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 26255.15353262 -.00000061 00000-0 00000-0 0 9994
2 44066 6.8023 69.8778 0009259 155.8662 204.3979 0.98986365 27225Epoch: 2026-09-12T03:41Z
TLE epoch observation values (Epoch: 2026-09-12T03:41:05.218Z)
Latitude
-0.00001°
Longitude
23.64795°
Altitude
36,186.07 km
Speed
3.059 km/s
True Right ascension
04h 40m 20s
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
02:30:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,191.257 km
Perigee altitude
36,112.5 km
Semi-major axis
42,530.016 km
Eccentricity
0.00093
Inclination
6.8023°
RAAN
69.8778°
Arg. of periapsis
155.8662°
True anomaly
204.35412°
Mean anomaly
204.3979°
Eccentric anomaly
204.376°
Mean motion
0.24746 °/min
Orbital period
1,454.8 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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