ATLAS 5 CENTAUR DEB, 44674
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 44674 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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44674 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 44674U 18079AL 25241.31833456 -.00000156 00000-0 00000-0 0 9990
2 44674 12.6490 62.8714 4341534 283.4891 32.8845 1.93753386 43884
Epoch: 2025-08-29T07:38Z
TLE epoch observation values (Epoch: 2025-08-29T07:38:24.105Z)
Latitude
-0.00003°
Longitude
-29.41928°
Altitude
13,642.369 km
Speed
5.015 km/s
True Right ascension
04h 11m 47s
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
16:54:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
32,603.887 km
Perigee altitude
9,002.258 km
Semi-major axis
27,181.21 km
Eccentricity
0.43415
Inclination
12.649°
RAAN
62.8714°
Arg. of periapsis
283.4891°
True anomaly
76.469°
Mean anomaly
32.8845°
Eccentric anomaly
52.66204°
Mean motion
0.48433 °/min
Orbital period
743.3 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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83 mins | 2025-08-31 07:53:34.559Z | 203.576° SW | 2025-08-31 08:25:34.559Z | 159.913° S | 15.697° | 2025-08-31 09:16:34.559Z | 114.738° 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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