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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-5E
1 62083U 24219C 25302.51781959 .00001242 00000-0 20420-3 0 9994
2 62083 97.9845 101.4554 0001394 69.8143 290.3214 14.72316346 49822Epoch: 2025-10-29T12:25Z
TLE epoch observation values (Epoch: 2025-10-29T12:25:39.612Z)
Latitude
-0.00006°
Longitude
-123.04946°
Altitude
656.351 km
Speed
7.529 km/s
True Right ascension
06h 45m 49s
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
17:50:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.718 km
Perigee altitude
649.758 km
Semi-major axis
7,028.875 km
Eccentricity
0.00014
Inclination
97.9845°
RAAN
101.4554°
Arg. of periapsis
69.8143°
True anomaly
290.30642°
Mean anomaly
290.3214°
Eccentric anomaly
290.31391°
Mean motion
3.68311 °/min
Orbital period
97.74 mins
BSTAR
0.0002042
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-29 22:47:58.246Z | 43.062° NE | 2025-10-29 22:50:58.246Z | 90.736° ESE | 23.432° | 2025-10-29 22:53:58.246Z | 143.822° SSE |
| 5 mins | 2025-10-30 00:25:58.246Z | 330.41° NNW | 2025-10-30 00:27:58.246Z | 289.205° WNW | 25.24° | 2025-10-30 00:30:58.246Z | 238.259° WSW |
| 5 mins | 2025-10-30 09:47:58.246Z | 99.569° ESE | 2025-10-30 09:49:58.246Z | 63.013° ENE | 20.809° | 2025-10-30 09:52:58.246Z | 18.638° NNE |
| 6 mins | 2025-10-30 11:23:58.246Z | 212.725° SW | 2025-10-30 11:25:58.246Z | 252.558° W | 28.228° | 2025-10-30 11:29:58.246Z | 324.878° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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