Showing default

T-MICROSAT-1, 66766

Orbit data source: Space-Track

T-MICROSAT-1, 66766 is a Taiwanese payload satellite in SSO that was launched on Fri, 28 Nov 2025 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
66766, 2025-276DE
Orbit
SSO
Country
Flag of TWTW / TWN
Related business
Manufacturer
TRON
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
15 kg wet, ~15 kg dry
Launch date (UTC)
2025-11-28 (9 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 T-MICROSAT-1
1 66766U 25276DE  26238.65969775  .00005310  00000-0  23923-3 0  9999
2 66766  97.4120 311.2978 0001193  87.0121 273.1251 15.21472064 41154
Epoch: 2026-08-26T15:49Z
TLE epoch observation values (Epoch: 2026-08-26T15:49:57.885Z)
Latitude
-0.00007°
Longitude
98.89711°
Altitude
504.447 km
Speed
7.612 km/s
True Right ascension
20h 45m 11s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
17:12:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.184 km
Perigee altitude
497.543 km
Semi-major axis
6,876.501 km
Eccentricity
0.00012
Inclination
97.412°
RAAN
311.2978°
Arg. of periapsis
87.0121°
True anomaly
273.11145°
Mean anomaly
273.1251°
Eccentric anomaly
273.11827°
Mean motion
3.8062 °/min
Orbital period
94.58 mins
BSTAR
0.00023923
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
|