ATLAS 5 CENTAUR DEB, 44038

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 44038 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
44038, 2014-055BY
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: 6 days ago

TLE from 6 days ago
0 ATLAS 5 CENTAUR DEB
1 44038U 14055BY  26293.48059114  .00000011  00000-0  00000-0 0  9990
2 44038  19.0228 178.8828 4639790 102.6778 311.3679  1.76615370 51488
Epoch: 2026-10-20T11:32Z
TLE epoch observation values (Epoch: 2026-10-20T11:32:03.074Z)
Latitude
0°
Longitude
-23.02018°
Altitude
18,879.198 km
Speed
4.216 km/s
True Right ascension
11h 55m 44s
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
14:56:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,948.357 km
Perigee altitude
9,119.278 km
Semi-major axis
28,911.955 km
Eccentricity
0.46398
Inclination
19.0228°
RAAN
178.8828°
Arg. of periapsis
102.6778°
True anomaly
257.3115°
Mean anomaly
311.3679°
Eccentric anomaly
285.78656°
Mean motion
0.4415 °/min
Orbital period
815.41 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

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