FREGAT R/B, 52146

Orbit data source: Space-Track

FREGAT R/B, 52146 is space debris in HEO originally from a launch on Tue, 22 Mar 2022 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
52146, 2022-030B
Orbit
HEO
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)
2022-03-22 (4 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: 6 days ago

TLE from 6 days ago
0 FREGAT R/B
1 52146U 22030B   26167.20613662  .00000125  00000-0  00000-0 0  9991
2 52146  62.7154 135.0474 6864336 274.5567  16.4059  2.00263499 30992
Epoch: 2026-06-16T04:56Z
TLE epoch observation values (Epoch: 2026-06-16T04:56:50.203Z)
Latitude
-0.00005°
Longitude
156.32431°
Altitude
6,973.26 km
Speed
6.687 km/s
True Right ascension
09h 00m 03s
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
21:28:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,457.549 km
Perigee altitude
1,958.369 km
Semi-major axis
26,586.096 km
Eccentricity
0.68643
Inclination
62.7154°
RAAN
135.0474°
Arg. of periapsis
274.5567°
True anomaly
85.49027°
Mean anomaly
16.4059°
Eccentric anomaly
43.45759°
Mean motion
0.50068 °/min
Orbital period
719.02 mins
BSTAR
0
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Other satellites on launch #30 in the year 2022 (2022-03-22 UTC)

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