ATLAS 5 CENTAUR DEB, 43985
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43985 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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43985 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 month ago
0 ATLAS 5 CENTAUR DEB
1 43985U 14055AQ 25162.59841530 -.00000022 00000-0 00000+0 0 9999
2 43985 19.3460 208.0363 4682437 48.1931 343.4652 1.76755759 43721
Epoch: 2025-06-11T14:21Z
TLE epoch observation values (Epoch: 2025-06-11T14:21:43.081Z)
Latitude
0.00001°
Longitude
92.49336°
Altitude
10,778.116 km
Speed
5.716 km/s
True Right ascension
13h 52m 24s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
18.88831°
Longitude
-168.62562°
Altitude
10,738.243 km
Speed
5.726 km/s
Apparent Right ascension
21h 20m 06s
Apparent Declination
4° 22' 34"
Sunlit
Visualization observer readout
Local Sidereal Time
12:33:09
Azimuth
56.932° ENE
Elevation
-27.396°
Doppler factor
1
Orbital elements
Apogee altitude
36,049.184 km
Perigee altitude
8,987.838 km
Semi-major axis
28,896.648 km
Eccentricity
0.46824
Inclination
19.346°
RAAN
208.0363°
Arg. of periapsis
48.1931°
True anomaly
312.12642°
Mean anomaly
343.4652°
Eccentric anomaly
330.08582°
Mean motion
0.44185 °/min
Orbital period
814.76 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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344 mins | 2025-07-19 13:47:29.772Z | 266.057° W | 2025-07-19 15:18:29.772Z | 234.017° WSW | 23.287° | 2025-07-19 19:31:29.772Z | 229.407° WSW |
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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