Showing default

KNACKSAT-2, 67683

Orbit data source: Space-Track

KNACKSAT-2, 67683 is a Thai payload satellite in LEO that was delivered to the ISS. 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
67683, 1998-067XZ
Orbit
LEO
Country
Flag of THTH / THAI
Related business
Manufacturer
Kyutech
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
1998-11-20 (27 years ago)
Launch vehicle
H3-24W
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 KNACKSAT-2
1 67683U 98067XZ  26087.26490943  .00044943  00000-0  70041-3 0  9999
2 67683  51.6323 339.4481 0009955 253.0442 106.9457 15.53355433  7671
Epoch: 2026-03-28T06:21Z
TLE epoch observation values (Epoch: 2026-03-28T06:21:28.174Z)
Latitude
-0.00006°
Longitude
58.39302°
Altitude
409.654 km
Speed
7.665 km/s
True Right ascension
22h 37m 47s
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
19:21:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
414.202 km
Perigee altitude
400.692 km
Semi-major axis
6,785.584 km
Eccentricity
0.001
Inclination
51.6323°
RAAN
339.4481°
Arg. of periapsis
253.0442°
True anomaly
107.05478°
Mean anomaly
106.9457°
Eccentric anomaly
107.00025°
Mean motion
3.88295 °/min
Orbital period
92.71 mins
BSTAR
0.00070041
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|