FREGAT R/B, 65591

Orbit data source: Space-Track

FREGAT R/B, 65591 is space debris in MEO originally from a launch on Sat, 13 Sep 2025 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
65591, 2025-206C
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)
2025-09-13 (7 months ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
8.354 m²

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 FREGAT R/B
1 65591U 25206C   26111.05229394 -.00000026  00000-0  00000-0 0  9995
2 65591  64.6755 316.8520 0010265 175.7245 184.3136  2.14651317  4731
Epoch: 2026-04-21T01:15Z
TLE epoch observation values (Epoch: 2026-04-21T01:15:18.196Z)
Latitude
-0.00004°
Longitude
88.90139°
Altitude
19,033.506 km
Speed
3.959 km/s
True Right ascension
21h 07m 26s
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
22:11:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,032.679 km
Perigee altitude
18,980.564 km
Semi-major axis
25,384.759 km
Eccentricity
0.00103
Inclination
64.6755°
RAAN
316.852°
Arg. of periapsis
175.7245°
True anomaly
184.30476°
Mean anomaly
184.3136°
Eccentric anomaly
184.30918°
Mean motion
0.53664 °/min
Orbital period
670.84 mins
BSTAR
0
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Other satellites on launch #206 in the year 2025 (2025-09-13 UTC)

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