KINEIS-4D, 63302
Orbit data source: Space-Track
KINEIS-4D, 63302 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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63302 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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 KINEIS-4D
1 63302U 25056C 25257.61122456 .00001689 00000-0 27462-3 0 9998
2 63302 97.9923 21.8898 0002752 119.6799 240.4682 14.72368094 26580Epoch: 2025-09-14T14:40Z
TLE epoch observation values (Epoch: 2025-09-14T14:40:09.801Z)
Latitude
-0.00013°
Longitude
168.02123°
Altitude
657.481 km
Speed
7.528 km/s
True Right ascension
01h 27m 33s
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
02:18:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
652.508 km
Perigee altitude
648.639 km
Semi-major axis
7,028.711 km
Eccentricity
0.00028
Inclination
97.9923°
RAAN
21.8898°
Arg. of periapsis
119.6799°
True anomaly
240.44077°
Mean anomaly
240.4682°
Eccentric anomaly
240.45448°
Mean motion
3.68324 °/min
Orbital period
97.74 mins
BSTAR
0.00027462
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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-4D 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 | 2025-09-15 20:36:45.737Z | 38.963° NE | 2025-09-15 20:39:45.737Z | 92.384° ESE | 28.253° | 2025-09-15 20:43:45.737Z | 160.18° S |
| 5 mins | 2025-09-15 22:14:45.737Z | 324.461° NNW | 2025-09-15 22:16:45.737Z | 287.464° WNW | 20.905° | 2025-09-15 22:19:45.737Z | 243.363° WSW |
| 6 mins | 2025-09-16 07:35:45.737Z | 116.635° SE | 2025-09-16 07:38:45.737Z | 59.087° ENE | 24.749° | 2025-09-16 07:41:45.737Z | 13.627° NNE |
| 6 mins | 2025-09-16 09:12:45.737Z | 221.631° SW | 2025-09-16 09:14:45.737Z | 257.706° W | 23.518° | 2025-09-16 09:18:45.737Z | 321.175° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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