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, 1.0 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 KINEIS-4B
1 63304U 25056E 26032.63316367 .00002350 00000-0 37869-3 0 9998
2 63304 98.0028 159.6381 0002279 5.5852 354.5380 14.72409428 47171Epoch: 2026-02-01T15:11Z
TLE epoch observation values (Epoch: 2026-02-01T15:11:45.341Z)
Latitude
-0.00005°
Longitude
159.85918°
Altitude
654.799 km
Speed
7.531 km/s
True Right ascension
10h 38m 33s
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
13:16:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.044 km
Perigee altitude
648.841 km
Semi-major axis
7,028.579 km
Eccentricity
0.00023
Inclination
98.0028°
RAAN
159.6381°
Arg. of periapsis
5.5852°
True anomaly
354.53551°
Mean anomaly
354.538°
Eccentric anomaly
354.53676°
Mean motion
3.68334 °/min
Orbital period
97.74 mins
BSTAR
0.00037869
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-03 19:59:31.400Z | 62.799° ENE | 2026-02-03 20:01:31.400Z | 89.764° E | 13.021° | 2026-02-03 20:03:31.400Z | 117.3° SE |
| 7 mins | 2026-02-03 21:35:31.400Z | 358.583° N | 2026-02-03 21:38:31.400Z | 296.268° NW | 38.881° | 2026-02-03 21:42:31.400Z | 211.64° SW |
| 7 mins | 2026-02-04 08:33:31.400Z | 178.442° S | 2026-02-04 08:36:31.400Z | 230.099° WSW | 41.84° | 2026-02-04 08:40:31.400Z | 339.77° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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