Showing default

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.

Loading next visibility...
Identifier
43786, 2018-099AE
Orbit
SSO
Country
Flag of UnknownUnknown / BRAZ
Related business
Manufacturer
ITA
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
2018-12-03 (7 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 ITASAT
1 43786U 18099AE  26034.41706898  .00008779  00000-0  44529-3 0  9991
2 43786  97.4238  88.6415 0014613  98.5888 261.7002 15.17078298392613
Epoch: 2026-02-03T10:00Z
TLE epoch observation values (Epoch: 2026-02-03T10:00:34.759Z)
Latitude
-0.00004°
Longitude
164.89837°
Altitude
519.231 km
Speed
7.603 km/s
True Right ascension
05h 54m 33s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
09:20:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.715 km
Perigee altitude
501.579 km
Semi-major axis
6,889.784 km
Eccentricity
0.00146
Inclination
97.4238°
RAAN
88.6415°
Arg. of periapsis
98.5888°
True anomaly
261.53455°
Mean anomaly
261.7002°
Eccentric anomaly
261.61737°
Mean motion
3.7952 °/min
Orbital period
94.86 mins
BSTAR
0.00044529
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|