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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41555 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,000 kg wet, 1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.8 m
Radar Cross Section
8.354 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 FREGAT R/B
1 41555U 16032B 26258.27829585 .00000023 00000-0 00000-0 0 9996
2 41555 63.7040 194.1530 0080536 117.9995 242.8186 2.08091457 78279Epoch: 2026-09-15T06:40Z
TLE epoch observation values (Epoch: 2026-09-15T06:40:44.761Z)
Latitude
-0°
Longitude
99.71603°
Altitude
19,634.891 km
Speed
3.907 km/s
True Right ascension
12h 56m 35s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:35:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,746.106 km
Perigee altitude
19,328.679 km
Semi-major axis
25,915.529 km
Eccentricity
0.00805
Inclination
63.704°
RAAN
194.153°
Arg. of periapsis
117.9995°
True anomaly
242.00143°
Mean anomaly
242.8186°
Eccentric anomaly
242.40964°
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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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FREGAT R/B Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 250 mins | 2026-10-14 04:54:36.994Z | 325.653° NNW | 2026-10-14 07:00:36.994Z | 277.128° WNW | 57.001° | 2026-10-14 09:04:36.994Z | 212.26° SW |
| 172 mins | 2026-10-14 14:22:36.994Z | 105.446° ESE | 2026-10-14 15:50:36.994Z | 62.269° ENE | 29.764° | 2026-10-14 17:14:36.994Z | 25.939° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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