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 25322.48873447 .00001915 00000-0 25964-3 0 9993
2 60083 98.0012 342.4651 0002405 85.1754 274.9732 14.80081270 76216Epoch: 2025-11-18T11:43Z
TLE epoch observation values (Epoch: 2025-11-18T11:43:46.658Z)
Latitude
-0.00003°
Longitude
108.7466°
Altitude
631.94 km
Speed
7.542 km/s
True Right ascension
22h 49m 51s
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
15:34:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.797 km
Perigee altitude
624.428 km
Semi-major axis
7,004.25 km
Eccentricity
0.00024
Inclination
98.0012°
RAAN
342.4651°
Arg. of periapsis
85.1754°
True anomaly
274.94574°
Mean anomaly
274.9732°
Eccentric anomaly
274.95947°
Mean motion
3.70255 °/min
Orbital period
97.23 mins
BSTAR
0.00025964
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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 | 2025-11-19 00:50:39.455Z | 131.052° SE | 2025-11-19 00:53:39.455Z | 81.63° E | 28.452° | 2025-11-19 00:57:39.455Z | 8.272° NNE |
| 4 mins | 2025-11-19 02:28:39.455Z | 235.547° WSW | 2025-11-19 02:30:39.455Z | 271.533° WNW | 19.028° | 2025-11-19 02:32:39.455Z | 304.082° NW |
| 6 mins | 2025-11-19 14:16:39.455Z | 19.781° NNE | 2025-11-19 14:19:39.455Z | 155.476° SSE | 42.51° | 2025-11-19 14:22:39.455Z | 186.968° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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