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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 KINEIS-5A
1 62084U 24219D 25258.30974659 .00000943 00000-0 15675-3 0 9996
2 62084 97.9815 58.1254 0003449 98.2748 261.8850 14.72365910 43324Epoch: 2025-09-15T07:26Z
TLE epoch observation values (Epoch: 2025-09-15T07:26:02.105Z)
Latitude
-0.00009°
Longitude
-47.8996°
Altitude
656.877 km
Speed
7.529 km/s
True Right ascension
03h 52m 30s
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
05:50:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.004 km
Perigee altitude
648.156 km
Semi-major axis
7,028.717 km
Eccentricity
0.00034
Inclination
97.9815°
RAAN
58.1254°
Arg. of periapsis
98.2748°
True anomaly
261.84588°
Mean anomaly
261.885°
Eccentric anomaly
261.86544°
Mean motion
3.68323 °/min
Orbital period
97.74 mins
BSTAR
0.00015675
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Other satellites on launch #219 in the year 2024 (2024-11-25 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-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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-15 22:42:38.702Z | 53.164° ENE | 2025-09-15 22:44:38.702Z | 84.662° E | 20.064° | 2025-09-15 22:47:38.702Z | 135.774° SSE |
| 6 mins | 2025-09-16 00:19:38.702Z | 338.729° N | 2025-09-16 00:21:38.702Z | 298.402° NW | 28.278° | 2025-09-16 00:25:38.702Z | 228.289° WSW |
| 4 mins | 2025-09-16 09:42:38.702Z | 86.452° E | 2025-09-16 09:43:38.702Z | 69.215° E | 18.185° | 2025-09-16 09:46:38.702Z | 24.208° NE |
| 6 mins | 2025-09-16 11:17:38.702Z | 203.064° SW | 2025-09-16 11:20:38.702Z | 273.739° WNW | 31.896° | 2025-09-16 11:23:38.702Z | 326.376° NNW |
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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