FREGAT R/B, 42940

Orbit data source: Space-Track

FREGAT R/B, 42940 is space debris in MEO originally from a launch on Fri, 22 Sep 2017 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
42940, 2017-055B
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)
2017-09-22 (9 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: 5 days ago

TLE from 5 days ago
0 FREGAT R/B
1 42940U 17055B   26168.48372680  .00000061  00000-0  00000-0 0  9995
2 42940  63.9588 197.6079 0085591 131.7686 229.0274  2.07651938 65715
Epoch: 2026-06-17T11:36Z
TLE epoch observation values (Epoch: 2026-06-17T11:36:33.995Z)
Latitude
-0.00005°
Longitude
117.73041°
Altitude
19,721.568 km
Speed
3.897 km/s
True Right ascension
13h 10m 27s
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
21:25:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,796.067 km
Perigee altitude
19,351.814 km
Semi-major axis
25,952.077 km
Eccentricity
0.00856
Inclination
63.9588°
RAAN
197.6079°
Arg. of periapsis
131.7686°
True anomaly
228.29205°
Mean anomaly
229.0274°
Eccentric anomaly
228.65921°
Mean motion
0.51914 °/min
Orbital period
693.45 mins
BSTAR
0
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Other satellites on launch #55 in the year 2017 (2017-09-22 UTC)

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