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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-2A
1 62932U 25028E 26171.42265801 .00000969 00000-0 15741-3 0 9999
2 62932 98.1300 226.8077 0005495 144.3571 215.8005 14.73388905 73082Epoch: 2026-06-20T10:08Z
TLE epoch observation values (Epoch: 2026-06-20T10:08:37.652Z)
Latitude
0.00006°
Longitude
166.0133°
Altitude
656.409 km
Speed
7.528 km/s
True Right ascension
15h 07m 13s
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
07:21:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.191 km
Perigee altitude
643.47 km
Semi-major axis
7,025.467 km
Eccentricity
0.00055
Inclination
98.13°
RAAN
226.8077°
Arg. of periapsis
144.3571°
True anomaly
215.76369°
Mean anomaly
215.8005°
Eccentric anomaly
215.78209°
Mean motion
3.68579 °/min
Orbital period
97.67 mins
BSTAR
0.00015741
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 02:35:59.693Z | 104.293° ESE | 2026-06-21 02:38:59.693Z | 59.335° ENE | 17.024° | 2026-06-21 02:40:59.693Z | 29.853° NE |
| 7 mins | 2026-06-21 04:11:59.693Z | 196.766° SSW | 2026-06-21 04:14:59.693Z | 260.907° W | 33.966° | 2026-06-21 04:18:59.693Z | 331.673° NNW |
| 7 mins | 2026-06-21 16:03:59.693Z | 36.29° NE | 2026-06-21 16:06:59.693Z | 94.604° ESE | 31.444° | 2026-06-21 16:10:59.693Z | 165.492° S |
| 4 mins | 2026-06-21 17:41:59.693Z | 320.102° NNW | 2026-06-21 17:43:59.693Z | 285.101° WNW | 18.287° | 2026-06-21 17:45:59.693Z | 255.086° W |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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