FREGAT R/B, 54032

Orbit data source: Space-Track

FREGAT R/B, 54032 is space debris in MEO originally from a launch on Mon, 10 Oct 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
54032, 2022-130B
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)
2022-10-10 (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: 3 days ago

TLE from 3 days ago
0 FREGAT R/B
1 54032U 22130B   26170.23698544 -.00000061  00000-0  00000-0 0  9997
2 54032  64.2715 315.4572 0027525 176.5045 183.5056  2.11046403 28433
Epoch: 2026-06-19T05:41Z
TLE epoch observation values (Epoch: 2026-06-19T05:41:15.542Z)
Latitude
-0.00004°
Longitude
-37.34188°
Altitude
19,366.29 km
Speed
3.93 km/s
True Right ascension
21h 01m 46s
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
21:38:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,365.56 km
Perigee altitude
19,224.23 km
Semi-major axis
25,673.032 km
Eccentricity
0.00275
Inclination
64.2715°
RAAN
315.4572°
Arg. of periapsis
176.5045°
True anomaly
183.48638°
Mean anomaly
183.5056°
Eccentric anomaly
183.49598°
Mean motion
0.52763 °/min
Orbital period
682.3 mins
BSTAR
0
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Other satellites on launch #130 in the year 2022 (2022-10-10 UTC)

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