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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-5B
1 62085U 24219E 26041.19243638 .00002132 00000-0 30296-3 0 9999
2 62085 97.9900 205.8902 0001270 353.5377 6.5817 14.77957787 65242Epoch: 2026-02-10T04:37Z
TLE epoch observation values (Epoch: 2026-02-10T04:37:06.503Z)
Latitude
-0°
Longitude
-3.66332°
Altitude
637.909 km
Speed
7.54 km/s
True Right ascension
13h 43m 33s
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
13:19:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
633.716 km
Perigee altitude
631.935 km
Semi-major axis
7,010.962 km
Eccentricity
0.00013
Inclination
97.99°
RAAN
205.8902°
Arg. of periapsis
353.5377°
True anomaly
6.58337°
Mean anomaly
6.5817°
Eccentric anomaly
6.58253°
Mean motion
3.69723 °/min
Orbital period
97.37 mins
BSTAR
0.00030296
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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 | 2026-02-10 11:13:59.983Z | 185.694° SSW | 2026-02-10 11:17:59.983Z | 273.063° WNW | 37.464° | 2026-02-10 11:20:59.983Z | 332.119° NNW |
| 6 mins | 2026-02-10 23:04:59.983Z | 45.016° ENE | 2026-02-10 23:07:59.983Z | 105.609° ESE | 26.385° | 2026-02-10 23:10:59.983Z | 154.713° SSE |
| 5 mins | 2026-02-11 00:41:59.983Z | 327.839° NNW | 2026-02-11 00:43:59.983Z | 290.377° WNW | 21.717° | 2026-02-11 00:46:59.983Z | 242.96° WSW |
| 5 mins | 2026-02-11 10:01:59.983Z | 100.865° ESE | 2026-02-11 10:03:59.983Z | 60.737° ENE | 22.211° | 2026-02-11 10:06:59.983Z | 15.903° NNE |
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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