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: 9 hours ago
TLE from 9 hours ago
0 ITASAT
1 43786U 18099AE 26087.10192492 .00007769 00000-0 38512-3 0 9997
2 43786 97.4132 140.2569 0011212 275.1277 84.8677 15.17960867400601Epoch: 2026-03-28T02:26Z
TLE epoch observation values (Epoch: 2026-03-28T02:26:46.313Z)
Latitude
-0.00002°
Longitude
-81.96306°
Altitude
514.409 km
Speed
7.607 km/s
True Right ascension
09h 21m 01s
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
17:18:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
516.695 km
Perigee altitude
501.251 km
Semi-major axis
6,887.11 km
Eccentricity
0.00112
Inclination
97.4132°
RAAN
140.2569°
Arg. of periapsis
275.1277°
True anomaly
84.99568°
Mean anomaly
84.8677°
Eccentric anomaly
84.93169°
Mean motion
3.79741 °/min
Orbital period
94.8 mins
BSTAR
0.00038512
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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 | 2026-03-28 15:40:32.165Z | 41.238° NE | 2026-03-28 15:43:32.165Z | 101.028° ESE | 23.482° | 2026-03-28 15:45:32.165Z | 143.366° SSE |
| 4 mins | 2026-03-28 17:15:32.165Z | 323.752° NNW | 2026-03-28 17:17:32.165Z | 283.072° WNW | 18.231° | 2026-03-28 17:19:32.165Z | 248.36° W |
| 6 mins | 2026-03-29 03:53:32.165Z | 194.202° SSW | 2026-03-29 03:55:32.165Z | 239.279° WSW | 34.408° | 2026-03-29 03:59:32.165Z | 335.101° 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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