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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 KINEIS-5E
1 62083U 24219C 25260.31463598 .00000739 00000-0 12463-3 0 9999
2 62083 97.9811 60.0047 0001670 108.5248 251.6141 14.72314884 43611Epoch: 2025-09-17T07:33Z
TLE epoch observation values (Epoch: 2025-09-17T07:33:04.548Z)
Latitude
-0.00004°
Longitude
-49.7566°
Altitude
657.067 km
Speed
7.529 km/s
True Right ascension
04h 00m 01s
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
19:14:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.916 km
Perigee altitude
649.569 km
Semi-major axis
7,028.88 km
Eccentricity
0.00017
Inclination
97.9811°
RAAN
60.0047°
Arg. of periapsis
108.5248°
True anomaly
251.59594°
Mean anomaly
251.6141°
Eccentric anomaly
251.60502°
Mean motion
3.6831 °/min
Orbital period
97.74 mins
BSTAR
0.00012463
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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 | 2025-09-18 09:48:03.622Z | 111.274° ESE | 2025-09-18 09:51:03.622Z | 61.311° ENE | 20.916° | 2025-09-18 09:54:03.622Z | 17.764° NNE |
| 6 mins | 2025-09-18 11:25:03.622Z | 214.108° SW | 2025-09-18 11:27:03.622Z | 254.957° W | 28.153° | 2025-09-18 11:31:03.622Z | 325.252° NNW |
| 7 mins | 2025-09-18 23:17:03.622Z | 29.986° NE | 2025-09-18 23:20:03.622Z | 105.542° ESE | 38.151° | 2025-09-18 23:24:03.622Z | 175.951° S |
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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