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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-1A
1 60084U 24114F 26255.31138072 .00000467 00000-0 67390-4 0 9991
2 60084 97.8909 277.4358 0003420 197.7825 162.3268 14.80730364120283Epoch: 2026-09-12T07:28Z
TLE epoch observation values (Epoch: 2026-09-12T07:28:23.294Z)
Latitude
-0.00003°
Longitude
174.01654°
Altitude
632.326 km
Speed
7.541 km/s
True Right ascension
18h 29m 44s
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
09:48:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.454 km
Perigee altitude
621.664 km
Semi-major axis
7,002.196 km
Eccentricity
0.00034
Inclination
97.8909°
RAAN
277.4358°
Arg. of periapsis
197.7825°
True anomaly
162.33869°
Mean anomaly
162.3268°
Eccentric anomaly
162.33275°
Mean motion
3.70418 °/min
Orbital period
97.19 mins
BSTAR
0.00006739
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-13 01:25:33.887Z | 159.014° S | 2026-09-13 01:29:33.887Z | 98.972° ESE | 70.907° | 2026-09-13 01:33:33.887Z | 352.524° N |
| 7 mins | 2026-09-13 14:51:33.887Z | 356.14° N | 2026-09-13 14:54:33.887Z | 292.602° NW | 48.688° | 2026-09-13 14:58:33.887Z | 213.833° 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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