KINEIS-5B, 62085
Orbit data source: Space-Track
KINEIS-5B, 62085 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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62085 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 hours ago
TLE from 5 hours ago
0 KINEIS-5B
1 62085U 24219E 25346.20186150 .00003659 00000-0 51838-3 0 9993
2 62085 97.9847 146.4240 0002632 132.0059 228.1376 14.77642720 56382Epoch: 2025-12-12T04:50Z
TLE epoch observation values (Epoch: 2025-12-12T04:50:40.833Z)
Latitude
-0.00001°
Longitude
-7.39301°
Altitude
641.023 km
Speed
7.537 km/s
True Right ascension
09h 45m 41s
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
08:43:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
635.668 km
Perigee altitude
631.977 km
Semi-major axis
7,011.96 km
Eccentricity
0.00026
Inclination
97.9847°
RAAN
146.424°
Arg. of periapsis
132.0059°
True anomaly
228.11514°
Mean anomaly
228.1376°
Eccentric anomaly
228.12637°
Mean motion
3.69644 °/min
Orbital period
97.39 mins
BSTAR
0.00051838
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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-5B Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-12 11:28:17.718Z | 203.648° SW | 2025-12-12 11:31:17.718Z | 262.615° W | 29.567° | 2025-12-12 11:34:17.718Z | 321.35° NNW |
| 7 mins | 2025-12-12 23:18:17.718Z | 32.582° NE | 2025-12-12 23:21:17.718Z | 96.493° ESE | 34.749° | 2025-12-12 23:25:17.718Z | 170.66° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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