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 (3 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: 21 hours ago

TLE from 21 hours ago
0 FREGAT R/B
1 54154U 22139E   25271.99014340  .00000047  00000-0  00000-0 0  9994
2 54154  89.9634  96.6963 0004990 115.4396 244.6757  4.97563042 50909
Epoch: 2025-09-28T23:45Z
TLE epoch observation values (Epoch: 2025-09-28T23:45:48.389Z)
Latitude
-0.00006°
Longitude
92.24057°
Altitude
8,119.864 km
Speed
5.243 km/s
True Right ascension
06h 26m 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
14:25:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
8,120.967 km
Perigee altitude
8,106.504 km
Semi-major axis
14,491.873 km
Eccentricity
0.0005
Inclination
89.9634°
RAAN
96.6963°
Arg. of periapsis
115.4396°
True anomaly
244.62403°
Mean anomaly
244.6757°
Eccentric anomaly
244.64986°
Mean motion
1.2441 °/min
Orbital period
289.37 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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