FREGAT R/B, 54224
Orbit data source: Space-Track
FREGAT R/B, 54224 is space debris originally from a launch on Wed, 02 Nov 2022 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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54224 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, 1.7 m
Radar Cross Section
8.354 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 FREGAT R/B
1 54224U 22145B 26167.33271496 -.00000812 00000-0 00000-0 0 9990
2 54224 63.6201 280.3405 7048068 265.7044 18.2904 2.02073863 26711Epoch: 2026-06-16T07:59Z
TLE epoch observation values (Epoch: 2026-06-16T07:59:06.572Z)
Latitude
-0.00001°
Longitude
-104.10116°
Altitude
7,688.229 km
Speed
6.45 km/s
True Right ascension
18h 41m 07s
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
21:33:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
38,674.638 km
Perigee altitude
1,422.907 km
Semi-major axis
26,426.909 km
Eccentricity
0.70481
Inclination
63.6201°
RAAN
280.3405°
Arg. of periapsis
265.7044°
True anomaly
94.62733°
Mean anomaly
18.2904°
Eccentric anomaly
48.56576°
Mean motion
0.50521 °/min
Orbital period
712.57 mins
BSTAR
0
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Other satellites on launch #145 in the year 2022 (2022-11-02 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. |
|---|---|---|---|---|---|---|---|
| 405 mins | 2026-06-22 10:31:39.252Z | 21.12° NNE | 2026-06-22 15:53:39.252Z | 61.563° ENE | 42.487° | 2026-06-22 17:16:39.252Z | 132.842° SE |
| 260 mins | 2026-06-23 06:11:39.252Z | 155.889° SSE | 2026-06-23 08:07:39.252Z | 60.06° ENE | 42.832° | 2026-06-23 10:31:39.252Z | 22.398° NNE |
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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