FENGYUN 2G DEB, 43646
Orbit data source: Space-Track
FENGYUN 2G DEB, 43646 is space debris in GEO originally from a launch on Wed, 31 Dec 2014 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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43646 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 FENGYUN 2G DEB
1 43646U 14090D 26167.27524378 -.00000014 00000-0 00000-0 0 9993
2 43646 7.5371 68.2836 0218261 291.7011 65.8330 1.00219676 41699Epoch: 2026-06-16T06:36Z
TLE epoch observation values (Epoch: 2026-06-16T06:36:21.062Z)
Latitude
0.00001°
Longitude
64.48669°
Altitude
35,442.564 km
Speed
3.1 km/s
True Right ascension
04h 32m 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
02:13:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,722.887 km
Perigee altitude
34,881.62 km
Semi-major axis
42,180.39 km
Eccentricity
0.02183
Inclination
7.5371°
RAAN
68.2836°
Arg. of periapsis
291.7011°
True anomaly
68.14002°
Mean anomaly
65.833°
Eccentric anomaly
66.98399°
Mean motion
0.25054 °/min
Orbital period
1,436.9 mins
BSTAR
0
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Other satellites on launch #90 in the year 2014 (2014-12-31 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 2G 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 2G DEB is likely not visible in the next few days. |
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43646 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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