[IGSREPORT-19656] Wk 1629 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Apr 14 05:05:13 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1629 (Mar 27, 2011 - Apr 02, 2011)
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
center's 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 2.1629.
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:
igl1629[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1629 in the SP3 format.
igl16297.sum Combination Report for GPS Week 1629.
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. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics initially.
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
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.
Starting 5-Nov-2006 (GPS Week 1400, day 0; MJD 54044) the absolute antenna
model was introduced (IGSMAIL #5438). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
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 | 389.6 ns
1 | 401.5 ns
2 | 385.1 ns
3 | 406.7 ns
4 | 384.3 ns
5 | 382.6 ns
6 | 402.5 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
----+--------+---------------
1 | BKG | R17
1 | GFZ | R17
2 | COD | R17
6 | BKG | R03
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 1.1629, 1a.1629).
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 2.1629.0-6)
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 3.1629.0-6).
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 1629 summary. (Mar 27, 2011 - Apr 02, 2011)
Table 1.1629.a GPS week : 1629 MJD: 55647.0-55653.0
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 149| -2 0 5 45 -3 -121 -.18 51 39 | 0 739 3127 3409
| 2 3 8 32 30 143 .10 | 0 530
cod 241| 0 1 8 96 -28 -19 -.14 26 25 | --- --- --- ---
| 1 1 3 19 40 61 .04 | --- ---
esx 131| -1 0 1 -40 0 -30 .43 20 19 | 39028 -1402 4681 9179
| 0 0 2 27 15 83 .04 | 10112 3581
gfz 190| 0 -1 0 -63 -19 105 -.14 25 23 | 241234 -781 4815 9043
| 2 2 3 18 37 254 .06 | 9930 4146
grg 130| 0 -1 10 56 56 12 -.08 50 49 | --- --- --- ---
| 3 1 8 52 45 143 .09 | --- ---
iac n/a| 2 0 -19 -6 85 26 -.20 32 32 | 393533 -379 4830 9391
| 1 1 9 18 21 69 .05 | 10039 2213
mcc n/a| 0 -2 33 48 91 665 -.10 129 129 | --- --- --- ---
| 8 3 17 92 84 147 .24 | --- ---
Table 1.1629.b GPS week : 1629 MJD: 55647.0-55653.0
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 | 10 12 14 11 12 12 11 |
R02 | 14 10 15 16 10 10 9 |
R03 | 21 20 9 9 12 16 14 |
R05 | 10 14 11 11 14 13 12 |
R06 | 12 11 13 12 13 13 19 |
R07 | 14 13 13 17 18 12 23 |
R08 | 10 11 11 10 10 11 13 |
R09 | 9 12 16 15 10 10 12 |
R10 | 13 11 11 12 10 10 13 |
R11 | 19 24 18 22 19 21 19 |
R12 | 12 15 14 12 12 11 14 |
R13 | 9 10 10 11 10 13 23 |
R15 | 16 17 12 14 15 15 13 |
R16 | 11 10 21 14 13 11 14 |
R17 | 20 69 61 22 25 22 23 |
R18 | 16 12 10 15 14 16 12 |
R19 | 15 18 12 8 17 12 10 |
R20 | 22 32 12 23 20 28 25 |
R21 | 11 12 15 10 13 15 20 |
R22 | 14 14 15 15 13 11 13 |
R23 | 18 15 13 14 11 14 11 |
R24 | 11 12 14 9 11 13 12 |
Table 1.1629.c GPS week : 1629 MJD: 55647.0-55653.0
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 1629 0 | 25 7 355 -155 -1104 -20320 87.6 1608 1608 | 389635 0
brd 1629 1 | -51 68 323 -275 1689 -19070 86.8 2205 2205 | 401475 0
brd 1629 2 | -85 -53 235 483 765 -12640 87.1 3600 3600 | 385136 0
brd 1629 3 | -144 -66 331 10 -4720 -36080 81.2 6038 6038 | 406723 0
brd 1629 4 | -251 -91 737 -4209 -1455 -25980 87.0 4342 4342 | 384317 0
brd 1629 5 | 238 59 340 -943 3436 -12920 85.8 3827 3827 | 382573 0
brd 1629 6 | -20 164 353 -1892 454 -17980 85.9 2670 2670 | 402486 0
-------------+------------------------------------------------------------+----------------
brd 1629 mean| -41 12 382 -997 -133 -20712 85.9 3469 3469 | 393192 0
brd 1629 sdev| 152 91 161 1610 2612 8166 2.2 1483 1483 | 10059 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 2.1629.0 GPS week: 1629 Day: 0 MJD: 55647
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 149| -3 -3 -3 55 44 -188 -.27 33 30 | 0 588 2818 3093
cod 241| 0 0 6 113 -49 -135 -.17 24 21 | --- --- --- ---
esx 131| -1 1 2 -86 -6 -201 .38 20 19 | 32947 2990 4342 9621
gfz 190| 0 1 -4 -55 -34 677 -.13 26 25 | 237081 3564 4832 9708
grg 130| -2 -3 22 55 32 -290 -.22 54 56 | --- --- --- ---
iac n/a| 2 0 -7 -35 95 -62 -.12 34 34 | 390761 965 4850 10319
mcc n/a| -15 -4 46 43 180 822 .27 110 110 | --- --- --- ---
Table 2.1629.1 GPS week: 1629 Day: 1 MJD: 55648
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 149| -1 2 -2 23 -6 19 -.23 39 30 | 0 52 2854 3073
cod 241| 2 1 5 87 -70 -17 -.18 26 24 | --- --- --- ---
esx 131| -2 -1 0 -19 11 40 .44 18 18 | 46614 -2309 4544 7135
gfz 190| -2 -3 1 -83 -7 -57 -.16 24 19 | 251740 -1892 4537 6974
grg 130| 3 0 18 24 31 11 -.12 50 51 | --- --- --- ---
iac n/a| 0 0 -16 -18 115 -39 -.19 33 33 | 402818 -2864 4620 8143
mcc n/a| -3 -1 34 -28 6 708 -.13 129 129 | --- --- --- ---
Table 2.1629.2 GPS week: 1629 Day: 2 MJD: 55649
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 149| 0 0 7 25 -29 -87 -.24 37 33 | 0 1487 3770 4275
cod 241| 2 0 7 119 -19 28 -.14 25 24 | --- --- --- ---
esx 131| -2 0 1 -36 5 -10 .49 22 20 | 35688 -3790 4277 9080
gfz 190| -3 -2 -3 -60 17 -4 -.12 22 24 | 236874 -4512 4746 10472
grg 130| -2 1 15 -34 59 47 .01 52 49 | --- --- --- ---
iac n/a| 4 0 -22 9 55 -13 -.25 32 32 | 385407 -2112 4728 10796
mcc n/a| 4 -3 28 -102 85 831 -.45 121 121 | --- --- --- ---
Table 2.1629.3 GPS week: 1629 Day: 3 MJD: 55650
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 149| 3 1 11 2 19 -118 -.22 35 28 | 0 1377 2840 3034
cod 241| 0 3 6 71 -24 38 -.13 26 24 | --- --- --- ---
esx 131| -2 0 -3 -52 26 -20 .47 23 22 | 57351 -3060 5248 9301
gfz 190| -1 -6 -1 -28 -69 46 -.06 26 24 | 256998 -1847 5256 9496
grg 130| -2 -3 2 61 40 77 -.14 50 47 | --- --- --- ---
iac n/a| 4 -1 -18 -15 56 80 -.26 31 31 | 406785 58 5251 9639
mcc n/a| 3 3 12 54 211 625 -.15 112 112 | --- --- --- ---
Table 2.1629.4 GPS week: 1629 Day: 4 MJD: 55651
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 149| -5 0 -1 38 -10 -93 -.17 49 38 | 0 336 2378 2597
cod 241| -1 0 6 110 34 28 -.12 27 28 | --- --- --- ---
esx 131| 0 0 0 -37 0 35 .38 19 18 | 28173 -71 4166 8091
gfz 190| 1 -1 2 -62 -53 13 -.12 23 21 | 233482 -176 4171 7818
grg 130| 4 -1 5 121 125 143 -.00 48 45 | --- --- --- ---
iac n/a| 3 -1 -13 7 85 14 -.22 33 33 | 383312 1697 4182 7560
mcc n/a| 6 -5 10 118 -5 487 -.20 127 127 | --- --- --- ---
Table 2.1629.5 GPS week: 1629 Day: 5 MJD: 55652
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 149| -4 6 4 77 -46 16 -.13 50 43 | 0 830 2968 3176
cod 241| -2 0 12 73 8 -20 -.17 31 30 | --- --- --- ---
esx 131| 0 0 1 -2 -12 -67 .43 18 16 | 31828 -6601 4516 10382
gfz 190| 0 0 0 -84 -24 46 -.26 28 23 | 229661 -6099 4479 9159
grg 130| 2 -2 4 110 -3 107 -.09 46 45 | --- --- --- ---
iac n/a| 1 1 -24 -7 91 83 -.17 31 31 | 383775 -2832 4508 9357
mcc n/a| -5 0 57 74 120 464 .16 164 164 | --- --- --- ---
Table 2.1629.6 GPS week: 1629 Day: 6 MJD: 55653
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 149| -1 -3 18 93 3 -402 .02 116 71 | 0 506 4266 4620
cod 241| 0 1 16 99 -76 -58 -.05 25 22 | --- --- --- ---
esx 131| 0 0 5 -52 -18 8 .44 22 20 | 40598 3026 5674 10644
gfz 190| 2 -1 5 -67 36 17 -.16 22 25 | 242806 5491 5684 9674
grg 130| -2 0 3 59 109 -13 -.02 53 51 | --- --- --- ---
iac n/a| 0 0 -36 16 96 118 -.23 29 29 | 401873 2432 5676 9925
mcc n/a| 4 -6 46 179 39 721 -.22 140 140 | --- --- --- ---
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 3.1629.0 GPS week: 1629 Day: 0 MJD: 55647
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2400 21 12 12 28 49 31 --- 10 | 48 24 28 39 33 34 --- 26
R02 | 1109 32 18 14 35 56 43 --- 14 | 49 49 50 49 29 32 --- 41
XR03 | 3508 35 14 --- --- --- 40 --- 21 | 116 111 --- --- --- 91 --- 104
R05 | 2074 20 11 17 29 72 15 92 9 | 61 59 39 67 38 52 25 50
R06 | 1448 35 19 13 23 63 31 --- 11 | 63 43 28 30 27 22 --- 30
R07 | 1953 27 20 21 39 27 27 --- 13 | 56 57 34 61 31 25 --- 41
R08 | 2423 16 17 14 24 48 23 135 9 | 41 48 33 41 41 36 58 36
R09 | 550 20 22 12 13 31 22 --- 9 | 72 61 70 71 63 70 --- 66
R10 | 1972 34 25 11 27 63 36 --- 13 | 114 86 100 101 111 80 --- 94
R11 | 1152 50 34 21 35 75 52 --- 18 | 170 144 163 159 154 154 --- 155
R12 | 873 44 18 19 19 29 17 --- 12 | 63 71 64 71 68 66 --- 64
R13 | 1039 19 12 12 15 79 29 --- 8 | 120 119 122 124 119 105 --- 118
R15 | 1321 21 16 25 22 68 64 --- 15 | 137 119 141 132 163 95 --- 124
R16 | 1874 22 21 18 20 43 26 --- 10 | 80 75 88 86 71 82 --- 80
R17 | 1725 44 43 23 29 66 58 --- 19 | 9999 9999 9999 9999 9999 9999 --- 9999
R18 | 1644 57 19 23 33 34 29 67 16 | 70 49 32 44 49 29 67 35
R19 | 2019 45 26 25 24 43 24 --- 14 | 67 45 36 35 38 36 --- 35
XR20 | 7156 54 24 --- 35 70 40 --- 22 | 160 134 --- 147 138 113 --- 137
R21 | 960 17 16 24 19 44 31 --- 11 | 64 52 47 47 51 41 --- 46
R22 | 1632 25 30 27 23 33 28 --- 13 | 51 58 40 49 42 42 --- 41
R23 | 1327 40 43 36 24 68 31 132 18 | 73 51 59 42 53 39 160 42
R24 | 936 32 19 11 26 49 22 --- 11 | 36 39 28 37 41 33 --- 27
------+----------------------------------------------+------------------------------------------
RMS | 1607 33 24 20 26 54 34 110 |T 81 71 63 71 68 60 77 66
WRMS | 1607 30 21 19 25 56 34 110 |NE 64 54 37 52 47 41 77 45
MEDI | 1632 32 19 18 24 49 29 92 |MD 67 58 47 49 49 42 58 46
Table 3.1629.1 GPS week: 1629 Day: 1 MJD: 55648
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 6234 26 30 17 12 49 29 --- 11 | 46 38 42 43 61 29 --- 33
R02 | 1542 17 26 19 16 37 18 --- 10 | 39 40 27 31 42 29 --- 26
XR03E | 4569 30 18 --- --- --- 36 --- 19 | 77 54 --- --- --- 61 --- 55
R05 | 2266 40 23 25 32 68 24 158 14 | 44 37 26 53 46 44 41 33
R06 | 1914 25 15 12 29 41 32 --- 11 | 57 35 36 59 27 25 --- 38
R07 | 2005 31 22 18 38 40 22 --- 13 | 65 44 43 38 48 23 --- 34
R08 | 3090 37 19 13 19 31 24 42 10 | 48 36 26 21 30 21 73 21
R09 | 1119 22 25 16 25 42 30 --- 11 | 77 78 89 110 88 85 --- 87
R10E | 1583 21 15 12 27 56 30 --- 10 | 57 53 49 51 68 29 --- 44
R11E | 2459 59 51 23 30 79 80 --- 24 | 145 110 133 135 136 102 --- 118
R12 | 891 58 21 13 30 56 22 --- 14 | 110 94 83 78 95 89 --- 85
R13E | 1044 22 13 13 17 37 32 --- 9 | 63 55 63 69 74 51 --- 57
R15E | 1757 58 31 14 23 39 44 --- 16 | 103 57 72 68 67 45 --- 62
R16 | 1709 18 21 7 26 65 26 --- 10 | 99 91 97 118 120 105 --- 100
XR17 |10117 975 34 --- 5652 --- 97 --- 68 | 9999 9999 --- 9999 --- 9999 --- 9999
R18 | 1526 43 23 19 19 59 18 119 12 | 56 30 26 31 59 21 80 25
R19 | 1408 82 23 21 23 44 24 --- 18 | 93 38 22 27 35 25 --- 28
XR20 | 6081 111 39 --- 27 --- 24 --- 32 | 190 157 --- 142 --- 131 --- 150
R21 | 1593 33 26 21 17 53 28 --- 12 | 55 36 29 44 56 42 --- 32
R22 | 1412 19 28 27 23 44 42 --- 14 | 25 35 34 46 42 32 --- 27
R23 | 1264 28 36 26 25 39 30 160 14 | 36 29 36 36 42 22 107 17
R24 | 759 32 20 20 21 34 24 --- 11 | 40 29 30 36 37 20 --- 23
------+----------------------------------------------+------------------------------------------
RMS | 2204 39 26 18 24 50 33 129 |T 72 56 50 61 61 49 75 52
WRMS | 2204 30 24 18 19 51 33 129 |NE 61 44 31 46 43 35 75 37
MEDI | 1593 31 23 18 25 44 28 119 |MD 57 40 36 46 56 32 73 34
Table 3.1629.2 GPS week: 1629 Day: 2 MJD: 55649
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 |12060 55 19 15 26 47 30 --- 14 | 60 33 42 50 55 37 --- 37
R02 | 1751 52 16 36 17 50 22 --- 14 | 66 35 33 28 38 37 --- 29
R03E | 3994 27 15 15 13 --- 19 --- 8 | 102 77 48 46 --- 72 --- 78
R05 | 2543 33 25 16 20 36 21 141 11 | 44 50 33 37 43 39 21 34
R06 | 2499 14 25 33 24 40 25 --- 13 | 36 37 34 51 31 38 --- 32
R07 | 2822 27 21 13 28 53 35 --- 12 | 53 35 26 42 54 22 --- 26
R08 | 3209 37 17 13 18 55 25 99 10 | 44 42 48 42 48 35 30 39
R09 | 903 51 27 21 24 62 40 --- 15 | 109 105 119 114 148 90 --- 106
R10E | 2346 26 17 19 21 43 26 --- 10 | 74 64 70 60 68 57 --- 61
R11E | 5565 45 45 17 28 64 36 --- 17 | 152 108 132 132 104 115 --- 123
R12E | 1823 30 24 29 15 65 43 --- 14 | 72 78 107 89 123 58 --- 82
R13E | 1086 24 13 20 18 40 23 --- 9 | 76 74 84 87 86 67 --- 77
R15E | 3148 38 17 21 19 62 30 --- 12 | 85 80 75 80 85 69 --- 75
R16 | 1494 49 34 25 36 71 64 --- 20 | 156 118 155 161 188 94 --- 135
XR17 |14573 99 355 --- 54 --- 112 --- 61 | 9999 9999 --- 9999 --- 9999 --- 9999
R18 | 1476 31 24 14 17 36 15 85 10 | 44 37 29 32 31 26 40 27
R19 | 1191 41 22 12 27 50 16 --- 12 | 45 39 32 27 36 22 --- 25
R20 | 3347 31 13 11 17 --- 44 --- 12 | 100 97 29 98 --- 92 --- 99
R21 | 2125 26 34 22 26 32 37 --- 14 | 51 60 47 48 30 48 --- 44
R22 | 1174 47 33 23 18 61 26 --- 14 | 84 46 47 36 82 41 --- 44
R23 | 1209 37 22 34 12 65 20 146 13 | 64 43 30 40 57 37 77 33
R24 | 761 25 28 29 23 36 35 --- 14 | 37 30 31 28 36 30 --- 16
------+----------------------------------------------+------------------------------------------
RMS | 3599 37 25 22 22 52 32 120 |T 74 61 59 63 70 53 42 58
WRMS | 3599 33 24 20 24 49 32 120 |NE 56 44 35 43 45 38 42 37
MEDI | 2125 33 22 20 20 50 26 99 |MD 66 50 47 48 55 41 30 44
Table 3.1629.3 GPS week: 1629 Day: 3 MJD: 55650
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 |14524 24 14 21 23 63 24 --- 10 | 32 35 44 40 39 33 --- 31
R02 | 1739 45 33 21 26 84 30 --- 15 | 45 45 29 42 44 28 --- 31
R03E | 4224 14 13 17 17 --- 22 --- 8 | 70 64 47 43 --- 57 --- 71
R05 | 3102 15 25 17 17 45 26 89 10 | 27 41 44 40 33 26 28 33
R06 | 8507 33 26 25 16 21 17 --- 12 | 38 55 34 46 51 46 --- 36
R07 | 4045 14 31 32 47 50 25 --- 16 | 33 42 44 69 53 32 --- 38
R08 | 1168 20 16 19 24 41 22 128 10 | 49 41 39 40 39 45 37 37
R09E | 1548 43 24 25 36 41 22 --- 15 | 120 119 143 162 142 151 --- 138
R10E | 6387 17 14 16 30 32 33 --- 11 | 47 53 62 59 60 55 --- 52
R11E | 9697 64 45 34 37 68 35 --- 21 | 100 110 133 121 122 99 --- 111
R12E | 3192 29 15 23 26 37 24 --- 12 | 100 110 121 106 131 95 --- 106
R13E | 2899 23 15 17 24 29 30 --- 11 | 70 89 97 95 90 73 --- 85
R15E | 7488 37 28 21 28 81 19 --- 13 | 54 64 66 70 83 53 --- 59
R16E | 2809 41 25 15 29 47 23 --- 13 | 131 135 153 170 145 156 --- 148
R17 |13503 48 43 24 26 --- 72 --- 22 | 9999 9999 891 9999 --- 9999 --- 9999
R18 | 3860 29 45 19 24 39 15 79 14 | 28 61 38 32 61 30 30 32
R19 | 3423 23 17 13 18 38 12 --- 8 | 45 51 31 38 40 48 --- 38
R20 | 2584 66 19 34 26 54 70 --- 22 | 133 115 37 109 67 105 --- 114
R21 | 3809 26 17 19 17 31 18 --- 9 | 35 51 48 39 37 39 --- 41
R22 | 3148 30 40 24 26 39 26 --- 15 | 50 61 33 31 47 33 --- 35
R23 | 2862 31 17 39 23 67 17 139 13 | 34 49 71 68 74 40 51 52
R24 | 1573 20 10 19 17 28 22 --- 9 | 40 35 25 51 59 32 --- 33
------+----------------------------------------------+------------------------------------------
RMS | 6038 35 26 23 26 50 31 112 |T 61 67 101 70 70 60 36 62
WRMS | 6038 28 24 22 24 47 31 112 |NE 45 52 100 49 49 41 36 42
MEDI | 3192 29 19 21 24 41 23 89 |MD 47 55 44 51 59 46 30 41
Table 3.1629.4 GPS week: 1629 Day: 4 MJD: 55651
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1731 53 22 9 22 53 22 --- 12 | 74 28 34 48 23 37 --- 35
R02 | 4686 40 15 9 18 86 18 --- 9 | 58 36 29 21 50 24 --- 27
R03E | 6524 54 13 14 18 --- 25 --- 11 | 92 61 45 47 --- 44 --- 57
R05 | 2381 19 44 21 16 28 30 52 14 | 25 42 35 30 27 32 26 24
R06 | 2830 19 19 23 13 49 44 --- 12 | 60 33 65 46 35 27 --- 42
R07 | 4797 69 18 21 50 51 18 --- 18 | 82 26 24 49 55 24 --- 20
R08 | 3002 24 16 17 20 48 23 170 9 | 55 35 35 56 51 42 74 39
R09E | 1090 23 15 11 15 38 32 --- 9 | 89 80 91 88 91 81 --- 84
R10E | 2695 20 22 14 17 39 25 --- 9 | 27 34 50 39 53 39 --- 37
R11E | 5892 68 38 29 34 47 27 --- 18 | 107 93 114 99 90 83 --- 97
R12E | 3190 47 21 22 15 32 25 --- 12 | 88 77 82 72 83 62 --- 73
R13E | 5460 31 13 15 17 33 23 --- 9 | 85 63 70 59 70 55 --- 63
R15E | 5488 54 27 13 29 36 35 --- 14 | 80 34 65 78 62 45 --- 54
R16E | 2605 45 21 14 23 26 35 --- 12 | 128 105 103 102 106 97 --- 102
R17 |10656 93 58 17 36 57 62 --- 25 | 9999 9999 765 9999 791 9999 --- 9999
R18 | 3492 29 40 16 22 49 29 115 13 | 32 53 33 23 45 18 68 26
R19 | 2170 71 21 37 22 34 25 --- 17 | 88 41 40 31 28 41 --- 32
R20 | 2677 68 26 24 18 73 68 --- 19 | 105 100 45 109 79 90 --- 102
R21 | 4214 56 21 23 16 47 18 --- 12 | 82 60 44 63 59 46 --- 52
R22 | 2936 27 39 17 18 51 20 --- 12 | 58 56 33 38 46 34 --- 37
R23 | 3361 45 16 12 19 38 26 140 11 | 58 44 44 45 37 41 71 42
R24 | 2451 28 17 12 19 50 32 --- 10 | 65 33 46 50 45 62 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 4341 49 27 19 23 48 33 127 |T 73 54 86 56 91 48 59 51
WRMS | 4341 38 28 18 21 45 33 127 |NE 64 45 90 46 97 39 59 40
MEDI | 3002 45 21 16 18 47 25 115 |MD 80 44 45 49 53 42 68 42
Table 3.1629.5 GPS week: 1629 Day: 5 MJD: 55652
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 3709 45 14 10 31 46 22 --- 11 | 38 31 30 41 43 21 --- 25
R02 | 4124 36 16 14 22 44 20 --- 10 | 56 35 36 39 51 25 --- 32
R03E | 6252 35 19 12 48 --- 40 --- 15 | 95 41 35 58 --- 41 --- 47
R05 | 839 35 32 15 28 43 26 59 13 | 44 41 26 24 44 25 25 22
R06 | 3521 47 19 18 22 53 31 --- 12 | 60 39 41 39 56 32 --- 33
R07 | 3690 54 19 11 25 35 21 --- 12 | 68 26 23 46 27 21 --- 24
R08 | 2994 29 14 15 29 35 27 171 11 | 65 34 42 56 51 48 38 42
R09E | 1254 33 16 13 18 38 25 --- 10 | 96 69 70 76 75 68 --- 72
R10E | 2594 29 14 14 16 48 31 --- 10 | 46 36 43 42 63 44 --- 37
R11E | 852 51 63 20 34 43 41 187 20 | 81 91 93 96 88 73 13 83
R12E | 2821 20 17 17 24 41 28 --- 10 | 89 67 72 66 73 71 --- 68
R13E | 4405 44 24 16 24 50 29 --- 12 | 94 48 59 60 54 49 --- 54
R15E | 3532 43 33 16 29 63 36 256 14 | 67 31 36 52 62 48 76 38
R16E | 2113 37 16 15 18 60 30 --- 11 | 55 52 59 55 70 51 --- 51
R17 | 4302 44 55 30 43 41 54 --- 22 | 9999 9999 694 9999 639 9999 --- 9999
R18 | 2496 44 39 33 19 59 27 102 16 | 65 52 32 42 43 40 37 33
R19 | 2078 37 24 15 22 56 23 --- 11 | 41 41 19 25 51 37 --- 25
R20 |10760 130 58 29 39 59 26 --- 27 | 115 94 47 82 70 78 --- 80
R21 | 562 51 33 16 32 30 30 --- 15 | 72 60 54 53 53 47 --- 49
R22 | 1995 44 28 10 16 30 21 --- 11 | 61 59 43 42 53 32 --- 41
R23 | 1273 63 24 16 20 38 30 137 14 | 101 37 43 44 42 33 45 41
R24 | 3532 55 17 13 19 29 37 --- 13 | 47 41 40 38 26 54 --- 37
------+----------------------------------------------+------------------------------------------
RMS | 3826 50 31 18 28 46 31 164 |T 69 48 74 51 82 44 39 44
WRMS | 3826 43 30 16 23 45 31 164 |NE 64 45 83 43 89 37 36 37
MEDI | 2821 44 19 15 24 43 28 137 |MD 65 41 42 46 53 44 37 41
Table 3.1629.6 GPS week: 1629 Day: 6 MJD: 55653
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2315 57 14 10 21 34 29 --- 11 | 35 26 24 26 33 27 --- 22
R02 | 1030 44 12 19 9 47 22 --- 9 | 63 38 31 38 34 36 --- 32
R03E | 3114 282 20 19 18 --- 37 --- 14 | 227 69 42 36 --- 70 --- 72
R05 | 1017 45 27 19 26 34 19 56 12 | 35 52 41 30 41 47 19 37
R06 | 3039 160 19 20 18 49 25 --- 19 | 135 40 36 41 39 25 --- 34
R07 | 1863 179 29 21 32 69 35 --- 23 | 143 42 29 52 61 21 --- 26
R08 | 1964 75 15 22 16 80 30 163 13 | 48 55 63 56 47 37 31 50
R09E | 2287 40 18 20 22 66 32 --- 12 | 104 102 118 119 120 101 --- 109
R10E | 1825 38 25 15 19 24 39 --- 13 | 66 60 69 63 68 63 --- 60
R11E | 912 95 38 26 32 50 39 211 19 | 139 115 151 141 131 124 9 130
R12E | 1447 59 23 21 22 60 33 --- 13 | 78 82 82 82 83 76 --- 78
R13E | 1556 173 23 30 31 27 36 --- 23 | 155 90 93 90 95 84 --- 86
R15E | 3178 45 19 26 23 42 30 171 13 | 47 64 72 65 59 49 15 59
R16E | 3969 67 22 21 23 64 30 --- 13 | 137 121 137 139 119 125 --- 128
R17 | 4459 152 28 41 26 45 40 --- 23 | 9999 9999 802 9999 741 9999 --- 9999
R18 | 2574 50 27 20 18 60 19 57 11 | 49 59 48 40 48 32 31 41
R19 | 1123 39 20 19 11 59 24 --- 10 | 51 54 45 45 50 36 --- 43
R20 | 7252 176 53 24 30 50 27 --- 25 | 155 97 26 93 67 87 --- 93
R21 | 574 144 33 32 22 --- 21 --- 20 | 148 74 42 46 --- 49 --- 47
R22 | 865 97 22 14 14 58 17 --- 13 | 74 71 52 56 37 51 --- 54
R23 | 1120 52 12 14 23 50 25 106 10 | 61 52 54 56 45 60 76 53
R24 | 803 67 20 20 19 65 23 --- 12 | 58 54 38 38 53 46 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 2670 116 25 22 22 53 29 140 |T 95 67 95 64 98 59 30 61
WRMS | 2670 71 21 20 25 51 29 140 |NE 81 54 95 47 99 42 39 44
MEDI | 1825 67 22 20 22 50 29 106 |MD 74 60 48 56 53 49 19 53
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