[IGSREPORT-27271] Wk 2104 IGLOS Final Orbits
acc
acc at igs.org
Sat May 23 19:06:43 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2104 (May 03, 2020 - May 09, 2020)
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 2.2104.
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:
igl2104[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2104 in the SP3 format.
igl21047.sum Combination Report for GPS Week 2104.
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 | -2.5 ns
1 | -3.4 ns
2 | -2.0 ns
3 | -2.0 ns
4 | 0.3 ns
5 | -0.6 ns
6 | -0.3 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 1.2104, 1a.2104).
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 2.2104.0-6)
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 3.2104.0-6).
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 2104 summary. (May 03, 2020 - May 09, 2020)
Table 1.2104.a GPS week : 2104 MJD: 58972.0-58978.0
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 0 0 22 -7 58 .09 19 15 | 19819 -379 3689 9404
| 0 1 0 19 14 24 .05 | 1284 1220
cof n/a| 0 0 0 19 15 55 .05 21 17 | 19812 -376 3693 9405
| 0 1 2 28 21 26 .05 | 1289 1228
emx n/a| 0 0 2 31 32 -29 -.05 32 31 | -4621 84 3304 8805
| 0 1 1 17 21 41 .07 | 6386 758
esx n/a| 1 0 -1 6 3 -39 .12 29 21 | -3248 193 3303 10662
| 0 1 2 8 6 32 .07 | 6876 1477
gfz n/a| 0 0 -3 -14 13 -42 .19 28 16 | 0 -559 3330 8098
| 1 0 0 20 18 18 .06 | 0 961
grg n/a| 0 0 1 -65 -22 -30 -.35 23 19 | -1186 -354 3295 7600
| 1 1 3 35 13 51 .03 | 1128 1288
iac n/a| -1 0 0 29 -8 36 -.00 21 21 | -459 275 3667 9543
| 1 1 2 10 23 61 .05 | 1524 1052
Table 1.2104.b GPS week : 2104 MJD: 58972.0-58978.0
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 | 14 13 15 15 16 15 19 |
R02 | 6 4 6 5 7 7 6 |
R03 | 7 5 5 6 5 6 7 |
R04 | 9 12 10 10 11 8 11 |
R05 | 8 9 6 9 8 9 7 |
R07 | 6 5 6 8 6 6 6 |
R08 | 7 9 7 7 7 7 5 |
R09 | 6 9 8 7 7 7 8 |
R11 | 7 7 6 7 6 7 7 |
R12 | 11 10 10 8 9 9 10 |
R13 | 23 25 25 17 18 20 21 |
R14 | 8 8 6 7 8 7 7 |
R15 | 10 9 7 8 8 7 8 |
R16 | 15 13 18 15 12 12 13 |
R17 | 8 6 7 7 8 7 7 |
R18 | 6 8 7 6 6 6 6 |
R19 | 18 18 16 18 18 20 21 |
R20 | 24 21 24 25 24 23 20 |
R21 | 7 8 8 8 7 8 8 |
R22 | 8 7 8 9 7 8 8 |
R23 | 10 9 11 11 9 8 9 |
R24 | 7 6 7 7 6 8 7 |
R26 | 15 13 27 24 21 16 19 |
Table 1.2104.c GPS week : 2104 MJD: 58972.0-58978.0
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 2104 0 | -65 60 296 -914 -20 -2244 82.4 1514 1514 | -2479 0
brd 2104 1 | -115 -75 373 -722 -1478 -210 84.2 1887 1887 | -3448 0
brd 2104 2 | -6 -28 358 -192 -2 2504 83.2 1680 1680 | -2038 0
brd 2104 3 | 27 53 275 -47 993 2339 82.3 1654 1654 | -2036 0
brd 2104 4 | 47 35 205 383 1279 788 81.6 1863 1863 | 310 0
brd 2104 5 | -96 42 239 -59 -1043 -1578 82.4 1567 1567 | -559 0
brd 2104 6 | 30 -1 177 -213 31 -144 82.7 1708 1708 | -255 0
-------------+------------------------------------------------------------+----------------
brd 2104 mean| -25 12 275 -252 -34 207 82.7 1696 1696 | -1500 0
brd 2104 sdev| 66 50 73 437 990 1809 .8 139 139 | 1356 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 2.2104.0 GPS week: 2104 Day: 0 MJD: 58972
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 -1 20 15 39 .09 19 16 | 19780 615 3725 10986
cof n/a| 1 -1 -2 -6 20 56 .09 20 17 | 19758 635 3734 10992
emx n/a| 0 2 1 42 44 -93 -.01 34 31 | -3201 1053 3446 8695
esx n/a| 0 0 -1 7 7 -6 .17 31 25 | 885 -604 3463 10543
gfz n/a| 0 -1 -4 -10 17 -14 .23 27 16 | 0 68 3501 8316
grg n/a| 0 0 4 -64 -40 -117 -.41 21 18 | -2510 394 3433 7444
iac n/a| -1 0 0 35 -47 162 .04 22 22 | -3003 287 3787 11149
Table 2.2104.1 GPS week: 2104 Day: 1 MJD: 58973
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 47 -1 59 .04 18 15 | 21492 -1288 3132 7750
cof n/a| 0 1 -1 53 39 78 .08 22 18 | 21512 -1317 3145 7724
emx n/a| 0 0 0 61 38 6 -.16 35 32 | -6299 -634 2878 7811
esx n/a| 0 0 -3 4 0 15 .13 28 20 | -7923 -381 2859 9782
gfz n/a| 0 0 -2 -42 15 -57 .16 24 16 | 0 -1901 2869 7146
grg n/a| -2 -1 6 -82 -26 -38 -.32 23 18 | -2612 -1454 2869 6949
iac n/a| 0 -2 -2 30 -26 22 .04 24 24 | -700 -1278 3103 7957
Table 2.2104.2 GPS week: 2104 Day: 2 MJD: 58974
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 8 0 56 .02 17 13 | 20590 -368 3794 9133
cof n/a| 0 0 0 17 -15 40 -.01 20 15 | 20572 -339 3798 9141
emx n/a| 0 0 1 40 47 -1 -.09 34 29 | -3920 -21 3278 9042
esx n/a| 0 1 1 11 -2 -39 .14 30 22 | -8469 -343 3279 11285
gfz n/a| 1 0 -3 -9 25 -28 .26 27 14 | 0 -867 3305 8249
grg n/a| 2 -1 1 -110 -6 -69 -.36 30 23 | -1714 -316 3267 7942
iac n/a| -2 0 2 34 -16 -1 -.06 22 22 | -1954 2106 3757 9175
Table 2.2104.3 GPS week: 2104 Day: 3 MJD: 58975
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 42 -11 54 .12 18 12 | 19715 -2363 4262 9859
cof n/a| 0 0 1 41 38 3 .00 24 16 | 19701 -2361 4264 9858
emx n/a| -1 0 3 10 4 -67 .04 31 31 | -6355 -694 3472 9302
esx n/a| 1 -2 1 -10 -1 -57 .14 28 21 | 9360 -1712 3490 11149
gfz n/a| 2 -1 -3 3 -9 -58 .12 28 17 | 0 -1292 3504 8515
grg n/a| -1 1 -3 -94 -4 28 -.35 25 18 | -612 -2274 3468 8191
iac n/a| -1 0 2 39 16 10 -.03 20 20 | 106 -295 4217 9639
Table 2.2104.4 GPS week: 2104 Day: 4 MJD: 58976
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 31 -16 42 .18 21 15 | 17528 679 3814 10901
cof n/a| 0 0 -4 30 -6 70 .03 22 17 | 17526 668 3819 10912
emx n/a| 0 1 1 19 50 8 -.01 32 32 | -4217 740 3188 9291
esx n/a| 0 0 -1 14 3 -57 -.01 27 21 | -7933 2565 3191 10752
gfz n/a| -2 0 -2 14 -8 -32 .13 32 15 | 0 933 3242 8485
grg n/a| 1 0 -4 -68 -29 -36 -.31 19 17 | -216 1197 3186 7946
iac n/a| -1 0 2 31 12 57 .01 17 17 | 360 188 3718 11256
Table 2.2104.5 GPS week: 2104 Day: 5 MJD: 58977
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 11 -31 111 .08 19 16 | 19027 962 3687 8485
cof n/a| 1 -2 1 -27 11 70 .04 21 17 | 19013 979 3685 8485
emx n/a| 1 0 3 18 40 -6 -.03 26 27 | 6680 762 3588 8691
esx n/a| 1 1 -5 4 4 -79 .08 31 20 | -8471 1793 3579 10585
gfz n/a| 0 0 -3 -27 14 -62 .20 30 17 | 0 50 3612 7912
grg n/a| 0 0 2 -26 -22 5 -.33 21 18 | -959 953 3585 7429
iac n/a| -2 0 -1 8 6 -26 .07 22 22 | 942 -27 3693 8645
Table 2.2104.6 GPS week: 2104 Day: 6 MJD: 58978
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 -6 -7 46 .08 18 17 | 20601 -895 3414 8719
cof n/a| 0 -1 1 27 21 68 .13 22 21 | 20607 -900 3410 8725
emx n/a| -1 -1 2 25 -1 -51 -.12 31 31 | -15038 -618 3280 8809
esx n/a| 0 0 -1 13 15 -47 .21 31 21 | -189 39 3262 10542
gfz n/a| 1 0 -4 -31 41 -40 .26 31 18 | 0 -908 3277 8066
grg n/a| 1 0 2 -12 -27 10 -.36 23 19 | 315 -984 3262 7300
iac n/a| -1 -1 0 23 -6 27 -.08 20 20 | 1031 950 3398 8986
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 3.2104.0 GPS week: 2104 Day: 0 MJD: 58972
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 950 26 18 46 34 30 25 25 13 | 76 70 81 50 53 64 50 58
R02 | 2484 6 12 10 15 12 15 14 5 | 45 48 42 44 48 51 47 45
R03 | 548 11 19 17 14 12 15 22 7 | 60 57 54 68 61 64 60 61
XR04 | 693 13 12 13 19 --- 16 21 8 | 69 68 66 54 --- 61 57 60
R05 | 498 17 15 20 13 25 13 16 8 | 47 58 50 60 70 53 55 53
R07 | 1355 14 19 8 9 12 17 16 6 | 52 56 56 61 60 70 67 60
R08 | 1510 12 9 15 7 10 21 22 7 | 48 52 49 53 57 60 65 55
R09 | 2183 16 22 16 14 12 12 11 6 | 61 61 61 67 65 60 60 61
R11 | 716 13 14 15 12 19 19 10 6 | 68 70 56 59 53 73 66 63
R12 | 753 20 19 39 30 14 17 17 10 | 91 87 43 54 81 71 87 73
R13 | 1545 21 40 70 88 42 32 47 23 | 117 127 55 43 124 120 138 101
R14 | 1046 16 13 24 19 13 23 12 8 | 78 76 59 61 73 64 73 67
R15 | 2611 11 13 24 37 23 10 15 9 | 81 85 60 51 90 74 82 73
R16 | 1687 26 18 38 34 29 41 25 14 | 60 79 49 74 85 102 89 75
R17E | 812 12 14 27 16 15 15 14 7 | 52 53 55 56 55 53 52 52
R18E | 766 9 12 12 13 15 16 12 6 | 43 42 46 44 40 41 41 41
R19E | 1233 36 30 55 38 53 24 31 17 | 52 49 65 56 75 54 42 49
R20E | 1149 41 35 72 56 72 38 45 24 | 110 118 117 122 130 119 109 110
R21E | 1623 13 16 26 14 14 11 16 7 | 116 115 117 118 117 118 124 118
R22E | 2921 17 13 24 15 18 11 13 7 | 88 87 77 88 91 87 91 86
R23E | 566 19 20 19 26 25 19 18 9 | 42 39 51 50 40 48 44 43
R24E | 1338 14 11 23 13 15 15 12 6 | 34 31 38 39 36 36 30 33
XR26E | 3343 16 43 --- --- --- --- 14 15 | 26 56 --- --- --- --- 36 29
------+----------------------------------------------+------------------------------------------
RMS | 1513 19 20 34 31 27 21 22 |T 65 68 61 62 71 70 68 63
WRMS | 1513 16 17 31 25 16 18 22 |NE 68 71 55 57 70 70 71 64
MEDI | 1233 16 16 23 15 15 16 16 |MD 60 61 55 56 65 64 60 60
Table 3.2104.1 GPS week: 2104 Day: 1 MJD: 58973
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1134 30 33 48 28 23 26 20 13 | 56 59 68 31 44 34 32 40
R02 | 2893 6 9 13 9 7 10 12 4 | 33 32 32 39 37 44 35 36
R03 | 1170 5 8 11 9 15 14 15 5 | 39 40 34 38 53 44 38 40
XR04 | 860 21 23 16 17 --- 19 37 12 | 49 48 42 35 --- 44 43 40
R05 | 816 16 20 19 19 26 19 13 8 | 35 34 38 45 51 40 40 38
R07 | 1026 9 13 10 8 11 10 18 5 | 36 33 39 37 37 35 40 36
R08 | 881 16 16 19 11 19 10 33 8 | 31 33 35 41 35 43 56 38
R09 | 2296 19 23 20 10 15 28 16 8 | 49 50 36 44 49 53 47 45
R11 | 830 10 15 26 10 21 16 12 7 | 51 51 45 50 57 56 52 50
R12 | 821 26 34 36 25 8 13 16 9 | 65 72 33 34 45 46 57 47
R13 | 1459 22 36 73 85 33 60 46 24 | 90 106 48 37 96 122 117 84
R14 | 1327 18 19 27 13 21 16 14 8 | 56 58 43 43 46 54 54 48
R15 | 2061 13 14 26 26 11 18 23 8 | 52 54 42 35 52 44 59 46
R16 | 2724 24 29 37 24 29 35 25 13 | 46 46 49 62 74 49 67 54
R17E | 2043 9 11 23 10 15 13 16 6 | 42 43 49 44 42 44 45 43
R18E | 863 10 10 17 19 16 22 14 7 | 34 34 38 41 37 43 42 37
R19E | 924 22 28 64 40 44 30 39 17 | 47 47 60 50 59 47 53 47
R20E | 958 36 32 70 49 59 25 44 21 | 87 91 86 97 98 85 85 85
R21E | 2899 16 20 25 17 15 16 24 8 | 123 124 122 119 123 124 136 124
R22E | 3903 11 15 26 14 13 13 16 6 | 112 115 114 111 116 113 112 112
R23E | 2833 16 20 25 22 25 17 19 9 | 38 38 40 39 31 35 32 32
R24E | 819 13 17 23 11 14 11 13 6 | 30 31 27 30 29 30 25 27
XR26E | 2882 11 73 --- --- --- --- 15 13 | 35 80 --- --- --- --- 40 35
------+----------------------------------------------+------------------------------------------
RMS | 1886 18 22 35 28 24 23 24 |T 53 57 50 50 57 55 56 51
WRMS | 1886 15 18 32 20 16 18 24 |NE 49 51 41 40 52 50 52 45
MEDI | 1170 16 20 25 17 16 16 16 |MD 47 48 42 41 49 44 47 43
Table 3.2104.2 GPS week: 2104 Day: 2 MJD: 58974
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1717 32 34 46 34 22 51 12 15 | 66 67 71 37 54 36 49 48
R02 | 2258 8 10 9 10 14 12 20 5 | 38 42 40 45 40 43 39 38
R03 | 904 7 10 15 9 9 15 12 5 | 46 51 45 55 49 46 48 47
XR04 | 788 17 25 15 17 --- 16 24 9 | 48 53 50 39 --- 41 41 43
R05 | 1122 11 13 14 16 11 18 15 6 | 37 38 40 40 46 48 39 39
R07 | 860 9 13 12 11 21 11 16 6 | 42 44 42 48 35 45 36 39
R08 | 842 12 11 18 18 15 12 18 7 | 38 37 42 35 40 40 41 37
R09 | 2127 11 11 12 9 15 36 17 8 | 69 71 71 80 81 73 77 73
R11 | 1591 10 11 19 8 14 12 20 6 | 52 55 43 44 45 48 63 49
R12 | 661 18 28 34 24 18 21 19 10 | 77 86 52 62 79 58 79 68
R13 | 1468 27 29 62 91 35 67 37 24 | 100 95 48 33 98 126 100 82
R14 | 926 7 14 23 14 15 12 14 6 | 60 66 46 53 68 59 54 57
R15 | 1255 10 12 22 22 12 22 11 7 | 56 50 39 38 50 65 48 49
R16 | 2076 24 23 39 19 51 63 32 17 | 47 55 46 46 58 73 73 51
R17E | 1824 13 17 26 18 19 10 11 7 | 38 42 42 37 32 41 38 36
R18E | 1487 8 15 21 15 19 14 12 6 | 24 27 32 29 27 24 28 24
R19E | 1125 24 32 50 30 42 32 39 15 | 31 39 34 38 50 57 52 36
R20E | 744 28 34 81 62 69 43 42 24 | 68 74 69 76 78 64 61 56
R21E | 2248 14 14 28 17 22 15 12 8 | 80 79 77 78 86 78 76 78
R22E | 2595 12 13 25 13 15 14 21 7 | 91 101 101 101 106 97 80 94
R23E | 2416 24 27 23 28 28 16 24 11 | 45 51 41 41 47 35 39 39
R24E | 2505 12 18 23 17 12 12 14 6 | 26 30 29 24 28 23 25 23
XR26E | 2834 21 48 --- --- --- --- 32 26 | 28 63 --- --- --- --- 50 34
------+----------------------------------------------+------------------------------------------
RMS | 1679 17 20 34 30 27 30 22 |T 52 57 50 49 57 55 53 49
WRMS | 1679 13 15 29 22 14 23 22 |NE 55 57 48 46 57 57 56 51
MEDI | 1487 12 15 23 17 18 15 18 |MD 47 53 43 41 50 48 49 47
Table 3.2104.3 GPS week: 2104 Day: 3 MJD: 58975
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1746 23 33 47 27 29 46 21 14 | 58 71 77 54 61 35 57 50
R02 | 1955 8 11 10 10 12 16 14 5 | 40 44 40 41 41 36 46 40
R03 | 857 7 9 10 14 16 9 18 5 | 53 55 53 52 58 53 59 53
XR04 | 768 15 17 22 10 --- 18 25 9 | 54 55 55 43 --- 55 37 46
R05 | 1089 15 18 22 23 24 18 19 9 | 41 41 45 34 38 37 25 32
R07 | 788 11 11 11 13 21 17 22 7 | 48 52 47 49 43 57 65 50
R08 | 984 8 16 12 15 18 14 18 6 | 38 48 37 48 38 43 54 42
R09 | 2155 14 12 24 17 15 14 11 7 | 41 40 40 36 49 35 46 39
R11 | 2694 7 14 22 12 17 13 19 6 | 59 60 44 58 60 71 75 61
R12 | 783 12 14 34 14 13 14 15 7 | 70 59 44 53 64 62 64 60
R13 | 2102 31 51 48 61 32 34 19 17 | 88 105 46 36 73 75 77 64
R14 | 863 8 10 27 17 13 12 14 6 | 66 64 55 56 72 70 75 66
R15 | 969 8 10 28 23 18 13 15 7 | 62 62 43 41 66 60 65 56
R16 | 1364 22 35 39 37 33 43 21 14 | 46 48 47 61 54 77 66 55
R17E | 882 9 12 22 17 19 8 13 6 | 35 37 30 35 49 36 37 36
R18E | 892 14 14 13 16 17 12 11 6 | 24 25 28 32 34 26 29 27
R19E | 1361 22 35 46 42 67 33 29 17 | 41 47 48 52 75 52 47 43
R20E | 1137 48 51 64 69 63 56 42 25 | 46 48 43 78 75 64 41 38
R21E | 888 11 11 27 20 17 17 21 8 | 126 123 120 133 131 139 125 128
R22E | 3314 14 16 32 16 17 18 24 9 | 130 129 127 126 125 127 121 125
R23E | 1245 18 20 15 25 30 21 28 10 | 39 43 38 46 34 42 38 37
R24E | 2922 9 17 30 16 20 12 10 7 | 22 31 21 27 30 21 23 20
XR26E | 3166 20 44 --- --- --- --- 27 23 | 24 38 --- --- --- --- 43 29
------+----------------------------------------------+------------------------------------------
RMS | 1654 18 24 31 28 28 25 20 |T 54 57 51 54 60 57 57 52
WRMS | 1654 12 16 31 21 17 18 20 |NE 54 57 48 47 55 54 57 51
MEDI | 1137 14 16 24 17 18 16 19 |MD 46 48 44 48 58 53 54 46
Table 3.2104.4 GPS week: 2104 Day: 4 MJD: 58976
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1592 32 33 48 36 59 25 17 16 | 62 80 78 73 72 41 45 53
R02 | 1058 12 16 21 10 16 22 9 7 | 32 28 38 29 28 31 29 28
R03 | 519 11 14 11 10 11 14 9 5 | 47 43 45 52 57 59 57 53
XR04 | 736 20 27 18 27 --- 21 18 10 | 55 55 52 41 --- 58 50 49
R05 | 723 15 14 26 16 26 17 13 8 | 37 36 42 40 40 37 33 34
R07 | 673 10 12 13 19 8 14 12 6 | 43 39 45 41 50 51 53 46
R08 | 721 12 19 16 13 19 17 12 6 | 41 34 35 57 54 48 47 47
R09 | 2270 13 16 19 13 22 16 14 7 | 78 81 84 83 90 75 87 81
R11 | 2641 6 11 19 17 13 13 13 6 | 51 56 42 50 47 55 49 48
R12 | 1517 17 25 31 28 20 15 14 9 | 58 66 42 37 63 61 61 52
R13 | 2676 40 33 48 49 62 22 19 17 | 78 74 44 44 76 57 64 56
R14 | 694 12 17 33 13 14 16 15 7 | 62 68 42 60 68 67 70 62
R15 | 983 14 18 27 22 15 16 14 8 | 65 71 46 45 60 63 66 58
R16 | 809 29 26 25 31 33 30 13 12 | 46 60 40 59 52 73 58 53
R17E | 1079 11 9 23 17 28 13 11 7 | 32 33 28 29 40 35 32 30
R18E | 632 16 17 12 18 17 10 11 6 | 22 26 25 34 34 27 29 27
R19E | 784 28 26 54 40 52 32 37 17 | 37 37 38 51 62 44 52 37
R20E | 1687 50 50 75 63 70 36 41 24 | 67 72 56 77 99 69 63 59
R21E | 936 12 14 24 17 16 11 13 6 | 47 50 48 54 45 47 46 46
R22E | 4859 12 13 26 19 16 16 12 7 | 67 66 65 76 62 63 64 65
R23E | 2008 16 17 21 22 25 18 16 8 | 31 34 41 35 30 33 35 31
R24E | 3192 14 15 25 13 10 10 11 6 | 27 33 27 28 30 30 25 25
XR26E | 3174 23 43 --- --- --- --- 18 20 | 22 49 --- --- --- --- 37 28
------+----------------------------------------------+------------------------------------------
RMS | 1862 21 22 32 27 32 19 17 |T 48 51 45 49 55 51 50 46
WRMS | 1862 15 17 32 21 15 17 17 |NE 53 56 48 50 58 55 54 51
MEDI | 1058 14 17 24 18 19 16 13 |MD 47 50 42 45 54 51 50 48
Table 3.2104.5 GPS week: 2104 Day: 5 MJD: 58977
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1111 38 38 24 44 42 33 15 15 | 50 48 43 51 41 48 45 39
R02 | 1203 11 9 16 16 23 11 17 7 | 20 24 33 23 36 31 26 25
R03 | 648 9 11 12 14 14 12 14 5 | 35 36 40 32 35 35 47 36
XR04 | 646 11 10 15 22 --- 16 18 8 | 45 40 46 36 --- 55 42 43
R05 | 894 13 17 20 20 29 13 27 9 | 35 31 35 49 51 41 29 36
R07 | 516 12 11 12 13 14 9 17 5 | 36 35 33 28 41 29 24 29
R08 | 638 10 8 9 8 22 17 14 6 | 30 38 32 36 43 37 34 34
R09 | 2563 13 15 12 12 18 19 15 7 | 96 96 91 94 97 94 91 93
R11 | 2475 9 7 18 13 14 20 11 6 | 61 60 48 60 66 49 60 56
R12 | 1912 18 19 28 30 12 13 16 9 | 71 61 61 65 70 71 71 67
R13 | 1351 29 33 44 76 36 40 43 20 | 66 75 37 50 52 83 76 55
R14 | 834 14 17 19 15 10 15 23 7 | 96 96 93 96 92 95 96 93
R15 | 800 18 18 21 17 9 14 15 7 | 57 57 39 45 47 43 49 46
R16 | 1443 18 21 23 17 42 35 13 11 | 37 47 43 39 43 58 40 39
R17E | 1248 10 13 24 15 13 11 15 6 | 53 54 58 48 53 45 47 49
R18E | 635 8 11 12 16 19 8 16 6 | 21 23 24 28 28 23 25 21
R19E | 1477 29 38 51 48 72 18 40 19 | 31 39 40 53 69 37 31 31
R20E | 1251 37 40 59 69 65 36 46 23 | 88 89 70 121 104 75 77 82
R21E | 806 10 14 22 19 20 17 19 8 | 78 79 82 86 76 80 80 79
R22E | 3736 13 12 24 15 14 16 17 7 | 156 162 158 164 162 156 167 160
R23E | 1412 15 12 12 26 24 19 13 8 | 44 46 45 52 46 43 33 40
R24E | 1748 17 15 27 16 17 14 10 7 | 23 25 31 31 28 31 27 25
XR26E | 4443 15 38 --- --- --- --- 16 15 | 19 36 --- --- --- --- 29 20
------+----------------------------------------------+------------------------------------------
RMS | 1567 19 21 26 31 30 21 22 |T 54 56 53 58 60 57 54 52
WRMS | 1567 16 17 27 20 17 18 22 |NE 52 53 48 50 54 54 52 49
MEDI | 1248 13 15 20 16 19 16 16 |MD 45 47 43 49 51 45 45 40
Table 3.2104.6 GPS week: 2104 Day: 6 MJD: 58978
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1056 41 41 28 67 56 33 21 19 | 80 85 74 63 57 67 64 59
R02 | 2307 9 16 14 12 14 12 18 6 | 46 43 48 46 48 53 48 47
R03 | 791 8 14 11 14 22 10 18 6 | 59 62 63 63 66 62 57 60
XR04 | 556 18 25 23 20 --- 32 18 11 | 67 69 66 41 --- 59 51 55
R05 | 553 10 12 17 18 18 16 15 7 | 46 47 52 58 52 49 44 48
R07 | 634 10 13 10 14 11 13 13 5 | 58 64 57 59 61 61 61 59
R08 | 1004 7 10 9 9 14 13 13 5 | 50 51 50 52 51 56 59 52
R09 | 3349 13 17 13 19 13 26 16 7 | 82 81 80 83 86 85 83 82
R11 | 1427 8 10 22 11 18 14 15 6 | 73 72 62 69 63 70 77 69
R12 | 2007 18 36 31 33 13 15 21 10 | 82 97 53 70 82 72 80 73
R13 | 1201 25 33 63 65 49 56 25 21 | 110 116 45 44 110 120 113 91
R14 | 1088 16 12 27 13 12 14 12 7 | 131 126 118 113 119 121 117 120
R15 | 1157 18 21 22 13 9 16 19 7 | 71 72 46 50 58 63 61 58
R16 | 3043 25 29 45 29 33 27 15 13 | 56 59 55 65 58 71 66 58
R17E | 1426 17 16 21 19 16 13 8 7 | 71 71 71 79 77 79 75 74
R18E | 1045 7 15 11 13 15 14 16 5 | 44 48 48 47 44 49 48 45
R19E | 779 27 26 44 52 76 43 34 20 | 59 57 58 60 89 57 54 54
R20E | 1525 25 37 70 48 55 25 45 20 | 131 128 116 127 140 123 118 123
R21E | 626 10 10 27 21 22 15 14 8 | 73 71 71 68 76 71 73 71
R22E | 3842 8 17 29 17 26 15 14 8 | 135 133 133 133 139 134 135 134
R23E | 560 17 23 13 30 19 26 12 9 | 65 68 66 65 58 75 61 63
R24E | 657 16 16 26 19 12 9 13 7 | 44 44 45 52 52 45 49 46
XR26E | 8696 18 50 --- --- --- --- 19 18 | 27 41 --- --- --- --- 38 28
------+----------------------------------------------+------------------------------------------
RMS | 1708 18 22 31 31 31 23 20 |T 72 74 67 68 75 74 70 68
WRMS | 1708 17 21 31 21 18 19 20 |NE 72 74 62 62 70 72 70 66
MEDI | 1088 16 17 22 19 18 15 16 |MD 67 69 58 63 63 67 61 59
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