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: 1 day ago
TLE from 1 day ago
0 KINEIS-5B
1 62085U 24219E 25315.32119147 .00003459 00000-0 49271-3 0 9990
2 62085 97.9847 115.8341 0000964 226.6941 133.4189 14.77449808 51826Epoch: 2025-11-11T07:42Z
TLE epoch observation values (Epoch: 2025-11-11T07:42:30.943Z)
Latitude
0.00001°
Longitude
-50.50425°
Altitude
640.866 km
Speed
7.537 km/s
True Right ascension
07h 43m 20s
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
04:37:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
635.11 km
Perigee altitude
633.757 km
Semi-major axis
7,012.571 km
Eccentricity
0.0001
Inclination
97.9847°
RAAN
115.8341°
Arg. of periapsis
226.6941°
True anomaly
133.42692°
Mean anomaly
133.4189°
Eccentric anomaly
133.42291°
Mean motion
3.69596 °/min
Orbital period
97.4 mins
BSTAR
0.00049271
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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 | 2025-11-12 09:51:35.996Z | 114.426° SE | 2025-11-12 09:54:35.996Z | 70.319° E | 19.614° | 2025-11-12 09:57:35.996Z | 22.829° NE |
| 6 mins | 2025-11-12 11:28:35.996Z | 210.197° SW | 2025-11-12 11:30:35.996Z | 250.817° W | 29.038° | 2025-11-12 11:34:35.996Z | 325.935° NNW |
| 6 mins | 2025-11-12 23:18:35.996Z | 36.572° NE | 2025-11-12 23:21:35.996Z | 117.215° SE | 34.265° | 2025-11-12 23:24:35.996Z | 168.343° S |
| 4 mins | 2025-11-13 00:55:35.996Z | 320.53° NNW | 2025-11-13 00:57:35.996Z | 288.634° WNW | 15.887° | 2025-11-13 00:59:35.996Z | 259.81° W |
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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