FREGAT R/B, 54154

Orbit data source: Space-Track

FREGAT R/B, 54154 is space debris originally from a launch on Sat, 22 Oct 2022 UTC launched from the Vostochny Cosmodrome (VOSTO). 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
54154, 2022-139E
Orbit
Active
Country
Flag of CISCIS
Related business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,624 kg wet, 1,000 kg dry
Launch date (UTC)
2022-10-22 (4 years ago)
Launch vehicle
Unknown
Launch site
Vostochny Cosmodrome (VOSTO)
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: 4 days ago

TLE from 4 days ago
0 FREGAT R/B
1 54154U 22139E   26169.30928315  .00000012  00000-0  00000+0 0  9993
2 54154  89.9484  96.6128 0004410  41.4177 318.6672  4.97563393 63953
Epoch: 2026-06-18T07:25Z
TLE epoch observation values (Epoch: 2026-06-18T07:25:22.064Z)
Latitude
-0.00003°
Longitude
78.72109°
Altitude
8,111.96 km
Speed
5.246 km/s
True Right ascension
06h 26m 28s
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
02:14:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,120.12 km
Perigee altitude
8,107.338 km
Semi-major axis
14,491.866 km
Eccentricity
0.00044
Inclination
89.9484°
RAAN
96.6128°
Arg. of periapsis
41.4177°
True anomaly
318.63381°
Mean anomaly
318.6672°
Eccentric anomaly
318.65051°
Mean motion
1.2441 °/min
Orbital period
289.36 mins
BSTAR
0
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Other satellites on launch #139 in the year 2022 (2022-10-22 UTC)

Documentation

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