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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-5E
1 62083U 24219C 26045.30374477 .00000966 00000-0 16070-3 0 9997
2 62083 97.9856 207.3754 0001482 97.2606 262.8770 14.72274513 65681Epoch: 2026-02-14T07:17Z
TLE epoch observation values (Epoch: 2026-02-14T07:17:23.548Z)
Latitude
0°
Longitude
-46.30145°
Altitude
656.954 km
Speed
7.529 km/s
True Right ascension
13h 49m 30s
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
14:36:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.913 km
Perigee altitude
649.83 km
Semi-major axis
7,029.008 km
Eccentricity
0.00015
Inclination
97.9856°
RAAN
207.3754°
Arg. of periapsis
97.2606°
True anomaly
262.86015°
Mean anomaly
262.877°
Eccentric anomaly
262.86857°
Mean motion
3.683 °/min
Orbital period
97.75 mins
BSTAR
0.0001607
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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 | 2026-02-14 22:33:34.627Z | 49.651° ENE | 2026-02-14 22:36:34.627Z | 93.215° ESE | 17.901° | 2026-02-14 22:39:34.627Z | 136.976° SSE |
| 7 mins | 2026-02-15 00:10:34.627Z | 348.381° N | 2026-02-15 00:13:34.627Z | 285.718° WNW | 31.699° | 2026-02-15 00:17:34.627Z | 221.423° SW |
| 7 mins | 2026-02-15 11:08:34.627Z | 192.431° SSW | 2026-02-15 11:11:34.627Z | 250.945° W | 35.511° | 2026-02-15 11:15:34.627Z | 332.278° NNW |
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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