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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-1B
1 60079U 24114A 26089.58776469 .00001628 00000-0 21975-3 0 9995
2 60079 97.9896 114.1344 0002564 27.3689 332.7658 14.80474915 95777Epoch: 2026-03-30T14:06Z
TLE epoch observation values (Epoch: 2026-03-30T14:06:22.869Z)
Latitude
0.00003°
Longitude
74.56195°
Altitude
629.247 km
Speed
7.545 km/s
True Right ascension
07h 36m 32s
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
05:13:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.665 km
Perigee altitude
623.074 km
Semi-major axis
7,003.007 km
Eccentricity
0.00026
Inclination
97.9896°
RAAN
114.1344°
Arg. of periapsis
27.3689°
True anomaly
332.75235°
Mean anomaly
332.7658°
Eccentric anomaly
332.75908°
Mean motion
3.70353 °/min
Orbital period
97.2 mins
BSTAR
0.00021975
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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 | 2026-03-31 01:34:15.892Z | 166.331° S | 2026-03-31 01:38:15.892Z | 170.147° S | 44.456° | 2026-03-31 01:42:15.892Z | 347.135° N |
| 6 mins | 2026-03-31 15:01:15.892Z | 343.367° N | 2026-03-31 15:03:15.892Z | 297.365° NW | 32.255° | 2026-03-31 15:07:15.892Z | 221.179° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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