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: 21 hours ago
TLE from 21 hours ago
0 KINEIS-5D
1 62082U 24219B 26088.17032626 -.00000861 00000-0 -12854-3 0 9997
2 62082 97.9306 249.1596 0004002 134.3372 225.8164 14.72331119 71984Epoch: 2026-03-29T04:05Z
TLE epoch observation values (Epoch: 2026-03-29T04:05:16.188Z)
Latitude
-0.00006°
Longitude
1.2621°
Altitude
658.609 km
Speed
7.527 km/s
True Right ascension
16h 36m 38s
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
06:10:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.501 km
Perigee altitude
647.876 km
Semi-major axis
7,028.826 km
Eccentricity
0.0004
Inclination
97.9306°
RAAN
249.1596°
Arg. of periapsis
134.3372°
True anomaly
225.78353°
Mean anomaly
225.8164°
Eccentric anomaly
225.79996°
Mean motion
3.68315 °/min
Orbital period
97.74 mins
BSTAR
-0.00012854
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-30 09:36:41.117Z | 99.933° ESE | 2026-03-30 09:38:41.117Z | 68.772° E | 17.866° | 2026-03-30 09:41:41.117Z | 24.376° NE |
| 6 mins | 2026-03-30 11:12:41.117Z | 202.403° SSW | 2026-03-30 11:15:41.117Z | 274.778° WNW | 32.412° | 2026-03-30 11:18:41.117Z | 327.135° NNW |
| 6 mins | 2026-03-30 23:05:41.117Z | 42.145° NE | 2026-03-30 23:07:41.117Z | 89.773° E | 33.584° | 2026-03-30 23:11:41.117Z | 167.705° S |
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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