Physics · Gravitation

JEE Main 2026 — 21 January, Morning Shift — Question 41

Initially a satellite of 100 kg is in a circular orbit of radius 1.5RE1.5 \mathrm{R}_{\mathrm{E}}. This satellite can be moved to a circular orbit of radius 3RE3 \mathrm{R}_{\mathrm{E}} by supplying α×106 J\alpha \times 10^{6} \mathrm{~J} of energy. The value of α\alpha is ____\_\_\_\_ . (Take Radius of Earth RE=6×106 m\mathrm{R}_{\mathrm{E}}=6 \times 10^{6} \mathrm{~m} and g=10m/s2\mathrm{g}=10 \mathrm{m} / \mathrm{s}^{2} )

  1. Option A:

    150

  2. Option B:

    500

  3. Option C:

    100

  4. Option D:

    1000

    Correct

Answer: D

Step-by-step solution

Energy of a satellite in a circular orbit is given as E=−GMEm2r;r=\mathrm{E}=\frac{-\mathrm{GM}_{\mathrm{E}} \mathrm{m}}{2 \mathrm{r}} ; \mathrm{r}= radius of circular orbit Required energy to be supplied =ΔE=Ef−Ei=\Delta \mathrm{E}=\mathrm{E}_{\mathrm{f}}-\mathrm{E}_{\mathrm{i}}

ΔE=(−GME m2(3RE))−(−GME m2(1.5RE))=GME m6RE\begin{aligned} \Delta \mathrm{E} & =\left(\frac{-\mathrm{GM}_{\mathrm{E}} \mathrm{~m}}{2\left(3 \mathrm{R}_{\mathrm{E}}\right)}\right)-\left(\frac{-\mathrm{GM}_{\mathrm{E}} \mathrm{~m}}{2\left(1.5 \mathrm{R}_{\mathrm{E}}\right)}\right) & =\frac{\mathrm{GM}_{\mathrm{E}} \mathrm{~m}}{6 \mathrm{R}_{\mathrm{E}}} \end{aligned}

Now, g=GMERE2⇒GMERE=gRE\mathrm{g}=\frac{\mathrm{GM}_{\mathrm{E}}}{\mathrm{R}_{\mathrm{E}}^{2}} \Rightarrow \frac{\mathrm{GM}_{\mathrm{E}}}{\mathrm{R}_{\mathrm{E}}}=\mathrm{gR}_{\mathrm{E}}

∴ΔE=16gmRE=16×10×100×6×106=1000×106\begin{aligned} \therefore \quad \Delta \mathrm{E} & =\frac{1}{6} \mathrm{gmR}_{\mathrm{E}} & =\frac{1}{6} \times 10 \times 100 \times 6 \times 10^{6} & =1000 \times 10^{6} \end{aligned}

α=1000\alpha=1000

Answer key and solution verified before publishing.

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Exam
JEE Main 2026
Subject
Physics
Chapter
Gravitation
Topic
Motion of Satellites and Escape Speed