KINEIS-1E, 60083
Orbit data source: Space-Track
KINEIS-1E, 60083 is a French payload satellite in SSO that was launched on Thu, 20 Jun 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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60083 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-1E
1 60083U 24114E 25364.60483568 .00001691 00000-0 22943-3 0 9999
2 60083 97.9979 24.4175 0000621 42.2600 317.8659 14.80200805 82440Epoch: 2025-12-30T14:30Z
TLE epoch observation values (Epoch: 2025-12-30T14:30:57.802Z)
Latitude
-0.00009°
Longitude
67.39095°
Altitude
631.386 km
Speed
7.543 km/s
True Right ascension
01h 37m 40s
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
21:43:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.17 km
Perigee altitude
625.3 km
Semi-major axis
7,003.872 km
Eccentricity
0.00006
Inclination
97.9979°
RAAN
24.4175°
Arg. of periapsis
42.26°
True anomaly
317.86113°
Mean anomaly
317.8659°
Eccentric anomaly
317.86351°
Mean motion
3.70285 °/min
Orbital period
97.22 mins
BSTAR
0.00022943
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Other satellites on launch #114 in the year 2024 (2024-06-20 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-1E 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-31 00:24:42.400Z | 101.022° ESE | 2025-12-31 00:26:42.400Z | 71.262° E | 16.443° | 2025-12-31 00:29:42.400Z | 26.313° NE |
| 6 mins | 2025-12-31 02:00:42.400Z | 203.769° SW | 2025-12-31 02:02:42.400Z | 251.246° W | 33.385° | 2025-12-31 02:06:42.400Z | 330.762° NNW |
| 6 mins | 2025-12-31 13:49:42.400Z | 48.191° ENE | 2025-12-31 13:51:42.400Z | 93.969° ESE | 29.558° | 2025-12-31 13:55:42.400Z | 163.281° S |
| 5 mins | 2025-12-31 15:25:42.400Z | 329.317° NNW | 2025-12-31 15:27:42.400Z | 296.029° NW | 19.154° | 2025-12-31 15:30:42.400Z | 248.939° W |
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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