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: 8 hours ago
TLE from 8 hours ago
0 KINEIS-5E
1 62083U 24219C 25295.17796413 .00001496 00000-0 24448-3 0 9993
2 62083 97.9840 94.2452 0001573 75.8406 284.2976 14.72296641 48743Epoch: 2025-10-22T04:16Z
TLE epoch observation values (Epoch: 2025-10-22T04:16:16.100Z)
Latitude
-0.00006°
Longitude
-0.67718°
Altitude
656.481 km
Speed
7.529 km/s
True Right ascension
06h 16m 58s
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
07:32:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.906 km
Perigee altitude
649.695 km
Semi-major axis
7,028.938 km
Eccentricity
0.00016
Inclination
97.984°
RAAN
94.2452°
Arg. of periapsis
75.8406°
True anomaly
284.28013°
Mean anomaly
284.2976°
Eccentric anomaly
284.28887°
Mean motion
3.68306 °/min
Orbital period
97.74 mins
BSTAR
0.00024448
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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 | 2025-10-22 22:48:05.270Z | 44.757° NE | 2025-10-22 22:51:05.270Z | 94.65° ESE | 23.438° | 2025-10-22 22:54:05.270Z | 145.503° SSE |
| 6 mins | 2025-10-23 00:25:05.270Z | 340.668° N | 2025-10-23 00:28:05.270Z | 285.001° WNW | 25.195° | 2025-10-23 00:31:05.270Z | 236.659° WSW |
| 5 mins | 2025-10-23 09:48:05.270Z | 97.06° ESE | 2025-10-23 09:50:05.270Z | 59.744° ENE | 20.616° | 2025-10-23 09:53:05.270Z | 17.27° NNE |
| 6 mins | 2025-10-23 11:24:05.270Z | 214.694° SW | 2025-10-23 11:26:05.270Z | 257.106° W | 28.524° | 2025-10-23 11:30:05.270Z | 326.06° 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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