FREGAT R/B, 43509

Orbit data source: Space-Track

FREGAT R/B, 43509 is space debris in MEO originally from a launch on Sat, 16 Jun 2018 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
43509, 2018-053B
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)
2018-06-16 (8 years ago)
Launch vehicle
Unknown
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.8 m
Radar Cross Section
8.354 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FREGAT R/B
1 43509U 18053B   26277.29299493  .00000050  00000-0  00000-0 0  9994
2 43509  65.6538  74.5609 0099304  88.1946 272.9603  2.09215489 63422
Epoch: 2026-10-04T07:01Z
TLE epoch observation values (Epoch: 2026-10-04T07:01:54.761Z)
Latitude
0.00003°
Longitude
-43.91846°
Altitude
19,434.896 km
Speed
3.93 km/s
True Right ascension
04h 58m 11s
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
01:25:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,700.845 km
Perigee altitude
19,187.988 km
Semi-major axis
25,822.554 km
Eccentricity
0.00993
Inclination
65.6538°
RAAN
74.5609°
Arg. of periapsis
88.1946°
True anomaly
271.82322°
Mean anomaly
272.9603°
Eccentric anomaly
272.39183°
Mean motion
0.52305 °/min
Orbital period
688.27 mins
BSTAR
0
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Other satellites on launch #53 in the year 2018 (2018-06-16 UTC)

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