KINEIS-4E, 63300
Orbit data source: Space-Track
KINEIS-4E, 63300 is a French payload satellite in SSO that was launched on Tue, 18 Mar 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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63300 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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-4E
1 63300U 25056A 26319.19153264 .00001767 00000-0 28720-3 0 9995
2 63300 97.9207 79.0558 0002490 64.1936 295.9529 14.72301466 89345Epoch: 2026-11-15T04:35Z
TLE epoch observation values (Epoch: 2026-11-15T04:35:48.420Z)
Latitude
0.00007°
Longitude
-44.18147°
Altitude
655.975 km
Speed
7.53 km/s
True Right ascension
05h 16m 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
06:17:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.533 km
Perigee altitude
649.032 km
Semi-major axis
7,028.92 km
Eccentricity
0.00025
Inclination
97.9207°
RAAN
79.0558°
Arg. of periapsis
64.1936°
True anomaly
295.92724°
Mean anomaly
295.9529°
Eccentric anomaly
295.94007°
Mean motion
3.68307 °/min
Orbital period
97.74 mins
BSTAR
0.0002872
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Other satellites on launch #56 in the year 2025 (2025-03-18 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-4E 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 | 2026-11-15 21:29:14.314Z | 352.171° N | 2026-11-15 21:32:14.314Z | 278.457° WNW | 46.347° | 2026-11-15 21:36:14.314Z | 214.815° SW |
| 7 mins | 2026-11-16 08:27:14.314Z | 185.286° SSW | 2026-11-16 08:30:14.314Z | 259.228° W | 57.984° | 2026-11-16 08:34:14.314Z | 337.944° N |
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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