BREEZE-M R/B, 42909
Orbit data source: Space-Track
BREEZE-M R/B, 42909 is space debris in GEO originally from a launch on Wed, 16 Aug 2017 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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42909 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 BREEZE-M R/B
1 42909U 17046C 26077.17087450 -.00000137 00000-0 00000+0 0 9997
2 42909 8.4416 69.1355 0755890 159.4595 203.9837 0.90332731 28336Epoch: 2026-03-18T04:06Z
TLE epoch observation values (Epoch: 2026-03-18T04:06:03.556Z)
Latitude
0°
Longitude
-167.94974°
Altitude
41,973.11 km
Speed
2.769 km/s
True Right ascension
04h 37m 12s
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
22:34:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
42,243.268 km
Perigee altitude
35,409.35 km
Semi-major axis
45,204.446 km
Eccentricity
0.07559
Inclination
8.4416°
RAAN
69.1355°
Arg. of periapsis
159.4595°
True anomaly
200.74514°
Mean anomaly
203.9837°
Eccentric anomaly
202.33767°
Mean motion
0.22582 °/min
Orbital period
1,594.16 mins
BSTAR
0
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Other satellites on launch #46 in the year 2017 (2017-08-16 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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42909 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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