BREEZE-M R/B, 43433
Orbit data source: Space-Track
BREEZE-M R/B, 43433 is space debris in GEO originally from a launch on Wed, 18 Apr 2018 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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43433 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BREEZE-M R/B
1 43433U 18037B 25255.89322051 -.00000164 00000-0 00000-0 0 9997
2 43433 7.3538 74.2096 0684467 21.7373 341.1994 0.90514293 24696
Epoch: 2025-09-12T21:26Z
TLE epoch observation values (Epoch: 2025-09-12T21:26:14.252Z)
Latitude
0.00001°
Longitude
120.67256°
Altitude
35,878.751 km
Speed
3.168 km/s
True Right ascension
04h 57m 27s
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
16:35:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
41,855.804 km
Perigee altitude
35,675.89 km
Semi-major axis
45,143.984 km
Eccentricity
0.06845
Inclination
7.3538°
RAAN
74.2096°
Arg. of periapsis
21.7373°
True anomaly
338.45082°
Mean anomaly
341.1994°
Eccentric anomaly
339.84835°
Mean motion
0.22628 °/min
Orbital period
1,590.96 mins
BSTAR
0
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Other satellites on launch #37 in the year 2018 (2018-04-18 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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43433 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 ascending 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 ascending order |
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