[IGSREPORT-24572] Wk 1902 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Jul 7 07:03:16 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1902 (Jun 19, 2016 - Jun 25, 2016)
Contact: acc at igs.org
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 2.1902.
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:
igl1902[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1902 in the SP3 format.
igl19027.sum Combination Report for GPS Week 1902.
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 | -9.7 ns
1 | -8.2 ns
2 | -9.8 ns
3 | -4.3 ns
4 | -6.0 ns
5 | -9.9 ns
6 | -3.7 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 | GRG | R10
1 | IAC | R10
3 | COD | R10
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 1.1902, 1a.1902).
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 2.1902.0-6)
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 3.1902.0-6).
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 1902 summary. (Jun 19, 2016 - Jun 25, 2016)
Table 1.1902.a GPS week : 1902 MJD: 57558.0-57564.0
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 1 -3 48 -69 -5 .21 31 23 | --- --- --- ---
| 1 1 2 37 23 29 .06 | --- ---
cof n/a| -1 0 -4 42 -61 -5 .16 35 25 | --- --- --- ---
| 1 1 2 38 24 26 .07 | --- ---
emx n/a| -1 0 5 -48 -32 -14 .07 26 24 | -10097 -626 4077 8175
| 0 0 2 16 17 34 .05 | 17724 1517
esx n/a| 0 0 0 -53 32 5 -.07 19 15 | -9193 -2914 4457 9576
| 1 0 2 32 19 35 .05 | 5162 4546
gfz n/a| 1 0 4 65 57 71 -.03 23 17 | 0 -1491 3902 7580
| 1 1 1 30 19 27 .09 | 0 3148
grg n/a| 0 0 0 -9 53 -57 -.30 33 30 | 202617 -1139 4514 150713
| 2 2 6 33 28 33 .09 | 554371 3268
iac n/a| 0 1 -5 15 -51 -14 .11 23 23 | 203558 -229 4659 150858
| 1 1 1 46 36 41 .05 | 555684 2032
mcc n/a| 0 4 -17 34 -109 -184 .05 151 151 | --- --- --- ---
| 7 5 12 169 125 630 .41 | --- ---
Table 1.1902.b GPS week : 1902 MJD: 57558.0-57564.0
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 9 9 12 12 11 |
R02 | 7 6 8 7 8 8 8 |
R03 | 9 6 11 8 8 6 6 |
R04 | 6 9 7 6 8 7 7 |
R05 | 12 15 14 17 16 12 12 |
R06 | 9 10 10 9 10 10 8 |
R07 | 8 8 7 6 11 7 7 |
R08 | 8 7 6 8 8 8 6 |
R09 | 7 8 7 7 8 7 8 |
R10 | 12 40 896 50 16 12 11 |
R11 | --- --- --- --- --- 0 16 |
R12 | 21 25 30 24 26 23 22 |
R13 | 12 10 10 10 8 9 11 |
R14 | 20 17 18 19 18 19 17 |
R15 | 11 10 9 11 12 12 9 |
R16 | 13 14 13 13 13 15 17 |
R17 | 8 9 7 7 8 8 8 |
R18 | 8 7 8 7 8 6 6 |
R19 | 9 10 8 9 9 9 8 |
R20 | 11 12 15 12 13 13 12 |
R21 | 10 8 7 8 8 10 9 |
R22 | 9 8 8 8 10 9 8 |
R23 | 8 8 10 10 8 12 10 |
R24 | 11 12 11 11 13 15 16 |
R26 | --- --- --- --- 2544 39 25 |
Table 1.1902.c GPS week : 1902 MJD: 57558.0-57564.0
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 1902 0 | 56 -5 124 2013 704 5870 84.5 1330 1330 | -9668 0
brd 1902 1 | -17 10 146 168 926 7367 83.6 1465 1465 | -8232 0
brd 1902 2 | 3 -19 154 1213 797 6633 84.1 1444 1444 | -9822 0
brd 1902 3 | 39 24 258 -391 121 8182 82.4 1662 1662 | -4349 0
brd 1902 4 | 71 72 134 106 74 3719 81.8 1504 1504 | -6016 0
brd 1902 5 | -3 47 172 305 369 5080 82.5 1828 1828 | -9913 0
brd 1902 6 | 14 -41 172 399 916 4857 84.3 2595 2595 | -3668 0
-------------+------------------------------------------------------------+----------------
brd 1902 mean| 23 12 166 545 558 5958 83.3 1689 1689 | -7381 0
brd 1902 sdev| 33 39 44 805 365 1548 1.1 430 430 | 2682 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 2.1902.0 GPS week: 1902 Day: 0 MJD: 57558
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 1 0 73 -78 -7 .22 30 24 | --- --- --- ---
cof n/a| -3 0 -3 87 -83 -24 .23 34 26 | --- --- --- ---
emx n/a| -1 0 2 -59 -43 -23 .15 23 21 | -15256 -1140 3662 8729
esx n/a| -2 -1 -2 -89 40 -15 -.13 20 15 | -11775 -2692 3656 10025
gfz n/a| 2 0 2 48 47 81 .02 23 18 | 0 -974 3339 7627
grg n/a| 3 2 9 9 19 -29 -.34 34 32 | -9577 -880 3680 8615
iac n/a| 0 0 -3 59 -8 3 .10 21 21 | -9017 -979 3666 8182
mcc n/a| 14 10 -9 271 -123 -553 -.48 148 148 | --- --- --- ---
Table 2.1902.1 GPS week: 1902 Day: 1 MJD: 57559
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 0 61 -84 -41 .16 29 22 | --- --- --- ---
cof n/a| 0 -1 -1 48 -48 -48 .17 33 25 | --- --- --- ---
emx n/a| -1 0 4 -63 1 38 -.02 24 24 | -41452 200 3429 8716
esx n/a| -1 -1 0 -17 12 -12 -.04 21 18 | -12774 2669 5367 13457
gfz n/a| 3 0 3 26 66 19 -.02 26 20 | 0 387 3316 7730
grg n/a| -1 3 -3 -42 85 -8 -.29 28 25 | -7767 3465 5268 13670
iac n/a| -1 0 -3 30 -62 39 .19 22 22 | -5475 3252 5243 13979
mcc n/a| 3 0 -31 163 -249 -284 .81 165 165 | --- --- --- ---
Table 2.1902.2 GPS week: 1902 Day: 2 MJD: 57560
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 -2 43 -74 8 .14 31 22 | --- --- --- ---
cof n/a| -2 -1 -1 24 -101 0 .09 34 24 | --- --- --- ---
emx n/a| 0 0 8 -37 -43 24 .05 26 23 | 14587 1483 3852 9579
esx n/a| 0 0 2 -57 22 10 -.10 20 15 | -13993 -1912 4412 10791
gfz n/a| 1 1 5 48 28 95 -.11 25 16 | 0 -383 3788 8214
grg n/a| -2 -2 -5 44 65 -96 -.20 35 30 | -9637 -1024 4338 9480
iac n/a| 1 0 -5 20 3 -60 .15 24 24 | -7681 -1429 5397 10815
mcc n/a| -2 -1 -13 -171 18 -754 .09 212 212 | --- --- --- ---
Table 2.1902.3 GPS week: 1902 Day: 3 MJD: 57561
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 -2 105 -80 11 .21 32 24 | --- --- --- ---
cof n/a| -1 0 -6 74 -57 5 .13 38 27 | --- --- --- ---
emx n/a| 0 0 6 -50 -32 -11 .05 25 23 | -14110 415 4395 7706
esx n/a| 0 0 0 -72 46 0 .01 15 12 | -1000 88 4442 9004
gfz n/a| 2 0 7 91 46 71 .02 24 18 | 0 -342 3821 7060
grg n/a| -1 0 -8 -41 77 -37 -.42 36 32 | 1459800 868 4433 999999
iac n/a| 0 1 -6 29 -67 -16 .09 23 23 | 1463727 -1788 4432 999999
mcc n/a| -6 12 0 -184 70 -453 -.17 152 152 | --- --- --- ---
Table 2.1902.4 GPS week: 1902 Day: 4 MJD: 57562
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| -4 0 -3 23 -20 -47 .18 31 22 | --- --- --- ---
cof n/a| -3 2 -4 73 -31 7 .28 35 25 | --- --- --- ---
emx n/a| 0 -1 4 -36 -23 -37 .07 29 26 | 4378 -994 4227 6868
esx n/a| 0 0 0 -34 35 36 -.06 19 15 | -8351 -2287 4346 7296
gfz n/a| 2 0 4 112 72 100 .08 22 15 | 0 1288 4764 7097
grg n/a| 0 -4 2 -27 13 -93 -.38 36 30 | -6262 -267 4943 7412
iac n/a| 0 4 -5 -82 -100 -42 .08 24 24 | -5123 1735 4945 7222
mcc n/a| -4 4 -8 90 -267 -323 -.19 99 99 | --- --- --- ---
Table 2.1902.5 GPS week: 1902 Day: 5 MJD: 57563
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 -7 45 -60 35 .32 30 23 | --- --- --- ---
cof n/a| 1 -1 -9 -4 -39 33 .06 34 24 | --- --- --- ---
emx n/a| -1 1 6 -66 -41 -54 .12 28 26 | -13845 -3271 4605 7423
esx n/a| 0 -1 -2 -92 61 -44 -.09 20 18 | -3349 -11871 4613 7771
gfz n/a| 0 -1 6 81 56 60 -.17 20 14 | 0 -8191 4147 7175
grg n/a| 0 0 1 18 39 -59 -.29 35 33 | -6236 -6962 4592 7681
iac n/a| 1 1 -5 45 -53 33 .16 23 23 | -7213 -2314 4595 7637
mcc n/a| 5 2 -26 -16 -130 -79 .21 137 137 | --- --- --- ---
Table 2.1902.6 GPS week: 1902 Day: 6 MJD: 57564
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 -4 -13 -87 1 .27 34 24 | --- --- --- ---
cof n/a| -2 2 -6 -7 -65 -13 .14 36 26 | --- --- --- ---
emx n/a| 0 0 3 -22 -46 -40 .06 30 26 | -4983 -1080 4370 8209
esx n/a| 1 0 2 -12 5 64 -.11 15 14 | -13113 -4394 4366 8694
gfz n/a| 1 -1 4 47 86 73 -.02 22 16 | 0 -2223 4139 8161
grg n/a| -4 0 3 -27 70 -77 -.19 31 24 | -2001 -3174 4349 8139
iac n/a| 3 1 -8 6 -73 -58 .03 21 21 | -4311 -86 4341 8176
mcc n/a| -4 1 -33 92 -83 1160 .09 143 143 | --- --- --- ---
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 3.1902.0 GPS week: 1902 Day: 0 MJD: 57558
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 | 1147 23 24 27 20 23 28 14 --- 10 | 52 52 56 62 68 65 53 --- 55
R02 | 914 13 17 14 9 13 30 14 --- 7 | 53 53 54 53 58 66 46 --- 52
R03 | 2035 16 15 16 24 15 19 23 178 8 | 70 69 75 87 75 55 58 28 69
R04 | 1245 10 11 16 9 14 20 13 --- 6 | 55 56 67 58 45 44 43 --- 51
R05 | 1943 25 25 26 17 14 51 29 --- 12 | 42 46 69 66 55 59 59 --- 57
R06 | 1156 33 33 10 11 10 19 28 --- 9 | 47 47 51 43 51 52 47 --- 46
R07 | 2153 15 21 18 13 21 27 17 160 8 | 66 70 63 65 78 65 51 90 62
R08 | 767 15 17 15 13 9 35 12 --- 7 | 60 60 67 61 65 57 52 --- 59
R09 | 1986 17 18 19 10 16 15 9 --- 6 | 24 24 25 30 38 30 36 --- 29
R10 | 1140 21 26 23 18 36 31 25 --- 11 | 9999 9999 611 9999 771 9999 9999 --- 9999
R12 | 914 78 97 41 36 41 44 42 --- 21 | 86 96 52 76 68 51 57 --- 54
R13 | 1219 47 53 23 17 28 23 18 --- 12 | 72 79 44 54 39 28 33 --- 42
R14 | 1085 54 24 37 48 44 56 33 --- 20 | 46 63 39 80 69 42 43 --- 46
XR15 | 6369 16 22 21 28 --- 24 16 --- 10 | 40 44 47 54 --- 44 36 --- 41
R16 | 783 20 16 34 17 26 56 22 --- 13 | 62 62 62 61 63 54 62 --- 57
R17E | 1619 19 14 24 12 18 23 14 --- 8 | 29 28 29 29 33 22 22 --- 23
R18E | 1555 22 20 15 14 16 20 15 --- 7 | 36 35 22 26 26 20 28 --- 21
R19E | 806 25 19 22 14 20 22 14 --- 8 | 34 27 20 26 26 29 22 --- 20
R20E | 1166 16 26 20 19 25 48 22 --- 11 | 31 35 28 40 35 36 26 --- 25
R21E | 780 19 27 19 17 16 43 18 93 9 | 27 36 28 29 28 41 26 69 22
R22E | 1528 21 26 25 13 17 26 17 --- 8 | 35 45 40 32 29 37 30 --- 28
R23E | 929 19 57 16 16 14 25 19 --- 8 | 32 69 28 39 36 30 32 --- 29
R24E | 728 35 42 16 20 21 30 20 --- 10 | 37 43 24 32 28 40 25 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1330 30 34 23 20 23 34 21 148 |T 47 51 69 50 81 43 40 62 41
WRMS | 1330 24 26 21 15 18 32 21 148 |NE 55 58 92 60 110 50 48 59 51
MEDI | 1156 20 24 20 17 17 27 18 160 |MD 42 47 47 53 45 42 36 69 42
Table 3.1902.1 GPS week: 1902 Day: 1 MJD: 57559
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 | 1489 17 19 29 34 16 31 21 --- 11 | 30 36 37 35 31 53 39 --- 28
R02 | 789 14 17 13 7 14 10 13 --- 5 | 37 37 29 34 33 38 31 --- 31
R03 | 1066 8 11 12 12 15 16 15 180 6 | 45 44 44 39 53 47 34 23 41
R04 | 1795 10 13 22 14 12 27 23 --- 8 | 35 36 45 42 30 34 22 --- 32
R05 | 1435 30 39 33 15 25 57 31 --- 15 | 35 28 36 44 38 45 37 --- 33
R06 | 1144 29 32 12 16 13 25 29 --- 9 | 28 30 32 28 28 31 21 --- 24
R07 | 2000 14 14 12 7 29 18 16 154 7 | 34 36 34 35 57 31 32 203 35
R08 | 693 11 14 15 12 21 12 14 --- 6 | 37 42 41 28 53 41 32 --- 36
R09 | 3180 17 15 19 12 16 23 15 --- 7 | 26 24 29 26 30 29 33 --- 24
XR10 | 1871 47 74 --- 34 --- 516 765 --- 40 | 9999 9999 --- 9999 --- 9999 9999 --- 9999
R12 | 952 86 86 45 46 57 46 49 --- 25 | 81 83 44 62 61 50 52 --- 41
R13 | 1450 38 47 19 15 25 19 13 --- 10 | 61 68 48 41 36 36 31 --- 39
R14 | 1617 27 48 51 36 46 33 25 --- 16 | 33 67 39 63 60 33 42 --- 38
XR15 | 2006 10 11 27 19 --- 17 14 --- 9 | 33 42 40 44 --- 39 31 --- 34
R16 | 1374 38 37 25 29 39 30 23 --- 13 | 41 39 42 52 61 41 55 --- 43
R17E | 1783 21 15 17 23 19 28 15 --- 9 | 29 28 26 34 32 24 20 --- 23
R18E | 1731 19 17 17 10 20 15 14 --- 7 | 28 26 33 25 27 29 27 --- 23
R19E | 819 16 16 17 16 21 32 21 --- 9 | 30 32 24 31 32 35 26 --- 23
R20E | 1169 19 45 24 23 31 30 26 --- 11 | 20 54 29 45 41 41 25 --- 28
R21E | 708 18 19 17 14 14 25 10 160 7 | 26 26 22 24 30 33 27 129 22
R22E | 1439 19 12 17 11 22 21 13 --- 7 | 34 28 27 29 33 42 30 --- 27
R23E | 1028 17 18 18 18 14 20 21 --- 8 | 22 30 30 38 30 31 26 --- 25
R24E | 736 30 44 24 29 20 24 24 --- 11 | 38 52 31 45 31 31 31 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1465 29 33 24 21 26 28 22 165 |T 35 40 34 38 39 37 32 118 30
WRMS | 1465 22 25 24 18 20 25 22 165 |NE 39 43 38 40 43 39 35 113 34
MEDI | 1435 19 18 18 16 20 25 21 160 |MD 33 36 33 35 33 35 31 129 28
Table 3.1902.2 GPS week: 1902 Day: 2 MJD: 57560
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 | 1201 17 23 15 14 19 29 25 --- 9 | 40 36 43 39 55 60 31 --- 40
R02 | 595 24 26 9 19 13 21 15 --- 7 | 38 38 35 28 30 27 31 --- 27
R03 | 1987 9 12 14 19 15 61 13 142 10 | 48 56 64 67 52 29 51 37 50
R04 | 1776 7 11 17 8 13 30 13 --- 6 | 38 43 52 38 40 24 37 --- 37
R05 | 704 34 28 13 16 15 64 36 --- 13 | 40 52 43 56 53 39 45 --- 43
R06 | 858 23 28 20 14 11 32 32 --- 10 | 38 44 46 45 35 21 23 --- 33
R07 | 1291 13 18 14 14 13 20 18 293 6 | 46 46 56 60 56 41 41 149 50
R08 | 612 12 11 11 9 11 18 14 --- 5 | 46 51 59 57 57 46 43 --- 51
R09 | 3958 12 18 16 13 16 18 14 --- 6 | 26 24 26 22 29 23 28 --- 22
XR10 |14215 986 1155 --- --- --- --- 813 --- 895 | 9999 9999 --- --- --- --- 9999 --- 9999
R12 | 798 95 102 71 38 70 50 63 --- 29 | 89 110 63 64 76 49 60 --- 49
R13 | 1745 39 38 18 12 27 16 11 --- 10 | 54 52 36 30 33 39 30 --- 31
R14 | 1210 39 29 48 34 43 49 23 --- 17 | 45 46 33 65 54 31 38 --- 38
XR15 | 2702 19 20 16 18 --- 21 13 --- 8 | 35 33 39 45 --- 35 37 --- 36
R16 | 1138 23 37 25 34 27 36 25 --- 12 | 46 61 39 50 41 52 53 --- 40
R17E | 1154 23 23 13 12 16 22 12 --- 7 | 38 40 27 37 34 29 26 --- 29
R18E | 1336 20 18 17 10 12 32 15 --- 7 | 33 36 27 25 25 35 28 --- 23
R19E | 702 27 14 20 9 19 18 16 --- 8 | 35 30 25 26 29 32 25 --- 22
R20E | 1049 30 49 34 27 31 48 30 --- 14 | 39 52 39 40 42 49 27 --- 29
R21E | 775 17 25 14 13 18 16 14 169 7 | 30 36 22 26 28 26 30 126 23
R22E | 977 16 17 24 13 16 22 12 --- 7 | 34 31 31 28 28 34 30 --- 26
R23E | 1662 23 25 28 21 10 21 25 --- 10 | 25 26 35 34 30 28 32 --- 27
R24E | 680 25 30 20 21 28 34 21 --- 11 | 36 40 32 41 44 47 28 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1444 31 34 26 20 25 35 24 212 |T 40 44 39 41 41 36 35 104 34
WRMS | 1444 22 24 23 15 16 30 24 212 |NE 44 49 45 47 47 36 39 93 39
MEDI | 1154 23 25 17 14 16 22 16 169 |MD 38 40 36 39 40 34 31 126 31
Table 3.1902.3 GPS week: 1902 Day: 3 MJD: 57561
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 | 862 30 29 25 13 19 26 12 --- 9 | 37 46 64 57 69 44 59 --- 54
R02 | 723 19 15 15 11 11 18 23 --- 7 | 49 43 47 45 48 36 26 --- 40
R03 | 2310 16 18 23 10 12 36 12 137 8 | 61 57 70 55 63 33 51 24 55
R04 | 1248 13 7 15 9 14 24 11 --- 6 | 47 42 52 47 40 32 39 --- 42
R05 | 656 20 25 26 15 18 88 47 --- 17 | 33 44 46 47 44 38 41 --- 37
R06 | 698 31 23 17 13 16 26 21 --- 9 | 38 38 34 35 39 32 29 --- 30
R07 | 819 12 17 10 11 16 24 13 205 6 | 47 49 46 49 55 27 38 70 44
R08 | 726 10 21 11 9 17 38 15 --- 7 | 48 43 58 50 45 68 49 --- 50
R09 | 3461 18 23 19 7 15 23 14 --- 7 | 27 34 35 32 29 19 39 --- 28
XR10 |29864 270 71 --- 54 --- 70 93 --- 50 | 9999 9999 --- 9999 --- 9999 9999 --- 9999
R12 | 931 93 114 59 18 41 72 40 --- 23 | 99 120 70 58 61 44 50 --- 49
R13 | 1170 36 43 21 9 26 23 26 --- 10 | 64 71 55 49 45 57 37 --- 46
R14 | 1644 40 42 50 32 45 60 33 --- 19 | 53 73 30 74 69 38 38 --- 45
R15 | 3815 21 29 15 19 34 21 28 --- 10 | 37 42 45 52 7 33 39 --- 38
R16 | 978 23 31 38 24 32 27 18 --- 12 | 62 75 66 74 64 76 71 --- 64
R17E | 1036 22 23 15 11 20 22 11 --- 7 | 37 39 27 31 40 33 25 --- 27
R18E | 1931 23 35 14 10 15 18 17 --- 7 | 32 38 25 26 27 33 25 --- 22
R19E | 958 30 34 22 11 23 19 21 --- 9 | 38 40 24 32 37 30 30 --- 26
R20E | 1421 37 25 25 18 26 32 23 --- 11 | 47 54 43 53 46 47 34 --- 41
R21E | 1030 23 21 16 12 22 15 14 91 7 | 39 37 26 26 29 27 32 57 25
R22E | 1093 27 24 17 13 20 15 12 --- 7 | 39 38 30 29 27 34 32 --- 27
R23E | 2736 30 37 21 14 12 21 29 --- 9 | 21 22 20 26 21 22 29 --- 18
R24E | 762 22 56 22 19 27 28 29 --- 10 | 46 71 34 56 57 44 35 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1662 32 38 25 15 24 36 23 151 |T 45 50 43 45 43 38 38 50 38
WRMS | 1662 24 27 23 12 18 32 23 151 |NE 50 55 51 51 48 41 43 47 44
MEDI | 1036 23 25 19 13 19 24 21 137 |MD 39 43 43 47 44 33 37 57 40
Table 3.1902.4 GPS week: 1902 Day: 4 MJD: 57562
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 | 976 30 37 21 23 21 44 17 --- 11 | 36 35 64 73 66 45 46 --- 55
R02 | 578 13 12 11 11 20 28 16 --- 7 | 40 50 50 43 61 54 35 --- 44
R03 | 1576 13 7 16 13 17 28 12 130 7 | 53 59 58 57 75 78 61 27 61
R04 | 1069 16 23 19 19 9 26 14 --- 7 | 40 48 36 24 32 48 42 --- 32
R05 | 1088 16 20 30 24 18 61 50 --- 15 | 33 29 36 41 41 35 29 --- 28
R06 | 1641 34 35 21 9 12 30 29 --- 10 | 32 38 45 41 47 37 34 --- 37
R07 | 898 18 16 22 18 18 54 21 103 11 | 44 47 51 55 52 36 26 37 40
R08 | 628 12 15 13 20 9 31 19 --- 8 | 40 48 47 54 44 35 32 --- 41
R09 | 3365 15 15 15 9 14 34 21 --- 8 | 30 30 34 35 44 48 39 --- 35
XR10 |16499 29 35 --- 36 25 41 24 --- 15 | 9999 9999 --- 895 500 879 9999 --- 9999
R12 | 1223 82 81 78 19 55 55 50 --- 25 | 109 114 110 73 55 64 55 --- 65
R13 | 1308 28 35 16 12 21 18 13 --- 8 | 50 56 38 43 40 39 33 --- 37
R14 | 902 36 61 56 38 27 58 30 --- 18 | 44 86 48 64 47 44 41 --- 38
XR15 | 4998 20 18 15 28 --- 33 13 --- 11 | 30 34 33 35 --- 41 35 --- 30
R16 | 993 26 29 35 21 30 30 27 --- 12 | 57 60 36 59 48 54 49 --- 45
R17E | 1512 23 27 15 18 18 20 12 --- 8 | 31 35 19 32 34 26 22 --- 22
R18E | 2020 26 25 14 15 16 17 17 --- 8 | 30 30 17 24 28 25 24 --- 20
R19E | 924 27 48 24 10 22 15 14 --- 8 | 36 52 38 32 39 34 23 --- 28
R20E | 2325 40 48 35 26 22 33 21 --- 13 | 44 52 51 52 51 42 32 --- 39
R21E | 921 31 31 16 7 20 19 13 41 8 | 39 44 29 32 38 38 28 44 29
R22E | 688 32 28 20 11 21 32 17 --- 9 | 44 46 29 31 36 50 29 --- 30
R23E | 2509 27 24 16 17 14 17 15 --- 8 | 25 35 22 31 32 37 26 --- 24
R24E | 959 25 38 28 27 23 43 31 --- 13 | 38 48 44 52 39 31 28 --- 33
XR26E | ---- 2872 2837 --- --- --- --- 2255 --- 2544 | 9999 9999 --- --- --- --- 61 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1504 31 35 29 19 22 36 24 99 |T 42 48 42 81 65 79 36 36 36
WRMS | 1504 22 25 26 15 15 30 24 99 |NE 45 52 49 106 82 102 39 32 42
MEDI | 1088 26 28 19 18 20 31 17 103 |MD 39 47 38 43 44 41 33 37 35
Table 3.1902.5 GPS week: 1902 Day: 5 MJD: 57563
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 | 1380 27 34 33 26 22 35 26 --- 12 | 31 56 55 58 47 47 22 --- 38
R02 | 533 11 18 21 11 18 27 17 --- 7 | 38 42 52 49 33 23 34 --- 37
R03 | 789 12 11 6 17 7 25 12 138 6 | 44 50 59 67 59 43 52 31 55
R04 | 784 8 10 12 10 17 22 20 --- 7 | 35 37 39 34 54 44 26 --- 37
R05 | 800 31 39 18 18 12 40 39 --- 12 | 31 40 39 39 40 34 27 --- 30
R06 | 2491 37 32 12 16 11 22 30 --- 10 | 27 21 30 24 29 47 35 --- 28
R07 | 1175 8 16 15 16 13 19 12 182 6 | 41 49 53 40 47 63 46 91 45
R08 | 736 9 13 17 18 18 21 18 --- 7 | 36 39 41 46 37 45 23 --- 35
R09 | 3054 14 13 21 9 14 24 13 --- 7 | 25 27 32 26 28 33 24 --- 23
R10 | 5195 17 24 46 24 18 35 17 --- 12 | 9999 9999 495 9999 400 978 9999 --- 9999
XR11 | 7123 8 125 --- --- --- --- --- --- 0 | 194 221 --- --- --- --- --- --- 199
R12 | 1063 78 95 54 24 41 68 49 --- 23 | 94 123 59 56 64 55 49 --- 53
R13 | 1646 35 31 16 11 21 21 13 --- 9 | 58 53 52 50 36 31 33 --- 40
R14 | 1928 43 31 62 36 21 63 28 --- 18 | 36 41 53 60 42 25 36 --- 36
XR15 | 3049 15 24 21 21 --- 41 17 --- 11 | 42 39 38 52 --- 39 33 --- 36
R16 | 833 33 37 39 28 27 53 27 --- 15 | 66 64 56 72 62 53 60 --- 56
R17E | 1151 19 29 14 16 13 28 11 --- 7 | 27 32 19 27 20 27 21 --- 19
R18E | 1271 14 17 13 11 15 17 15 --- 6 | 22 26 23 26 24 23 24 --- 19
R19E | 1303 22 18 18 14 23 24 15 --- 8 | 33 32 24 30 34 32 24 --- 24
XR20E | 1053 28 32 33 17 24 --- 30 --- 13 | 51 62 55 49 57 --- 25 --- 42
R21E | 1021 30 30 23 16 16 27 19 65 9 | 37 37 29 32 32 38 27 48 25
R22E | 1041 30 24 21 11 21 22 12 --- 9 | 40 37 32 36 32 39 34 --- 31
R23E | 2398 29 32 19 25 16 51 19 --- 11 | 29 31 28 35 26 45 29 --- 24
R24E | 935 35 47 31 36 32 36 24 --- 14 | 26 51 41 56 45 32 30 --- 29
XR26E | ---- 44 198 --- --- --- --- 35 --- 39 | 9999 9999 --- --- --- --- 74 --- 740
------+---------------------------------------------------+-----------------------------------------------
RMS | 1828 30 34 28 20 20 35 23 137 |T 46 52 61 43 56 81 34 56 70
WRMS | 1828 23 24 26 18 14 33 23 137 |NE 53 60 76 48 69 104 35 61 49
MEDI | 1151 27 30 21 17 18 27 18 138 |MD 36 40 41 40 37 39 30 48 36
Table 3.1902.6 GPS week: 1902 Day: 6 MJD: 57564
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 | 1168 25 18 32 16 30 24 20 --- 10 | 53 57 64 65 77 63 54 --- 60
R02 | 587 14 19 21 11 9 35 12 --- 7 | 54 58 66 54 58 52 49 --- 54
R03 | 867 14 15 11 14 12 14 12 124 5 | 69 70 81 84 72 67 67 56 74
R04 | 1028 14 18 12 10 13 14 21 --- 6 | 51 55 63 59 60 59 42 --- 55
R05 | 1132 56 39 14 15 15 20 27 --- 11 | 40 46 52 63 67 55 54 --- 54
R06 | 1883 27 32 12 14 13 22 19 --- 8 | 49 48 53 46 51 47 48 --- 47
R07 | 1003 13 15 22 8 15 21 17 204 7 | 60 63 71 62 67 57 63 75 62
R08 | 1377 17 24 12 8 14 21 11 --- 6 | 54 57 58 59 55 58 52 --- 55
R09 | 2251 17 16 15 13 19 26 13 --- 7 | 18 24 19 25 31 26 21 --- 20
R10 |10588 26 25 23 23 17 29 22 --- 10 | 9999 9999 412 9999 476 9999 9999 --- 9999
XR11 | 2047 37 50 --- 22 24 29 --- --- 15 | 176 196 --- 13 5 6 --- --- 184
R12 | 933 95 108 56 11 31 53 48 --- 22 | 113 120 61 43 46 55 48 --- 45
R13 | 1205 30 37 25 13 36 22 14 --- 10 | 76 83 57 60 67 55 49 --- 57
R14 | 2132 36 41 60 27 27 55 25 --- 17 | 46 57 28 42 54 37 38 --- 35
XR15 | 3588 23 16 23 18 --- 15 12 --- 9 | 43 45 48 50 --- 51 51 --- 46
R16 | 743 37 41 53 25 29 54 36 --- 17 | 69 82 58 65 67 56 61 --- 57
R17E | 1384 28 22 17 9 19 19 12 --- 7 | 34 29 18 22 24 24 22 --- 19
R18E | 1164 15 14 13 10 15 14 13 --- 6 | 22 20 20 21 27 19 25 --- 20
R19E | 669 19 20 28 9 21 22 13 --- 8 | 34 36 35 28 36 29 27 --- 27
R20E | 809 27 24 34 16 30 34 15 --- 11 | 35 41 39 31 49 35 30 --- 29
R21E | 1372 29 40 14 10 25 24 14 64 8 | 38 43 22 29 39 35 26 38 26
R22E | 828 34 37 16 11 19 20 12 --- 8 | 42 46 26 26 31 32 28 --- 25
R23E | 1232 34 32 26 16 11 30 20 --- 10 | 25 30 25 28 22 26 24 --- 21
R24E | 1962 40 34 48 26 25 52 29 --- 16 | 36 54 70 54 53 33 40 --- 40
XR26E | ---- 32 59 --- --- --- --- 20 --- 25 | 866 885 --- --- --- --- 45 --- 413
------+---------------------------------------------------+-----------------------------------------------
RMS | 2595 34 36 30 15 22 31 21 143 |T 87 93 62 44 66 42 41 56 63
WRMS | 2595 24 26 26 14 16 24 21 143 |NE 64 70 79 52 83 49 49 65 60
MEDI | 1168 27 25 22 13 19 22 15 124 |MD 46 54 53 46 53 47 45 56 46
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