TRISAT-S, 100612
Orbit data source: Space-Track
TRISAT-S, 100612 is a payload satellite owned by U. Maribor (SI) in SSO that was launched on Sat, 05 Sep 2026 UTC launched from the (ANSP). 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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100612 intel report (Beta)
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Identifier
Orbit
Country
SI / SVNRelated business
Manufacturer
U. Maribor
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Unknown
Object type
Shape & HBR
BOX, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TRISAT-S
1 A0612U 26203D 26283.19354417 .00001622 00000-0 12181-3 0 9994
2 A0612 97.4165 357.0444 0058641 158.4436 201.9278 15.02604118 5164Epoch: 2026-10-10T04:38Z
TLE epoch observation values (Epoch: 2026-10-10T04:38:42.216Z)
Latitude
-0.00004°
Longitude
-91.43568°
Altitude
599.714 km
Speed
7.539 km/s
True Right ascension
23h 48m 10s
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
02:44:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
596.521 km
Perigee altitude
515.198 km
Semi-major axis
6,933.996 km
Eccentricity
0.00586
Inclination
97.4165°
RAAN
357.0444°
Arg. of periapsis
158.4436°
True anomaly
201.67855°
Mean anomaly
201.9278°
Eccentric anomaly
201.80301°
Mean motion
3.75896 °/min
Orbital period
95.77 mins
BSTAR
0.00012181
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Other satellites on launch #203 in the year 2026 (2026-09-05 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.TRISAT-S 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-11 17:57:53.093Z | 9.818° NNE | 2026-10-11 18:01:53.093Z | 211.38° SW | 65.442° | 2026-10-11 18:04:53.093Z | 196.129° SSW |
| 6 mins | 2026-10-12 04:43:53.093Z | 141.868° SSE | 2026-10-12 04:46:53.093Z | 58.086° ENE | 47.238° | 2026-10-12 04:49:53.093Z | 2.369° 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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