What are the different methods for calculating satellite altitude?

AI Thread Summary
Calculating satellite altitude can be achieved through various methods, including pressure sensors at near-space levels and accelerometers, although the latter is less effective in orbit due to the lack of acceleration. Satellites often rely on a combination of Earth sensors, sun sensors, star trackers, directed antennas, and ground-based lasers for accurate altitude measurements. In low Earth orbit, GPS technology is also utilized for precise positioning. Each method has its own mathematical formulas and applications, depending on the satellite's operational altitude. Understanding these techniques is crucial for effective satellite navigation and positioning.
trunet
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Hi,

I'd like to know how it's possible to calculate the altitude of a satellite using some kind sensor.

I know that near-space(28~30km) you can still read a very low pressure so I can calculate the altitude using pressure. But and after this? I read that you can use gravity so, can I use an accelerometer? How's the math/formulas on this?
 
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Radar?

A satellite can't feel any acceleration so that's not going to work afaik.
 
Satellites will typically use some combination of Earth sensors, sun sensors, star trackers, directed antennas or lasers from the ground, and accelerometers. Low Earth orbit also gives you the ability to use GPS.
 
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/
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