ATLAS 5 CENTAUR DEB, 44002

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 44002 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
44002, 2014-055BH
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: 1 day ago

TLE from 1 day ago
0 ATLAS 5 CENTAUR DEB
1 44002U 14055BH  26144.14955628 -.00000007  00000-0  00000-0 0  9990
2 44002  19.8760 150.9935 4789370 150.4922 248.2914  1.83902630 51936
Epoch: 2026-05-24T03:35Z
TLE epoch observation values (Epoch: 2026-05-24T03:35:21.662Z)
Latitude
0.00001°
Longitude
-144.56583°
Altitude
30,771.025 km
Speed
2.701 km/s
True Right ascension
10h 04m 07s
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
18:35:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,243.836 km
Perigee altitude
8,286.227 km
Semi-major axis
28,143.169 km
Eccentricity
0.47894
Inclination
19.876°
RAAN
150.9935°
Arg. of periapsis
150.4922°
True anomaly
209.55566°
Mean anomaly
248.2914°
Eccentric anomaly
227.92331°
Mean motion
0.45971 °/min
Orbital period
783.1 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|