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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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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-2B
1 62934U 25028G 26007.70794971 .00001474 00000-0 23776-3 0 9994
2 62934 97.9900 63.3512 0002501 320.3830 39.7195 14.72902390 49034Epoch: 2026-01-07T16:59Z
TLE epoch observation values (Epoch: 2026-01-07T16:59:26.854Z)
Latitude
-0.00003°
Longitude
61.21678°
Altitude
653.474 km
Speed
7.532 km/s
True Right ascension
04h 13m 24s
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
23:15:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.63 km
Perigee altitude
647.115 km
Semi-major axis
7,027.009 km
Eccentricity
0.00025
Inclination
97.99°
RAAN
63.3512°
Arg. of periapsis
320.383°
True anomaly
39.73782°
Mean anomaly
39.7195°
Eccentric anomaly
39.72866°
Mean motion
3.68457 °/min
Orbital period
97.7 mins
BSTAR
0.00023776
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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 | 2026-01-08 02:54:30.742Z | 129.943° SE | 2026-01-08 02:57:30.742Z | 82.031° E | 28.179° | 2026-01-08 03:01:30.742Z | 9.389° NNE |
| 5 mins | 2026-01-08 04:32:30.742Z | 228.177° WSW | 2026-01-08 04:34:30.742Z | 261.823° W | 20.259° | 2026-01-08 04:37:30.742Z | 310.239° NW |
| 7 mins | 2026-01-08 16:23:30.742Z | 15.914° NNE | 2026-01-08 16:26:30.742Z | 40.495° NE | 43.264° | 2026-01-08 16:30:30.742Z | 189.302° SSW |
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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