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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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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-1C
1 60081U 24114C 26089.55401378 .00002359 00000-0 31526-3 0 9994
2 60081 97.9915 113.9308 0002541 90.5854 269.5649 14.80475553 95743Epoch: 2026-03-30T13:17Z
TLE epoch observation values (Epoch: 2026-03-30T13:17:46.790Z)
Latitude
-0.00004°
Longitude
86.54196°
Altitude
630.857 km
Speed
7.543 km/s
True Right ascension
07h 35m 43s
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
05:10:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.647 km
Perigee altitude
623.088 km
Semi-major axis
7,003.005 km
Eccentricity
0.00025
Inclination
97.9915°
RAAN
113.9308°
Arg. of periapsis
90.5854°
True anomaly
269.53578°
Mean anomaly
269.5649°
Eccentric anomaly
269.55034°
Mean motion
3.70354 °/min
Orbital period
97.2 mins
BSTAR
0.00031526
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-31 00:47:12.463Z | 125.187° SE | 2026-03-31 00:50:12.463Z | 79.947° E | 24.201° | 2026-03-31 00:54:12.463Z | 12.193° NNE |
| 5 mins | 2026-03-31 02:25:12.463Z | 231.082° WSW | 2026-03-31 02:27:12.463Z | 272.729° WNW | 22.674° | 2026-03-31 02:30:12.463Z | 318.587° NNW |
| 6 mins | 2026-03-31 14:13:12.463Z | 29.461° NE | 2026-03-31 14:15:12.463Z | 79.273° E | 40.106° | 2026-03-31 14:19:12.463Z | 179.265° S |
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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