[IGSREPORT-17768] Wk 1545 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Mon Sep 7 07:40:50 PDT 2009
******************************************************************************
IGS Electronic Report 07 Sep 07:41:18 PDT 2009 Message Number 17768
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1545 (Aug 16, 2009 - Aug 22, 2009)
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 2.1545.
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:
igl1545[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1545 in the SP3 format.
igl15457.sum Combination Report for GPS Week 1545.
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 | 166.0 ns
1 | 134.2 ns
2 | 108.9 ns
3 | 228.2 ns
4 | 223.9 ns
5 | 224.8 ns
6 | 222.2 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESX | R02
2 | BKG | R24
2 | IAC | R24
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 1.1545, 1a.1545).
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 2.1545.0-6)
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 3.1545.0-6).
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 1545 summary. (Aug 16, 2009 - Aug 22, 2009)
Table 1.1545.a GPS week : 1545 MJD: 55059.0-55065.0
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 106| 2 -1 -6 23 11 48 -.15 45 29 | 0 219 3606 4183
| 1 2 8 49 30 115 .07 | 0 876
cod 233| -2 0 -1 -3 12 41 -.13 18 13 | --- --- --- ---
| 1 1 2 15 14 38 .05 | --- ---
esx 131| 1 0 3 -10 -13 28 .48 47 27 | 88797 2541 5434 11200
| 2 3 4 64 42 60 .06 | 55029 3819
iac n/a| 1 0 7 -20 -12 -130 -.11 36 36 | 1343107 -3369 250791 294563
| 1 1 9 28 34 87 .04 | 1962272 3994
mcc n/a| -7 0 26 10 -8 1002 .08 156 156 | --- --- --- ---
| 11 12 20 50 93 410 .53 | --- ---
Table 1.1545.b GPS week : 1545 MJD: 55059.0-55065.0
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
------+------------------------------------+------------------------------------------
R02 | 14 23 24 32 22 14 9 |
R03 | 11 14 14 9 13 10 10 |
R07 | 9 10 13 13 15 13 12 |
R08 | 8 9 9 12 10 8 10 |
R10 | 13 14 16 15 12 12 13 |
R11 | 12 15 11 14 11 12 13 |
R13 | 9 11 9 9 13 14 8 |
R14 | 10 13 9 9 10 14 8 |
R15 | 13 12 12 10 14 11 10 |
R17 | 10 10 12 16 17 21 11 |
R18 | 9 9 12 8 10 10 9 |
R19 | 8 11 10 10 17 29 13 |
R20 | 14 15 14 17 33 35 17 |
R21 | 12 13 10 11 18 24 13 |
R22 | 16 9 11 13 14 24 15 |
R23 | 19 21 21 21 17 30 25 |
R24 | 38 24 25 23 13 35 30 |
Table 1.1545.c GPS week : 1545 MJD: 55059.0-55065.0
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 1545 0 | 31 72 246 -1387 2941 -9397 87.8 2712 2712 | 166011 0
brd 1545 1 |49490 ---- -1535 -210700 -283300 691800 21.0 >>>>> >>>>> | 134235 0
brd 1545 2 | -39 63 422 -87 -815 -3961 86.5 4629 4629 | 108886 0
brd 1545 3 | -3 -72 484 -1473 -430 -6824 86.6 3852 3852 | 228213 0
brd 1545 4 | -37 54 388 81 1199 -9288 89.3 3234 3234 | 223888 0
brd 1545 5 | -114 -171 539 6357 -3030 -10900 88.6 3747 3747 | 224834 0
brd 1545 6 | 0 -82 446 -636 -2361 -11460 90.5 3537 3537 | 222222 0
-------------+------------------------------------------------------------+----------------
brd 1545 mean| 7046 ---- 141 -29692 -40828 91424 78.6 >>>>> >>>>> | 186898 0
brd 1545 sdev|18715 27480 745 79862 106939 264753 25.5 >>>>> >>>>> | 50095 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 2.1545.0 GPS week: 1545 Day: 0 MJD: 55059
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 106| 1 1 -13 24 -3 158 -.09 32 21 | 0 612 2511 2924
cod 233| -4 1 -6 -24 24 18 -.08 17 12 | --- --- --- ---
esx 131| 1 0 3 -24 22 -4 .43 153 32 | 63307 3037 5243 8262
iac n/a| 1 -1 20 34 -21 -163 -.08 27 27 | 165485 -792 5266 9262
mcc n/a| -8 -4 16 -17 112 531 .02 111 111 | --- --- --- ---
Table 2.1545.1 GPS week: 1545 Day: 1 MJD: 55060
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 106| 2 0 -9 -7 49 162 -.11 28 27 | 0 188 2970 3536
cod 233| -3 0 -1 9 -8 21 -.18 15 13 | --- --- --- ---
esx 131| 2 -3 0 -1 2 -29 .42 25 23 | 31574 -234 4122 9177
iac n/a| 1 0 12 -16 5 -203 -.06 28 28 | 135019 -992 4144 9587
mcc n/a| 1 -1 67 48 -53 362 -.88 129 129 | --- --- --- ---
Table 2.1545.2 GPS week: 1545 Day: 2 MJD: 55061
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 106| 2 0 -10 -25 26 72 -.16 109 27 | 0 -1534 4065 4862
cod 233| -3 0 0 -26 15 72 -.17 15 14 | --- --- --- ---
esx 131| 5 1 1 82 -14 -10 .43 23 22 | 3901 -51 5004 8814
iac n/a| 1 0 9 -47 -37 -198 -.11 89 89 | 4181896 -8270 813494 999999
mcc n/a| -19 26 6 -72 114 1118 .84 228 228 | --- --- --- ---
Table 2.1545.3 GPS week: 1545 Day: 3 MJD: 55062
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 106| 1 -5 -5 12 4 66 -.14 30 27 | 0 211 2869 3355
cod 233| -3 1 -4 0 -3 26 -.14 15 13 | --- --- --- ---
esx 131| 2 5 2 -8 -32 55 .51 26 22 | 128644 9490 4825 9998
iac n/a| 2 -1 14 -14 -7 -125 -.15 25 25 | 4248124 -6208 913909 999999
mcc n/a| -25 -3 22 -10 -92 1014 .44 338 338 | --- --- --- ---
Table 2.1545.4 GPS week: 1545 Day: 4 MJD: 55063
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 106| 2 -3 -13 6 40 -168 -.24 40 40 | 0 1285 3874 4640
cod 233| -1 0 1 2 6 69 -.15 16 13 | --- --- --- ---
esx 131| 0 -2 10 6 -78 46 .47 26 25 | 129234 -1901 5957 11904
iac n/a| 0 2 2 -36 53 -3 -.09 31 31 | 226679 -6946 5838 11996
mcc n/a| 5 -10 34 5 -122 1358 .09 72 72 | --- --- --- ---
Table 2.1545.5 GPS week: 1545 Day: 5 MJD: 55064
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 106| 3 -1 0 129 -38 81 -.24 47 38 | 0 696 4976 5459
cod 233| -2 -1 -1 8 24 -13 -.09 28 17 | --- --- --- ---
esx 131| 0 0 9 -134 49 -2 .60 41 34 | 133443 4740 7083 17882
iac n/a| 2 0 -3 -13 -48 -12 -.16 30 30 | 220472 2840 7091 18562
mcc n/a| -3 -2 24 70 -27 1465 -.09 89 89 | --- --- --- ---
Table 2.1545.6 GPS week: 1545 Day: 6 MJD: 55065
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 106| 4 -1 10 23 -2 -29 -.06 30 21 | 0 81 3981 4510
cod 233| -1 0 0 4 29 96 -.07 17 12 | --- --- --- ---
esx 131| -3 5 -2 10 -44 146 .51 33 29 | 131480 2710 5804 12368
iac n/a| 0 -1 -6 -47 -31 -203 -.13 24 24 | 224075 -3220 5796 12539
mcc n/a| -3 -6 15 53 10 1165 .15 123 123 | --- --- --- ---
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 3.1545.0 GPS week: 1545 Day: 0 MJD: 55059
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 4418 16 14 621 26 --- 13 | 24 45 323 40 --- 34
R03 | 5065 22 14 17 20 --- 10 | 43 40 40 35 --- 36
R07 | 4022 22 10 19 15 --- 9 | 39 47 56 45 --- 45
R08 | 762 13 9 23 11 70 8 | 18 23 33 23 44 18
R10 | 3969 24 14 27 27 --- 13 | 18 20 34 20 --- 16
R11 | 2565 26 11 25 23 125 12 | 18 17 23 25 32 14
R13 | 1043 17 13 21 13 --- 9 | 18 30 33 23 --- 23
R14 | 2248 20 11 19 18 --- 9 | 12 26 28 20 --- 19
R15 | 3064 22 13 32 27 91 13 | 17 19 35 21 6 17
R17 | 1979 19 13 14 24 --- 10 | 44 52 52 63 --- 52
R18 | 1439 14 9 21 20 --- 9 | 30 28 36 33 --- 29
R19 | 1342 11 12 11 20 --- 8 | 43 44 55 55 --- 47
R20 | 1328 30 12 31 29 --- 14 | 22 31 47 31 --- 29
R21 | 1114 14 16 32 14 --- 11 | 41 39 49 42 --- 40
R22 | 2045 28 13 32 36 --- 15 | 52 61 47 53 --- 52
R23 | 1845 52 16 38 26 144 18 | 58 88 106 94 115 85
R24 | 2614 94 47 71 61 --- 38 | 580 631 642 605 --- 611
------+------------------------------------+--------------------------------
RMS | 2712 32 17 153 27 111 |T 63 73 96 72 49 68
WRMS | 2712 21 12 32 27 111 |NE 20 28 126 29 38 22
MEDI | 2045 22 13 25 23 91 |MD 30 39 47 35 32 34
Table 3.1545.1 GPS week: 1545 Day: 1 MJD: 55060
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 |>>>>> 32 32 --- 33 --- 23 | 32 75 --- 44 --- 50
R03 |>>>>> 23 16 32 23 --- 13 | 25 32 47 19 --- 26
R07 |>>>>> 16 13 25 16 --- 10 | 34 46 51 37 --- 39
R08 |>>>>> 19 9 14 17 83 8 | 17 18 22 24 84 16
R10 |69837 27 15 35 19 --- 14 | 28 35 38 26 --- 25
R11 |>>>>> 27 14 37 24 168 14 | 23 28 59 24 63 28
R13 |>>>>> 18 13 20 25 --- 10 | 12 21 19 26 --- 16
R14 | ---- 32 17 22 19 --- 13 | 22 26 28 22 --- 19
R15 |>>>>> 22 9 27 24 80 11 | 12 22 41 23 8 20
R17 |>>>>> 22 8 17 20 --- 9 | 28 39 44 54 --- 40
R18 |>>>>> 22 10 12 15 --- 8 | 29 21 29 29 --- 23
R19 |>>>>> 16 9 20 27 --- 10 | 43 47 54 60 --- 49
R20 |>>>>> 36 12 24 31 --- 14 | 22 35 33 38 --- 28
R21 |>>>>> 20 16 20 31 --- 12 | 22 30 36 42 --- 28
R22 |>>>>> 16 11 15 19 --- 8 | 33 45 39 43 --- 40
R23 |>>>>> 57 20 29 36 158 20 | 34 78 72 78 167 64
R24 |>>>>> 36 33 35 61 --- 23 | 654 668 685 690 --- 667
------+------------------------------------+--------------------------------
RMS |>>>>> 28 15 25 28 129 |T 62 74 81 75 80 69
WRMS |>>>>> 27 13 23 28 129 |NE 24 40 40 30 73 31
MEDI |>>>>> 22 13 22 24 83 |MD 28 35 39 37 63 28
Table 3.1545.2 GPS week: 1545 Day: 2 MJD: 55061
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 2712 33 29 --- 39 --- 23 | 33 65 --- 40 --- 46
R03 |16058 35 14 25 21 --- 13 | 23 36 46 27 --- 30
R07 | 5075 17 18 23 26 --- 12 | 37 54 51 38 --- 44
R08 | 1128 17 14 14 20 125 9 | 26 21 31 30 104 23
R10 | 3608 24 23 38 21 --- 16 | 25 28 33 26 --- 14
R11 | 937 18 13 22 24 71 11 | 24 34 41 27 55 26
R13 | 2197 18 10 15 17 --- 8 | 22 20 31 23 --- 21
R14 | 3726 20 8 20 15 --- 9 | 15 17 33 16 --- 15
R15 | 1437 22 15 16 31 --- 12 | 17 22 39 25 --- 20
R17 | 2213 31 12 21 20 --- 12 | 34 44 46 50 --- 42
R18 | 1357 24 16 25 20 --- 12 | 30 30 41 22 --- 26
R19 | 1234 16 13 19 19 --- 9 | 35 39 34 41 --- 35
R20 | 789 36 11 25 22 --- 13 | 23 40 53 38 --- 36
R21 | 671 16 16 15 19 --- 9 | 47 52 67 58 --- 54
R22 | 1207 19 11 17 25 --- 10 | 29 45 45 35 --- 37
R23 | 3207 58 19 26 40 367 20 | 38 80 78 91 102 71
R24 | 1465 425 18 32 346 --- 25 | 9999 9999 9999 9999 --- 9999
------+------------------------------------+--------------------------------
RMS | 4628 109 15 23 89 228 |T 28 39 44 36 87 33
WRMS | 4628 27 14 22 89 228 |NE 27 40 36 32 79 31
MEDI | 1465 22 14 21 21 125 |MD 26 36 41 30 102 30
Table 3.1545.3 GPS week: 1545 Day: 3 MJD: 55062
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 1680 24 38 --- 61 --- 31 | 30 53 --- 42 --- 34
R03 |10507 23 13 13 15 --- 9 | 27 39 36 35 --- 31
R07 | 4871 13 13 38 19 --- 12 | 53 52 67 62 --- 54
R08 | 971 16 17 28 24 81 12 | 25 25 34 21 62 17
R10 | 2844 35 22 27 18 --- 14 | 23 42 59 33 --- 35
R11 | 996 23 15 36 18 77 13 | 34 29 51 37 40 29
R13 | 1248 14 8 19 18 --- 8 | 19 26 42 18 --- 23
R14 | 3257 13 8 19 18 --- 8 | 15 19 30 25 --- 17
R15 | 2019 14 8 21 22 --- 9 | 30 27 36 26 --- 25
R17 | 1182 42 16 18 35 --- 16 | 39 47 38 54 --- 40
R18 | 1245 13 9 18 14 --- 7 | 34 45 39 43 --- 39
R19 | 1794 23 12 15 20 --- 10 | 56 58 50 55 --- 53
R20 | 1062 47 17 22 27 --- 16 | 30 49 55 63 --- 42
R21 | 980 11 14 28 19 --- 10 | 39 38 52 46 --- 38
R22 | 738 32 18 17 20 --- 12 | 34 48 42 31 --- 34
R23 | 3838 56 16 47 28 575 20 | 58 74 102 104 75 81
R24 | 7311 42 27 29 56 --- 22 | 392 393 386 409 --- 393
------+------------------------------------+--------------------------------
RMS | 3852 30 15 26 25 338 |T 55 62 69 64 59 57
WRMS | 3852 27 13 22 25 338 |NE 29 35 42 33 51 26
MEDI | 1680 23 15 21 20 81 |MD 34 45 42 42 62 35
Table 3.1545.4 GPS week: 1545 Day: 4 MJD: 55063
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 5721 43 18 --- 37 --- 21 | 34 32 --- 40 --- 27
R03M | 6134 17 10 33 30 --- 13 | 36 32 48 43 --- 33
R07M | 2849 27 16 36 22 --- 14 | 58 71 74 68 --- 66
R08 | 1168 15 12 19 21 56 9 | 25 30 33 34 39 27
R10M | 2594 34 13 19 21 --- 12 | 31 29 32 19 --- 23
R11 | 1329 20 17 22 16 85 11 | 20 29 32 25 29 23
R13M | 875 24 9 29 29 --- 13 | 25 17 34 20 --- 16
R14M | 3643 22 6 21 19 --- 9 | 33 21 46 22 --- 25
R15M | 2060 23 20 21 29 --- 13 | 26 34 51 26 --- 29
R17 | 916 45 17 23 34 --- 16 | 51 66 65 76 --- 61
R18 | 931 15 9 23 20 --- 9 | 31 27 41 39 --- 31
R19 | 1534 44 18 23 35 --- 16 | 62 70 79 91 --- 70
R20 | 691 101 28 42 66 --- 33 | 56 79 107 60 --- 65
R21 | 1134 52 14 30 37 --- 18 | 100 92 107 114 --- 97
R22 | 1041 37 16 21 26 --- 14 | 53 58 50 60 --- 51
R23 | 3254 37 25 23 38 --- 17 | 74 89 102 102 --- 89
R24 | 8711 34 12 29 21 --- 13 | 557 583 576 592 --- 577
------+------------------------------------+--------------------------------
RMS | 3233 40 16 26 31 72 |T 74 79 92 84 34 77
WRMS | 3233 40 13 25 31 72 |NE 26 30 32 33 34 25
MEDI | 1534 34 16 23 29 56 |MD 36 34 50 43 29 33
Table 3.1545.5 GPS week: 1545 Day: 5 MJD: 55064
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1773 30 18 30 23 --- 14 | 26 37 114 23 --- 20
R03 |10628 16 15 21 17 --- 10 | 21 24 29 20 --- 19
R07 | 2010 37 11 29 14 --- 13 | 56 48 53 53 --- 48
R08 | 1511 16 8 19 12 68 8 | 33 37 30 28 26 30
R10 | 2175 22 20 20 21 --- 12 | 14 33 46 25 --- 25
R11 | 1650 20 19 16 26 105 12 | 25 38 44 30 34 29
R13 | 1050 27 12 41 18 --- 14 | 26 15 36 23 --- 12
R14 | 2213 37 15 22 22 --- 13 | 25 30 35 31 --- 23
R15 | 1963 27 11 19 18 --- 10 | 13 30 34 28 --- 24
R17E | 890 62 29 34 20 --- 20 | 45 95 104 68 --- 76
R18E | 897 24 12 19 18 --- 10 | 48 39 44 45 --- 39
R19 | 1399 76 30 66 33 --- 28 | 53 113 151 81 --- 92
R20E | 1256 35 39 83 71 --- 34 | 173 222 211 227 --- 205
R21E | 1721 60 32 45 33 --- 24 | 76 123 127 89 --- 100
R22E | 1370 56 30 57 27 --- 24 | 52 85 103 63 --- 69
R23 | 3416 75 47 50 39 --- 29 | 39 94 98 86 --- 73
R24 | 8789 88 61 52 45 --- 35 | 544 495 520 527 --- 514
------+------------------------------------+--------------------------------
RMS | 3746 47 28 41 30 89 |T 74 91 104 85 30 82
WRMS | 3746 38 17 34 30 89 |NE 28 37 62 27 30 26
MEDI | 1721 35 19 30 22 68 |MD 39 39 53 45 26 39
Table 3.1545.6 GPS week: 1545 Day: 6 MJD: 55065
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2272 14 13 18 16 --- 9 | 21 21 69 16 --- 17
R03 |12314 15 12 22 22 --- 10 | 31 36 45 42 --- 36
R07 | 3251 15 14 25 26 --- 11 | 68 67 62 66 --- 64
R08 | 2030 14 13 28 16 99 10 | 29 28 39 26 55 25
R10 | 870 18 13 37 25 --- 13 | 23 20 46 28 --- 22
R11 | 1177 14 15 33 27 142 13 | 34 30 38 32 42 27
R13 | 921 15 10 16 16 --- 8 | 17 17 24 25 --- 15
R14 | 3021 14 7 23 15 --- 8 | 17 26 29 30 --- 23
R15 | 1022 24 6 25 16 --- 10 | 26 23 30 20 --- 20
R17E | 1285 20 15 21 21 --- 11 | 67 73 61 76 --- 69
R18E | 857 18 10 23 14 --- 9 | 65 56 58 62 --- 59
R19E | 923 22 17 29 20 --- 12 | 93 96 89 95 --- 93
R20E | 674 39 15 47 22 --- 17 | 362 351 362 348 --- 354
R21E | 878 28 16 29 17 --- 12 | 69 82 90 77 --- 77
R22E | 886 29 15 36 25 --- 14 | 56 76 94 68 --- 70
R23E | 3665 63 25 56 36 --- 25 | 96 141 166 137 --- 131
R24E | 3049 69 43 58 46 --- 30 | 688 712 705 690 --- 698
------+------------------------------------+--------------------------------
RMS | 3536 30 17 33 24 122 |T 103 109 118 108 48 105
WRMS | 3536 21 12 29 24 122 |NE 28 26 48 24 48 23
MEDI | 1177 18 14 28 21 99 |MD 56 56 61 62 42 59
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