KINEIS-2B, 62934
Orbit data source: Space-Track
KINEIS-2B, 62934 is a French payload satellite in SSO that was launched on Sat, 08 Feb 2025 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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62934 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: 9 hours ago
TLE from 9 hours ago
0 KINEIS-2B
1 62934U 25028G 26171.46790903 .00000976 00000-0 15815-3 0 9991
2 62934 97.9666 224.2706 0004753 129.3295 230.8335 14.73391598 73141Epoch: 2026-06-20T11:13Z
TLE epoch observation values (Epoch: 2026-06-20T11:13:47.340Z)
Latitude
-0.00001°
Longitude
147.14125°
Altitude
655.383 km
Speed
7.529 km/s
True Right ascension
14h 57m 04s
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
07:22:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.653 km
Perigee altitude
643.975 km
Semi-major axis
7,025.451 km
Eccentricity
0.00048
Inclination
97.9666°
RAAN
224.2706°
Arg. of periapsis
129.3295°
True anomaly
230.79129°
Mean anomaly
230.8335°
Eccentric anomaly
230.81239°
Mean motion
3.6858 °/min
Orbital period
97.67 mins
BSTAR
0.00015815
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Other satellites on launch #28 in the year 2025 (2025-02-08 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-2B 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 | 2026-06-21 03:39:55.912Z | 174.487° S | 2026-06-21 03:42:55.912Z | 304.082° NW | 43.416° | 2026-06-21 03:46:55.912Z | 344.209° N |
| 5 mins | 2026-06-21 15:32:55.912Z | 63.845° ENE | 2026-06-21 15:34:55.912Z | 101.548° ESE | 20.773° | 2026-06-21 15:37:55.912Z | 145.378° SSE |
| 6 mins | 2026-06-21 17:08:55.912Z | 338.929° N | 2026-06-21 17:10:55.912Z | 300.469° NW | 27.291° | 2026-06-21 17:14:55.912Z | 229.888° WSW |
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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