S5 DEB, 44066
Orbit data source: Space-Track
S5 DEB, 44066 is space debris in GEO originally from a launch on Fri, 22 Feb 2019 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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44066 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 S5 DEB
1 44066U 19009E 26155.14271979 -.00000225 00000-0 00000-0 0 9998
2 44066 6.5545 71.1074 0002115 195.5242 164.2702 0.98986717 26234Epoch: 2026-06-04T03:25Z
TLE epoch observation values (Epoch: 2026-06-04T03:25:30.989Z)
Latitude
0°
Longitude
126.93965°
Altitude
36,158.949 km
Speed
3.061 km/s
True Right ascension
04h 43m 38s
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
09:20:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,160.774 km
Perigee altitude
36,142.784 km
Semi-major axis
42,529.916 km
Eccentricity
0.00021
Inclination
6.5545°
RAAN
71.1074°
Arg. of periapsis
195.5242°
True anomaly
164.27677°
Mean anomaly
164.2702°
Eccentric anomaly
164.27348°
Mean motion
0.24746 °/min
Orbital period
1,454.79 mins
BSTAR
0
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Other satellites on launch #9 in the year 2019 (2019-02-22 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.S5 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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| S5 DEB is likely not visible in the next few days. |
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44066 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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