FREGAT R/B, 40316

Orbit data source: Space-Track

FREGAT R/B, 40316 is space debris in MEO originally from a launch on Sun, 30 Nov 2014 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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
40316, 2014-075B
Orbit
MEO
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)
2014-11-30 (11 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.7 m
Radar Cross Section
8.354 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FREGAT R/B
1 40316U 14075B   25287.05753484 -.00000024  00000-0  00000-0 0  9998
2 40316  63.5552 205.1065 0044268 135.7547 224.6248  2.08635426 82821
Epoch: 2025-10-14T01:22Z
TLE epoch observation values (Epoch: 2025-10-14T01:22:51.010Z)
Latitude
0.00005°
Longitude
161.53807°
Altitude
19,574.961 km
Speed
3.913 km/s
True Right ascension
13h 40m 24s
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
01:07:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,606.854 km
Perigee altitude
19,377.808 km
Semi-major axis
25,870.468 km
Eccentricity
0.00443
Inclination
63.5552°
RAAN
205.1065°
Arg. of periapsis
135.7547°
True anomaly
224.26986°
Mean anomaly
224.6248°
Eccentric anomaly
224.44719°
Mean motion
0.5216 °/min
Orbital period
690.19 mins
BSTAR
0
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Other satellites on launch #75 in the year 2014 (2014-11-30 UTC)

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