[IGSREPORT-19037] Wk 1602 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Oct 7 02:59:27 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1602 (Sep 19, 2010 - Sep 25, 2010)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
absolute deviation to the unweighted average orbit after removing small
differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1602.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed to
the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl1602[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1602 in the SP3 format.
igl16027.sum Combination Report for GPS Week 1602.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 380.2 ns
1 | 458.4 ns
2 | 455.7 ns
3 | 456.8 ns
4 | 456.5 ns
5 | 397.7 ns
6 | 396.1 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1602, 1a.1602).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.1602.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.1602.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 1602 summary. (Sep 19, 2010 - Sep 25, 2010)
Table 1.1602.a GPS week : 1602 MJD: 55458.0-55464.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 1 -7 -7 -9 81 -.17 20 20 | 0 -35 1780 1861
| 1 1 4 30 22 77 .05 | 0 210
cod 229| -1 -1 -2 24 -20 33 -.14 17 16 | --- --- --- ---
| 1 1 5 18 11 67 .03 | --- ---
esx 131| 0 0 -3 3 24 55 .44 22 20 | 85893 2429 3815 7842
| 1 1 4 24 28 93 .06 | 35040 2187
gfz 193| 2 2 -3 -65 -25 27 -.13 28 29 | 245919 1883 3798 7677
| 1 1 6 59 66 90 .06 | 34079 1937
iac n/a| 4 2 61 -46 2 -518 -.31 49 49 | 428950 -656 3822 8112
| 4 5 69 26 18 528 .08 | 35480 892
mcc n/a| -2 5 13 -127 12 -133 -.51 112 112 | --- --- --- ---
| 7 10 29 91 91 305 .28 | --- ---
Table 1.1602.b GPS week : 1602 MJD: 55458.0-55464.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 12 21 18 17 13 16 12 |
R02 | 12 14 16 16 10 8 8 |
R04 | 12 12 16 13 14 9 12 |
R05 | 13 14 13 16 12 14 8 |
R07 | 11 15 15 11 10 13 12 |
R08 | 15 12 15 14 12 12 9 |
R10 | 14 15 17 17 13 16 12 |
R11 | 23 19 18 21 18 14 18 |
R13 | 13 18 11 11 12 14 13 |
R14 | 16 16 13 16 16 15 13 |
R15 | 15 13 18 13 11 13 9 |
R17 | 17 19 14 16 12 9 10 |
R18 | 15 14 13 17 10 10 12 |
R19 | 12 14 14 13 10 11 13 |
R20 | 13 15 18 16 15 21 12 |
R21 | 12 15 16 14 10 8 25 |
R22 | 10 14 15 15 13 11 11 |
R23 | 12 15 14 14 17 12 9 |
R24 | 11 21 16 16 11 10 8 |
Table 1.1602.c GPS week : 1602 MJD: 55458.0-55464.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1602 0 | 76 -10 245 -1084 -1103 -12270 86.5 2699 2699 | 380197 0
brd 1602 1 | 44 -35 135 -39 764 -11350 86.5 2416 2416 | 458361 0
brd 1602 2 | -62 48 23 -1469 1578 -10370 86.5 1877 1877 | 455746 0
brd 1602 3 | 29 -29 -104 935 1114 -6326 85.7 1874 1874 | 456787 0
brd 1602 4 | 91 -28 4 358 -138 -9471 87.9 1794 1794 | 456454 0
brd 1602 5 | -33 3 28 445 -717 -15670 87.2 1734 1734 | 397696 0
brd 1602 6 | -26 9 56 -882 -1640 -17300 87.1 1949 1949 | 396089 0
-------------+------------------------------------------------------------+----------------
brd 1602 mean| 16 -6 55 -248 -20 -11822 86.8 2049 2049 | 428761 0
brd 1602 sdev| 58 29 109 902 1207 3721 .7 363 363 | 35467 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.1602.0 GPS week: 1602 Day: 0 MJD: 55458
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| 1 -1 -8 -38 -6 194 -.22 20 19 | 0 -457 2108 2227
cod 229| -2 0 -3 22 -42 130 -.12 18 15 | --- --- --- ---
esx 131| 0 1 -6 30 36 179 .37 21 20 | 31110 291 3583 6966
gfz 193| 0 2 -4 -74 -111 115 -.14 28 26 | 201940 71 3578 6797
iac n/a| 1 -3 50 -62 14 -1310 -.24 43 43 | 379857 365 3589 7233
mcc n/a| -15 -3 24 -219 -131 120 -.56 121 121 | --- --- --- ---
Table 2.1602.1 GPS week: 1602 Day: 1 MJD: 55459
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 0 -12 -11 -8 8 -.20 20 20 | 0 96 1633 1695
cod 229| -4 -3 -7 19 -10 115 -.14 17 18 | --- --- --- ---
esx 131| 0 0 -1 29 1 191 .48 25 22 | 113522 2091 3918 7583
gfz 193| 1 2 -7 -85 -67 184 -.14 29 45 | 275703 -107 3894 7765
iac n/a| 9 1 94 -15 0 -1059 -.33 66 66 | 458928 -1928 3922 8082
mcc n/a| 1 16 31 -187 46 -69 -.52 99 99 | --- --- --- ---
Table 2.1602.2 GPS week: 1602 Day: 2 MJD: 55460
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 3 -11 -40 18 158 -.21 19 19 | 0 75 1655 1716
cod 229| 0 -2 -6 30 -14 -41 -.17 16 14 | --- --- --- ---
esx 131| -1 -4 -9 6 8 -36 .38 20 20 | 115700 1049 3763 9294
gfz 193| 3 0 -12 -155 27 -16 -.10 28 26 | 271615 1300 3750 8874
iac n/a| 7 12 139 -35 -12 -507 -.38 78 78 | 457088 -1652 3721 8834
mcc n/a| 4 -2 35 -136 8 -644 -.64 81 81 | --- --- --- ---
Table 2.1602.3 GPS week: 1602 Day: 3 MJD: 55461
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 2 -11 4 15 61 -.13 16 16 | 0 91 1702 1750
cod 229| 0 -1 -8 -11 -18 36 -.16 18 17 | --- --- --- ---
esx 131| -2 -1 -8 -3 -19 49 .42 20 19 | 112889 3131 3659 7895
gfz 193| 1 5 -9 -50 90 23 -.09 28 24 | 272970 1807 3648 7612
iac n/a| 10 6 157 -27 24 -682 -.45 80 80 | 457054 -525 3728 8512
mcc n/a| -3 -3 39 -53 81 -16 .02 72 72 | --- --- --- ---
Table 2.1602.4 GPS week: 1602 Day: 4 MJD: 55462
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 2 -2 50 -15 -5 -.22 22 21 | 0 -164 1991 2087
cod 229| -1 -1 5 28 -14 -7 -.17 19 18 | --- --- --- ---
esx 131| -1 -1 -1 -43 50 -6 .50 19 18 | 109331 6318 3779 8206
gfz 193| 1 3 4 25 -25 -62 -.25 27 32 | 271885 5098 3778 7702
iac n/a| 0 0 1 -30 -3 3 -.31 28 28 | 454892 366 3783 8289
mcc n/a| 1 5 19 39 124 238 -.44 68 68 | --- --- --- ---
Table 2.1602.5 GPS week: 1602 Day: 5 MJD: 55463
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| 0 1 -7 -13 -34 32 -.09 23 23 | 0 123 1705 1783
cod 229| -2 0 1 33 -28 22 -.12 15 16 | --- --- --- ---
esx 131| 1 0 1 0 52 28 .41 24 21 | 55669 3828 3753 7862
gfz 193| 3 1 1 -105 -54 -4 -.08 28 23 | 213485 3889 3761 8028
iac n/a| 2 0 -1 -89 20 -46 -.25 26 26 | 398185 -440 3753 8243
mcc n/a| 2 5 -11 -194 48 -150 -.89 91 91 | --- --- --- ---
Table 2.1602.6 GPS week: 1602 Day: 6 MJD: 55464
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
bkg 131| -1 0 -1 -2 -39 121 -.12 22 21 | 0 -10 1671 1772
cod 229| 0 0 3 49 -14 -25 -.10 16 15 | --- --- --- ---
esx 131| 0 0 3 2 45 -17 .54 25 19 | 63035 297 4250 7093
gfz 193| 4 3 4 -12 -38 -46 -.10 28 25 | 213841 1129 4183 6967
iac n/a| 0 2 -10 -63 -26 -31 -.24 22 22 | 396652 -780 4259 7594
mcc n/a| -9 22 -41 -142 -87 -412 -.58 256 256 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.1602.0 GPS week: 1602 Day: 0 MJD: 55458
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1224 13 19 17 15 41 --- 12 | 49 56 51 44 61 --- 48
R02 | 3494 15 17 23 27 32 --- 12 | 50 58 46 51 84 --- 51
R04 | 2339 19 18 17 22 34 --- 12 | 32 53 47 52 72 --- 43
R05 | 3901 17 11 22 32 44 --- 12 | 39 50 45 47 66 --- 42
R07 | 3143 17 16 18 20 31 --- 11 | 33 52 49 49 60 --- 43
R08 | 2494 19 30 19 20 38 114 15 | 28 44 42 40 67 45 35
R10 | 1347 20 12 26 24 42 --- 13 | 37 48 68 61 45 --- 48
R11 | 1145 38 26 42 45 58 --- 22 | 52 74 79 82 99 --- 65
R13 | 1254 26 13 17 25 41 --- 13 | 33 37 37 40 47 --- 33
R14 | 1460 21 23 22 15 52 --- 15 | 34 42 31 37 43 --- 30
R15 | 7707 27 19 20 51 42 137 14 | 54 49 57 76 43 28 51
R17 | 2630 24 18 23 22 59 --- 16 | 38 50 68 60 64 --- 51
R18 | 2502 24 24 17 16 43 --- 14 | 21 36 25 32 26 --- 21
R19 | 1008 15 8 21 28 44 --- 12 | 27 26 21 32 33 --- 22
R20 | 1829 12 20 19 28 47 --- 13 | 26 32 32 26 41 --- 24
R21 | 1092 12 12 19 37 42 --- 11 | 20 28 39 38 35 --- 27
R22 | 916 12 11 15 25 34 --- 9 | 13 16 28 21 32 --- 17
R23 | 826 23 15 12 28 38 110 12 | 18 25 33 30 32 43 21
R24 | 1184 16 11 20 16 37 --- 11 | 21 20 40 28 28 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 2699 20 18 21 28 43 121 |T 32 41 44 44 51 38 36
WRMS | 2699 19 15 20 26 43 121 |NE 32 41 44 44 51 38 36
MEDI | 1460 19 17 19 25 42 114 |MD 33 44 42 40 45 43 35
Table 3.1602.1 GPS week: 1602 Day: 1 MJD: 55459
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1903 17 15 32 17 108 --- 20 | 37 46 72 42 24 --- 44
R02 | 3195 18 25 19 23 50 --- 14 | 40 55 44 51 76 --- 45
R04 | 2905 20 13 19 18 46 --- 12 | 42 42 43 47 95 --- 42
R05 | 2201 19 23 14 25 59 --- 14 | 15 40 32 47 48 --- 26
R07 | 2136 15 22 29 34 48 --- 14 | 22 37 25 27 36 --- 23
R08 | 1390 12 14 13 21 57 115 11 | 43 28 42 33 57 35 35
R10 | 776 20 14 19 26 73 --- 15 | 37 35 40 38 44 --- 35
R11 | 1146 28 23 34 20 59 --- 18 | 61 54 65 48 57 --- 52
R13 | 1524 32 15 38 63 46 --- 18 | 37 30 44 58 28 --- 28
R14 | 2331 20 27 19 40 58 --- 15 | 34 36 37 46 41 --- 31
R15 | 6882 15 14 11 30 69 100 13 | 71 63 56 59 66 27 62
R17 | 1650 25 18 21 30 91 --- 18 | 39 43 51 38 83 --- 43
R18 | 3042 20 8 16 19 70 --- 14 | 33 30 40 42 46 --- 32
R19 | 1366 11 17 15 25 69 --- 13 | 12 29 18 24 27 --- 15
R20 | 1851 19 10 24 25 70 --- 15 | 17 28 52 45 38 --- 28
R21 | 1078 13 15 23 19 70 --- 14 | 20 27 19 26 27 --- 17
R22 | 999 12 17 14 34 71 --- 13 | 20 34 27 31 31 --- 22
R23 | 708 23 9 32 25 53 78 15 | 17 24 49 43 31 37 24
R24 | 570 28 18 51 25 57 --- 21 | 20 29 55 28 37 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2416 20 17 25 29 66 99 |T 32 37 42 40 46 33 33
WRMS | 2416 20 18 22 45 66 99 |NE 32 37 42 40 46 33 33
MEDI | 1650 19 15 19 25 59 100 |MD 34 35 43 42 41 35 31
Table 3.1602.2 GPS week: 1602 Day: 2 MJD: 55460
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1468 24 18 28 20 80 --- 17 | 24 36 57 32 66 --- 36
R02 | 1723 21 14 24 27 76 --- 15 | 27 40 50 29 66 --- 35
R04 | 2798 22 20 27 17 62 --- 15 | 30 42 33 31 105 --- 32
R05 | 981 20 21 12 24 48 --- 12 | 34 56 49 61 102 --- 46
R07 | 1474 16 12 20 40 84 --- 15 | 37 44 47 46 66 --- 41
R08 | 970 18 15 17 22 81 119 15 | 35 42 40 34 68 53 37
R10 | 972 21 19 14 48 92 --- 16 | 37 37 38 48 60 --- 35
R11 | 956 24 18 26 31 82 --- 17 | 51 59 71 66 72 --- 58
R13 | 1454 12 13 11 18 58 --- 10 | 28 29 37 36 55 --- 28
R14 | 1801 9 20 19 22 59 --- 12 | 41 44 49 44 65 --- 43
R15 | 4704 25 15 31 22 75 50 17 | 52 29 37 32 56 30 33
R17 | 1335 19 13 20 31 71 --- 14 | 50 59 64 55 66 --- 57
R18 | 1810 11 12 15 38 76 --- 13 | 35 23 43 56 39 --- 31
R19 | 2084 15 11 15 31 79 --- 13 | 22 34 32 35 43 --- 26
R20 | 2522 24 17 20 31 94 --- 17 | 23 21 20 25 52 --- 13
R21 | 1404 18 9 24 17 87 --- 15 | 40 41 53 45 51 --- 41
R22 | 1224 18 17 15 18 84 --- 15 | 26 18 31 28 45 --- 19
R23 | 570 16 11 11 24 88 56 14 | 19 27 34 32 55 41 24
R24 | 985 24 18 15 25 83 --- 16 | 27 23 30 25 44 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 1876 19 16 20 28 78 81 |T 33 37 42 40 61 41 34
WRMS | 1876 19 14 20 26 78 81 |NE 33 37 42 40 61 41 34
MEDI | 1454 19 15 19 24 80 56 |MD 34 37 40 35 60 41 35
Table 3.1602.3 GPS week: 1602 Day: 3 MJD: 55461
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2122 14 30 19 25 78 --- 16 | 31 47 44 42 67 --- 36
R02 | 2725 7 17 10 23 102 --- 15 | 42 44 44 30 82 --- 41
R04 | 3469 10 11 18 30 80 --- 13 | 46 58 56 59 107 --- 53
R05 | 1762 16 30 27 33 63 --- 16 | 46 61 45 52 128 --- 52
R07 | 2806 15 13 16 33 45 --- 10 | 28 42 46 54 104 --- 39
R08 | 2160 22 11 23 18 57 91 13 | 47 42 55 47 73 73 43
R10 | 1641 23 20 18 27 92 --- 17 | 33 43 50 52 60 --- 37
R11 | 915 24 26 30 34 102 --- 20 | 60 64 70 69 101 --- 63
R13 | 964 12 10 14 24 64 --- 11 | 30 31 34 38 51 --- 28
R14 | 1416 21 19 22 18 73 --- 15 | 30 41 42 36 50 --- 31
R15 | 2569 11 12 17 24 73 61 12 | 71 73 74 69 51 46 69
R17 | 627 11 19 20 39 89 --- 15 | 43 42 48 38 48 --- 39
R18 | 1364 15 20 34 40 72 --- 16 | 42 38 59 47 45 --- 39
R19 | 1910 16 9 18 21 70 --- 13 | 24 29 34 37 49 --- 23
R20 | 1431 15 20 19 21 87 --- 15 | 51 28 34 29 79 --- 37
R21 | 2080 13 7 18 14 82 --- 13 | 30 27 36 26 62 --- 29
R22 | 919 13 10 12 23 93 --- 14 | 22 25 42 26 63 --- 27
R23 | 704 18 17 14 29 78 59 14 | 24 34 32 31 61 31 25
R24 | 641 14 10 20 35 99 --- 16 | 31 25 32 40 62 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1873 16 18 20 28 80 72 |T 38 41 46 43 70 50 38
WRMS | 1873 16 17 19 24 80 72 |NE 38 41 46 43 70 50 38
MEDI | 1641 15 17 18 25 78 61 |MD 33 42 44 40 62 46 37
Table 3.1602.4 GPS week: 1602 Day: 4 MJD: 55462
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2249 31 17 20 13 22 --- 13 | 33 37 40 34 46 --- 30
R02 | 2689 15 18 7 22 23 --- 9 | 30 37 32 42 40 --- 29
R04 | 2248 23 25 23 23 27 --- 14 | 30 42 53 49 47 --- 35
R05 | 2627 23 11 16 17 28 --- 11 | 42 47 49 48 53 --- 43
R07 | 2585 21 13 14 43 22 --- 10 | 35 48 54 66 45 --- 42
R08 | 2155 17 16 25 26 20 70 11 | 30 33 29 41 49 36 25
R10 | 1385 29 21 17 40 24 --- 13 | 41 40 45 43 81 --- 40
R11 | 739 38 20 22 38 43 --- 18 | 55 61 60 64 63 --- 52
R13 | 791 21 18 16 18 27 --- 11 | 47 57 59 46 79 --- 54
R14 | 1627 21 22 18 17 46 --- 15 | 39 41 45 35 66 --- 37
R15 | 2180 17 15 19 21 24 55 11 | 51 58 72 58 91 32 59
R17 | 868 21 16 21 29 24 --- 11 | 43 47 56 61 76 --- 47
R18 | 2508 15 14 18 23 20 --- 9 | 41 37 41 53 43 --- 33
R19 | 838 15 18 14 13 22 --- 10 | 33 31 33 30 60 --- 28
R20 | 1158 22 16 24 30 36 --- 14 | 24 29 48 39 76 --- 29
R21 | 1986 15 15 15 36 24 --- 10 | 44 32 58 62 59 --- 41
R22 | 998 19 17 20 24 33 --- 12 | 29 20 36 34 62 --- 23
R23 | 711 24 33 23 29 33 75 16 | 27 50 31 40 65 32 29
R24 | 710 18 15 19 19 21 --- 10 | 23 30 35 33 59 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1793 22 19 19 27 28 68 |T 36 40 46 46 61 33 36
WRMS | 1793 21 18 18 32 28 68 |NE 36 40 46 46 61 33 36
MEDI | 1627 21 17 19 23 24 70 |MD 35 40 45 43 60 32 35
Table 3.1602.5 GPS week: 1602 Day: 5 MJD: 55463
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1865 18 27 37 20 23 --- 16 | 26 33 45 28 43 --- 24
R02 | 2817 14 9 15 25 19 --- 8 | 25 33 26 25 44 --- 27
R04 | 959 19 11 19 38 16 --- 9 | 36 28 30 25 40 --- 28
R05 | 3344 25 11 17 20 42 --- 14 | 38 32 37 32 55 --- 34
R07 | 1637 17 20 32 21 12 --- 12 | 30 46 58 41 46 --- 40
R08 | 989 32 15 16 24 16 72 11 | 35 32 38 42 48 33 32
R10 | 809 31 16 37 33 24 --- 15 | 34 32 52 54 38 --- 31
R11 | 1010 24 21 13 47 37 --- 14 | 82 76 61 60 77 --- 69
R13 | 1013 29 18 24 24 23 --- 13 | 46 51 47 54 48 --- 44
R14 | 760 36 13 19 21 34 --- 14 | 25 31 27 23 32 --- 25
R15 | 4113 24 11 22 34 35 85 13 | 74 74 76 69 65 24 70
R17 | 654 18 9 12 25 20 --- 8 | 37 36 36 27 34 --- 34
R18 | 1497 17 14 13 24 25 --- 10 | 30 27 35 38 31 --- 30
R19 | 1240 17 15 15 28 24 --- 10 | 25 21 37 36 32 --- 24
R20 | 1221 28 16 60 22 34 --- 21 | 34 31 62 31 52 --- 33
R21 | 1071 20 10 10 40 14 --- 8 | 24 19 38 59 35 --- 22
R22 | 767 22 16 15 23 19 --- 10 | 18 23 34 36 33 --- 22
R23 | 664 18 18 19 21 24 110 11 | 21 45 31 33 31 21 29
R24 | 1365 23 7 15 18 21 --- 9 | 14 25 28 29 34 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1734 23 15 24 28 26 91 |T 34 36 42 39 43 26 33
WRMS | 1734 23 16 21 23 26 91 |NE 34 36 42 39 43 26 33
MEDI | 1071 22 15 17 24 23 85 |MD 30 32 37 36 40 24 30
Table 3.1602.6 GPS week: 1602 Day: 6 MJD: 55464
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 741 16 26 18 28 15 --- 11 | 35 52 53 57 48 --- 44
R02 | 2081 10 14 18 28 11 --- 8 | 39 42 40 43 44 --- 39
R04 | 1160 26 14 11 16 29 --- 12 | 32 38 38 34 43 --- 34
R05 | 2377 16 9 15 19 13 --- 7 | 47 53 46 43 46 --- 46
R07 | 2091 16 21 21 30 21 --- 11 | 43 69 57 46 46 --- 53
R08 | 1233 15 11 16 17 18 105 8 | 34 51 54 45 37 43 42
R10 | 1375 29 11 20 23 19 --- 11 | 44 39 44 36 54 --- 40
R11 | 1784 39 21 24 26 37 --- 17 | 57 75 66 74 64 --- 64
R13 | 877 23 15 27 34 23 --- 12 | 53 67 93 96 77 --- 69
R14 | 789 31 11 25 30 16 --- 12 | 33 37 36 30 45 --- 33
R15 | 4736 15 14 13 21 19 400 9 | 55 61 71 61 70 34 61
R17 | 1329 22 13 18 28 17 --- 10 | 30 44 37 38 52 --- 36
R18 | 1508 31 11 9 23 22 --- 11 | 26 27 29 39 33 --- 25
R19 | 1231 15 22 18 23 29 --- 12 | 20 21 26 25 30 --- 16
R20 | 1119 19 10 29 52 23 --- 12 | 32 32 46 64 43 --- 29
R21 | 2658 25 24 76 32 28 --- 24 | 38 28 77 39 39 --- 39
R22 | 829 15 15 20 20 24 --- 10 | 22 23 29 20 35 --- 20
R23 | 903 18 12 11 24 17 159 8 | 25 24 35 41 37 34 26
R24 | 3185 13 12 15 35 16 --- 8 | 19 20 26 31 28 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 1949 22 16 25 28 22 256 |T 36 42 47 45 45 37 38
WRMS | 1949 21 15 19 25 22 256 |NE 36 42 47 45 45 37 38
MEDI | 1329 18 14 18 26 19 159 |MD 34 39 44 41 44 34 39
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