BREEZE-M R/B, 33598
Orbit data source: Space-Track
BREEZE-M R/B, 33598 is space debris in GEO originally from a launch on Wed, 11 Feb 2009 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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33598 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 BREEZE-M R/B
1 33598U 09007D 26194.71203669 -.00000101 00000-0 00000+0 0 9992
2 33598 12.4837 36.2327 0202473 61.9639 131.1531 0.97631292 62530Epoch: 2026-07-13T17:05Z
TLE epoch observation values (Epoch: 2026-07-13T17:05:19.970Z)
Latitude
-3.1766°
Longitude
42.83396°
Altitude
37,127.076 km
Speed
3.006 km/s
True Right ascension
15h 23m 02s
True Declination
-3° 10' 25"
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
16:31:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,413.502 km
Perigee altitude
35,675.369 km
Semi-major axis
42,922.573 km
Eccentricity
0.02025
Inclination
12.4837°
RAAN
36.2327°
Arg. of periapsis
61.9639°
True anomaly
132.87119°
Mean anomaly
131.1531°
Eccentric anomaly
132.01501°
Mean motion
0.24407 °/min
Orbital period
1,474.99 mins
BSTAR
0
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Other satellites on launch #7 in the year 2009 (2009-02-11 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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33598 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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