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: 4 hours ago
TLE from 4 hours ago
0 KINEIS-1B
1 60079U 24114A 25304.86023839 .00001479 00000-0 20254-3 0 9994
2 60079 98.0028 325.0055 0003811 108.4035 251.7591 14.79998391 73623Epoch: 2025-10-31T20:38Z
TLE epoch observation values (Epoch: 2025-10-31T20:38:44.596Z)
Latitude
-0.00007°
Longitude
-25.07892°
Altitude
633.185 km
Speed
7.541 km/s
True Right ascension
21h 40m 01s
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
20:34:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
629.044 km
Perigee altitude
623.705 km
Semi-major axis
7,004.512 km
Eccentricity
0.00038
Inclination
98.0028°
RAAN
325.0055°
Arg. of periapsis
108.4035°
True anomaly
251.71763°
Mean anomaly
251.7591°
Eccentric anomaly
251.73836°
Mean motion
3.70234 °/min
Orbital period
97.24 mins
BSTAR
0.00020254
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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 | 2025-11-01 01:38:01.999Z | 175.337° S | 2025-11-01 01:42:01.999Z | 300.286° NW | 42.013° | 2025-11-01 01:45:01.999Z | 340.825° N |
| 4 mins | 2025-11-01 13:29:01.999Z | 67.535° E | 2025-11-01 13:30:01.999Z | 85.906° E | 19.953° | 2025-11-01 13:33:01.999Z | 137.512° SSE |
| 6 mins | 2025-11-01 15:04:01.999Z | 343.288° N | 2025-11-01 15:07:01.999Z | 282.381° WNW | 27.316° | 2025-11-01 15:10:01.999Z | 231.765° WSW |
| 4 mins | 2025-11-02 00:24:01.999Z | 94.332° ESE | 2025-11-02 00:26:01.999Z | 61.548° ENE | 16.784° | 2025-11-02 00:28:01.999Z | 31.052° NE |
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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