ATLAS 5 CENTAUR DEB, 45474

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 45474 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
45474, 2018-079BW
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: 4 days ago

TLE from 4 days ago
0 ATLAS 5 CENTAUR DEB
1 45474U 18079BW  26153.44738031 -.00000095  00000-0  00000+0 0  9990
2 45474  13.0504  63.6981 4462367 252.5932  54.9704  1.74188786 42737
Epoch: 2026-06-02T10:44Z
TLE epoch observation values (Epoch: 2026-06-02T10:44:13.658Z)
Latitude
0.00006°
Longitude
11.62968°
Altitude
20,615.818 km
Speed
3.984 km/s
True Right ascension
04h 14m 25s
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
08:42:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,822.95 km
Perigee altitude
9,780.638 km
Semi-major axis
29,179.931 km
Eccentricity
0.44624
Inclination
13.0504°
RAAN
63.6981°
Arg. of periapsis
252.5932°
True anomaly
107.34358°
Mean anomaly
54.9704°
Eccentric anomaly
80.1619°
Mean motion
0.43543 °/min
Orbital period
826.77 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|