ITASAT, 43786
Orbit data source: Space-Track
ITASAT, 43786 is a payload satellite owned by ITA (BR) in SSO that was launched on Mon, 03 Dec 2018 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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43786 intel report (Beta)
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Identifier
Orbit
Country
BR / BRAZRelated business
Manufacturer
ITA
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ITASAT
1 43786U 18099AE 26140.41759563 .00004945 00000-0 24132-3 0 9995
2 43786 97.4045 192.4886 0014390 91.1121 269.1762 15.18653930408690Epoch: 2026-05-20T10:01Z
TLE epoch observation values (Epoch: 2026-05-20T10:01:20.262Z)
Latitude
-0.00004°
Longitude
164.07673°
Altitude
513.153 km
Speed
7.607 km/s
True Right ascension
12h 49m 57s
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
20:12:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.783 km
Perigee altitude
496.968 km
Semi-major axis
6,885.012 km
Eccentricity
0.00144
Inclination
97.4045°
RAAN
192.4886°
Arg. of periapsis
91.1121°
True anomaly
269.01132°
Mean anomaly
269.1762°
Eccentric anomaly
269.09376°
Mean motion
3.79915 °/min
Orbital period
94.76 mins
BSTAR
0.00024132
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.ITASAT 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 | 2026-05-21 16:37:46.300Z | 357.9° N | 2026-05-21 16:40:46.300Z | 271.902° WNW | 37.588° | 2026-05-21 16:43:46.300Z | 210.578° SW |
| 5 mins | 2026-05-22 03:16:46.300Z | 147.63° SSE | 2026-05-22 03:18:46.300Z | 92.569° ESE | 39.608° | 2026-05-22 03:21:46.300Z | 359.59° N |
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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