ATLAS 5 CENTAUR DEB, 43984
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43984 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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43984 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ATLAS 5 CENTAUR DEB
1 43984U 14055AP 26111.67436986 -.00000148 00000-0 00000-0 0 9997
2 43984 21.0600 99.0376 5114555 243.5667 55.9280 1.91692795 53345Epoch: 2026-04-21T16:11Z
TLE epoch observation values (Epoch: 2026-04-21T16:11:05.555Z)
Latitude
-0.00004°
Longitude
6.46517°
Altitude
19,764.218 km
Speed
3.992 km/s
True Right ascension
06h 35m 56s
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
01:30:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,998.9 km
Perigee altitude
6,996.073 km
Semi-major axis
27,375.623 km
Eccentricity
0.51146
Inclination
21.06°
RAAN
99.0376°
Arg. of periapsis
243.5667°
True anomaly
116.47903°
Mean anomaly
55.928°
Eccentric anomaly
85.12629°
Mean motion
0.47918 °/min
Orbital period
751.29 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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