ATLAS 5 CENTAUR DEB, 43983
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43983 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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43983 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ATLAS 5 CENTAUR DEB
1 43983U 14055AN 25240.61237267 -.00000105 00000-0 00000-0 0 9996
2 43983 20.2998 145.8634 4931678 160.0830 229.1125 1.90080488 48435
Epoch: 2025-08-28T14:41Z
TLE epoch observation values (Epoch: 2025-08-28T14:41:48.998Z)
Latitude
0.00005°
Longitude
-51.67622°
Altitude
32,488.008 km
Speed
2.456 km/s
True Right ascension
09h 43m 24s
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
15:43:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,728.989 km
Perigee altitude
7,575.027 km
Semi-major axis
27,530.145 km
Eccentricity
0.49317
Inclination
20.2998°
RAAN
145.8634°
Arg. of periapsis
160.083°
True anomaly
199.89823°
Mean anomaly
229.1125°
Eccentric anomaly
213.51185°
Mean motion
0.47515 °/min
Orbital period
757.66 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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669 mins | 2025-08-31 11:30:59.096Z | 202.213° SSW | 2025-08-31 21:29:59.096Z | 166.403° S | 40.533° | 2025-08-31 22:39:59.096Z | 98.009° 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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