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: 1 week ago
TLE from 1 week ago
0 KINEIS-4A
1 63303U 25056D 25281.77555052 .00003132 00000-0 50158-3 0 9998
2 63303 97.9962 45.5650 0002911 42.6651 317.4782 14.72446456 30133Epoch: 2025-10-08T18:36Z
TLE epoch observation values (Epoch: 2025-10-08T18:36:47.564Z)
Latitude
-0.00007°
Longitude
108.72157°
Altitude
654.769 km
Speed
7.531 km/s
True Right ascension
03h 02m 15s
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
10:09:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.37 km
Perigee altitude
648.278 km
Semi-major axis
7,028.461 km
Eccentricity
0.00029
Inclination
97.9962°
RAAN
45.565°
Arg. of periapsis
42.6651°
True anomaly
317.45565°
Mean anomaly
317.4782°
Eccentric anomaly
317.46692°
Mean motion
3.68343 °/min
Orbital period
97.73 mins
BSTAR
0.00050158
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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 | 2025-10-15 20:48:24.170Z | 30.601° NE | 2025-10-15 20:51:24.170Z | 83.728° E | 34.548° | 2025-10-15 20:55:24.170Z | 168.861° S |
| 4 mins | 2025-10-15 22:26:24.170Z | 322.477° NNW | 2025-10-15 22:28:24.170Z | 291.082° WNW | 16.492° | 2025-10-15 22:30:24.170Z | 261.539° W |
| 6 mins | 2025-10-16 07:47:24.170Z | 127.014° SE | 2025-10-16 07:50:24.170Z | 58.628° ENE | 30.617° | 2025-10-16 07:53:24.170Z | 8.558° NNE |
| 4 mins | 2025-10-16 09:25:24.170Z | 241.049° WSW | 2025-10-16 09:26:24.170Z | 257.692° W | 18.065° | 2025-10-16 09:29:24.170Z | 305.484° NW |
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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