FENGYUN 1C DEB, 29885
Orbit data source: Space-Track
FENGYUN 1C DEB, 29885 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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29885 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: 20 hours ago
TLE from 20 hours ago
0 FENGYUN 1C DEB
1 29885U 99025GF 26207.61013025 .00000158 00000-0 98800-4 0 9995
2 29885 98.3662 133.1511 0116885 234.0732 249.5520 14.13716659 6492Epoch: 2026-07-26T14:38Z
TLE epoch observation values (Epoch: 2026-07-26T14:38:35.253Z)
Latitude
56.77249°
Longitude
162.10297°
Altitude
886.528 km
Speed
7.399 km/s
True Right ascension
21h 44m 13s
True Declination
56° 37' 03"
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
00:28:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
928.246 km
Perigee altitude
759.418 km
Semi-major axis
7,221.969 km
Eccentricity
0.01169
Inclination
98.3662°
RAAN
133.1511°
Arg. of periapsis
234.0732°
True anomaly
248.30347°
Mean anomaly
249.552°
Eccentric anomaly
248.92709°
Mean motion
3.53639 °/min
Orbital period
101.8 mins
BSTAR
0.0000988
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-27 17:25:31.960Z | 82.748° E | 2026-07-27 17:27:31.960Z | 61.506° ENE | 13.815° | 2026-07-27 17:30:31.960Z | 30.182° NE |
| 9 mins | 2026-07-27 19:03:31.960Z | 165.527° S | 2026-07-27 19:07:31.960Z | 187.006° SSW | 44.999° | 2026-07-27 19:12:31.960Z | 346.81° N |
| 8 mins | 2026-07-28 07:26:31.960Z | 36.386° NE | 2026-07-28 07:29:31.960Z | 88.771° E | 34.879° | 2026-07-28 07:34:31.960Z | 168.859° S |
| 6 mins | 2026-07-28 09:07:31.960Z | 333.049° NNW | 2026-07-28 09:10:31.960Z | 289.333° WNW | 22.128° | 2026-07-28 09:13:31.960Z | 250.261° W |
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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