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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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-4D
1 63302U 25056C 26124.15973646 -.00000321 00000-0 -43138-4 0 9999
2 63302 97.9242 249.4896 0003650 102.1439 258.0178 14.72346383 60654Epoch: 2026-05-04T03:50Z
TLE epoch observation values (Epoch: 2026-05-04T03:50:01.230Z)
Latitude
0.00002°
Longitude
-30.06846°
Altitude
657.132 km
Speed
7.529 km/s
True Right ascension
16h 37m 57s
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
18:50:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.205 km
Perigee altitude
648.074 km
Semi-major axis
7,028.777 km
Eccentricity
0.00037
Inclination
97.9242°
RAAN
249.4896°
Arg. of periapsis
102.1439°
True anomaly
257.97689°
Mean anomaly
258.0178°
Eccentric anomaly
257.99734°
Mean motion
3.68319 °/min
Orbital period
97.74 mins
BSTAR
-0.000043138
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-04 20:42:40.160Z | 27.598° NE | 2026-05-04 20:46:40.160Z | 92.069° ESE | 33.399° | 2026-05-04 20:50:40.160Z | 167.596° S |
| 4 mins | 2026-05-04 22:21:40.160Z | 320.729° NNW | 2026-05-04 22:23:40.160Z | 287.735° WNW | 17.25° | 2026-05-04 22:25:40.160Z | 258.163° W |
| 6 mins | 2026-05-05 07:42:40.160Z | 123.222° SE | 2026-05-05 07:45:40.160Z | 56.296° ENE | 28.826° | 2026-05-05 07:48:40.160Z | 9.421° NNE |
| 4 mins | 2026-05-05 09:20:40.160Z | 241.482° WSW | 2026-05-05 09:21:40.160Z | 259.219° W | 19.465° | 2026-05-05 09:24:40.160Z | 307.99° 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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