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: 12 hours ago
TLE from 12 hours ago
0 KINEIS-1C
1 60081U 24114C 26308.50829894 .00000568 00000-0 80499-4 0 9994
2 60081 97.9771 331.8701 0002391 93.5532 266.5953 14.80806224128149Epoch: 2026-11-04T12:11Z
TLE epoch observation values (Epoch: 2026-11-04T12:11:57.028Z)
Latitude
-0.00008°
Longitude
105.12689°
Altitude
629.901 km
Speed
7.543 km/s
True Right ascension
22h 07m 28s
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
20:07:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.498 km
Perigee altitude
622.15 km
Semi-major axis
7,001.961 km
Eccentricity
0.00024
Inclination
97.9771°
RAAN
331.8701°
Arg. of periapsis
93.5532°
True anomaly
266.56795°
Mean anomaly
266.5953°
Eccentric anomaly
266.58162°
Mean motion
3.70436 °/min
Orbital period
97.18 mins
BSTAR
0.000080499
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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 | 2026-11-05 01:17:34.546Z | 145.447° SSE | 2026-11-05 01:21:34.546Z | 72.579° E | 47.186° | 2026-11-05 01:25:34.546Z | 0.171° NNE |
| 7 mins | 2026-11-05 14:43:34.546Z | 7.227° NNE | 2026-11-05 14:46:34.546Z | 261.958° W | 75.146° | 2026-11-05 14:50:34.546Z | 199.497° SSW |
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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