ATLAS 5 CENTAUR DEB, 44673
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 44673 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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44673 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ATLAS 5 CENTAUR DEB
1 44673U 18079AK 25241.23821735 -.00000145 00000-0 00000-0 0 9995
2 44673 13.0314 67.1113 4709565 248.7319 55.8036 1.77547028 44687
Epoch: 2025-08-29T05:43Z
TLE epoch observation values (Epoch: 2025-08-29T05:43:01.979Z)
Latitude
0°
Longitude
3.74769°
Altitude
20,643.96 km
Speed
3.958 km/s
True Right ascension
04h 28m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:54:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,001.511 km
Perigee altitude
8,864.107 km
Semi-major axis
28,810.946 km
Eccentricity
0.47096
Inclination
13.0314°
RAAN
67.1113°
Arg. of periapsis
248.7319°
True anomaly
111.32445°
Mean anomaly
55.8036°
Eccentric anomaly
82.56026°
Mean motion
0.44382 °/min
Orbital period
811.14 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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729 mins | 2025-08-31 10:16:33.549Z | 211.59° SW | 2025-08-31 18:30:33.549Z | 165.505° S | 40.139° | 2025-08-31 22:25:33.549Z | 124.129° SE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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