learn.howToCalculate
learn.whatIsHeading
Satellite orbital period (Kepler third law) depends on orbital radius and central body mass: T² ∝ a³.
सूत्र
Apply T = 2π√(a³/GM)
- T
- 2π√(a³/GM) — 2π√(a³/GM)
- GM
- GM value — Variable used in the calculation
चरण-दर-चरण मार्गदर्शिका
- 1Input orbital radius or planet name with altitude
- 2Apply T = 2π√(a³/GM)
- 3Results show period in hours/days
हल किए गए उदाहरण
इनपुट
ISS at 400 km altitude around Earth
परिणाम
T ≈ 90 minutes
16 orbits per day
सामान्य गलतियां जिनसे बचना है
- ✕Confusing orbital radius with altitude
- ✕Forgetting Earth radius in altitude conversion
अक्सर पूछे जाने वाले प्रश्न
Does satellite speed change with altitude?
Yes, inverse √r relationship; lower orbits faster.
learn.ctaText
इसे स्वयं आज़माएँ →