BLOCK DM-SL DEB, 46091
Orbit data source: Space-Track
BLOCK DM-SL DEB, 46091 is space debris in GEO originally from a launch on Tue, 24 Dec 2019 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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46091 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BLOCK DM-SL DEB
1 46091U 19095E 26317.61303565 -.00000004 00000-0 00000+0 0 9996
2 46091 5.6879 71.3997 0104544 206.7570 152.5556 1.03274763 25287Epoch: 2026-11-13T14:42Z
TLE epoch observation values (Epoch: 2026-11-13T14:42:46.280Z)
Latitude
0.00001°
Longitude
157.80784°
Altitude
35,350.065 km
Speed
3.076 km/s
True Right ascension
04h 44m 55s
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
13:12:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,398.523 km
Perigee altitude
34,534.061 km
Semi-major axis
41,344.429 km
Eccentricity
0.01045
Inclination
5.6879°
RAAN
71.3997°
Arg. of periapsis
206.757°
True anomaly
153.1014°
Mean anomaly
152.5556°
Eccentric anomaly
152.82913°
Mean motion
0.25818 °/min
Orbital period
1,394.39 mins
BSTAR
0
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Other satellites on launch #95 in the year 2019 (2019-12-24 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.BLOCK DM-SL 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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| BLOCK DM-SL DEB is likely not visible in the next few days. |
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46091 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
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