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: 11 hours ago
TLE from 11 hours ago
0 KINEIS-4D
1 63302U 25056C 25353.90957177 .00001687 00000-0 27529-3 0 9995
2 63302 98.0024 116.6448 0001999 152.2569 207.8746 14.72210877 40756Epoch: 2025-12-19T21:49Z
TLE epoch observation values (Epoch: 2025-12-19T21:49:47.000Z)
Latitude
0.00002°
Longitude
60.455°
Altitude
658.27 km
Speed
7.528 km/s
True Right ascension
07h 46m 34s
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
07:46:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.48 km
Perigee altitude
649.67 km
Semi-major axis
7,029.212 km
Eccentricity
0.0002
Inclination
98.0024°
RAAN
116.6448°
Arg. of periapsis
152.2569°
True anomaly
207.86389°
Mean anomaly
207.8746°
Eccentric anomaly
207.86925°
Mean motion
3.68284 °/min
Orbital period
97.75 mins
BSTAR
0.00027529
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-20 09:22:34.904Z | 223.506° SW | 2025-12-20 09:25:34.904Z | 270.297° WNW | 18.943° | 2025-12-20 09:28:34.904Z | 313.193° NW |
| 7 mins | 2025-12-20 21:14:34.904Z | 13.561° NNE | 2025-12-20 21:17:34.904Z | 22.853° NE | 44.237° | 2025-12-20 21:21:34.904Z | 192.849° SSW |
| 7 mins | 2025-12-21 08:13:34.904Z | 154.842° SSE | 2025-12-21 08:16:34.904Z | 30.882° NE | 42.392° | 2025-12-21 08:20:34.904Z | 351.683° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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