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: 5 days ago
TLE from 5 days ago
0 KINEIS-5D
1 62082U 24219B 25288.70457819 .00001394 00000-0 22799-3 0 9991
2 62082 97.9837 87.7710 0002824 71.2427 288.9087 14.72359959 47784Epoch: 2025-10-15T16:54Z
TLE epoch observation values (Epoch: 2025-10-15T16:54:35.555Z)
Latitude
-0.00001°
Longitude
169.64803°
Altitude
655.91 km
Speed
7.53 km/s
True Right ascension
05h 51m 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
21:15:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.584 km
Perigee altitude
648.614 km
Semi-major axis
7,028.736 km
Eccentricity
0.00028
Inclination
97.9837°
RAAN
87.771°
Arg. of periapsis
71.2427°
True anomaly
288.87808°
Mean anomaly
288.9087°
Eccentric anomaly
288.89339°
Mean motion
3.68322 °/min
Orbital period
97.74 mins
BSTAR
0.00022799
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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 | 2025-10-21 10:02:54.330Z | 130.45° SE | 2025-10-21 10:06:54.330Z | 56.768° ENE | 27.895° | 2025-10-21 10:09:54.330Z | 10.243° NNE |
| 5 mins | 2025-10-21 11:40:54.330Z | 226.301° WSW | 2025-10-21 11:42:54.330Z | 259.114° W | 20.285° | 2025-10-21 11:45:54.330Z | 308.896° NW |
| 7 mins | 2025-10-21 23:32:54.330Z | 16.923° NNE | 2025-10-21 23:35:54.330Z | 139.155° SSE | 44.387° | 2025-10-21 23:39:54.330Z | 189.968° SSW |
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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