def to_sv(arr, form):
return StateVector(
arr,
ref_kepl_hyper.date,
form,
ref_kepl_hyper.frame,
)
def ref_kepl_hyper(ref_date):
return StateVector(
[
-7192631.11295, 1.00218439, 1.71926101045,
5.51044449998, 1.17890601985, 0.1,
],
ref_date,
KEPL,
"EME2000"
)
def ref_tle(ref_date):
return StateVector(
[
1.71926101e+00, 5.51044450e+00, 2.18439000e-03,
1.17890602e+00, 3.04334144e+00, 1.03499315e-03
],
ref_date,
TLE,
"EME2000"
)
def ref_kepl_c(ref_date):
return StateVector(
[
7.19263111e+06, 8.34297391e-04, 2.01878863e-03,
1.71926101e+00, 5.51044450e+00, 4.22224746e+00
],
ref_date,
KEPL_C,
"EME2000"
)
def ref_sphe(ref_date):
return StateVector(
[
7.20826718e+06, 2.09815148e+00, -1.06082733e+00,
1.58820333e+00, -6.39690485e-04, -9.82054932e-04
],
ref_date,
SPHE,
"EME2000"
)
def ref_cart(ref_date):
return StateVector(
[
-1.77079285e+06, 3.04066799e+06, -6.29108469e+06,
5.05386814e+03, -4.20539932e+03, -3.45695948e+03
],
ref_date,
CART,
"EME2000"
)
def ref_kepl_m(ref_date):
return StateVector(
[
7192631.11295, 0.00218439, np.deg2rad(98.50639978),
np.deg2rad(315.72521309), np.deg2rad(67.54633938), np.deg2rad(174.37062038)
],
ref_date,
KEPL_M,
"EME2000"
)
def ref_cyl(ref_date):
return StateVector(
[
3.51871697e+06, 2.09815148e+00, -6.29108469e+06,
-6.17741547e+03, -6.39690485e-04, -3.45695948e+03
],
ref_date,
CYL,
"EME2000"
)
def ref_equi(ref_date):
return StateVector(
[
7.19263111e+06, 2.00667384e-03, 8.63029427e-04,
8.31052761e-01, -8.10276759e-01, 9.73311935e+00
],
ref_date,
EQUI,
"EME2000"
)
def ref_kepl(ref_date):
return StateVector(
[
7192631.11295, 0.00218439, 1.71926101045,
5.51044449998, 1.17890601985, 3.04376883055,
],
ref_date,
KEPL,
"EME2000"
)