ATLAS 5 CENTAUR DEB, 44676
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 44676 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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44676 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 ATLAS 5 CENTAUR DEB
1 44676U 18079AN 25112.78985214 -.00000040 00000-0 00000+0 0 9991
2 44676 12.9959 62.1312 4836573 260.0852 44.1776 1.82796239 39196
Epoch: 2025-04-22T18:57Z
TLE epoch observation values (Epoch: 2025-04-22T18:57:23.224Z)
Latitude
-0.00002°
Longitude
-73.35296°
Altitude
17,223.116 km
Speed
4.435 km/s
True Right ascension
04h 08m 18s
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
16:54:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,545.333 km
Perigee altitude
8,212.077 km
Semi-major axis
28,256.842 km
Eccentricity
0.48366
Inclination
12.9959°
RAAN
62.1312°
Arg. of periapsis
260.0852°
True anomaly
100.04416°
Mean anomaly
44.1776°
Eccentric anomaly
70.26078°
Mean motion
0.45694 °/min
Orbital period
787.85 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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705 mins | 2025-08-31 11:50:23.864Z | 221.196° SW | 2025-08-31 18:28:23.864Z | 162.291° S | 39.862° | 2025-08-31 23:35:23.864Z | 134.746° 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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Authenticating...
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