SGP4

The SGP4 model to calculate orbital state vectors of near-Earth satellites

Version 2.1.1 (1.76 MB)
6.4K Downloads
(25)
30 Aug 2023
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Cite As

Meysam Mahooti (2026). SGP4 (https://in.mathworks.com/matlabcentral/fileexchange/62013-sgp4), MATLAB Central File Exchange. Retrieved .

Acknowledgements

Inspired: epoch2datevec(tle_epoch)

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General Information

MATLAB Release Compatibility

  • Compatible with any release

Platform Compatibility

  • Windows
  • macOS
  • Linux
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Version Published Release Notes
2.1.1

test_sgp4.m was modified.
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2.1.0

The vectorized SGP4 package was added.
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2.0.1

satdata.xndt2o in test_sgp4.m was corrected.
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2.0.0

Mjday.m was modified.
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1.1.1

test_sgp4.m is modified.
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1.1.0

Satellite's state vector is computed in four different coordinate systems, i.e. Earth-centered inertial (ECI), Earth-centered Earth-fixed (ECEF), true of date (TOD) and true equator mean equinox (TEME).
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1.0.0

.
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