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: 18 hours ago
TLE from 18 hours ago
0 KINEIS-4E
1 63300U 25056A 26267.33661075 .00001068 00000-0 17646-3 0 9996
2 63300 97.9149 28.5445 0001776 157.9570 202.1714 14.72327626 81710Epoch: 2026-09-24T08:04Z
TLE epoch observation values (Epoch: 2026-09-24T08:04:43.168Z)
Latitude
-0.00008°
Longitude
-95.81019°
Altitude
657.815 km
Speed
7.528 km/s
True Right ascension
01h 54m 10s
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
19:36:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.947 km
Perigee altitude
649.451 km
Semi-major axis
7,028.836 km
Eccentricity
0.00018
Inclination
97.9149°
RAAN
28.5445°
Arg. of periapsis
157.957°
True anomaly
202.16372°
Mean anomaly
202.1714°
Eccentric anomaly
202.16756°
Mean motion
3.68314 °/min
Orbital period
97.74 mins
BSTAR
0.00017646
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-25 07:04:39.478Z | 98.998° ESE | 2026-09-25 07:06:39.478Z | 69.317° E | 17.614° | 2026-09-25 07:09:39.478Z | 25.925° NE |
| 6 mins | 2026-09-25 08:40:39.478Z | 198.928° SSW | 2026-09-25 08:43:39.478Z | 274.736° WNW | 43.073° | 2026-09-25 08:46:39.478Z | 328.818° NNW |
| 6 mins | 2026-09-25 20:33:39.478Z | 43.298° NE | 2026-09-25 20:35:39.478Z | 87.339° E | 38.6° | 2026-09-25 20:39:39.478Z | 164.739° S |
| 4 mins | 2026-09-25 22:10:39.478Z | 323.538° NNW | 2026-09-25 22:12:39.478Z | 290.249° WNW | 19.385° | 2026-09-25 22:14:39.478Z | 258.921° W |
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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