Question on projecting orbits using TLE

1. A concise explanation of the problem you're experiencing.

I'm doing a project in cesium and trying to find a way to project orbit paths about ten years in advance. I'm very confused about the tools that I could use to do this; I've looked into AGI STK, sgp4, etc. and nothing is quite making sense to me.

2. A minimal code example. If you've found a bug, this helps us reproduce and repair it.

3. Context. Why do you need to do this? We might know a better way to accomplish your goal.

Essentially, I have my own data on a current orbit path, and I want to be able to project in the future so that if I pick a future date, I will see the satellites' projected location over earth. I am not worried about the date selector or the display of the satellite, but rather my issue is regarding how to actually generate future orbit paths.

4. The Cesium version you're using, your operating system and browser.

Hi there,

Cesium is more of a visualization tool. The goal is to perform more intensive analytical work offline, then view it in Cesium. I think what you need is AGI’s STK Components, which provides more analytical services. We have a showcase that gives an overview and how it’s related to Cesium.