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gomezzz committed Jul 14, 2023
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4 changes: 2 additions & 2 deletions examples/Orekit_example/orekit_integration.ipynb
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"utc = TimeScalesFactory.getUTC()\n",
"epoch = AbsoluteDate(2020, 1, 1, 0, 0, 00.000, utc)\n",
"\n",
"# Let's define some orbit and a satellite mass\n",
"# We use an orbit with a semi-major axis of 7000 km, a eccentricity of 0.5 and an inclination of 0°\n",
"# Let's define some orbit and a satellite mass of 1000 kg\n",
"# We use an orbit with a semi-major axis of 10000 km, a eccentricity of 0.75 and an inclination of 1e-4°\n",
"orbital_elements = [10000000.0, 0.75, 0.0001, 0.0, 0.0, 0.0]\n",
"satellite_mass = 1000.0\n",
"\n",
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