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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 KINEIS-4C
1 63301U 25056B 25260.33392997 .00002075 00000-0 33561-3 0 9996
2 63301 97.9922 24.5571 0002457 120.8166 239.3283 14.72351201 26980Epoch: 2025-09-17T08:00Z
TLE epoch observation values (Epoch: 2025-09-17T08:00:51.549Z)
Latitude
-0.00007°
Longitude
-92.16905°
Altitude
657.462 km
Speed
7.528 km/s
True Right ascension
01h 38m 13s
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
09:18:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.354 km
Perigee altitude
648.9 km
Semi-major axis
7,028.764 km
Eccentricity
0.00025
Inclination
97.9922°
RAAN
24.5571°
Arg. of periapsis
120.8166°
True anomaly
239.30409°
Mean anomaly
239.3283°
Eccentric anomaly
239.31619°
Mean motion
3.68319 °/min
Orbital period
97.74 mins
BSTAR
0.00033561
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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 | 2025-09-17 21:38:53.377Z | 352.744° N | 2025-09-17 21:40:53.377Z | 310.329° NW | 37.088° | 2025-09-17 21:44:53.377Z | 214.344° SW |
| 7 mins | 2025-09-18 08:36:53.377Z | 183.028° SSW | 2025-09-18 08:39:53.377Z | 282.747° WNW | 41.28° | 2025-09-18 08:43:53.377Z | 340.529° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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