KINEIS-5E, 62083
Orbit data source: Space-Track
KINEIS-5E, 62083 is a French payload satellite in SSO that was launched on Mon, 25 Nov 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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62083 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
KINEIS
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
28 kg wet, 28 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Ant, 1.0 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 KINEIS-5E
1 62083U 24219C 26133.65358141 .00000371 00000-0 66394-4 0 9998
2 62083 97.8965 293.5847 0006854 29.6134 330.5460 14.72272986 78689Epoch: 2026-05-13T15:41Z
TLE epoch observation values (Epoch: 2026-05-13T15:41:09.433Z)
Latitude
-0.00011°
Longitude
-173.1151°
Altitude
652.635 km
Speed
7.534 km/s
True Right ascension
19h 34m 20s
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
19:02:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.69 km
Perigee altitude
646.055 km
Semi-major axis
7,029.009 km
Eccentricity
0.00069
Inclination
97.8965°
RAAN
293.5847°
Arg. of periapsis
29.6134°
True anomaly
330.50735°
Mean anomaly
330.546°
Eccentric anomaly
330.52668°
Mean motion
3.683 °/min
Orbital period
97.75 mins
BSTAR
0.000066394
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Other satellites on launch #219 in the year 2024 (2024-11-25 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.KINEIS-5E 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-15 11:52:01.725Z | 239.372° WSW | 2026-05-15 11:54:01.725Z | 268.496° W | 14.686° | 2026-05-15 11:56:01.725Z | 297.411° NW |
| 8 mins | 2026-05-15 23:42:01.725Z | 7.231° NNE | 2026-05-15 23:46:01.725Z | 318.852° NNW | 42.238° | 2026-05-15 23:50:01.725Z | 203.848° SW |
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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