BREEZE-M R/B, 39376
Orbit data source: Space-Track
BREEZE-M R/B, 39376 is space debris in GEO originally from a launch on Mon, 11 Nov 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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39376 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 BREEZE-M R/B
1 39376U 13062B 26171.03934240 -.00000128 00000-0 00000+0 0 9993
2 39376 9.4251 51.7267 0232450 116.1579 246.1892 1.04209043 47977Epoch: 2026-06-20T00:56Z
TLE epoch observation values (Epoch: 2026-06-20T00:56:39.183Z)
Latitude
-0.00001°
Longitude
129.26224°
Altitude
35,117.503 km
Speed
3.084 km/s
True Right ascension
03h 26m 44s
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
23:08:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,674.091 km
Perigee altitude
33,763.495 km
Semi-major axis
41,096.93 km
Eccentricity
0.02325
Inclination
9.4251°
RAAN
51.7267°
Arg. of periapsis
116.1579°
True anomaly
243.78122°
Mean anomaly
246.1892°
Eccentric anomaly
244.98232°
Mean motion
0.26051 °/min
Orbital period
1,381.89 mins
BSTAR
0
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Other satellites on launch #62 in the year 2013 (2013-11-11 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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39376 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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