KINEIS-4C, 63301
Orbit data source: Space-Track
KINEIS-4C, 63301 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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63301 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: 18 hours ago
TLE from 18 hours ago
0 KINEIS-4C
1 63301U 25056B 25349.29038833 .00001938 00000-0 31505-3 0 9998
2 63301 98.0006 112.0916 0001364 163.6636 196.4615 14.72217719 40077Epoch: 2025-12-15T06:58Z
TLE epoch observation values (Epoch: 2025-12-15T06:58:09.551Z)
Latitude
-0.00009°
Longitude
-76.63926°
Altitude
657.925 km
Speed
7.528 km/s
True Right ascension
07h 28m 21s
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
23:41:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.012 km
Perigee altitude
650.094 km
Semi-major axis
7,029.19 km
Eccentricity
0.00014
Inclination
98.0006°
RAAN
112.0916°
Arg. of periapsis
163.6636°
True anomaly
196.45707°
Mean anomaly
196.4615°
Eccentric anomaly
196.45929°
Mean motion
3.68286 °/min
Orbital period
97.75 mins
BSTAR
0.00031505
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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-4C 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 | 2025-12-16 07:34:53.114Z | 121.013° SE | 2025-12-16 07:37:53.114Z | 69.171° E | 25.214° | 2025-12-16 07:40:53.114Z | 17.13° NNE |
| 5 mins | 2025-12-16 09:12:53.114Z | 229.889° WSW | 2025-12-16 09:14:53.114Z | 270.636° WNW | 23.479° | 2025-12-16 09:17:53.114Z | 317.529° NNW |
| 7 mins | 2025-12-16 21:03:53.114Z | 20.93° NNE | 2025-12-16 21:06:53.114Z | 71.273° E | 41.933° | 2025-12-16 21:10:53.114Z | 182.859° 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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