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: 15 hours ago
TLE from 15 hours ago
0 KINEIS-2A
1 62932U 25028E 25299.11299782 .00001992 00000-0 32280-3 0 9994
2 62932 98.0162 351.2345 0002919 161.1926 198.9390 14.72335557 38169Epoch: 2025-10-26T02:42Z
TLE epoch observation values (Epoch: 2025-10-26T02:42:43.011Z)
Latitude
-0.00001°
Longitude
-84.17857°
Altitude
658.571 km
Speed
7.527 km/s
True Right ascension
23h 24m 56s
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
12:44:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.73 km
Perigee altitude
648.627 km
Semi-major axis
7,028.815 km
Eccentricity
0.00029
Inclination
98.0162°
RAAN
351.2345°
Arg. of periapsis
161.1926°
True anomaly
198.92815°
Mean anomaly
198.939°
Eccentric anomaly
198.93357°
Mean motion
3.68315 °/min
Orbital period
97.74 mins
BSTAR
0.0003228
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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-2A 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 | 2025-10-27 03:19:01.474Z | 146.073° SSE | 2025-10-27 03:22:01.474Z | 62.297° ENE | 40.045° | 2025-10-27 03:26:01.474Z | 356.262° N |
| 7 mins | 2025-10-27 16:48:01.474Z | 0.319° NNE | 2025-10-27 16:51:01.474Z | 299.631° NW | 39.884° | 2025-10-27 16:55:01.474Z | 209.793° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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