FENGYUN 1C DEB, 32088
Orbit data source: Space-Track
FENGYUN 1C DEB, 32088 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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32088 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: 2 months ago
TLE from 2 months ago
0 FENGYUN 1C DEB
1 32088U 99025CQE 26026.87112242 .00001055 00000-0 14528-2 0 9992
2 32088 102.4080 266.6230 0459572 260.7241 94.1635 13.25355927604423Epoch: 2026-01-26T20:54Z
TLE epoch observation values (Epoch: 2026-01-26T20:54:24.977Z)
Latitude
0.00001°
Longitude
-173.14173°
Altitude
1,207.902 km
Speed
7.231 km/s
True Right ascension
17h 46m 29s
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
14:40:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,508.328 km
Perigee altitude
815.298 km
Semi-major axis
7,539.95 km
Eccentricity
0.04596
Inclination
102.408°
RAAN
266.623°
Arg. of periapsis
260.7241°
True anomaly
99.38685°
Mean anomaly
94.1635°
Eccentric anomaly
96.77825°
Mean motion
3.31505 °/min
Orbital period
108.6 mins
BSTAR
0.0014528
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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 | 2026-03-15 14:06:02.302Z | 69.489° E | 2026-03-15 14:08:02.302Z | 53.156° ENE | 12.931° | 2026-03-15 14:11:02.302Z | 27.543° NE |
| 13 mins | 2026-03-15 15:47:02.302Z | 143.934° SSE | 2026-03-15 15:54:02.302Z | 62.639° ENE | 41.839° | 2026-03-15 16:00:02.302Z | 350.148° N |
| 11 mins | 2026-03-15 17:35:02.302Z | 210.228° SW | 2026-03-15 17:41:02.302Z | 264.298° W | 24.715° | 2026-03-15 17:46:02.302Z | 312.039° NW |
| 8 mins | 2026-03-16 05:00:02.302Z | 43.979° NE | 2026-03-16 05:03:02.302Z | 92.764° ESE | 31.441° | 2026-03-16 05:08:02.302Z | 169.467° S |
| 7 mins | 2026-03-16 06:47:02.302Z | 343.756° N | 2026-03-16 06:50:02.302Z | 300.229° NW | 23.42° | 2026-03-16 06:54:02.302Z | 247.81° 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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