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: 4 hours ago
TLE from 4 hours ago
0 KINEIS-5E
1 62083U 24219C 26315.30930677 .00000722 00000-0 12179-3 0 9993
2 62083 97.9150 110.2710 0007078 146.1239 214.0422 14.72347894105417Epoch: 2026-11-11T07:25Z
TLE epoch observation values (Epoch: 2026-11-11T07:25:24.104Z)
Latitude
-0.00005°
Longitude
-51.53843°
Altitude
660.719 km
Speed
7.525 km/s
True Right ascension
07h 21m 05s
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
07:17:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.609 km
Perigee altitude
645.659 km
Semi-major axis
7,028.771 km
Eccentricity
0.00071
Inclination
97.915°
RAAN
110.271°
Arg. of periapsis
146.1239°
True anomaly
213.99683°
Mean anomaly
214.0422°
Eccentric anomaly
214.01951°
Mean motion
3.68319 °/min
Orbital period
97.74 mins
BSTAR
0.00012179
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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 | 2026-11-11 22:41:34.939Z | 42.463° NE | 2026-11-11 22:44:34.939Z | 99.582° ESE | 30.974° | 2026-11-11 22:47:34.939Z | 152.891° SSE |
| 6 mins | 2026-11-12 00:18:34.939Z | 334.897° NNW | 2026-11-12 00:21:34.939Z | 281.916° WNW | 23.171° | 2026-11-12 00:24:34.939Z | 239.946° WSW |
| 6 mins | 2026-11-12 09:40:34.939Z | 111.505° ESE | 2026-11-12 09:42:34.939Z | 75.905° E | 26.18° | 2026-11-12 09:46:34.939Z | 12.754° NNE |
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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