ATLAS 5 CENTAUR DEB, 44849
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 44849 is space debris in HEO originally from a launch on Wed, 17 Sep 2014 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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44849 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 ATLAS 5 CENTAUR DEB
1 44849U 14055CH 26227.15501595 .00000068 00000-0 00000+0 0 9997
2 44849 21.3014 79.9835 5054087 279.2660 29.0803 1.95518927 50154Epoch: 2026-08-15T03:43Z
TLE epoch observation values (Epoch: 2026-08-15T03:43:13.378Z)
Latitude
0.00001°
Longitude
60.70067°
Altitude
12,239.321 km
Speed
5.298 km/s
True Right ascension
05h 20m 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
00:14:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,293.974 km
Perigee altitude
6,984.395 km
Semi-major axis
27,017.321 km
Eccentricity
0.50541
Inclination
21.3014°
RAAN
79.9835°
Arg. of periapsis
279.266°
True anomaly
80.60655°
Mean anomaly
29.0803°
Eccentric anomaly
51.85377°
Mean motion
0.48874 °/min
Orbital period
736.58 mins
BSTAR
0
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Other satellites on launch #55 in the year 2014 (2014-09-17 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ATLAS 5 CENTAUR DEB Visibility
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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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| ATLAS 5 CENTAUR DEB is likely not visible in the next few days. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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