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: 2 days ago
TLE from 2 days ago
0 ITASAT
1 43786U 18099AE 26171.11764083 .00005183 00000-0 24987-3 0 9992
2 43786 97.4025 222.5709 0011788 349.8108 10.2885 15.19087166413356Epoch: 2026-06-20T02:49Z
TLE epoch observation values (Epoch: 2026-06-20T02:49:24.167Z)
Latitude
-0.00012°
Longitude
-88.11664°
Altitude
503.698 km
Speed
7.617 km/s
True Right ascension
14h 50m 17s
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
21:38:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.68 km
Perigee altitude
497.45 km
Semi-major axis
6,883.702 km
Eccentricity
0.00118
Inclination
97.4025°
RAAN
222.5709°
Arg. of periapsis
349.8108°
True anomaly
10.31266°
Mean anomaly
10.2885°
Eccentric anomaly
10.30058°
Mean motion
3.80023 °/min
Orbital period
94.73 mins
BSTAR
0.00024987
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 15:29:12.043Z | 59.208° ENE | 2026-06-22 15:31:12.043Z | 99.289° ESE | 18.444° | 2026-06-22 15:33:12.043Z | 135.818° SSE |
| 4 mins | 2026-06-22 17:03:12.043Z | 328.057° NNW | 2026-06-22 17:05:12.043Z | 280.091° WNW | 22.82° | 2026-06-22 17:07:12.043Z | 240.939° WSW |
| 5 mins | 2026-06-23 03:41:12.043Z | 184.271° SSW | 2026-06-23 03:43:12.043Z | 268.598° W | 41.901° | 2026-06-23 03:46:12.043Z | 340.147° 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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