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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ITASAT
1 43786U 18099AE 26305.10131516 .00005241 00000-0 24260-3 0 9998
2 43786 97.3859 353.8881 0010848 228.1958 131.8352 15.20501300433700Epoch: 2026-11-01T02:25Z
TLE epoch observation values (Epoch: 2026-11-01T02:25:53.629Z)
Latitude
-0°
Longitude
-82.98287°
Altitude
512.404 km
Speed
7.605 km/s
True Right ascension
23h 35m 33s
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
06:26:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.755 km
Perigee altitude
493.829 km
Semi-major axis
6,879.429 km
Eccentricity
0.00108
Inclination
97.3859°
RAAN
353.8881°
Arg. of periapsis
228.1958°
True anomaly
131.92773°
Mean anomaly
131.8352°
Eccentric anomaly
131.88148°
Mean motion
3.80377 °/min
Orbital period
94.64 mins
BSTAR
0.0002426
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-01 15:38:51.317Z | 45.376° ENE | 2026-11-01 15:40:51.317Z | 87.381° E | 27.214° | 2026-11-01 15:43:51.317Z | 152.082° SSE |
| 5 mins | 2026-11-02 03:50:51.317Z | 205.303° SW | 2026-11-02 03:52:51.317Z | 277.959° WNW | 42.214° | 2026-11-02 03:55:51.317Z | 333.167° NNW |
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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