BREEZE-M R/B, 55842
Orbit data source: Space-Track
BREEZE-M R/B, 55842 is space debris in GEO originally from a launch on Sun, 12 Mar 2023 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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55842 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 BREEZE-M R/B
1 55842U 23031B 26034.56742061 -.00000101 00000-0 00000-0 0 9992
2 55842 2.4821 81.1355 0066758 6.5333 353.7054 0.98959688 10457Epoch: 2026-02-03T13:37Z
TLE epoch observation values (Epoch: 2026-02-03T13:37:05.140Z)
Latitude
0°
Longitude
103.3035°
Altitude
35,876.057 km
Speed
3.082 km/s
True Right ascension
05h 25m 17s
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
04:11:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,443.513 km
Perigee altitude
35,875.567 km
Semi-major axis
42,537.677 km
Eccentricity
0.00668
Inclination
2.4821°
RAAN
81.1355°
Arg. of periapsis
6.5333°
True anomaly
353.62082°
Mean anomaly
353.7054°
Eccentric anomaly
353.66318°
Mean motion
0.24739 °/min
Orbital period
1,455.19 mins
BSTAR
0
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Other satellites on launch #31 in the year 2023 (2023-03-12 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.BREEZE-M 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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| BREEZE-M R/B is likely not visible in the next few days. |
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55842 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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