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: 15 hours ago
TLE from 15 hours ago
0 KINEIS-1C
1 60081U 24114C 25345.25409753 .00002646 00000-0 35523-3 0 9990
2 60081 98.0003 5.0506 0002381 83.9491 276.1992 14.80170153 79575Epoch: 2025-12-11T06:05Z
TLE epoch observation values (Epoch: 2025-12-11T06:05:54.026Z)
Latitude
-0.00003°
Longitude
-166.63722°
Altitude
631.626 km
Speed
7.543 km/s
True Right ascension
00h 20m 12s
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
19:31:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.5 km
Perigee altitude
624.165 km
Semi-major axis
7,003.969 km
Eccentricity
0.00024
Inclination
98.0003°
RAAN
5.0506°
Arg. of periapsis
83.9491°
True anomaly
276.17207°
Mean anomaly
276.1992°
Eccentric anomaly
276.18564°
Mean motion
3.70277 °/min
Orbital period
97.22 mins
BSTAR
0.00035523
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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
Loading observer location...
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 | 2025-12-12 01:41:33.447Z | 178.451° S | 2025-12-12 01:44:33.447Z | 236.987° WSW | 42.089° | 2025-12-12 01:48:33.447Z | 340.27° N |
| 5 mins | 2025-12-12 13:31:33.447Z | 57.564° ENE | 2025-12-12 13:33:33.447Z | 94.025° ESE | 21.182° | 2025-12-12 13:36:33.447Z | 143.158° SSE |
| 6 mins | 2025-12-12 15:07:33.447Z | 337.461° NNW | 2025-12-12 15:09:33.447Z | 298.385° NW | 26.247° | 2025-12-12 15:13:33.447Z | 230.266° 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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