ATLAS 5 CENTAUR DEB, 46862

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 46862 is space debris in HEO originally from a launch on Wed, 17 Oct 2018 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	46862, 2018-079DT
Orbit	HEO
Last TLE update	5 months ago
Origin	ULA (US)
Manufacturer	ULA Decatur
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2018-10-17 (6 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	RCS unknown

Expand to show TLE details & history

TLE from 5 months ago

0 ATLAS 5 CENTAUR DEB
1 46862U 18079DT  24195.47924339 -.00000053  00000-0  00000-0 0  9992
2 46862  11.0677 129.2711 5109835 107.6729 312.4559  1.50438403 20320

Epoch: 2024-07-13T11:30Z

Definitive object data (Epoch: 2024-07-13T11:30:06.628Z)

Latitude	0.00001°
Longitude	24.73037°
Altitude	21,843.887 km
Speed	3.982 km/s
True Right ascension	08h 36m 23s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-10.99216°
Longitude	-63.59566°
Altitude	37,553.315 km
Speed	2.4 km/s
Apparent Right ascension	03h 07m 38s
Apparent Declination	-16° 47' 24"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	22:26:26
Azimuth	115.434° SE
Elevation	3.564°
Doppler factor	1

Orbital elements

Apogee altitude	42,238.342 km
Perigee altitude	9,356.158 km
Semi-major axis	32,175.387 km
Eccentricity	0.5109835
Inclination	11.0677°
RAAN	129.2711°
Arg. of periapsis	107.6729°
True anomaly	252.17478°
Mean anomaly	312.4559°
Eccentric anomaly	284.0552°
Mean motion	0.37606 °/min
BSTAR	Unknown
Orbital period	957.29 mins