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: 17 hours ago
TLE from 17 hours ago
0 KINEIS-5B
1 62085U 24219E 25341.25850533 .00003838 00000-0 54380-3 0 9990
2 62085 97.9848 141.5266 0002430 142.7755 217.3624 14.77610327 55657Epoch: 2025-12-07T06:12Z
TLE epoch observation values (Epoch: 2025-12-07T06:12:14.860Z)
Latitude
-0.00004°
Longitude
-27.80978°
Altitude
641.248 km
Speed
7.537 km/s
True Right ascension
09h 26m 06s
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
21:11:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
635.629 km
Perigee altitude
632.221 km
Semi-major axis
7,012.062 km
Eccentricity
0.00024
Inclination
97.9848°
RAAN
141.5266°
Arg. of periapsis
142.7755°
True anomaly
217.34551°
Mean anomaly
217.3624°
Eccentric anomaly
217.35395°
Mean motion
3.69636 °/min
Orbital period
97.39 mins
BSTAR
0.0005438
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-07 23:03:51.028Z | 58.409° ENE | 2025-12-07 23:05:51.028Z | 104.447° ESE | 26.076° | 2025-12-07 23:08:51.028Z | 153.923° SSE |
| 5 mins | 2025-12-08 00:39:51.028Z | 328.993° NNW | 2025-12-08 00:41:51.028Z | 291.718° WNW | 21.945° | 2025-12-08 00:44:51.028Z | 243.164° WSW |
| 5 mins | 2025-12-08 09:59:51.028Z | 103.595° ESE | 2025-12-08 10:01:51.028Z | 65.142° ENE | 22.203° | 2025-12-08 10:04:51.028Z | 17.858° NNE |
| 5 mins | 2025-12-08 11:35:51.028Z | 218.776° SW | 2025-12-08 11:37:51.028Z | 259.374° W | 25.994° | 2025-12-08 11:40:51.028Z | 316.251° NNW |
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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