[IGSREPORT-23720] Wk 1850 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Jul 10 08:49:11 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1850 (Jun 21, 2015 - Jun 27, 2015)
Contact: igs.acc 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 2.1850.
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:
igl1850[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1850 in the SP3 format.
igl18507.sum Combination Report for GPS Week 1850.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
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 until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
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) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -8.6 ns
1 | 0.9 ns
2 | 0.0 ns
3 | -0.5 ns
4 | -0.4 ns
5 | -0.1 ns
6 | 8.4 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 | COD | R12
5 | COD | R11 R12
6 | COD | R11 R12
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 1.1850, 1a.1850).
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 2.1850.0-6)
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 3.1850.0-6).
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 1850 summary. (Jun 21, 2015 - Jun 27, 2015)
Table 1.1850.a GPS week : 1850 MJD: 57194.0-57200.0
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -2 55 -29 2 .32 56 46 | --- --- --- ---
| 1 2 4 34 25 29 .05 | --- ---
cof n/a| -1 -1 -3 37 -19 11 .27 59 47 | --- --- --- ---
| 1 2 3 16 44 39 .05 | --- ---
emx n/a| -1 0 6 31 -40 -30 .26 29 28 | -1808 -826 4536 7219
| 1 1 2 20 24 13 .04 | 8200 1218
esx n/a| 0 0 -1 -33 8 16 -.00 21 19 | -3917 -1975 4245 7679
| 0 0 1 18 17 29 .04 | 4173 1109
gfz n/a| 0 0 0 16 54 38 .13 21 18 | 0 -778 4169 6673
| 0 1 1 21 10 19 .07 | 0 1493
grg n/a| -1 1 1 -3 28 165 -.30 36 33 | -773617 -1226 9534 692784
| 1 1 3 28 29 21 .06 | 8843 1852
iac n/a| 2 0 -1 -17 -19 -84 -.23 20 20 | 1605 -360 4647 7459
| 1 1 1 26 23 28 .03 | 4728 1185
mcc n/a| 2 0 22 0 -106 -717 -.47 171 171 | --- --- --- ---
| 10 7 28 53 155 827 .24 | --- ---
Table 1.1850.b GPS week : 1850 MJD: 57194.0-57200.0
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 10 10 9 10 10 11 |
R02 | 7 8 7 7 7 7 8 |
R03 | 9 9 8 7 8 9 8 |
R04 | 7 9 9 8 8 7 6 |
R05 | 12 11 10 12 15 11 16 |
R06 | 8 7 12 9 11 11 10 |
R07 | 6 8 7 7 7 7 7 |
R08 | 9 7 7 7 9 7 8 |
R09 | 12 13 13 15 15 12 15 |
R10 | 9 10 7 8 9 15 8 |
R11 | 22 21 22 23 25 15 14 |
R12 | 19 23 20 23 26 20 18 |
R13 | 10 10 11 12 12 10 10 |
R14 | 16 20 20 17 20 17 16 |
R15 | 9 9 10 9 13 12 10 |
R16 | 11 10 10 12 10 9 11 |
R17 | 25 22 22 25 23 23 21 |
R18 | 11 9 9 7 8 9 10 |
R19 | 12 11 10 10 9 10 9 |
R20 | 14 14 15 13 16 16 18 |
R21 | 12 13 13 14 13 10 11 |
R22 | 10 11 12 13 12 11 11 |
R23 | 9 10 10 10 11 10 10 |
R24 | 12 13 13 14 15 15 13 |
Table 1.1850.c GPS week : 1850 MJD: 57194.0-57200.0
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 1850 0 | 154 55 302 416 851 1393 85.0 2258 2258 | -8611 0
brd 1850 1 | -154 -86 30 1638 1887 -865 91.2 8571 8571 | 887 0
brd 1850 2 | 42 -31 231 1095 -1509 261 86.8 2760 2760 | 0 0
brd 1850 3 | -36 -36 186 1231 -104 735 86.3 1697 1697 | -465 0
brd 1850 4 | -106 8 224 -751 -461 912 87.0 1574 1574 | -428 0
brd 1850 5 | -49 -17 306 1660 -1248 1988 86.0 1648 1648 | -139 0
brd 1850 6 | -17 -79 111 -226 478 4516 86.1 1872 1872 | 8425 0
-------------+------------------------------------------------------------+----------------
brd 1850 mean| -23 -26 198 723 -15 1277 86.9 2911 2911 | -47 0
brd 1850 sdev| 100 49 99 938 1195 1686 2.0 2530 2530 | 4938 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 2.1850.0 GPS week: 1850 Day: 0 MJD: 57194
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 3 -11 -36 -8 .34 51 46 | --- --- --- ---
cof n/a| -4 -4 1 4 -41 -26 .31 56 47 | --- --- --- ---
emx n/a| 0 2 7 38 -20 -9 .28 29 27 | -8392 -2712 4299 7558
esx n/a| 0 -1 -2 -22 -11 -20 -.00 20 19 | -5561 -3089 4318 8728
gfz n/a| 0 2 -1 40 53 28 .09 20 20 | 0 -2990 4275 7627
grg n/a| 0 0 0 -10 64 157 -.38 33 29 | -780624 -3299 4376 694544
iac n/a| 2 -1 -1 -51 -16 -70 -.27 18 18 | -6110 -2050 4375 8002
mcc n/a| 1 -12 15 26 -211 202 -.33 119 119 | --- --- --- ---
Table 2.1850.1 GPS week: 1850 Day: 1 MJD: 57195
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 0 0 49 -20 -16 .34 50 35 | --- --- --- ---
cof n/a| -3 0 -2 35 12 44 .33 50 35 | --- --- --- ---
emx n/a| -1 0 9 56 -28 -40 .31 30 28 | 2206 613 4797 8174
esx n/a| 0 -1 -2 -44 3 -17 .06 21 18 | -8627 -809 3806 7324
gfz n/a| 0 0 -1 14 66 58 .23 23 21 | 0 525 3811 6293
grg n/a| -3 1 0 12 25 169 -.35 37 33 | -755173 1386 38291 684460
iac n/a| 2 1 0 -19 -49 -62 -.22 18 18 | 1992 1374 4839 8140
mcc n/a| -3 4 -15 19 -184 524 -.62 132 132 | --- --- --- ---
Table 2.1850.2 GPS week: 1850 Day: 2 MJD: 57196
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 1 71 8 8 .37 49 42 | --- --- --- ---
cof n/a| -1 -2 0 43 63 5 .26 54 45 | --- --- --- ---
emx n/a| 0 0 6 2 -69 -30 .26 33 32 | 5651 -1299 4788 7268
esx n/a| 0 -1 -2 -62 31 18 .04 22 20 | -2153 -2579 3936 6989
gfz n/a| 0 0 1 -19 34 59 .07 19 19 | 0 -678 3969 5952
grg n/a| -1 0 0 7 50 179 -.29 37 34 | -772877 -2745 6251 695109
iac n/a| 2 0 0 30 -21 -82 -.22 17 17 | 3533 -1580 5479 9187
mcc n/a| 21 11 12 46 137 -416 -.27 143 143 | --- --- --- ---
Table 2.1850.3 GPS week: 1850 Day: 3 MJD: 57197
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 2 0 77 -54 47 .30 56 52 | --- --- --- ---
cof n/a| -3 2 -4 38 -69 10 .22 60 53 | --- --- --- ---
emx n/a| -2 -1 6 21 -54 -32 .22 30 27 | -5243 -808 4404 6404
esx n/a| 0 0 -1 -9 2 56 -.01 18 18 | -5692 -2854 4246 7271
gfz n/a| 1 1 -1 22 51 17 .07 19 20 | 0 -2027 4218 6155
grg n/a| -2 1 6 -38 28 174 -.21 38 35 | -777159 -1400 4412 694085
iac n/a| 2 0 0 -12 20 -134 -.21 20 20 | 125 598 4406 6250
mcc n/a| 11 3 39 24 50 -1221 -.84 148 148 | --- --- --- ---
Table 2.1850.4 GPS week: 1850 Day: 4 MJD: 57198
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -4 -4 92 -46 7 .36 59 58 | --- --- --- ---
cof n/a| 0 -3 -4 38 -25 76 .23 62 62 | --- --- --- ---
emx n/a| -4 -2 3 49 -66 -35 .26 28 26 | -13604 -1795 3588 6343
esx n/a| 0 0 0 -48 -8 50 -.03 22 20 | -680 -2872 3580 6978
gfz n/a| 0 0 0 44 55 28 .07 24 16 | 0 -1156 3577 6487
grg n/a| 0 0 -1 -36 45 166 -.25 37 36 | -778172 -2726 3561 694780
iac n/a| 2 0 0 -7 -18 -113 -.22 23 23 | 924 -378 3572 6283
mcc n/a| -9 0 39 35 -92 -1393 -.64 187 187 | --- --- --- ---
Table 2.1850.5 GPS week: 1850 Day: 5 MJD: 57199
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 -7 38 0 24 .29 62 42 | --- --- --- ---
cof n/a| 0 0 -7 57 -25 4 .22 65 45 | --- --- --- ---
emx n/a| 1 0 2 12 -5 -18 .20 28 28 | -3121 -320 4879 6685
esx n/a| 0 0 0 -27 14 14 -.04 19 17 | -7740 -1072 4831 7540
gfz n/a| 0 0 0 10 61 58 .19 20 14 | 0 -591 4823 6542
grg n/a| -2 3 0 43 -24 122 -.31 40 36 | -780003 -727 4870 693554
iac n/a| 0 -2 -3 -23 -43 -69 -.27 21 21 | 939 -508 4862 6559
mcc n/a| -2 0 67 -101 -132 -1134 -.42 228 228 | --- --- --- ---
Table 2.1850.6 GPS week: 1850 Day: 6 MJD: 57200
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 2 -7 72 -53 -44 .23 62 43 | --- --- --- ---
cof n/a| 0 0 -8 42 -51 -36 .30 65 45 | --- --- --- ---
emx n/a| -1 1 6 42 -35 -49 .26 29 28 | 9841 538 4997 8103
esx n/a| 0 -1 0 -18 30 13 -.04 21 18 | 3031 -553 4999 8923
gfz n/a| 1 -1 -1 6 55 18 .20 22 14 | 0 1468 4516 7660
grg n/a| 0 0 7 -1 5 189 -.30 33 28 | -771315 928 4979 692961
iac n/a| 1 0 -2 -40 -7 -61 -.21 18 18 | 9832 21 4998 7796
mcc n/a| -1 0 -5 -44 -312 -1582 -.15 241 241 | --- --- --- ---
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 3.1850.0 GPS week: 1850 Day: 0 MJD: 57194
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1897 28 42 31 22 20 17 13 --- 9 | 42 52 45 31 39 34 40 --- 33
R02 | 1271 18 23 12 16 11 21 16 92 7 | 54 58 47 33 43 35 42 52 39
R03 | 1380 16 16 18 11 22 31 16 --- 8 | 56 56 65 67 60 72 60 --- 61
R04 | 1406 21 26 22 10 13 10 14 --- 6 | 66 69 67 54 50 54 47 --- 53
R05 | 1466 18 16 23 31 16 43 21 --- 11 | 59 58 52 55 60 60 58 --- 55
R06 | 1125 16 12 19 16 9 33 13 --- 8 | 52 51 58 52 50 42 51 --- 48
R07 | 1285 19 22 12 11 8 27 8 126 6 | 68 67 70 62 58 57 61 78 61
R08 | 1283 19 16 29 20 15 22 14 --- 8 | 60 57 66 41 46 47 56 --- 49
R09 | 1744 15 23 28 27 23 47 18 --- 12 | 29 35 30 40 32 35 26 --- 26
R10 | 1089 18 18 21 21 14 31 12 --- 8 | 27 30 26 36 23 28 24 --- 22
R11 | 1568 119 110 34 22 31 56 22 --- 21 | 100 97 35 29 43 57 40 --- 27
R12 | 1705 159 177 63 20 34 51 16 152 18 | 115 130 40 33 54 61 39 82 35
R13 | 5272 26 30 22 18 15 34 20 --- 9 | 42 45 34 34 25 30 23 --- 23
R14 | 3259 34 46 50 34 21 53 26 --- 16 | 33 42 30 41 30 36 26 --- 21
R15 | 2120 13 20 24 25 14 14 18 --- 8 | 29 35 30 38 27 18 20 --- 22
R16 | 2092 29 37 28 25 28 21 13 --- 11 | 27 37 27 36 37 23 22 --- 23
XR17E | 853 42 57 51 --- --- 26 43 --- 24 | 47 52 45 --- --- 45 40 --- 36
R18E | 993 46 49 25 11 19 37 16 47 11 | 50 52 28 22 27 40 20 27 22
R19E | 1077 40 47 28 16 17 21 31 --- 11 | 87 93 83 83 86 82 88 --- 83
R20E | 5834 50 56 31 21 30 32 25 --- 13 | 91 89 86 91 102 98 95 --- 91
R21E | 1435 54 65 23 15 16 34 19 148 11 | 63 72 33 29 40 44 24 47 30
R22E | 1581 47 55 24 15 12 24 13 --- 10 | 65 69 58 56 60 76 57 --- 57
R23E | 1204 29 31 20 14 12 27 18 --- 8 | 37 45 35 45 46 45 42 --- 40
R24E | 1531 49 57 24 23 22 17 22 --- 11 | 50 61 36 39 36 25 32 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 2257 51 56 29 20 20 33 18 119 |T 56 60 46 45 46 47 43 57 41
WRMS | 2257 46 47 27 19 20 29 18 119 |NE 53 57 45 42 42 43 39 70 37
MEDI | 1435 28 31 24 20 16 27 16 126 |MD 52 56 40 40 43 44 40 52 35
Table 3.1850.1 GPS week: 1850 Day: 1 MJD: 57195
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 3337 27 31 32 21 12 34 10 --- 9 | 33 28 39 37 39 40 28 --- 30
R02 | 2352 24 31 15 10 13 40 9 106 8 | 37 42 36 26 36 22 35 84 29
R03 | 4751 13 13 18 18 22 33 12 --- 8 | 44 46 37 39 37 40 37 --- 36
R04 | 7233 29 32 27 13 24 17 13 --- 8 | 43 46 45 33 31 30 29 --- 30
R05 | 9632 29 35 21 20 15 50 15 --- 10 | 37 43 30 43 33 49 35 --- 33
R06 | 4843 18 15 17 14 16 9 12 --- 6 | 35 29 30 23 31 46 32 --- 26
R07 |11005 22 28 20 13 17 37 10 174 8 | 43 52 45 46 51 37 38 76 40
R08 |10138 18 26 22 14 13 28 9 --- 7 | 37 45 44 32 35 27 38 --- 33
XR09 | 4197 23 38 22 34 --- 31 16 --- 13 | 25 43 25 40 --- 23 22 --- 20
R10 |10349 12 30 20 27 20 33 20 --- 10 | 27 39 26 34 31 38 17 --- 22
R11 |13401 108 105 43 33 24 67 29 --- 20 | 77 77 36 43 44 40 30 --- 29
R12 |16063 131 107 54 21 39 67 27 119 23 | 83 69 48 43 55 48 36 106 36
R13 |12384 28 29 23 17 26 35 7 --- 9 | 34 37 22 31 26 36 15 --- 18
R14 | 4354 43 42 58 37 38 58 40 --- 19 | 30 37 38 57 46 40 36 --- 32
R15 | 5374 12 12 24 21 18 19 15 --- 8 | 19 19 26 23 23 22 19 --- 16
R16 | 2422 18 16 24 28 20 27 15 --- 10 | 23 26 21 34 31 35 18 --- 19
XR17E |13346 46 56 39 --- --- 38 35 --- 22 | 37 53 35 --- --- 61 38 --- 32
R18E | 5451 43 51 20 14 15 28 9 70 8 | 41 52 24 28 28 35 21 43 21
R19E | 4074 52 60 23 20 19 29 13 --- 10 | 57 63 36 55 53 57 40 --- 43
R20E |13541 55 60 35 25 33 25 22 --- 13 | 98 104 93 91 103 108 83 --- 90
R21E | 2848 66 65 30 15 27 29 17 163 12 | 69 73 30 32 40 40 30 43 29
R22E | 7531 56 59 25 13 22 32 14 --- 11 | 67 73 48 56 64 61 42 --- 50
R23E | 6631 37 38 24 19 13 25 18 --- 9 | 64 68 51 55 58 59 47 --- 51
R24E | 9694 50 56 31 21 26 31 23 --- 12 | 58 62 42 41 45 47 28 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 8570 50 50 30 21 23 37 18 132 |T 46 51 37 40 42 43 33 70 33
WRMS | 8570 35 35 28 18 21 33 18 132 |NE 39 42 34 36 36 35 29 88 28
MEDI | 6631 29 35 24 20 20 31 15 119 |MD 37 46 36 39 37 40 32 76 30
Table 3.1850.2 GPS week: 1850 Day: 2 MJD: 57196
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 953 29 55 32 26 10 22 15 --- 9 | 29 75 53 41 37 34 36 --- 34
R02 | 7698 24 23 19 15 13 27 10 141 7 | 42 43 45 32 37 42 42 65 36
R03 | 1734 35 31 17 20 11 19 10 --- 7 | 49 60 63 71 59 58 60 --- 60
R04 | 790 15 21 19 12 15 30 21 --- 8 | 50 54 61 51 56 47 39 --- 48
R05 | 1190 18 23 25 24 19 38 15 --- 10 | 52 56 50 47 51 44 40 --- 43
R06 | 3504 16 21 14 21 20 65 14 --- 11 | 45 51 38 40 33 60 39 --- 33
R07 | 1061 16 18 27 15 14 14 9 169 7 | 56 46 56 53 62 60 62 51 57
R08 | 886 18 17 23 10 10 25 15 --- 7 | 49 50 55 41 47 42 33 --- 41
R09 | 1179 25 38 29 40 27 26 17 --- 12 | 26 51 34 45 35 30 30 --- 24
R10 | 1364 9 16 13 18 15 23 13 --- 7 | 19 21 24 23 21 27 14 --- 14
R11 | 1043 118 128 55 13 31 53 28 --- 21 | 84 90 41 35 39 44 30 --- 23
R12 | 1973 113 114 40 19 27 59 24 206 19 | 81 81 23 26 31 50 29 148 22
R13 | 1575 37 54 21 21 24 28 21 --- 10 | 46 60 33 32 21 18 21 --- 19
R14 | 2380 35 32 91 30 12 61 25 --- 20 | 33 45 42 49 35 35 28 --- 25
R15 | 5163 15 20 16 29 21 42 12 --- 10 | 25 31 21 33 20 28 24 --- 15
R16 | 2981 19 25 25 29 19 37 9 --- 10 | 20 27 23 27 19 19 18 --- 14
XR17E | 1143 49 34 43 --- --- 37 28 --- 21 | 35 29 39 --- --- 43 40 --- 30
R18E | 1969 33 33 29 15 14 27 14 57 9 | 41 43 27 34 29 42 21 49 24
R19E | 1926 44 49 25 14 16 24 19 --- 10 | 58 63 44 41 47 42 47 --- 41
R20E | 1083 68 81 34 28 20 58 18 --- 15 | 86 92 58 63 61 80 63 --- 60
R21E | 1923 72 79 29 15 22 30 19 90 13 | 71 78 30 28 44 34 28 20 29
R22E | 4974 59 49 23 17 23 29 20 --- 12 | 80 78 70 71 77 83 65 --- 69
R23E | 662 47 46 8 20 18 27 17 --- 9 | 34 42 34 43 35 45 33 --- 32
R24E | 2494 58 71 32 22 25 32 16 --- 13 | 56 80 35 47 53 32 33 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 2760 49 54 33 22 19 37 17 143 |T 48 56 41 42 41 43 36 66 34
WRMS | 2760 42 45 32 20 19 34 17 143 |NE 44 52 41 40 37 39 34 88 31
MEDI | 1575 33 33 25 20 19 29 16 141 |MD 46 51 39 41 37 42 33 51 32
Table 3.1850.3 GPS week: 1850 Day: 3 MJD: 57197
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 903 33 22 19 22 12 23 20 --- 9 | 53 48 53 48 53 46 46 --- 45
R02 | 817 20 24 25 12 12 10 11 143 6 | 48 48 53 35 31 38 36 51 36
R03 | 655 30 34 19 11 15 18 10 --- 7 | 56 51 60 66 70 67 64 --- 63
R04 | 917 15 15 23 13 10 32 19 --- 8 | 57 54 66 51 59 41 55 --- 53
R05 | 1202 22 35 24 25 17 55 20 --- 12 | 64 74 65 60 58 79 56 --- 58
R06 | 1334 22 24 20 9 14 43 18 --- 9 | 59 60 59 56 44 30 57 --- 49
R07 | 999 16 19 22 14 8 14 17 185 7 | 62 64 58 66 57 67 52 55 58
R08 | 918 15 19 13 15 16 25 11 --- 7 | 62 62 62 47 65 66 60 --- 57
R09 | 933 29 36 37 28 20 64 29 --- 15 | 39 41 28 35 27 42 35 --- 23
R10 | 1412 10 33 22 25 12 17 8 --- 8 | 23 37 31 30 19 27 16 --- 18
R11 | 649 139 131 59 12 30 54 33 --- 22 | 96 88 47 41 54 63 48 --- 36
R12 | 1451 136 145 53 16 40 59 22 162 22 | 98 107 40 43 59 65 40 89 36
R13 | 1728 47 51 11 28 18 38 22 --- 11 | 56 57 28 44 28 24 16 --- 25
R14 | 2815 48 43 62 28 19 37 34 --- 16 | 43 44 48 43 45 53 28 --- 33
R15 | 3585 23 27 21 15 20 28 14 --- 8 | 30 33 29 27 22 31 19 --- 17
R16 | 1155 25 40 22 25 19 55 12 --- 11 | 30 43 23 35 23 40 21 --- 21
XR17E | 1539 54 70 46 --- --- 58 30 --- 25 | 44 59 56 --- --- 60 41 --- 37
R18E | 2142 25 28 18 9 13 19 13 61 6 | 35 37 34 32 33 29 28 32 29
R19E | 2228 37 33 24 11 16 37 14 --- 9 | 59 59 57 51 54 54 41 --- 48
R20E | 1233 62 79 27 14 23 35 25 --- 12 | 97 109 92 97 107 93 88 --- 93
R21E | 2397 87 99 35 13 21 32 19 158 14 | 86 96 41 35 46 47 30 15 35
R22E | 1491 63 79 28 15 20 36 28 --- 12 | 93 103 84 91 99 99 69 --- 85
R23E | 1428 54 58 18 17 18 28 16 --- 10 | 69 75 69 68 67 59 60 --- 62
R24E | 2612 63 63 27 22 24 43 26 --- 13 | 59 67 49 46 50 51 44 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1697 56 60 30 18 19 38 20 148 |T 59 63 51 49 50 52 43 48 44
WRMS | 1697 52 53 27 18 20 35 20 148 |NE 54 56 46 45 44 48 40 65 39
MEDI | 1334 30 35 23 15 18 35 19 158 |MD 57 59 53 46 53 51 41 51 37
Table 3.1850.4 GPS week: 1850 Day: 4 MJD: 57198
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1072 33 29 25 17 21 19 22 --- 10 | 47 58 50 56 65 42 56 --- 50
R02 | 1012 18 22 19 7 10 19 14 142 6 | 43 46 32 42 46 51 33 43 39
R03 | 509 28 25 19 20 17 9 17 --- 8 | 46 54 54 65 60 59 61 --- 58
R04 | 1017 23 21 20 14 12 21 13 --- 7 | 57 55 56 39 48 37 44 --- 44
R05 | 1025 23 23 25 32 25 66 17 --- 14 | 53 61 59 76 68 55 61 --- 61
R06 | 1520 18 20 12 21 15 48 26 --- 11 | 45 55 56 56 59 39 64 --- 53
R07 | 929 22 24 20 8 12 18 15 219 7 | 62 65 58 53 49 46 59 73 53
R08 | 709 18 21 22 22 18 16 17 --- 8 | 54 55 58 53 32 53 43 --- 46
R09 | 1725 23 22 37 25 27 57 20 --- 14 | 29 36 30 39 34 40 33 --- 27
R10 | 1156 10 27 25 22 16 23 19 --- 9 | 28 34 38 30 30 59 17 --- 25
R11 | 858 150 156 47 30 43 55 34 --- 25 | 99 103 52 60 64 51 46 --- 39
R12 | 1204 161 171 46 22 44 58 40 152 26 | 107 114 35 54 70 69 51 38 41
R13 | 1761 47 53 18 23 25 39 10 --- 11 | 47 54 27 33 32 29 20 --- 21
R14 | 2385 61 66 59 29 32 47 40 --- 19 | 40 59 38 43 54 24 30 --- 29
R15 | 2197 25 44 27 38 20 35 18 --- 12 | 37 56 25 51 28 33 26 --- 24
R16 | 1165 29 30 26 16 20 29 15 --- 9 | 37 39 28 30 30 27 24 --- 23
XR17E | 988 62 53 40 --- --- 37 29 --- 22 | 56 59 27 --- --- 37 38 --- 24
R18E | 1706 30 33 14 16 14 22 11 66 7 | 39 45 29 32 26 30 26 22 24
R19E | 2507 32 42 22 15 15 26 18 --- 9 | 59 62 53 56 54 64 49 --- 52
R20E | 1279 66 54 24 27 30 32 41 --- 15 | 89 81 52 73 81 77 65 --- 64
R21E | 2589 51 53 23 17 20 49 19 281 12 | 66 69 36 48 49 55 40 22 41
R22E | 1194 64 64 24 19 20 24 20 --- 12 | 86 86 59 66 70 61 62 --- 61
R23E | 846 55 60 18 16 22 24 15 --- 10 | 54 57 53 50 56 45 38 --- 46
R24E | 2762 62 60 28 26 29 30 33 --- 14 | 60 56 34 45 41 38 20 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1574 59 62 28 22 24 37 23 187 |T 55 60 43 50 49 46 41 39 40
WRMS | 1574 58 62 26 20 16 36 23 187 |NE 51 59 43 48 48 44 41 51 39
MEDI | 1165 30 33 24 21 20 29 18 152 |MD 53 56 38 51 49 45 40 38 41
Table 3.1850.5 GPS week: 1850 Day: 5 MJD: 57199
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1177 20 21 31 19 14 31 15 --- 9 | 30 32 50 50 53 51 55 --- 47
R02 | 808 22 24 20 9 11 24 17 145 7 | 34 37 35 27 24 26 25 51 25
R03 | 813 21 29 25 15 14 28 16 --- 8 | 40 41 39 54 54 41 47 --- 46
R04 | 1428 22 30 13 10 10 30 10 --- 6 | 47 53 43 38 38 66 46 --- 43
R05 | 771 28 27 34 11 15 55 14 --- 11 | 38 34 52 62 61 42 57 --- 53
R06 | 1538 27 37 25 14 17 34 30 --- 10 | 36 34 38 63 57 64 56 --- 52
R07 | 1025 12 15 17 11 8 33 14 272 7 | 47 49 46 62 56 49 55 122 53
R08 | 836 17 17 17 16 11 16 17 --- 7 | 41 41 42 38 34 38 47 --- 38
R09 | 1541 14 21 32 24 25 51 18 --- 12 | 29 33 30 38 33 35 32 --- 27
R10 | 1425 19 20 16 19 18 101 13 --- 15 | 21 26 28 33 21 91 17 --- 26
R11 | 993 167 176 33 26 25 49 23 --- 14 | 101 113 46 54 53 40 36 --- 43
R12 | 1195 182 183 53 35 34 59 30 155 20 | 108 114 37 67 64 37 44 33 46
R13 | 1414 42 40 15 18 18 40 10 --- 10 | 40 36 18 28 19 27 16 --- 16
R14 | 1692 55 38 41 33 27 25 40 --- 16 | 31 47 49 66 66 61 31 --- 46
R15 | 2801 42 33 19 27 23 26 18 --- 11 | 36 32 26 30 33 22 20 --- 20
R16 | 1276 33 41 21 15 17 28 12 --- 8 | 37 46 26 23 26 23 17 --- 18
XR17E | 1017 57 53 36 --- --- 36 31 --- 22 | 58 57 51 --- --- 54 43 --- 41
R18E | 1757 28 35 18 15 11 33 22 72 9 | 40 45 27 31 32 41 27 49 26
R19E | 2040 40 48 25 13 17 25 17 --- 9 | 59 68 52 51 49 37 35 --- 44
R20E | 1768 63 69 41 20 29 45 33 --- 16 | 102 105 95 93 101 91 81 --- 87
R21E | 3249 43 43 26 11 20 22 17 367 10 | 56 58 41 38 36 30 25 33 31
R22E | 1668 47 54 22 13 18 36 18 --- 10 | 66 69 43 50 56 57 45 --- 47
R23E | 2632 47 45 27 14 15 25 17 --- 10 | 55 56 38 37 34 50 27 --- 33
R24E | 1098 64 78 26 26 30 23 29 --- 14 | 62 74 43 44 35 39 35 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1648 62 65 28 19 20 40 21 228 |T 50 54 41 46 45 46 38 57 39
WRMS | 1648 42 45 28 17 14 36 21 228 |NE 44 48 37 45 43 44 37 68 37
MEDI | 1414 33 37 25 15 17 31 17 155 |MD 40 46 41 44 38 41 35 49 41
Table 3.1850.6 GPS week: 1850 Day: 6 MJD: 57200
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1028 27 25 21 33 19 26 24 --- 11 | 54 52 61 51 60 67 65 --- 56
R02 | 890 17 17 21 15 15 11 23 90 8 | 56 55 52 47 46 48 49 82 47
R03 | 1759 17 13 28 13 13 12 15 --- 7 | 58 61 62 69 70 65 68 --- 65
R04 | 1556 15 15 11 8 8 26 12 --- 6 | 69 69 72 64 66 80 63 --- 66
R05 | 1023 29 33 49 13 29 64 24 --- 16 | 61 62 68 70 69 59 74 --- 66
R06 | 1860 29 33 17 32 11 25 13 --- 9 | 53 56 60 82 67 54 62 --- 62
R07 | 653 19 18 16 17 11 14 15 164 7 | 76 80 87 86 87 81 86 180 84
R08 | 864 12 17 13 19 16 19 16 --- 7 | 69 69 69 58 70 71 62 --- 64
R09 | 1028 22 39 23 29 41 57 25 --- 15 | 31 48 26 36 44 30 31 --- 26
R10 | 1431 15 19 26 18 11 27 12 --- 8 | 30 31 34 31 31 42 20 --- 23
R11 | 921 170 173 47 16 30 33 12 --- 14 | 116 119 49 61 81 61 57 --- 58
R12 | 1058 187 187 47 36 24 47 22 110 17 | 133 139 35 62 65 54 55 94 48
R13 | 1457 40 48 15 20 17 30 11 --- 9 | 49 55 30 34 25 28 26 --- 24
R14 | 1385 32 34 40 34 38 50 17 --- 15 | 28 46 26 56 66 43 41 --- 39
R15 | 5658 24 35 20 28 16 26 13 --- 9 | 34 39 33 46 24 35 22 --- 25
R16 | 1827 38 39 23 14 27 29 17 --- 11 | 44 47 24 28 35 28 20 --- 21
XR17E | 1454 57 65 45 45 --- 39 26 --- 21 | 50 60 39 13 --- 54 41 --- 33
R18E | 2523 35 33 22 11 21 30 19 134 10 | 45 44 32 32 32 36 33 51 30
R19E | 1105 40 45 21 10 15 19 17 --- 9 | 60 63 42 45 49 44 36 --- 42
R20E | 1012 71 89 51 21 35 34 23 --- 17 | 107 109 98 81 81 88 79 --- 80
R21E | 2650 39 31 23 12 22 28 19 474 10 | 54 56 44 46 49 47 39 127 41
R22E | 1633 41 34 27 14 20 32 18 --- 11 | 73 74 76 75 83 73 69 --- 72
R23E | 1930 37 43 23 20 16 23 21 --- 10 | 39 45 31 30 30 32 32 --- 26
R24E | 1019 65 75 18 18 22 26 17 --- 12 | 68 87 42 48 53 54 42 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1872 62 65 29 21 22 33 18 241 |T 60 65 49 52 55 53 48 106 47
WRMS | 1872 43 45 28 18 14 28 18 241 |NE 60 64 49 55 56 52 50 118 48
MEDI | 1385 32 34 23 18 19 27 17 134 |MD 54 56 42 48 60 54 42 94 43
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