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: 15 hours ago
TLE from 15 hours ago
0 KINEIS-5B
1 62085U 24219E 25311.32536596 .00002976 00000-0 42528-3 0 9998
2 62085 97.9844 111.8767 0000820 253.4340 106.6780 14.77423916 51239Epoch: 2025-11-07T07:48Z
TLE epoch observation values (Epoch: 2025-11-07T07:48:31.618Z)
Latitude
-0.00008°
Longitude
-52.02598°
Altitude
640.648 km
Speed
7.538 km/s
True Right ascension
07h 27m 30s
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
19:09:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
635.091 km
Perigee altitude
633.94 km
Semi-major axis
7,012.652 km
Eccentricity
0.00008
Inclination
97.9844°
RAAN
111.8767°
Arg. of periapsis
253.434°
True anomaly
106.687°
Mean anomaly
106.678°
Eccentric anomaly
106.6825°
Mean motion
3.6959 °/min
Orbital period
97.41 mins
BSTAR
0.00042528
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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 | 2025-11-07 23:01:08.392Z | 39.447° NE | 2025-11-07 23:04:08.392Z | 88.648° E | 25.886° | 2025-11-07 23:08:08.392Z | 156.573° SSE |
| 5 mins | 2025-11-08 00:39:08.392Z | 323.521° NNW | 2025-11-08 00:41:08.392Z | 283.45° WNW | 21.973° | 2025-11-08 00:44:08.392Z | 239.512° WSW |
| 5 mins | 2025-11-08 09:59:08.392Z | 98.433° ESE | 2025-11-08 10:01:08.392Z | 58.295° ENE | 21.746° | 2025-11-08 10:04:08.392Z | 15.31° NNE |
| 5 mins | 2025-11-08 11:35:08.392Z | 222.952° SW | 2025-11-08 11:37:08.392Z | 267.403° W | 26.237° | 2025-11-08 11:40:08.392Z | 319.41° NNW |
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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