FENGYUN 1C DEB, 29828
Orbit data source: Space-Track
FENGYUN 1C DEB, 29828 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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29828 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: 13 hours ago
TLE from 13 hours ago
0 FENGYUN 1C DEB
1 29828U 99025DW 26176.81921550 .00000768 00000-0 46338-3 0 9995
2 29828 98.7502 221.6816 0059674 327.0073 85.9447 14.08675840994834Epoch: 2026-06-25T19:39Z
TLE epoch observation values (Epoch: 2026-06-25T19:39:40.219Z)
Latitude
52.83846°
Longitude
1.15386°
Altitude
869.679 km
Speed
7.424 km/s
True Right ascension
14h 00m 06s
True Declination
52° 40' 31"
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
20:18:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
904.281 km
Perigee altitude
817.883 km
Semi-major axis
7,239.219 km
Eccentricity
0.00597
Inclination
98.7502°
RAAN
221.6816°
Arg. of periapsis
327.0073°
True anomaly
86.62715°
Mean anomaly
85.9447°
Eccentric anomaly
86.28589°
Mean motion
3.52375 °/min
Orbital period
102.16 mins
BSTAR
0.00046338
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-26 14:46:31.764Z | 50.806° ENE | 2026-06-26 14:49:31.764Z | 87.141° E | 20.793° | 2026-06-26 14:53:31.764Z | 137.395° SSE |
| 9 mins | 2026-06-26 16:27:31.764Z | 355.205° N | 2026-06-26 16:31:31.764Z | 275.298° WNW | 37.321° | 2026-06-26 16:36:31.764Z | 215.995° SW |
| 8 mins | 2026-06-27 02:14:31.764Z | 123.014° SE | 2026-06-27 02:17:31.764Z | 73.381° E | 31.153° | 2026-06-27 02:22:31.764Z | 3.892° NNE |
| 7 mins | 2026-06-27 03:55:31.764Z | 217.128° SW | 2026-06-27 03:58:31.764Z | 260.703° W | 25.102° | 2026-06-27 04:02:31.764Z | 316.893° 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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