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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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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-5A
1 62084U 24219D 26124.58129715 .00001494 00000-0 24390-3 0 9990
2 62084 97.9214 285.0624 0007189 73.9217 286.2782 14.72314879 77358Epoch: 2026-05-04T13:57Z
TLE epoch observation values (Epoch: 2026-05-04T13:57:04.073Z)
Latitude
-0.00002°
Longitude
-146.67301°
Altitude
655.284 km
Speed
7.531 km/s
True Right ascension
19h 00m 14s
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
02:59:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
655.793 km
Perigee altitude
645.687 km
Semi-major axis
7,028.877 km
Eccentricity
0.00072
Inclination
97.9214°
RAAN
285.0624°
Arg. of periapsis
73.9217°
True anomaly
286.1991°
Mean anomaly
286.2782°
Eccentric anomaly
286.23865°
Mean motion
3.68311 °/min
Orbital period
97.74 mins
BSTAR
0.0002439
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-04 22:41:22.957Z | 43.196° NE | 2026-05-04 22:44:22.957Z | 88.075° E | 21.877° | 2026-05-04 22:47:22.957Z | 140.256° SSE |
| 5 mins | 2026-05-05 00:19:22.957Z | 333.991° NNW | 2026-05-05 00:21:22.957Z | 292.715° NW | 26.628° | 2026-05-05 00:24:22.957Z | 237.34° WSW |
| 5 mins | 2026-05-05 09:41:22.957Z | 100.238° ESE | 2026-05-05 09:43:22.957Z | 66.37° ENE | 19.401° | 2026-05-05 09:46:22.957Z | 21.48° NNE |
| 6 mins | 2026-05-05 11:17:22.957Z | 207.826° SW | 2026-05-05 11:20:22.957Z | 277.267° WNW | 29.68° | 2026-05-05 11:23:22.957Z | 325.61° 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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