ATLAS 5 CENTAUR DEB, 43974
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 43974 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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43974 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 ATLAS 5 CENTAUR DEB
1 43974U 14055AD 24275.23317249 -.00000023 00000-0 00000-0 0 9999
2 43974 19.6556 194.9279 5015527 70.9832 335.4443 1.84493390 41008
Epoch: 2024-10-01T05:35Z
TLE epoch observation values (Epoch: 2024-10-01T05:35:46.103Z)
Latitude
0.00006°
Longitude
100.53264°
Altitude
11,708.713 km
Speed
5.466 km/s
True Right ascension
12h 59m 41s
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
15:44:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,790.211 km
Perigee altitude
7,619.839 km
Semi-major axis
28,083.162 km
Eccentricity
0.50155
Inclination
19.6556°
RAAN
194.9279°
Arg. of periapsis
70.9832°
True anomaly
288.83185°
Mean anomaly
335.4443°
Eccentric anomaly
315.19275°
Mean motion
0.46118 °/min
Orbital period
780.6 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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94 mins | 2025-08-31 02:45:37.948Z | 265.522° W | 2025-08-31 03:38:37.948Z | 195.567° SSW | 36.676° | 2025-08-31 04:19:37.948Z | 125.246° SE |
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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