ATLAS 5 CENTAUR DEB, 43980
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43980 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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43980 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 43980U 14055AK 25241.72990802 -.00000032 00000-0 00000-0 0 9996
2 43980 19.5021 175.3282 4848780 106.0165 310.8775 1.83780530 46826
Epoch: 2025-08-29T17:31Z
TLE epoch observation values (Epoch: 2025-08-29T17:31:04.052Z)
Latitude
0.00004°
Longitude
-65.68168°
Altitude
18,518.206 km
Speed
4.226 km/s
True Right ascension
11h 41m 02s
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
15:44:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,429.593 km
Perigee altitude
8,125.466 km
Semi-major axis
28,155.667 km
Eccentricity
0.48488
Inclination
19.5021°
RAAN
175.3282°
Arg. of periapsis
106.0165°
True anomaly
253.93521°
Mean anomaly
310.8775°
Eccentric anomaly
283.91084°
Mean motion
0.4594 °/min
Orbital period
783.62 mins
BSTAR
0
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Other satellites on launch #55 in the year 2014 (2014-09-17 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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723 mins | 2025-08-31 11:31:23.133Z | 240.489° WSW | 2025-08-31 22:51:23.133Z | 166.22° S | 37.765° | 2025-08-31 23:34:23.133Z | 96.524° ESE |
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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