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Satellite Orbit Time Period Higher Orbits, Longer Loops

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https://youtu.be/l2JLFyjfDQ0

Автор: Engineer's India Solution

Загружено: 2025-09-18

Просмотров: 73

Описание: #   • Exploring Satellite Orbits Velocity and Pe...  
*Satellite Orbit Time Period – Higher Orbits, Longer Loops*
The motion of satellites around the Earth is governed by the laws of orbital mechanics, derived primarily from Newton’s law of gravitation and Kepler’s laws of planetary motion. A satellite in orbit is essentially in free fall, continuously “falling” toward the Earth but moving forward fast enough to avoid hitting it. The balance between gravitational attraction and the satellite’s tangential velocity determines the nature of its orbit. One of the most important parameters in this context is the **orbital time period**, i.e., the time taken by a satellite to complete one full revolution around the Earth.

#### *Relation Between Altitude and Orbital Time Period*

The orbital time period of a satellite depends directly on the altitude of its orbit. According to Kepler’s Third Law, the square of the orbital period is proportional to the cube of the semi-major axis of the orbit (the average distance from the Earth’s center). Mathematically:

$$
T^2 \propto r^3
$$

where:

*T* = orbital time period
*r* = distance from the Earth’s center (Earth’s radius + altitude of satellite)

This relationship means that as the satellite’s orbit becomes higher, the distance from the Earth’s center increases, leading to a longer orbital time period. In other words, **higher orbits correspond to longer loops and longer times to complete them**.

#### *Low Earth Orbit (LEO)*

Satellites placed in **Low Earth Orbit (LEO)**, at altitudes between 200 km and 2,000 km, travel at very high speeds to counteract Earth’s strong gravitational pull. Their orbital period is relatively short, typically around **90 to 120 minutes**. Because of this, a LEO satellite completes multiple revolutions each day. Examples include Earth observation satellites, the International Space Station (ISS), and many scientific research satellites.

#### *Medium Earth Orbit (MEO)*

When satellites are positioned at **Medium Earth Orbits (MEO)**, ranging from 2,000 km to 35,786 km, their orbital periods increase. For instance, navigation satellites in the GPS constellation are placed in MEO at about 20,200 km altitude, with orbital periods of roughly **12 hours**. These satellites provide continuous coverage with fewer satellites compared to LEO systems because their longer loops allow them to “see” a larger portion of the Earth at once.

#### *Geostationary Orbit (GEO)*

At an altitude of about **35,786 km**, satellites achieve a special orbit known as the **geostationary orbit**. At this distance, the orbital time period becomes exactly **24 hours**, matching the Earth’s rotation. This synchronization makes the satellite appear stationary relative to a fixed point on the Earth’s surface. Such satellites are ideal for communications, weather monitoring, and television broadcasting. Achieving this long time period is possible only because of the great distance from Earth, which creates a much larger orbital loop.

#### *Why Higher Orbits Mean Longer Loops*

The explanation is twofold:

1. *Larger Circumference* – A higher orbit naturally means a larger path (loop) around the Earth, so the satellite must travel a longer distance for one revolution.
2. *Lower Orbital Speed* – Gravity weakens with distance from Earth. At higher altitudes, satellites need less speed to stay in orbit. This slower speed, combined with the larger path, increases the orbital time period significantly.

#### *Conclusion*

In summary, the time period of a satellite is strongly influenced by its altitude. *Low Earth Orbit satellites zip around quickly with short periods, while higher orbit satellites move slower and take much longer to complete a revolution.* The principle of “higher orbits, longer loops” is fundamental to satellite communication, navigation, and Earth observation system design. Understanding this relationship enables engineers to place satellites precisely where they are most effective—whether for rapid coverage in LEO or fixed communication points in GEO.

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