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: 19 hours ago
TLE from 19 hours ago
0 KINEIS-1E
1 60083U 24114E 25260.21920307 .00000868 00000-0 12214-3 0 9993
2 60083 98.0078 280.4068 0000500 85.4571 274.6697 14.79830597 67001Epoch: 2025-09-17T05:15Z
TLE epoch observation values (Epoch: 2025-09-17T05:15:39.145Z)
Latitude
-0.00007°
Longitude
-154.90459°
Altitude
632.848 km
Speed
7.542 km/s
True Right ascension
18h 41m 37s
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
16:51:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.255 km
Perigee altitude
626.555 km
Semi-major axis
7,005.042 km
Eccentricity
0.00005
Inclination
98.0078°
RAAN
280.4068°
Arg. of periapsis
85.4571°
True anomaly
274.66399°
Mean anomaly
274.6697°
Eccentric anomaly
274.66684°
Mean motion
3.70192 °/min
Orbital period
97.25 mins
BSTAR
0.00012214
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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 | 2025-09-18 00:51:42.148Z | 136.65° SSE | 2025-09-18 00:55:42.148Z | 62.498° ENE | 30.848° | 2025-09-18 00:58:42.148Z | 8.836° NNE |
| 4 mins | 2025-09-18 02:30:42.148Z | 246.526° WSW | 2025-09-18 02:31:42.148Z | 263.899° W | 17.496° | 2025-09-18 02:34:42.148Z | 309.142° NW |
| 7 mins | 2025-09-18 14:17:42.148Z | 14.983° NNE | 2025-09-18 14:20:42.148Z | 81.03° E | 44.828° | 2025-09-18 14:24:42.148Z | 191.48° 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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