ATLAS 5 CENTAUR DEB, 43955

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43955 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
43955, 2014-055J
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: 4 days ago

TLE from 4 days ago
0 ATLAS 5 CENTAUR DEB
1 43955U 14055J   26205.58662498 -.00000160  00000-0  00000-0 0  9992
2 43955  21.0886  96.5800 4907575 247.5501  54.4129  1.93302654 55695
Epoch: 2026-07-24T14:04Z
TLE epoch observation values (Epoch: 2026-07-24T14:04:44.398Z)
Latitude
0.00005°
Longitude
-56.89245°
Altitude
19,090.474 km
Speed
4.082 km/s
True Right ascension
06h 26m 24s
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
20:35:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,205.286 km
Perigee altitude
7,485.153 km
Semi-major axis
27,223.357 km
Eccentricity
0.49076
Inclination
21.0886°
RAAN
96.58°
Arg. of periapsis
247.5501°
True anomaly
112.42803°
Mean anomaly
54.4129°
Eccentric anomaly
82.27612°
Mean motion
0.4832 °/min
Orbital period
745.03 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|