BREEZE-M R/B, 39128
Orbit data source: Space-Track
BREEZE-M R/B, 39128 is space debris in HEO originally from a launch on Mon, 15 Apr 2013 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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39128 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 39128U 13014B 25241.53517053 -.00000148 00000-0 00000-0 0 9999
2 39128 15.3805 31.6493 4792596 156.4246 236.1400 1.90430071 86064
Epoch: 2025-08-29T12:50Z
TLE epoch observation values (Epoch: 2025-08-29T12:50:38.733Z)
Latitude
-0.00004°
Longitude
-138.9725°
Altitude
31,370.248 km
Speed
2.573 km/s
True Right ascension
02h 06m 41s
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
15:52:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,296.432 km
Perigee altitude
7,940.439 km
Semi-major axis
27,496.573 km
Eccentricity
0.47926
Inclination
15.3805°
RAAN
31.6493°
Arg. of periapsis
156.4246°
True anomaly
203.66552°
Mean anomaly
236.14°
Eccentric anomaly
218.89739°
Mean motion
0.47602 °/min
Orbital period
756.27 mins
BSTAR
0
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Other satellites on launch #14 in the year 2013 (2013-04-15 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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146 mins | 2025-08-31 17:25:27.450Z | 262.678° W | 2025-08-31 19:11:27.450Z | 199.314° SSW | 35.105° | 2025-08-31 19:51:27.450Z | 128.019° SE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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