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 spacecraft
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.6 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 T.MICROSAT-2
1 68433U 26067T 26171.42380403 .00004548 00000-0 23062-3 0 9993
2 68433 97.4571 129.7476 0007414 60.8272 299.3702 15.17420167 12421Epoch: 2026-06-20T10:10Z
TLE epoch observation values (Epoch: 2026-06-20T10:10:16.668Z)
Latitude
-0.00006°
Longitude
68.53952°
Altitude
514.223 km
Speed
7.608 km/s
True Right ascension
08h 38m 59s
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
10:41:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.72 km
Perigee altitude
505.505 km
Semi-major axis
6,888.749 km
Eccentricity
0.00074
Inclination
97.4571°
RAAN
129.7476°
Arg. of periapsis
60.8272°
True anomaly
299.29613°
Mean anomaly
299.3702°
Eccentric anomaly
299.33317°
Mean motion
3.79606 °/min
Orbital period
94.84 mins
BSTAR
0.00023062
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 10:12:58.418Z | 7.185° NNE | 2026-06-22 10:15:58.418Z | 240.904° WSW | 43.386° | 2026-06-22 10:18:58.418Z | 198.83° SSW |
| 5 mins | 2026-06-22 20:52:58.418Z | 126.526° SE | 2026-06-22 20:54:58.418Z | 57.425° ENE | 32.36° | 2026-06-22 20:57:58.418Z | 3.804° NNE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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