ATLAS 5 CENTAUR DEB, 43972
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43972 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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43972 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 4 days ago
0 ATLAS 5 CENTAUR DEB
1 43972U 14055AB 25195.79371037 -.00000002 00000-0 00000-0 0 9992
2 43972 19.5790 176.7389 4860268 106.3899 310.7752 1.85389754 46464
Epoch: 2025-07-14T19:02Z
TLE epoch observation values (Epoch: 2025-07-14T19:02:56.575Z)
Latitude
-0.00002°
Longitude
-41.96302°
Altitude
18,397.841 km
Speed
4.235 km/s
True Right ascension
11h 46m 40s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-15.88982°
Longitude
-95.48426°
Altitude
33,375.44 km
Speed
2.411 km/s
Apparent Right ascension
07h 45m 16s
Apparent Declination
-22° 27' 41"
Sunlit
Visualization observer readout
Local Sidereal Time
12:18:06
Azimuth
239.121° WSW
Elevation
1.029°
Doppler factor
1
Orbital elements
Apogee altitude
35,219.502 km
Perigee altitude
8,009.269 km
Semi-major axis
27,992.523 km
Eccentricity
0.48603
Inclination
19.579°
RAAN
176.7389°
Arg. of periapsis
106.3899°
True anomaly
253.66659°
Mean anomaly
310.7752°
Eccentric anomaly
283.72282°
Mean motion
0.46343 °/min
Orbital period
776.82 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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138 mins | 2025-07-19 02:27:29.303Z | 245.854° WSW | 2025-07-19 04:03:29.303Z | 178.631° S | 39.388° | 2025-07-19 04:45:29.303Z | 103.842° 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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