[IGSREPORT-26280] Wk 2028 IGLOS Final Orbits
acc
acc at igs.org
Mon Dec 10 15:05:35 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2028 (Nov 18, 2018 - Nov 24, 2018)
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 2.2028.
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:
igl2028[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2028 in the SP3 format.
igl20287.sum Combination Report for GPS Week 2028.
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
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.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 | 7.5 ns
1 | 7.5 ns
2 | 7.8 ns
3 | 7.9 ns
4 | 6.6 ns
5 | 4.3 ns
6 | 1.4 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2028, 1a.2028).
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 2.2028.0-6)
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 3.2028.0-6).
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 2028 summary. (Nov 18, 2018 - Nov 24, 2018)
Table 1.2028.a GPS week : 2028 MJD: 58440.0-58446.0
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| 0 -1 0 20 14 38 .09 22 18 | 4680 -712 3676 9871
| 1 0 1 18 6 21 .03 | 1259 2078
cof n/a| -1 -1 -1 22 11 32 .09 25 20 | 4673 -714 3672 9873
| 1 1 1 12 17 36 .05 | 1259 2082
emx n/a| 0 0 -1 -27 -35 3 -.01 22 22 | 1724 -1016 3626 9346
| 1 1 3 8 17 26 .02 | 8596 1818
esx n/a| 0 0 0 9 -11 37 .14 19 15 | 4512 -562 3649 11793
| 1 1 1 18 20 32 .04 | 10307 2425
gfz n/a| -1 0 0 18 26 32 .07 23 18 | 0 -807 3634 9415
| 1 1 2 20 20 33 .08 | 0 2266
grg n/a| 1 1 -4 -22 -14 -87 -.30 25 21 | 6640 -862 3672 9310
| 1 1 4 25 22 75 .04 | 1913 2153
iac n/a| 0 0 6 2 22 -49 -.04 24 23 | 7784 -561 4412 10462
| 0 0 1 29 52 64 .05 | 1743 1424
mcc n/a| 4 0 3 35 25 707 -.15 185 185 | --- --- --- ---
| 12 6 26 149 108 518 .53 | --- ---
Table 1.2028.b GPS week : 2028 MJD: 58440.0-58446.0
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 | 17 19 18 12 12 14 19 |
R02 | 8 6 8 6 7 7 7 |
R03 | 6 6 5 7 8 7 5 |
R04 | 6 7 5 6 6 8 8 |
R05 | 8 8 8 10 12 11 12 |
R07 | 7 6 7 6 6 6 7 |
R08 | 7 11 9 9 8 7 9 |
R09 | 8 7 6 7 5 7 6 |
R10 | 7 6 7 8 7 8 6 |
R11 | 8 7 8 8 7 9 8 |
R13 | 8 9 9 9 8 8 8 |
R14 | 9 9 7 8 8 9 8 |
R15 | 16 17 19 19 17 24 --- |
R16 | 14 13 11 14 15 14 16 |
R17 | 6 7 8 9 8 6 9 |
R18 | 8 7 6 7 8 7 8 |
R19 | 18 16 16 18 17 17 19 |
R20 | 15 12 12 12 13 13 13 |
R21 | 7 7 7 8 6 7 9 |
R22 | 7 7 7 8 7 8 8 |
R23 | 11 11 10 13 11 10 10 |
R24 | 12 14 11 13 10 13 13 |
R26 | 0 0 0 0 0 0 45 |
Table 1.2028.c GPS week : 2028 MJD: 58440.0-58446.0
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 2028 0 | 37 -45 93 -358 -2193 -8041 83.0 1778 1778 | 7525 0
brd 2028 1 | -32 13 46 -670 -1581 -2819 85.2 1848 1848 | 7480 0
brd 2028 2 | 23 -53 -35 -299 -1435 -639 81.9 2077 2077 | 7817 0
brd 2028 3 | -37 0 29 -878 -746 -819 83.3 1922 1922 | 7930 0
brd 2028 4 | 49 106 -22 145 -687 -1481 83.6 1491 1491 | 6562 0
brd 2028 5 | -115 -38 -133 -1939 -971 -5680 82.3 1456 1456 | 4273 0
brd 2028 6 | 97 -36 6 1723 891 -4099 84.2 1324 1324 | 1378 0
-------------+------------------------------------------------------------+----------------
brd 2028 mean| 3 -7 -2 -325 -960 -3368 83.4 1699 1699 | 6137 0
brd 2028 sdev| 70 56 72 1114 972 2754 1.1 278 278 | 2451 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 2.2028.0 GPS week: 2028 Day: 0 MJD: 58440
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 1 6 17 47 .07 24 22 | 5016 -77 2791 10045
cof n/a| -2 0 -1 13 -8 7 .12 27 23 | 5009 -71 2798 10050
emx n/a| 0 0 -1 -23 -43 -10 .02 24 24 | 2246 7 2783 9247
esx n/a| 0 -1 0 22 11 -15 .10 22 18 | 5052 153 2789 11915
gfz n/a| -2 -1 -3 34 29 -32 .17 22 14 | 0 -84 2790 9645
grg n/a| 0 2 0 -35 -16 -27 -.29 22 19 | 7688 -14 2797 9531
iac n/a| 2 0 3 -16 0 5 -.04 21 20 | 7867 1120 3849 10098
mcc n/a| 1 6 -20 0 104 175 -.38 162 162 | --- --- --- ---
Table 2.2028.1 GPS week: 2028 Day: 1 MJD: 58441
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 -1 30 22 2 .06 24 19 | 5007 -871 3252 10384
cof n/a| -1 0 -1 31 30 -12 .11 25 19 | 5000 -862 3252 10387
emx n/a| -3 0 -1 -28 -6 13 -.02 22 22 | 9706 -1086 3253 9759
esx n/a| 1 1 2 4 2 40 .13 20 16 | 15905 -614 3261 12123
gfz n/a| 1 -3 0 11 25 24 .09 23 16 | 0 -479 3253 9888
grg n/a| 0 2 -5 -43 -33 32 -.31 22 19 | 8228 -1209 3251 9920
iac n/a| 0 0 6 41 -25 -123 .01 24 24 | 7705 425 4033 10709
mcc n/a| -13 -4 1 111 -34 693 -.44 151 151 | --- --- --- ---
Table 2.2028.2 GPS week: 2028 Day: 2 MJD: 58442
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 0 -1 6 42 .05 23 21 | 3582 743 3561 9869
cof n/a| -2 0 -2 8 8 39 .16 26 23 | 3600 712 3556 9872
emx n/a| -1 0 -3 -21 -26 -22 -.00 21 21 | 4056 534 3545 9680
esx n/a| 0 0 1 14 -19 14 .13 17 14 | 9567 953 3556 11918
gfz n/a| -2 0 2 5 14 44 .05 24 19 | 0 32 3534 9575
grg n/a| 3 1 -10 -10 -2 -69 -.35 26 20 | 7749 394 3555 9036
iac n/a| 1 0 5 0 30 -56 .04 23 23 | 10230 197 4342 12449
mcc n/a| -9 -7 17 130 4 708 -.64 150 150 | --- --- --- ---
Table 2.2028.3 GPS week: 2028 Day: 3 MJD: 58443
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 35 15 57 .07 21 18 | 6217 716 3894 9369
cof n/a| -2 -2 1 8 6 81 .05 22 18 | 6215 699 3881 9365
emx n/a| 1 -2 -6 -26 -62 56 -.02 23 23 | -7263 221 3887 9063
esx n/a| 0 0 -2 32 -13 56 .12 19 16 | -4538 713 3880 11558
gfz n/a| -2 1 1 -15 14 64 .13 25 21 | 0 1014 3861 8914
grg n/a| 4 0 0 -20 -21 -172 -.27 30 20 | 7940 175 3967 9104
iac n/a| 2 0 7 -31 53 -67 -.05 23 23 | 9854 -1179 5045 9951
mcc n/a| 18 -6 55 54 236 1635 -.38 233 233 | --- --- --- ---
Table 2.2028.4 GPS week: 2028 Day: 4 MJD: 58444
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 33 7 64 .09 20 19 | 6150 -1434 3584 9634
cof n/a| -2 -1 0 32 39 57 .07 30 21 | 6136 -1437 3570 9634
emx n/a| 1 1 0 -20 -42 -13 -.03 22 22 | 6906 -1655 3579 9138
esx n/a| -2 0 0 -14 3 54 .12 18 15 | 17754 -1519 3604 11884
gfz n/a| -2 1 -1 15 20 45 .11 22 19 | 0 -1670 3571 9153
grg n/a| 2 0 -1 -34 -2 -75 -.24 26 21 | 7099 -919 3743 9167
iac n/a| 0 0 6 34 -21 -136 -.05 27 27 | 6974 -1864 3848 9324
mcc n/a| 19 -2 -6 -11 -60 56 .88 177 177 | --- --- --- ---
Table 2.2028.5 GPS week: 2028 Day: 5 MJD: 58445
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 0 41 19 25 .13 19 14 | 3765 914 3875 9241
cof n/a| 0 -1 -2 25 -5 -5 .04 24 19 | 3737 948 3871 9243
emx n/a| -1 -1 3 -44 -28 -6 -.05 20 20 | 9200 -375 3776 8613
esx n/a| 0 1 -2 -14 -11 27 .19 16 13 | -6517 1853 3875 10844
gfz n/a| 0 0 -2 38 71 62 -.04 24 17 | 0 1037 3877 8815
grg n/a| 0 0 -9 -42 22 -132 -.30 27 23 | 3674 977 3807 8406
iac n/a| 0 1 9 18 -4 8 -.09 25 25 | 6406 202 4263 8913
mcc n/a| 5 4 -3 -251 -18 777 .22 223 223 | --- --- --- ---
Table 2.2028.6 GPS week: 2028 Day: 6 MJD: 58446
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 0 -1 10 28 .12 23 16 | 3027 -4976 4775 10560
cof n/a| 0 -2 -2 39 8 58 .05 23 17 | 3014 -4988 4778 10561
emx n/a| 0 -2 1 -26 -40 9 .01 25 25 | -12782 -4762 4560 9923
esx n/a| 0 1 0 24 -51 84 .21 22 15 | -5636 -5474 4580 12315
gfz n/a| -3 0 -3 37 13 15 -.01 24 17 | 0 -5499 4553 9915
grg n/a| 2 1 0 28 -45 -166 -.33 25 23 | 4104 -5440 4587 10006
iac n/a| 0 0 5 -29 123 22 -.07 22 22 | 5458 -2828 5505 11790
mcc n/a| 9 5 -16 215 -52 903 -.34 201 201 | --- --- --- ---
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 3.2028.0 GPS week: 2028 Day: 0 MJD: 58440
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 | 692 52 56 31 53 22 24 36 --- 17 | 96 103 84 68 81 65 49 --- 68
R02 | 924 14 14 15 29 18 12 10 131 7 | 62 61 56 50 65 53 44 154 53
R03 | 784 13 15 8 15 13 10 13 240 5 | 68 70 61 61 63 65 49 54 60
R04 | 961 13 15 10 11 12 10 18 --- 5 | 58 59 54 55 61 50 43 --- 53
R05 | 955 14 16 22 17 22 10 18 --- 8 | 52 51 57 51 49 44 41 --- 45
R07 | 736 13 15 12 14 19 16 17 --- 7 | 69 69 69 56 58 68 56 --- 61
R08 | 1124 13 16 12 19 13 15 21 --- 7 | 81 83 78 87 89 82 76 --- 81
R09 | 3774 11 12 11 21 14 26 9 --- 7 | 57 56 55 54 56 61 59 --- 56
R10 | 3253 12 11 17 18 13 15 16 --- 6 | 61 59 43 63 52 52 46 --- 52
R11 | 826 17 15 18 13 11 15 22 145 7 | 62 59 42 56 63 42 41 59 50
R13 | 2861 21 25 16 11 12 22 19 --- 7 | 68 73 54 60 55 45 43 --- 53
R14 | 664 24 26 21 11 12 25 14 --- 8 | 65 69 50 53 60 41 44 --- 50
R15 | 1958 44 45 23 40 45 20 36 --- 16 | --- --- --- --- --- --- --- --- 0
R16 | 1079 32 39 50 18 29 28 28 --- 14 | 70 85 53 76 82 73 58 --- 66
R17E | 1169 12 11 15 14 9 11 13 --- 5 | 59 60 58 60 65 59 61 --- 59
R18E | 1021 10 16 18 21 15 17 17 --- 7 | 25 28 26 36 33 32 27 --- 27
R19E | 2456 43 46 50 32 44 39 31 --- 18 | 48 62 50 70 72 61 65 --- 55
R20E | 1325 28 23 37 21 42 38 21 --- 14 | 29 36 44 48 58 48 37 --- 38
R21E | 1037 15 19 20 16 11 15 16 95 7 | 27 30 32 30 32 33 34 65 31
R22E | 1449 14 30 23 11 13 15 12 --- 6 | 43 47 42 46 45 47 46 --- 43
R23E | 1772 23 20 23 20 23 32 19 --- 10 | 65 68 59 71 68 64 57 --- 62
R24E | 2878 26 35 25 19 23 34 23 --- 11 | 48 59 50 55 56 68 56 --- 53
XR26E | 3698 --- --- --- --- --- --- 2 --- 0 | --- --- --- --- --- --- 59 --- 62
------+---------------------------------------------------+-----------------------------------------------
RMS | 1777 24 27 24 22 22 22 21 162 |T 57 61 53 57 60 54 49 83 53
WRMS | 1777 22 23 24 18 14 19 20 162 |NE 66 69 58 60 64 57 49 89 57
MEDI | 1124 14 16 18 18 14 16 18 131 |MD 61 60 54 56 60 53 46 59 53
Table 3.2028.1 GPS week: 2028 Day: 1 MJD: 58441
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 | 1141 58 62 44 43 34 23 39 --- 18 | 64 70 58 43 45 43 32 --- 40
R02 | 786 11 19 11 16 9 14 16 93 6 | 44 48 44 35 38 47 34 111 38
R03 | 618 16 14 11 16 9 9 7 189 5 | 50 47 47 40 44 43 41 17 42
R04 | 1140 12 15 12 14 18 15 13 --- 6 | 45 44 43 36 47 34 33 --- 38
R05 | 790 18 14 19 11 19 23 11 --- 8 | 40 39 41 37 42 22 37 --- 34
R07 | 578 12 9 15 10 13 10 21 --- 6 | 54 51 57 48 52 50 38 --- 49
R08 | 627 18 16 19 26 27 14 38 --- 11 | 73 74 74 85 91 80 66 --- 77
R09 | 4534 10 18 14 14 15 18 12 --- 6 | 50 55 50 51 59 49 57 --- 52
R10 | 4110 10 14 13 11 14 12 16 --- 5 | 42 45 33 43 41 34 34 --- 36
R11 | 1038 19 18 15 17 15 12 15 147 7 | 46 45 32 39 41 33 31 46 35
R13 | 843 23 20 18 9 14 15 32 --- 8 | 52 49 41 43 51 34 34 --- 41
R14 | 506 21 16 16 15 18 25 18 --- 8 | 45 41 38 43 40 20 30 --- 34
R15 | 2672 45 43 24 35 45 25 50 --- 17 | --- --- --- --- --- --- --- --- 0
R16 | 679 17 29 31 23 23 41 21 --- 12 | 50 67 45 55 59 52 46 --- 48
R17E | 1092 13 17 14 12 17 17 12 --- 6 | 64 65 65 71 75 70 60 --- 67
R18E | 1095 15 12 16 21 13 19 9 --- 7 | 25 25 22 30 25 29 20 --- 22
R19E | 3032 49 45 32 22 44 23 38 --- 16 | 38 49 47 52 62 55 52 --- 41
R20E | 1314 16 22 35 15 24 35 26 --- 11 | 28 33 31 33 43 41 32 --- 29
R21E | 1107 17 23 21 10 13 18 12 159 7 | 29 32 32 30 31 30 26 35 28
R22E | 1380 14 15 24 15 11 10 15 --- 7 | 37 43 38 52 41 41 34 --- 39
R23E | 1136 21 22 18 18 33 25 22 --- 10 | 36 41 41 43 36 49 36 --- 37
R24E | 2299 27 20 23 31 33 38 30 --- 13 | 65 62 69 74 79 65 57 --- 64
XR26E | 3304 --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 64 --- 61
------+---------------------------------------------------+-----------------------------------------------
RMS | 1847 24 25 22 20 23 22 24 151 |T 46 48 45 46 49 43 40 52 43
WRMS | 1847 19 19 22 16 16 19 24 151 |NE 50 51 46 46 50 41 39 58 43
MEDI | 1107 17 18 18 15 17 18 16 147 |MD 45 47 43 43 44 43 34 35 39
Table 3.2028.2 GPS week: 2028 Day: 2 MJD: 58442
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 | 848 48 36 51 40 36 18 27 --- 17 | 78 73 78 43 56 57 46 --- 55
R02 | 940 8 12 14 15 12 21 32 86 8 | 50 53 45 55 54 64 27 76 47
R03 | 1041 6 9 9 8 7 9 18 139 4 | 50 53 50 50 50 56 36 29 48
R04 | 818 6 5 6 9 11 19 16 --- 5 | 49 49 49 51 52 44 59 --- 49
R05 | 708 18 19 19 11 18 24 7 --- 7 | 48 51 54 45 44 32 48 --- 44
R07 | 840 14 16 12 11 25 11 16 --- 7 | 51 55 55 50 72 58 45 --- 53
R08 | 453 16 18 15 15 14 14 32 --- 8 | 58 60 68 68 66 78 51 --- 64
R09 | 4324 17 19 12 8 20 10 11 --- 6 | 36 36 37 32 36 34 32 --- 32
R10 | 4239 8 12 17 10 15 15 18 --- 6 | 53 55 41 56 60 57 48 --- 51
R11 | 1263 12 19 20 10 30 15 16 140 8 | 51 54 40 47 68 40 40 36 46
R13 | 1779 31 35 16 21 10 19 16 --- 9 | 61 64 37 51 41 31 35 --- 42
R14 | 997 16 20 14 14 15 16 18 --- 7 | 55 61 44 49 63 52 44 --- 50
R15 | 3685 46 51 23 35 54 42 55 --- 19 | --- --- --- --- --- --- --- --- 0
R16 | 464 21 27 28 19 28 38 20 --- 11 | 47 49 37 59 69 54 48 --- 49
R17E | 1515 17 15 21 10 24 19 11 --- 7 | 62 61 61 57 66 51 56 --- 57
R18E | 1314 9 56 17 11 13 21 14 --- 6 | 22 64 25 30 25 35 23 --- 24
R19E | 4471 45 26 36 16 36 48 27 --- 15 | 38 43 48 47 56 64 47 --- 42
R20E | 1459 16 32 21 20 29 33 33 --- 11 | 32 45 37 47 50 41 30 --- 34
R21E | 887 11 12 18 8 19 20 15 208 6 | 24 30 31 30 37 34 25 36 27
R22E | 879 16 28 20 11 17 19 10 --- 7 | 33 36 30 29 38 32 32 --- 30
R23E | 888 21 15 19 16 20 42 17 --- 10 | 30 38 31 47 44 43 35 --- 35
R24E | 2325 15 22 21 18 19 47 14 --- 10 | 40 48 52 50 52 53 40 --- 44
XR26E | 3590 --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 49 --- 50
------+---------------------------------------------------+-----------------------------------------------
RMS | 2077 23 26 21 17 24 26 23 150 |T 46 51 45 47 52 48 40 44 44
WRMS | 2077 21 23 21 14 19 20 23 150 |NE 52 54 48 50 56 50 43 47 48
MEDI | 1041 16 19 18 11 19 19 16 139 |MD 49 53 44 49 52 51 40 36 46
Table 3.2028.3 GPS week: 2028 Day: 3 MJD: 58443
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 | 783 30 32 24 22 20 37 27 --- 12 | 83 90 80 77 80 52 58 --- 70
R02 | 1013 11 13 10 9 15 11 16 149 5 | 54 56 54 54 58 45 38 32 50
R03 | 1137 9 9 13 13 18 14 24 92 7 | 56 50 55 61 69 66 40 46 57
R04 | 881 5 10 13 11 16 10 17 --- 5 | 46 48 53 52 55 45 36 --- 47
R05 | 695 28 35 25 16 14 20 29 --- 10 | 58 67 64 53 52 32 32 --- 47
R07 | 592 13 11 10 10 20 8 13 394 5 | 54 52 61 57 64 61 56 313 57
R08 | 841 18 15 18 20 14 17 24 --- 8 | 55 57 57 73 72 72 54 --- 63
R09 | 3354 15 17 14 18 21 13 13 --- 7 | 26 27 23 18 37 22 22 --- 21
R10 | 2714 10 10 21 13 18 21 19 --- 7 | 49 51 31 44 60 60 33 --- 44
R11 | 1204 12 13 21 7 25 17 21 176 7 | 59 61 37 53 69 52 39 41 50
R13 | 3563 30 29 18 12 24 17 15 --- 9 | 61 60 36 50 46 37 39 --- 43
R14 | 1341 21 13 21 13 19 14 15 --- 7 | 56 53 38 49 56 53 45 --- 47
R15 | 2352 42 44 36 35 44 43 52 --- 18 | --- --- --- --- --- --- --- --- 0
R16 | 608 21 26 37 24 20 52 19 --- 13 | 36 43 36 57 52 44 46 --- 42
R17E | 810 17 18 17 22 22 16 16 --- 8 | 47 45 49 65 58 49 43 --- 50
R18E | 1491 9 11 19 13 15 23 19 --- 7 | 19 19 21 28 26 27 24 --- 21
R19E | 4770 33 31 37 31 47 62 33 --- 18 | 58 59 53 48 96 100 49 --- 58
R20E | 1045 17 18 25 19 31 43 19 --- 11 | 27 27 31 34 32 45 30 --- 25
XR21E | 1074 19 15 17 10 17 --- 17 221 8 | 26 26 28 31 32 --- 23 48 26
R22E | 1461 19 15 21 12 21 22 14 --- 8 | 36 45 34 34 39 52 31 --- 34
R23E | 868 31 20 27 23 24 42 20 --- 12 | 35 46 38 48 53 67 41 --- 40
R24E | 1497 13 21 22 28 45 37 26 --- 13 | 51 51 46 57 71 74 55 --- 52
XR26E | 3567 --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 35 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1922 21 22 23 19 25 30 23 233 |T 47 49 44 49 56 52 39 96 44
WRMS | 1922 18 18 23 16 21 20 23 233 |NE 53 55 48 53 59 49 41 108 49
MEDI | 1137 17 15 21 13 20 20 19 176 |MD 51 51 38 52 56 52 39 46 47
Table 3.2028.4 GPS week: 2028 Day: 4 MJD: 58444
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 | 592 26 31 25 27 33 23 23 --- 12 | 83 91 61 75 108 69 75 --- 76
R02 | 1399 11 8 11 13 18 17 25 242 7 | 52 48 45 51 57 45 36 73 47
R03 | 923 14 18 20 10 13 17 27 190 7 | 58 62 57 53 55 43 36 49 50
R04 | 612 6 10 18 10 11 8 24 --- 6 | 51 50 55 42 51 48 36 --- 46
R05 | 539 24 27 29 23 15 19 47 --- 12 | 53 56 58 54 54 37 37 --- 45
R07 | 1054 13 11 11 11 17 14 17 179 6 | 57 60 63 61 69 64 48 192 60
R08 | 1021 17 18 9 18 21 21 16 --- 8 | 62 58 64 58 76 75 64 --- 65
R09 | 2628 11 13 11 12 13 12 13 --- 5 | 34 36 32 37 36 43 33 --- 35
R10 | 1324 9 10 16 12 12 17 19 --- 6 | 49 42 38 49 51 51 34 --- 45
R11 | 1100 16 15 13 11 10 16 22 94 6 | 50 48 37 39 44 35 33 55 38
R13 | 1820 26 26 21 14 13 13 19 --- 8 | 63 61 48 50 50 51 39 --- 49
R14 | 971 16 21 23 15 20 12 21 --- 8 | 58 62 42 57 61 50 50 --- 52
R15 | 2041 40 41 31 34 29 42 55 --- 17 | --- --- --- --- --- --- --- --- 0
R16 | 579 29 38 36 17 23 59 22 --- 15 | 38 37 28 39 40 30 43 --- 31
R17E | 629 17 19 18 16 21 14 14 --- 7 | 41 51 37 52 60 44 44 --- 45
R18E | 767 10 17 14 12 22 16 23 --- 7 | 25 32 26 27 38 37 24 --- 27
R19E | 4472 37 80 32 30 48 47 36 --- 17 | 40 120 53 47 75 78 58 --- 51
R20E | 772 19 22 23 26 34 33 40 --- 13 | 45 48 44 51 53 53 44 --- 42
R21E | 955 12 14 19 11 12 17 12 147 6 | 33 32 32 33 35 33 37 39 31
R22E | 760 8 9 21 8 13 24 12 --- 6 | 26 29 26 28 29 27 25 --- 24
R23E | 521 24 58 29 23 23 26 24 --- 11 | 38 62 48 42 48 57 36 --- 41
R24E | 966 17 36 25 14 25 28 30 --- 10 | 42 55 41 44 61 56 36 --- 43
XR26E | 3877 --- --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- 54 --- 55
------+---------------------------------------------------+-----------------------------------------------
RMS | 1490 20 30 22 18 22 26 27 177 |T 47 54 44 47 54 48 41 81 45
WRMS | 1490 19 21 22 15 19 21 27 177 |NE 54 54 48 51 57 49 43 92 49
MEDI | 966 16 18 20 14 18 17 22 179 |MD 49 51 44 49 53 48 37 55 45
Table 3.2028.5 GPS week: 2028 Day: 5 MJD: 58445
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 | 1157 34 39 32 24 16 39 37 --- 13 | 76 80 63 69 70 48 56 --- 63
R02 | 1337 8 26 10 12 12 17 26 296 6 | 47 63 41 55 51 46 33 123 45
R03 | 653 13 16 12 15 12 18 27 166 7 | 51 56 50 54 46 40 34 35 46
R04 | 829 7 17 11 17 19 17 29 --- 7 | 46 53 47 54 53 44 35 --- 46
R05 | 632 12 10 23 17 22 20 43 --- 10 | 38 35 47 36 54 40 19 --- 36
R07 | 772 8 8 10 11 20 13 11 333 5 | 51 48 52 46 46 55 45 139 48
R08 | 935 17 16 14 15 17 13 14 --- 6 | 53 61 58 69 65 72 58 --- 61
R09 | 3211 10 19 13 10 14 22 21 --- 6 | 24 29 31 28 35 24 44 --- 28
R10 | 1604 8 12 18 12 19 31 14 --- 7 | 38 45 36 45 53 36 41 --- 39
R11 | 912 13 19 17 12 29 24 21 110 8 | 40 44 39 30 54 27 32 56 35
R13 | 1289 16 28 19 8 16 21 31 --- 8 | 58 65 48 51 62 65 41 --- 52
R14 | 1167 19 25 13 14 19 27 24 --- 8 | 53 53 49 51 55 39 44 --- 47
XR15 | 1293 45 46 --- 31 38 --- 52 --- 23 | --- --- --- --- --- --- --- --- 0
R16 | 1152 15 32 26 26 23 62 23 --- 13 | 40 44 41 53 41 32 45 --- 40
R17E | 1039 13 11 20 8 15 12 11 --- 6 | 24 26 27 27 32 24 29 --- 25
R18E | 799 11 20 13 11 13 18 23 --- 6 | 25 28 25 29 30 29 27 --- 26
R19E | 3598 45 38 29 31 49 33 31 --- 16 | 34 41 47 49 77 45 53 --- 43
R20E | 888 32 45 25 18 38 25 35 --- 13 | 33 48 40 46 60 62 43 --- 41
R21E | 814 15 15 18 12 11 24 14 106 7 | 48 44 46 46 47 31 46 39 44
R22E | 1246 11 14 22 11 22 27 17 --- 8 | 24 25 25 31 37 31 23 --- 25
R23E | 572 21 10 26 15 24 32 16 --- 10 | 27 31 34 37 39 37 35 --- 31
R24E | 1522 24 38 22 22 41 33 33 --- 13 | 34 52 37 51 70 37 30 --- 39
XR26E | 4207 --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 59 --- 55
------+---------------------------------------------------+-----------------------------------------------
RMS | 1455 19 24 20 16 24 27 25 223 |T 41 46 42 45 51 41 39 78 41
WRMS | 1455 14 19 20 13 17 23 25 223 |NE 47 52 46 49 52 43 40 88 45
MEDI | 1152 13 19 18 14 19 24 23 166 |MD 40 45 41 46 53 39 41 56 41
Table 3.2028.6 GPS week: 2028 Day: 6 MJD: 58446
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 | 1833 55 51 40 36 55 24 29 --- 18 | 99 101 80 67 85 72 55 --- 73
R02 | 737 8 9 19 14 15 15 16 329 6 | 65 67 48 65 67 65 49 173 59
R03 | 906 10 10 14 12 9 11 10 178 5 | 70 72 67 66 69 66 56 45 65
R04 | 1053 10 12 13 18 15 10 26 --- 7 | 68 67 67 64 73 62 48 --- 63
R05 | 1075 26 21 34 26 26 25 15 --- 11 | 64 61 67 52 57 44 35 --- 50
R07 | 534 10 14 14 17 16 14 13 --- 6 | 63 63 63 64 65 67 59 --- 62
R08 | 1457 18 23 11 21 24 31 12 --- 9 | 65 63 66 79 82 67 69 --- 70
R09 | 2771 11 11 13 9 15 11 13 --- 5 | 48 45 51 48 49 48 56 --- 48
R10 | 1667 9 12 21 9 10 14 14 --- 6 | 62 64 47 63 64 65 54 --- 58
R11 | 621 14 11 13 13 18 31 18 117 8 | 59 58 45 56 61 41 40 68 49
R13 | 920 13 14 15 15 11 26 15 --- 7 | 73 71 58 64 57 49 54 --- 58
R14 | 729 15 14 18 13 11 21 21 --- 7 | 65 65 50 55 64 60 50 --- 56
R16 | 988 34 38 40 24 29 53 27 --- 16 | 65 57 50 70 58 55 59 --- 58
R17E | 1601 17 14 16 19 21 16 25 --- 8 | 39 43 46 47 48 51 44 --- 43
R18E | 930 9 14 19 11 24 24 14 --- 7 | 33 33 33 37 35 44 31 --- 33
R19E | 1776 42 35 56 44 40 28 41 --- 19 | 57 64 83 67 83 66 54 --- 61
R20E | 929 25 32 23 17 32 33 34 --- 12 | 29 32 44 36 43 56 40 --- 33
R21E | 1190 16 12 21 19 14 16 25 94 8 | 60 59 61 56 58 56 52 28 55
R22E | 794 13 13 18 12 17 26 17 --- 7 | 53 54 48 57 64 53 54 --- 54
R23E | 877 25 25 21 22 20 17 24 --- 9 | 59 60 56 66 68 56 61 --- 59
R24E | 1976 26 30 26 36 23 31 29 --- 13 | 75 76 67 72 67 67 60 --- 63
XR26E | 3261 41 43 --- --- --- --- 47 --- 44 | 4 4 --- --- --- --- 53 --- 72
------+---------------------------------------------------+-----------------------------------------------
RMS | 1323 23 23 25 21 24 25 22 201 |T 57 58 57 59 62 57 51 78 56
WRMS | 1323 16 17 25 15 17 23 22 201 |NE 66 65 58 62 65 58 52 95 59
MEDI | 988 15 14 19 17 18 24 18 117 |MD 62 61 56 64 64 56 54 45 58
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