
Originally Posted by
randzg
1. elliptical orbit is easier because if you are trying to achieve a circular orbit, the velocity and fuel burning you will need has to be very accurate. If you burn fuel a little to much, elliptical na dayon, a little to less, elliptical na pud dayon. if this is the case, aw, mas sayon cguro mag achieve nalang elliptical orbit.
Very good answer! Actually, the answer is more detailed than that, because not only does the burn need to be "very accurate", you need to constantly make very fine changes in
pitch (relative to the local horizon, in this case, Earth horizon) just to make sure that you arrive at a circular orbit, and yes, these changes in pitch can be very demanding (esp. if the spacecraft/rocket is being flown manually!) and needs a high degree of accuracy in order to ensure an orbit with the least eccentricity (nearly circular). On the other hand, if you launch a rocket that does not have the sophisticated pitch corrections needed to achieve a circular orbit, then all you need is a timer that changes pitch at measured intervals while the rocket is trying to achieve orbit, and when fuel nears zero, all you need to ensure is that the pitch angle (the orientation of the nose of the rocket with respect to the horizon) should be zero.

Originally Posted by
randzg
2. Earth is not a perfect sphere to begin with.. naa cguro changes in gravitational pull (small maybe).
Correct, but too small (i.e. negligible) to matter.

Originally Posted by
randzg
3. Earth is also rotating around the sun and has velocity - assuming ari ta sa equator dapit mo orbit.
Sun has negligible influence in this exercise.

Originally Posted by
randzg
4. Gravity from other bodies like moon might also affect orbit.
Same answer with sun.
All in all, a pretty good answer

Will supplement your answer with my illustrations later.
-RODION