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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Identifier
41623, 2016-041B
Orbit
HEO
Last TLE update
18 hours ago
Origin
Manufacturer
LMSS Denver
Mission
Spacecraft
Bus & Motor
CENTAUR SEC, RL10C-1
Mass
~2,020 kg wet, 2,020 kg dry
Launch date (UTC)
2016-06-24 (9 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 5.8 m
Radar Cross Section
32.260 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 18 hours ago
0 ATLAS 5 CENTAUR R/B
1 41623U 16041B   25211.26446141 -.00000145  00000-0  00000-0 0  9998
2 41623  19.0164  67.2635 6096098 221.7776  70.6658  2.09536029 69652
Epoch: 2025-07-30T06:20Z
TLE epoch observation values (Epoch: 2025-07-30T06:20:49.465Z)
Latitude
Longitude
23.97729°
Altitude
23,334.688 km
Speed
3.373 km/s
True Right ascension
04h 29m 19s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
18.48796°
Longitude
99.28568°
Altitude
26,315.302 km
Speed
2.989 km/s
Apparent Right ascension
08h 55m 29s
Apparent Declination
12° 04' 59"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
13:54:14
Azimuth
269.688° W
Elevation
19.413°
Doppler factor
1
Orbital elements
Apogee altitude
35,149.009 km
Perigee altitude
3,693.739 km
Semi-major axis
25,799.511 km
Eccentricity
0.60961
Inclination
19.0164°
RAAN
67.2635°
Arg. of periapsis
221.7776°
True anomaly
138.24323°
Mean anomaly
70.6658°
Eccentric anomaly
104.4838°
Mean motion
0.52375 °/min
Orbital period
687.35 mins
BSTAR
0
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