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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-5E
1 62083U 24219C 26304.50363016 .00000360 00000-0 64552-4 0 9991
2 62083 97.9145 99.7473 0006377 178.3777 181.7452 14.72333860103827Epoch: 2026-10-31T12:05Z
TLE epoch observation values (Epoch: 2026-10-31T12:05:13.645Z)
Latitude
-0.00009°
Longitude
-121.36796°
Altitude
661.121 km
Speed
7.524 km/s
True Right ascension
06h 38m 59s
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
15:04:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.161 km
Perigee altitude
646.197 km
Semi-major axis
7,028.816 km
Eccentricity
0.00064
Inclination
97.9145°
RAAN
99.7473°
Arg. of periapsis
178.3777°
True anomaly
181.74298°
Mean anomaly
181.7452°
Eccentric anomaly
181.74409°
Mean motion
3.68315 °/min
Orbital period
97.74 mins
BSTAR
0.000064552
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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 | 2026-10-31 22:27:24.466Z | 43.636° NE | 2026-10-31 22:30:24.466Z | 86.338° E | 21.966° | 2026-10-31 22:33:24.466Z | 137.145° SSE |
| 6 mins | 2026-11-01 00:05:24.466Z | 337.103° NNW | 2026-11-01 00:07:24.466Z | 295.787° NW | 32.318° | 2026-11-01 00:11:24.466Z | 228.137° WSW |
| 5 mins | 2026-11-01 09:27:24.466Z | 98.959° ESE | 2026-11-01 09:29:24.466Z | 66.848° ENE | 19.507° | 2026-11-01 09:32:24.466Z | 23.041° NE |
| 6 mins | 2026-11-01 11:03:24.466Z | 204.598° SW | 2026-11-01 11:06:24.466Z | 278.01° WNW | 38.238° | 2026-11-01 11:09:24.466Z | 327.279° 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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