ATLAS 5 CENTAUR DEB, 43985

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 43985 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
43985, 2014-055AQ
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 43985U 14055AQ  26208.28268725 -.00000043  00000-0  00000-0 0  9990
2 43985  19.0394 170.2623 4717083 113.0487 302.5609  1.76689676 12736
Epoch: 2026-07-27T06:47Z
TLE epoch observation values (Epoch: 2026-07-27T06:47:04.178Z)
Latitude
0.00001°
Longitude
123.43065°
Altitude
21,197.883 km
Speed
3.888 km/s
True Right ascension
11h 20m 39s
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
21:23:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,159.935 km
Perigee altitude
8,891.54 km
Semi-major axis
28,903.874 km
Eccentricity
0.47171
Inclination
19.0394°
RAAN
170.2623°
Arg. of periapsis
113.0487°
True anomaly
246.97101°
Mean anomaly
302.5609°
Eccentric anomaly
275.66605°
Mean motion
0.44168 °/min
Orbital period
815.07 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|