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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-1B
1 60079U 24114A 25299.51912112 .00001552 00000-0 21225-3 0 9991
2 60079 98.0033 319.6837 0003644 119.4139 240.7437 14.79982328 72839Epoch: 2025-10-26T12:27Z
TLE epoch observation values (Epoch: 2025-10-26T12:27:32.064Z)
Latitude
-0.00001°
Longitude
97.66595°
Altitude
633.647 km
Speed
7.541 km/s
True Right ascension
21h 18m 44s
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
17:50:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.978 km
Perigee altitude
623.873 km
Semi-major axis
7,004.562 km
Eccentricity
0.00036
Inclination
98.0033°
RAAN
319.6837°
Arg. of periapsis
119.4139°
True anomaly
240.70728°
Mean anomaly
240.7437°
Eccentric anomaly
240.72549°
Mean motion
3.7023 °/min
Orbital period
97.24 mins
BSTAR
0.00021225
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-27 01:33:26.599Z | 171.094° S | 2025-10-27 01:37:26.599Z | 296.14° NW | 44.075° | 2025-10-27 01:41:26.599Z | 344.601° N |
| 4 mins | 2025-10-27 13:24:26.599Z | 65.478° ENE | 2025-10-27 13:26:26.599Z | 100.957° ESE | 18.325° | 2025-10-27 13:28:26.599Z | 132.455° SE |
| 5 mins | 2025-10-27 15:00:26.599Z | 336.579° NNW | 2025-10-27 15:02:26.599Z | 288.812° WNW | 29.604° | 2025-10-27 15:05:26.599Z | 230.537° WSW |
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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