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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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: 13 hours ago
TLE from 13 hours ago
0 KINEIS-4D
1 63302U 25056C 26163.84901094 .00001526 00000-0 24890-3 0 9995
2 63302 97.9010 288.0915 0002475 25.7578 334.3752 14.72336110 66497Epoch: 2026-06-12T20:22Z
TLE epoch observation values (Epoch: 2026-06-12T20:22:34.545Z)
Latitude
-0.00007°
Longitude
81.27501°
Altitude
655.062 km
Speed
7.531 km/s
True Right ascension
19h 12m 21s
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
19:39:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.411 km
Perigee altitude
648.932 km
Semi-major axis
7,028.808 km
Eccentricity
0.00025
Inclination
97.901°
RAAN
288.0915°
Arg. of periapsis
25.7578°
True anomaly
334.36293°
Mean anomaly
334.3752°
Eccentric anomaly
334.36907°
Mean motion
3.68316 °/min
Orbital period
97.74 mins
BSTAR
0.0002489
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-13 09:33:53.675Z | 240.169° WSW | 2026-06-13 09:35:53.675Z | 268.176° W | 13.794° | 2026-06-13 09:37:53.675Z | 296.298° NW |
| 7 mins | 2026-06-13 21:24:53.675Z | 3.461° NNE | 2026-06-13 21:27:53.675Z | 313.148° NW | 41.254° | 2026-06-13 21:31:53.675Z | 206.39° SW |
| 7 mins | 2026-06-14 08:23:53.675Z | 172.818° S | 2026-06-14 08:26:53.675Z | 318.717° NNW | 43.183° | 2026-06-14 08:30:53.675Z | 345.192° N |
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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