[IGSREPORT-24547] Wk 1900 IGLOS Final Orbits
IGS ACC
acc at igs.org
Sat Jun 25 19:07:09 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1900 (Jun 05, 2016 - Jun 11, 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 2.1900.
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:
igl1900[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1900 in the SP3 format.
igl19007.sum Combination Report for GPS Week 1900.
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 | -3.6 ns
1 | -5.7 ns
2 | -5.0 ns
3 | -6.0 ns
4 | -7.1 ns
5 | -4.9 ns
6 | -4.5 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 1.1900, 1a.1900).
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 2.1900.0-6)
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 3.1900.0-6).
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 1900 summary. (Jun 05, 2016 - Jun 11, 2016)
Table 1.1900.a GPS week : 1900 MJD: 57544.0-57550.0
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 7 65 -57 12 .15 34 30 | --- --- --- ---
| 1 1 2 12 17 53 .03 | --- ---
cof n/a| 0 0 6 45 -48 -2 .18 37 31 | --- --- --- ---
| 1 1 3 32 45 62 .09 | --- ---
emx n/a| -1 0 5 -56 -35 -84 .14 29 26 | -7294 -502 4361 8267
| 1 1 2 22 43 59 .04 | 5216 1157
esx n/a| 0 -1 -1 -12 -15 -6 -.11 21 17 | -10261 -1106 4361 9524
| 0 1 1 11 14 64 .03 | 3102 2248
gfz n/a| 0 0 -1 29 49 38 .00 23 17 | 0 -986 3869 7302
| 1 1 1 26 29 38 .07 | 0 1606
grg n/a| 0 2 -1 -39 105 111 -.20 96 92 | -5175 -1041 4363 8223
| 1 2 6 22 46 289 .10 | 1309 1820
iac n/a| 0 0 -3 4 -10 33 .03 21 21 | -4016 -1194 4345 7987
| 1 1 1 18 44 103 .03 | 1677 1132
mcc n/a| 4 0 11 81 -54 680 -.16 110 110 | --- --- --- ---
| 5 4 23 138 122 347 .32 | --- ---
Table 1.1900.b GPS week : 1900 MJD: 57544.0-57550.0
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 | 12 8 10 10 12 11 21 |
R02 | 8 7 7 9 7 10 20 |
R03 | 8 8 8 8 9 8 20 |
R04 | 7 7 8 8 7 7 20 |
R05 | 14 13 14 15 13 13 21 |
R06 | 10 10 9 9 9 9 20 |
R07 | 9 7 8 8 7 9 21 |
R08 | 7 7 8 10 10 8 20 |
R09 | 13 23 14 10 24 11 21 |
R10 | 9 7 8 9 8 11 21 |
R12 | 24 25 21 25 20 20 32 |
R13 | 12 11 10 10 10 10 22 |
R14 | 19 16 19 15 15 22 28 |
R15 | 9 7 8 9 10 12 25 |
R16 | 15 12 14 15 12 14 24 |
R17 | 9 10 9 9 8 10 22 |
R18 | 9 9 7 9 8 8 22 |
R19 | 9 9 9 8 9 8 21 |
R20 | 16 14 12 12 13 12 22 |
R21 | 8 9 10 9 9 8 21 |
R22 | 9 9 10 11 10 9 21 |
R23 | 10 10 9 10 11 9 21 |
R24 | 12 10 12 14 15 14 25 |
Table 1.1900.c GPS week : 1900 MJD: 57544.0-57550.0
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 1900 0 | 41 -63 106 1062 640 5909 84.4 1632 1632 | -3599 0
brd 1900 1 | 73 26 128 62 1933 5182 84.8 1456 1456 | -5734 0
brd 1900 2 | 32 -64 124 8 979 5406 83.0 63500 63500 | -5033 0
brd 1900 3 | -63 -11 60 189 804 6356 82.9 1499 1499 | -5975 0
brd 1900 4 | 22 -15 201 -1104 535 4240 83.4 1392 1392 | -7093 0
brd 1900 5 | 47 31 106 422 96 7432 85.2 1530 1530 | -4927 0
brd 1900 6 | -41 2 41 -8 730 4155 85.3 1562 1562 | -4550 0
-------------+------------------------------------------------------------+----------------
brd 1900 mean| 16 -13 110 90 817 5525 84.1 10367 10367 | -5273 0
brd 1900 sdev| 49 38 51 646 563 1164 1.0 23429 23429 | 1119 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 2.1900.0 GPS week: 1900 Day: 0 MJD: 57544
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 10 82 -43 0 .14 39 35 | --- --- --- ---
cof n/a| 0 1 12 46 -18 -49 .33 38 35 | --- --- --- ---
emx n/a| -1 0 3 -84 -67 -123 .23 30 28 | -4702 -724 4493 8104
esx n/a| 0 -1 0 -2 -27 -68 -.11 19 14 | -5464 -3322 4469 9450
gfz n/a| -2 1 -3 -5 30 58 .02 24 22 | 0 598 3811 7537
grg n/a| 1 0 2 -3 73 75 -.25 32 29 | -3473 -855 4457 8193
iac n/a| 0 0 -4 16 12 91 .07 21 21 | -621 -2770 4400 7850
mcc n/a| 8 3 27 -157 26 1132 .03 97 97 | --- --- --- ---
Table 2.1900.1 GPS week: 1900 Day: 1 MJD: 57545
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 2 9 46 -46 -32 .16 35 30 | --- --- --- ---
cof n/a| 2 0 9 -3 8 -39 .10 41 32 | --- --- --- ---
emx n/a| 0 0 1 -80 40 -94 .15 28 26 | -8647 -2374 4584 8782
esx n/a| 0 -1 0 -8 7 -108 -.11 26 19 | -9059 -2640 4550 10185
gfz n/a| 0 -1 -1 30 62 11 -.09 21 13 | 0 -4336 3842 6584
grg n/a| 0 4 0 -62 118 90 -.22 37 30 | -5617 -2983 4536 8883
iac n/a| 1 0 -5 26 -88 121 .02 19 19 | -4509 -2117 4478 8401
mcc n/a| 8 -5 26 157 -183 1103 .04 80 80 | --- --- --- ---
Table 2.1900.2 GPS week: 1900 Day: 2 MJD: 57546
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 -2 8 77 -72 21 .14 32 27 | --- --- --- ---
cof n/a| -1 -1 6 107 -134 30 .16 35 29 | --- --- --- ---
emx n/a| 1 0 2 -42 -12 -31 .16 28 26 | -10045 104 3954 8512
esx n/a| 0 -1 0 0 -28 26 -.16 17 15 | -13439 -432 3940 9469
gfz n/a| -2 0 -3 27 21 104 .10 24 21 | 0 -708 3739 7463
grg n/a| 0 2 6 -30 111 22 -.27 34 27 | -4733 -714 3969 8539
iac n/a| 0 0 -3 -19 12 -110 .02 20 20 | -3746 -383 3945 8523
mcc n/a| -1 -1 14 156 -49 383 -.04 92 92 | --- --- --- ---
Table 2.1900.3 GPS week: 1900 Day: 3 MJD: 57547
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 7 72 -36 -11 .14 32 27 | --- --- --- ---
cof n/a| 0 -1 4 36 -37 -68 .21 32 27 | --- --- --- ---
emx n/a| -4 0 5 -53 -7 -130 .13 34 31 | 2906 -472 3987 7831
esx n/a| 0 -3 -1 -33 -14 5 -.08 16 15 | -14394 -2107 3975 8582
gfz n/a| 0 0 0 62 9 -17 .07 22 16 | 0 -549 3773 7594
grg n/a| 1 3 1 -49 64 -58 -.23 34 29 | -5177 -1759 3966 7739
iac n/a| 0 0 -4 6 10 144 .02 22 22 | -5082 -1412 3975 7632
mcc n/a| 11 4 -39 272 -89 412 .30 139 139 | --- --- --- ---
Table 2.1900.4 GPS week: 1900 Day: 4 MJD: 57548
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 7 60 -81 -10 .18 33 27 | --- --- --- ---
cof n/a| 0 0 6 55 -71 55 .22 37 30 | --- --- --- ---
emx n/a| 0 3 9 -18 -57 -7 .12 27 26 | -6794 -215 4471 8154
esx n/a| 0 0 0 -8 -20 69 -.08 28 21 | -8438 1316 4459 9324
gfz n/a| 0 0 -1 47 70 30 -.01 21 18 | 0 -934 4169 7748
grg n/a| -2 3 -5 -60 62 -73 -.29 35 32 | -7067 -229 4451 8013
iac n/a| 2 -3 -4 -20 -5 -17 .06 19 19 | -5726 -398 4474 8047
mcc n/a| 6 3 21 18 -73 792 -.49 118 118 | --- --- --- ---
Table 2.1900.5 GPS week: 1900 Day: 5 MJD: 57549
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 -1 7 55 -68 127 .20 35 38 | --- --- --- ---
cof n/a| -2 0 6 45 -49 94 .21 35 36 | --- --- --- ---
emx n/a| -2 0 7 -51 -76 -38 .11 26 24 | -12449 -1216 4293 7385
esx n/a| 0 0 -1 -20 -27 50 -.12 19 17 | -11673 -2963 4307 8916
gfz n/a| 0 0 0 49 94 55 -.06 22 17 | 0 -1193 3788 6590
grg n/a| 0 -1 -7 -50 108 -29 -.19 36 31 | -3776 -3012 4312 7172
iac n/a| 1 -1 0 22 -55 -85 .04 21 21 | -3540 -1739 4305 6857
mcc n/a| 1 -4 18 110 -181 267 -.49 109 109 | --- --- --- ---
Table 2.1900.6 GPS week: 1900 Day: 6 MJD: 57550
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 3 64 -51 -5 .11 32 23 | --- --- --- ---
cof n/a| -1 0 2 32 -36 -43 .05 39 28 | --- --- --- ---
emx n/a| 0 -1 7 -66 -67 -166 .12 28 26 | -11331 1377 4751 9104
esx n/a| 0 -1 -3 -17 1 -18 -.10 19 16 | -9360 2402 4828 10745
gfz n/a| 0 -2 -2 -3 55 27 -.02 24 13 | 0 215 3965 7601
grg n/a| -2 3 -11 -17 197 752 .01 462 462 | -6384 2261 4854 9026
iac n/a| 0 1 -3 0 38 88 -.03 24 24 | -4888 457 4843 8600
mcc n/a| -4 -6 7 12 166 675 -.49 136 136 | --- --- --- ---
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 3.1900.0 GPS week: 1900 Day: 0 MJD: 57544
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 | 1570 52 40 24 25 20 21 19 --- 12 | 51 50 36 62 62 40 40 --- 44
R02 | 893 26 27 17 8 17 21 16 --- 7 | 43 44 38 34 36 52 31 --- 33
R03 | 694 17 22 20 10 16 24 18 113 7 | 65 69 61 56 50 69 42 36 53
R04 | 820 13 13 20 10 10 22 14 --- 6 | 56 57 67 59 56 60 49 --- 56
R05 | 758 35 38 24 21 16 57 25 --- 13 | 44 55 66 57 56 51 43 --- 49
R06 | 857 27 33 31 7 18 29 25 --- 10 | 54 57 45 38 37 46 32 --- 36
R07 | 858 26 17 28 18 16 21 11 92 8 | 61 57 56 49 51 43 44 61 47
R08 | 1309 18 17 23 13 10 20 15 --- 7 | 54 51 49 44 39 40 34 --- 40
R09 | 1777 20 26 23 38 11 32 34 --- 13 | 19 32 30 58 36 52 29 --- 32
R10 | 842 15 27 20 20 14 27 18 --- 8 | 40 45 45 49 42 62 38 --- 40
R12 | 2005 109 85 59 26 53 43 32 --- 23 | 97 87 50 42 56 45 38 --- 34
R13 | 1242 40 48 22 18 20 40 20 --- 11 | 56 59 38 38 26 41 28 --- 31
R14 | 893 53 57 63 30 36 46 24 --- 18 | 34 43 49 69 62 63 35 --- 45
XR15 | 4092 20 24 22 13 --- 19 14 --- 8 | 35 43 31 35 --- 58 28 --- 30
R16 | 1355 33 17 45 20 41 30 26 --- 14 | 50 55 51 62 57 71 42 --- 48
R17E | 1649 29 35 30 12 19 26 13 --- 9 | 43 46 43 45 48 53 31 --- 38
R18E | 1452 27 27 17 12 18 29 14 --- 8 | 39 39 40 35 45 46 40 --- 35
R19E | 980 33 37 20 11 24 25 10 --- 9 | 84 82 97 93 90 75 90 --- 89
R20E | 689 30 27 29 23 31 60 34 --- 15 | 32 42 32 42 59 48 41 --- 35
R21E | 1242 31 39 20 8 18 22 14 83 8 | 36 40 30 27 31 41 27 73 24
R22E | 756 36 32 21 11 23 18 10 --- 8 | 72 73 73 78 88 94 75 --- 76
R23E | 5381 32 41 23 19 12 23 20 --- 9 | 127 129 125 132 121 134 123 --- 124
R24E | 1000 41 58 28 13 31 18 25 --- 11 | 41 68 32 41 50 37 38 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1632 39 38 30 19 24 32 21 97 |T 53 57 51 54 54 57 44 56 46
WRMS | 1632 35 35 28 14 22 29 21 97 |NE 50 53 47 50 47 52 36 48 41
MEDI | 1000 30 32 23 13 18 25 18 92 |MD 50 55 45 49 50 52 38 61 40
Table 3.1900.1 GPS week: 1900 Day: 1 MJD: 57545
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 | 2662 25 44 16 13 18 16 13 --- 7 | 37 50 32 37 37 42 26 --- 29
R02 | 758 29 28 20 9 10 15 14 --- 7 | 32 31 34 31 30 37 21 --- 25
R03 | 539 29 31 20 11 13 21 7 95 7 | 44 49 37 36 38 45 29 29 33
R04 | 563 18 24 21 15 14 20 10 --- 7 | 37 44 49 53 36 48 38 --- 41
R05 | 873 32 28 25 20 13 44 33 --- 12 | 37 46 47 40 48 41 28 --- 34
R06 | 1174 25 23 24 16 15 34 18 --- 9 | 35 40 30 40 35 36 20 --- 27
R07 | 901 20 19 16 6 7 34 10 80 7 | 37 37 36 41 33 36 27 24 31
R08 | 1171 21 17 14 8 8 28 17 --- 7 | 39 36 31 41 36 37 23 --- 32
R09 | 1248 22 21 25 89 18 86 25 --- 23 | 18 26 21 70 28 65 20 --- 22
R10 | 831 10 9 20 16 14 13 12 --- 6 | 27 28 30 35 28 40 27 --- 26
R12 | 1881 99 117 74 28 51 59 31 --- 25 | 68 91 62 46 48 37 37 --- 35
R13 | 1703 43 40 21 12 28 27 12 --- 10 | 45 42 32 29 34 36 26 --- 27
R14 | 1193 35 22 50 33 19 54 23 --- 15 | 32 45 32 51 36 46 27 --- 28
XR15 | 8026 16 15 11 11 --- 19 12 --- 6 | 32 30 32 29 --- 50 20 --- 26
R16 | 908 24 71 28 27 25 46 16 --- 12 | 40 79 39 42 31 50 33 --- 31
R17E | 1759 30 28 22 17 20 34 10 --- 9 | 36 34 29 28 33 54 20 --- 24
R18E | 1214 27 33 18 14 22 24 16 --- 8 | 44 44 49 45 54 42 43 --- 43
R19E | 1068 36 43 18 14 19 19 13 --- 8 | 70 72 76 70 78 56 77 --- 72
R20E | 634 25 25 28 23 33 45 32 --- 14 | 29 37 37 38 55 52 36 --- 33
R21E | 1222 35 36 22 14 17 22 16 63 9 | 40 39 27 27 33 44 26 52 26
R22E | 868 33 42 21 12 17 24 13 --- 8 | 86 86 73 87 92 97 74 --- 80
R23E | 3795 21 23 26 13 12 26 28 --- 9 | 136 138 145 151 152 164 129 --- 142
R24E | 586 32 43 21 21 21 22 20 --- 10 | 38 49 31 36 32 42 31 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1456 35 41 28 26 21 37 19 80 |T 45 51 43 47 46 52 36 35 38
WRMS | 1456 30 32 26 19 13 30 19 80 |NE 37 44 36 41 35 43 26 26 29
MEDI | 1171 27 28 21 14 17 26 16 80 |MD 37 44 34 40 36 44 27 29 31
Table 3.1900.2 GPS week: 1900 Day: 2 MJD: 57546
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 | 3432 33 24 23 15 21 28 21 --- 10 | 39 37 38 37 44 57 38 --- 33
R02 | 868 17 18 10 14 17 26 11 --- 7 | 37 42 34 30 35 69 28 --- 31
R03 | 611 26 26 15 14 9 21 21 87 8 | 54 56 43 38 38 74 31 40 38
R04 | 683 24 19 20 13 23 20 8 --- 8 | 37 35 30 29 28 39 30 --- 26
R05 | 545 19 24 30 21 27 55 31 --- 13 | 31 37 35 44 43 51 30 --- 30
R06 | 1336 27 25 10 17 21 31 18 --- 9 | 36 45 28 40 45 55 25 --- 33
R07 | 636 15 21 8 17 13 30 21 110 8 | 43 52 37 52 44 42 30 34 37
R08 | 1083 24 26 25 13 13 18 16 --- 8 | 38 39 36 26 16 54 25 --- 21
R09 | 1235 22 30 27 32 24 51 23 --- 13 | 21 33 20 28 22 70 25 --- 20
R10 | 2615 12 15 21 16 21 25 14 --- 8 | 30 34 31 39 24 47 29 --- 28
R12 | 1908 82 96 48 18 38 59 38 --- 20 | 78 84 33 43 43 46 35 --- 32
R13 | 1188 34 33 28 10 18 11 21 --- 9 | 46 46 35 31 27 29 25 --- 27
R14 | 873 27 56 64 28 38 62 27 --- 18 | 35 71 41 52 52 49 30 --- 35
XR15 | 7815 18 27 19 12 --- 23 11 --- 8 | 28 40 31 25 --- 36 20 --- 22
R16 | 753 37 21 41 23 33 47 16 --- 14 | 51 42 39 48 39 45 39 --- 36
R17E | 1651 27 25 17 9 27 28 13 --- 8 | 43 43 34 36 51 50 27 --- 33
R18E | 746 21 26 17 8 16 14 13 --- 6 | 42 46 36 36 38 43 30 --- 34
R19E | 894 34 35 20 10 21 18 12 --- 8 | 52 53 52 54 64 48 51 --- 51
R20E | 789 32 32 21 18 35 24 25 --- 11 | 27 34 34 33 53 37 34 --- 29
R21E | 755 34 35 24 11 25 28 17 78 10 | 39 42 31 32 39 33 25 53 27
R22E | 1289 36 31 26 12 20 15 21 --- 9 | 71 73 71 73 72 76 56 --- 66
R23E | 2773 24 24 26 15 13 28 16 --- 9 | 85 89 92 87 89 107 80 --- 86
R24E |>>>>> 37 29 34 20 20 28 20 --- 11 | 42 42 36 33 37 45 32 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS |63497 32 35 28 17 24 34 20 92 |T 43 48 39 41 42 52 33 42 34
WRMS |63497 27 29 26 15 21 27 20 92 |NE 40 46 34 37 35 50 29 37 29
MEDI | 1083 27 26 23 15 21 28 18 87 |MD 39 42 35 37 39 48 30 40 32
Table 3.1900.3 GPS week: 1900 Day: 3 MJD: 57547
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 | 3461 30 36 19 16 19 22 22 --- 9 | 34 44 29 36 37 40 25 --- 24
R02 | 837 18 12 20 19 16 17 21 --- 8 | 44 40 48 36 44 60 39 --- 37
R03 | 690 17 19 24 13 18 20 20 101 8 | 58 62 68 57 70 66 49 49 56
R04 | 738 20 20 15 12 9 23 27 --- 8 | 45 44 41 39 41 76 27 --- 36
R05 | 908 36 22 61 21 25 45 23 --- 15 | 45 40 65 42 39 62 34 --- 35
R06 | 644 28 33 27 14 11 19 24 --- 9 | 40 40 38 46 38 53 23 --- 35
R07 | 599 10 12 17 6 13 29 23 163 7 | 55 54 46 49 50 79 31 67 46
R08 | 773 22 24 26 15 16 24 27 --- 9 | 43 44 46 35 33 44 16 --- 29
R09 | 1300 21 22 29 16 18 33 21 --- 10 | 25 33 44 31 30 40 22 --- 20
R10 | 3405 13 21 15 21 25 13 18 --- 8 | 39 47 29 52 37 43 29 --- 36
R12 | 2352 81 78 75 23 39 87 42 --- 25 | 91 95 60 41 44 42 35 --- 39
R13 | 856 37 39 18 8 28 28 15 --- 10 | 59 61 48 39 39 37 29 --- 36
R14 | 1020 33 33 62 20 20 42 22 --- 14 | 46 54 55 56 46 41 41 --- 44
XR15 | 7980 16 13 21 14 --- 23 16 --- 8 | 28 29 29 36 --- 58 29 --- 26
R16 | 789 29 36 47 23 22 53 28 --- 14 | 42 55 36 51 45 71 47 --- 39
R17E | 1549 26 28 20 10 18 28 15 --- 8 | 38 39 33 28 38 44 20 --- 28
R18E | 773 18 16 28 10 21 24 15 --- 8 | 59 61 70 60 65 39 53 --- 58
R19E | 1271 27 28 19 9 24 24 11 --- 8 | 92 90 89 85 93 55 81 --- 84
R20E | 843 30 35 24 15 29 37 22 --- 11 | 41 50 23 29 41 40 28 --- 22
R21E | 1113 30 28 26 9 23 15 16 147 8 | 38 34 25 29 30 42 21 139 23
R22E | 1182 40 36 28 11 27 26 16 --- 11 | 81 79 70 78 89 95 79 --- 76
R23E | 1298 32 31 20 23 15 21 20 --- 10 | 94 91 95 104 95 115 94 --- 95
R24E | 1625 30 37 43 26 30 44 26 --- 14 | 44 61 47 57 66 53 35 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1498 32 32 34 16 22 34 22 139 |T 51 54 49 48 50 56 38 85 42
WRMS | 1498 27 27 31 15 16 29 22 139 |NE 46 49 45 43 42 54 31 58 35
MEDI | 1020 28 28 24 15 20 24 21 147 |MD 44 50 46 42 41 53 31 67 36
Table 3.1900.4 GPS week: 1900 Day: 4 MJD: 57548
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 | 2482 31 37 29 23 21 40 19 --- 11 | 44 56 38 51 50 66 37 --- 37
R02 | 669 18 23 25 12 9 22 11 --- 7 | 38 40 44 28 32 62 24 --- 28
R03 | 1098 22 19 30 12 13 27 12 152 8 | 58 54 70 39 38 60 37 91 42
R04 | 701 18 22 10 10 13 27 13 --- 6 | 55 59 56 57 53 64 42 --- 49
R05 | 1362 34 44 32 20 13 56 25 --- 13 | 50 61 54 39 46 62 37 --- 39
R06 | 783 32 25 23 13 11 31 14 --- 9 | 51 46 39 37 41 79 41 --- 41
R07 | 894 14 17 14 13 10 29 12 104 6 | 53 56 55 53 45 68 42 74 45
R08 | 582 19 17 23 24 23 33 16 --- 10 | 43 45 53 34 47 67 33 --- 37
R09 | 2435 30 35 32 102 36 47 26 --- 24 | 24 30 30 86 33 64 23 --- 25
R10 | 2301 13 12 16 20 19 33 10 --- 8 | 39 38 38 44 33 66 31 --- 34
R12 | 1956 86 102 38 27 38 53 30 --- 20 | 77 87 42 52 49 61 39 --- 40
R13 | 1221 34 35 22 16 18 17 21 --- 9 | 57 58 38 42 39 60 31 --- 36
R14 | 1379 31 38 48 25 24 50 24 --- 14 | 47 58 41 43 54 69 33 --- 36
XR15 | 5488 14 15 17 21 --- 33 12 --- 9 | 35 35 34 48 --- 52 37 --- 35
R16 | 1032 26 32 29 29 27 31 15 --- 11 | 57 64 43 54 50 72 52 --- 46
R17E | 1411 29 25 19 11 16 19 16 --- 8 | 43 37 35 35 29 68 30 --- 31
R18E | 659 19 16 21 12 13 21 15 --- 7 | 39 39 41 41 40 68 41 --- 38
R19E | 1573 28 26 17 11 23 25 10 --- 8 | 73 83 77 85 91 84 77 --- 79
R20E | 722 35 48 24 19 22 46 26 --- 12 | 42 54 31 32 41 82 34 --- 30
R21E | 1500 32 28 22 12 21 13 13 91 8 | 39 38 31 38 42 68 28 83 31
R22E | 924 39 38 26 10 18 25 15 --- 9 | 55 56 41 47 50 76 38 --- 43
R23E | 991 32 40 24 26 13 33 18 --- 10 | 47 55 40 60 47 67 47 --- 45
R24E | 1305 35 31 39 22 29 49 29 --- 14 | 43 50 40 40 56 93 38 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1392 33 37 27 28 21 35 19 118 |T 48 52 43 47 45 68 37 82 39
WRMS | 1392 27 30 26 21 18 32 19 118 |NE 48 52 45 47 43 64 35 82 38
MEDI | 1221 30 28 24 19 18 31 15 104 |MD 47 54 41 43 45 67 37 83 37
Table 3.1900.5 GPS week: 1900 Day: 5 MJD: 57549
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 | 788 28 34 18 25 28 23 25 --- 11 | 45 54 40 61 67 160 42 --- 48
R02 | 717 20 16 22 24 21 24 14 --- 9 | 44 41 47 48 45 157 35 --- 41
R03 | 1193 18 18 15 12 10 33 15 114 7 | 52 53 55 54 50 153 36 40 46
R04 | 1460 20 20 20 9 15 12 12 --- 6 | 55 55 48 45 49 149 41 --- 45
R05 | 1822 24 22 21 13 24 64 25 --- 13 | 59 79 62 69 77 150 49 --- 59
R06 | 1310 24 39 14 11 21 19 27 --- 9 | 51 63 46 54 60 146 33 --- 44
R07 | 1938 27 26 25 20 18 19 12 141 9 | 56 53 49 45 45 139 43 31 45
R08 | 825 11 12 12 15 11 35 16 --- 7 | 46 42 41 51 46 163 43 --- 46
R09 | 2648 22 20 27 28 21 28 17 --- 10 | 26 29 34 35 31 127 21 --- 24
R10 | 1629 17 18 21 24 21 39 19 --- 10 | 37 40 30 50 33 150 28 --- 35
R12 | 1591 95 87 25 27 32 41 40 --- 19 | 69 61 50 37 40 127 38 --- 33
R13 | 1415 42 44 16 11 23 20 16 --- 9 | 53 49 30 33 30 124 29 --- 31
R14 | 1233 56 35 64 35 30 80 31 --- 21 | 42 50 48 60 54 129 32 --- 38
XR15 | 3800 14 14 21 28 --- 19 22 --- 11 | 36 37 34 47 --- 127 32 --- 34
R16 | 1482 16 34 33 23 18 69 20 --- 14 | 55 72 57 57 52 152 51 --- 50
R17E | 1490 35 44 22 10 19 28 16 --- 9 | 48 56 36 34 43 132 23 --- 32
R18E | 911 26 27 19 12 16 18 17 --- 8 | 43 44 45 37 45 119 36 --- 38
R19E | 2211 25 27 18 12 17 22 12 --- 7 | 112 113 116 120 121 99 110 --- 114
R20E | 1188 36 29 25 13 30 30 24 --- 11 | 44 41 29 37 49 149 32 --- 32
R21E | 1591 27 32 20 12 20 22 9 55 8 | 39 41 31 35 39 129 26 41 29
R22E | 1658 38 36 20 10 20 20 13 --- 9 | 65 64 66 60 65 160 56 --- 59
R23E | 1575 31 35 26 17 13 20 16 --- 9 | 84 83 94 96 90 201 87 --- 90
R24E | 1500 41 38 33 23 29 33 32 --- 14 | 38 44 48 46 50 148 35 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1529 35 35 26 19 22 36 21 109 |T 52 54 49 52 53 143 41 37 45
WRMS | 1529 38 36 24 17 17 31 21 109 |NE 48 51 44 49 48 143 36 35 41
MEDI | 1490 26 29 21 15 20 24 17 114 |MD 48 53 47 48 49 148 36 40 41
Table 3.1900.6 GPS week: 1900 Day: 6 MJD: 57550
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 | 1443 20 20 30 14 11 457 26 --- 21 | 46 52 41 49 45 186 43 --- 39
R02 | 1031 21 23 17 16 13 453 12 --- 20 | 48 50 48 33 36 178 29 --- 35
R03 | 887 22 25 16 13 8 458 16 86 20 | 69 71 64 57 56 195 48 49 56
R04 | 1354 17 16 18 13 7 458 16 --- 20 | 67 65 63 53 54 189 46 --- 54
R05 | 1092 27 31 34 16 28 416 25 --- 20 | 60 64 78 60 57 194 63 --- 60
R06 | 1078 14 19 16 14 14 453 15 --- 19 | 61 65 61 58 59 189 46 --- 55
R07 | 1270 17 23 17 17 15 466 18 208 20 | 66 70 59 61 65 195 49 30 58
R08 | 771 26 30 16 18 16 449 15 --- 20 | 56 58 51 46 42 187 35 --- 42
R09 | 2376 17 17 35 13 13 470 12 --- 21 | 28 32 31 25 33 161 25 --- 25
R10 | 922 13 21 17 19 19 485 11 --- 21 | 44 48 38 49 36 182 38 --- 39
R12 | 1183 82 97 53 34 49 440 61 --- 31 | 88 110 43 61 64 171 40 --- 44
R13 | 2336 40 52 22 13 29 460 17 --- 22 | 59 68 40 47 45 168 36 --- 41
R14 | 1141 49 58 51 40 43 498 35 --- 28 | 43 83 49 83 85 186 39 --- 53
XR15 | 3473 13 19 18 26 --- 454 16 --- 25 | 44 44 41 50 --- 162 39 --- 41
R16 | 1296 16 21 30 26 32 499 27 --- 23 | 73 75 62 74 79 154 66 --- 68
R17E | 1084 31 41 20 12 27 458 21 --- 21 | 46 53 31 36 43 166 29 --- 32
R18E | 966 28 41 22 10 17 470 21 --- 21 | 48 56 37 39 39 175 35 --- 37
R19E | 3691 28 28 22 12 17 466 15 --- 21 | 102 109 106 102 113 208 102 --- 104
R20E | 1798 28 38 24 22 28 447 35 --- 22 | 47 52 38 45 46 184 50 --- 38
R21E | 1186 21 19 25 12 23 471 14 68 21 | 39 37 37 36 41 165 27 51 32
R22E | 1594 30 50 19 11 25 456 13 --- 21 | 57 70 60 63 73 151 53 --- 58
R23E | 1035 28 31 26 17 14 463 17 --- 21 | 86 88 89 94 88 150 85 --- 87
R24E | 1733 48 54 36 29 32 470 24 --- 24 | 41 48 49 39 37 166 33 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1562 32 39 28 19 24 462 24 136 |T 57 63 52 54 56 176 45 43 49
WRMS | 1562 23 28 26 16 13 462 24 136 |NE 56 63 51 53 54 179 42 39 47
MEDI | 1186 26 28 22 16 17 458 17 86 |MD 56 64 49 50 46 178 40 49 42
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