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: 15 hours ago
TLE from 15 hours ago
0 ITASAT
1 43786U 18099AE 26235.85318234 .00005380 00000-0 25384-3 0 9998
2 43786 97.3982 286.0281 0014026 113.7449 246.5258 15.19792675423189Epoch: 2026-08-23T20:28Z
TLE epoch observation values (Epoch: 2026-08-23T20:28:34.954Z)
Latitude
-0.00009°
Longitude
6.73919°
Altitude
513.416 km
Speed
7.605 km/s
True Right ascension
19h 04m 06s
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
02:50:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.085 km
Perigee altitude
493.78 km
Semi-major axis
6,881.569 km
Eccentricity
0.0014
Inclination
97.3982°
RAAN
286.0281°
Arg. of periapsis
113.7449°
True anomaly
246.37848°
Mean anomaly
246.5258°
Eccentric anomaly
246.45213°
Mean motion
3.802 °/min
Orbital period
94.69 mins
BSTAR
0.00025384
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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 | 2026-08-24 16:00:37.882Z | 28.142° NE | 2026-08-24 16:03:37.882Z | 127.508° SE | 36.054° | 2026-08-24 16:06:37.882Z | 176.213° S |
| 4 mins | 2026-08-25 02:39:37.882Z | 103.698° ESE | 2026-08-25 02:41:37.882Z | 60.924° ENE | 18.988° | 2026-08-25 02:43:37.882Z | 24.961° NE |
| 4 mins | 2026-08-25 04:13:37.882Z | 231.781° WSW | 2026-08-25 04:14:37.882Z | 254.354° W | 21.209° | 2026-08-25 04:17:37.882Z | 315.208° 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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