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: 13 hours ago
TLE from 13 hours ago
0 KINEIS-1B
1 60079U 24114A 25350.02001648 .00000992 00000-0 13762-3 0 9992
2 60079 97.9982 9.9913 0002130 4.1940 355.9290 14.80170332 80306Epoch: 2025-12-16T00:28Z
TLE epoch observation values (Epoch: 2025-12-16T00:28:49.423Z)
Latitude
0.00003°
Longitude
-82.12486°
Altitude
630.316 km
Speed
7.544 km/s
True Right ascension
00h 39m 57s
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
12:11:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.323 km
Perigee altitude
624.34 km
Semi-major axis
7,003.969 km
Eccentricity
0.00021
Inclination
97.9982°
RAAN
9.9913°
Arg. of periapsis
4.194°
True anomaly
355.92727°
Mean anomaly
355.929°
Eccentric anomaly
355.92813°
Mean motion
3.70277 °/min
Orbital period
97.22 mins
BSTAR
0.00013762
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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 | 2025-12-16 14:01:40.760Z | 25.219° NE | 2025-12-16 14:05:40.760Z | 107.31° ESE | 37.302° | 2025-12-16 14:09:40.760Z | 175.532° S |
| 6 mins | 2025-12-17 00:57:40.760Z | 129.312° SE | 2025-12-17 01:00:40.760Z | 60.606° ENE | 31.009° | 2025-12-17 01:03:40.760Z | 8.153° NNE |
| 4 mins | 2025-12-17 02:35:40.760Z | 247.897° W | 2025-12-17 02:36:40.760Z | 265.255° W | 17.234° | 2025-12-17 02:39:40.760Z | 309.697° NW |
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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