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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Edit Public Description
Identifier
Orbit
Country
Unknown / 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: 8 hours ago
TLE from 8 hours ago
0 ITASAT
1 43786U 18099AE 25291.10173662 .00014442 00000-0 77736-3 0 9998
2 43786 97.4419 342.5966 0015195 113.3531 246.9301 15.14840324376202Epoch: 2025-10-18T02:26Z
TLE epoch observation values (Epoch: 2025-10-18T02:26:30.043Z)
Latitude
-0.00011°
Longitude
-80.86615°
Altitude
528.668 km
Speed
7.596 km/s
True Right ascension
22h 50m 23s
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
04:57:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.917 km
Perigee altitude
507.958 km
Semi-major axis
6,896.575 km
Eccentricity
0.00152
Inclination
97.4419°
RAAN
342.5966°
Arg. of periapsis
113.3531°
True anomaly
246.77002°
Mean anomaly
246.9301°
Eccentric anomaly
246.85005°
Mean motion
3.7896 °/min
Orbital period
95 mins
BSTAR
0.00077736
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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 | 2025-10-18 15:42:06.543Z | 46.096° ENE | 2025-10-18 15:45:06.543Z | 108.364° ESE | 21.334° | 2025-10-18 15:47:06.543Z | 144.956° SSE |
| 4 mins | 2025-10-18 17:17:06.543Z | 323.314° NNW | 2025-10-18 17:19:06.543Z | 280.221° WNW | 19.065° | 2025-10-18 17:21:06.543Z | 245.373° WSW |
| 5 mins | 2025-10-19 03:57:06.543Z | 200.804° SSW | 2025-10-19 03:59:06.543Z | 276.041° WNW | 35.765° | 2025-10-19 04:02:06.543Z | 334.289° 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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