FREGAT R/B, 41176

Orbit data source: Space-Track

FREGAT R/B, 41176 is space debris originally from a launch on Thu, 17 Dec 2015 UTC launched from the French Guiana (FRGUI). 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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Last TLE update5 days ago
ManufacturerLavochkin
MissionSpacecraft
Bus & MotorFREGAT, Unknown motor
Mass1,050 kg wet, 1,050 kg dry
Shape & HBRIrr, 3.3 m
Radar Cross Section11.055 m², Large (>1 m²)

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TLE from 5 days ago
0 FREGAT R/B
1 41176U 15079C   25077.22566462  .00000033  00000-0  00000-0 0  9991
2 41176  55.5069 117.2920 0013577 249.6388 110.2953  1.67560995 56613
Epoch: 2025-03-18T05:24Z
Definitive object data (Epoch: 2025-03-18T05:24:57.423Z)
Latitude-0.00002°
Longitude-139.96948°
Altitude23,578.639 km
Speed3.647 km/s
True Right ascension07h 49m 12s
True Declination0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude34.36897°
Longitude-112.10299°
Altitude23,603.319 km
Speed3.645 km/s
Apparent Right ascension10h 16m 55s
Apparent Declination30° 51' 30"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time06:45:52
Azimuth84.976° E
Elevation46.68°
Doppler factor1
Orbital elements
Apogee altitude23,604.903 km
Perigee altitude23,523.597 km
Semi-major axis29,942.387 km
Eccentricity0.0013577
Inclination55.5069°
RAAN117.292°
Arg. of periapsis249.6388°
True anomaly110.44114°
Mean anomaly110.2953°
Eccentric anomaly110.36823°
Mean motion0.4189 °/min
BSTARUnknown
Orbital period859.39 mins
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Other satellites on launch #79 in the year 2015 (2015-12-17 UTC)

FREGAT R/B Visibility forecast

Observer location: undefined°, undefined°

Span
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
170 mins2025-03-23 01:43:07.237Z85.011° E2025-03-23 01:53:07.237Z79.56° E36.144°2025-03-23 04:33:07.237Z44.333° NE
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