FREGAT R/B, 43088

Orbit data source: Space-Track

FREGAT R/B, 43088 is space debris in GEO originally from a launch on Tue, 26 Dec 2017 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.

Not visible in the next 10 days

FREGAT R/B details

Identifier	43088, 2017-086B
Orbit	GEO
Last TLE update	17 hours ago
Origin	Lavochkin (CIS)
Manufacturer	Lavochkin
Mission	Spacecraft
Bus & Motor	FREGAT, Unknown motor
Mass	1,000 kg wet, 1,000 kg dry
Launch date (UTC)	2017-12-26 (7 years ago)
Launch vehicle	Unknown
Launch site	Tyuratam Missile And Space Complex (TTMTR)
Object type	Payload Rocket body Debris
Shape & HBR	Cyl, 3.3 m
Radar Cross Section	8.683 m²

Expand to show TLE details & history

TLE from 17 hours ago

0 FREGAT R/B
1 43088U 17086B   24360.86453031 -.00000054  00000-0  00000-0 0  9990
2 43088   6.1772  72.1092 0128872  14.5974 345.6094  0.98389984 25148

Epoch: 2024-12-25T20:44Z

Definitive object data (Epoch: 2024-12-25T20:44:55.418Z)

Latitude	-0°
Longitude	25.85474°
Altitude	35,787.078 km
Speed	3.094 km/s
True Right ascension	04h 47m 45s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-5.72795°
Longitude	-86.63965°
Altitude	36,652.473 km
Speed	3.032 km/s
Apparent Right ascension	21h 37m 47s
Apparent Declination	-10° 20' 29"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	12:56:36
Azimuth	70.169° E
Elevation	-37.098°
Doppler factor	1

Orbital elements

Apogee altitude	36,873.868 km
Perigee altitude	35,773.257 km
Semi-major axis	42,701.699 km
Eccentricity	0.0128872
Inclination	6.1772°
RAAN	72.1092°
Arg. of periapsis	14.5974°
True anomaly	345.23657°
Mean anomaly	345.6094°
Eccentric anomaly	345.42357°
Mean motion	0.24597 °/min
BSTAR	Unknown
Orbital period	1463.62 mins