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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Identifier
63131, 2025-042B
Orbit
MEO
Country
Flag of CISCIS
Related business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,000 kg wet, 1,000 kg dry
Launch date (UTC)
2025-03-02 (6 months ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.7 m
Radar Cross Section
8.354 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 FREGAT R/B
1 63131U 25042B   25255.23354230  .00000025  00000-0  00000-0 0  9995
2 63131  64.9251  82.2220 0016933 193.4234 166.5824  2.13753533  4128
Epoch: 2025-09-12T05:36Z
TLE epoch observation values (Epoch: 2025-09-12T05:36:18.054Z)
Latitude
-0.00008°
Longitude
6.65632°
Altitude
19,120.469 km
Speed
3.951 km/s
True Right ascension
05h 28m 51s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:11:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,120.749 km
Perigee altitude
19,034.54 km
Semi-major axis
25,455.781 km
Eccentricity
0.00169
Inclination
64.9251°
RAAN
82.222°
Arg. of periapsis
193.4234°
True anomaly
166.62733°
Mean anomaly
166.5824°
Eccentric anomaly
166.60488°
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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