BLOCK DM-SL R/B, 44904
Orbit data source: Space-Track
BLOCK DM-SL R/B, 44904 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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44904 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 BLOCK DM-SL R/B
1 44904U 19095B 26047.91042868 -.00000051 00000-0 00000+0 0 9998
2 44904 5.0341 75.0660 0071143 270.4719 88.9179 1.02970547 23154Epoch: 2026-02-16T21:51Z
TLE epoch observation values (Epoch: 2026-02-16T21:51:01.037Z)
Latitude
0.00001°
Longitude
-39.36303°
Altitude
35,043.762 km
Speed
3.102 km/s
True Right ascension
05h 01m 09s
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
20:35:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,342.399 km
Perigee altitude
34,752.967 km
Semi-major axis
41,425.82 km
Eccentricity
0.00711
Inclination
5.0341°
RAAN
75.066°
Arg. of periapsis
270.4719°
True anomaly
89.7331°
Mean anomaly
88.9179°
Eccentric anomaly
89.32549°
Mean motion
0.25742 °/min
Orbital period
1,398.51 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 R/B 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 R/B is likely not visible in the next few days. |
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44904 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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