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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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: 17 hours ago
TLE from 17 hours ago
0 KINEIS-2A
1 62932U 25028E 26308.11541856 .00000677 00000-0 11164-3 0 9995
2 62932 98.1140 3.6546 0005789 85.3923 274.7946 14.73659044 93217Epoch: 2026-11-04T02:46Z
TLE epoch observation values (Epoch: 2026-11-04T02:46:12.163Z)
Latitude
-0.00002°
Longitude
-81.26444°
Altitude
652.08 km
Speed
7.532 km/s
True Right ascension
00h 14m 37s
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
16:02:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.537 km
Perigee altitude
642.404 km
Semi-major axis
7,024.607 km
Eccentricity
0.00058
Inclination
98.114°
RAAN
3.6546°
Arg. of periapsis
85.3923°
True anomaly
274.72849°
Mean anomaly
274.7946°
Eccentric anomaly
274.76155°
Mean motion
3.68646 °/min
Orbital period
97.65 mins
BSTAR
0.00011164
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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 | 2026-11-05 03:20:56.301Z | 136.392° SSE | 2026-11-05 03:23:56.301Z | 80.211° E | 41.329° | 2026-11-05 03:27:56.301Z | 3.766° NNE |
| 4 mins | 2026-11-05 04:59:56.301Z | 249.411° W | 2026-11-05 05:00:56.301Z | 265.801° W | 17.188° | 2026-11-05 05:03:56.301Z | 308.37° NW |
| 7 mins | 2026-11-05 16:49:56.301Z | 9.777° NNE | 2026-11-05 16:52:56.301Z | 258.818° W | 81.325° | 2026-11-05 16:56:56.301Z | 197.382° 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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