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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-5E
1 62083U 24219C 26186.65776307 .00000690 00000-0 11688-3 0 9993
2 62083 97.9014 345.0980 0005979 194.3506 165.7533 14.72291040 86484Epoch: 2026-07-05T15:47Z
TLE epoch observation values (Epoch: 2026-07-05T15:47:10.729Z)
Latitude
0.00001°
Longitude
-175.35065°
Altitude
660.851 km
Speed
7.525 km/s
True Right ascension
23h 00m 23s
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
10:07:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.018 km
Perigee altitude
646.612 km
Semi-major axis
7,028.952 km
Eccentricity
0.0006
Inclination
97.9014°
RAAN
345.098°
Arg. of periapsis
194.3506°
True anomaly
165.77015°
Mean anomaly
165.7533°
Eccentric anomaly
165.76173°
Mean motion
3.68305 °/min
Orbital period
97.75 mins
BSTAR
0.00011688
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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 | 2026-07-05 22:53:28.660Z | 34.727° NE | 2026-07-05 22:56:28.660Z | 83.85° E | 29.746° | 2026-07-05 23:00:28.660Z | 161.122° S |
| 5 mins | 2026-07-06 00:31:28.660Z | 326.796° NNW | 2026-07-06 00:33:28.660Z | 292.964° NW | 19.517° | 2026-07-06 00:36:28.660Z | 247.888° W |
| 6 mins | 2026-07-06 09:52:28.660Z | 121.822° SE | 2026-07-06 09:55:28.660Z | 65.728° ENE | 26.607° | 2026-07-06 09:58:28.660Z | 14.68° NNE |
| 6 mins | 2026-07-06 11:29:28.660Z | 220.295° SW | 2026-07-06 11:32:28.660Z | 273.236° WNW | 22.1° | 2026-07-06 11:35:28.660Z | 317.436° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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