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.
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68433 intel report (Beta)
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Identifier
Orbit
Country
TW / TWNRelated business
Manufacturer
TRON
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 T.MICROSAT-2
1 68433U 26067T 26217.44576044 .00003546 00000-0 17852-3 0 9991
2 68433 97.4597 175.0866 0003736 241.4586 118.6272 15.17837375 19407Epoch: 2026-08-05T10:41Z
TLE epoch observation values (Epoch: 2026-08-05T10:41:53.702Z)
Latitude
0.00001°
Longitude
60.61279°
Altitude
516.698 km
Speed
7.605 km/s
True Right ascension
11h 40m 20s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:01:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.922 km
Perigee altitude
506.776 km
Semi-major axis
6,887.486 km
Eccentricity
0.00037
Inclination
97.4597°
RAAN
175.0866°
Arg. of periapsis
241.4586°
True anomaly
118.66477°
Mean anomaly
118.6272°
Eccentric anomaly
118.64599°
Mean motion
3.7971 °/min
Orbital period
94.81 mins
BSTAR
0.00017852
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Other satellites on launch #67 in the year 2026 (2026-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.T.MICROSAT-2 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-06 09:25:38.335Z | 45.554° ENE | 2026-08-06 09:27:38.335Z | 83.266° E | 22.436° | 2026-08-06 09:30:38.335Z | 147.154° SSE |
| 4 mins | 2026-08-06 11:00:38.335Z | 318.337° NNW | 2026-08-06 11:01:38.335Z | 297.796° NW | 18.505° | 2026-08-06 11:04:38.335Z | 243.922° WSW |
| 5 mins | 2026-08-06 21:38:38.335Z | 196.123° SSW | 2026-08-06 21:40:38.335Z | 251.798° W | 35.561° | 2026-08-06 21:43:38.335Z | 331.144° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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