BREEZE-M R/B, 40385
Orbit data source: Space-Track
BREEZE-M R/B, 40385 is space debris in HEO originally from a launch on Sun, 01 Feb 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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40385 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 40385U 15005B 25256.19941096 -.00000255 00000-0 00000-0 0 9993
2 40385 27.4055 298.9349 7593259 89.7187 347.5697 1.11107049 43078
Epoch: 2025-09-13T04:47Z
TLE epoch observation values (Epoch: 2025-09-13T04:47:09.106Z)
Latitude
-0.00032°
Longitude
-125.17308°
Altitude
10,158.046 km
Speed
6.171 km/s
True Right ascension
19h 56m 12s
True Declination
0° 00' 01"
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
16:01:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
62,903.457 km
Perigee altitude
3,099.519 km
Semi-major axis
39,379.625 km
Eccentricity
0.75933
Inclination
27.4055°
RAAN
298.9349°
Arg. of periapsis
89.7187°
True anomaly
269.47728°
Mean anomaly
347.5697°
Eccentric anomaly
319.06348°
Mean motion
0.27774 °/min
Orbital period
1,296.18 mins
BSTAR
0
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Other satellites on launch #5 in the year 2015 (2015-02-01 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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