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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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-1B
1 60079U 24114A 26255.29427422 .00000510 00000-0 73105-4 0 9992
2 60079 97.9811 279.0619 0003040 145.3543 214.7868 14.80742598120293Epoch: 2026-09-12T07:03Z
TLE epoch observation values (Epoch: 2026-09-12T07:03:45.292Z)
Latitude
0.00001°
Longitude
-178.18216°
Altitude
631.751 km
Speed
7.542 km/s
True Right ascension
18h 36m 14s
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
10:37:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.153 km
Perigee altitude
621.896 km
Semi-major axis
7,002.162 km
Eccentricity
0.0003
Inclination
97.9811°
RAAN
279.0619°
Arg. of periapsis
145.3543°
True anomaly
214.76693°
Mean anomaly
214.7868°
Eccentric anomaly
214.77687°
Mean motion
3.7042 °/min
Orbital period
97.19 mins
BSTAR
0.000073105
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-13 01:02:21.843Z | 129.137° SE | 2026-09-13 01:05:21.843Z | 76.632° E | 32.678° | 2026-09-13 01:09:21.843Z | 7.696° NNE |
| 4 mins | 2026-09-13 02:40:21.843Z | 238.372° WSW | 2026-09-13 02:41:21.843Z | 256.096° W | 20.486° | 2026-09-13 02:44:21.843Z | 306.969° NW |
| 7 mins | 2026-09-13 14:27:21.843Z | 18.939° NNE | 2026-09-13 14:30:21.843Z | 95.035° ESE | 73.576° | 2026-09-13 14:34:21.843Z | 186.938° SSW |
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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