FENGYUN 2H DEB, 43645
Orbit data source: Space-Track
FENGYUN 2H DEB, 43645 is space debris in GEO originally from a launch on Tue, 05 Jun 2018 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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43645 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FENGYUN 2H DEB
1 43645U 18050D 26316.80580528 -.00000236 00000-0 00000+0 0 9991
2 43645 5.2722 74.2127 0062008 268.4613 90.6699 1.00305932 30411Epoch: 2026-11-12T19:20Z
TLE epoch observation values (Epoch: 2026-11-12T19:20:21.576Z)
Latitude
0°
Longitude
92.00298°
Altitude
35,780.201 km
Speed
3.075 km/s
True Right ascension
04h 56m 06s
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
10:41:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,039.485 km
Perigee altitude
35,516.68 km
Semi-major axis
42,156.219 km
Eccentricity
0.0062
Inclination
5.2722°
RAAN
74.2127°
Arg. of periapsis
268.4613°
True anomaly
91.38033°
Mean anomaly
90.6699°
Eccentric anomaly
91.02512°
Mean motion
0.25076 °/min
Orbital period
1,435.66 mins
BSTAR
0
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Other satellites on launch #50 in the year 2018 (2018-06-05 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 2H 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 2H DEB is likely not visible in the next few days. |
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43645 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
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