Step 1: Definition of a geostationary orbit (GEO).
A geostationary satellite appears fixed to an observer on the Earth because its angular velocity about the Earth's axis equals that of the Earth's rotation.
This requires: (i) zero inclination (orbit in the equatorial plane), (ii) zero eccentricity (circular), and (iii) orbital period equal to one sidereal day.
Step 2: Check each statement against GEO requirements.
(A) GEO must have inclination \(i=0^\circ\), i.e., the orbit lies in the equatorial plane. \(\Rightarrow\) True.
(B) For a satellite to remain over the same ground longitude, its orbital speed must be constant; hence the orbit is circular and centered at the Earth's center (geocentric). \(\Rightarrow\) True.
(C) The orbital period of GEO is not 90 minutes. Using Kepler's third law, \[ T = 2\pi\sqrt{\frac{a^3}{\mu}},\quad a\approx 42{,}164\,\text{km},\;\mu=3.986\times10^{14}\,\text{m}^3\text{s}^{-2}. \] This gives \(T\approx 86{,}164\,\text{s}\approx 23\,\text{h}\,56\,\text{min}\,(= \text{sidereal day})\approx 1436\,\text{min}.\)
A 90-minute period corresponds to low Earth orbit (LEO), not GEO. \(\Rightarrow\) False.
(D) A GEO satellite is not visible from all points on Earth. From geometry, the maximum latitude from which GEO is visible is roughly \[ \phi_{\max} \approx \cos^{-1}\!\left(\frac{R_E}{a}\right)\approx \cos^{-1}\!\left(\frac{6378}{42164}\right)\approx 81^\circ, \] so it is not visible from the polar regions, nor from the opposite hemisphere beyond the Earth's horizon. \(\Rightarrow\) False.
\[ \boxed{\text{Correct statements: (A), (B).}} \]
F and G denote two points on a spacecraft’s orbit around a planet, as indicated in the figure. O is the center of the planet, P is the periapsis, and the angles are as indicated in the figure. If \( OF = 8000 \, {km} \), \( OG = 10000 \, {km} \), \( \theta_F = 0^\circ \), and \( \theta_G = 60^\circ \), the eccentricity of the spacecraft's orbit is __________ (rounded off to two decimal places).
F and G denote two points on a spacecraft’s orbit around a planet, as indicated in the figure. O is the center of the planet, P is the periapsis, and the angles are as indicated in the figure. If \( OF = 8000 \, {km} \), \( OG = 10000 \, {km} \), \( \theta_F = 0^\circ \), and \( \theta_G = 60^\circ \), the eccentricity of the spacecraft's orbit is ___________ (rounded off to two decimal places).
