FREGAT R/B, 68572

Orbit data source: Space-Track

FREGAT R/B, 68572 is space debris originally from a launch on Fri, 03 Apr 2026 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
68572, 2026-071B
Orbit
Molniya
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)
2026-04-03 (3 months ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 3 months ago

TLE from 3 months ago
0 FREGAT R/B
1 68572U 26071B   26093.32132148 -.00001541  00000-0  35052-3 0  9998
2 68572  63.0589 237.9448 7313820 284.9724  10.3188  2.01041412    15
Epoch: 2026-04-03T07:42Z
TLE epoch observation values (Epoch: 2026-04-03T07:42:42.175Z)
Latitude
0.00039°
Longitude
-69.44239°
Altitude
3,988.367 km
Speed
7.866 km/s
True Right ascension
15h 51m 33s
True Declination
0° 00' 01"
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
07:18:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,533.367 km
Perigee altitude
744.876 km
Semi-major axis
26,517.258 km
Eccentricity
0.73138
Inclination
63.0589°
RAAN
237.9448°
Arg. of periapsis
284.9724°
True anomaly
74.53178°
Mean anomaly
10.3188°
Eccentric anomaly
33.36597°
Mean motion
0.50263 °/min
Orbital period
716.23 mins
BSTAR
0.00035052
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Other satellites on launch #71 in the year 2026 (2026-04-03 UTC)

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