ATLAS 5 CENTAUR DEB, 43981

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43981 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
43981, 2014-055AL
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
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 ATLAS 5 CENTAUR DEB
1 43981U 14055AL  26007.29909847 -.00000064  00000-0  00000-0 0  9994
2 43981  19.6477 154.0225 5177312 140.2459 272.3437  1.78794641 47906
Epoch: 2026-01-07T07:10Z
TLE epoch observation values (Epoch: 2026-01-07T07:10:42.107Z)
Latitude
0.00002°
Longitude
-60.58316°
Altitude
28,487.677 km
Speed
2.994 km/s
True Right ascension
10h 15m 50s
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
17:32:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,145.464 km
Perigee altitude
7,451.766 km
Semi-major axis
28,676.752 km
Eccentricity
0.51773
Inclination
19.6477°
RAAN
154.0225°
Arg. of periapsis
140.2459°
True anomaly
219.77315°
Mean anomaly
272.3437°
Eccentric anomaly
245.37721°
Mean motion
0.44694 °/min
Orbital period
805.48 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

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