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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-5D
1 62082U 24219B 26128.26676948 .00000794 00000-0 13298-3 0 9999
2 62082 97.9116 288.1970 0005954 53.2741 306.9013 14.72374841 77886Epoch: 2026-05-08T06:24Z
TLE epoch observation values (Epoch: 2026-05-08T06:24:08.883Z)
Latitude
0.00002°
Longitude
-33.94103°
Altitude
653.995 km
Speed
7.532 km/s
True Right ascension
19h 12m 47s
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
21:28:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.733 km
Perigee altitude
646.364 km
Semi-major axis
7,028.685 km
Eccentricity
0.0006
Inclination
97.9116°
RAAN
288.197°
Arg. of periapsis
53.2741°
True anomaly
306.84672°
Mean anomaly
306.9013°
Eccentric anomaly
306.87401°
Mean motion
3.68326 °/min
Orbital period
97.74 mins
BSTAR
0.00013298
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-08 23:16:37.610Z | 20.127° NNE | 2026-05-08 23:20:37.610Z | 87.915° E | 41.32° | 2026-05-08 23:24:37.610Z | 180.632° SSW |
| 6 mins | 2026-05-09 10:16:37.610Z | 136.964° SSE | 2026-05-09 10:18:37.610Z | 91.599° ESE | 36.706° | 2026-05-09 10:22:37.610Z | 1.225° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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