See attachments Essay Example | Topics and Well Written Essays - 10000 words

See attachments - Essay role modelUnited States also used Gemini capsules to set out weapons and do surveillance of the outer blank space and the earth. This task highlights the endeavors taken by the United Nations in securing the use of the space. This task looks at the possibility of having the future day war in the space. With the increased superiority struggle between incompatible states over control of the space, there is a possibility that, indeed, the future war could be in the space.Satellites follow definite paths as they go around the earth. Likewise, other celestial bodies that move around other bodies follow regular pathways. Classification of orbits takes different approaches depending on the position of the orbit. They can be classified based on a number of considerations. Astronauts hurt devised taxonomy of orbits based on Centric Classifications, Inclination Classifications, Altitude Classification in Geocentric Orbits, Classifications based on Eccentricity, Sy nchronicity Classifications, Classifications based on galaxies and Galaxy Models, Pseudo-Orbital Classifications and other special classifications3.Special taxonomy of orbits classifies orbits into sun synchronous orbits and lunar month orbits. Sun synchronous orbits are those that combine inclination and altitude in such a vogue that the satellite on the orbits passes over a particular point on the surface of the planet at the same local solar time. Such orbits place a satellite on a eternal sunlight exposure and are useful for spying, imaging and as weather satellites. Moon orbits have the orbital traits of the Earths Moon. They lie at an average altitude of 238,857 miles and are elliptically inclined. Pseudo-Orbit Classification classifies orbits into Horseshoe Orbits, lunar Transfer Orbits (LTO), Retrograde Orbits, Prograde Orbits and Halo Orbits4. To a ground observer, a Horseshoe Orbit appears to be orbiting some other planet while in real sense they usually co-orbit anoth er