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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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: 12 hours ago
TLE from 12 hours ago
0 KINEIS-1E
1 60083U 24114E 26269.60266752 .00000525 00000-0 74808-4 0 9991
2 60083 97.8925 291.4273 0001555 210.9410 149.1711 14.80782304122398Epoch: 2026-09-26T14:27Z
TLE epoch observation values (Epoch: 2026-09-26T14:27:50.473Z)
Latitude
-0.00004°
Longitude
69.05863°
Altitude
630.814 km
Speed
7.542 km/s
True Right ascension
19h 25m 42s
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
19:57:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.984 km
Perigee altitude
622.807 km
Semi-major axis
7,002.032 km
Eccentricity
0.00016
Inclination
97.8925°
RAAN
291.4273°
Arg. of periapsis
210.941°
True anomaly
149.18023°
Mean anomaly
149.1711°
Eccentric anomaly
149.17567°
Mean motion
3.70431 °/min
Orbital period
97.18 mins
BSTAR
0.000074808
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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 | 2026-09-27 13:44:54.493Z | 38.883° NE | 2026-09-27 13:47:54.493Z | 88.005° E | 29.081° | 2026-09-27 13:51:54.493Z | 156.734° SSE |
| 5 mins | 2026-09-27 15:21:54.493Z | 334.433° NNW | 2026-09-27 15:23:54.493Z | 300.849° NW | 23.333° | 2026-09-27 15:26:54.493Z | 247.359° WSW |
| 5 mins | 2026-09-28 00:40:54.493Z | 105.113° ESE | 2026-09-28 00:42:54.493Z | 69.264° E | 22.786° | 2026-09-28 00:45:54.493Z | 20.625° NNE |
| 6 mins | 2026-09-28 02:16:54.493Z | 217.196° SW | 2026-09-28 02:18:54.493Z | 259.507° W | 30.715° | 2026-09-28 02:22:54.493Z | 325.907° NNW |
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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