ATLAS 5 CENTAUR R/B, 41623
Orbit data source: Space-Track
ATLAS 5 CENTAUR R/B, 41623 is space debris in HEO originally from a launch on Fri, 24 Jun 2016 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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41623 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 ATLAS 5 CENTAUR R/B
1 41623U 16041B 25199.34233368 -.00000080 00000-0 00000-0 0 9995
2 41623 18.9886 69.3891 6098052 217.8305 77.5362 2.09534951 69407
Epoch: 2025-07-18T08:12Z
TLE epoch observation values (Epoch: 2025-07-18T08:12:57.629Z)
Latitude
0.00001°
Longitude
9.80496°
Altitude
24,883.402 km
Speed
3.17 km/s
True Right ascension
04h 37m 45s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
8.60825°
Longitude
35.65195°
Altitude
34,042.756 km
Speed
2.067 km/s
Apparent Right ascension
06h 42m 56s
Apparent Declination
2° 38' 03"
Sunlit
Visualization observer readout
Local Sidereal Time
22:05:55
Azimuth
60.321° ENE
Elevation
-27.085°
Doppler factor
1
Orbital elements
Apogee altitude
35,154.198 km
Perigee altitude
3,688.734 km
Semi-major axis
25,799.603 km
Eccentricity
0.60981
Inclination
18.9886°
RAAN
69.3891°
Arg. of periapsis
217.8305°
True anomaly
142.15802°
Mean anomaly
77.5362°
Eccentric anomaly
110.30442°
Mean motion
0.52375 °/min
Orbital period
687.35 mins
BSTAR
0
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Other satellites on launch #41 in the year 2016 (2016-06-24 UTC)
ATLAS 5 CENTAUR R/B 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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586 mins | 2025-07-19 17:35:41.684Z | 234.759° WSW | 2025-07-20 02:57:41.684Z | 225.694° WSW | 27.619° | 2025-07-20 03:21:41.684Z | 163.107° S |
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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