FREGAT R/B, 46806

Orbit data source: Space-Track

FREGAT R/B, 46806 is space debris in MEO originally from a launch on Sun, 25 Oct 2020 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
46806, 2020-075B
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)
2020-10-25 (6 years 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: 2 days ago

TLE from 2 days ago
0 FREGAT R/B
1 46806U 20075B   26171.47461377  .00000062  00000-0  00000+0 0  9991
2 46806  64.5711 195.6391 0054640 129.1429 231.3927  2.08518318 43034
Epoch: 2026-06-20T11:23Z
TLE epoch observation values (Epoch: 2026-06-20T11:23:26.629Z)
Latitude
0.00002°
Longitude
116.09283°
Altitude
19,591.595 km
Speed
3.911 km/s
True Right ascension
13h 02m 34s
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
21:30:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,643.39 km
Perigee altitude
19,360.572 km
Semi-major axis
25,880.118 km
Eccentricity
0.00546
Inclination
64.5711°
RAAN
195.6391°
Arg. of periapsis
129.1429°
True anomaly
230.9055°
Mean anomaly
231.3927°
Eccentric anomaly
231.14889°
Mean motion
0.52131 °/min
Orbital period
690.57 mins
BSTAR
0
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Other satellites on launch #75 in the year 2020 (2020-10-25 UTC)

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