Satellite Period ಅನ್ನು ಹೇಗೆ ಲೆಕ್ಕ ಹಾಕುವುದು

Satellite Period ಎಂದರೇನು?

Satellite orbital period (Kepler third law) depends on orbital radius and central body mass: T² ∝ a³.

ಸೂತ್ರ

T

2π√(a³/GM) — 2π√(a³/GM)

GM

GM value — Variable used in the calculation

ಹಂತ-ಹಂತದ ಮಾರ್ಗದರ್ಶಿ

1. 1Input orbital radius or planet name with altitude
2. 2Apply T = 2π√(a³/GM)
3. 3Results show period in hours/days

Worked Examples

Common Mistakes to Avoid

• ✕Confusing orbital radius with altitude
• ✕Forgetting Earth radius in altitude conversion

Frequently Asked Questions