FREGAT R/B, 58585

Orbit data source: Space-Track

FREGAT R/B, 58585 is space debris in HEO originally from a launch on Sat, 16 Dec 2023 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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
58585, 2023-198B
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)
2023-12-16 (3 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
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 58585U 23198B   26167.25915534 -.00000206  00000-0  00000+0 0  9998
2 58585  63.2486 154.1059 6950378 266.2825  18.8089  1.99078193 18185
Epoch: 2026-06-16T06:13Z
TLE epoch observation values (Epoch: 2026-06-16T06:13:11.021Z)
Latitude
0.00002°
Longitude
156.24208°
Altitude
8,089.611 km
Speed
6.338 km/s
True Right ascension
10h 16m 17s
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
21:42:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,864.878 km
Perigee altitude
1,761.746 km
Semi-major axis
26,691.449 km
Eccentricity
0.69504
Inclination
63.2486°
RAAN
154.1059°
Arg. of periapsis
266.2825°
True anomaly
93.77576°
Mean anomaly
18.8089°
Eccentric anomaly
48.74855°
Mean motion
0.49772 °/min
Orbital period
723.3 mins
BSTAR
0
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Other satellites on launch #198 in the year 2023 (2023-12-16 UTC)

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