ATLAS 5 CENTAUR DEB, 43972

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43972 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.

Not visible in the next 10 days
Identifier
43972, 2014-055AB
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)
2014-09-17 (12 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <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 43972U 14055AB  26171.01435216 -.00000048  00000-0  00000+0 0  9991
2 43972  20.0979 143.3701 4763258 164.4938 217.6743  1.85389515 52779
Epoch: 2026-06-20T00:20Z
TLE epoch observation values (Epoch: 2026-06-20T00:20:40.026Z)
Latitude
0.00001°
Longitude
-130.05856°
Altitude
33,611.057 km
Speed
2.387 km/s
True Right ascension
09h 33m 22s
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
21:37:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,947.9 km
Perigee altitude
8,280.808 km
Semi-major axis
27,992.491 km
Eccentricity
0.47633
Inclination
20.0979°
RAAN
143.3701°
Arg. of periapsis
164.4938°
True anomaly
195.53345°
Mean anomaly
217.6743°
Eccentric anomaly
205.79735°
Mean motion
0.46343 °/min
Orbital period
776.82 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

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