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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-5E
1 62083U 24219C 26268.62004709 .00000479 00000-0 83450-4 0 9993
2 62083 97.9119 64.8105 0005261 312.7540 47.3224 14.72297818 98544Epoch: 2026-09-25T14:52Z
TLE epoch observation values (Epoch: 2026-09-25T14:52:52.068Z)
Latitude
-0.00008°
Longitude
-162.84629°
Altitude
654.245 km
Speed
7.532 km/s
True Right ascension
04h 19m 14s
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
16:50:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.492 km
Perigee altitude
647.096 km
Semi-major axis
7,028.931 km
Eccentricity
0.00053
Inclination
97.9119°
RAAN
64.8105°
Arg. of periapsis
312.754°
True anomaly
47.36674°
Mean anomaly
47.3224°
Eccentric anomaly
47.34457°
Mean motion
3.68306 °/min
Orbital period
97.74 mins
BSTAR
0.00008345
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-25 23:36:22.779Z | 5.463° NNE | 2026-09-25 23:40:22.779Z | 252.703° W | 64.291° | 2026-09-25 23:44:22.779Z | 203.095° SW |
| 7 mins | 2026-09-26 10:35:22.779Z | 169.71° S | 2026-09-26 10:38:22.779Z | 317.056° NNW | 78.945° | 2026-09-26 10:42:22.779Z | 346.094° N |
| 5 mins | 2026-09-26 22:28:22.779Z | 55.252° ENE | 2026-09-26 22:30:22.779Z | 87.355° E | 21.394° | 2026-09-26 22:33:22.779Z | 136.535° SSE |
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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