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.

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Identifier
43972, 2014-055AB
Orbit
HEO
Last TLE update
4 days ago
Origin
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
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 4 days ago
0 ATLAS 5 CENTAUR DEB
1 43972U 14055AB  25195.79371037 -.00000002  00000-0  00000-0 0  9992
2 43972  19.5790 176.7389 4860268 106.3899 310.7752  1.85389754 46464
Epoch: 2025-07-14T19:02Z
TLE epoch observation values (Epoch: 2025-07-14T19:02:56.575Z)
Latitude
-0.00002°
Longitude
-41.96302°
Altitude
18,397.841 km
Speed
4.235 km/s
True Right ascension
11h 46m 40s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-15.88982°
Longitude
-95.48426°
Altitude
33,375.44 km
Speed
2.411 km/s
Apparent Right ascension
07h 45m 16s
Apparent Declination
-22° 27' 41"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:18:06
Azimuth
239.121° WSW
Elevation
1.029°
Doppler factor
1
Orbital elements
Apogee altitude
35,219.502 km
Perigee altitude
8,009.269 km
Semi-major axis
27,992.523 km
Eccentricity
0.48603
Inclination
19.579°
RAAN
176.7389°
Arg. of periapsis
106.3899°
True anomaly
253.66659°
Mean anomaly
310.7752°
Eccentric anomaly
283.72282°
Mean motion
0.46343 °/min
Orbital period
776.82 mins
BSTAR
0
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