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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-4E
1 63300U 25056A 25362.87148413 .00003524 00000-0 56496-3 0 9991
2 63300 98.0008 125.3309 0001943 106.0251 254.1171 14.72319357 42069Epoch: 2025-12-28T20:54Z
TLE epoch observation values (Epoch: 2025-12-28T20:54:56.228Z)
Latitude
0°
Longitude
74.01937°
Altitude
657.056 km
Speed
7.529 km/s
True Right ascension
08h 21m 19s
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
01:17:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.095 km
Perigee altitude
649.363 km
Semi-major axis
7,028.866 km
Eccentricity
0.00019
Inclination
98.0008°
RAAN
125.3309°
Arg. of periapsis
106.0251°
True anomaly
254.09569°
Mean anomaly
254.1171°
Eccentric anomaly
254.10639°
Mean motion
3.68311 °/min
Orbital period
97.74 mins
BSTAR
0.00056496
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-12-29 08:28:14.510Z | 174.2° S | 2025-12-29 08:31:14.510Z | 307.882° NW | 43.327° | 2025-12-29 08:35:14.510Z | 344.338° N |
| 5 mins | 2025-12-29 20:21:14.510Z | 56.954° ENE | 2025-12-29 20:23:14.510Z | 91.652° ESE | 21.063° | 2025-12-29 20:26:14.510Z | 140.703° SSE |
| 5 mins | 2025-12-29 21:58:14.510Z | 332.969° NNW | 2025-12-29 22:00:14.510Z | 288.316° WNW | 27.742° | 2025-12-29 22:03:14.510Z | 234.298° WSW |
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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