FREGAT R/B, 41106

Orbit data source: Space-Track

FREGAT R/B, 41106 is space debris in GEO originally from a launch on Fri, 11 Dec 2015 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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FREGAT R/B details

Identifier	41106, 2015-074B
Orbit	GEO
Last TLE update	10 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)	2015-12-11 (9 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 10 hours ago

0 FREGAT R/B
1 41106U 15074B   24361.12300798 -.00000199  00000-0  00000-0 0  9995
2 41106   6.8532  68.0005 0195129 344.0386  15.2340  1.02895063 33973

Epoch: 2024-12-26T02:57Z

Definitive object data (Epoch: 2024-12-26T02:57:07.889Z)

Latitude	-0.00001°
Longitude	-71.52726°
Altitude	34,285.368 km
Speed	3.16 km/s
True Right ascension	04h 31m 27s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	3.25336°
Longitude	80.32515°
Altitude	35,854.892 km
Speed	3.043 km/s
Apparent Right ascension	14h 56m 41s
Apparent Declination	-2° 30' 00"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	12:08:40
Azimuth	127.329° SE
Elevation	32.78°
Doppler factor	1

Orbital elements

Apogee altitude	35,876.662 km
Perigee altitude	34,259.197 km
Semi-major axis	41,446.067 km
Eccentricity	0.0195129
Inclination	6.8532°
RAAN	68.0005°
Arg. of periapsis	344.0386°
True anomaly	15.83567°
Mean anomaly	15.234°
Eccentric anomaly	15.5334°
Mean motion	0.25723 °/min
BSTAR	Unknown
Orbital period	1399.54 mins