BREEZE-M R/B, 40346
Orbit data source: Space-Track
BREEZE-M R/B, 40346 is space debris originally from a launch on Mon, 15 Dec 2014 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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40346 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 BREEZE-M R/B
1 40346U 14082B 26070.43458865 -.00000175 00000-0 00000+0 0 9993
2 40346 8.4606 52.7433 0660679 186.1506 173.0998 1.11336083 45471Epoch: 2026-03-11T10:25Z
TLE epoch observation values (Epoch: 2026-03-11T10:25:48.459Z)
Latitude
0.00001°
Longitude
87.27105°
Altitude
35,519.152 km
Speed
2.982 km/s
True Right ascension
03h 31m 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
13:32:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,543.837 km
Perigee altitude
30,347.739 km
Semi-major axis
39,323.925 km
Eccentricity
0.06607
Inclination
8.4606°
RAAN
52.7433°
Arg. of periapsis
186.1506°
True anomaly
173.94023°
Mean anomaly
173.0998°
Eccentric anomaly
173.52658°
Mean motion
0.27833 °/min
Orbital period
1,293.44 mins
BSTAR
0
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Other satellites on launch #82 in the year 2014 (2014-12-15 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. |
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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