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 26073.56222009 .00002806 00000-0 45112-3 0 9999
2 63303 97.9942 199.8586 0002049 214.5023 145.6052 14.72350565 53206Epoch: 2026-03-14T13:29Z
TLE epoch observation values (Epoch: 2026-03-14T13:29:35.815Z)
Latitude
-0.00001°
Longitude
-174.72225°
Altitude
657.772 km
Speed
7.528 km/s
True Right ascension
13h 19m 26s
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
23:39:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.07 km
Perigee altitude
649.189 km
Semi-major axis
7,028.766 km
Eccentricity
0.0002
Inclination
97.9942°
RAAN
199.8586°
Arg. of periapsis
214.5023°
True anomaly
145.61846°
Mean anomaly
145.6052°
Eccentric anomaly
145.61183°
Mean motion
3.68319 °/min
Orbital period
97.74 mins
BSTAR
0.00045112
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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 | 2026-03-14 20:35:35.810Z | 34.184° NE | 2026-03-14 20:39:35.810Z | 104.77° ESE | 28.668° | 2026-03-14 20:42:35.810Z | 156.744° SSE |
| 5 mins | 2026-03-14 22:13:35.810Z | 331.714° NNW | 2026-03-14 22:15:35.810Z | 298.885° NW | 20.549° | 2026-03-14 22:18:35.810Z | 249.408° W |
| 5 mins | 2026-03-15 07:35:35.810Z | 111.875° ESE | 2026-03-15 07:37:35.810Z | 72.616° E | 25.516° | 2026-03-15 07:40:35.810Z | 18.136° NNE |
| 5 mins | 2026-03-15 09:12:35.810Z | 228.326° WSW | 2026-03-15 09:14:35.810Z | 267.654° W | 23.26° | 2026-03-15 09:17:35.810Z | 316.004° 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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