FREGAT R/B, 41943 (Decayed)
Orbit data source: Space-Track
FREGAT R/B, 41943 was space debris in LEO originally from a launch on Sat, 28 Jan 2017 UTC launched from the French Guiana (FRGUI). 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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41943 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Lavochkin
Mission
Decayed spacecraft
Bus & Motor
FREGAT, Unknown motor
Mass
1,050 kg wet, 1,050 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Irr, 1.6 m
Radar Cross Section
11.055 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 FREGAT R/B
1 41943U 17006B 24177.00033565 .00009157 -28936-4 00000+0 0 9992
2 41943 5.2036 315.6612 0546908 194.0633 342.7898 15.24445037 96473Epoch: 2024-06-25T00:00Z
TLE epoch observation values (Epoch: 2024-06-25T00:00:29Z)
Latitude
0.46635°
Longitude
-143.18414°
Altitude
132.424 km
Speed
8.03 km/s
True Right ascension
08h 42m 15s
True Declination
0° 27' 48"
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
01:43:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
874.927 km
Perigee altitude
122.714 km
Semi-major axis
6,876.958 km
Eccentricity
0.05469
Inclination
5.2036°
RAAN
315.6612°
Arg. of periapsis
194.0633°
True anomaly
340.80674°
Mean anomaly
342.7898°
Eccentric anomaly
341.81169°
Mean motion
3.80582 °/min
Orbital period
94.59 mins
BSTAR
0
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Other satellites on launch #6 in the year 2017 (2017-01-28 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
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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