FREGAT R/B, 43509
Orbit data source: Space-Track
FREGAT R/B, 43509 is space debris in MEO originally from a launch on Sat, 16 Jun 2018 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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43509 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: 2 days ago
TLE from 2 days ago
0 FREGAT R/B
1 43509U 18053B 26096.13910918 .00000016 00000-0 00000-0 0 9990
2 43509 65.5521 80.3453 0095889 89.2884 271.7996 2.09215771 59636Epoch: 2026-04-06T03:20Z
TLE epoch observation values (Epoch: 2026-04-06T03:20:19.033Z)
Latitude
0.00009°
Longitude
-164.18439°
Altitude
19,439.993 km
Speed
3.93 km/s
True Right ascension
05h 21m 19s
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
10:58:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,692.007 km
Perigee altitude
19,196.787 km
Semi-major axis
25,822.534 km
Eccentricity
0.00959
Inclination
65.5521°
RAAN
80.3453°
Arg. of periapsis
89.2884°
True anomaly
270.70099°
Mean anomaly
271.7996°
Eccentric anomaly
271.25033°
Mean motion
0.52305 °/min
Orbital period
688.27 mins
BSTAR
0
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Other satellites on launch #53 in the year 2018 (2018-06-16 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. |
|---|---|---|---|---|---|---|---|
| 100 mins | 2026-04-08 04:52:57.611Z | 48.996° ENE | 2026-04-08 04:52:57.611Z | 48.996° ENE | 32.437° | 2026-04-08 06:32:57.611Z | 97.97° ESE |
| 330 mins | 2026-04-08 23:18:57.611Z | 193.417° SSW | 2026-04-09 01:42:57.611Z | 294.893° NW | 44.258° | 2026-04-09 04:48:57.611Z | 71.82° E |
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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