FREGAT R/B, 68537 (Decayed)
Orbit data source: Space-Track
FREGAT R/B, 68537 was space debris in LEO originally from a launch on Mon, 23 Mar 2026 UTC via a SOYUZ-2-1B launch vehicle 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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68537 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown (RU)
Mission
Decayed spacecraft
Bus & Motor
OBZP, Unknown motor
Mass
~2,360 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 3.8 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 FREGAT R/B
1 68537U 26061S 26136.73612394 .12102578 -12032-5 10642-3 0 9993
2 68537 82.2910 46.3768 0011375 231.6889 128.3394 16.51508772 8652Epoch: 2026-05-16T17:40Z
TLE epoch observation values (Epoch: 2026-05-16T17:40:01.108Z)
Latitude
0.00002°
Longitude
-93.07663°
Altitude
143.225 km
Speed
7.817 km/s
True Right ascension
03h 05m 30s
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
13:26:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
139.578 km
Perigee altitude
124.767 km
Semi-major axis
6,510.309 km
Eccentricity
0.00114
Inclination
82.291°
RAAN
46.3768°
Arg. of periapsis
231.6889°
True anomaly
128.44155°
Mean anomaly
128.3394°
Eccentric anomaly
128.39048°
Mean motion
4.13181 °/min
Orbital period
87.13 mins
BSTAR
0.00010642
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Other satellites on launch #61 in the year 2026 (2026-03-23 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.FREGAT 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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