UITMSAT, 67686
Orbit data source: Space-Track
UITMSAT, 67686 is a payload satellite owned by UiTM (JP) in LEO that was delivered to the ISS. 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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67686 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
UiTM
Mission
Operational spacecraft
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 UITMSAT
1 67686U 98067YC 26089.04035350 .00070850 00000-0 10299-2 0 9991
2 67686 51.6316 330.3073 0009168 228.7087 131.3115 15.55077953 7957Epoch: 2026-03-30T00:58Z
TLE epoch observation values (Epoch: 2026-03-30T00:58:06.542Z)
Latitude
-0.00004°
Longitude
128.34241°
Altitude
406.775 km
Speed
7.666 km/s
True Right ascension
22h 01m 13s
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
03:34:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
408.653 km
Perigee altitude
396.22 km
Semi-major axis
6,780.573 km
Eccentricity
0.00092
Inclination
51.6316°
RAAN
330.3073°
Arg. of periapsis
228.7087°
True anomaly
131.39035°
Mean anomaly
131.3115°
Eccentric anomaly
131.35093°
Mean motion
3.88726 °/min
Orbital period
92.61 mins
BSTAR
0.0010299
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Other satellites on launch #67 in the year 1998 (1998-11-20 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.UITMSAT 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 | 2026-03-31 00:34:24.567Z | 331.916° NNW | 2026-03-31 00:36:24.567Z | 30.213° NE | 29.228° | 2026-03-31 00:38:24.567Z | 87.754° E |
| 4 mins | 2026-03-31 02:11:24.567Z | 263.767° W | 2026-03-31 02:12:24.567Z | 236.458° WSW | 23.098° | 2026-03-31 02:15:24.567Z | 168.151° S |
| 4 mins | 2026-03-31 18:49:24.567Z | 249.13° W | 2026-03-31 18:51:24.567Z | 353.847° N | 40.958° | 2026-03-31 18:53:24.567Z | 43.84° NE |
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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