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: 6 hours ago
TLE from 6 hours ago
0 KINEIS-4C
1 63301U 25056B 25298.93424994 .00003333 00000-0 53226-3 0 9994
2 63301 97.9982 62.5253 0001754 53.0164 307.1204 14.72531642 32667Epoch: 2025-10-25T22:25Z
TLE epoch observation values (Epoch: 2025-10-25T22:25:19.194Z)
Latitude
-0.00003°
Longitude
51.63765°
Altitude
655.262 km
Speed
7.53 km/s
True Right ascension
04h 10m 06s
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
23:29:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.286 km
Perigee altitude
648.82 km
Semi-major axis
7,028.19 km
Eccentricity
0.00018
Inclination
97.9982°
RAAN
62.5253°
Arg. of periapsis
53.0164°
True anomaly
307.10437°
Mean anomaly
307.1204°
Eccentric anomaly
307.11239°
Mean motion
3.68365 °/min
Orbital period
97.73 mins
BSTAR
0.00053226
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-26 08:19:34.754Z | 164.269° S | 2025-10-26 08:23:34.754Z | 14.042° NNE | 44.663° | 2025-10-26 08:27:34.754Z | 348.435° N |
| 4 mins | 2025-10-26 20:14:34.754Z | 73.364° E | 2025-10-26 20:15:34.754Z | 90.278° ESE | 17.649° | 2025-10-26 20:18:34.754Z | 134.998° SE |
| 7 mins | 2025-10-26 21:49:34.754Z | 349.948° N | 2025-10-26 21:52:34.754Z | 290.757° WNW | 32.015° | 2025-10-26 21:56:34.754Z | 221.776° SW |
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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