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: 14 hours ago
TLE from 14 hours ago
0 BLOCK DM-SL R/B
1 44904U 19095B 26097.43550934 -.00000177 00000-0 00000+0 0 9997
2 44904 5.1579 74.3930 0070913 272.9613 86.2991 1.02973064 23660Epoch: 2026-04-07T10:27Z
TLE epoch observation values (Epoch: 2026-04-07T10:27:08.006Z)
Latitude
-0°
Longitude
81.97144°
Altitude
35,027.372 km
Speed
3.103 km/s
True Right ascension
04h 57m 52s
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
06:59:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,340.765 km
Perigee altitude
34,753.249 km
Semi-major axis
41,425.144 km
Eccentricity
0.00709
Inclination
5.1579°
RAAN
74.393°
Arg. of periapsis
272.9613°
True anomaly
87.11045°
Mean anomaly
86.2991°
Eccentric anomaly
86.70473°
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
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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