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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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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-4A
1 63303U 25056D 26034.28094093 .00002155 00000-0 34901-3 0 9996
2 63303 97.9969 161.2138 0002701 26.9970 333.1377 14.72271275 47423Epoch: 2026-02-03T06:44Z
TLE epoch observation values (Epoch: 2026-02-03T06:44:33.296Z)
Latitude
-0.00006°
Longitude
-73.38905°
Altitude
655.14 km
Speed
7.531 km/s
True Right ascension
10h 44m 51s
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
13:22:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.781 km
Perigee altitude
648.984 km
Semi-major axis
7,029.019 km
Eccentricity
0.00027
Inclination
97.9969°
RAAN
161.2138°
Arg. of periapsis
26.997°
True anomaly
333.12371°
Mean anomaly
333.1377°
Eccentric anomaly
333.13071°
Mean motion
3.68299 °/min
Orbital period
97.75 mins
BSTAR
0.00034901
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-03 20:23:11.867Z | 50.01° ENE | 2026-02-03 20:26:11.867Z | 102.643° ESE | 22.036° | 2026-02-03 20:29:11.867Z | 147.207° SSE |
| 6 mins | 2026-02-03 22:00:11.867Z | 337.933° N | 2026-02-03 22:02:11.867Z | 300.785° NW | 26.282° | 2026-02-03 22:06:11.867Z | 231.935° WSW |
| 5 mins | 2026-02-04 07:22:11.867Z | 104.44° ESE | 2026-02-04 07:24:11.867Z | 72.221° E | 19.662° | 2026-02-04 07:27:11.867Z | 24.223° NE |
| 6 mins | 2026-02-04 08:58:11.867Z | 205.214° SW | 2026-02-04 09:01:11.867Z | 267.874° W | 29.921° | 2026-02-04 09:04:11.867Z | 322.778° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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