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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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, 1.0 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 KINEIS-5D
1 62082U 24219B 25350.00549794 .00000021 00000-0 11113-4 0 9993
2 62082 97.9810 147.9935 0001838 180.3888 179.7319 14.72305781 56802Epoch: 2025-12-16T00:07Z
TLE epoch observation values (Epoch: 2025-12-16T00:07:55.022Z)
Latitude
0.00007°
Longitude
61.11831°
Altitude
658.018 km
Speed
7.528 km/s
True Right ascension
09h 51m 58s
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
08:10:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.063 km
Perigee altitude
649.48 km
Semi-major axis
7,028.909 km
Eccentricity
0.00018
Inclination
97.981°
RAAN
147.9935°
Arg. of periapsis
180.3888°
True anomaly
179.732°
Mean anomaly
179.7319°
Eccentric anomaly
179.73195°
Mean motion
3.68308 °/min
Orbital period
97.74 mins
BSTAR
0.000011113
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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
Loading observer location...
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 | 2025-12-16 10:02:43.725Z | 133.616° SE | 2025-12-16 10:06:43.725Z | 67.671° E | 28.975° | 2025-12-16 10:09:43.725Z | 12.845° NNE |
| 5 mins | 2025-12-16 11:41:43.725Z | 234.988° WSW | 2025-12-16 11:43:43.725Z | 270.971° WNW | 20.029° | 2025-12-16 11:46:43.725Z | 314.54° NW |
| 7 mins | 2025-12-16 23:32:43.725Z | 15.455° NNE | 2025-12-16 23:35:43.725Z | 48.4° ENE | 44.277° | 2025-12-16 23:39:43.725Z | 190.427° SSW |
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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