BREEZE-M R/B, 40883
Orbit data source: Space-Track
BREEZE-M R/B, 40883 is space debris in HEO originally from a launch on Fri, 28 Aug 2015 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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40883 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 BREEZE-M R/B
1 40883U 15042B 25336.44745770 -.00000044 00000-0 00000-0 0 9991
2 40883 26.1186 99.1495 7958376 123.3099 337.2081 1.10227852 41331Epoch: 2025-12-02T10:44Z
TLE epoch observation values (Epoch: 2025-12-02T10:44:20.345Z)
Latitude
0.00004°
Longitude
-133.72129°
Altitude
19,467.236 km
Speed
4.558 km/s
True Right ascension
06h 35m 35s
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
06:17:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
64,718.207 km
Perigee altitude
1,704.554 km
Semi-major axis
39,589.518 km
Eccentricity
0.79584
Inclination
26.1186°
RAAN
99.1495°
Arg. of periapsis
123.3099°
True anomaly
237.025°
Mean anomaly
337.2081°
Eccentric anomaly
296.34635°
Mean motion
0.27553 °/min
Orbital period
1,306.56 mins
BSTAR
0
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Other satellites on launch #42 in the year 2015 (2015-08-28 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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