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: 2 days ago
TLE from 2 days ago
0 KINEIS-5E
1 62083U 24219C 26086.48802338 .00000293 00000-0 53987-4 0 9995
2 62083 97.9358 247.7160 0005534 117.3564 242.8208 14.72335915 71748Epoch: 2026-03-27T11:42Z
TLE epoch observation values (Epoch: 2026-03-27T11:42:45.220Z)
Latitude
0.00007°
Longitude
-112.89433°
Altitude
658.41 km
Speed
7.527 km/s
True Right ascension
16h 30m 51s
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
04:23:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.563 km
Perigee altitude
646.784 km
Semi-major axis
7,028.811 km
Eccentricity
0.00055
Inclination
97.9358°
RAAN
247.716°
Arg. of periapsis
117.3564°
True anomaly
242.7644°
Mean anomaly
242.8208°
Eccentric anomaly
242.7926°
Mean motion
3.68316 °/min
Orbital period
97.74 mins
BSTAR
0.000053987
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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 | 2026-03-29 23:00:31.140Z | 33.375° NE | 2026-03-29 23:04:31.140Z | 113.174° SE | 30.513° | 2026-03-29 23:07:31.140Z | 162.017° S |
| 5 mins | 2026-03-30 00:38:31.140Z | 327.081° NNW | 2026-03-30 00:40:31.140Z | 294.168° NW | 18.864° | 2026-03-30 00:43:31.140Z | 249.385° W |
| 6 mins | 2026-03-30 09:59:31.140Z | 123.923° SE | 2026-03-30 10:02:31.140Z | 67.568° E | 27.407° | 2026-03-30 10:05:31.140Z | 14.331° NNE |
| 5 mins | 2026-03-30 11:37:31.140Z | 233.635° WSW | 2026-03-30 11:39:31.140Z | 271.491° WNW | 21.218° | 2026-03-30 11:42:31.140Z | 315.985° 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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