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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 KINEIS-2A
1 62932U 25028E 25257.72450599 .00000957 00000-0 15939-3 0 9992
2 62932 98.0214 310.4113 0001784 346.4794 13.6366 14.72263362 32071Epoch: 2025-09-14T17:23Z
TLE epoch observation values (Epoch: 2025-09-14T17:23:17.317Z)
Latitude
0.00005°
Longitude
55.64974°
Altitude
655.64 km
Speed
7.53 km/s
True Right ascension
20h 41m 38s
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
04:51:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.162 km
Perigee altitude
649.654 km
Semi-major axis
7,029.045 km
Eccentricity
0.00018
Inclination
98.0214°
RAAN
310.4113°
Arg. of periapsis
346.4794°
True anomaly
13.64142°
Mean anomaly
13.6366°
Eccentric anomaly
13.63901°
Mean motion
3.68297 °/min
Orbital period
97.75 mins
BSTAR
0.00015939
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-15 16:48:33.140Z | 356.733° N | 2025-09-15 16:51:33.140Z | 260.315° W | 39.208° | 2025-09-15 16:54:33.140Z | 211.074° SW |
| 7 mins | 2025-09-16 03:46:33.140Z | 178.031° S | 2025-09-16 03:49:33.140Z | 281.246° WNW | 42.993° | 2025-09-16 03:53:33.140Z | 342.221° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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