ATLAS 5 CENTAUR DEB, 44649

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 44649 is space debris in HEO originally from a launch on Wed, 17 Oct 2018 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
44649, 2018-079K
Orbit
HEO
Country
Flag of USUS
Related business
Flag of USUnited Launch Alliance/Lockheed Martin (US)
Manufacturer
ULA Decatur
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2018-10-17 (8 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: 16 hours ago

TLE from 16 hours ago
0 ATLAS 5 CENTAUR DEB
1 44649U 18079K   26235.36467105 -.00000179  00000-0  00000-0 0  9990
2 44649  13.3836  21.6333 4717978 344.9699   4.6686  1.83973262 49642
Epoch: 2026-08-23T08:45Z
TLE epoch observation values (Epoch: 2026-08-23T08:45:07.578Z)
Latitude
-0.00002°
Longitude
-81.282°
Altitude
8,647.179 km
Speed
6.236 km/s
True Right ascension
01h 26m 38s
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
16:20:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,032.592 km
Perigee altitude
8,483.441 km
Semi-major axis
28,136.153 km
Eccentricity
0.4718
Inclination
13.3836°
RAAN
21.6333°
Arg. of periapsis
344.9699°
True anomaly
14.65103°
Mean anomaly
4.6686°
Eccentric anomaly
8.80771°
Mean motion
0.45988 °/min
Orbital period
782.81 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|