ORBTEST.txt


Test Case 1: Creating an empty KO object and loading the data.
Position ko1: -20600504.579, -5085526.7283, 15744265.516, 
Test Case 2: Creating KO object with data.
Position ko2: (-20600504.579, -5085526.7283, 15744265.516)
Velocity ko2: (-1216.0801672, -1697.1735683, -2052.5095001)
Test Case 3: Creating KO object with raw legacy nav message data.
Position ko3: (-20600504.542, -5085526.629, 15744265.515)
Velocity ko3: (-1216.0801725, -1697.173575, -2052.5094957)
Test Case 4: Creating KO object with raw legacy nav message data.
Position ko4: (-20600504.542, -5085526.629, 15744265.515)
Velocity ko4: (-1216.0801725, -1697.173575, -2052.5094957)
RelCorr ko4: -3.0398069803e-08
Test Case 5: Creating KO object with data from RINEX file.
Position ko5: (-20600504.542, -5085526.6291, 15744265.515)
Velocity ko5: (-1216.0801725, -1697.173575, -2052.5094957)
Test Case 6: Calculated position using 'classic' EngEphemeris.
Position EE: (-21049506.346, -6909958.4549, 14455463.08)
Velocity EE: (-1090.4179237, -1584.5085344, -2247.7563296)
RelCorr EE:  -3.1324366045e-08
EE dump: 
****************************************************************************
Broadcast Ephemeris (Engineering Units)

PRN :  0

              Week(10bt)     SOW     DOW   UTD     SOD   MM/DD/YYYY   HH:MM:SS
Clock Epoch:  1638(     )  388800   Thu-4   153   43200  06/02/2011   12:00:00
Eph Epoch:    1638(     )     512   Sun-0   149     512  05/29/2011   00:08:32
Transmit Week:1638
Fit interval flag :  1

          SUBFRAME OVERHEAD

               SOW    DOW:HH:MM:SS     IOD    ALERT   A-S
SF1 HOW:    381606  Thu-4:10:00:06   0x016      0      on
SF2 HOW:    381612  Thu-4:10:00:12    0x16      0      on
SF3 HOW:    381618  Thu-4:10:00:18    0x16      0      on

           CLOCK

Bias T0:       0.00000000E+00 sec
Drift:         5.11590770E-12 sec/sec
Drift rate:    0.00000000E+00 sec/(sec**2)
Group delay:                0 sec

           ORBIT PARAMETERS

Semi-major axis:         5.15365528E+03 m**.5
Motion correction:       5.39093884E-09 rad/sec
Eccentricity:            1.42575260E-02
Arg of perigee:          1.09154605E+00 rad
Mean anomaly at epoch:   1.05539163E+00 rad
Right ascension:        -2.16947563E+00 rad     -8.56285668E-09 rad/sec
Inclination:             9.28692498E-01 rad      0.00000000E+00 rad/sec

           HARMONIC CORRECTIONS

Radial        Sine:   1.87812500E+01 m    Cosine:   2.03562500E+02 m
Inclination   Sine:   5.02914190E-08 rad  Cosine:  -2.30967999E-07 rad
In-track      Sine:   8.35768878E-06 rad  Cosine:   9.57399607E-07 rad

           SV STATUS

Health bits:   0x00      URA index:    0
Code on L2:    P only      L2 P Nav data:          on


ko4 dump: 
****************************************************************************
Broadcast Ephemeris (Engineering Units)

PRN :  3

              Week(10bt)     SOW     DOW   UTD     SOD   MM/DD/YYYY   HH:MM:SS

Eph Epoch:    1638(     )  388800   Thu-4   153   43200  06/02/2011   12:00:00

           ORBIT PARAMETERS

Semi-major axis:         5.15365528E+03 m**.5
Motion correction:       5.39093884E-09 rad/sec
Eccentricity:            1.42575260E-02
Arg of perigee:          1.09154605E+00 rad
Mean anomaly at epoch:   1.05539163E+00 rad
Right ascension:        -2.16947563E+00 rad     -8.56285668E-09 rad/sec
Inclination:             9.28692498E-01 rad      5.52880173E-10 rad/sec

           HARMONIC CORRECTIONS

Radial        Sine:   1.87812500E+01 m    Cosine:   2.03562500E+02 m
Inclination   Sine:   5.02914190E-08 rad  Cosine:  -2.30967999E-07 rad
In-track      Sine:   8.35768878E-06 rad  Cosine:   9.57399607E-07 rad


