KINEIS-4B, 63304
Orbit data source: Space-Track
KINEIS-4B, 63304 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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63304 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: 10 hours ago
TLE from 10 hours ago
0 KINEIS-4B
1 63304U 25056E 26178.54515389 .00001620 00000-0 26412-3 0 9995
2 63304 97.9131 302.3661 0004151 259.6062 100.4678 14.72280643 68647Epoch: 2026-06-27T13:05Z
TLE epoch observation values (Epoch: 2026-06-27T13:05:01.296Z)
Latitude
0.00001°
Longitude
-169.54707°
Altitude
657.339 km
Speed
7.528 km/s
True Right ascension
20h 09m 27s
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
10:56:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.766 km
Perigee altitude
647.931 km
Semi-major axis
7,028.986 km
Eccentricity
0.00042
Inclination
97.9131°
RAAN
302.3661°
Arg. of periapsis
259.6062°
True anomaly
100.51457°
Mean anomaly
100.4678°
Eccentric anomaly
100.49119°
Mean motion
3.68302 °/min
Orbital period
97.75 mins
BSTAR
0.00026412
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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-4B 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 | 2026-06-28 07:11:32.396Z | 98.062° ESE | 2026-06-28 07:13:32.396Z | 67.184° ENE | 17.321° | 2026-06-28 07:16:32.396Z | 24.147° NE |
| 6 mins | 2026-06-28 08:47:32.396Z | 201.555° SSW | 2026-06-28 08:50:32.396Z | 278.527° WNW | 33.18° | 2026-06-28 08:53:32.396Z | 328.753° NNW |
| 7 mins | 2026-06-28 20:39:32.396Z | 34.038° NE | 2026-06-28 20:42:32.396Z | 91.258° ESE | 32.834° | 2026-06-28 20:46:32.396Z | 166.527° S |
| 4 mins | 2026-06-28 22:17:32.396Z | 321.473° NNW | 2026-06-28 22:19:32.396Z | 288.193° WNW | 17.765° | 2026-06-28 22:21:32.396Z | 258.058° 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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