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   26062.11548708 -.00000137  00000-0  00000+0 0  9999
2 51282   4.3074  77.1130 0263134  11.0224 349.8698  0.95002354 10181
Epoch: 2026-03-03T02:46Z
TLE epoch observation values (Epoch: 2026-03-03T02:46:18.083Z)
Latitude
0.00001°
Longitude
-124.99325°
Altitude
36,205.822 km
Speed
3.099 km/s
True Right ascension
05h 09m 55s
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
11:40:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,482.882 km
Perigee altitude
36,182.52 km
Semi-major axis
43,710.838 km
Eccentricity
0.02631
Inclination
4.3074°
RAAN
77.113°
Arg. of periapsis
11.0224°
True anomaly
349.32174°
Mean anomaly
349.8698°
Eccentric anomaly
349.59758°
Mean motion
0.2375 °/min
Orbital period
1,515.8 mins
BSTAR
0
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Other satellites on launch #6 in the year 2022 (2022-01-21 UTC)

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