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: 8 hours ago
TLE from 8 hours ago
0 KINEIS-2A
1 62932U 25028E 26278.17133356 .00000860 00000-0 13997-3 0 9999
2 62932 98.1184 333.7023 0005011 161.7329 198.4060 14.73600654 88800Epoch: 2026-10-05T04:06Z
TLE epoch observation values (Epoch: 2026-10-05T04:06:43.219Z)
Latitude
0.00001°
Longitude
-101.83184°
Altitude
655.945 km
Speed
7.528 km/s
True Right ascension
22h 14m 48s
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
05:56:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.176 km
Perigee altitude
643.136 km
Semi-major axis
7,024.793 km
Eccentricity
0.0005
Inclination
98.1184°
RAAN
333.7023°
Arg. of periapsis
161.7329°
True anomaly
198.38788°
Mean anomaly
198.406°
Eccentric anomaly
198.39694°
Mean motion
3.68632 °/min
Orbital period
97.66 mins
BSTAR
0.00013997
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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 | 2026-10-05 16:06:20.368Z | 38.679° NE | 2026-10-05 16:09:20.368Z | 94.61° ESE | 34.117° | 2026-10-05 16:13:20.368Z | 162.268° S |
| 4 mins | 2026-10-05 17:44:20.368Z | 321.365° NNW | 2026-10-05 17:46:20.368Z | 284.443° WNW | 21.326° | 2026-10-05 17:48:20.368Z | 252.938° W |
| 5 mins | 2026-10-06 03:05:20.368Z | 109.257° ESE | 2026-10-06 03:07:20.368Z | 66.769° ENE | 29.305° | 2026-10-06 03:10:20.368Z | 15.331° NNE |
| 6 mins | 2026-10-06 04:41:20.368Z | 219.879° SW | 2026-10-06 04:44:20.368Z | 274.45° WNW | 24.487° | 2026-10-06 04:47:20.368Z | 318.259° NNW |
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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