FREGAT R/B, 45609
Orbit data source: Space-Track
FREGAT R/B, 45609 is space debris originally from a launch on Fri, 22 May 2020 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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45609 intel report (Beta)
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Edit Public Description
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, 1.7 m
Radar Cross Section
8.354 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 FREGAT R/B
1 45609U 20031B 26032.98513822 -.00000899 00000-0 00000+0 0 9997
2 45609 63.5295 81.0900 7115484 258.1732 20.8232 2.01389944 41936Epoch: 2026-02-01T23:38Z
TLE epoch observation values (Epoch: 2026-02-01T23:38:35.942Z)
Latitude
0.00012°
Longitude
-45.67552°
Altitude
8,929.676 km
Speed
6.086 km/s
True Right ascension
05h 24m 38s
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
00:34:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,955.118 km
Perigee altitude
1,261.992 km
Semi-major axis
26,486.692 km
Eccentricity
0.71155
Inclination
63.5295°
RAAN
81.09°
Arg. of periapsis
258.1732°
True anomaly
101.87734°
Mean anomaly
20.8232°
Eccentric anomaly
53.6652°
Mean motion
0.5035 °/min
Orbital period
714.99 mins
BSTAR
0
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Other satellites on launch #31 in the year 2020 (2020-05-22 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. |
|---|---|---|---|---|---|---|---|
| 600 mins | 2026-02-04 23:31:45.968Z | 92.221° ESE | 2026-02-05 04:24:45.968Z | 37.828° NE | 36.701° | 2026-02-05 09:31:45.968Z | 77.023° E |
| 216 mins | 2026-02-05 15:58:45.968Z | 336.207° NNW | 2026-02-05 18:06:45.968Z | 337.92° N | 12.499° | 2026-02-05 19:34:45.968Z | 332.443° NNW |
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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