[IGSREPORT-28741] Wk 2213 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 24 04:26:16 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2213 (Jun 05, 2022 - Jun 11, 2022)
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 2.2213.
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:
igl2213[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2213 in the SP3 format.
igl22137.sum Combination Report for GPS Week 2213.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | -0.8 ns
1 | -0.1 ns
2 | -6.0 ns
3 | 1.4 ns
4 | 1.6 ns
5 | 1.1 ns
6 | 0.7 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
----+--------+---------------
3 | EMX | R19
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 1.2213, 1a.2213).
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 2.2213.0-6)
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 3.2213.0-6).
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 2213 summary. (Jun 05, 2022 - Jun 11, 2022)
Table 1.2213.a GPS week : 2213 MJD: 59735.0-59741.0
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 0 -13 -32 7 .13 20 16 | 33918 486 2978 8367
| 0 1 2 13 17 21 .03 | 3772 1469
emx n/a| -2 0 -10 3 29 -46 -.06 50 35 | -6343 461 2944 8016
| 1 1 2 40 27 66 .05 | 14466 782
esx n/a| -1 1 1 22 28 -2 -.10 33 26 | -4840 1170 2949 11039
| 1 1 1 13 14 39 .03 | 9190 1874
gfz n/a| 0 0 8 -2 2 13 -.09 24 17 | 0 315 2974 7978
| 1 1 3 27 19 20 .05 | 0 1436
grg n/a| 3 0 -7 -15 15 -7 .33 29 24 | -640 321 2933 7645
| 1 1 5 38 35 36 .05 | 2581 1532
iac n/a| 0 0 -3 5 2 8 -.20 22 20 | 1848 9 2940 8738
| 0 2 2 19 43 68 .04 | 3142 1135
Table 1.2213.b GPS week : 2213 MJD: 59735.0-59741.0
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 16 17 18 19 18 17 |
R02 | 7 8 6 9 7 7 8 |
R03 | 5 6 7 8 6 8 7 |
R04 | 9 6 8 9 10 7 9 |
R05 | 9 8 8 7 9 9 8 |
R07 | 6 6 9 7 6 6 7 |
R08 | 7 9 9 9 7 8 7 |
R09 | 9 8 9 8 9 9 8 |
R11 | 9 9 9 11 10 10 9 |
R12 | 10 8 9 8 9 7 9 |
R13 | 20 20 17 20 16 18 16 |
R14 | 8 9 8 9 9 8 9 |
R15 | 8 8 7 8 8 8 7 |
R17 | 8 7 8 7 6 7 9 |
R18 | 9 9 8 8 8 9 10 |
R19 | 23 22 25 23 25 23 24 |
R20 | 27 27 21 27 25 23 23 |
R21 | 9 9 10 9 10 8 8 |
R24 | 11 10 9 9 11 12 10 |
Table 1.2213.c GPS week : 2213 MJD: 59735.0-59741.0
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 2213 0 | 24 -1 161 639 317 -1440 81.7 1725 1725 | -806 0
brd 2213 1 | -22 -5 178 24 599 -1904 83.2 2065 2065 | -127 0
brd 2213 2 | -65 30 199 -1550 -758 -136 82.2 2016 2016 | -5999 0
brd 2213 3 | -26 -8 221 -1155 -1879 -869 81.3 2029 2029 | 1423 0
brd 2213 4 | -35 36 261 -1407 -2957 -8550 82.4 1454 1454 | 1562 0
brd 2213 5 | -56 -68 279 -1439 -928 1628 81.6 1170 1170 | 1144 0
brd 2213 6 | 82 -7 245 -68 700 5251 80.9 1291 1291 | 739 0
-------------+------------------------------------------------------------+----------------
brd 2213 mean| -14 -3 220 -707 -700 -860 81.9 1678 1678 | -294 0
brd 2213 sdev| 51 34 43 884 1367 4175 .7 375 375 | 2657 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 2.2213.0 GPS week: 2213 Day: 0 MJD: 59735
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 -1 -2 -38 8 .14 17 12 | 35591 -2366 2829 8263
emx n/a| 0 0 -4 7 -23 -2 -.13 53 36 | -21912 -673 2819 7887
esx n/a| 0 0 0 20 9 8 -.09 37 26 | 2632 -1918 2832 11315
gfz n/a| 1 0 7 5 8 41 -.13 27 13 | 0 -2141 2837 7970
grg n/a| 4 1 -2 -34 30 -18 .27 29 27 | 228 -2196 2825 7496
iac n/a| 0 -2 -7 -15 56 -45 -.19 21 21 | 2066 -2061 2834 8672
Table 2.2213.1 GPS week: 2213 Day: 1 MJD: 59736
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 -3 -2 -60 17 .09 20 18 | 34162 -179 2730 7189
emx n/a| -4 0 -11 32 41 27 -.05 50 35 | 5077 -232 2732 6961
esx n/a| -1 -1 0 -2 7 -5 -.09 36 31 | 1995 -274 2747 10309
gfz n/a| 0 0 9 -52 -23 -12 -.05 23 16 | 0 -970 2741 6850
grg n/a| 2 3 -2 -16 -5 43 .30 26 23 | 284 -1084 2733 6596
iac n/a| 0 -2 -1 25 70 -49 -.24 22 19 | 2222 715 2730 7650
Table 2.2213.2 GPS week: 2213 Day: 2 MJD: 59737
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 1 -3 -5 .15 17 15 | 25689 432 2777 9030
emx n/a| -3 2 -9 55 29 14 -.03 46 31 | -26771 463 2750 8890
esx n/a| 0 3 3 40 35 63 -.17 33 29 | -8798 1379 2760 11641
gfz n/a| 0 0 0 -9 -3 15 -.15 23 20 | 0 130 2804 8715
grg n/a| 2 -1 -2 -84 -47 -41 .33 29 22 | -6433 334 2725 8510
iac n/a| 0 -2 -2 17 -2 1 -.17 22 21 | -5091 1431 2748 9409
Table 2.2213.3 GPS week: 2213 Day: 3 MJD: 59738
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 -16 -19 49 .10 21 16 | 33737 1039 3557 8164
emx n/a| -3 1 -12 28 61 -43 -.11 55 33 | -12281 1307 3495 7749
esx n/a| -2 1 3 16 29 -17 -.10 35 27 | 5107 963 3504 10497
gfz n/a| 0 1 11 -4 20 -1 -.08 27 15 | 0 1801 3536 7448
grg n/a| 3 1 -5 0 6 32 .33 28 19 | 824 989 3511 7446
iac n/a| 0 -1 -2 4 -28 -69 -.19 23 22 | 3482 -492 3497 8433
Table 2.2213.4 GPS week: 2213 Day: 4 MJD: 59739
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 0 -35 -40 1 .14 22 19 | 35587 2046 2959 8199
emx n/a| -2 0 -11 -21 33 -59 .02 52 38 | 10761 1524 2917 7726
esx n/a| 0 3 0 19 42 25 -.10 33 22 | -1567 3137 2933 11056
gfz n/a| -2 0 9 -7 32 38 .01 22 17 | 0 1691 2944 7899
grg n/a| 3 0 -8 -6 22 -38 .30 29 22 | 361 2065 2897 7609
iac n/a| 2 1 -6 32 -31 36 -.27 24 22 | 4068 495 2922 8648
Table 2.2213.5 GPS week: 2213 Day: 5 MJD: 59740
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 -12 -32 4 .16 21 16 | 35901 679 2852 9247
emx n/a| 0 0 -9 -16 45 -140 -.04 46 37 | -4533 246 2789 8778
esx n/a| -1 1 4 33 38 -45 -.10 32 21 | -15897 1406 2807 11138
gfz n/a| -1 0 7 19 -4 11 -.11 22 18 | 0 828 2842 8878
grg n/a| 6 1 -11 -5 60 11 .35 29 22 | 631 310 2798 8263
iac n/a| 0 1 -3 -12 -34 70 -.18 20 18 | 3419 -483 2787 9570
Table 2.2213.6 GPS week: 2213 Day: 6 MJD: 59741
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 3 -25 -32 -20 .13 22 18 | 36760 1752 3143 8479
emx n/a| -1 1 -10 -63 17 -124 -.07 48 34 | 5252 594 3107 8122
esx n/a| -2 0 1 28 36 -47 -.10 28 22 | -17357 3503 3065 11320
gfz n/a| -2 -3 10 32 -14 0 -.10 25 18 | 0 868 3117 8091
grg n/a| 4 0 -16 40 43 -40 .43 30 30 | -375 1835 3044 7601
iac n/a| 0 2 0 -11 -11 113 -.14 19 18 | 2775 463 3066 8784
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 3.2213.0 GPS week: 2213 Day: 0 MJD: 59735
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 540 37 39 65 31 31 15 17 | 95 52 41 85 83 69 71
R02 | 2958 13 28 13 15 11 15 6 | 75 44 67 77 68 70 69
R03 | 722 6 12 11 11 17 12 5 | 75 62 70 79 77 65 72
XR04 | 918 19 18 9 --- 13 25 9 | 84 79 79 --- 72 70 76
R05 | 911 15 23 21 24 18 20 8 | 62 61 70 75 59 55 61
R07 | 704 6 20 11 11 11 23 6 | 74 61 71 82 77 79 75
R08 | 752 6 22 9 12 26 15 6 | 72 54 73 80 91 78 75
R09 | 4508 13 19 18 18 26 20 8 | 48 53 52 54 52 53 49
XR11 | 3343 --- 15 14 16 24 15 8 | --- 28 38 29 41 34 32
R12 | 1234 13 37 14 29 17 23 9 | 53 33 61 79 65 65 59
R13 | 656 30 64 56 66 30 17 19 | 78 40 46 107 65 72 68
R14 | 1263 9 27 16 18 22 17 7 | 60 43 67 74 62 79 65
R15 | 1099 10 24 14 13 21 26 7 | 53 37 52 57 50 69 53
R17 | 694 6 44 10 13 12 25 8 | 49 39 42 45 49 57 46
R18 | 924 14 20 24 19 17 25 9 | 37 38 41 35 40 50 38
R19 | 1882 24 132 51 24 69 24 23 | 63 46 45 57 66 65 53
R20 | 2727 25 111 98 52 55 33 26 | 85 68 46 97 90 89 77
R21 | 1016 9 34 25 9 22 23 8 | 48 38 49 43 52 55 47
R24 | 813 8 69 19 12 24 15 10 | 54 48 49 54 62 56 53
------+-----------------------------------------+-------------------------------------
RMS | 1724 17 53 37 27 29 21 |T 64 48 55 67 64 64 59
WRMS | 1724 12 36 26 13 27 21 |NE 64 48 55 67 64 64 59
MEDI | 924 13 27 16 16 22 20 |MD 62 46 52 74 65 65 61
Table 3.2213.1 GPS week: 2213 Day: 1 MJD: 59736
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 658 32 38 54 26 38 20 15 | 68 48 43 67 65 49 55
R02 | 1913 11 35 18 17 11 22 8 | 57 41 59 66 61 42 54
R03 | 580 11 20 13 10 15 8 5 | 56 51 44 56 64 55 54
XR04 | 925 9 18 9 --- 16 10 6 | 64 66 68 --- 63 62 63
R05 | 1353 21 19 16 24 12 13 8 | 42 47 52 57 44 42 44
R07 | 836 6 24 16 14 12 14 6 | 57 45 55 64 64 55 57
R08 | 2203 13 34 12 20 20 18 8 | 53 46 55 68 71 69 60
R09 | 4115 18 11 23 16 19 19 8 | 37 37 36 48 40 51 39
XR11 | 3554 --- 16 13 16 14 24 8 | --- 22 31 28 30 38 27
R12 | 642 10 31 13 10 22 18 7 | 40 32 46 43 63 43 44
R13 | 852 31 53 47 54 43 41 19 | 63 44 35 68 46 80 54
R14 | 662 16 27 17 18 15 25 8 | 49 44 62 68 63 77 60
R15 | 652 11 29 12 19 18 14 7 | 53 41 47 61 56 50 51
R17 | 613 10 35 8 11 14 19 7 | 26 23 26 21 28 36 24
R18 | 976 17 27 21 14 19 19 8 | 23 28 25 22 30 34 23
R19 | 3481 44 111 55 32 32 26 21 | 60 52 36 44 27 40 38
R20 | 4888 29 114 98 29 55 37 26 | 38 100 46 40 40 35 37
R21 | 760 10 37 27 10 19 21 9 | 26 23 35 30 33 31 27
R24 | 1954 7 59 16 15 26 17 10 | 28 38 36 32 34 35 30
------+-----------------------------------------+-------------------------------------
RMS | 2065 20 50 36 23 26 22 |T 46 43 44 49 48 48 44
WRMS | 2065 18 35 31 16 23 19 |NE 46 43 44 49 48 48 44
MEDI | 925 11 31 16 16 19 19 |MD 49 44 44 48 46 43 44
Table 3.2213.2 GPS week: 2213 Day: 2 MJD: 59737
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 650 24 42 61 24 41 35 17 | 78 62 47 75 80 89 71
R02 | 1522 13 23 15 11 12 9 6 | 66 47 53 59 57 57 58
R03 | 598 8 19 11 24 8 21 7 | 61 51 68 80 58 52 62
XR04 | 725 13 20 17 --- 23 11 8 | 67 64 59 --- 61 73 64
R05 | 1795 8 21 15 15 21 20 7 | 46 58 52 46 62 56 49
R07 | 1283 11 29 17 22 22 20 8 | 64 49 72 85 60 83 69
R08 | 1681 13 24 14 18 14 28 8 | 58 47 70 58 66 79 62
R09 | 4498 18 13 26 20 26 19 9 | 40 47 55 49 46 46 42
XR11 | 4010 --- 16 13 15 25 18 9 | --- 29 29 29 34 27 26
R12 | 522 10 36 16 14 27 22 9 | 55 39 57 60 69 51 54
R13 | 975 36 48 36 45 43 16 16 | 63 48 44 54 58 50 50
R14 | 836 13 23 17 12 15 22 7 | 50 47 63 58 65 61 55
R15 | 1048 9 25 11 12 17 19 6 | 55 46 56 56 51 64 54
R17 | 737 7 36 21 26 10 12 8 | 34 34 25 43 35 36 33
R18 | 825 14 27 19 19 12 13 7 | 25 23 29 34 28 27 25
R19 | 4268 32 128 57 26 72 22 24 | 53 32 31 44 58 35 40
R20 | 3459 18 78 76 42 46 22 20 | 55 58 39 64 65 50 52
R21 | 646 10 32 22 16 15 34 9 | 33 32 38 32 36 43 32
R24 | 1789 11 39 23 16 15 15 8 | 32 35 29 36 46 35 31
------+-----------------------------------------+-------------------------------------
RMS | 2015 17 46 33 23 29 22 |T 51 44 48 53 54 53 48
WRMS | 2015 15 31 29 20 22 21 |NE 51 44 48 53 54 53 48
MEDI | 1048 13 27 17 18 21 20 |MD 55 47 52 54 58 51 52
Table 3.2213.3 GPS week: 2213 Day: 3 MJD: 59738
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 709 38 36 56 36 37 30 17 | 79 42 32 74 48 77 57
R02 | 1591 7 29 9 19 14 31 8 | 59 39 60 67 49 79 58
R03 | 664 10 20 18 13 10 27 7 | 66 47 65 72 61 45 59
XR04 | 652 16 21 10 --- 16 22 8 | 52 41 51 --- 40 59 48
R05 | 1346 14 21 14 12 13 21 7 | 43 39 47 42 39 40 38
R07 | 1474 8 24 16 21 12 15 7 | 66 56 61 85 69 73 68
R08 | 1133 24 29 11 17 16 25 9 | 54 45 76 83 78 82 69
R09 | 4190 15 22 16 21 20 10 8 | 14 24 24 33 24 21 17
XR11 | 3992 --- 18 15 15 30 20 10 | --- 20 26 28 22 28 18
R12 | 667 13 34 14 11 17 22 8 | 53 32 56 58 55 52 50
R13 | 890 41 57 55 59 36 15 20 | 80 35 46 105 55 76 65
R14 | 753 12 23 23 16 19 24 8 | 48 38 66 51 66 63 54
R15 | 836 8 26 15 23 14 22 8 | 52 38 45 60 49 54 48
R17 | 649 14 25 9 17 12 19 7 | 29 22 30 36 36 42 30
R18 | 1288 17 27 18 10 16 12 7 | 23 20 29 23 30 27 23
R19 | 4602 33 173 64 29 66 16 23 | 54 39 39 60 64 49 51
R20 | 3977 25 86 91 55 61 37 26 | 51 51 37 71 79 66 54
R21 | 596 16 31 11 16 15 31 9 | 26 25 26 28 31 32 23
R24 | 1342 11 49 14 17 14 12 9 | 39 33 35 40 46 39 37
------+-----------------------------------------+-------------------------------------
RMS | 2030 21 55 35 27 28 23 |T 49 36 44 56 49 52 45
WRMS | 2030 16 33 27 15 19 22 |NE 49 36 44 56 49 52 45
MEDI | 1133 14 27 15 17 16 22 |MD 52 38 45 58 49 52 50
Table 3.2213.4 GPS week: 2213 Day: 4 MJD: 59739
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 775 49 41 56 39 26 23 18 | 78 39 36 68 54 61 55
R02 | 1436 8 29 14 11 15 23 7 | 58 39 50 58 47 69 54
R03 | 648 10 23 16 12 10 14 6 | 62 42 51 61 57 59 56
XR04 | 770 16 15 16 --- 11 31 9 | 61 51 57 --- 58 55 55
R05 | 756 16 35 15 24 18 20 9 | 52 44 57 63 56 48 51
R07 | 961 10 21 8 16 11 15 5 | 56 44 57 65 63 55 57
R08 | 1448 14 25 7 8 19 20 7 | 54 45 61 63 70 70 61
R09 | 3020 15 21 26 15 12 30 9 | 37 44 48 50 41 53 41
XR11 | 4504 --- 20 20 16 23 14 9 | --- 36 35 34 37 40 31
R12 | 634 9 37 19 23 19 23 9 | 57 42 65 72 65 59 59
R13 | 763 24 65 40 39 27 19 15 | 76 47 45 89 64 68 65
R14 | 939 11 32 18 13 13 33 9 | 58 44 71 64 61 79 63
R15 | 606 12 25 10 17 19 28 8 | 55 50 63 75 63 74 63
R17 | 894 7 31 15 7 12 12 6 | 45 40 45 46 48 47 44
R18 | 1447 15 33 27 10 11 17 8 | 41 37 44 41 45 45 41
R19 | 3198 44 138 43 28 71 35 25 | 49 50 54 57 49 64 47
R20 | 1180 35 81 87 32 63 40 25 | 63 43 51 49 58 60 47
R21 | 767 15 46 24 21 17 18 9 | 42 35 39 52 49 46 42
R24 | 1672 12 57 17 12 35 18 10 | 48 41 49 48 63 52 47
------+-----------------------------------------+-------------------------------------
RMS | 1454 22 52 33 22 29 24 |T 55 42 51 58 55 58 51
WRMS | 1454 19 38 22 17 22 22 |NE 55 42 51 58 55 58 51
MEDI | 939 14 32 18 16 18 20 |MD 55 43 51 58 57 59 54
Table 3.2213.5 GPS week: 2213 Day: 5 MJD: 59740
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 735 40 42 63 39 22 14 17 | 65 47 40 68 71 51 53
R02 | 1376 9 32 11 13 12 15 6 | 54 41 49 57 46 53 50
R03 | 518 9 31 11 17 17 21 7 | 57 45 55 66 50 70 57
XR04 | 1111 15 16 13 --- 16 10 7 | 69 71 65 --- 59 59 63
R05 | 1039 13 38 17 13 12 23 8 | 65 54 64 62 67 73 63
R07 | 888 5 24 10 10 14 14 5 | 50 45 54 44 52 45 47
R08 | 837 11 18 15 14 19 22 7 | 51 46 63 60 58 49 53
R09 | 2785 14 21 25 23 20 10 8 | 52 54 64 53 50 50 52
XR11 | 3657 --- 19 12 22 24 21 10 | --- 39 38 49 26 38 36
R12 | 556 13 26 15 10 17 16 7 | 53 40 51 47 51 36 45
R13 | 437 33 56 41 51 30 33 17 | 74 45 47 95 65 48 62
R14 | 1337 14 32 18 17 15 17 8 | 57 40 66 60 57 58 56
R15 | 809 9 30 12 11 22 19 7 | 70 57 63 67 66 73 67
R17 | 1486 8 35 13 15 15 15 7 | 32 41 26 26 41 33 30
R18 | 720 13 25 24 18 16 23 8 | 26 29 22 19 27 39 24
R19 | 1251 49 103 35 23 78 22 22 | 48 60 39 44 28 31 34
R20 | 1048 27 79 89 28 50 31 22 | 37 40 48 32 37 30 30
R21 | 500 9 41 15 8 17 19 7 | 41 35 46 40 37 40 38
R24 | 1281 16 63 14 20 39 13 11 | 35 32 31 43 51 28 33
------+-----------------------------------------+-------------------------------------
RMS | 1169 21 46 32 22 29 20 |T 52 45 49 51 49 47 47
WRMS | 1169 16 37 21 18 22 18 |NE 52 45 49 51 49 47 47
MEDI | 1039 13 32 15 17 17 19 |MD 52 45 49 49 51 48 50
Table 3.2213.6 GPS week: 2213 Day: 6 MJD: 59741
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 526 43 48 41 35 40 17 16 | 89 61 46 75 80 62 66
R02 | 1195 10 35 9 21 15 16 7 | 81 61 70 82 67 81 74
R03 | 572 11 23 11 15 22 16 7 | 78 67 76 86 84 77 78
XR04 | 1072 21 19 12 --- 21 15 9 | 87 83 84 --- 71 70 78
R05 | 1121 14 26 14 26 20 13 8 | 75 73 69 81 70 72 72
R07 | 2081 6 29 15 14 14 16 6 | 72 62 70 78 74 68 70
R08 | 695 13 28 14 11 18 13 6 | 67 61 75 78 84 71 72
R09 | 3018 16 13 21 19 11 15 7 | 57 59 64 61 58 58 58
XR11 | 3510 --- 19 18 17 23 17 9 | --- 39 34 39 43 34 34
R12 | 734 17 31 15 20 16 24 9 | 73 54 71 81 71 59 67
R13 | 705 42 40 38 47 33 13 16 | 103 77 61 109 68 79 81
R14 | 1229 10 33 19 19 21 18 8 | 84 67 94 95 84 79 84
R15 | 1026 11 32 9 13 17 19 7 | 95 79 90 95 87 96 91
R17 | 954 8 35 14 14 24 24 8 | 52 43 44 50 57 52 49
R18 | 988 11 27 28 12 23 22 9 | 36 37 43 41 47 45 39
R19 | 1079 45 116 42 39 76 27 24 | 77 41 59 78 66 70 64
R20 | 1524 29 92 75 40 49 28 22 | 78 46 37 75 81 79 64
R21 | 656 13 36 14 22 16 14 8 | 53 46 47 53 56 54 50
R24 | 1306 18 52 15 14 21 17 9 | 59 35 54 58 67 62 57
------+-----------------------------------------+-------------------------------------
RMS | 1291 22 48 28 25 30 19 |T 73 57 62 73 69 66 65
WRMS | 1291 18 34 22 18 30 18 |NE 73 57 62 73 69 66 65
MEDI | 1072 13 32 15 19 21 17 |MD 75 61 64 78 70 70 67
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