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
Identifier
Orbit
Country
USRelated business
Manufacturer
LMSS Denver
Mission
Spacecraft
Bus & Motor
CENTAUR SEC, RL10C-1
Mass
~2,020 kg wet, 2,020 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 5.8 m
Radar Cross Section
32.260 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 ATLAS 5 CENTAUR R/B
1 41623U 16041B 25258.48405477 -.00000276 00000-0 00000-0 0 9995
2 41623 19.1041 58.9008 6089450 237.3044 49.5552 2.09538398 70643Epoch: 2025-09-15T11:37Z
TLE epoch observation values (Epoch: 2025-09-15T11:37:02.332Z)
Latitude
-0.00006°
Longitude
-110.04218°
Altitude
17,794.653 km
Speed
4.187 km/s
True Right ascension
03h 55m 37s
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
08:22:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,131.528 km
Perigee altitude
3,710.811 km
Semi-major axis
25,799.307 km
Eccentricity
0.60895
Inclination
19.1041°
RAAN
58.9008°
Arg. of periapsis
237.3044°
True anomaly
122.82476°
Mean anomaly
49.5552°
Eccentric anomaly
84.2709°
Mean motion
0.52376 °/min
Orbital period
687.34 mins
BSTAR
0
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Other satellites on launch #41 in the year 2016 (2016-06-24 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ATLAS 5 CENTAUR R/B Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 115 mins | 2025-09-18 15:31:31.269Z | 125.964° SE | 2025-09-18 15:31:31.269Z | 125.964° SE | 38.609° | 2025-09-18 17:26:31.269Z | 106.577° ESE |
| 488 mins | 2025-09-19 07:23:31.269Z | 109.892° ESE | 2025-09-19 13:55:31.269Z | 108.333° ESE | 33.422° | 2025-09-19 15:31:31.269Z | 104.362° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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