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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Identifier
43497, 2018-050C
Orbit
GEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
China ARMT
Mission
Spacecraft
Bus & Motor
SHANXI AKM, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2018-06-05 (7 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 0.8 m
Radar Cross Section
1.571 m²

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 FENGYUN 2H AKM
1 43497U 18050C   25308.24048045 -.00000268  00000-0  00000-0 0  9993
2 43497   4.2887  79.5337 0085509 318.5278  40.8181  1.00072915 27054
Epoch: 2025-11-04T05:46Z
TLE epoch observation values (Epoch: 2025-11-04T05:46:17.510Z)
Latitude
-0°
Longitude
-50.81431°
Altitude
35,568.277 km
Speed
3.093 km/s
True Right ascension
05h 17m 57s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:01:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,204.531 km
Perigee altitude
35,482.465 km
Semi-major axis
42,221.635 km
Eccentricity
0.00855
Inclination
4.2887°
RAAN
79.5337°
Arg. of periapsis
318.5278°
True anomaly
41.4638°
Mean anomaly
40.8181°
Eccentric anomaly
41.14043°
Mean motion
0.25017 °/min
Orbital period
1,439 mins
BSTAR
0
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Other satellites on launch #50 in the year 2018 (2018-06-05 UTC)

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