ATLAS 5 CENTAUR DEB, 43962

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43962 is space debris in HEO originally from a launch on Wed, 17 Sep 2014 UTC launched from the Air Force Eastern Test Range (AFETR). 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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ATLAS 5 CENTAUR DEB details

Identifier	43962, 2014-055R
Orbit	HEO
Last TLE update	2 days ago
Origin	ULA (US)
Manufacturer	Unknown
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2014-09-17 (10 years ago)
Launch vehicle	Unknown
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 days ago

0 ATLAS 5 CENTAUR DEB
1 43962U 14055R   24359.90269888 -.00000004  00000-0  00000-0 0  9997
2 43962  20.0354 169.0263 5106173 123.2857 296.2700  1.90776271 43999

Epoch: 2024-12-24T21:39Z

Definitive object data (Epoch: 2024-12-24T21:39:53.183Z)

Latitude	-0.00002°
Longitude	110.1676°
Altitude	21,789.345 km
Speed	3.713 km/s
True Right ascension	11h 16m 10s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-19.04363°
Longitude	38.74483°
Altitude	33,540.257 km
Speed	2.336 km/s
Apparent Right ascension	06h 26m 02s
Apparent Declination	-21° 51' 49"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	17:51:40
Azimuth	335.43° NNW
Elevation	-70.525°
Doppler factor	1

Orbital elements

Apogee altitude	35,108.338 km
Perigee altitude	7,061.907 km
Semi-major axis	27,463.26 km
Eccentricity	0.5106173
Inclination	20.0354°
RAAN	169.0263°
Arg. of periapsis	123.2857°
True anomaly	236.79346°
Mean anomaly	296.27°
Eccentric anomaly	267.05249°
Mean motion	0.47689 °/min
BSTAR	Unknown
Orbital period	754.9 mins