KINEIS-1B, 60079
Orbit data source: Space-Track
KINEIS-1B, 60079 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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60079 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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-1B
1 60079U 24114A 26038.82750517 .00001625 00000-0 22000-3 0 9999
2 60079 97.9952 63.5816 0003315 135.1618 224.9862 14.80334639 88269Epoch: 2026-02-07T19:51Z
TLE epoch observation values (Epoch: 2026-02-07T19:51:36.446Z)
Latitude
-0.00005°
Longitude
-12.26569°
Altitude
632.931 km
Speed
7.541 km/s
True Right ascension
04h 14m 19s
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
03:29:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.634 km
Perigee altitude
622.991 km
Semi-major axis
7,003.45 km
Eccentricity
0.00033
Inclination
97.9952°
RAAN
63.5816°
Arg. of periapsis
135.1618°
True anomaly
224.95935°
Mean anomaly
224.9862°
Eccentric anomaly
224.97278°
Mean motion
3.70318 °/min
Orbital period
97.21 mins
BSTAR
0.00022
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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-1B 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-08 02:28:10.654Z | 215.838° SW | 2026-02-08 02:31:10.654Z | 261.134° W | 20.251° | 2026-02-08 02:34:10.654Z | 310.77° NW |
| 7 mins | 2026-02-08 14:17:10.654Z | 20.861° NNE | 2026-02-08 14:20:10.654Z | 110.259° ESE | 43.157° | 2026-02-08 14:24:10.654Z | 185.519° SSW |
| 5 mins | 2026-02-09 01:12:10.654Z | 140.924° SSE | 2026-02-09 01:15:10.654Z | 53.915° ENE | 37.303° | 2026-02-09 01:17:10.654Z | 7.674° NNE |
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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