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: 16 hours ago
TLE from 16 hours ago
0 KINEIS-4B
1 63304U 25056E 25312.81703531 .00004292 00000-0 68558-3 0 9997
2 63304 97.9997 76.1453 0001769 237.3711 122.7325 14.72370967 34691Epoch: 2025-11-08T19:36Z
TLE epoch observation values (Epoch: 2025-11-08T19:36:31.850Z)
Latitude
-0.00013°
Longitude
93.7714°
Altitude
657.19 km
Speed
7.528 km/s
True Right ascension
05h 04m 34s
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
08:02:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.808 km
Perigee altitude
649.321 km
Semi-major axis
7,028.702 km
Eccentricity
0.00018
Inclination
97.9997°
RAAN
76.1453°
Arg. of periapsis
237.3711°
True anomaly
122.74955°
Mean anomaly
122.7325°
Eccentric anomaly
122.74103°
Mean motion
3.68324 °/min
Orbital period
97.74 mins
BSTAR
0.00068558
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-09 20:39:00.353Z | 33.3° NE | 2025-11-09 20:43:00.353Z | 106.767° ESE | 29.898° | 2025-11-09 20:46:00.353Z | 159.051° S |
| 5 mins | 2025-11-09 22:17:00.353Z | 330.159° NNW | 2025-11-09 22:19:00.353Z | 297.694° NW | 19.681° | 2025-11-09 22:22:00.353Z | 250.188° W |
| 5 mins | 2025-11-10 07:39:00.353Z | 112.7° SE | 2025-11-10 07:41:00.353Z | 71.153° E | 26.685° | 2025-11-10 07:44:00.353Z | 16.333° NNE |
| 5 mins | 2025-11-10 09:16:00.353Z | 230.722° WSW | 2025-11-10 09:18:00.353Z | 268.916° W | 22.121° | 2025-11-10 09:21:00.353Z | 315.479° NNW |
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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