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: 2 days ago
TLE from 2 days ago
0 BLOCK DM-SL DEB
1 46091U 19095E 26275.98125485 -.00000169 00000-0 00000-0 0 9995
2 46091 5.5847 71.9338 0070747 194.4353 165.5043 1.03276527 24852Epoch: 2026-10-02T23:33Z
TLE epoch observation values (Epoch: 2026-10-02T23:33:00.419Z)
Latitude
0.00001°
Longitude
67.10169°
Altitude
35,246.626 km
Speed
3.084 km/s
True Right ascension
04h 48m 11s
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
16:34:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,258.318 km
Perigee altitude
34,673.325 km
Semi-major axis
41,343.959 km
Eccentricity
0.00707
Inclination
5.5847°
RAAN
71.9338°
Arg. of periapsis
194.4353°
True anomaly
165.7055°
Mean anomaly
165.5043°
Eccentric anomaly
165.60507°
Mean motion
0.25818 °/min
Orbital period
1,394.37 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
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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