FENGYUN 1C DEB, 29754
Orbit data source: Space-Track
FENGYUN 1C DEB, 29754 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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29754 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 29754U 99025AU 26207.25592502 .00001589 00000-0 76523-3 0 9998
2 29754 98.8921 315.7483 0033830 315.3632 74.0447 14.19920685 5407Epoch: 2026-07-26T06:08Z
TLE epoch observation values (Epoch: 2026-07-26T06:08:31.921Z)
Latitude
29.43731°
Longitude
-85.37962°
Altitude
822.65 km
Speed
7.448 km/s
True Right ascension
20h 42m 50s
True Declination
29° 17' 30"
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
00:01:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.149 km
Perigee altitude
798.428 km
Semi-major axis
7,200.926 km
Eccentricity
0.00338
Inclination
98.8921°
RAAN
315.7483°
Arg. of periapsis
315.3632°
True anomaly
74.41786°
Mean anomaly
74.0447°
Eccentric anomaly
74.23124°
Mean motion
3.5519 °/min
Orbital period
101.35 mins
BSTAR
0.00076523
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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 | 2026-07-27 19:47:28.044Z | 25.238° NE | 2026-07-27 19:52:28.044Z | 110.111° ESE | 38.669° | 2026-07-27 19:57:28.044Z | 177.29° S |
| 6 mins | 2026-07-27 21:29:28.044Z | 330.74° NNW | 2026-07-27 21:32:28.044Z | 289.519° WNW | 19.506° | 2026-07-27 21:35:28.044Z | 253.883° W |
| 9 mins | 2026-07-28 07:10:28.044Z | 161.537° S | 2026-07-28 07:14:28.044Z | 25.174° NE | 44.655° | 2026-07-28 07:19:28.044Z | 347.718° N |
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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