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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Identifier
41106, 2015-074B
Orbit
GEO
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)
2015-12-11 (11 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.9 m
Radar Cross Section
8.683 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 FREGAT R/B
1 41106U 15074B   26272.49931742 -.00000174  00000-0  00000+0 0  9999
2 41106   8.3647  60.5889 0197932   1.9104 358.2373  1.02894842 40580
Epoch: 2026-09-29T11:59Z
TLE epoch observation values (Epoch: 2026-09-29T11:59:01.025Z)
Latitude
-0.00001°
Longitude
-127.37851°
Altitude
34,247.5 km
Speed
3.163 km/s
True Right ascension
04h 02m 33s
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
23:54:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,888.329 km
Perigee altitude
34,247.627 km
Semi-major axis
41,446.115 km
Eccentricity
0.01979
Inclination
8.3647°
RAAN
60.5889°
Arg. of periapsis
1.9104°
True anomaly
358.16576°
Mean anomaly
358.2373°
Eccentric anomaly
358.20171°
Mean motion
0.25723 °/min
Orbital period
1,399.54 mins
BSTAR
0
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