FREGAT R/B, 43088
Orbit data source: Space-Track
FREGAT R/B, 43088 is space debris in GEO originally from a launch on Tue, 26 Dec 2017 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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43088 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
2 days ago
Origin
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, 3.3 m
Radar Cross Section
8.683 m²
Expand to show TLE details & history
TLE from 2 days ago
0 FREGAT R/B
1 43088U 17086B 25183.90009515 -.00000186 00000-0 00000-0 0 9999
2 43088 6.6576 70.1329 0130040 19.1762 341.2158 0.98391286 27000Epoch: 2025-07-02T21:36Z
TLE epoch observation values (Epoch: 2025-07-02T21:36:08.22Z)
Latitude
-0.00001°
Longitude
-175.16485°
Altitude
35,794.912 km
Speed
3.093 km/s
True Right ascension
04h 40m 10s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
0.26203°
Longitude
2.56758°
Altitude
36,838.707 km
Speed
3.019 km/s
Apparent Right ascension
16h 05m 08s
Apparent Declination
-5° 11' 54"
Sunlit
Visualization observer readout
Local Sidereal Time
21:48:03
Azimuth
263.277° W
Elevation
-0.072°
Doppler factor
1
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43088 neighbors
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Other satellites on launch #86 in the year 2017 (2017-12-26 UTC)
FREGAT R/B Visibility
Observer location: undefined°, undefined°
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. |
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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