ATLAS 5 CENTAUR DEB, 44677

Orbit data source: Space-Track

ATLAS 5 CENTAUR DEB, 44677 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
44677, 2018-079AP
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: 2 days ago

TLE from 2 days ago
0 ATLAS 5 CENTAUR DEB
1 44677U 18079AP  26234.47680976 -.00000166  00000-0  00000-0 0  9991
2 44677  13.1283  51.3405 4412548 280.7768  33.8885  1.78496467 46964
Epoch: 2026-08-22T11:26Z
TLE epoch observation values (Epoch: 2026-08-22T11:26:36.363Z)
Latitude
-0.00005°
Longitude
-91.01908°
Altitude
14,967.385 km
Speed
4.844 km/s
True Right ascension
03h 25m 40s
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
14:58:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,998.268 km
Perigee altitude
9,662.655 km
Semi-major axis
28,708.598 km
Eccentricity
0.44125
Inclination
13.1283°
RAAN
51.3405°
Arg. of periapsis
280.7768°
True anomaly
79.14658°
Mean anomaly
33.8885°
Eccentric anomaly
54.461°
Mean motion
0.4462 °/min
Orbital period
806.82 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|