FREGAT R/B, 63131
Orbit data source: Space-Track
FREGAT R/B, 63131 is space debris in MEO originally from a launch on Sun, 02 Mar 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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63131 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,000 kg wet, 1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.8 m
Radar Cross Section
8.354 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 weeks ago
TLE from 4 weeks ago
0 FREGAT R/B
1 63131U 25042B 26251.86567126 .00000031 00000-0 00000+0 0 9997
2 63131 65.1382 69.8360 0015746 194.0895 165.9157 2.13754713 11854Epoch: 2026-09-08T20:46Z
TLE epoch observation values (Epoch: 2026-09-08T20:46:33.996Z)
Latitude
-0.00005°
Longitude
130.26183°
Altitude
19,117.318 km
Speed
3.951 km/s
True Right ascension
04h 39m 19s
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
08:51:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,117.626 km
Perigee altitude
19,037.461 km
Semi-major axis
25,455.68 km
Eccentricity
0.00157
Inclination
65.1382°
RAAN
69.836°
Arg. of periapsis
194.0895°
True anomaly
165.95953°
Mean anomaly
165.9157°
Eccentric anomaly
165.93762°
Mean motion
0.5344 °/min
Orbital period
673.65 mins
BSTAR
0
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Other satellites on launch #42 in the year 2025 (2025-03-02 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 324 mins | 2026-10-04 14:59:01.826Z | 263.047° W | 2026-10-04 17:33:01.826Z | 20.27° NNE | 57.975° | 2026-10-04 20:23:01.826Z | 135.356° SSE |
| 172 mins | 2026-10-05 12:07:01.826Z | 212.429° SW | 2026-10-05 14:40:01.826Z | 316.005° NNW | 63.287° | 2026-10-05 14:59:01.826Z | 339.456° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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