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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-1E
1 60083U 24114E 25308.49417900 .00001254 00000-0 17266-3 0 9998
2 60083 98.0030 328.5215 0002378 103.6629 256.4847 14.80011270 74148Epoch: 2025-11-04T11:51Z
TLE epoch observation values (Epoch: 2025-11-04T11:51:37.065Z)
Latitude
-0.00008°
Longitude
106.63668°
Altitude
632.697 km
Speed
7.542 km/s
True Right ascension
21h 54m 05s
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
14:07:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628 km
Perigee altitude
624.668 km
Semi-major axis
7,004.471 km
Eccentricity
0.00024
Inclination
98.003°
RAAN
328.5215°
Arg. of periapsis
103.6629°
True anomaly
256.45821°
Mean anomaly
256.4847°
Eccentric anomaly
256.47145°
Mean motion
3.70237 °/min
Orbital period
97.23 mins
BSTAR
0.00017266
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-05 00:58:06.279Z | 139.577° SSE | 2025-11-05 01:02:06.279Z | 59.331° ENE | 32.901° | 2025-11-05 01:05:06.279Z | 6.178° NNE |
| 7 mins | 2025-11-05 14:24:06.279Z | 11.717° NNE | 2025-11-05 14:27:06.279Z | 227.281° WSW | 44.884° | 2025-11-05 14:31:06.279Z | 195.084° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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