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: 18 hours ago
TLE from 18 hours ago
0 ITASAT
1 43786U 18099AE 25258.66059631 .00006640 00000-0 36733-3 0 9994
2 43786 97.4471 310.8595 0013004 221.4983 138.5262 15.14118694371299Epoch: 2025-09-15T15:51Z
TLE epoch observation values (Epoch: 2025-09-15T15:51:15.521Z)
Latitude
-0.00005°
Longitude
78.18278°
Altitude
533.468 km
Speed
7.592 km/s
True Right ascension
20h 43m 26s
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
02:22:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.602 km
Perigee altitude
511.66 km
Semi-major axis
6,898.768 km
Eccentricity
0.0013
Inclination
97.4471°
RAAN
310.8595°
Arg. of periapsis
221.4983°
True anomaly
138.62477°
Mean anomaly
138.5262°
Eccentric anomaly
138.5755°
Mean motion
3.78779 °/min
Orbital period
95.04 mins
BSTAR
0.00036733
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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 | 2025-09-16 16:12:58.844Z | 23.204° NE | 2025-09-16 16:15:58.844Z | 113.419° SE | 40.338° | 2025-09-16 16:18:58.844Z | 178.896° S |
| 5 mins | 2025-09-17 02:53:58.844Z | 116.151° SE | 2025-09-17 02:55:58.844Z | 74.85° E | 23.308° | 2025-09-17 02:58:58.844Z | 17.09° NNE |
| 4 mins | 2025-09-17 04:28:58.844Z | 237.658° WSW | 2025-09-17 04:29:58.844Z | 257.988° W | 19.028° | 2025-09-17 04:32:58.844Z | 312.378° NW |
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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