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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 KINEIS-5D
1 62082U 24219B 25260.63653125 .00000790 00000-0 13255-3 0 9997
2 62082 97.9812 60.2070 0002735 124.4307 235.7160 14.72364621 43657Epoch: 2025-09-17T15:16Z
TLE epoch observation values (Epoch: 2025-09-17T15:16:36.3Z)
Latitude
0.00008°
Longitude
-165.75389°
Altitude
657.622 km
Speed
7.528 km/s
True Right ascension
04h 00m 49s
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
12:21:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.506 km
Perigee altitude
648.662 km
Semi-major axis
7,028.721 km
Eccentricity
0.00027
Inclination
97.9812°
RAAN
60.207°
Arg. of periapsis
124.4307°
True anomaly
235.69011°
Mean anomaly
235.716°
Eccentric anomaly
235.70305°
Mean motion
3.68323 °/min
Orbital period
97.74 mins
BSTAR
0.00013255
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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 | 2025-09-18 22:50:32.290Z | 37.493° NE | 2025-09-18 22:54:32.290Z | 102.183° ESE | 24.741° | 2025-09-18 22:57:32.290Z | 150.585° SSE |
| 6 mins | 2025-09-19 00:28:32.290Z | 335.657° NNW | 2025-09-19 00:30:32.290Z | 300.939° NW | 23.571° | 2025-09-19 00:34:32.290Z | 236.097° WSW |
| 5 mins | 2025-09-19 09:50:32.290Z | 107.805° ESE | 2025-09-19 09:52:32.290Z | 73.267° E | 21.961° | 2025-09-19 09:55:32.290Z | 22.255° NNE |
| 6 mins | 2025-09-19 11:26:32.290Z | 209.627° SW | 2025-09-19 11:29:32.290Z | 266.733° W | 27.017° | 2025-09-19 11:32:32.290Z | 319.45° NNW |
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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