KINEIS-5A, 62084
Orbit data source: Space-Track
KINEIS-5A, 62084 is a French payload satellite in SSO that was launched on Mon, 25 Nov 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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62084 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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-5A
1 62084U 24219D 25327.49364192 .00000945 00000-0 15714-3 0 9994
2 62084 97.9856 126.0852 0001319 209.6060 150.5073 14.72328637 53504Epoch: 2025-11-23T11:50Z
TLE epoch observation values (Epoch: 2025-11-23T11:50:50.661Z)
Latitude
-0.00005°
Longitude
-114.33305°
Altitude
657.46 km
Speed
7.528 km/s
True Right ascension
08h 24m 20s
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
18:23:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.626 km
Perigee altitude
649.772 km
Semi-major axis
7,028.836 km
Eccentricity
0.00013
Inclination
97.9856°
RAAN
126.0852°
Arg. of periapsis
209.606°
True anomaly
150.51474°
Mean anomaly
150.5073°
Eccentric anomaly
150.51102°
Mean motion
3.68314 °/min
Orbital period
97.74 mins
BSTAR
0.00015714
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Other satellites on launch #219 in the year 2024 (2024-11-25 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.KINEIS-5A 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 | 2025-11-23 23:50:23.205Z | 3.777° NNE | 2025-11-23 23:53:23.205Z | 307.388° NW | 41.904° | 2025-11-23 23:57:23.205Z | 205.518° SW |
| 7 mins | 2025-11-24 10:48:23.205Z | 170.867° S | 2025-11-24 10:51:23.205Z | 196.309° SSW | 43.355° | 2025-11-24 10:55:23.205Z | 344.224° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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