BLOCK DM-SL R/B, 54034
Orbit data source: Space-Track
BLOCK DM-SL R/B, 54034 is space debris in GEO originally from a launch on Wed, 12 Oct 2022 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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54034 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BLOCK DM-SL R/B
1 54034U 22131B 25257.94849280 -.00000088 00000-0 00000-0 0 9997
2 54034 2.6568 82.3867 0078767 31.4624 329.4231 0.97748506 10432
Epoch: 2025-09-14T22:45Z
TLE epoch observation values (Epoch: 2025-09-14T22:45:49.777Z)
Latitude
-0°
Longitude
107.18149°
Altitude
36,219.634 km
Speed
3.069 km/s
True Right ascension
05h 31m 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
15:50:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,848.003 km
Perigee altitude
36,172.367 km
Semi-major axis
42,888.322 km
Eccentricity
0.00788
Inclination
2.6568°
RAAN
82.3867°
Arg. of periapsis
31.4624°
True anomaly
328.96003°
Mean anomaly
329.4231°
Eccentric anomaly
329.19196°
Mean motion
0.24436 °/min
Orbital period
1,473.22 mins
BSTAR
0
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Other satellites on launch #131 in the year 2022 (2022-10-12 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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54034 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 ascending 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 ascending order |
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