ATLAS 5 CENTAUR DEB, 43982

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43982 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
43982, 2014-055AM
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: 3 days ago

TLE from 3 days ago
0 ATLAS 5 CENTAUR DEB
1 43982U 14055AM  26170.44272089 -.00000040  00000-0  00000-0 0  9998
2 43982  19.0548 191.8742 4710460  81.7734 327.2819  1.75458819 49855
Epoch: 2026-06-19T10:37Z
TLE epoch observation values (Epoch: 2026-06-19T10:37:31.084Z)
Latitude
-0.00001°
Longitude
124.84682°
Altitude
14,755.603 km
Speed
4.898 km/s
True Right ascension
12h 47m 35s
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
23:19:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,339.379 km
Perigee altitude
8,982.09 km
Semi-major axis
29,038.872 km
Eccentricity
0.47105
Inclination
19.0548°
RAAN
191.8742°
Arg. of periapsis
81.7734°
True anomaly
278.3646°
Mean anomaly
327.2819°
Eccentric anomaly
305.23847°
Mean motion
0.4386 °/min
Orbital period
820.78 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|