ATLAS 5 CENTAUR DEB, 46668
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 46668 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.
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46668 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 ATLAS 5 CENTAUR DEB
1 46668U 18079CW 25200.07282429 -.00000150 00000-0 00000-0 0 9995
2 46668 12.8866 62.3614 4642820 264.5123 42.6840 1.83684648 32056
Epoch: 2025-07-19T01:44Z
TLE epoch observation values (Epoch: 2025-07-19T01:44:52.018Z)
Latitude
0.00002°
Longitude
99.05947°
Altitude
16,759.532 km
Speed
4.506 km/s
True Right ascension
04h 09m 33s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
12.85091°
Longitude
-165.50922°
Altitude
34,243.668 km
Speed
2.339 km/s
Apparent Right ascension
10h 32m 22s
Apparent Declination
6° 21' 12"
Sunlit
Visualization observer readout
Local Sidereal Time
22:41:11
Azimuth
3.028° NNE
Elevation
-43.686°
Doppler factor
1
Orbital elements
Apogee altitude
34,864.242 km
Perigee altitude
8,710.681 km
Semi-major axis
28,165.599 km
Eccentricity
0.46428
Inclination
12.8866°
RAAN
62.3614°
Arg. of periapsis
264.5123°
True anomaly
95.38023°
Mean anomaly
42.684°
Eccentric anomaly
67.20835°
Mean motion
0.45916 °/min
Orbital period
784.04 mins
BSTAR
0
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Other satellites on launch #79 in the year 2018 (2018-10-17 UTC)
ATLAS 5 CENTAUR DEB Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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697 mins | 2025-07-20 16:19:56.181Z | 231.004° WSW | 2025-07-20 20:52:56.181Z | 205.27° SW | 39.359° | 2025-07-21 03:56:56.181Z | 141.358° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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