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 (11 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

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FENGYUN 2G DEB
1 43646U 14090D   26060.51109839 -.00000241  00000-0  00000-0 0  9995
2 43646   7.2705  69.5862 0224733 284.6095  73.0672  1.00217738 40623
Epoch: 2026-03-01T12:15Z
TLE epoch observation values (Epoch: 2026-03-01T12:15:58.900Z)
Latitude
-0.00001°
Longitude
86.47055°
Altitude
35,547.234 km
Speed
3.093 km/s
True Right ascension
04h 39m 08s
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
07:34:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,750.744 km
Perigee altitude
34,854.854 km
Semi-major axis
42,180.936 km
Eccentricity
0.02247
Inclination
7.2705°
RAAN
69.5862°
Arg. of periapsis
284.6095°
True anomaly
75.55034°
Mean anomaly
73.0672°
Eccentric anomaly
74.30683°
Mean motion
0.25054 °/min
Orbital period
1,436.92 mins
BSTAR
0
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Other satellites on launch #90 in the year 2014 (2014-12-31 UTC)

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