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 25309.94338609 .00003126 00000-0 50107-3 0 9991
2 63302 97.9992 73.3586 0001085 6.6634 353.4587 14.72405270 34286Epoch: 2025-11-05T22:38Z
TLE epoch observation values (Epoch: 2025-11-05T22:38:28.558Z)
Latitude
-0.00008°
Longitude
48.33081°
Altitude
655.65 km
Speed
7.53 km/s
True Right ascension
04h 53m 26s
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
02:39:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.218 km
Perigee altitude
649.693 km
Semi-major axis
7,028.592 km
Eccentricity
0.00011
Inclination
97.9992°
RAAN
73.3586°
Arg. of periapsis
6.6634°
True anomaly
353.45728°
Mean anomaly
353.4587°
Eccentric anomaly
353.45799°
Mean motion
3.68333 °/min
Orbital period
97.74 mins
BSTAR
0.00050107
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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 | 2025-11-06 08:33:10.620Z | 177.621° S | 2025-11-06 08:36:10.620Z | 233.236° WSW | 42.466° | 2025-11-06 08:40:10.620Z | 340.587° N |
| 5 mins | 2025-11-06 20:27:10.620Z | 60.201° ENE | 2025-11-06 20:29:10.620Z | 99.963° ESE | 23.185° | 2025-11-06 20:32:10.620Z | 147.479° SSE |
| 6 mins | 2025-11-06 22:03:10.620Z | 338.248° N | 2025-11-06 22:06:10.620Z | 279.023° WNW | 25.067° | 2025-11-06 22:09:10.620Z | 234.408° 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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