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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-5E
1 62083U 24219C 25309.31389779 .00001063 00000-0 17586-3 0 9993
2 62083 97.9847 108.1320 0001206 67.9557 292.1778 14.72332928 50820Epoch: 2025-11-05T07:32Z
TLE epoch observation values (Epoch: 2025-11-05T07:32:00.769Z)
Latitude
-0.00005°
Longitude
-49.65955°
Altitude
656.319 km
Speed
7.529 km/s
True Right ascension
07h 12m 31s
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
12:11:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.533 km
Perigee altitude
649.838 km
Semi-major axis
7,028.822 km
Eccentricity
0.00012
Inclination
97.9847°
RAAN
108.132°
Arg. of periapsis
67.9557°
True anomaly
292.165°
Mean anomaly
292.1778°
Eccentric anomaly
292.1714°
Mean motion
3.68315 °/min
Orbital period
97.74 mins
BSTAR
0.00017586
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-05 22:47:37.636Z | 40.642° NE | 2025-11-05 22:50:37.636Z | 84.546° E | 23.115° | 2025-11-05 22:54:37.636Z | 150.543° SSE |
| 5 mins | 2025-11-06 00:25:37.636Z | 334.221° NNW | 2025-11-06 00:27:37.636Z | 295.973° NW | 25.158° | 2025-11-06 00:30:37.636Z | 240.934° WSW |
| 5 mins | 2025-11-06 09:47:37.636Z | 103.336° ESE | 2025-11-06 09:49:37.636Z | 68.471° E | 20.877° | 2025-11-06 09:52:37.636Z | 21.154° NNE |
| 6 mins | 2025-11-06 11:23:37.636Z | 209.632° SW | 2025-11-06 11:26:37.636Z | 273.208° WNW | 28.216° | 2025-11-06 11:29:37.636Z | 322.863° 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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