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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-5D
1 62082U 24219B 25319.55912903 .00000160 00000-0 33152-4 0 9995
2 62082 97.9850 118.0817 0001167 0.6240 359.4968 14.72292948 52325Epoch: 2025-11-15T13:25Z
TLE epoch observation values (Epoch: 2025-11-15T13:25:08.748Z)
Latitude
-0.00008°
Longitude
-138.09128°
Altitude
655.945 km
Speed
7.53 km/s
True Right ascension
07h 52m 19s
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
21:14:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.633 km
Perigee altitude
649.992 km
Semi-major axis
7,028.95 km
Eccentricity
0.00012
Inclination
97.985°
RAAN
118.0817°
Arg. of periapsis
0.624°
True anomaly
359.49668°
Mean anomaly
359.4968°
Eccentric anomaly
359.49674°
Mean motion
3.68305 °/min
Orbital period
97.75 mins
BSTAR
0.000033152
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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 | 2025-11-16 10:43:55.460Z | 167.624° S | 2025-11-16 10:47:55.460Z | 181.139° SSW | 43.877° | 2025-11-16 10:51:55.460Z | 346.042° N |
| 5 mins | 2025-11-16 22:38:55.460Z | 61.347° ENE | 2025-11-16 22:40:55.460Z | 95.484° ESE | 19.377° | 2025-11-16 22:43:55.460Z | 140.151° SSE |
| 6 mins | 2025-11-17 00:14:55.460Z | 345.149° N | 2025-11-17 00:17:55.460Z | 282.358° WNW | 29.737° | 2025-11-17 00:20:55.460Z | 229.597° WSW |
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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