Showing default

T.MICROSAT-2, 68433

Orbit data source: Space-Track

T.MICROSAT-2, 68433 is a Taiwanese payload satellite in SSO that was launched on Mon, 30 Mar 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
68433, 2026-067T
Orbit
SSO
Country
Flag of TWTW / TWN
Related business
Manufacturer
TRON
Mission
Operational spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2026-03-30 (1 month ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 T.MICROSAT-2
1 68433U 26067T   26126.83964216  .00004711  00000-0  24167-3 0  9997
2 68433  97.4553  85.8689 0005217 185.7345 174.3829 15.17008842  5668
Epoch: 2026-05-06T20:09Z
TLE epoch observation values (Epoch: 2026-05-06T20:09:05.082Z)
Latitude
-0.00009°
Longitude
-81.09663°
Altitude
521.551 km
Speed
7.601 km/s
True Right ascension
05h 43m 28s
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
02:58:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.453 km
Perigee altitude
508.264 km
Semi-major axis
6,889.996 km
Eccentricity
0.00052
Inclination
97.4553°
RAAN
85.8689°
Arg. of periapsis
185.7345°
True anomaly
174.38875°
Mean anomaly
174.3829°
Eccentric anomaly
174.38582°
Mean motion
3.79503 °/min
Orbital period
94.86 mins
BSTAR
0.00024167
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
|