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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-1E
1 60083U 24114E 25352.97759242 .00000711 00000-0 10051-3 0 9990
2 60083 97.9986 12.8364 0001279 45.2720 314.8596 14.80171082 80725Epoch: 2025-12-18T23:27Z
TLE epoch observation values (Epoch: 2025-12-18T23:27:43.985Z)
Latitude
0.00003°
Longitude
-66.92223°
Altitude
631.171 km
Speed
7.543 km/s
True Right ascension
00h 51m 20s
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
05:03:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.725 km
Perigee altitude
624.933 km
Semi-major axis
7,003.966 km
Eccentricity
0.00013
Inclination
97.9986°
RAAN
12.8364°
Arg. of periapsis
45.272°
True anomaly
314.84921°
Mean anomaly
314.8596°
Eccentric anomaly
314.85441°
Mean motion
3.70277 °/min
Orbital period
97.22 mins
BSTAR
0.00010051
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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 | 2025-12-19 14:38:35.212Z | 1.164° NNE | 2025-12-19 14:41:35.212Z | 268.446° W | 41.375° | 2025-12-19 14:45:35.212Z | 205.321° SW |
| 6 mins | 2025-12-20 01:33:35.212Z | 169.507° S | 2025-12-20 01:36:35.212Z | 332.32° NNW | 43.259° | 2025-12-20 01:39:35.212Z | 345.623° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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