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: 2 days ago
TLE from 2 days ago
0 KINEIS-4E
1 63300U 25056A 25348.12353867 .00003010 00000-0 48336-3 0 9998
2 63300 98.0004 110.8137 0001683 125.0471 235.0894 14.72358524 39895Epoch: 2025-12-14T02:57Z
TLE epoch observation values (Epoch: 2025-12-14T02:57:53.741Z)
Latitude
-0.00005°
Longitude
-16.70119°
Altitude
657.234 km
Speed
7.528 km/s
True Right ascension
07h 23m 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
23:41:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.787 km
Perigee altitude
649.421 km
Semi-major axis
7,028.741 km
Eccentricity
0.00017
Inclination
98.0004°
RAAN
110.8137°
Arg. of periapsis
125.0471°
True anomaly
235.07359°
Mean anomaly
235.0894°
Eccentric anomaly
235.08149°
Mean motion
3.68321 °/min
Orbital period
97.74 mins
BSTAR
0.00048336
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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 | 2025-12-16 07:19:02.405Z | 103.908° ESE | 2025-12-16 07:21:02.405Z | 73.497° E | 18.44° | 2025-12-16 07:24:02.405Z | 26.282° NE |
| 7 mins | 2025-12-16 08:55:02.405Z | 201.781° SSW | 2025-12-16 08:58:02.405Z | 265.742° W | 31.703° | 2025-12-16 09:02:02.405Z | 330.516° NNW |
| 6 mins | 2025-12-16 20:48:02.405Z | 38.339° NE | 2025-12-16 20:50:02.405Z | 80.334° E | 33.823° | 2025-12-16 20:54:02.405Z | 167.679° S |
| 4 mins | 2025-12-16 22:25:02.405Z | 324.142° NNW | 2025-12-16 22:27:02.405Z | 292.913° NW | 16.728° | 2025-12-16 22:29:02.405Z | 262.569° 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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