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.

Loading next visibility...
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 (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: 3 weeks ago

TLE from 3 weeks ago
0 ATLAS 5 CENTAUR DEB
1 43972U 14055AB  25289.08412600 -.00000006  00000-0  00000-0 0  9994
2 43972  19.6683 167.3812 4838242 122.2382 293.8090  1.85388555 48190
Epoch: 2025-10-16T02:01Z
TLE epoch observation values (Epoch: 2025-10-16T02:01:08.486Z)
Latitude
-0°
Longitude
112.29052°
Altitude
22,520.304 km
Speed
3.653 km/s
True Right ascension
11h 09m 41s
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
18:19:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,158.007 km
Perigee altitude
8,070.982 km
Semi-major axis
27,992.632 km
Eccentricity
0.48382
Inclination
19.6683°
RAAN
167.3812°
Arg. of periapsis
122.2382°
True anomaly
237.74913°
Mean anomaly
293.809°
Eccentric anomaly
266.15046°
Mean motion
0.46342 °/min
Orbital period
776.83 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|