KINEIS-1C, 60081
Orbit data source: Space-Track
KINEIS-1C, 60081 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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60081 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-1C
1 60081U 24114C 25301.64916932 .00001442 00000-0 19749-3 0 9992
2 60081 98.0048 321.6025 0001188 138.8286 221.3016 14.80014513 73124Epoch: 2025-10-28T15:34Z
TLE epoch observation values (Epoch: 2025-10-28T15:34:48.229Z)
Latitude
0.00005°
Longitude
50.66791°
Altitude
632.922 km
Speed
7.542 km/s
True Right ascension
21h 26m 24s
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
17:36:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.156 km
Perigee altitude
625.492 km
Semi-major axis
7,004.461 km
Eccentricity
0.00012
Inclination
98.0048°
RAAN
321.6025°
Arg. of periapsis
138.8286°
True anomaly
221.29262°
Mean anomaly
221.3016°
Eccentric anomaly
221.29711°
Mean motion
3.70238 °/min
Orbital period
97.23 mins
BSTAR
0.00019749
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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-1C 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-29 01:26:08.165Z | 165.041° S | 2025-10-29 01:30:08.165Z | 357.785° N | 44.331° | 2025-10-29 01:34:08.165Z | 347.995° N |
| 4 mins | 2025-10-29 13:17:08.165Z | 68.793° E | 2025-10-29 13:18:08.165Z | 84.493° E | 15.724° | 2025-10-29 13:21:08.165Z | 129.991° SE |
| 6 mins | 2025-10-29 14:52:08.165Z | 350.941° N | 2025-10-29 14:55:08.165Z | 285.857° WNW | 33.186° | 2025-10-29 14:58:08.165Z | 224.438° SW |
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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