| /dports/astro/libgal/libgal-0.5.0/sgp4/ |
| H A D | gal_sgp4.c | 114 mvt , rdotl , rl , rvdot , rvdotl , sinim , in gal_sgp4() local
382 rvdotl = sqrt ( pl ) / rl ; in gal_sgp4()
411 rvdot = rvdotl + nm * temp1 * ( sgp4->x1mth2 * cos2u + 1.5 * sgp4->con41 ) / sgp4->xke ; in gal_sgp4()
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| /dports/astro/pykep/pykep-2.6/src/third_party/cspice/ |
| H A D | zzsgp4.c | 104 rvdotl, rtemsq; in zzsgp4_0_() local
1708 rvdotl = sqrt(pl) / rl; in zzsgp4_0_()
1734 rvdot = rvdotl + xn * temp1 * (x1mth2 * cos2u + con41 * 1.5) / xke; in zzsgp4_0_()
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| /dports/astro/py-pykep/pykep-2.6/src/third_party/cspice/ |
| H A D | zzsgp4.c | 104 rvdotl, rtemsq; in zzsgp4_0_() local
1708 rvdotl = sqrt(pl) / rl; in zzsgp4_0_()
1734 rvdot = rvdotl + xn * temp1 * (x1mth2 * cos2u + con41 * 1.5) / xke; in zzsgp4_0_()
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| /dports/astro/kstars/kstars-3.5.6/kstars/skyobjects/ |
| H A D | satellite.cpp | 719 …mrt = 0.0, mvt, rdotl, rl, rvdot, rvdotl, sinim, dndt, sin2u, sineo1 = 0, sini, sinip, sinsu, sinu… in sgp4() local
1071 rvdotl = sqrt(pl) / rl; in sgp4()
1096 rvdot = rvdotl + nm * temp1 * (x1mth2 * cos2u + 1.5 * con41) / XKE; in sgp4()
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| /dports/astro/marble/marble-21.12.3/src/3rdparty/sgp4/ |
| H A D | sgp4unit.cpp | 1704 mvt , rdotl , rl , rvdot , rvdotl, sinim , in sgp4() local
1913 rvdotl = sqrt(pl) / rl; in sgp4()
1939 rvdot = rvdotl + nm * temp1 * (satrec.x1mth2 * cos2u + in sgp4()
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| /dports/astro/stellarium/stellarium-0.21.3/plugins/Satellites/src/gsatellite/ |
| H A D | sgp4unit.cpp | 1659 mvt , rdotl , rl , rvdot , rvdotl, sinim , in sgp4() local
1865 rvdotl = std::sqrt(pl) / rl; in sgp4()
1891 rvdot = rvdotl + nm * temp1 * (satrec.x1mth2 * cos2u + 1.5 * satrec.con41) / xke; in sgp4()
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| /dports/astro/py-sgp4/python-sgp4-2.20/extension/ |
| H A D | SGP4.cpp | 1756 mvt, rdotl, rl, rvdot, rvdotl, sinim, in sgp4() local
1975 rvdotl = sqrt(pl) / rl; in sgp4()
2001 rvdot = rvdotl + nm * temp1 * (satrec.x1mth2 * cos2u + in sgp4()
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| /dports/astro/py-sgp4/python-sgp4-2.20/sgp4/ |
| H A D | propagation.py | 1889 rvdotl = sqrt(pl) / rl;
1915 rvdot = rvdotl + nm * temp1 * (satrec.x1mth2 * cos2u +
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| /dports/astro/p5-Astro-satpass/Astro-satpass-0.122/lib/Astro/Coord/ECI/ |
| H A D | TLE.pm | 6700 $omgadf, $pl, $rdotl, $rl, $rvdot, $rvdotl, $sinim, $sin2u,
6884 $rvdotl= sqrt($pl)/$rl;
6910 $rvdot= $rvdotl+ $xn*$temp1*
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