UVSQ-SAT, 47438 (Decayed)
Orbit data source: Space-Track
UVSQ-SAT, 47438 was a French payload satellite in LEO that was launched on Sun, 24 Jan 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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47438 intel report (Beta)
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UVSQ-SAT radio frequencies
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 UVSQ-SAT
1 47438U 21006AB 24298.11681880 .03670113 23594-5 18855-2 0 9991
2 47438 97.2775 3.3666 0006581 273.2868 86.7668 16.20433421208899
Epoch: 2024-10-24T02:48Z
TLE epoch observation values (Epoch: 2024-10-24T02:48:13.144Z)
Latitude
-0.00006°
Longitude
-71.6932°
Altitude
221.362 km
Speed
7.774 km/s
True Right ascension
00h 13m 27s
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
19:41:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
219.542 km
Perigee altitude
210.864 km
Semi-major axis
6,593.34 km
Eccentricity
0.00066
Inclination
97.2775°
RAAN
3.3666°
Arg. of periapsis
273.2868°
True anomaly
86.8421°
Mean anomaly
86.7668°
Eccentric anomaly
86.80445°
Mean motion
4.05401 °/min
Orbital period
88.8 mins
BSTAR
0.0018855
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Other satellites on launch #6 in the year 2021 (2021-01-24 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.UVSQ-SAT 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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