ATLAS 5 CENTAUR DEB, 52943
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 52943 is space debris in GEO originally from a launch on Fri, 01 Jul 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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52943 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 ATLAS 5 CENTAUR DEB
1 52943U 22073D 26170.36020607 -.00000007 00000-0 00000-0 0 9995
2 52943 3.7689 78.8241 0007413 44.8683 314.8800 0.98670713 11654Epoch: 2026-06-19T08:38Z
TLE epoch observation values (Epoch: 2026-06-19T08:38:41.804Z)
Latitude
0°
Longitude
41.26342°
Altitude
36,218.565 km
Speed
3.06 km/s
True Right ascension
05h 14m 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
21:50:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,274.139 km
Perigee altitude
36,210.95 km
Semi-major axis
42,620.682 km
Eccentricity
0.00074
Inclination
3.7689°
RAAN
78.8241°
Arg. of periapsis
44.8683°
True anomaly
314.81977°
Mean anomaly
314.88°
Eccentric anomaly
314.84989°
Mean motion
0.24667 °/min
Orbital period
1,459.45 mins
BSTAR
0
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Other satellites on launch #73 in the year 2022 (2022-07-01 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 DEB 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 DEB is likely not visible in the next few days. |
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52943 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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