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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-2B
1 62934U 25028G 26091.12280489 .00001807 00000-0 28783-3 0 9990
2 62934 97.9748 145.3660 0004428 56.7532 303.4100 14.73184980 61318Epoch: 2026-04-01T02:56Z
TLE epoch observation values (Epoch: 2026-04-01T02:56:50.342Z)
Latitude
-0.00001°
Longitude
-88.33392°
Altitude
652.215 km
Speed
7.532 km/s
True Right ascension
09h 41m 27s
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
15:51:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.083 km
Perigee altitude
644.861 km
Semi-major axis
7,026.109 km
Eccentricity
0.00044
Inclination
97.9748°
RAAN
145.366°
Arg. of periapsis
56.7532°
True anomaly
303.36763°
Mean anomaly
303.41°
Eccentric anomaly
303.38882°
Mean motion
3.68528 °/min
Orbital period
97.69 mins
BSTAR
0.00028783
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-01 16:32:44.300Z | 9.482° NNE | 2026-04-01 16:36:44.300Z | 331.886° NNW | 43.509° | 2026-04-01 16:40:44.300Z | 199.712° SSW |
| 7 mins | 2026-04-02 03:31:44.300Z | 163.86° S | 2026-04-02 03:34:44.300Z | 130.202° SE | 44.745° | 2026-04-02 03:38:44.300Z | 348.641° N |
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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