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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-5D
1 62082U 24219B 26134.92668565 .00000533 00000-0 91897-4 0 9998
2 62082 97.9120 294.6795 0005513 35.3456 324.8117 14.72383263 78864Epoch: 2026-05-14T22:14Z
TLE epoch observation values (Epoch: 2026-05-14T22:14:25.640Z)
Latitude
0.00007°
Longitude
88.40731°
Altitude
653.313 km
Speed
7.533 km/s
True Right ascension
19h 38m 43s
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
17:58:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.397 km
Perigee altitude
646.647 km
Semi-major axis
7,028.659 km
Eccentricity
0.00055
Inclination
97.912°
RAAN
294.6795°
Arg. of periapsis
35.3456°
True anomaly
324.77527°
Mean anomaly
324.8117°
Eccentric anomaly
324.79349°
Mean motion
3.68328 °/min
Orbital period
97.74 mins
BSTAR
0.000091897
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-15 09:47:49.518Z | 121.585° SE | 2026-05-15 09:50:49.518Z | 76.162° E | 23.317° | 2026-05-15 09:53:49.518Z | 21.892° NNE |
| 5 mins | 2026-05-15 11:25:49.518Z | 223.097° SW | 2026-05-15 11:27:49.518Z | 263.766° W | 25.123° | 2026-05-15 11:30:49.518Z | 316.544° NNW |
| 6 mins | 2026-05-15 23:17:49.518Z | 26.771° NE | 2026-05-15 23:20:49.518Z | 131.62° SE | 40.384° | 2026-05-15 23:23:49.518Z | 179.291° S |
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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