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I have to be honest. Been learning python for few months but when I saw this code I was blown away, mainly by its simplicity and secondly by not understanding it .. can someone help me understand how to use "h_x && h_y" ? I have no clue where to start looking for this info. Thank you <3

import math
 
def calculate_longitude_of_ascending_node(h_x, h_y, h_z):
    # Calculate the magnitude of the specific relative angular momentum vector (|h|)
    h_magnitude = math.sqrt(h_x**2 + h_y**2 + h_z**2)
 
    # Calculate the unit vector n using the cross product of r and v
    n_x = h_y * h_z
    n_y = -h_x * h_z
    n_z = h_x**2 + h_y**2
 
    # Calculate the longitude of the ascending node (Ω) in radians
    omega = math.atan2(n_y, n_x)
    if omega < 0:
        omega += 2 * math.pi
 
    # Convert Ω from radians to degrees, minutes, and seconds
    omega_deg = math.degrees(omega)
    omega_deg_int = int(omega_deg)
    omega_min = (omega_deg - omega_deg_int) * 60
    omega_min_int = int(omega_min)
    omega_sec = (omega_min - omega_min_int) * 60
 
    return omega_deg_int, omega_min_int, omega_sec
 
# Example usage:
# Use the provided position data
x = 3.470705658033574E+05
y = -9.265520886744432E+04
z = -2.653599067380910E+04
vx = -9.011403192706635E-02
vy = 1.110259691085033E+00
vz = 5.115987924302562E-02
 
# Calculate h_x, h_y, h_z by taking the cross product of r and v
h_x = y * vz - z * vy
h_y = z * vx - x * vz
h_z = x * vy - y * vx
 
# Calculate the longitude of the ascending node in DMS
longitude_deg, longitude_min, longitude_sec = calculate_longitude_of_ascending_node(h_x, h_y, h_z)
print(f"Longitude of Ascending Node (Ω): {longitude_deg}° {longitude_min}' {longitude_sec:.2f}\"")

edit*** so I was able to get the x, y and z from Horizon

*******************************************************************************
 Revised: July 31, 2013             Moon / (Earth)                          301
 
 GEOPHYSICAL DATA (updated 2018-Aug-15):
  Vol. mean radius, km  = 1737.53+-0.03    Mass, x10^22 kg       =    7.349
  Radius (gravity), km  = 1738.0           Surface emissivity    =    0.92
  Radius (IAU), km      = 1737.4           GM, km^3/s^2          = 4902.800066
  Density, g/cm^3       =    3.3437        GM 1-sigma, km^3/s^2  =  +-0.0001  
  V(1,0)                =   +0.21          Surface accel., m/s^2 =    1.62
  Earth/Moon mass ratio = 81.3005690769    Farside crust. thick. = ~80 - 90 km
  Mean crustal density  = 2.97+-.07 g/cm^3 Nearside crust. thick.= 58+-8 km 
  Heat flow, Apollo 15  = 3.1+-.6 mW/m^2   Mean angular diameter = 31'05.2"
  Heat flow, Apollo 17  = 2.2+-.5 mW/m^2   Sid. rot. rate, rad/s = 0.0000026617
  Geometric Albedo      = 0.12             Mean solar day        = 29.5306 d
  Obliquity to orbit    = 6.67 deg         Orbit period          = 27.321582 d
  Semi-major axis, a    = 384400 km        Eccentricity          = 0.05490
  Mean motion, rad/s    = 2.6616995x10^-6  Inclination           = 5.145 deg
  Apsidal period        = 3231.50 d        Nodal period          = 6798.38 d
                                 Perihelion  Aphelion    Mean
  Solar Constant (W/m^2)         1414+-7     1323+-7     1368+-7
  Maximum Planetary IR (W/m^2)   1314        1226        1268
  Minimum Planetary IR (W/m^2)      5.2         5.2         5.2
********************************************************************************
 
 
*******************************************************************************
Ephemeris / WWW_USER Fri Sep 29 12:13:59 2023 Pasadena, USA      / Horizons
*******************************************************************************
Target body name: Moon (301)                      {source: DE441}
Center body name: Earth (399)                     {source: DE441}
Center-site name: Heaven on Earth Observatory, Mayhill
*******************************************************************************
Start time      : A.D. 2023-Sep-28 00:00:00.0000 TDB
Stop  time      : A.D. 2023-Oct-01 00:00:00.0000 TDB
Step-size       : 1440 minutes
*******************************************************************************
Center geodetic : 254.471, 32.9035384, 2.23607    {E-lon(deg),Lat(deg),Alt(km)}
Center cylindric: 254.471, 5362.17112, 3446.19639 {E-lon(deg),Dxy(km),Dz(km)}
Center pole/equ : ITRF93                          {East-longitude positive}
Center radii    : 6378.137, 6378.137, 6356.752 km {Equator_a, b, pole_c}
Output units    : KM-S
Calendar mode   : Mixed Julian/Gregorian
Output type     : GEOMETRIC cartesian states
Output format   : 3 (position, velocity, LT, range, range-rate)
EOP file        : eop.230927.p231221
EOP coverage    : DATA-BASED 1962-JAN-20 TO 2023-SEP-27. PREDICTS-> 2023-DEC-20
Reference frame : Ecliptic of J2000.0
*******************************************************************************
JDTDB
   X     Y     Z
   VX    VY    VZ
   LT    RG    RR
*******************************************************************************
$$SOE
2460215.500000000 = A.D. 2023-Sep-28 00:00:00.0000 TDB 
 X = 3.470705658033574E+05 Y =-9.265520886744432E+04 Z =-2.653599067380910E+04
 VX=-9.011403192706635E-02 VY= 1.110259691085033E+00 VZ= 5.115987924302562E-02
 LT= 1.201512151373686E+00 RG= 3.602042811771854E+05 RR=-3.761888927526311E-01
2460216.500000000 = A.D. 2023-Sep-29 00:00:00.0000 TDB 
 X = 3.612178246289230E+05 Y = 2.175102251481885E+02 Z =-1.933391485093577E+04
 VX=-3.538761876322111E-01 VY= 1.141964183533681E+00 VZ= 6.712048003763832E-02
 LT= 1.206617868501206E+00 RG= 3.617349366646974E+05 RR=-3.562710879736578E-01
2460217.500000000 = A.D. 2023-Sep-30 00:00:00.0000 TDB 
 X = 3.525900479296140E+05 Y = 9.334101334405206E+04 Z =-1.122942013890661E+04
 VX=-6.159050044487818E-01 VY= 1.104174316562248E+00 VZ= 7.721989291731685E-02
 LT= 1.217204527827483E+00 RG= 3.649087372861304E+05 RR=-3.150496228123838E-01
2460218.500000000 = A.D. 2023-Oct-01 00:00:00.0000 TDB 
 X = 3.221837310026606E+05 Y = 1.808849216335789E+05 Z =-2.748397019656826E+03
 VX=-8.568131300802702E-01 VY= 1.002000203732668E+00 VZ= 8.112992260778490E-02
 LT= 1.232514886108716E+00 RG= 3.694986672281219E+05 RR=-2.571795472029340E-01
$$EOE
*******************************************************************************
 
TIME
 
  Barycentric Dynamical Time ("TDB" or T_eph) output was requested. This
continuous coordinate time is equivalent to the relativistic proper time
of a clock at rest in a reference frame co-moving with the solar system
barycenter but outside the system's gravity well. It is the independent
variable in the solar system relativistic equations of motion.
 
  TDB runs at a uniform rate of one SI second per second and is independent
of irregularities in Earth's rotation.
 
CALENDAR SYSTEM
 
  Mixed calendar mode was active such that calendar dates after AD 1582-Oct-15
(if any) are in the modern Gregorian system. Dates prior to 1582-Oct-5 (if any)
are in the Julian calendar system, which is automatically extended for dates
prior to its adoption on 45-Jan-1 BC.  The Julian calendar is useful for
matching historical dates. The Gregorian calendar more accurately corresponds
to the Earth's orbital motion and seasons. A "Gregorian-only" calendar mode is
available if such physical events are the primary interest.
 
REFERENCE FRAME AND COORDINATES
 
  Ecliptic at the standard reference epoch
 
    Reference epoch: J2000.0
    X-Y plane: adopted Earth orbital plane at the reference epoch
               Note: IAU76 obliquity of 84381.448 arcseconds wrt ICRF X-Y plane
    X-axis   : ICRF
    Z-axis   : perpendicular to the X-Y plane in the directional (+ or -) sense
               of Earth's north pole at the reference epoch.
 
  Symbol meaning:
 
    JDTDB    Julian Day Number, Barycentric Dynamical Time
      X      X-component of position vector (km)
      Y      Y-component of position vector (km)
      Z      Z-component of position vector (km)
      VX     X-component of velocity vector (km/sec)                           
      VY     Y-component of velocity vector (km/sec)                           
      VZ     Z-component of velocity vector (km/sec)                           
      LT     One-way down-leg Newtonian light-time (sec)
      RG     Range; distance from coordinate center (km)
      RR     Range-rate; radial velocity wrt coord. center (km/sec)
 
ABERRATIONS AND CORRECTIONS

and came up with: "python nodemath.py Longitude of Ascending Node (Ω): 4.156300512180232" .. now I am not quite sure its correct or I got it right. This is not matching with the current NN coordinates so the code is off

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  • 1
    $\begingroup$ Would need to see where you got the code to make judgments on how it's intended to work, and if h_x and h_y are the x- and y- components of the specific relative angular momentum vector, it looks like the calculation to get its magnitude is wrong, unless the z- component of said vector is zero. $\endgroup$
    – notovny
    Sep 29, 2023 at 15:49
  • 1
    $\begingroup$ As notovny said, that code is a bit weird. The specific angular momentum vector, $\mathbf{ h=r\times v}$ is normal to the orbit plane. And if your XY plane is the ecliptic, then the z component of the normal to the Moon's orbit plane isn't zero. $\endgroup$
    – PM 2Ring
    Sep 29, 2023 at 16:26
  • 1
    $\begingroup$ FWIW, if the h vector is (a, b, c), the orbit plane intersects the XY plane in the line $ax+by=0$, which is the line of nodes. Which means $\tan(\Omega)$ is $(-a/b)$ or $(a/-b)$. $\endgroup$
    – PM 2Ring
    Sep 29, 2023 at 16:34
  • 2
    $\begingroup$ Ah, that's the issue... Looking at Wikipedia's Longitude of the Ascending Node article, the code has misnamed and incorrectly described a variable. h_magnitude should be called n_magnitude, because it's the magnitude of the vector $\textbf{n}$ (I don't know if it has a customary name, I usually call it the node vector), which points from the central body towards the Ascending Node. Also, in the code as above, as in the wikipedia article, $\textbf{n}$ is not a unit vector. $\endgroup$
    – notovny
    Sep 29, 2023 at 18:09
  • 1
    $\begingroup$ lets see if it allows me to post a link pastebin.com/7rwzgNLD $\endgroup$
    – dimitri33
    Sep 29, 2023 at 19:21

1 Answer 1

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It looks like you're trying to find the Moon's ascending node from position and velocity vectors as in this Wikipedia article. h = r × v is perpendicular to the Moon's orbital plane, and its projection onto the ecliptic plane (ignoring hz) is 90° behind the ascending node.

These lines of your HORIZONS output show a coordinate center in southern New Mexico, possibly from looking up 'earth' instead of '@earth'.

Center-site name: Heaven on Earth Observatory, Mayhill
⋮
Center geodetic : 254.471, 32.9035384, 2.23607    {E-lon(deg),Lat(deg),Alt(km)}

This puts r off by 6000 km, v off by 0.4 km/s, and the computed longitude off by several degrees. With coordinate center Geocentric [code: 500], HORIZONS gives this output:

2460215.500000000 = A.D. 2023-Sep-28 00:00:00.0000 TDB 
 X = 3.461836628403760E+05 Y =-9.613409075264385E+04 Z =-2.126911943880732E+04
 VX= 2.954176491446214E-01 VY= 1.050043302428879E+00 VZ= 7.630639995108085E-02

Your cross product implementation looks correct, but you don't need the magnitude just to compute an angle. I recommend numpy for vector math.

import math
import numpy

# HORIZONS geocentric state vectors for the Moon at 2023-09-28 0:00 TDB
r = numpy.array([3.461837e+5, -9.613409e+4, -2.126912e+4])
v = numpy.array([2.954176e-1, 1.050043, 7.630640e-2])
h = numpy.cross(r, v)

# J2000 longitude of ascending node
omega = math.degrees(math.atan2(h[1], h[0])) + 90
if omega < 0:
    omega += 360

print('omega = {0:.2f}'.format(omega))

gives this output:

omega = 24.64

which agrees with OM in HORIZONS's osculating orbital elements:

2460215.500000000 = A.D. 2023-Sep-28 00:00:00.0000 TDB 
 EC= 6.651987996774227E-02 QR= 3.599111933878179E+05 IN= 5.244703685174947E+00
 OM= 2.463901296089877E+01 W = 3.204209825950677E+02 Tp=  2460215.546430446208
 N = 1.520234985695220E-04 MA= 3.593901439672831E+02 TA= 3.593016826209310E+02

As PM 2Ring commented, that's relative to the J2000 equinox. For 2023-09-28, add 0.33° for precession, making Ω = 24.97° relative to the equinox of date.

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