SOYUZ 2.1B R/B, 65266
Orbit data source: Space-Track
SOYUZ 2.1B R/B, 65266 is space debris in LEO originally from a launch on Wed, 20 Aug 2025 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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65266 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Spacecraft
Bus & Motor
BLOK-I, Unknown motor
Mass
~0 kg wet, 2,350 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 hours ago
TLE from 3 hours ago
0 SOYUZ 2.1B R/B
1 65266U 25181B 25240.91241172 .02479330 22481-5 63026-3 0 9992
2 65266 96.9429 309.1479 0060387 24.0399 336.3690 16.23693976 1328Epoch: 2025-08-28T21:53Z
TLE epoch observation values (Epoch: 2025-08-28T21:53:52.372Z)
Latitude
-0.00006°
Longitude
3.31108°
Altitude
176.369 km
Speed
7.822 km/s
True Right ascension
20h 36m 35s
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
16:13:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
246.112 km
Perigee altitude
166.588 km
Semi-major axis
6,584.487 km
Eccentricity
0.00604
Inclination
96.9429°
RAAN
309.1479°
Arg. of periapsis
24.0399°
True anomaly
336.08969°
Mean anomaly
336.369°
Eccentric anomaly
336.22954°
Mean motion
4.06219 °/min
Orbital period
88.62 mins
BSTAR
0.00063026
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Other satellites on launch #181 in the year 2025 (2025-08-20 UTC)
SOYUZ 2.1B R/B Visibility
Observer location: undefined°, undefined°
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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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