ATLAS 5 CENTAUR DEB, 43976

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43976 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
43976, 2014-055AF
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 week ago

TLE from 1 week ago
0 ATLAS 5 CENTAUR DEB
1 43976U 14055AF  26153.15039377 -.00000048  00000-0  00000-0 0  9999
2 43976  19.8552 150.4826 4769551 149.2181 250.5977  1.83492582 51924
Epoch: 2026-06-02T03:36Z
TLE epoch observation values (Epoch: 2026-06-02T03:36:34.021Z)
Latitude
0.00001°
Longitude
-154.26579°
Altitude
30,467.923 km
Speed
2.737 km/s
True Right ascension
10h 02m 00s
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
13:08:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,249.944 km
Perigee altitude
8,363.919 km
Semi-major axis
28,185.069 km
Eccentricity
0.47696
Inclination
19.8552°
RAAN
150.4826°
Arg. of periapsis
149.2181°
True anomaly
210.84538°
Mean anomaly
250.5977°
Eccentric anomaly
229.7427°
Mean motion
0.45868 °/min
Orbital period
784.85 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|