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how How to find tlethe TLE (two-line element) for a satellite using orbitorbital parameters?

Can I calculate the two line-line element for a new satellite using the orbital parameters, and how to? How do I calculate mean motion for a satellite, is?

Is BSTAR drag term in tleTLE same for all satellites? ifIf not, then how todo I calculate BSTAR drag term  ?

how to find tle for a satellite using orbit parameters?

Can I calculate two line element for a new satellite using the orbital parameters, and how to calculate mean motion for a satellite, is BSTAR drag term in tle same for all satellites? if not then how to calculate BSTAR drag term  ?

How to find the TLE (two-line element) for a satellite using orbital parameters?

Can I calculate the two-line element for a new satellite using the orbital parameters? How do I calculate mean motion for a satellite?

Is BSTAR drag term in TLE same for all satellites? If not, then how do I calculate BSTAR drag term?

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how to find tle for a satellite using orbit parameters?

Can I calculate two line element for a new satellite using the orbital parameters, and how to calculate mean motion for a satellite, is BSTAR drag term in tle same for all satellites? if not then how to calculate BSTAR drag term ?