Showing default

KINEIS-1E, 60083

Orbit data source: Space-Track

KINEIS-1E, 60083 is a French payload satellite in SSO that was launched on Thu, 20 Jun 2024 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
60083, 2024-114E
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)
2024-06-20 (1 year 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: 6 hours ago

TLE from 6 hours ago
0 KINEIS-1E
1 60083U 24114E   25347.02870200  .00001593  00000-0  21671-3 0  9997
2 60083  97.9992   6.9108 0001609  51.6362 308.4994 14.80159590 79844
Epoch: 2025-12-13T00:41Z
TLE epoch observation values (Epoch: 2025-12-13T00:41:19.852Z)
Latitude
-0.00005°
Longitude
-85.38376°
Altitude
631.137 km
Speed
7.543 km/s
True Right ascension
00h 27m 38s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
05:27:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.992 km
Perigee altitude
624.739 km
Semi-major axis
7,004.003 km
Eccentricity
0.00016
Inclination
97.9992°
RAAN
6.9108°
Arg. of periapsis
51.6362°
True anomaly
308.48497°
Mean anomaly
308.4994°
Eccentric anomaly
308.49218°
Mean motion
3.70274 °/min
Orbital period
97.23 mins
BSTAR
0.00021671
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
|