7.337 km/s
True Right ascension
22h 10m 34s
True Declination
13° 05' 56"
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
09:03:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,090.3 km
Perigee altitude
834.929 km
Semi-major axis
7,340.751 km
Eccentricity
0.01739
Inclination
98.5394°
RAAN
334.647°
Arg. of periapsis
119.0089°
True anomaly
254.3493°
Mean anomaly
256.2753°
Eccentric anomaly
255.31126°
Mean motion
3.4509 °/min
Orbital period
104.32 mins
BSTAR
0.00011881
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-09-18 17:40:10.664Z | 19.513° NNE | 2026-09-18 17:45:10.664Z | 83.934° E | 64.218° | 2026-09-18 17:50:10.664Z | 182.28° SSW |
| 5 mins | 2026-09-18 19:26:10.664Z | 321.559° NNW | 2026-09-18 19:28:10.664Z | 296.193° NW | 16.51° | 2026-09-18 19:31:10.664Z | 261.986° W |
| 7 mins | 2026-09-19 03:42:10.664Z | 101.438° ESE | 2026-09-19 03:45:10.664Z | 65.867° ENE | 20.955° | 2026-09-19 03:49:10.664Z | 19.264° NNE |
| 10 mins | 2026-09-19 05:23:10.664Z | 183.432° SSW | 2026-09-19 05:28:10.664Z | 266.446° W | 57.386° | 2026-09-19 05:33:10.664Z | 336.919° NNW |
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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