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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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Identifier
63300, 2025-056A
Orbit
SSO
Last TLE update
1 day ago
Origin
Manufacturer
KINEIS
Mission
Operational spacecraft
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
28 kg wet, 28 kg dry
Launch date (UTC)
2025-03-18 (1 month ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 1 day ago
0 KINEIS-4E
1 63300U 25056A   25119.16233917  .00002582  00000-0  41249-3 0  9990
2 63300  97.9755 245.7887 0001930 130.2373 229.9004 14.72693298  6204
Epoch: 2025-04-29T03:53Z
Definitive object data (Epoch: 2025-04-29T03:53:46.104Z)
Latitude
0.00001°
Longitude
-30.01937°
Altitude
656.367 km
Speed
7.529 km/s
True Right ascension
16h 23m 09s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
-73.40003°
Longitude
-0.89784°
Altitude
680.662 km
Speed
7.515 km/s
Apparent Right ascension
05h 56m 50s
Apparent Declination
-75° 04' 29"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
18:06:14
Azimuth
178.95° S
Elevation
-54.825°
Doppler factor
1
Orbital elements
Apogee altitude
650.894 km
Perigee altitude
648.181 km
Semi-major axis
7,027.674 km
Eccentricity
0.000193
Inclination
97.9755°
RAAN
245.7887°
Arg. of periapsis
130.2373°
True anomaly
229.88349°
Mean anomaly
229.9004°
Eccentric anomaly
229.89194°
Mean motion
3.68405 °/min
BSTAR
0.00041249
Orbital period
97.72 mins
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KINEIS-4E Visibility forecast

Observer location: undefined°, undefined°

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 mins2025-04-30 21:14:12.926Z14.93° NNE2025-04-30 21:17:12.926Z32.547° NE43.352°2025-04-30 21:21:12.926Z190.63° SSW
6 mins2025-05-01 08:13:12.926Z151.338° SSE2025-05-01 08:15:12.926Z114.446° SE41.365°2025-05-01 08:19:12.926Z354.729° N
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