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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-5E
1 62083U 24219C 25339.28458142 .00001657 00000-0 26963-3 0 9991
2 62083 97.9855 137.5792 0000775 107.2333 252.8959 14.72350023 55238Epoch: 2025-12-05T06:49Z
TLE epoch observation values (Epoch: 2025-12-05T06:49:47.834Z)
Latitude
-0.00007°
Longitude
-39.19897°
Altitude
656.745 km
Speed
7.529 km/s
True Right ascension
09h 10m 19s
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
15:22:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.176 km
Perigee altitude
650.086 km
Semi-major axis
7,028.768 km
Eccentricity
0.00008
Inclination
97.9855°
RAAN
137.5792°
Arg. of periapsis
107.2333°
True anomaly
252.88741°
Mean anomaly
252.8959°
Eccentric anomaly
252.89166°
Mean motion
3.68319 °/min
Orbital period
97.74 mins
BSTAR
0.00026963
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Other satellites on launch #219 in the year 2024 (2024-11-25 UTC)
Did you know?
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 | 2025-12-05 23:42:29.467Z | 9.165° NNE | 2025-12-05 23:46:29.467Z | 246.307° WSW | 44.023° | 2025-12-05 23:50:29.467Z | 198.815° SSW |
| 7 mins | 2025-12-06 10:41:29.467Z | 163.788° S | 2025-12-06 10:44:29.467Z | 42.678° NE | 44.881° | 2025-12-06 10:48:29.467Z | 348.538° N |
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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