BREEZE-M DEB (TANK), 64469 (Decayed)
Orbit data source: Space-Track
BREEZE-M DEB (TANK), 64469 was space debris in LEO originally from a launch on Thu, 19 Jun 2025 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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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64469 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 BREEZE-M DEB (TANK)
1 64469U 25131D 26060.53966455 .79572978 21587-5 11765-2 0 9992
2 64469 60.2602 180.2151 0399333 199.5692 158.9711 15.65141535 8754Epoch: 2026-03-01T12:57Z
TLE epoch observation values (Epoch: 2026-03-01T12:57:07.017Z)
Latitude
-0.00006°
Longitude
-173.41014°
Altitude
627.445 km
Speed
7.403 km/s
True Right ascension
12h 00m 51s
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
00:45:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
641.535 km
Perigee altitude
102.426 km
Semi-major axis
6,750.117 km
Eccentricity
0.03993
Inclination
60.2602°
RAAN
180.2151°
Arg. of periapsis
199.5692°
True anomaly
160.53974°
Mean anomaly
158.9711°
Eccentric anomaly
159.76255°
Mean motion
3.9136 °/min
Orbital period
91.99 mins
BSTAR
0.0011765
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Other satellites on launch #131 in the year 2025 (2025-06-19 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 DEB (TANK) 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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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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