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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51282 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ATLAS 5 CENTAUR R/B
1 51282U 22006C 26011.59152875 -.00000144 00000-0 00000-0 0 9990
2 51282 4.1711 77.6792 0262691 9.9928 350.3698 0.95002620 9709Epoch: 2026-01-11T14:11Z
TLE epoch observation values (Epoch: 2026-01-11T14:11:48.084Z)
Latitude
-0°
Longitude
113.47716°
Altitude
36,196.745 km
Speed
3.099 km/s
True Right ascension
05h 10m 06s
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
21:20:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,480.862 km
Perigee altitude
36,184.378 km
Semi-major axis
43,710.757 km
Eccentricity
0.02627
Inclination
4.1711°
RAAN
77.6792°
Arg. of periapsis
9.9928°
True anomaly
349.84941°
Mean anomaly
350.3698°
Eccentric anomaly
350.11132°
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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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
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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. |
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| ATLAS 5 CENTAUR R/B is likely not visible in the next few days. |
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51282 neighbors
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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 descending 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 descending order |
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