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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 KINEIS-4D
1 63302U 25056C 25260.53343966 .00002055 00000-0 33222-3 0 9993
2 63302 97.9923 24.7628 0002816 114.8949 245.2552 14.72381205 27015Epoch: 2025-09-17T12:48Z
TLE epoch observation values (Epoch: 2025-09-17T12:48:09.186Z)
Latitude
0.00003°
Longitude
-163.9835°
Altitude
657.314 km
Speed
7.528 km/s
True Right ascension
01h 39m 03s
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
11:41:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.511 km
Perigee altitude
648.553 km
Semi-major axis
7,028.669 km
Eccentricity
0.00028
Inclination
97.9923°
RAAN
24.7628°
Arg. of periapsis
114.8949°
True anomaly
245.2259°
Mean anomaly
245.2552°
Eccentric anomaly
245.24055°
Mean motion
3.68327 °/min
Orbital period
97.74 mins
BSTAR
0.00033222
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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 | 2025-09-18 20:22:19.424Z | 42.005° NE | 2025-09-18 20:26:19.424Z | 104.941° ESE | 21.277° | 2025-09-18 20:29:19.424Z | 147.512° SSE |
| 6 mins | 2025-09-18 22:00:19.424Z | 337.042° NNW | 2025-09-18 22:02:19.424Z | 297.741° NW | 26.942° | 2025-09-18 22:06:19.424Z | 230.223° WSW |
| 5 mins | 2025-09-19 07:22:19.424Z | 101.785° ESE | 2025-09-19 07:24:19.424Z | 69.038° E | 19.286° | 2025-09-19 07:27:19.424Z | 23.016° NE |
| 6 mins | 2025-09-19 08:58:19.424Z | 205.848° SW | 2025-09-19 09:01:19.424Z | 273.381° WNW | 30.353° | 2025-09-19 09:04:19.424Z | 324.835° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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