Showing default

K-RADCUBE, 68541

Orbit data source: Space-Track

K-RADCUBE, 68541 is a South Korean payload satellite in HEO that was launched on Wed, 01 Apr 2026 UTC via an SLS BLOCK 1 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
68541, 2026-069D
Orbit
HEO
Country
Flag of KRKR / SKOR
Related business
Manufacturer
KASA
Mission
Operational spacecraft
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2026-04-01 (4 days ago)
Launch vehicle
SLS BLOCK 1
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 K-RADCUBE
1 68541U 26069D   26092.67815972 -.00078411  19505-5 -17218-4 0  9992
2 68541  28.3341 359.8703 8450105  77.6642 243.1767  1.02517944    33
Epoch: 2026-04-02T16:16Z
TLE epoch observation values (Epoch: 2026-04-02T16:16:32.999Z)
Latitude
-28.33358°
Longitude
-167.34017°
Altitude
63,684.913 km
Speed
1.336 km/s
True Right ascension
17h 51m 16s
True Declination
-28° 19' 08"
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
23:09:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
70,284.25 km
Perigee altitude
61.862 km
Semi-major axis
41,551.193 km
Eccentricity
0.84501
Inclination
28.3341°
RAAN
359.8703°
Arg. of periapsis
77.6642°
True anomaly
190.51896°
Mean anomaly
243.1767°
Eccentric anomaly
215.24048°
Mean motion
0.25625 °/min
Orbital period
1,404.86 mins
BSTAR
-0.000017218
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...
Other satellites on launch #69 in the year 2026 (2026-04-01 UTC)

Documentation

Showing up to 5 results
|