KINEIS-4E, 63300
Orbit data source: Space-Track
KINEIS-4E, 63300 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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63300 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: 1 day ago
TLE from 1 day ago
0 KINEIS-4E
1 63300U 25056A 26086.83240197 .00000702 00000-0 11885-3 0 9991
2 63300 97.9728 212.8182 0001356 143.5789 216.5511 14.72273762 55150Epoch: 2026-03-27T19:58Z
TLE epoch observation values (Epoch: 2026-03-27T19:58:39.530Z)
Latitude
0°
Longitude
87.89215°
Altitude
657.594 km
Speed
7.528 km/s
True Right ascension
14h 11m 16s
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
07:09:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.826 km
Perigee altitude
649.92 km
Semi-major axis
7,029.01 km
Eccentricity
0.00014
Inclination
97.9728°
RAAN
212.8182°
Arg. of periapsis
143.5789°
True anomaly
216.54185°
Mean anomaly
216.5511°
Eccentric anomaly
216.54647°
Mean motion
3.683 °/min
Orbital period
97.75 mins
BSTAR
0.00011885
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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-4E 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-03-29 07:58:39.599Z | 149.347° SSE | 2026-03-29 08:02:39.599Z | 89.215° E | 38.206° | 2026-03-29 08:06:39.599Z | 359.536° N |
| 7 mins | 2026-03-29 21:29:39.599Z | 0.002° NNE | 2026-03-29 21:32:39.599Z | 265.925° W | 41.029° | 2026-03-29 21:36:39.599Z | 206.026° SW |
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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