ATLAS 5 CENTAUR DEB, 50214
Orbit data source: Space-Track
ATLAS 5 CENTAUR DEB, 50214 is space debris in GEO originally from a launch on Tue, 07 Dec 2021 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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50214 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 ATLAS 5 CENTAUR DEB
1 50214U 21118D 25299.73327785 -.00000298 00000-0 00000-0 0 9994
2 50214 3.7082 80.3777 0012021 54.8841 305.2463 0.99332386 14104Epoch: 2025-10-26T17:35Z
TLE epoch observation values (Epoch: 2025-10-26T17:35:55.206Z)
Latitude
0°
Longitude
141.03462°
Altitude
36,022.348 km
Speed
3.067 km/s
True Right ascension
05h 21m 26s
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
10:34:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,104.08 km
Perigee altitude
36,002.067 km
Semi-major axis
42,431.21 km
Eccentricity
0.0012
Inclination
3.7082°
RAAN
80.3777°
Arg. of periapsis
54.8841°
True anomaly
305.1337°
Mean anomaly
305.2463°
Eccentric anomaly
305.19001°
Mean motion
0.24832 °/min
Orbital period
1,449.73 mins
BSTAR
0
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Other satellites on launch #118 in the year 2021 (2021-12-07 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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50214 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 ascending 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 ascending order |
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