KINEIS-1A, 60084
Orbit data source: Space-Track
KINEIS-1A, 60084 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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60084 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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-1A
1 60084U 24114F 26038.84492630 .00002233 00000-0 29947-3 0 9999
2 60084 97.9964 63.6220 0003583 164.7732 195.3588 14.80367405 88252Epoch: 2026-02-07T20:16Z
TLE epoch observation values (Epoch: 2026-02-07T20:16:41.632Z)
Latitude
-0.00004°
Longitude
-18.51407°
Altitude
633.605 km
Speed
7.54 km/s
True Right ascension
04h 14m 29s
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
03:25:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.719 km
Perigee altitude
622.7 km
Semi-major axis
7,003.346 km
Eccentricity
0.00036
Inclination
97.9964°
RAAN
63.622°
Arg. of periapsis
164.7732°
True anomaly
195.34793°
Mean anomaly
195.3588°
Eccentric anomaly
195.35336°
Mean motion
3.70326 °/min
Orbital period
97.21 mins
BSTAR
0.00029947
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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-1A 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 | 2026-02-08 01:16:04.009Z | 151.317° SSE | 2026-02-08 01:20:04.009Z | 56.013° ENE | 40.112° | 2026-02-08 01:23:04.009Z | 358.53° N |
| 7 mins | 2026-02-08 14:42:04.009Z | 0.546° NNE | 2026-02-08 14:45:04.009Z | 270.928° WNW | 40.995° | 2026-02-08 14:49:04.009Z | 206.08° 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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