Version 2.24

setup.py

@@ -54,18 +54,15 @@
         'Intended Audience :: Science/Research',
         'License :: OSI Approved :: MIT License',
         'Programming Language :: Python :: 2',
-        'Programming Language :: Python :: 2.6',
         'Programming Language :: Python :: 2.7',
         'Programming Language :: Python :: 3',
-        'Programming Language :: Python :: 3.3',
-        'Programming Language :: Python :: 3.4',
-        'Programming Language :: Python :: 3.5',
-        'Programming Language :: Python :: 3.6',
-        'Programming Language :: Python :: 3.7',
         'Programming Language :: Python :: 3.8',
         'Programming Language :: Python :: 3.9',
+        'Programming Language :: Python :: 3.10',
+        'Programming Language :: Python :: 3.11',
+        'Programming Language :: Python :: 3.12',
         'Topic :: Scientific/Engineering :: Astronomy',
-        ],
+      ],
       packages = ['sgp4'],
       package_data = {'sgp4': ['SGP4-VER.TLE', 'sample*', 'tcppver.out']},
       ext_modules = ext_modules,

sgp4/__init__.py

@@ -652,13 +652,15 @@
 Changelog
 ---------
 
-Unreleased — 2.24
+2024-02-15 — 2.24
 
 * The documentation now specifies the acceptable range for orbital
   element angles like inclination and mean anomaly, and a new function
   ``check_satrec(sat)`` will tell the caller if any of the angles are
   out of bounds.
 
+* The documentation now gives an example of loading elements from JSON.
+
 * Tweaked the fallback Python code to accept TLE lines without a final
   checksum character in the 69th column, to match the C++ code.
 
@@ -753,4 +755,4 @@
 | 2012-08-27 — 1.0 — Initial release
 
 """
-__version__ = '2.23'
+__version__ = '2.24'