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Types of Orbits

typesoforbits

Here’s a breakdown of the main types of orbits, categorized by altitude, shape, and purpose. Each orbit serves a specific function in satellite and space mission design:


πŸ›°οΈ By Altitude (Distance from Earth)

🟒 1. Low Earth Orbit (LEO)

  • Altitude: 160 to 2,000 km (100–1,200 miles)

  • Use: Earth observation, the ISS, communication satellites

  • Orbit Time: ~90 minutes

  • Key Feature: Fast orbit, ideal for imaging and monitoring

🟠 2. Medium Earth Orbit (MEO)

  • Altitude: 2,000 to 35,786 km

  • Use: GPS, navigation systems

  • Orbit Time: ~12 hours

  • Key Feature: Balanced coverage and speed

πŸ”΅ 3. Geostationary Orbit (GEO)

  • Altitude: 35,786 km (22,236 miles)

  • Use: Weather, TV, communication satellites

  • Orbit Time: 24 hours

  • Key Feature: Appears stationary over one point on Earth


πŸŒ€ By Shape

πŸŒ“ 4. Circular Orbit

  • Shape: Constant altitude and speed

  • Use: Many communication and scientific satellites

  • Key Feature: Uniform coverage and stable conditions

πŸŒ™ 5. Elliptical Orbit

  • Shape: Varying altitude (apogee = farthest, perigee = closest)

  • Use: Molniya orbits, some science missions

  • Key Feature: High coverage of one hemisphere during apogee


πŸ“ By Inclination / Purpose

🌍 6. Polar Orbit

  • Path: Passes over Earth’s poles

  • Use: Earth observation, weather, mapping

  • Key Feature: Global coverage as Earth rotates beneath

πŸ” 7. Sun-Synchronous Orbit

  • Path: A type of polar orbit that stays aligned with the sun

  • Use: Satellites that need consistent lighting (e.g., imaging)

  • Key Feature: Same local solar time on every pass

πŸ›°οΈ 8. Geosynchronous Orbit

  • Path: Same period as Earth’s rotation, but not necessarily equatorial

  • Use: Communication satellites

  • Key Feature: Same location in the sky each day (not fixed over one point)


πŸŒ• Other Specialized Orbits

πŸŒ— 9. Molniya Orbit

  • Path: Highly elliptical, high inclination

  • Use: Coverage of high latitudes (e.g., Russia, Canada)

  • Key Feature: Long dwell time over northern regions

πŸŒ‘ 10. Halo Orbit

  • Path: Around Lagrange points (gravitationally stable areas)

  • Use: Space telescopes, solar observatories

  • Key Feature: Ideal for stable long-term observation positions

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