KINEIS-1D, 60082
Orbit data source: Space-Track
KINEIS-1D, 60082 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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60082 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 KINEIS-1D
1 60082U 24114D 26038.84715318 .00001357 00000-0 20415-3 0 9995
2 60082 97.9990 60.3471 0000523 175.9252 184.1962 14.76058211 88049Epoch: 2026-02-07T20:19Z
TLE epoch observation values (Epoch: 2026-02-07T20:19:54.034Z)
Latitude
-0.00002°
Longitude
-22.59284°
Altitude
645.174 km
Speed
7.535 km/s
True Right ascension
04h 01m 23s
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
03:30:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.212 km
Perigee altitude
638.478 km
Semi-major axis
7,016.982 km
Eccentricity
0.00005
Inclination
97.999°
RAAN
60.3471°
Arg. of periapsis
175.9252°
True anomaly
184.19576°
Mean anomaly
184.1962°
Eccentric anomaly
184.19598°
Mean motion
3.69248 °/min
Orbital period
97.5 mins
BSTAR
0.00020415
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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-1D 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 | 2026-02-08 01:19:33.659Z | 166.574° S | 2026-02-08 01:23:33.659Z | 183.478° SSW | 44.92° | 2026-02-08 01:27:33.659Z | 346.998° N |
| 4 mins | 2026-02-08 13:12:33.659Z | 63.752° ENE | 2026-02-08 13:14:33.659Z | 97.003° ESE | 17.682° | 2026-02-08 13:16:33.659Z | 128.401° SE |
| 6 mins | 2026-02-08 14:48:33.659Z | 343.977° N | 2026-02-08 14:50:33.659Z | 303.676° NW | 30.763° | 2026-02-08 14:54:33.659Z | 224.507° SW |
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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