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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-4B
1 63304U 25056E 25292.97216333 .00004940 00000-0 79036-3 0 9993
2 63304 97.9971 56.6189 0001905 338.5640 21.5487 14.72232278 31772Epoch: 2025-10-19T23:19Z
TLE epoch observation values (Epoch: 2025-10-19T23:19:54.911Z)
Latitude
-0.00007°
Longitude
37.95895°
Altitude
655.713 km
Speed
7.53 km/s
True Right ascension
03h 46m 28s
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
01:02:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.345 km
Perigee altitude
649.667 km
Semi-major axis
7,029.143 km
Eccentricity
0.00019
Inclination
97.9971°
RAAN
56.6189°
Arg. of periapsis
338.564°
True anomaly
21.55672°
Mean anomaly
21.5487°
Eccentric anomaly
21.55271°
Mean motion
3.6829 °/min
Orbital period
97.75 mins
BSTAR
0.00079036
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-20 07:37:54.238Z | 122.852° SE | 2025-10-20 07:40:54.238Z | 68.852° E | 26.497° | 2025-10-20 07:43:54.238Z | 15.678° NNE |
| 5 mins | 2025-10-20 09:15:54.238Z | 231.715° WSW | 2025-10-20 09:17:54.238Z | 270.61° WNW | 22.173° | 2025-10-20 09:20:54.238Z | 316.357° NNW |
| 7 mins | 2025-10-20 21:06:54.238Z | 18.999° NNE | 2025-10-20 21:09:54.238Z | 65.24° ENE | 42.916° | 2025-10-20 21:13:54.238Z | 185.54° SSW |
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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