FENGYUN 1C DEB, 29888
Orbit data source: Space-Track
FENGYUN 1C DEB, 29888 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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29888 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: 17 hours ago
TLE from 17 hours ago
0 FENGYUN 1C DEB
1 29888U 99025GJ 26166.83922101 .00000882 00000-0 30153-3 0 9990
2 29888 99.1835 11.9583 0272059 218.6045 139.5401 14.20418505 1295Epoch: 2026-06-15T20:08Z
TLE epoch observation values (Epoch: 2026-06-15T20:08:28.695Z)
Latitude
0.00001°
Longitude
165.71889°
Altitude
978.126 km
Speed
7.285 km/s
True Right ascension
00h 47m 49s
True Declination
0° 00' 00"
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
23:49:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,016.978 km
Perigee altitude
625.254 km
Semi-major axis
7,199.253 km
Eccentricity
0.02721
Inclination
99.1835°
RAAN
11.9583°
Arg. of periapsis
218.6045°
True anomaly
141.51167°
Mean anomaly
139.5401°
Eccentric anomaly
140.53096°
Mean motion
3.55314 °/min
Orbital period
101.32 mins
BSTAR
0.00030153
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-16 13:10:13.433Z | 144.969° SSE | 2026-06-16 13:15:13.433Z | 72.571° E | 40.348° | 2026-06-16 13:21:13.433Z | 354.47° N |
| 8 mins | 2026-06-16 14:52:13.433Z | 226.842° WSW | 2026-06-16 14:55:13.433Z | 261.602° W | 21.719° | 2026-06-16 15:00:13.433Z | 316.039° NNW |
| 5 mins | 2026-06-17 01:32:13.433Z | 65.669° ENE | 2026-06-17 01:34:13.433Z | 95.35° ESE | 18.494° | 2026-06-17 01:37:13.433Z | 135.642° SSE |
| 7 mins | 2026-06-17 03:11:13.433Z | 353.542° N | 2026-06-17 03:14:13.433Z | 298.725° NW | 35.39° | 2026-06-17 03:18:13.433Z | 222.976° SW |
| 10 mins | 2026-06-17 12:51:13.433Z | 129.384° SE | 2026-06-17 12:56:13.433Z | 57.69° ENE | 33.025° | 2026-06-17 13:01:13.433Z | 1.841° NNE |
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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