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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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: 20 hours ago
TLE from 20 hours ago
0 KINEIS-4B
1 63304U 25056E 26084.75876858 -.00000358 00000-0 -48902-4 0 9993
2 63304 97.9844 210.9142 0003916 150.2131 209.9300 14.72339106 54840Epoch: 2026-03-25T18:12Z
TLE epoch observation values (Epoch: 2026-03-25T18:12:37.605Z)
Latitude
-0.00002°
Longitude
114.54005°
Altitude
659.006 km
Speed
7.527 km/s
True Right ascension
14h 03m 39s
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
19:31:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.418 km
Perigee altitude
647.913 km
Semi-major axis
7,028.803 km
Eccentricity
0.00039
Inclination
97.9844°
RAAN
210.9142°
Arg. of periapsis
150.2131°
True anomaly
209.90762°
Mean anomaly
209.93°
Eccentric anomaly
209.91881°
Mean motion
3.68316 °/min
Orbital period
97.74 mins
BSTAR
-0.000048902
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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 | 2026-03-26 20:52:52.266Z | 25.589° NE | 2026-03-26 20:56:52.266Z | 115.205° SE | 37.689° | 2026-03-26 21:00:52.266Z | 176.534° S |
| 7 mins | 2026-03-27 07:51:52.266Z | 135.263° SSE | 2026-03-27 07:54:52.266Z | 70.538° E | 34.09° | 2026-03-27 07:58:52.266Z | 2.32° NNE |
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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