BREEZE-M R/B, 64468
Orbit data source: Space-Track
BREEZE-M R/B, 64468 is space debris in HEO 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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64468 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
None
Manufacturer
Khrunichev
Mission
Spacecraft
Bus & Motor
BRIZ, Unknown motor
Mass
~1,600 kg wet, 1,600 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 2.0 m
Radar Cross Section
15.135 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 BREEZE-M R/B
1 64468U 25131B 25173.80781051 -.00000145 00000-0 00000+0 0 9998
2 64468 1.4224 285.7735 3876101 171.5822 241.3112 1.04440359 39Epoch: 2025-06-22T19:23Z
TLE epoch observation values (Epoch: 2025-06-22T19:23:14.828Z)
Latitude
0.53575°
Longitude
106.30196°
Altitude
45,844.889 km
Speed
2.356 km/s
True Right ascension
20h 33m 21s
True Declination
0° 32' 07"
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
14:26:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
50,564.618 km
Perigee altitude
18,752.242 km
Semi-major axis
41,036.567 km
Eccentricity
0.38761
Inclination
1.4224°
RAAN
285.7735°
Arg. of periapsis
171.5822°
True anomaly
211.11644°
Mean anomaly
241.3112°
Eccentric anomaly
225.47722°
Mean motion
0.26109 °/min
Orbital period
1,378.85 mins
BSTAR
0
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Other satellites on launch #131 in the year 2025 (2025-06-19 UTC)
BREEZE-M R/B Visibility
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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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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Authenticating...
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