FREGAT R/B, 41555

Orbit data source: Space-Track

FREGAT R/B, 41555 is space debris in MEO originally from a launch on Sun, 29 May 2016 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
41555, 2016-032B
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)
2016-05-29 (10 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: 4 days ago

TLE from 4 days ago
0 FREGAT R/B
1 41555U 16032B   26293.35904519  .00000000  00000-0  00000-0 0  9990
2 41555  63.7015 193.0085 0080590 117.6144 243.2615  2.08091454 79008
Epoch: 2026-10-20T08:37Z
TLE epoch observation values (Epoch: 2026-10-20T08:37:01.504Z)
Latitude
-0.00002°
Longitude
34.92703°
Altitude
19,633.658 km
Speed
3.907 km/s
True Right ascension
12h 52m 01s
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
09:39:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,746.246 km
Perigee altitude
19,328.539 km
Semi-major axis
25,915.53 km
Eccentricity
0.00806
Inclination
63.7015°
RAAN
193.0085°
Arg. of periapsis
117.6144°
True anomaly
242.44051°
Mean anomaly
243.2615°
Eccentric anomaly
242.85063°
Mean motion
0.52024 °/min
Orbital period
691.99 mins
BSTAR
0
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Other satellites on launch #32 in the year 2016 (2016-05-29 UTC)

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