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: 12 hours ago
TLE from 12 hours ago
0 KINEIS-1B
1 60079U 24114A 26308.47450322 .00000582 00000-0 82369-4 0 9997
2 60079 97.9751 331.9563 0002738 32.4114 327.7265 14.80810659128169Epoch: 2026-11-04T11:23Z
TLE epoch observation values (Epoch: 2026-11-04T11:23:17.078Z)
Latitude
-0.00009°
Longitude
117.41286°
Altitude
628.165 km
Speed
7.545 km/s
True Right ascension
22h 07m 49s
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
19:14:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.727 km
Perigee altitude
621.892 km
Semi-major axis
7,001.947 km
Eccentricity
0.00027
Inclination
97.9751°
RAAN
331.9563°
Arg. of periapsis
32.4114°
True anomaly
327.70974°
Mean anomaly
327.7265°
Eccentric anomaly
327.71812°
Mean motion
3.70438 °/min
Orbital period
97.18 mins
BSTAR
0.000082369
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-05 00:31:59.962Z | 91.728° ESE | 2026-11-05 00:33:59.962Z | 61.615° ENE | 15.144° | 2026-11-05 00:35:59.962Z | 32.944° NE |
| 6 mins | 2026-11-05 02:06:59.962Z | 193.697° SSW | 2026-11-05 02:09:59.962Z | 277.976° WNW | 47.385° | 2026-11-05 02:12:59.962Z | 332.038° NNW |
| 6 mins | 2026-11-05 13:55:59.962Z | 50.054° ENE | 2026-11-05 13:57:59.962Z | 90.532° ESE | 29.867° | 2026-11-05 14:01:59.962Z | 158.095° S |
| 5 mins | 2026-11-05 15:31:59.962Z | 332.897° NNW | 2026-11-05 15:33:59.962Z | 298.551° NW | 23.131° | 2026-11-05 15:36:59.962Z | 246.743° 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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