ATLAS 5 CENTAUR R/B, 51282

Orbit data source: Space-Track

ATLAS 5 CENTAUR R/B, 51282 is space debris in GEO originally from a launch on Fri, 21 Jan 2022 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
51282, 2022-006C
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
LMSS Denver
Mission
Spacecraft
Bus & Motor
CENTAUR SEC, RL10C-1
Mass
~2,020 kg wet, 2,020 kg dry
Launch date (UTC)
2022-01-21 (4 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

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ATLAS 5 CENTAUR R/B
1 51282U 22006C   26152.63319002 -.00000163  00000-0  00000-0 0  9999
2 51282   4.5544  76.1332 0264271  13.4562 346.8989  0.95003202 11041
Epoch: 2026-06-01T15:11Z
TLE epoch observation values (Epoch: 2026-06-01T15:11:47.617Z)
Latitude
-0°
Longitude
-42.27899°
Altitude
36,201.422 km
Speed
3.099 km/s
True Right ascension
05h 03m 08s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
03:32:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,487.584 km
Perigee altitude
36,177.296 km
Semi-major axis
43,710.577 km
Eccentricity
0.02643
Inclination
4.5544°
RAAN
76.1332°
Arg. of periapsis
13.4562°
True anomaly
346.1897°
Mean anomaly
346.8989°
Eccentric anomaly
346.54662°
Mean motion
0.2375 °/min
Orbital period
1,515.79 mins
BSTAR
0
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Other satellites on launch #6 in the year 2022 (2022-01-21 UTC)

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