Showing default

KINEIS-2C, 62929

Orbit data source: Space-Track

KINEIS-2C, 62929 is a French payload satellite in SSO that was launched on Sat, 08 Feb 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.

Loading next visibility...
Identifier
62929, 2025-028B
Orbit
SSO
Country
Flag of FRFR
Related business
Manufacturer
KINEIS
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
28 kg wet, 28 kg dry
Launch date (UTC)
2025-02-08 (10 months ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 KINEIS-2C
1 62929U 25028B   25349.86267551  .00001218  00000-0  20057-3 0  9997
2 62929  98.0229  41.1054 0001056 175.1120 185.0097 14.72288402 45630
Epoch: 2025-12-15T20:42Z
TLE epoch observation values (Epoch: 2025-12-15T20:42:15.164Z)
Latitude
-0.00008°
Longitude
5.78708°
Altitude
657.519 km
Speed
7.528 km/s
True Right ascension
02h 44m 25s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:23:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.571 km
Perigee altitude
650.087 km
Semi-major axis
7,028.966 km
Eccentricity
0.00011
Inclination
98.0229°
RAAN
41.1054°
Arg. of periapsis
175.112°
True anomaly
185.00864°
Mean anomaly
185.0097°
Eccentric anomaly
185.00917°
Mean motion
3.68304 °/min
Orbital period
97.75 mins
BSTAR
0.00020057
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|