[IGSREPORT-27153] Wk 2095 IGLOS Final Orbits
acc
acc at igs.org
Sun Mar 22 03:58:30 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2095 (Mar 01, 2020 - Mar 07, 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 2.2095.
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:
igl2095[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2095 in the SP3 format.
igl20957.sum Combination Report for GPS Week 2095.
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 | -4.7 ns
1 | -1.7 ns
2 | -5.7 ns
3 | -3.9 ns
4 | -3.5 ns
5 | -3.9 ns
6 | -2.2 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 1.2095, 1a.2095).
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 2.2095.0-6)
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 3.2095.0-6).
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 2095 summary. (Mar 01, 2020 - Mar 07, 2020)
Table 1.2095.a GPS week : 2095 MJD: 58909.0-58915.0
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 1 11 -18 65 .09 19 15 | 18919 -182 3077 8178
| 1 1 1 19 18 17 .04 | 1499 1484
cof n/a| 0 0 2 9 3 61 .12 22 19 | 18918 -185 3075 8176
| 1 1 2 13 19 27 .06 | 1501 1473
emx n/a| 0 0 -4 71 23 -71 .07 30 30 | -4332 393 3058 8241
| 1 0 3 14 27 50 .06 | 8310 1178
esx n/a| -1 0 -3 2 -38 -67 .15 32 30 | -7123 592 3067 9984
| 1 1 2 29 19 27 .05 | 14977 1860
gfz n/a| 0 -1 1 -10 7 -31 .15 22 18 | 0 -340 3095 7783
| 0 0 2 11 15 16 .07 | 0 2050
grg n/a| 1 0 0 -84 5 -9 -.33 24 20 | -3457 -192 3074 7249
| 1 1 3 30 18 26 .04 | 630 2014
iac n/a| 0 0 2 16 16 27 -.05 18 17 | -2179 8 3074 8307
| 1 1 2 29 31 56 .05 | 1128 1116
mcc n/a| 0 -2 -7 184 -23 189 -.28 229 229 | --- --- --- ---
| 12 10 15 89 295 599 .53 | --- ---
Table 1.2095.b GPS week : 2095 MJD: 58909.0-58915.0
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 | 19 18 19 17 16 18 17 |
R02 | 7 8 7 8 7 7 7 |
R03 | 6 7 9 8 9 9 9 |
R04 | 11 8 14 13 11 11 16 |
R05 | 9 8 9 8 8 11 11 |
R07 | 8 8 8 6 8 8 12 |
R08 | 7 8 8 9 9 9 10 |
R09 | 7 6 7 6 6 8 7 |
R11 | 5 5 8 8 8 7 7 |
R12 | 7 6 9 7 8 7 8 |
R13 | 16 14 17 17 15 14 14 |
R14 | 7 5 6 6 6 7 6 |
R15 | 5 6 6 7 5 7 7 |
R16 | 13 11 13 11 10 13 16 |
R17 | 9 7 10 9 8 10 9 |
R18 | 10 9 8 8 7 7 7 |
R19 | 19 17 17 17 18 15 20 |
R20 | 18 15 15 18 16 15 15 |
R21 | 9 9 12 13 10 10 9 |
R22 | 9 10 9 10 10 9 9 |
R23 | 8 8 9 9 11 9 8 |
R26 | 23 17 10 23 13 18 21 |
Table 1.2095.c GPS week : 2095 MJD: 58909.0-58915.0
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 2095 0 | -49 -3 189 -451 456 2120 83.1 1177 1177 | -4739 0
brd 2095 1 | -27 12 141 -1969 -75 -1650 83.5 1152 1152 | -1675 0
brd 2095 2 | 28 24 131 -862 1232 -1128 80.8 2761 2761 | -5727 0
brd 2095 3 | -3 -4 206 323 -356 -5395 82.4 1536 1536 | -3869 0
brd 2095 4 | 2 24 229 -242 -862 -3880 84.5 1789 1789 | -3459 0
brd 2095 5 | 0 22 197 -426 -512 -2126 83.6 1561 1561 | -3857 0
brd 2095 6 | 21 53 108 -568 495 -4532 82.3 1336 1336 | -2212 0
-------------+------------------------------------------------------------+----------------
brd 2095 mean| -4 18 171 -599 53 -2370 82.9 1615 1615 | -3648 0
brd 2095 sdev| 26 19 44 704 717 2529 1.2 553 553 | 1390 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 2.2095.0 GPS week: 2095 Day: 0 MJD: 58909
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 16 -43 43 .09 19 15 | 19183 -894 3018 8573
cof n/a| 0 -1 1 20 1 13 .06 24 19 | 19177 -880 3015 8572
emx n/a| 0 0 0 94 29 -55 .08 30 30 | 2454 177 3008 8663
esx n/a| -3 1 -6 0 -32 -129 .12 33 33 | 5701 -298 3014 10454
gfz n/a| 0 -1 1 -7 -1 -55 .22 24 17 | 0 -1718 3062 8342
grg n/a| 3 1 1 -87 38 10 -.37 23 16 | -3805 -1774 3004 7428
iac n/a| 0 0 0 8 37 69 -.08 19 16 | -3437 -1119 3012 8786
mcc n/a| 2 1 7 166 255 191 .05 292 292 | --- --- --- ---
Table 2.2095.1 GPS week: 2095 Day: 1 MJD: 58910
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 28 -17 57 .16 17 15 | 22039 1092 3001 7671
cof n/a| 0 -1 -1 0 -26 54 .15 19 17 | 22047 1077 3001 7669
emx n/a| 0 -1 -4 62 35 22 .11 30 30 | -2408 1640 2984 7772
esx n/a| -2 0 -5 -29 -25 -56 .20 33 31 | -6125 1967 3011 9525
gfz n/a| -1 -1 -2 -13 5 -29 .08 29 19 | 0 1641 3031 7045
grg n/a| 0 0 5 -64 5 7 -.30 18 16 | -2276 1524 3019 7025
iac n/a| 0 2 0 -5 2 -66 .01 15 14 | -819 1545 3010 7753
mcc n/a| 8 -12 -17 297 52 567 -.25 263 263 | --- --- --- ---
Table 2.2095.2 GPS week: 2095 Day: 2 MJD: 58911
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 -12 0 62 .05 18 18 | 18029 -2302 2985 8189
cof n/a| 0 1 2 16 3 71 .16 20 20 | 18025 -2295 2986 8189
emx n/a| 1 -1 -2 82 11 -55 .01 30 30 | -20087 -540 2977 8275
esx n/a| -3 1 -5 -16 -74 -52 .21 31 32 | -32433 -1803 2984 10594
gfz n/a| -1 0 4 2 -6 -37 .20 22 21 | 0 -3150 3062 7850
grg n/a| 0 2 -5 -39 5 3 -.39 25 20 | -4272 -2565 2975 7448
iac n/a| 0 2 5 -30 37 2 -.03 20 19 | -3924 -638 2975 8270
mcc n/a| 13 -14 -17 171 57 1335 .23 227 227 | --- --- --- ---
Table 2.2095.3 GPS week: 2095 Day: 3 MJD: 58912
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 -2 -12 79 .05 19 15 | 19156 -983 3620 8765
cof n/a| -1 0 1 -6 -9 82 .05 22 19 | 19150 -982 3621 8768
emx n/a| 1 -1 -1 75 0 -102 .02 26 26 | -700 -700 3586 8816
esx n/a| -2 0 -1 -27 -30 -65 .13 31 28 | 11673 -467 3589 10383
gfz n/a| 0 -1 1 4 -13 -26 .21 23 20 | 0 -722 3652 8534
grg n/a| 1 0 -1 -67 11 -17 -.32 30 24 | -3299 -1001 3628 7922
iac n/a| 1 0 4 12 40 35 -.10 19 18 | -1491 -764 3598 8895
mcc n/a| 3 8 -31 52 70 -470 .01 154 154 | --- --- --- ---
Table 2.2095.4 GPS week: 2095 Day: 4 MJD: 58913
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 -10 -33 97 .06 18 13 | 17574 346 2801 7404
cof n/a| 1 0 0 4 25 99 .22 25 19 | 17590 316 2798 7401
emx n/a| 0 0 -2 60 9 -136 .01 31 32 | -5084 415 2780 7495
esx n/a| -1 1 -1 18 -29 -61 .20 31 32 | -18348 -68 2788 8590
gfz n/a| 0 -2 1 -22 21 -3 .16 20 15 | 0 -669 2679 7035
grg n/a| 3 0 0 -92 4 -7 -.27 26 23 | -3437 -134 2787 6337
iac n/a| 0 0 1 54 32 3 -.11 17 17 | -2368 -120 2794 7528
mcc n/a| 0 -11 -6 238 238 -179 .01 156 156 | --- --- --- ---
Table 2.2095.5 GPS week: 2095 Day: 5 MJD: 58914
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 2 20 -33 58 .10 21 17 | 18032 -681 3170 8322
cof n/a| 2 0 6 30 -1 59 .09 23 19 | 18017 -669 3170 8322
emx n/a| 0 -1 -7 70 0 -89 .14 31 32 | -9106 -567 3146 8300
esx n/a| 1 0 -1 49 -56 -55 .10 30 24 | -17 963 3154 10283
gfz n/a| 0 -1 0 -9 25 -25 .11 19 15 | 0 -756 3212 7775
grg n/a| 2 1 4 -128 -23 -63 -.31 23 21 | -3279 -716 3176 7446
iac n/a| -3 -1 0 27 13 112 -.08 18 17 | -1553 -461 3175 8420
mcc n/a| 0 5 14 95 -275 -121 -.83 194 194 | --- --- --- ---
Table 2.2095.6 GPS week: 2095 Day: 6 MJD: 58915
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 4 38 7 56 .10 20 15 | 18421 2148 2946 8322
cof n/a| 1 1 4 1 28 51 .10 24 18 | 18422 2135 2935 8317
emx n/a| -1 0 -10 53 78 -85 .13 34 34 | 4607 2328 2926 8370
esx n/a| -1 -1 -5 22 -22 -49 .08 33 30 | -10314 3855 2931 10060
gfz n/a| 0 0 0 -26 22 -41 .05 21 19 | 0 2989 2971 7902
grg n/a| 1 1 -2 -115 -1 3 -.32 24 20 | -3837 3320 2933 7137
iac n/a| -2 0 7 47 -47 37 .01 21 20 | -1663 1619 2954 8498
mcc n/a| -26 8 -5 266 -563 2 -1.19 318 318 | --- --- --- ---
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 3.2095.0 GPS week: 2095 Day: 0 MJD: 58909
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 841 35 33 62 48 50 24 33 --- 18 | 64 66 60 88 95 64 53 --- 64
R02E | 1758 12 11 30 11 13 14 10 185 7 | 45 45 34 47 47 41 49 83 43
R03E | 1284 9 12 25 16 14 10 11 460 6 | 64 62 61 70 64 58 62 150 62
XR04E | 987 10 16 27 20 --- 24 24 --- 10 | 43 41 39 48 --- 52 47 --- 44
R05E | 1694 11 16 34 25 17 12 15 --- 8 | 56 61 51 66 58 57 47 --- 53
R07E | 749 13 15 31 17 18 14 14 218 8 | 65 68 56 63 69 65 65 79 63
R08E | 1159 11 10 26 12 12 13 13 --- 6 | 81 80 76 79 76 85 79 --- 79
R09 | 812 13 18 13 21 22 13 13 --- 7 | 28 31 29 23 32 37 29 --- 27
R11 | 509 5 13 6 18 9 11 13 331 4 | 23 25 24 31 30 29 27 154 25
R12 | 746 7 15 12 11 15 23 13 --- 6 | 34 39 37 31 35 34 33 --- 32
R13 | 2058 22 37 36 49 42 42 22 --- 15 | 30 38 46 33 37 50 30 --- 33
R14 | 692 10 15 10 16 18 20 18 --- 7 | 27 29 31 28 32 35 33 --- 27
R15 | 1041 5 10 15 12 10 13 14 --- 5 | 28 30 25 28 28 33 33 --- 26
R16 | 2044 35 43 24 32 38 16 23 --- 13 | 32 38 39 36 42 29 30 --- 29
R17 | 571 14 11 24 38 13 13 11 --- 8 | 74 72 62 53 79 77 78 --- 71
R18 | 457 17 20 29 26 19 21 22 --- 10 | 51 52 42 45 69 70 70 --- 58
R19 | 870 34 48 41 88 29 24 34 --- 19 | 92 97 52 34 72 84 90 --- 72
R20 | 1171 42 45 46 16 32 63 18 --- 18 | 54 54 47 47 74 47 62 --- 53
R21 | 1556 5 7 27 37 14 14 19 152 8 | 69 68 50 44 76 78 77 64 67
R22 | 827 10 11 27 31 15 12 19 --- 8 | 69 68 46 41 76 65 76 --- 64
R23 | 507 13 18 13 36 18 12 13 --- 8 | 43 50 40 66 45 48 50 --- 46
XR26 | ---- 21 51 --- --- --- --- 24 --- 22 | 44 66 --- --- --- --- 63 --- 50
------+---------------------------------------------------+-----------------------------------------------
RMS | 1177 19 24 30 33 24 23 19 292 |T 50 53 45 47 56 54 53 106 49
WRMS | 1177 15 19 30 33 17 16 16 292 |NE 46 50 40 38 51 51 52 109 45
MEDI | 870 12 15 27 21 17 14 15 218 |MD 45 52 46 45 58 52 50 83 50
Table 3.2095.1 GPS week: 2095 Day: 1 MJD: 58910
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 689 28 28 57 58 61 20 26 --- 17 | 51 51 48 42 68 44 36 --- 40
R02E | 767 9 8 31 23 25 12 7 73 7 | 44 43 38 53 43 44 42 60 42
R03E | 1673 10 11 30 18 16 13 15 444 7 | 71 72 72 75 73 65 76 150 71
XR04E | 872 6 12 32 22 --- 13 10 --- 8 | 34 37 41 31 --- 32 33 --- 31
R05E | 1642 13 22 29 21 17 19 12 --- 8 | 48 49 51 41 42 44 49 --- 43
R07E | 1376 6 15 30 22 29 13 9 125 7 | 48 50 43 46 61 50 47 89 47
R08E | 2198 14 21 28 23 17 14 12 --- 7 | 68 68 68 73 68 72 76 --- 69
R09 | 1173 11 13 15 15 17 9 15 --- 6 | 27 29 24 33 40 29 32 --- 29
R11 | 692 5 7 12 13 17 12 8 329 5 | 13 15 18 17 14 12 20 161 10
R12 | 729 8 17 21 15 18 13 12 --- 6 | 15 16 18 23 23 25 15 --- 13
R13 | 666 23 35 45 55 35 25 17 --- 14 | 24 45 39 26 33 18 19 --- 19
R14 | 573 9 16 11 10 13 12 13 --- 5 | 22 27 22 25 25 19 20 --- 18
R15 | 589 8 9 13 24 17 11 10 --- 5 | 12 16 15 20 17 17 16 --- 10
R16 | 2277 18 16 18 20 47 26 14 --- 11 | 32 33 22 24 42 19 21 --- 21
R17 | 912 13 15 21 31 21 8 9 --- 7 | 45 45 45 50 49 47 46 --- 46
R18 | 516 14 16 24 21 27 24 14 --- 9 | 34 36 32 30 53 46 30 --- 35
R19 | 899 39 36 39 73 44 22 23 --- 17 | 48 42 46 23 23 38 35 --- 32
R20 | 775 29 29 41 20 44 42 16 --- 14 | 26 34 52 25 45 25 35 --- 25
R21 | 932 7 9 28 42 14 9 19 140 8 | 40 39 32 32 43 39 44 37 39
R22 | 755 7 9 32 45 17 13 18 --- 9 | 37 37 27 28 49 50 49 --- 41
R23 | 775 10 17 25 33 17 12 16 --- 8 | 33 28 23 45 37 45 39 --- 35
XR26 | ---- 17 49 --- --- --- --- 16 --- 16 | 35 59 --- --- --- --- 51 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1151 17 19 30 33 29 18 15 263 |T 36 39 36 36 42 37 37 99 34
WRMS | 1151 15 17 30 31 19 16 14 263 |NE 29 33 29 28 35 30 31 99 27
MEDI | 775 10 16 28 22 17 13 14 140 |MD 34 37 38 31 42 39 35 89 35
Table 3.2095.2 GPS week: 2095 Day: 2 MJD: 58911
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 664 33 39 56 52 52 29 25 --- 18 | 72 77 74 81 94 72 61 --- 70
R02E | 2385 9 12 27 10 10 11 16 119 6 | 45 45 38 43 47 40 41 97 41
R03E | 2100 16 17 36 13 11 20 14 305 8 | 55 57 51 47 49 55 48 179 49
XR04E | 1135 13 15 52 18 --- 21 24 --- 13 | 38 42 41 38 --- 45 48 --- 40
R05E | 1685 13 18 26 22 16 19 19 --- 8 | 44 49 43 48 49 43 45 --- 42
R07E | 1038 10 9 27 12 22 15 19 156 8 | 28 28 25 30 35 23 34 103 26
R08E |10933 12 15 25 15 19 21 20 --- 8 | 46 48 48 45 42 49 49 --- 44
R09 | 1028 10 14 15 11 13 16 18 --- 6 | 26 32 36 27 29 33 29 --- 26
R11 | 746 12 13 15 13 13 14 28 319 7 | 23 25 25 35 31 23 30 184 25
R12 | 910 18 18 28 21 19 12 19 --- 8 | 28 25 36 35 28 24 32 --- 26
R13 | 2215 30 20 40 46 38 46 27 --- 16 | 30 33 38 30 29 33 28 --- 24
R14 | 594 8 10 14 11 14 13 15 --- 5 | 24 25 29 27 21 28 21 --- 21
R15 | 1093 10 16 10 12 14 21 14 --- 6 | 28 29 27 38 38 41 26 --- 30
R16 | 1641 24 28 41 21 24 44 14 --- 13 | 34 40 38 29 23 38 28 --- 26
R17 | 964 9 14 26 45 18 11 18 --- 10 | 53 58 51 36 64 50 60 --- 51
R18 | 535 14 15 22 17 18 18 21 --- 8 | 48 51 48 44 62 47 48 --- 48
R19 | 1454 37 37 34 60 24 34 29 --- 16 | 63 59 50 43 62 42 39 --- 45
R20 | 816 26 35 50 30 24 46 24 --- 15 | 49 40 33 34 58 35 54 --- 41
R21 | 684 7 8 30 50 23 23 20 154 11 | 47 52 38 32 67 59 59 42 49
R22 | 971 11 16 23 36 14 9 15 --- 8 | 50 54 39 35 50 41 51 --- 44
R23 | 1230 12 9 15 32 24 17 13 --- 8 | 36 46 42 50 43 42 51 --- 41
XR26 | ---- 9 31 --- --- --- --- 10 --- 10 | 30 39 --- --- --- --- 33 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 2761 18 20 30 31 22 25 20 227 |T 40 43 40 39 46 41 41 121 38
WRMS | 2761 18 20 30 32 21 20 19 227 |NE 37 40 37 35 43 38 39 113 35
MEDI | 1038 12 15 27 21 18 19 19 156 |MD 38 42 38 36 43 41 41 103 41
Table 3.2095.3 GPS week: 2095 Day: 3 MJD: 58912
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 913 43 39 43 48 40 24 24 --- 17 | 56 61 59 67 72 55 40 --- 50
R02E | 3024 15 9 27 13 13 20 14 106 7 | 54 59 54 65 60 66 63 128 59
R03E | 769 14 13 29 16 14 18 14 151 8 | 103 103 94 103 98 104 99 214 99
XR04E | 905 15 21 44 28 --- 21 17 --- 13 | 32 35 32 32 --- 25 31 --- 27
R05E | 1900 14 15 24 22 17 18 14 --- 8 | 33 35 32 42 36 36 35 --- 32
R07E | 1130 12 15 23 11 11 12 12 --- 6 | 41 44 45 41 42 46 48 --- 42
R08E | 1710 13 15 25 7 23 27 18 --- 9 | 59 61 62 63 62 61 73 --- 62
R09 | 1402 7 11 13 13 17 15 16 --- 6 | 29 31 36 29 23 26 35 --- 27
R11 | 712 12 16 12 20 14 17 25 228 7 | 21 23 18 30 32 30 27 201 23
R12 | 1104 13 15 17 22 15 11 15 --- 7 | 29 34 33 25 36 24 25 --- 28
R13 | 3822 28 35 26 44 46 61 20 --- 17 | 31 29 48 34 45 28 40 --- 34
R14 | 690 11 14 10 8 8 16 19 --- 6 | 30 31 25 31 26 26 27 --- 25
R15 | 806 8 9 12 9 18 24 17 --- 6 | 28 25 25 33 24 35 28 --- 25
R16 | 1200 23 26 20 31 14 42 16 --- 11 | 32 43 24 33 36 30 25 --- 26
R17 | 1282 12 12 24 38 14 17 13 --- 9 | 62 60 49 37 66 64 60 --- 56
R18 | 701 12 18 24 12 15 19 17 --- 7 | 40 34 36 48 53 54 57 --- 46
R19 | 1397 32 41 29 61 29 55 21 --- 17 | 55 66 48 54 65 46 56 --- 47
R20 | 663 28 38 50 38 38 62 26 --- 18 | 52 73 37 44 81 39 77 --- 54
R21 | 586 5 9 35 51 26 21 25 94 12 | 59 59 40 38 74 69 76 55 59
R22 | 1429 14 11 23 36 16 12 21 --- 9 | 54 54 42 38 56 46 64 --- 50
R23 | 998 13 25 17 34 22 22 14 --- 9 | 24 24 27 45 31 30 29 --- 25
XR26 | ---- 22 45 --- --- --- --- 24 --- 23 | 19 61 --- --- --- --- 50 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1535 19 22 26 31 23 30 19 154 |T 42 47 41 44 50 44 48 149 42
WRMS | 1535 15 19 26 28 20 24 18 154 |NE 37 43 34 37 46 39 45 128 37
MEDI | 1104 13 15 24 22 16 20 17 106 |MD 33 43 37 38 45 39 40 128 34
Table 3.2095.4 GPS week: 2095 Day: 4 MJD: 58913
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1437 33 33 45 46 42 32 23 --- 16 | 42 50 58 49 66 50 38 --- 43
R02E | 5240 13 15 27 11 12 16 13 174 7 | 33 34 31 29 28 29 29 62 28
R03E | 1228 16 22 34 26 11 19 14 90 8 | 68 69 58 59 70 73 76 141 67
XR04E | 1505 20 22 34 24 --- 17 13 --- 10 | 40 41 28 29 --- 34 31 --- 29
R05E | 2669 17 17 31 18 13 14 16 --- 8 | 41 42 38 45 47 43 42 --- 40
R07E | 1517 10 15 26 22 19 18 13 --- 7 | 44 52 42 48 53 37 40 --- 42
R08E | 743 21 22 29 12 19 21 19 --- 9 | 31 32 30 30 33 30 32 --- 28
R09 | 2311 15 20 14 10 12 19 10 --- 6 | 19 32 23 24 27 31 25 --- 21
R11 | 722 11 14 17 14 15 26 25 222 8 | 16 21 19 28 29 19 24 147 18
R12 | 863 15 14 15 25 24 17 10 --- 8 | 23 27 35 36 50 39 36 --- 34
R13 | 1804 21 28 56 40 31 44 19 --- 15 | 24 45 53 31 27 23 21 --- 20
R14 | 636 7 16 15 8 12 20 15 --- 6 | 26 39 35 36 28 35 38 --- 29
R15 | 663 9 12 10 9 11 11 10 --- 4 | 23 26 26 30 21 28 30 --- 24
R16 | 1153 15 34 25 32 21 29 11 --- 9 | 18 39 27 34 24 22 20 --- 17
R17 | 1565 10 22 31 30 17 13 12 --- 8 | 58 60 50 47 66 62 57 --- 57
R18 | 1125 10 20 26 13 10 13 16 --- 6 | 47 56 38 42 45 46 47 --- 44
R19 | 1888 37 56 30 68 20 47 31 --- 17 | 53 68 54 42 51 51 52 --- 45
R20 | 561 28 40 56 28 30 57 12 --- 16 | 54 59 45 46 60 39 50 --- 48
R21 | 402 5 6 34 41 9 18 21 98 9 | 51 47 37 42 53 61 62 28 51
R22 | 1725 10 18 31 45 14 14 20 --- 10 | 50 56 34 25 47 45 54 --- 44
R23 | 441 21 24 28 41 13 23 21 --- 10 | 34 38 32 46 34 43 49 --- 36
XR26 | ---- 12 28 --- --- --- --- 14 --- 13 | 43 57 --- --- --- --- 42 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1788 18 25 31 31 20 26 17 156 |T 38 45 37 38 42 40 40 94 36
WRMS | 1788 13 19 32 32 15 23 17 156 |NE 35 44 36 36 40 38 40 87 35
MEDI | 1228 15 20 29 25 14 19 14 98 |MD 40 42 35 36 45 39 38 62 36
Table 3.2095.5 GPS week: 2095 Day: 5 MJD: 58914
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1403 33 35 63 51 41 29 26 --- 18 | 40 44 64 73 67 42 40 --- 46
R02E | 3148 12 14 28 11 12 13 12 270 6 | 46 43 47 44 47 44 48 74 44
R03E | 1138 14 17 33 22 12 20 14 122 8 | 109 107 106 108 114 106 120 114 111
XR04E | 1381 15 24 35 20 --- 18 17 --- 10 | 36 39 28 36 --- 39 37 --- 32
R05E | 2941 21 19 31 19 28 27 23 --- 11 | 62 61 58 64 61 69 52 --- 58
R07E | 1485 17 16 31 19 16 13 12 --- 8 | 71 67 66 70 65 61 78 --- 67
R08E | 623 17 23 23 17 13 22 23 --- 8 | 59 61 55 59 53 56 51 --- 53
R09 | 2808 18 16 18 17 15 21 9 --- 7 | 15 18 15 21 23 25 20 --- 15
R11 | 873 8 12 12 12 13 15 21 224 6 | 14 18 17 21 15 16 20 113 13
R12 | 1048 7 10 14 26 10 13 14 --- 6 | 17 20 23 22 20 19 26 --- 18
R13 | 1503 36 32 29 41 29 28 25 --- 14 | 33 35 24 31 38 36 33 --- 23
R14 | 1007 18 14 11 28 13 13 13 --- 7 | 14 18 18 34 22 26 13 --- 16
R15 | 578 11 13 12 21 12 20 8 --- 6 | 18 22 19 23 18 18 14 --- 14
R16 | 676 19 21 16 36 31 46 16 --- 13 | 26 28 27 35 31 27 17 --- 20
R17 | 630 12 15 34 40 12 14 18 --- 9 | 46 47 44 43 40 39 53 --- 42
R18 | 1225 11 10 30 7 11 20 13 --- 7 | 39 37 24 33 29 40 30 --- 31
R19 | 1455 34 43 41 59 20 26 19 --- 15 | 47 53 43 30 46 46 47 --- 41
R20 | 851 36 38 53 25 23 41 26 --- 15 | 39 36 24 34 31 30 29 --- 25
R21 | 585 7 12 32 39 18 12 21 112 10 | 35 43 22 27 43 34 44 41 35
R22 | 2277 13 11 29 36 16 13 12 --- 8 | 36 34 24 32 40 33 34 --- 32
R23 | 445 27 34 24 15 11 23 13 --- 8 | 32 38 31 41 47 48 37 --- 37
XR26 | ---- 16 32 --- --- --- --- 19 --- 18 | 34 38 --- --- --- --- 28 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1560 21 23 31 30 19 23 18 194 |T 39 41 37 41 42 40 39 85 36
WRMS | 1560 17 19 32 24 15 21 17 194 |NE 29 32 25 30 31 31 29 77 26
MEDI | 1138 16 16 29 22 13 20 16 122 |MD 36 38 27 34 40 39 34 74 32
Table 3.2095.6 GPS week: 2095 Day: 6 MJD: 58915
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1075 39 52 58 52 36 24 22 --- 17 | 59 66 65 72 65 53 50 --- 52
R02E | 1664 13 12 27 9 14 11 16 357 6 | 56 56 48 53 57 59 56 85 54
R03E | 974 12 15 32 21 15 19 19 324 8 | 94 96 93 98 92 92 90 141 91
XR04E | 538 18 16 32 37 --- 26 42 --- 15 | 44 41 42 45 --- 45 58 --- 41
R05E | 2855 24 15 34 28 21 11 29 --- 11 | 68 64 52 51 56 59 78 --- 59
R07E | 2094 24 26 37 32 18 14 32 466 11 | 76 77 67 74 77 76 79 163 72
R08E | 744 12 20 35 16 20 19 28 --- 10 | 83 81 81 81 77 73 85 --- 78
R09 | 1743 11 32 16 10 18 18 13 --- 6 | 19 37 20 27 36 27 24 --- 23
R11 | 1011 13 14 18 12 7 19 18 197 6 | 18 20 21 29 25 31 31 131 22
R12 | 1631 11 13 12 26 14 19 19 --- 7 | 29 31 33 39 31 32 30 --- 28
R13 | 806 19 44 23 26 38 49 17 --- 14 | 28 46 27 39 48 35 44 --- 33
R14 | 799 9 15 18 12 13 12 13 --- 5 | 25 27 21 22 33 23 29 --- 23
R15 | 1179 12 13 15 31 9 15 12 --- 7 | 29 29 27 28 28 34 28 --- 27
R16 | 647 30 23 61 30 23 47 16 --- 15 | 27 30 41 27 20 25 22 --- 18
R17 | 502 8 7 26 33 16 22 20 --- 9 | 71 70 61 54 75 73 78 --- 68
R18 | 905 13 17 23 10 11 13 18 --- 6 | 58 54 47 51 56 67 62 --- 56
R19 | 770 28 30 58 84 33 28 38 --- 20 | 85 79 55 40 91 64 93 --- 71
R20 | 1149 35 36 47 17 28 46 19 --- 15 | 54 60 32 45 66 54 53 --- 49
R21 | 1044 15 14 23 40 11 14 15 129 9 | 71 71 46 43 72 71 78 61 65
R22 | 1896 12 11 28 39 22 8 10 --- 9 | 69 70 46 43 74 61 72 --- 62
R23 | 454 15 18 27 29 9 10 15 --- 8 | 38 41 36 63 43 47 49 --- 43
XR26 | ---- 18 29 --- --- --- --- 23 --- 20 | 46 59 --- --- --- --- 41 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1335 20 24 34 33 21 24 21 318 |T 52 54 45 48 56 52 55 116 48
WRMS | 1335 15 18 34 30 19 20 20 318 |NE 44 48 36 39 49 46 48 96 41
MEDI | 1011 13 16 27 28 16 19 18 324 |MD 54 56 46 45 56 54 53 131 49
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