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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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: 3 days ago
TLE from 3 days ago
0 KINEIS-1E
1 60083U 24114E 26086.59644626 .00000317 00000-0 48266-4 0 9994
2 60083 97.9711 111.0440 0002475 98.8882 261.2610 14.80538337 95313Epoch: 2026-03-27T14:18Z
TLE epoch observation values (Epoch: 2026-03-27T14:18:52.956Z)
Latitude
-0.00007°
Longitude
71.29459°
Altitude
630.909 km
Speed
7.543 km/s
True Right ascension
07h 24m 10s
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
03:39:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.402 km
Perigee altitude
622.936 km
Semi-major axis
7,002.806 km
Eccentricity
0.00025
Inclination
97.9711°
RAAN
111.044°
Arg. of periapsis
98.8882°
True anomaly
261.23297°
Mean anomaly
261.261°
Eccentric anomaly
261.24698°
Mean motion
3.70369 °/min
Orbital period
97.2 mins
BSTAR
0.000048266
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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 | 2026-03-31 01:10:14.147Z | 142.014° SSE | 2026-03-31 01:13:14.147Z | 83.625° E | 36.1° | 2026-03-31 01:17:14.147Z | 0.993° NNE |
| 7 mins | 2026-03-31 14:35:14.147Z | 7.706° NNE | 2026-03-31 14:38:14.147Z | 313.777° NW | 43.818° | 2026-03-31 14:42:14.147Z | 200.09° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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