FENGYUN 1C DEB, 29836
Orbit data source: Space-Track
FENGYUN 1C DEB, 29836 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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29836 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: 17 hours ago
TLE from 17 hours ago
0 FENGYUN 1C DEB
1 29836U 99025EE 26107.53888214 .00001536 00000-0 31644-3 0 9994
2 29836 98.1825 205.8340 0153630 173.1540 203.8424 14.54752754653847Epoch: 2026-04-17T12:55Z
TLE epoch observation values (Epoch: 2026-04-17T12:55:59.416Z)
Latitude
16.10759°
Longitude
163.79858°
Altitude
812.374 km
Speed
7.396 km/s
True Right ascension
13h 33m 52s
True Declination
16° 01' 01"
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
12:53:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
816.107 km
Perigee altitude
598.401 km
Semi-major axis
7,085.391 km
Eccentricity
0.01536
Inclination
98.1825°
RAAN
205.834°
Arg. of periapsis
173.154°
True anomaly
203.14309°
Mean anomaly
203.8424°
Eccentric anomaly
203.49153°
Mean motion
3.63913 °/min
Orbital period
98.92 mins
BSTAR
0.00031644
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-18 07:07:39.885Z | 196.836° SSW | 2026-04-18 07:11:39.885Z | 255.497° W | 31.815° | 2026-04-18 07:15:39.885Z | 325.081° NNW |
| 7 mins | 2026-04-18 19:09:39.885Z | 23.97° NE | 2026-04-18 19:12:39.885Z | 82.755° E | 40.208° | 2026-04-18 19:16:39.885Z | 179.914° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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