Home
last modified time | relevance | path

Searched refs:vkmpersec (Results 1 – 9 of 9) sorted by relevance

/dports/astro/libgal/libgal-0.5.0/sgp4/
H A Dgal_sgp4.c441 pv[1][0] = ( mvt * ux + rvdot * vx) * sgp4->vkmpersec * GAL_KM2M ; in gal_sgp4()
442 pv[1][1] = ( mvt * uy + rvdot * vy) * sgp4->vkmpersec * GAL_KM2M ; in gal_sgp4()
443 pv[1][2] = ( mvt * uz + rvdot * vz) * sgp4->vkmpersec * GAL_KM2M ; in gal_sgp4()
H A Dgal_sgp4t.h99 double vkmpersec ; member
H A Dgal_sgp4init.c180 sgp4->vkmpersec = sgp4->radiusearthkm * sgp4->xke / 60.0 ; in gal_sgp4init()
/dports/astro/kstars/kstars-3.5.6/kstars/skyobjects/
H A Dsatellite.cpp723 … coslat, thetageo, sintheta, costheta, c, sq, achcp, vkmpersec; in sgp4() local
730 vkmpersec = RADIUSEARTHKM * XKE / 60.0; in sgp4()
1119 sat_velx = (mvt * ux + rvdot * vx) * vkmpersec; in sgp4()
1120 sat_vely = (mvt * uy + rvdot * vy) * vkmpersec; in sgp4()
1121 sat_velz = (mvt * uz + rvdot * vz) * vkmpersec; in sgp4()
/dports/astro/marble/marble-21.12.3/src/3rdparty/sgp4/
H A Dsgp4unit.cpp1712 mu, vkmpersec; in sgp4() local
1724 vkmpersec = radiusearthkm * xke/60.0; in sgp4()
1962 v[0] = (mvt * ux + rvdot * vx) * vkmpersec; in sgp4()
1963 v[1] = (mvt * uy + rvdot * vy) * vkmpersec; in sgp4()
1964 v[2] = (mvt * uz + rvdot * vz) * vkmpersec; in sgp4()
/dports/astro/stellarium/stellarium-0.21.3/plugins/Satellites/src/gsatellite/
H A Dsgp4unit.cpp1667 radiusearthkm, mu, vkmpersec; in sgp4() local
1687 vkmpersec = radiusearthkm * xke/60.0; in sgp4()
1913 v[0] = (mvt * ux + rvdot * vx) * vkmpersec; in sgp4()
1914 v[1] = (mvt * uy + rvdot * vy) * vkmpersec; in sgp4()
1915 v[2] = (mvt * uz + rvdot * vz) * vkmpersec; in sgp4()
/dports/astro/py-sgp4/python-sgp4-2.20/sgp4/
H A Dpropagation.py1698 vkmpersec = satrec.radiusearthkm * satrec.xke/60.0;
1937 v = ((mvt * ux + rvdot * vx) * vkmpersec,
1938 (mvt * uy + rvdot * vy) * vkmpersec,
1939 (mvt * uz + rvdot * vz) * vkmpersec)
/dports/astro/py-sgp4/python-sgp4-2.20/extension/
H A DSGP4.cpp1763 twopi, x2o3, vkmpersec, delmtemp; in sgp4() local
1775 vkmpersec = satrec.radiusearthkm * satrec.xke / 60.0; in sgp4()
2024 v[0] = (mvt * ux + rvdot * vx) * vkmpersec; in sgp4()
2025 v[1] = (mvt * uy + rvdot * vy) * vkmpersec; in sgp4()
2026 v[2] = (mvt * uz + rvdot * vz) * vkmpersec; in sgp4()
/dports/astro/p5-Astro-satpass/Astro-satpass-0.122/lib/Astro/Coord/ECI/
H A DTLE.pm6706 my ($mr, $mv, $vkmpersec, $temp4);
6723 $vkmpersec= $parm->{radiusearthkm}* $parm->{xke}/60;
6932 $v[1] = ($mv*$ux+ $rvdot*$vx) * $vkmpersec;
6933 $v[2] = ($mv*$uy+ $rvdot*$vy) * $vkmpersec;
6934 $v[3] = ($mv*$uz+ $rvdot*$vz) * $vkmpersec;