FREGAT R/B, 40130

Orbit data source: Space-Track

FREGAT R/B, 40130 is space debris in HEO originally from a launch on Fri, 22 Aug 2014 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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FREGAT R/B details

Identifier	40130, 2014-050C
Orbit	HEO
Last TLE update	1 day ago
Origin	Lavochkin (CIS)
Manufacturer	Lavochkin
Mission	Spacecraft
Bus & Motor	FREGAT, Unknown motor
Mass	1,050 kg wet, 1,050 kg dry
Launch date (UTC)	2014-08-22 (10 years ago)
Launch vehicle	Unknown
Launch site	French Guiana (FRGUI)
Object type	Payload Rocket body Debris
Shape & HBR	Irr, 3.3 m
Radar Cross Section	11.055 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 FREGAT R/B
1 40130U 14050C   25045.25703974  .00000015  00000-0  00000-0 0  9997
2 40130  48.7251 242.7402 2553234 203.5173 142.3871  2.05031305 78519

Epoch: 2025-02-14T06:10Z

Definitive object data (Epoch: 2025-02-14T06:10:08.233Z)

Latitude	-0°
Longitude	5.6911°
Altitude	25,563.894 km
Speed	3.119 km/s
True Right ascension	16h 10m 59s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	47.69916°
Longitude	80.26335°
Altitude	22,156.361 km
Speed	3.566 km/s
Apparent Right ascension	21h 44m 32s
Apparent Declination	36° 36' 22"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	12:12:20
Azimuth	29.043° NE
Elevation	-6.281°
Doppler factor	1

Orbital elements

Apogee altitude	26,477.937 km
Perigee altitude	13,112.577 km
Semi-major axis	26,173.394 km
Eccentricity	0.2553234
Inclination	48.7251°
RAAN	242.7402°
Arg. of periapsis	203.5173°
True anomaly	156.48492°
Mean anomaly	142.3871°
Eccentric anomaly	149.75556°
Mean motion	0.51257 °/min
BSTAR	Unknown
Orbital period	702.34 mins