KINEIS-4B, 63304
Orbit data source: Space-Track
KINEIS-4B, 63304 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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63304 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-4B
1 63304U 25056E 25257.08810672 .00001640 00000-0 26623-3 0 9990
2 63304 97.9923 21.3308 0003797 81.6029 278.5608 14.72475807 26498Epoch: 2025-09-14T02:06Z
TLE epoch observation values (Epoch: 2025-09-14T02:06:52.42Z)
Latitude
-0.00012°
Longitude
-3.69974°
Altitude
655.787 km
Speed
7.53 km/s
True Right ascension
01h 25m 19s
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
02:17:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.899 km
Perigee altitude
647.562 km
Semi-major axis
7,028.367 km
Eccentricity
0.00038
Inclination
97.9923°
RAAN
21.3308°
Arg. of periapsis
81.6029°
True anomaly
278.51777°
Mean anomaly
278.5608°
Eccentric anomaly
278.53929°
Mean motion
3.68351 °/min
Orbital period
97.73 mins
BSTAR
0.00026623
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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-4B 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-15 21:05:14.024Z | 18.722° NNE | 2025-09-15 21:09:14.024Z | 118.825° SE | 42.984° | 2025-09-15 21:13:14.024Z | 185.234° SSW |
| 7 mins | 2025-09-16 08:04:14.024Z | 146.236° SSE | 2025-09-16 08:07:14.024Z | 72.639° E | 39.81° | 2025-09-16 08:11:14.024Z | 357.12° 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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