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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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-1A
1 60084U 24114F 26308.49198435 .00000568 00000-0 80426-4 0 9995
2 60084 97.8854 329.7371 0005150 57.7826 302.3885 14.80805332128159Epoch: 2026-11-04T11:48Z
TLE epoch observation values (Epoch: 2026-11-04T11:48:27.447Z)
Latitude
-0.00006°
Longitude
108.88322°
Altitude
627.875 km
Speed
7.546 km/s
True Right ascension
21h 58m 56s
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
20:07:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.428 km
Perigee altitude
620.216 km
Semi-major axis
7,001.959 km
Eccentricity
0.00052
Inclination
97.8854°
RAAN
329.7371°
Arg. of periapsis
57.7826°
True anomaly
302.33865°
Mean anomaly
302.3885°
Eccentric anomaly
302.36358°
Mean motion
3.70437 °/min
Orbital period
97.18 mins
BSTAR
0.000080426
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-05 00:55:18.827Z | 127.073° SE | 2026-11-05 00:58:18.827Z | 70.406° E | 32.28° | 2026-11-05 01:01:18.827Z | 13.806° NNE |
| 5 mins | 2026-11-05 02:32:18.827Z | 226.979° WSW | 2026-11-05 02:34:18.827Z | 260.232° W | 20.857° | 2026-11-05 02:37:18.827Z | 309.704° NW |
| 7 mins | 2026-11-05 14:20:18.827Z | 19.468° NNE | 2026-11-05 14:23:18.827Z | 129.759° SE | 71.965° | 2026-11-05 14:27:18.827Z | 187.299° SSW |
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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