Converting a state vector/orbital elements to a TLE

版本 1.0.1 (323.3 KB) 作者: David Eagle
MATLAB scripts that can be used to calculate an a Two Line Element (TLE) from a user-provided osculating state vector or orbital elements.
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更新时间 2022/12/28

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MATLAB script that can be used to calculate an approximate Two Line Element (TLE) set from a user-provided osculating state vector or classical orbital elements. It is valid for spacecraft that can be modeled using the NORAD SGP4 algorithm. Includes PDF users guide.

引用格式

David Eagle (2024). Converting a state vector/orbital elements to a TLE (https://www.mathworks.com/matlabcentral/fileexchange/104065-converting-a-state-vector-orbital-elements-to-a-tle), MATLAB Central File Exchange. 检索来源 .

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创建方式 R2019b
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版本 已发布 发行说明
1.0.1

Added Scott Campbell's algorithm
1.0.0