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The U.S. Space Force's Simplified General Perturbations software, version 4, must be used to correctly interpret the orbit data format known as TLE (Two-Line Elements).

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Conversion of osculating orbital elements to TLE mean elements

However, the propagation of TLE by SGP4 returns state vector, which can be transformed to osculating elements. Is it possible to transform osculating to TLE mean elements? … In our case, this model is SGP4. However, on what time scales should the averaging be done over? …
klobaska soslaninou's user avatar