EPHEMERIS FOR SATELLITE 2 :
PRN number for data .................. 2
Issue of ephemeris data .............. 224
Semi-Major Axis (meters) ............. 2.65603E+07
C(ic) (rad) .......................... 1.88127E-07
C(is) (rad) .......................... -1.00583E-07
C(rc) (meters) ....................... 321.656
C(rs) (meters) ....................... 87.6875
C(uc) (rad) .......................... 4.36418E-06
C(us) (rad) .......................... 2.70829E-06
Mean motion difference (rad/sec) ..... 5.04521E-09
Eccentricity (dimensionless) ......... 0.0139305
Rate of inclination angle (rad/sec) .. 4.11089E-10
Inclination angle @ ref. time (rad) .. 0.950462
Mean Anomaly at reference time (rad) . -2.62555
Corrected Mean Motion (rad/sec) ...... 0.000145859
Computed Mean Motion (rad/sec) ....... 0.000145854
Argument of perigee (rad) ............ -2.56865
Rate of right ascension (rad/sec) .... -8.43857E-09
Right ascension @ ref time (rad) ..... 1.75048
Sqrt (1 - e^2) ....................... 0.999903
Sqr root semi-major axis, (m^1/2) .... 5153.67
Reference time ephemeris (sec) ....... 240704
CLOCK FOR SATELLITE 2 :
PRN number for data ......... 2
Week number...... ........... 797
Predicted user range accuracy 32
Health of satellite ......... 0
L1 - L2 Correction term ..... 9.31323E-10
Issue of clock data ......... 224
Time of clock data .......... 240704
Clock offset ................ -0.000158074
Clock drift ................. -2.50111E-12
Rate of clock drift ......... 0
EPHEMERIS FOR SATELLITE 4 :
PRN number for data .................. 4
Issue of ephemeris data .............. 157
Semi-Major Axis (meters) ............. 2.65616E+07
C(ic) (rad) .......................... 3.72529E-08
C(is) (rad) .......................... -5.96046E-08
C(rc) (meters) ....................... 175.406
C(rs) (meters) ....................... -60.2188
C(uc) (rad) .......................... -3.33972E-06
C(us) (rad) .......................... 1.06301E-05
Mean motion difference (rad/sec) ..... 4.1616E-09
Eccentricity (dimensionless) ......... 0.00354898
Rate of inclination angle (rad/sec) .. 7.64318E-11
Inclination angle @ ref. time (rad) .. 0.96687
Mean Anomaly at reference time (rad) . 1.41596
Corrected Mean Motion (rad/sec) ...... 0.000145848
Computed Mean Motion (rad/sec) ....... 0.000145844
Argument of perigee (rad) ............ -1.14906
Rate of right ascension (rad/sec) .... -7.79854E-09
Right ascension @ ref time (rad) ..... -2.39929
Sqrt (1 - e^2) ....................... 0.999994
Sqr root semi-major axis, (m^1/2) .... 5153.79
Reference time ephemeris (sec) ....... 252000
CLOCK FOR SATELLITE 4 :
PRN number for data ......... 4
Week number...... ........... 797
Predicted user range accuracy 32
Health of satellite ......... 0
L1 - L2 Correction term ..... 1.39698E-09
Issue of clock data ......... 669
Time of clock data .......... 252000
Clock offset ................ 2.19094E-05
Clock drift ................. 1.81899E-12
Rate of clock drift ......... 0
EPHEMERIS FOR SATELLITE 7 :
PRN number for data .................. 7
Issue of ephemeris data .............. 5
Semi-Major Axis (meters) ............. 2.656E+07
C(ic) (rad) .......................... 1.91852E-07
C(is) (rad) .......................... -1.08033E-07
C(rc) (meters) ....................... 300.719
C(rs) (meters) ....................... -94.0938
C(uc) (rad) .......................... -4.81494E-06
C(us) (rad) .......................... 4.06802E-06
Mean motion difference (rad/sec) ..... 4.6902E-09
Eccentricity (dimensionless) ......... 0.00693839
Rate of inclination angle (rad/sec) .. -1.53578E-10
Inclination angle @ ref. time (rad) .. 0.964094
Mean Anomaly at reference time (rad) . -2.73317
Corrected Mean Motion (rad/sec) ...... 0.000145862
Computed Mean Motion (rad/sec) ....... 0.000145857
Argument of perigee (rad) ............ -2.56914
Rate of right ascension (rad/sec) .... -8.3357E-09
Right ascension @ ref time (rad) ..... 2.81765
Sqrt (1 - e^2) ....................... 0.999976
Sqr root semi-major axis, (m^1/2) .... 5153.63
Reference time ephemeris (sec) ....... 247904
CLOCK FOR SATELLITE 7 :
PRN number for data ......... 7
Week number...... ........... 797
Predicted user range accuracy 32
Health of satellite ......... 0
L1 - L2 Correction term ..... 1.39698E-09
Issue of clock data ......... 5
Time of clock data .......... 247904
Clock offset ................ 0.000703468
Clock drift ................. 2.27374E-13
Rate of clock drift ......... 0
EPHEMERIS FOR SATELLITE 12 :
PRN number for data .................. 12
Issue of ephemeris data .............. 52
Semi-Major Axis (meters) ............. 2.65577E+07
C(ic) (rad) .......................... -2.10479E-07
C(is) (rad) .......................... 9.12696E-08
C(rc) (meters) ....................... 246.875
C(rs) (meters) ....................... 112.5
C(uc) (rad) .......................... 5.89341E-06
C(us) (rad) .......................... 9.87016E-06
Mean motion difference (rad/sec) ..... 1.56721E-09
Eccentricity (dimensionless) ......... 0.0154782
Rate of inclination angle (rad/sec) .. 2.91441E-10
Inclination angle @ ref. time (rad) .. 1.08541
Mean Anomaly at reference time (rad) . 2.79641
Corrected Mean Motion (rad/sec) ...... 0.000145878
Computed Mean Motion (rad/sec) ....... 0.000145876
Argument of perigee (rad) ............ -0.0994882
Rate of right ascension (rad/sec) .... -6.41491E-09
Right ascension @ ref time (rad) ..... 1.12752
Sqrt (1 - e^2) ....................... 0.99988
Sqr root semi-major axis, (m^1/2) .... 5153.41
Reference time ephemeris (sec) ....... 255600
CLOCK FOR SATELLITE 12 :
PRN number for data ......... 12
Week number...... ........... 797
Predicted user range accuracy 2.8
Health of satellite ......... 0
L1 - L2 Correction term ..... 2.79397E-09
Issue of clock data ......... 52
Time of clock data .......... 255600
Clock offset ................ -0.000519538
Clock drift ................. -3.5584E-11
Rate of clock drift ......... 0
EPHEMERIS FOR SATELLITE 15 :
PRN number for data .................. 15
Issue of ephemeris data .............. 16
Semi-Major Axis (meters) ............. 2.65598E+07
C(ic) (rad) .......................... -8.00937E-08
C(is) (rad) .......................... 1.86265E-09
C(rc) (meters) ....................... 171.938
C(rs) (meters) ....................... -56.0312
C(uc) (rad) .......................... -2.87965E-06
C(us) (rad) .......................... 1.09263E-05
Mean motion difference (rad/sec) ..... 4.1266E-09
Eccentricity (dimensionless) ......... 0.00671411
Rate of inclination angle (rad/sec) .. 1.63578E-10
Inclination angle @ ref. time (rad) .. 0.971519
Mean Anomaly at reference time (rad) . -0.820821
Corrected Mean Motion (rad/sec) ...... 0.000145862
Computed Mean Motion (rad/sec) ....... 0.000145858
Argument of perigee (rad) ............ 1.74644
Rate of right ascension (rad/sec) .... -7.9014E-09
Right ascension @ ref time (rad) ..... -2.3653
Sqrt (1 - e^2) ....................... 0.999977
Sqr root semi-major axis, (m^1/2) .... 5153.62
Reference time ephemeris (sec) ....... 244800
CLOCK FOR SATELLITE 15 :
PRN number for data ......... 15
Week number...... ........... 797
Predicted user range accuracy 4
Health of satellite ......... 0
L1 - L2 Correction term ..... 2.79397E-09
Issue of clock data ......... 16
Time of clock data .......... 244800
Clock offset ................ 0.000178255
Clock drift ................. 3.41061E-12
Rate of clock drift ......... 0
EPHEMERIS FOR SATELLITE 24 :
PRN number for data .................. 24
Issue of ephemeris data .............. 179
Semi-Major Axis (meters) ............. 2.65599E+07
C(ic) (rad) .......................... -1.02445E-07
C(is) (rad) .......................... -1.22935E-07
C(rc) (meters) ....................... 168.656
C(rs) (meters) ....................... -63.3125
C(uc) (rad) .......................... -3.48687E-06
C(us) (rad) .......................... 1.1526E-05
Mean motion difference (rad/sec) ..... 3.94802E-09
Eccentricity (dimensionless) ......... 0.00623617
Rate of inclination angle (rad/sec) .. 1.05004E-10
Inclination angle @ ref. time (rad) .. 0.976756
Mean Anomaly at reference time (rad) . 1.79689
Corrected Mean Motion (rad/sec) ...... 0.000145861
Computed Mean Motion (rad/sec) ....... 0.000145858
Argument of perigee (rad) ............ -2.06498
Rate of right ascension (rad/sec) .... -7.67032E-09
Right ascension @ ref time (rad) ..... -2.4059
Sqrt (1 - e^2) ....................... 0.999981
Sqr root semi-major axis, (m^1/2) .... 5153.63
Reference time ephemeris (sec) ....... 252000
CLOCK FOR SATELLITE 24 :
PRN number for data ......... 24
Week number...... ........... 797
Predicted user range accuracy 32
Health of satellite ......... 0
L1 - L2 Correction term ..... 6.0536E-09
Issue of clock data ......... 435
Time of clock data .......... 252000
Clock offset ................ 0.000693584
Clock drift ................. 3.50155E-11
Rate of clock drift ......... 0
EPHEMERIS FOR SATELLITE 27 :
PRN number for data .................. 27
Issue of ephemeris data .............. 158
Semi-Major Axis (meters) ............. 2.65602E+07
C(ic) (rad) .......................... 2.66358E-07
C(is) (rad) .......................... 1.73226E-07
C(rc) (meters) ....................... 160.781
C(rs) (meters) ....................... 63.2188
C(uc) (rad) .......................... 3.40119E-06
C(us) (rad) .......................... 1.08313E-05
Mean motion difference (rad/sec) ..... 4.54662E-09
Eccentricity (dimensionless) ......... 0.0112431
Rate of inclination angle (rad/sec) .. -7.39317E-11
Inclination angle @ ref. time (rad) .. 0.945988
Mean Anomaly at reference time (rad) . 1.27438
Corrected Mean Motion (rad/sec) ...... 0.00014586
Computed Mean Motion (rad/sec) ....... 0.000145855
Argument of perigee (rad) ............ 2.57836
Rate of right ascension (rad/sec) .... -7.94747E-09
Right ascension @ ref time (rad) ..... 0.720816
Sqrt (1 - e^2) ....................... 0.999937
Sqr root semi-major axis, (m^1/2) .... 5153.66
Reference time ephemeris (sec) ....... 252000
CLOCK FOR SATELLITE 27 :
PRN number for data ......... 27
Week number...... ........... 797
Predicted user range accuracy 32
Health of satellite ......... 0
L1 - L2 Correction term ..... 1.39698E-09
Issue of clock data ......... 157
Time of clock data .......... 240704
Clock offset ................ 2.7555E-05
Clock drift ................. 1.25056E-12
Rate of clock drift ......... 0