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, 0.8 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 25261.30106368 .00000920 00000-0 12911-3 0 9990
2 60083 98.0078 281.4853 0000488 92.3395 267.7872 14.79832928 67165Epoch: 2025-09-18T07:13Z
TLE epoch observation values (Epoch: 2025-09-18T07:13:31.901Z)
Latitude
-0.00009°
Longitude
175.63776°
Altitude
632.883 km
Speed
7.542 km/s
True Right ascension
18h 45m 56s
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
06:32:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.239 km
Perigee altitude
626.556 km
Semi-major axis
7,005.034 km
Eccentricity
0.00005
Inclination
98.0078°
RAAN
281.4853°
Arg. of periapsis
92.3395°
True anomaly
267.78161°
Mean anomaly
267.7872°
Eccentric anomaly
267.78441°
Mean motion
3.70193 °/min
Orbital period
97.25 mins
BSTAR
0.00012911
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-18 14:16:59.137Z | 14.342° NNE | 2025-09-18 14:20:59.137Z | 161.177° S | 44.471° | 2025-09-18 14:24:59.137Z | 191.655° SSW |
| 6 mins | 2025-09-19 01:12:59.137Z | 149.383° SSE | 2025-09-19 01:15:59.137Z | 48.523° ENE | 40.923° | 2025-09-19 01:18:59.137Z | 356.681° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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