KINEIS-4A, 63303
Orbit data source: Space-Track
KINEIS-4A, 63303 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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63303 intel report (Beta)
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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-4A
1 63303U 25056D 26253.59163140 .00001015 00000-0 16835-3 0 9993
2 63303 97.9201 15.3846 0002253 50.7333 309.4074 14.72275795 79692Epoch: 2026-09-10T14:11Z
TLE epoch observation values (Epoch: 2026-09-10T14:11:56.952Z)
Latitude
-0.00008°
Longitude
172.77017°
Altitude
655.817 km
Speed
7.53 km/s
True Right ascension
01h 01m 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
12:02:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.448 km
Perigee altitude
649.281 km
Semi-major axis
7,029.001 km
Eccentricity
0.00023
Inclination
97.9201°
RAAN
15.3846°
Arg. of periapsis
50.7333°
True anomaly
309.38745°
Mean anomaly
309.4074°
Eccentric anomaly
309.39742°
Mean motion
3.68301 °/min
Orbital period
97.75 mins
BSTAR
0.00016835
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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-4A 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 | 2026-09-10 21:18:11.331Z | 4.054° NNE | 2026-09-10 21:21:11.331Z | 287.134° WNW | 68.505° | 2026-09-10 21:25:11.331Z | 203.476° SW |
| 7 mins | 2026-09-11 08:16:11.331Z | 168.935° S | 2026-09-11 08:19:11.331Z | 201.929° SSW | 81.218° | 2026-09-11 08:23:11.331Z | 345.958° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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