KINEIS-2A, 62932
Orbit data source: Space-Track
KINEIS-2A, 62932 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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62932 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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-2A
1 62932U 25028E 26038.64354515 .00001725 00000-0 28264-3 0 9991
2 62932 98.0506 94.3900 0004340 268.8055 91.2654 14.72017071 53546Epoch: 2026-02-07T15:26Z
TLE epoch observation values (Epoch: 2026-02-07T15:26:42.300Z)
Latitude
-0.00014°
Longitude
84.94965°
Altitude
657.711 km
Speed
7.529 km/s
True Right ascension
06h 17m 33s
True Declination
0° 00' 01"
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
22:12:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
654.745 km
Perigee altitude
648.644 km
Semi-major axis
7,029.831 km
Eccentricity
0.00043
Inclination
98.0506°
RAAN
94.39°
Arg. of periapsis
268.8055°
True anomaly
91.31512°
Mean anomaly
91.2654°
Eccentric anomaly
91.29026°
Mean motion
3.68236 °/min
Orbital period
97.76 mins
BSTAR
0.00028264
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Other satellites on launch #28 in the year 2025 (2025-02-08 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.KINEIS-2A Visibility forecast
Loading observer location...
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 | 2026-02-08 03:00:14.871Z | 130.425° SE | 2026-02-08 03:03:14.871Z | 74.878° E | 30.452° | 2026-02-08 03:07:14.871Z | 6.109° NNE |
| 5 mins | 2026-02-08 04:38:14.871Z | 232.777° WSW | 2026-02-08 04:40:14.871Z | 266.002° W | 19.006° | 2026-02-08 04:43:14.871Z | 310.866° NW |
| 7 mins | 2026-02-08 16:30:14.871Z | 14.053° NNE | 2026-02-08 16:33:14.871Z | 182.679° SSW | 44.277° | 2026-02-08 16:37:14.871Z | 193.073° 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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