ATLAS 5 CENTAUR DEB, 46857

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 46857 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.

Not visible in the next 10 days
Identifier
46857, 2018-079DN
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
RCS unknown

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago
0 ATLAS 5 CENTAUR DEB
1 46857U 18079DN  26119.03922988 -.00000069  00000-0  00000-0 0  9991
2 46857  12.5351  77.8265 4632584 229.2685  80.2538  1.69096314 33898
Epoch: 2026-04-29T00:56Z
TLE epoch observation values (Epoch: 2026-04-29T00:56:29.461Z)
Latitude
-0.00001°
Longitude
-153.38413°
Altitude
27,108.618 km
Speed
3.227 km/s
True Right ascension
05h 10m 58s
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
17:56:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,172.637 km
Perigee altitude
9,596.835 km
Semi-major axis
29,762.873 km
Eccentricity
0.46326
Inclination
12.5351°
RAAN
77.8265°
Arg. of periapsis
229.2685°
True anomaly
130.77532°
Mean anomaly
80.2538°
Eccentric anomaly
105.79442°
Mean motion
0.4227 °/min
Orbital period
851.67 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

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