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 26317.87173230 -.00000157 00000-0 00000-0 0 9999
2 44904 5.6968 71.4958 0070302 279.5515 79.5147 1.02972962 25937Epoch: 2026-11-13T20:55Z
TLE epoch observation values (Epoch: 2026-11-13T20:55:17.670Z)
Latitude
-0°
Longitude
64.52031°
Altitude
34,993.358 km
Speed
3.106 km/s
True Right ascension
04h 45m 18s
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
35,338.259 km
Perigee altitude
34,755.805 km
Semi-major axis
41,425.169 km
Eccentricity
0.00703
Inclination
5.6968°
RAAN
71.4958°
Arg. of periapsis
279.5515°
True anomaly
80.30809°
Mean anomaly
79.5147°
Eccentric anomaly
79.91127°
Mean motion
0.25742 °/min
Orbital period
1,398.48 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
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