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, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 T.MICROSAT-2
1 68433U 26067T 26153.81600093 .00005625 00000-0 28584-3 0 9997
2 68433 97.4569 112.4128 0007687 106.0775 254.1306 15.17246393 9752Epoch: 2026-06-02T19:35Z
TLE epoch observation values (Epoch: 2026-06-02T19:35:02.480Z)
Latitude
0.00004°
Longitude
-72.63109°
Altitude
518.705 km
Speed
7.603 km/s
True Right ascension
07h 29m 39s
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
03:12:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.435 km
Perigee altitude
505.843 km
Semi-major axis
6,889.276 km
Eccentricity
0.00077
Inclination
97.4569°
RAAN
112.4128°
Arg. of periapsis
106.0775°
True anomaly
254.04589°
Mean anomaly
254.1306°
Eccentric anomaly
254.08824°
Mean motion
3.79562 °/min
Orbital period
94.85 mins
BSTAR
0.00028584
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-06 20:17:30.008Z | 103.439° ESE | 2026-06-06 20:19:30.008Z | 69.39° E | 15.319° | 2026-06-06 20:21:30.008Z | 34.179° NE |
| 5 mins | 2026-06-06 21:51:30.008Z | 214.285° SW | 2026-06-06 21:53:30.008Z | 267.818° W | 27.521° | 2026-06-06 21:56:30.008Z | 325.67° NNW |
| 4 mins | 2026-06-07 09:23:30.008Z | 62.584° ENE | 2026-06-07 09:24:30.008Z | 84.379° E | 20.801° | 2026-06-07 09:27:30.008Z | 144.834° SSE |
| 4 mins | 2026-06-07 10:57:30.008Z | 320.146° NNW | 2026-06-07 10:58:30.008Z | 298.79° NW | 19.743° | 2026-06-07 11:01:30.008Z | 242.092° WSW |
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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