FENGYUN 2F DEB, 43396
Orbit data source: Space-Track
FENGYUN 2F DEB, 43396 is space debris in GEO originally from a launch on Fri, 13 Jan 2012 UTC launched from the Xichang Space Center, China (XSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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43396 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SISE
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 0.3 m
Radar Cross Section
0.137 m²
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 2F DEB
1 43396U 12002D 26133.20465124 -.00000368 00000-0 00000-0 0 9997
2 43396 9.0300 57.7594 0275550 305.1227 52.2401 1.00305564 42419Epoch: 2026-05-13T04:54Z
TLE epoch observation values (Epoch: 2026-05-13T04:54:41.867Z)
Latitude
-0.00001°
Longitude
113.01022°
Altitude
35,081.05 km
Speed
3.126 km/s
True Right ascension
03h 50m 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
17:33:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,939.778 km
Perigee altitude
34,616.544 km
Semi-major axis
42,156.298 km
Eccentricity
0.02756
Inclination
9.03°
RAAN
57.7594°
Arg. of periapsis
305.1227°
True anomaly
54.78932°
Mean anomaly
52.2401°
Eccentric anomaly
53.50937°
Mean motion
0.25075 °/min
Orbital period
1,435.66 mins
BSTAR
0
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Other satellites on launch #2 in the year 2012 (2012-01-13 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 2F DEB Visibility
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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. |
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| FENGYUN 2F DEB is likely not visible in the next few days. |
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43396 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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