FENGYUN 1C DEB, 29798
Orbit data source: Space-Track
FENGYUN 1C DEB, 29798 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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29798 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: 20 hours ago
TLE from 20 hours ago
0 FENGYUN 1C DEB
1 29798U 99025CQ 26134.64672211 .00001572 00000-0 10434-2 0 9994
2 29798 99.2828 205.8950 0107401 214.7929 303.2246 14.00181196980649Epoch: 2026-05-14T15:31Z
TLE epoch observation values (Epoch: 2026-05-14T15:31:16.790Z)
Latitude
22.71963°
Longitude
-75.41087°
Altitude
853.679 km
Speed
7.449 km/s
True Right ascension
01h 59m 11s
True Declination
22° 35' 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
20:05:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
968.445 km
Perigee altitude
812.316 km
Semi-major axis
7,268.517 km
Eccentricity
0.01074
Inclination
99.2828°
RAAN
205.895°
Arg. of periapsis
214.7929°
True anomaly
302.18749°
Mean anomaly
303.2246°
Eccentric anomaly
302.70681°
Mean motion
3.50247 °/min
Orbital period
102.78 mins
BSTAR
0.0010434
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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 | 2026-05-15 17:05:30.130Z | 30.221° NE | 2026-05-15 17:10:30.130Z | 108.067° ESE | 34.45° | 2026-05-15 17:14:30.130Z | 166.764° S |
| 7 mins | 2026-05-15 18:48:30.130Z | 337.439° NNW | 2026-05-15 18:51:30.130Z | 295.046° NW | 23.288° | 2026-05-15 18:55:30.130Z | 245.097° WSW |
| 4 mins | 2026-05-16 02:59:30.130Z | 73.233° E | 2026-05-16 03:00:30.130Z | 62.561° ENE | 13.959° | 2026-05-16 03:03:30.130Z | 31.242° NE |
| 11 mins | 2026-05-16 04:36:30.130Z | 162.762° S | 2026-05-16 04:41:30.130Z | 115.351° SE | 44.954° | 2026-05-16 04:47:30.130Z | 346.444° 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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