FENGYUN 1C DEB, 32243
Orbit data source: Space-Track
FENGYUN 1C DEB, 32243 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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32243 intel report (Beta)
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Edit Public Description
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: 14 hours ago
TLE from 14 hours ago
0 FENGYUN 1C DEB
1 32243U 99025CWR 25364.04660475 .00006202 00000-0 28147-2 0 9995
2 32243 98.2674 27.1535 0268928 74.3674 288.6997 14.04751435938318Epoch: 2025-12-30T01:07Z
TLE epoch observation values (Epoch: 2025-12-30T01:07:06.650Z)
Latitude
-0.00002°
Longitude
-88.35971°
Altitude
822.496 km
Speed
7.471 km/s
True Right ascension
01h 48m 36s
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
15:01:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,069.588 km
Perigee altitude
679.499 km
Semi-major axis
7,252.681 km
Eccentricity
0.02689
Inclination
98.2674°
RAAN
27.1535°
Arg. of periapsis
74.3674°
True anomaly
285.7502°
Mean anomaly
288.6997°
Eccentric anomaly
287.22799°
Mean motion
3.51395 °/min
Orbital period
102.45 mins
BSTAR
0.0028147
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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 | 2025-12-30 15:24:32.779Z | 303.736° NW | 2025-12-30 15:25:32.779Z | 278.151° WNW | 29.879° | 2025-12-30 15:29:32.779Z | 226.977° WSW |
| 7 mins | 2025-12-31 01:11:32.779Z | 133.767° SE | 2025-12-31 01:14:32.779Z | 72.738° E | 34.184° | 2025-12-31 01:18:32.779Z | 3.055° NNE |
| 4 mins | 2025-12-31 02:54:32.779Z | 242.824° WSW | 2025-12-31 02:56:32.779Z | 273.37° WNW | 16.581° | 2025-12-31 02:58:32.779Z | 301.338° NW |
| 6 mins | 2025-12-31 13:37:32.779Z | 61.439° ENE | 2025-12-31 13:39:32.779Z | 93.132° ESE | 22.19° | 2025-12-31 13:43:32.779Z | 145.39° SSE |
| 7 mins | 2025-12-31 15:17:32.779Z | 350.076° N | 2025-12-31 15:21:32.779Z | 275.802° WNW | 31.635° | 2025-12-31 15:24:32.779Z | 230.178° WSW |
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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