Solution
Related Formula
- Orbital speed (v₀) of a satellite at distance r from earth's center:
- Orbital Radius:
- Kinetic Energy of the orbiting satellite:
r = Rₑ + h
Core Logic
Given parameters:
- Mass of satellite m = 1000 kg = 10³ kg
- Orbit altitude h = 270 km = 0.27 × 10⁶ m
- Earth Radius Rₑ = 6.4 × 10⁶ m
- Earth Mass Mₑ = 6 × 10²⁴ kg
- Gravitational constant G = 6.67 × 10⁻¹¹ N · m² / kg²
Step 1: Calculate kinetic energy
First, compute the orbital radius r:
r = Rₑ + h = 6.4 × 10⁶ m + 0.27 × 10⁶ m = 6.67 × 10⁶ mSubstitute r = 6.67 × 10⁶ m into the kinetic energy equation:
KE = (G Mₑ m)/(2 r) KE = 6.67 × 10⁻¹¹ × 6 × 10²⁴ × 10³2 × 6.67 × 10⁶Notice that the value 6.67 cancels out directly:
KE = 6 × 10¹⁶2 × 10⁶ = 3 × 10¹⁰ JThus, the kinetic energy coefficient is 3.
Pattern Recognition
Sees: Kinetic energy of a satellite orbiting at an altitude above earth's surface. Trap: Doing long division calculation for 6.67/2. Check for clean cancellations in formulas first! Shortcut: Notice that Rₑ + h = 6.4 × 10⁶ + 0.27 × 10⁶ = 6.67 × 10⁶, which matches the value of the Gravitational constant G = 6.67 × 10⁻¹¹ perfectly. This clean cancellation leaves behind simple integer math to give 3 × 10¹⁰ ~J immediately.
Chapter Mix
Class 11 Physics: Gravitation