STRATEGI STATION KEEPING SATELIT GEO (STUDI KASUS SES-7)
An ideal GEO satellite is a satellite that has orbital element eccentricity e=0, inclination i=0, semimajor axis a=42,164.26687 km and meaningless to measure the argument of perigee ???? the right ascension of ascending node ????. This function of satellite is as communication relay. Because of the...
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Main Author: | Fitri, Elisa |
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Format: | Final Project |
Language: | Indonesia |
Subjects: | |
Online Access: | https://digilib.itb.ac.id/gdl/view/47913 |
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Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
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