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: 14 hours ago
TLE from 14 hours ago
0 KINEIS-2B
1 62934U 25028G 26277.87723736 .00000785 00000-0 12807-3 0 9999
2 62934 97.9553 328.6988 0004305 144.2858 215.8639 14.73602106 88811Epoch: 2026-10-04T21:03Z
TLE epoch observation values (Epoch: 2026-10-04T21:03:13.307Z)
Latitude
-0.00004°
Longitude
-0.67082°
Altitude
655.056 km
Speed
7.529 km/s
True Right ascension
21h 54m 47s
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
04:36:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
649.668 km
Perigee altitude
643.62 km
Semi-major axis
7,024.781 km
Eccentricity
0.00043
Inclination
97.9553°
RAAN
328.6988°
Arg. of periapsis
144.2858°
True anomaly
215.83501°
Mean anomaly
215.8639°
Eccentric anomaly
215.84945°
Mean motion
3.68633 °/min
Orbital period
97.66 mins
BSTAR
0.00012807
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-10-05 15:34:19.247Z | 47.432° ENE | 2026-10-05 15:37:19.247Z | 99.743° ESE | 25.011° | 2026-10-05 15:40:19.247Z | 147.148° SSE |
| 6 mins | 2026-10-05 17:11:19.247Z | 337.623° N | 2026-10-05 17:13:19.247Z | 301.838° NW | 28.135° | 2026-10-05 17:17:19.247Z | 233.555° WSW |
| 5 mins | 2026-10-06 02:33:19.247Z | 98.572° ESE | 2026-10-06 02:35:19.247Z | 63.015° ENE | 21.487° | 2026-10-06 02:38:19.247Z | 19.343° NNE |
| 6 mins | 2026-10-06 04:09:19.247Z | 212.261° SW | 2026-10-06 04:11:19.247Z | 254.699° W | 34.348° | 2026-10-06 04:15:19.247Z | 326.509° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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