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 & history
TLE from 2 days ago
0 BREEZE-M R/B
1 43433U 18037B 25198.44537592 -.00000154 00000-0 00000-0 0 9991
2 43433 7.1919 74.8423 0687101 20.3599 342.2648 0.90514609 24172
Epoch: 2025-07-17T10:41Z
TLE epoch observation values (Epoch: 2025-07-17T10:41:20.479Z)
Latitude
-0.00003°
Longitude
-21.02041°
Altitude
35,824.892 km
Speed
3.172 km/s
True Right ascension
04h 59m 18s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
3.2424°
Longitude
132.3887°
Altitude
40,752.932 km
Speed
2.843 km/s
Apparent Right ascension
15h 29m 06s
Apparent Declination
-1° 51' 37"
Sunlit
Visualization observer readout
Local Sidereal Time
12:38:44
Azimuth
126.311° SE
Elevation
32.925°
Doppler factor
1
Orbital elements
Apogee altitude
41,867.584 km
Perigee altitude
35,663.903 km
Semi-major axis
45,143.88 km
Eccentricity
0.06871
Inclination
7.1919°
RAAN
74.8423°
Arg. of periapsis
20.3599°
True anomaly
339.65443°
Mean anomaly
342.2648°
Eccentric anomaly
340.98193°
Mean motion
0.22628 °/min
Orbital period
1,590.95 mins
BSTAR
0
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Other satellites on launch #37 in the year 2018 (2018-04-18 UTC)
BREEZE-M R/B Visibility forecast
Observer location: undefined°, undefined°
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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1440 mins | 2025-07-18 23:51:03.760Z | 126.324° SE | 2025-07-19 22:13:03.760Z | 166.724° S | 38.022° | 2025-07-19 23:51:03.760Z | 170.619° S |
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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
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