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 (10 months ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
8.354 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FREGAT R/B
1 63131U 25042B   26006.25541761 -.00000018  00000-0  00000-0 0  9992
2 63131  64.9894  78.2435 0016815 195.5215 164.4873  2.13753619  6606
Epoch: 2026-01-06T06:07Z
TLE epoch observation values (Epoch: 2026-01-06T06:07:48.081Z)
Latitude
0.00001°
Longitude
-119.53089°
Altitude
19,119.835 km
Speed
3.951 km/s
True Right ascension
05h 13m 02s
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
15:32:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,120.439 km
Perigee altitude
19,034.832 km
Semi-major axis
25,455.772 km
Eccentricity
0.00168
Inclination
64.9894°
RAAN
78.2435°
Arg. of periapsis
195.5215°
True anomaly
164.53873°
Mean anomaly
164.4873°
Eccentric anomaly
164.51303°
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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