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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 KINEIS-5B
1 62085U 24219E 25257.61300505 .00001158 00000-0 17098-3 0 9993
2 62085 97.9808 58.7095 0003134 85.4303 274.7265 14.77132088 43306Epoch: 2025-09-14T14:42Z
TLE epoch observation values (Epoch: 2025-09-14T14:42:43.636Z)
Latitude
-0.00002°
Longitude
-155.80182°
Altitude
641.226 km
Speed
7.537 km/s
True Right ascension
03h 54m 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
23:32:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
637.638 km
Perigee altitude
633.242 km
Semi-major axis
7,013.577 km
Eccentricity
0.00031
Inclination
97.9808°
RAAN
58.7095°
Arg. of periapsis
85.4303°
True anomaly
274.69071°
Mean anomaly
274.7265°
Eccentric anomaly
274.7086°
Mean motion
3.69517 °/min
Orbital period
97.42 mins
BSTAR
0.00017098
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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
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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 | 2025-09-15 10:21:16.910Z | 138.536° SSE | 2025-09-15 10:24:16.910Z | 83.724° E | 33.911° | 2025-09-15 10:28:16.910Z | 3.402° NNE |
| 7 mins | 2025-09-15 23:48:16.910Z | 9.356° NNE | 2025-09-15 23:51:16.910Z | 302.148° NW | 44.591° | 2025-09-15 23:55:16.910Z | 197.812° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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