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, 8.0 m
Radar Cross Section
8.354 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 FREGAT R/B
1 63131U 25042B 26088.12555938 .00000037 00000-0 00000-0 0 9999
2 63131 65.0397 75.4363 0015905 197.8340 162.1179 2.13753819 8358Epoch: 2026-03-29T03:00Z
TLE epoch observation values (Epoch: 2026-03-29T03:00:48.330Z)
Latitude
-0°
Longitude
-156.31458°
Altitude
19,117.078 km
Speed
3.951 km/s
True Right ascension
05h 01m 41s
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
19:39:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,118.105 km
Perigee altitude
19,037.13 km
Semi-major axis
25,455.755 km
Eccentricity
0.00159
Inclination
65.0397°
RAAN
75.4363°
Arg. of periapsis
197.834°
True anomaly
162.17376°
Mean anomaly
162.1179°
Eccentric anomaly
162.14584°
Mean motion
0.5344 °/min
Orbital period
673.66 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. |
|---|---|---|---|---|---|---|---|
| 71 mins | 2026-04-01 14:00:27.937Z | 283.213° WNW | 2026-04-01 14:00:27.937Z | 283.213° WNW | 27.72° | 2026-04-01 15:11:27.937Z | 248.838° W |
| 229 mins | 2026-04-01 20:20:27.937Z | 138.468° SSE | 2026-04-01 22:14:27.937Z | 77.277° E | 37.848° | 2026-04-02 00:09:27.937Z | 30.046° NE |
| 219 mins | 2026-04-02 10:21:27.937Z | 329.354° NNW | 2026-04-02 12:17:27.937Z | 281.598° WNW | 38.482° | 2026-04-02 14:00:27.937Z | 222.378° SW |
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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