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
1 day 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 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
Object was in daylight at epoch
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
Object is in daylight
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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