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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-1E
1 60083U 24114E 25304.30246074 .00001536 00000-0 20997-3 0 9994
2 60083 98.0035 324.3448 0002296 109.3412 250.8048 14.79998899 73528Epoch: 2025-10-31T07:15Z
TLE epoch observation values (Epoch: 2025-10-31T07:15:32.607Z)
Latitude
-0.00005°
Longitude
175.6101°
Altitude
632.875 km
Speed
7.542 km/s
True Right ascension
21h 37m 22s
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
13:25:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.981 km
Perigee altitude
624.765 km
Semi-major axis
7,004.51 km
Eccentricity
0.00023
Inclination
98.0035°
RAAN
324.3448°
Arg. of periapsis
109.3412°
True anomaly
250.77995°
Mean anomaly
250.8048°
Eccentric anomaly
250.79238°
Mean motion
3.70234 °/min
Orbital period
97.24 mins
BSTAR
0.00020997
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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 | 2025-11-01 01:14:09.084Z | 152.378° SSE | 2025-11-01 01:17:09.084Z | 102.989° ESE | 40.722° | 2025-11-01 01:21:09.084Z | 355.856° N |
| 6 mins | 2025-11-01 14:40:09.084Z | 357.663° N | 2025-11-01 14:43:09.084Z | 264.022° W | 39.357° | 2025-11-01 14:46:09.084Z | 210.902° SW |
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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