FENGYUN 2H AKM, 43497
Orbit data source: Space-Track
FENGYUN 2H AKM, 43497 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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43497 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 FENGYUN 2H AKM
1 43497U 18050C 26317.96562123 .00000157 00000-0 00000-0 0 9997
2 43497 5.2475 74.5753 0087336 329.5272 29.8178 1.00067338 30804Epoch: 2026-11-13T23:10Z
TLE epoch observation values (Epoch: 2026-11-13T23:10:29.674Z)
Latitude
0°
Longitude
33.69681°
Altitude
35,522.578 km
Speed
3.096 km/s
True Right ascension
04h 57m 35s
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
10:41:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,213.823 km
Perigee altitude
35,476.302 km
Semi-major axis
42,223.199 km
Eccentricity
0.00873
Inclination
5.2475°
RAAN
74.5753°
Arg. of periapsis
329.5272°
True anomaly
30.32019°
Mean anomaly
29.8178°
Eccentric anomaly
30.06852°
Mean motion
0.25016 °/min
Orbital period
1,439.08 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 AKM 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 AKM is likely not visible in the next few days. |
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43497 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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