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: 19 hours ago
TLE from 19 hours ago
0 KINEIS-4C
1 63301U 25056B 25257.61553557 .00001679 00000-0 27327-3 0 9996
2 63301 97.9923 21.8846 0002362 125.1119 235.0311 14.72338934 26586Epoch: 2025-09-14T14:46Z
TLE epoch observation values (Epoch: 2025-09-14T14:46:22.273Z)
Latitude
0.00008°
Longitude
166.45979°
Altitude
657.572 km
Speed
7.528 km/s
True Right ascension
01h 27m 32s
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
02:16:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.327 km
Perigee altitude
649.006 km
Semi-major axis
7,028.803 km
Eccentricity
0.00024
Inclination
97.9923°
RAAN
21.8846°
Arg. of periapsis
125.1119°
True anomaly
235.00892°
Mean anomaly
235.0311°
Eccentric anomaly
235.02001°
Mean motion
3.68316 °/min
Orbital period
97.74 mins
BSTAR
0.00027327
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-15 20:42:46.104Z | 34.17° NE | 2025-09-15 20:45:46.104Z | 86.049° E | 31.243° | 2025-09-15 20:49:46.104Z | 163.785° S |
| 5 mins | 2025-09-15 22:20:46.104Z | 324.624° NNW | 2025-09-15 22:22:46.104Z | 291.102° WNW | 18.619° | 2025-09-15 22:25:46.104Z | 248.244° W |
| 6 mins | 2025-09-16 07:41:46.104Z | 122.92° SE | 2025-09-16 07:44:46.104Z | 62.43° ENE | 27.833° | 2025-09-16 07:47:46.104Z | 12.208° NNE |
| 5 mins | 2025-09-16 09:19:46.104Z | 237.062° WSW | 2025-09-16 09:21:46.104Z | 275.047° WNW | 20.578° | 2025-09-16 09:24:46.104Z | 317.074° NNW |
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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