KINEIS-5D, 62082
Orbit data source: Space-Track
KINEIS-5D, 62082 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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62082 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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-5D
1 62082U 24219B 26293.52675905 .00001067 00000-0 17523-3 0 9992
2 62082 97.9295 89.2572 0004129 219.9604 140.1301 14.72638633102209Epoch: 2026-10-20T12:38Z
TLE epoch observation values (Epoch: 2026-10-20T12:38:31.981Z)
Latitude
0.00001°
Longitude
-129.36515°
Altitude
657.897 km
Speed
7.527 km/s
True Right ascension
05h 57m 01s
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
13:10:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.611 km
Perigee altitude
646.807 km
Semi-major axis
7,027.846 km
Eccentricity
0.00041
Inclination
97.9295°
RAAN
89.2572°
Arg. of periapsis
219.9604°
True anomaly
140.16042°
Mean anomaly
140.1301°
Eccentric anomaly
140.14526°
Mean motion
3.68392 °/min
Orbital period
97.72 mins
BSTAR
0.00017523
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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-5D 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 | 2026-10-20 23:00:20.111Z | 28.344° NE | 2026-10-20 23:03:20.111Z | 78.963° E | 46.216° | 2026-10-20 23:07:20.111Z | 170.827° S |
| 6 mins | 2026-10-21 09:59:20.111Z | 128.37° SE | 2026-10-21 10:02:20.111Z | 56.348° ENE | 38.231° | 2026-10-21 10:05:20.111Z | 7.272° NNE |
| 4 mins | 2026-10-21 11:37:20.111Z | 242.835° WSW | 2026-10-21 11:38:20.111Z | 259.066° W | 18.364° | 2026-10-21 11:41:20.111Z | 305.29° NW |
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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