SOYUZ 2.1B R/B, 65266 (Decayed)
Orbit data source: Space-Track
SOYUZ 2.1B R/B, 65266 was 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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Identifier
Orbit
Country
CISRelated business
Manufacturer
TsSKB-Progress
Mission
Decayed 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
Cyl, 8.0 m
Radar Cross Section
17.919 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 SOYUZ 2.1B R/B
1 65266U 25181B 25243.18111148 .10406097 23687-5 16263-3 0 9992
2 65266 96.9316 311.6082 0021481 6.7566 353.4023 16.46588403 1699Epoch: 2025-08-31T04:20Z
TLE epoch observation values (Epoch: 2025-08-31T04:20:48.031Z)
Latitude
-0.00009°
Longitude
-93.19666°
Altitude
137.679 km
Speed
7.832 km/s
True Right ascension
20h 46m 25s
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
07:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
159.126 km
Perigee altitude
131.101 km
Semi-major axis
6,523.25 km
Eccentricity
0.00215
Inclination
96.9316°
RAAN
311.6082°
Arg. of periapsis
6.7566°
True anomaly
353.37394°
Mean anomaly
353.4023°
Eccentric anomaly
353.38813°
Mean motion
4.11952 °/min
Orbital period
87.39 mins
BSTAR
0.00016263
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Other satellites on launch #181 in the year 2025 (2025-08-20 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.SOYUZ 2.1B 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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| 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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