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: 5 hours ago
TLE from 5 hours ago
0 KINEIS-4E
1 63300U 25056A 26139.22969162 .00000930 00000-0 15451-3 0 9999
2 63300 97.9002 263.9305 0000699 188.1727 171.9469 14.72390735 62867Epoch: 2026-05-19T05:30Z
TLE epoch observation values (Epoch: 2026-05-19T05:30:45.355Z)
Latitude
-0.0001°
Longitude
-55.66506°
Altitude
656.944 km
Speed
7.529 km/s
True Right ascension
17h 35m 43s
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
19:22:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
650.989 km
Perigee altitude
650.006 km
Semi-major axis
7,028.634 km
Eccentricity
0.00007
Inclination
97.9002°
RAAN
263.9305°
Arg. of periapsis
188.1727°
True anomaly
171.94802°
Mean anomaly
171.9469°
Eccentric anomaly
171.94746°
Mean motion
3.6833 °/min
Orbital period
97.74 mins
BSTAR
0.00015451
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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 | 2026-05-19 20:46:21.931Z | 29.887° NE | 2026-05-19 20:49:21.931Z | 85.954° E | 35.665° | 2026-05-19 20:53:21.931Z | 170.659° S |
| 4 mins | 2026-05-19 22:24:21.931Z | 321.004° NNW | 2026-05-19 22:26:21.931Z | 290.014° WNW | 15.818° | 2026-05-19 22:28:21.931Z | 261.406° W |
| 6 mins | 2026-05-20 07:45:21.931Z | 127.709° SE | 2026-05-20 07:48:21.931Z | 57.117° ENE | 31.155° | 2026-05-20 07:51:21.931Z | 7.839° NNE |
| 4 mins | 2026-05-20 09:23:21.931Z | 241.999° WSW | 2026-05-20 09:24:21.931Z | 258.397° W | 17.687° | 2026-05-20 09:27:21.931Z | 305.371° NW |
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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