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: 4 hours ago
TLE from 4 hours ago
0 KINEIS-4D
1 63302U 25056C 25309.33177172 .00002878 00000-0 46204-3 0 9996
2 63302 97.9991 72.7566 0001118 9.2949 350.8279 14.72400692 34193Epoch: 2025-11-05T07:57Z
TLE epoch observation values (Epoch: 2025-11-05T07:57:45.076Z)
Latitude
-0.00003°
Longitude
-91.48718°
Altitude
655.646 km
Speed
7.53 km/s
True Right ascension
04h 51m 01s
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
07:46:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.256 km
Perigee altitude
649.684 km
Semi-major axis
7,028.607 km
Eccentricity
0.00011
Inclination
97.9991°
RAAN
72.7566°
Arg. of periapsis
9.2949°
True anomaly
350.82586°
Mean anomaly
350.8279°
Eccentric anomaly
350.82688°
Mean motion
3.68332 °/min
Orbital period
97.74 mins
BSTAR
0.00046204
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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 | 2025-11-05 21:35:07.661Z | 359.131° N | 2025-11-05 21:38:07.661Z | 295.27° NW | 39.409° | 2025-11-05 21:42:07.661Z | 210.683° SW |
| 7 mins | 2025-11-06 08:33:07.661Z | 177.467° S | 2025-11-06 08:36:07.661Z | 229.209° WSW | 42.291° | 2025-11-06 08:40:07.661Z | 340.459° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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