M = E - e·sin E
Name | Description | |
---|---|---|
A | Main program, initialise registers | |
0 | Newton’s algorithm |
Name | Description | |
---|---|---|
.0 | Anomaly M (in degrees) | |
.1 | Initial orbit eccentricity e | |
.2 | Updated orbit eccentricity e | |
.3 | Control variable |
Line | Display | Key Sequence | Line | Display | Key Sequence | ||
---|---|---|---|---|---|---|---|
000 | 019 | 45 .2 | RCL . 2 | ||||
001 | 42,21,11 | f LBL A | 020 | 23 | SIN | ||
002 | 44 .0 | STO . 0 | 021 | 45 .0 | RCL . 0 | ||
003 | 34 | x↔y | 022 | 20 | × | ||
004 | 42 3 | f → RAD | 023 | 40 | + | ||
005 | 44 .1 | STO . 1 | 024 | 45 .2 | RCL . 2 | ||
006 | 44 .2 | STO . 2 | 025 | 24 | COS | ||
007 | 43 8 | g RAD | 026 | 45 .0 | RCL . 0 | ||
008 | 1 | 1 | 027 | 20 | × | ||
009 | 48 | . | 028 | 1 | 1 | ||
010 | 0 | 0 | 029 | 30 | − | ||
011 | 1 | 1 | 030 | 10 | ÷ | ||
012 | 4 | 4 | 031 | 30 | − | ||
013 | 44 .3 | STO . 3 | 032 | 44 .2 | STO . 2 | ||
014 | 45 .2 | RCL . 2 | 033 | 42, 6, .3 | f ISG . 3 | ||
015 | 42,21, 0 | f LBL 0 | 034 | 22 0 | GTO 0 | ||
016 | 45 .1 | RCL . 1 | 035 | 43 3 | g →DEG | ||
017 | 45 .2 | RCL . 2 | 036 | 43 7 | g DEG | ||
018 | 30 | − | 037 | 43 32 | g RTN |