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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-1C
1 60081U 24114C 26130.51032773 .00000613 00000-0 86880-4 0 9991
2 60081 97.9866 154.7151 0000970 56.2801 303.8503 14.80564050101809Epoch: 2026-05-10T12:14Z
TLE epoch observation values (Epoch: 2026-05-10T12:14:52.315Z)
Latitude
-0.00008°
Longitude
102.68476°
Altitude
630.185 km
Speed
7.544 km/s
True Right ascension
10h 18m 51s
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
07:08:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.268 km
Perigee altitude
623.909 km
Semi-major axis
7,002.725 km
Eccentricity
0.0001
Inclination
97.9866°
RAAN
154.7151°
Arg. of periapsis
56.2801°
True anomaly
303.84107°
Mean anomaly
303.8503°
Eccentric anomaly
303.84568°
Mean motion
3.70376 °/min
Orbital period
97.2 mins
BSTAR
0.00008688
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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 | 2026-05-11 01:20:58.281Z | 152.213° SSE | 2026-05-11 01:24:58.281Z | 41.866° NE | 39.976° | 2026-05-11 01:27:58.281Z | 356.743° N |
| 6 mins | 2026-05-11 14:46:58.281Z | 357.408° N | 2026-05-11 14:48:58.281Z | 317.031° NNW | 39.087° | 2026-05-11 14:52:58.281Z | 209.488° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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