ATLAS 5 CENTAUR DEB, 43980

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43980 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.

Loading next visibility...
Identifier
43980, 2014-055AK
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 (11 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: 23 hours ago

TLE from 23 hours ago
0 ATLAS 5 CENTAUR DEB
1 43980U 14055AK  25318.43034203  .00000000  00000-0  00000+0 0  9996
2 43980  19.5757 167.7086 4838933 118.9790 297.7482  1.83785296 48233
Epoch: 2025-11-14T10:19Z
TLE epoch observation values (Epoch: 2025-11-14T10:19:41.551Z)
Latitude
-0.00001°
Longitude
-40.90145°
Altitude
21,747.836 km
Speed
3.766 km/s
True Right ascension
11h 11m 10s
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
06:22:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,401.136 km
Perigee altitude
8,152.937 km
Semi-major axis
28,155.174 km
Eccentricity
0.48389
Inclination
19.5757°
RAAN
167.7086°
Arg. of periapsis
118.979°
True anomaly
241.08028°
Mean anomaly
297.7482°
Eccentric anomaly
270.02316°
Mean motion
0.45942 °/min
Orbital period
783.6 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|