ATLAS 5 CENTAUR DEB, 43984

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43984 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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Identifier
43984, 2014-055AP
Orbit
HEO
Country
Flag of USUS
Related business
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Icon of a cake. It is the launch day of the satellite!2014-09-17 (11 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
Last TLE update: 2 days ago

TLE from 2 days ago
0 ATLAS 5 CENTAUR DEB
1 43984U 14055AP  25258.19312005 -.00000089  00000-0  00000-0 0  9994
2 43984  20.7836 122.3691 5089834 201.0878 126.6945  1.91685905 49159
Epoch: 2025-09-15T04:38Z
TLE epoch observation values (Epoch: 2025-09-15T04:38:05.572Z)
Latitude
0.00003°
Longitude
58.4941°
Altitude
32,245.822 km
Speed
2.466 km/s
True Right ascension
08h 09m 40s
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
17:28:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,932.217 km
Perigee altitude
7,064.071 km
Semi-major axis
27,376.281 km
Eccentricity
0.50898
Inclination
20.7836°
RAAN
122.3691°
Arg. of periapsis
201.0878°
True anomaly
158.92837°
Mean anomaly
126.6945°
Eccentric anomaly
143.8837°
Mean motion
0.47916 °/min
Orbital period
751.31 mins
BSTAR
0
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