FENGYUN 2E AKM, 33465

Orbit data source: Space-Track

FENGYUN 2E AKM, 33465 is space debris in GEO originally from a launch on Tue, 23 Dec 2008 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
33465, 2008-066C
Orbit
GEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
China ARMT
Mission
Spacecraft
Bus & Motor
SHANXI AKM, Unknown motor
Mass
Wet unknown, ~50 kg dry
Launch date (UTC)
2008-12-23 (17 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, Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 FENGYUN 2E AKM
1 33465U 08066C   26170.63847777 -.00000224  00000-0  00000-0 0  9995
2 33465   9.8470  44.1641 0033807 325.2964  34.4444  1.02097977 47560
Epoch: 2026-06-19T15:19Z
TLE epoch observation values (Epoch: 2026-06-19T15:19:24.479Z)
Latitude
-0°
Longitude
-93.57986°
Altitude
35,166.257 km
Speed
3.102 km/s
True Right ascension
02h 56m 32s
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
23:07:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,424.174 km
Perigee altitude
35,142.485 km
Semi-major axis
41,661.467 km
Eccentricity
0.00338
Inclination
9.847°
RAAN
44.1641°
Arg. of periapsis
325.2964°
True anomaly
34.66428°
Mean anomaly
34.4444°
Eccentric anomaly
34.55426°
Mean motion
0.25524 °/min
Orbital period
1,410.46 mins
BSTAR
0
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Other satellites on launch #66 in the year 2008 (2008-12-23 UTC)

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