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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-5D
1 62082U 24219B 25259.68510501 .00000804 00000-0 13484-3 0 9990
2 62082 97.9811 59.2728 0002698 126.1537 233.9920 14.72363031 43519Epoch: 2025-09-16T16:26Z
TLE epoch observation values (Epoch: 2025-09-16T16:26:33.072Z)
Latitude
-0.00009°
Longitude
176.76315°
Altitude
657.659 km
Speed
7.528 km/s
True Right ascension
03h 57m 05s
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
17:54:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.486 km
Perigee altitude
648.693 km
Semi-major axis
7,028.726 km
Eccentricity
0.00027
Inclination
97.9811°
RAAN
59.2728°
Arg. of periapsis
126.1537°
True anomaly
233.967°
Mean anomaly
233.992°
Eccentric anomaly
233.9795°
Mean motion
3.68322 °/min
Orbital period
97.74 mins
BSTAR
0.00013484
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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 | 2025-09-17 10:30:28.463Z | 154.049° SSE | 2025-09-17 10:34:28.463Z | 47.578° ENE | 41.54° | 2025-09-17 10:38:28.463Z | 353.778° N |
| 7 mins | 2025-09-18 00:00:28.463Z | 356.193° N | 2025-09-18 00:03:28.463Z | 288.85° WNW | 37.711° | 2025-09-18 00:07:28.463Z | 213.159° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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