KINEIS-4D, 63302
Orbit data source: Space-Track
KINEIS-4D, 63302 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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63302 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, 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-4D
1 63302U 25056C 25323.94200686 .00002703 00000-0 43337-3 0 9997
2 63302 98.0002 87.1382 0000525 277.3979 82.7169 14.72511448 36346Epoch: 2025-11-19T22:36Z
TLE epoch observation values (Epoch: 2025-11-19T22:36:29.392Z)
Latitude
-0.00002°
Longitude
48.80923°
Altitude
656.023 km
Speed
7.529 km/s
True Right ascension
05h 48m 33s
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
03:23:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.486 km
Perigee altitude
649.748 km
Semi-major axis
7,028.254 km
Eccentricity
0.00005
Inclination
98.0002°
RAAN
87.1382°
Arg. of periapsis
277.3979°
True anomaly
82.72287°
Mean anomaly
82.7169°
Eccentric anomaly
82.71988°
Mean motion
3.6836 °/min
Orbital period
97.73 mins
BSTAR
0.00043337
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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-4D 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 | 2025-11-20 08:31:15.837Z | 175.903° S | 2025-11-20 08:34:15.837Z | 237.809° WSW | 43.35° | 2025-11-20 08:38:15.837Z | 341.932° N |
| 5 mins | 2025-11-20 20:25:15.837Z | 63.273° ENE | 2025-11-20 20:27:15.837Z | 102.712° ESE | 22.143° | 2025-11-20 20:30:15.837Z | 147.433° SSE |
| 6 mins | 2025-11-20 22:01:15.837Z | 337.582° N | 2025-11-20 22:03:15.837Z | 300.312° NW | 26.139° | 2025-11-20 22:07:15.837Z | 232.019° WSW |
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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