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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-5D
1 62082U 24219B 25305.62717030 .00001245 00000-0 20462-3 0 9996
2 62082 97.9846 104.3940 0002095 37.4244 322.7109 14.72316924 50271Epoch: 2025-11-01T15:03Z
TLE epoch observation values (Epoch: 2025-11-01T15:03:07.513Z)
Latitude
-0.00006°
Longitude
-162.54183°
Altitude
655.518 km
Speed
7.53 km/s
True Right ascension
06h 57m 34s
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
19:34:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.209 km
Perigee altitude
649.264 km
Semi-major axis
7,028.873 km
Eccentricity
0.00021
Inclination
97.9846°
RAAN
104.394°
Arg. of periapsis
37.4244°
True anomaly
322.69635°
Mean anomaly
322.7109°
Eccentric anomaly
322.70363°
Mean motion
3.68311 °/min
Orbital period
97.74 mins
BSTAR
0.00020462
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-01 23:49:20.342Z | 345.418° N | 2025-11-01 23:50:20.342Z | 272.599° WNW | 43.254° | 2025-11-01 23:54:20.342Z | 202.297° SSW |
| 7 mins | 2025-11-02 10:45:20.342Z | 168.273° S | 2025-11-02 10:48:20.342Z | 219.551° SW | 44.899° | 2025-11-02 10:52:20.342Z | 346.287° N |
| 4 mins | 2025-11-02 22:39:20.342Z | 66.296° ENE | 2025-11-02 22:41:20.342Z | 101.878° ESE | 19.119° | 2025-11-02 22:43:20.342Z | 132.997° SE |
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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