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.

Not visible in the next 10 days
Identifier
43646, 2014-090D
Orbit
GEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SISE
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2014-12-31 (12 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.3 m
Radar Cross Section
0.137 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 FENGYUN 2G DEB
1 43646U 14090D   26289.97357657  .00000067  00000-0  00000-0 0  9996
2 43646   7.8367  66.7434 0202106 291.2970  66.5750  1.00266621 42927
Epoch: 2026-10-16T23:21Z
TLE epoch observation values (Epoch: 2026-10-16T23:21:57.015Z)
Latitude
0°
Longitude
50.75978°
Altitude
35,459.288 km
Speed
3.099 km/s
True Right ascension
04h 26m 56s
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
20:37:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,641.309 km
Perigee altitude
34,936.86 km
Semi-major axis
42,167.222 km
Eccentricity
0.02021
Inclination
7.8367°
RAAN
66.7434°
Arg. of periapsis
291.297°
True anomaly
68.72113°
Mean anomaly
66.575°
Eccentric anomaly
67.64596°
Mean motion
0.25066 °/min
Orbital period
1,436.22 mins
BSTAR
0
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Other satellites on launch #90 in the year 2014 (2014-12-31 UTC)

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