Satellite with period equal to that of its planet?

In summary, it is possible to have a satellite orbiting Earth slowly enough that it always stays between Earth and the sun, but it would be much farther away than geosynchronous satellites.
  • #1
Humaj
1
0
Would it be possible to have a satellite orbiting Earth slowly enough that it always stays between Earth and the sun? Not necessarily directly between so that its shadow is always on Earth, but such that, with an orbit that would take it "behind" Earth, it would orbit at a speed such that when it gets halfway through its orbit, Earth has gone halfway through its own, and its still on the inside of Earth's orbit? Probably much farther away than geosynchronous satellites?
This wouldn't be the same thing as an L1 point in my understanding of Lagrange points, because the object is solely in orbit around Earth, but might not be possible.
And please be specific as to why it's not possible if it's not, so I know whether to go with a fabricated excuse as to how it could be possible, or go with an actual possible story.
 
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  • #2
I suggest you could calculate the distance and see if it makes sense. My guess (I can be completely wrong) is that it would be as far away as the sun, since planetary orbits depend almost entirely on the distance from the sun.
 
  • #3
Humaj said:
Would it be possible to have a satellite orbiting Earth slowly enough that it always stays between Earth and the sun?

This wouldn't be the same thing as an L1 point in my understanding of Lagrange points, because the object is solely in orbit around Earth,

Why do you say this isn't the Lagrange point L1? In order to stay between the Earth and the Sun, it needs to orbit both the Sun and the Earth. Relative to the fixed stars, in one year, it will have made one orbit around the Sun, and it will have made one orbit around the Earth. I think this is what is meant by the Lagrange point L1. So the answer is, yes it is possible.
 
  • #4
Yes, but your radius would be beyond the L1/L2 Lagrange points.

Nothing wrong with that in theory, but keep in mind the Lagrange points are just orbits around the Sun where orbital perturbations from the Earth would keep a spaceship in a constant location relative to the Earth.

Your radius is so big (over 2 million kilometers) that it doesn't take much for other objects (the Moon, which is only 385,000 kilometers away, and the Sun, 150 million kilometers away) to alter your orbit. Just calculating the orbital period and saying you're good really wouldn't be good enough and I'm not positive you could even find a stable orbit like that around the Earth. Or else it would wind up putting you at the Lagrange point. (I've never actually started from that direction, but it would make sense. Edit: In fact, it has to work out that way regardless of your frame of reference. I've just become so accustomed to visualizing them as orbits around the Sun that it seems almost bizarre to use a geocentric frame of reference.)

So, in practice, it would make more sense to use the Lagrange points, since they accomplish the same thing.

And, no, that distance wouldn't match the Earth's distance from the Sun. Orbital period depends both upon the distance and the mass of the object you're orbiting around. The Earth's mass is much less than the Sun's. However, if you're talking only about how long for planets to orbit the Sun, or only how long for spacecraft to orbit the Earth, the mass of the object that you're orbiting around is usually treated as a constant (hence the possible confusion).
 
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  • #5


I can confirm that it is not possible for a satellite to have the same period as its planet while also maintaining a constant position between the planet and the sun. This is due to the laws of orbital mechanics and the gravitational forces at play.

Firstly, the period of an object in orbit is determined by its distance from the planet and its mass. The closer an object is to the planet, the shorter its period will be. In order for a satellite to have the same period as its planet, it would need to be at the exact same distance as the planet, which is not possible.

Secondly, the gravitational pull of the sun on the satellite would cause it to either speed up or slow down in its orbit, making it impossible for the satellite to maintain a constant position between the planet and the sun.

Additionally, the concept of a satellite being "behind" the planet and still maintaining a constant position is not possible. The satellite would need to be in a synchronized orbit with the planet, which would require precise timing and adjustments, making it highly unlikely and impractical.

In terms of the L1 point, this is a specific point in space where the gravitational forces of two objects (in this case, the Earth and the sun) cancel each other out, allowing for a stable orbit. However, this point is located outside of the Earth's orbit and would not allow for the satellite to be in a position between the planet and the sun.

In conclusion, while it may seem like a plausible scenario, the laws of orbital mechanics and the gravitational forces at play make it impossible for a satellite to have the same period as its planet while also maintaining a constant position between the planet and the sun. I would suggest exploring other possibilities or using a fabricated explanation for your story.
 

1. What is a satellite with a period equal to that of its planet?

A satellite with a period equal to that of its planet means that the satellite completes one orbit around its planet in the same amount of time as the planet completes one rotation on its axis. This is also known as synchronous rotation.

2. How does a satellite achieve a period equal to that of its planet?

A satellite can achieve a period equal to that of its planet through tidal locking, where the gravitational forces between the planet and the satellite cause the satellite's rotational and orbital periods to synchronize.

3. What are some examples of satellites with periods equal to their planets?

The most well-known example is the Moon, which has a period of 27.3 days and orbits around Earth in the same amount of time as Earth's rotation. Other examples include Pluto's moon Charon and Neptune's moon Triton.

4. What are the advantages of a satellite having a period equal to its planet?

A satellite with a period equal to its planet can have a stable orbit and maintain a fixed position relative to the planet. This is useful for communication and observation satellites, as they can continuously monitor a specific location on the planet's surface.

5. Are there any drawbacks to having a satellite with a period equal to its planet?

One potential drawback is that the satellite will always be facing the same side of the planet, limiting its ability to gather data from different angles. This can be overcome by using multiple satellites with different orbital periods. Additionally, the satellite may experience more intense radiation and tidal forces due to its close proximity to the planet.

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