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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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: 7 hours ago
TLE from 7 hours ago
0 KINEIS-4E
1 63300U 25056A 25300.95713988 .00003375 00000-0 54260-3 0 9998
2 63300 97.9980 64.3963 0000554 51.6284 308.4973 14.72230133 32956Epoch: 2025-10-27T22:58Z
TLE epoch observation values (Epoch: 2025-10-27T22:58:16.885Z)
Latitude
-0.00004°
Longitude
43.27442°
Altitude
656.723 km
Speed
7.529 km/s
True Right ascension
04h 17m 35s
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
01:50:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.403 km
Perigee altitude
650.624 km
Semi-major axis
7,029.15 km
Eccentricity
0.00006
Inclination
97.998°
RAAN
64.3963°
Arg. of periapsis
51.6284°
True anomaly
308.49233°
Mean anomaly
308.4973°
Eccentric anomaly
308.49482°
Mean motion
3.68289 °/min
Orbital period
97.75 mins
BSTAR
0.0005426
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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 | 2025-10-28 07:17:02.568Z | 105.246° ESE | 2025-10-28 07:20:02.568Z | 59.217° ENE | 17.727° | 2025-10-28 07:22:02.568Z | 29.347° NE |
| 7 mins | 2025-10-28 08:53:02.568Z | 198.128° SSW | 2025-10-28 08:56:02.568Z | 258.178° W | 32.863° | 2025-10-28 09:00:02.568Z | 330.367° NNW |
| 6 mins | 2025-10-28 20:46:02.568Z | 37.008° NE | 2025-10-28 20:49:02.568Z | 107.488° ESE | 33.391° | 2025-10-28 20:52:02.568Z | 164.068° S |
| 4 mins | 2025-10-28 22:24:02.568Z | 314.704° NW | 2025-10-28 22:25:02.568Z | 298.076° NW | 17.411° | 2025-10-28 22:28:02.568Z | 253.774° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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