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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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 ATLAS 5 CENTAUR R/B
1 51282U 22006C 26225.26090685 -.00000181 00000-0 00000-0 0 9992
2 51282 4.7442 75.3300 0263380 15.5592 345.4338 0.95003092 11738Epoch: 2026-08-13T06:15Z
TLE epoch observation values (Epoch: 2026-08-13T06:15:42.351Z)
Latitude
0.00001°
Longitude
19.90713°
Altitude
36,221.364 km
Speed
3.098 km/s
True Right ascension
05h 02m 08s
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
09:03:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,483.723 km
Perigee altitude
36,181.223 km
Semi-major axis
43,710.61 km
Eccentricity
0.02634
Inclination
4.7442°
RAAN
75.33°
Arg. of periapsis
15.5592°
True anomaly
344.64983°
Mean anomaly
345.4338°
Eccentric anomaly
345.04436°
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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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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