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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-1A
1 60084U 24114F 25345.16977260 .00001493 00000-0 20372-3 0 9991
2 60084 98.0001 5.1738 0003986 37.3372 322.8116 14.80138640 79579Epoch: 2025-12-11T04:04Z
TLE epoch observation values (Epoch: 2025-12-11T04:04:28.352Z)
Latitude
-0.00005°
Longitude
-136.07393°
Altitude
629.68 km
Speed
7.545 km/s
True Right ascension
00h 20m 41s
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
09:32:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.724 km
Perigee altitude
623.14 km
Semi-major axis
7,004.069 km
Eccentricity
0.0004
Inclination
98.0001°
RAAN
5.1738°
Arg. of periapsis
37.3372°
True anomaly
322.78398°
Mean anomaly
322.8116°
Eccentric anomaly
322.79779°
Mean motion
3.70269 °/min
Orbital period
97.23 mins
BSTAR
0.00020372
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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 | 2025-12-11 14:22:52.479Z | 13.662° NNE | 2025-12-11 14:25:52.479Z | 22.732° NE | 43.817° | 2025-12-11 14:29:52.479Z | 192.594° SSW |
| 7 mins | 2025-12-12 01:17:52.479Z | 152.893° SSE | 2025-12-12 01:20:52.479Z | 88.258° E | 41.982° | 2025-12-12 01:24:52.479Z | 354.545° N |
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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