ATLAS 5 CENTAUR DEB, 44679
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 44679 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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44679 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ATLAS 5 CENTAUR DEB
1 44679U 18079AR 25242.17644917 -.00000147 00000-0 00000-0 0 9992
2 44679 13.1111 63.0888 4689726 256.7501 48.5737 1.79402031 41456
Epoch: 2025-08-30T04:14Z
TLE epoch observation values (Epoch: 2025-08-30T04:14:05.208Z)
Latitude
-0.00006°
Longitude
21.03138°
Altitude
18,610.569 km
Speed
4.239 km/s
True Right ascension
04h 12m 40s
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
20:44:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,652.135 km
Perigee altitude
8,815.629 km
Semi-major axis
28,612.019 km
Eccentricity
0.46897
Inclination
13.1111°
RAAN
63.0888°
Arg. of periapsis
256.7501°
True anomaly
103.29616°
Mean anomaly
48.5737°
Eccentric anomaly
74.4618°
Mean motion
0.44846 °/min
Orbital period
802.75 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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13 mins | 2025-08-31 05:06:37.746Z | 177.971° S | 2025-08-31 05:06:37.746Z | 177.971° S | 13.34° | 2025-08-31 05:19:37.746Z | 159.648° S |
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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