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: 4 hours ago
TLE from 4 hours ago
0 KINEIS-5B
1 62085U 24219E 26036.85948094 .00003694 00000-0 51978-3 0 9998
2 62085 97.9892 201.5927 0001560 8.6291 351.4946 14.77941119 64603Epoch: 2026-02-05T20:37Z
TLE epoch observation values (Epoch: 2026-02-05T20:37:39.153Z)
Latitude
-0.00002°
Longitude
116.1739°
Altitude
637.764 km
Speed
7.54 km/s
True Right ascension
13h 26m 22s
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
02:22:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
633.972 km
Perigee altitude
631.784 km
Semi-major axis
7,011.015 km
Eccentricity
0.00016
Inclination
97.9892°
RAAN
201.5927°
Arg. of periapsis
8.6291°
True anomaly
351.49196°
Mean anomaly
351.4946°
Eccentric anomaly
351.49328°
Mean motion
3.69719 °/min
Orbital period
97.37 mins
BSTAR
0.00051978
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-06 00:26:53.881Z | 345.385° N | 2026-02-06 00:29:53.881Z | 287.429° WNW | 28.133° | 2026-02-06 00:32:53.881Z | 232.721° WSW |
| 4 mins | 2026-02-06 09:47:53.881Z | 93.354° ESE | 2026-02-06 09:49:53.881Z | 60.429° ENE | 16.893° | 2026-02-06 09:51:53.881Z | 30.373° NE |
| 6 mins | 2026-02-06 11:22:53.881Z | 199.256° SSW | 2026-02-06 11:25:53.881Z | 269.399° W | 33.125° | 2026-02-06 11:28:53.881Z | 326.915° NNW |
| 6 mins | 2026-02-06 23:12:53.881Z | 39.9° NE | 2026-02-06 23:15:53.881Z | 107.061° ESE | 30.665° | 2026-02-06 23:18:53.881Z | 160.797° S |
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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