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: 12 hours ago
TLE from 12 hours ago
0 KINEIS-1E
1 60083U 24114E 25258.32594138 .00001061 00000-0 14789-3 0 9996
2 60083 98.0079 278.5194 0000533 74.0607 286.0663 14.79828836 66721Epoch: 2025-09-15T07:49Z
TLE epoch observation values (Epoch: 2025-09-15T07:49:21.335Z)
Latitude
-0.00003°
Longitude
166.6483°
Altitude
632.779 km
Speed
7.542 km/s
True Right ascension
18h 34m 04s
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
12:30:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.284 km
Perigee altitude
626.537 km
Semi-major axis
7,005.047 km
Eccentricity
0.00005
Inclination
98.0079°
RAAN
278.5194°
Arg. of periapsis
74.0607°
True anomaly
286.06043°
Mean anomaly
286.0663°
Eccentric anomaly
286.06337°
Mean motion
3.70192 °/min
Orbital period
97.25 mins
BSTAR
0.00014789
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-16 00:12:51.639Z | 97.402° ESE | 2025-09-16 00:14:51.639Z | 69.793° E | 14.112° | 2025-09-16 00:16:51.639Z | 39.708° NE |
| 7 mins | 2025-09-16 01:47:51.639Z | 188.243° SSW | 2025-09-16 01:50:51.639Z | 249.572° W | 37.557° | 2025-09-16 01:54:51.639Z | 334.886° NNW |
| 5 mins | 2025-09-16 13:37:51.639Z | 50.853° ENE | 2025-09-16 13:39:51.639Z | 90.687° ESE | 25.751° | 2025-09-16 13:42:51.639Z | 148.665° SSE |
| 5 mins | 2025-09-16 15:13:51.639Z | 334.318° NNW | 2025-09-16 15:15:51.639Z | 300.121° NW | 21.842° | 2025-09-16 15:18:51.639Z | 246.671° WSW |
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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