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 (9 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, Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FREGAT R/B
1 65591U 25206C   26165.55946471 -.00000055  00000-0  00000-0 0  9993
2 65591  64.6441 314.9242 0010642 176.1747 183.8186  2.14651315  5901
Epoch: 2026-06-14T13:25Z
TLE epoch observation values (Epoch: 2026-06-14T13:25:37.750Z)
Latitude
-0.00001°
Longitude
-149.3586°
Altitude
19,034.475 km
Speed
3.958 km/s
True Right ascension
20h 59m 37s
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
12:38:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,033.638 km
Perigee altitude
18,979.609 km
Semi-major axis
25,384.76 km
Eccentricity
0.00106
Inclination
64.6441°
RAAN
314.9242°
Arg. of periapsis
176.1747°
True anomaly
183.81049°
Mean anomaly
183.8186°
Eccentric anomaly
183.81454°
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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