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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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: 13 hours ago
TLE from 13 hours ago
0 KINEIS-5B
1 62085U 24219E 26306.51936111 .00000727 00000-0 10651-3 0 9995
2 62085 98.0199 109.7109 0002193 152.0317 208.1012 14.78574036104442Epoch: 2026-11-02T12:27Z
TLE epoch observation values (Epoch: 2026-11-02T12:27:52.799Z)
Latitude
-0.00005°
Longitude
-119.0543°
Altitude
638.202 km
Speed
7.538 km/s
True Right ascension
07h 18m 50s
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
21:01:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.414 km
Perigee altitude
629.34 km
Semi-major axis
7,009.014 km
Eccentricity
0.00022
Inclination
98.0199°
RAAN
109.7109°
Arg. of periapsis
152.0317°
True anomaly
208.08937°
Mean anomaly
208.1012°
Eccentric anomaly
208.09528°
Mean motion
3.69877 °/min
Orbital period
97.33 mins
BSTAR
0.00010651
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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-5B 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 | 2026-11-03 11:19:35.644Z | 184.03° SSW | 2026-11-03 11:22:35.644Z | 242.165° WSW | 55.62° | 2026-11-03 11:26:35.644Z | 336.75° NNW |
| 5 mins | 2026-11-03 23:10:35.644Z | 56.635° ENE | 2026-11-03 23:12:35.644Z | 97.755° ESE | 27.026° | 2026-11-03 23:15:35.644Z | 149.043° SSE |
| 5 mins | 2026-11-04 00:46:35.644Z | 333.229° NNW | 2026-11-04 00:48:35.644Z | 296.052° NW | 25.854° | 2026-11-04 00:51:35.644Z | 242.668° 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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