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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 T.MICROSAT-2
1 68433U 26067T 26263.39094786 .00002862 00000-0 14336-3 0 9998
2 68433 97.4669 220.4050 0007561 89.7565 270.4536 15.18158666 26371Epoch: 2026-09-20T09:22Z
TLE epoch observation values (Epoch: 2026-09-20T09:22:57.895Z)
Latitude
0.00006°
Longitude
80.37796°
Altitude
514.455 km
Speed
7.606 km/s
True Right ascension
14h 41m 37s
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
12:54:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.584 km
Perigee altitude
503.17 km
Semi-major axis
6,886.514 km
Eccentricity
0.00076
Inclination
97.4669°
RAAN
220.405°
Arg. of periapsis
89.7565°
True anomaly
270.36696°
Mean anomaly
270.4536°
Eccentric anomaly
270.41028°
Mean motion
3.7979 °/min
Orbital period
94.79 mins
BSTAR
0.00014336
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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 | 2026-09-20 20:35:55.639Z | 122.623° SE | 2026-09-20 20:38:55.639Z | 58.582° ENE | 25.257° | 2026-09-20 20:40:55.639Z | 20.363° NNE |
| 4 mins | 2026-09-20 22:10:55.639Z | 235.413° WSW | 2026-09-20 22:12:55.639Z | 276.302° WNW | 18.328° | 2026-09-20 22:14:55.639Z | 309.825° NW |
| 5 mins | 2026-09-21 09:41:55.639Z | 45.101° ENE | 2026-09-21 09:43:55.639Z | 109.893° ESE | 38.35° | 2026-09-21 09:46:55.639Z | 167.334° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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