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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-4D
1 63302U 25056C 26319.13924177 .00001970 00000-0 31961-3 0 9997
2 63302 97.9183 79.1881 0002239 183.2884 176.8309 14.72270490 89341Epoch: 2026-11-15T03:20Z
TLE epoch observation values (Epoch: 2026-11-15T03:20:30.488Z)
Latitude
-0.00008°
Longitude
-25.17289°
Altitude
658.412 km
Speed
7.527 km/s
True Right ascension
05h 16m 45s
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
06:09:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.455 km
Perigee altitude
649.307 km
Semi-major axis
7,029.018 km
Eccentricity
0.00022
Inclination
97.9183°
RAAN
79.1881°
Arg. of periapsis
183.2884°
True anomaly
176.83232°
Mean anomaly
176.8309°
Eccentric anomaly
176.83161°
Mean motion
3.683 °/min
Orbital period
97.75 mins
BSTAR
0.00031961
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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 | 2026-11-15 20:14:13.272Z | 41.805° NE | 2026-11-15 20:17:13.272Z | 87.984° E | 25.858° | 2026-11-15 20:21:13.272Z | 151.907° SSE |
| 5 mins | 2026-11-15 21:52:13.272Z | 331.883° NNW | 2026-11-15 21:54:13.272Z | 292.195° WNW | 28.037° | 2026-11-15 21:57:13.272Z | 239.621° WSW |
| 5 mins | 2026-11-16 07:14:13.272Z | 100.72° ESE | 2026-11-16 07:16:13.272Z | 64.895° ENE | 22.469° | 2026-11-16 07:19:13.272Z | 19.708° NNE |
| 6 mins | 2026-11-16 08:50:13.272Z | 211.497° SW | 2026-11-16 08:52:13.272Z | 249.942° W | 32.609° | 2026-11-16 08:56:13.272Z | 324.362° NNW |
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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