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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-5D
1 62082U 24219B 25343.20945171 .00001499 00000-0 24458-3 0 9991
2 62082 97.9855 141.3199 0000928 198.8669 161.2504 14.72361714 55800Epoch: 2025-12-09T05:01Z
TLE epoch observation values (Epoch: 2025-12-09T05:01:36.627Z)
Latitude
-0.00006°
Longitude
-12.28012°
Altitude
657.165 km
Speed
7.529 km/s
True Right ascension
09h 25m 16s
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
10:05:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.246 km
Perigee altitude
649.941 km
Semi-major axis
7,028.731 km
Eccentricity
0.00009
Inclination
97.9855°
RAAN
141.3199°
Arg. of periapsis
198.8669°
True anomaly
161.25382°
Mean anomaly
161.2504°
Eccentric anomaly
161.25211°
Mean motion
3.68322 °/min
Orbital period
97.74 mins
BSTAR
0.00024458
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Other satellites on launch #219 in the year 2024 (2024-11-25 UTC)
Did you know?
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 | 2025-12-09 23:31:49.125Z | 14.537° NNE | 2025-12-09 23:35:49.125Z | 52.677° ENE | 44.382° | 2025-12-09 23:39:49.125Z | 190.405° SSW |
| 7 mins | 2025-12-10 10:30:49.125Z | 154.424° SSE | 2025-12-10 10:33:49.125Z | 107.783° ESE | 41.765° | 2025-12-10 10:37:49.125Z | 354.653° N |
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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