Showing default

KINEIS-1A, 60084

Orbit data source: Space-Track

KINEIS-1A, 60084 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
60084, 2024-114F
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, 0.8 m
Radar Cross Section
0.229 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 KINEIS-1A
1 60084U 24114F   25258.29196843  .00001143  00000-0  15881-3 0  9999
2 60084  98.0087 278.5930 0002138 318.9967  41.1084 14.79816649 66727
Epoch: 2025-09-15T07:00Z
TLE epoch observation values (Epoch: 2025-09-15T07:00:26.072Z)
Latitude
0.00003°
Longitude
178.98564°
Altitude
631.792 km
Speed
7.543 km/s
True Right ascension
18h 34m 22s
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
10:18:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.447 km
Perigee altitude
625.451 km
Semi-major axis
7,005.086 km
Eccentricity
0.00021
Inclination
98.0087°
RAAN
278.593°
Arg. of periapsis
318.9967°
True anomaly
41.12451°
Mean anomaly
41.1084°
Eccentric anomaly
41.11646°
Mean motion
3.70189 °/min
Orbital period
97.25 mins
BSTAR
0.00015881
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
|