ATLAS 5 CENTAUR DEB, 46637

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 46637 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
46637, 2014-055CM
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: 3 days ago

TLE from 3 days ago
0 ATLAS 5 CENTAUR DEB
1 46637U 14055CM  26251.18169734  .00000016  00000-0  00000-0 0  9993
2 46637  21.3078  76.9888 5097340 284.7404  25.8594  1.94669019 42095
Epoch: 2026-09-08T04:21Z
TLE epoch observation values (Epoch: 2026-09-08T04:21:38.650Z)
Latitude
-0.00013°
Longitude
24.41092°
Altitude
11,369.927 km
Speed
5.496 km/s
True Right ascension
05h 08m 17s
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
00:11:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,529.475 km
Perigee altitude
6,906.065 km
Semi-major axis
27,095.907 km
Eccentricity
0.50973
Inclination
21.3078°
RAAN
76.9888°
Arg. of periapsis
284.7404°
True anomaly
75.13005°
Mean anomaly
25.8594°
Eccentric anomaly
47.33519°
Mean motion
0.48662 °/min
Orbital period
739.8 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|