ATLAS 5 CENTAUR DEB, 43980

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43980 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
43980, 2014-055AK
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: 21 hours ago

TLE from 21 hours ago
0 ATLAS 5 CENTAUR DEB
1 43980U 14055AK  26250.92838626 -.00000100  00000-0  00000-0 0  9990
2 43980  20.0868 139.4454 4740968 168.4898 208.0289  1.83783896 53709
Epoch: 2026-09-07T22:16Z
TLE epoch observation values (Epoch: 2026-09-07T22:16:52.572Z)
Latitude
0.00004°
Longitude
178.23137°
Altitude
34,402.089 km
Speed
2.322 km/s
True Right ascension
09h 17m 48s
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
11:43:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,125.444 km
Perigee altitude
8,428.805 km
Semi-major axis
28,155.262 km
Eccentricity
0.4741
Inclination
20.0868°
RAAN
139.4454°
Arg. of periapsis
168.4898°
True anomaly
191.49365°
Mean anomaly
208.0289°
Eccentric anomaly
199.12793°
Mean motion
0.45941 °/min
Orbital period
783.61 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|