[IGSREPORT-25438] Wk 1959 IGLOS Final Orbits
acc
acc at igs.org
Sat Aug 12 05:01:46 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1959 (Jul 23, 2017 - Jul 29, 2017)
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 2.1959.
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:
igl1959[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1959 in the SP3 format.
igl19597.sum Combination Report for GPS Week 1959.
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 | -18.7 ns
1 | -21.4 ns
2 | -22.2 ns
3 | -16.7 ns
4 | -20.0 ns
5 | -19.7 ns
6 | 1.4 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1959, 1a.1959).
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 2.1959.0-6)
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 3.1959.0-6).
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 1959 summary. (Jul 23, 2017 - Jul 29, 2017)
Table 1.1959.a GPS week : 1959 MJD: 57957.0-57963.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 4 -47 -10 55 .07 32 33 | -8842 359 3157 11059
| 0 0 1 20 25 17 .03 | 8499 1993
cof n/a| 0 2 5 -28 14 72 .13 36 35 | -8840 341 3157 11059
| 1 1 3 24 11 30 .03 | 8496 1984
emx n/a| 0 0 7 17 -34 3 .04 21 21 | -23114 -264 3167 10216
| 0 0 2 10 16 23 .03 | 14713 1154
esx n/a| 0 0 -1 5 23 -6 .14 17 15 | -18084 -1339 3169 12908
| 0 1 1 18 17 38 .03 | 9325 1514
gfz n/a| 0 0 -3 -25 45 49 .08 23 20 | 0 361 3171 10707
| 1 1 1 15 23 16 .04 | 0 1993
grg n/a| 0 0 -4 -54 24 -54 -.37 32 29 | -17024 508 3158 10201
| 1 1 5 16 18 67 .04 | 7661 1848
iac n/a| 0 -1 -2 48 -34 -14 -.08 20 20 | -15697 157 3166 10152
| 1 0 2 30 20 28 .06 | 8041 836
mcc n/a| 2 2 4 54 -2 -542 -.19 124 124 | --- --- --- ---
| 7 9 11 54 49 369 .24 | --- ---
Table 1.1959.b GPS week : 1959 MJD: 57957.0-57963.0
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 | 9 11 10 10 12 15 15 |
R02 | 7 8 8 8 7 8 10 |
R03 | 8 6 8 8 8 6 7 |
R04 | 7 10 6 7 8 8 7 |
R05 | 11 13 14 13 14 10 16 |
R06 | 8 9 11 7 9 12 10 |
R07 | 6 9 8 10 10 8 8 |
R08 | 10 8 7 7 8 8 8 |
R09 | 7 9 8 9 7 7 11 |
R10 | 10 8 8 6 8 9 7 |
R11 | 6 6 8 7 8 6 7 |
R13 | 8 7 9 9 8 8 7 |
R15 | 17 15 11 11 11 8 9 |
R16 | 12 11 10 11 12 12 12 |
R17 | 11 11 11 9 8 11 11 |
R18 | 8 9 9 10 7 9 9 |
R19 | 16 16 14 14 15 14 16 |
R20 | 17 16 13 12 15 16 16 |
R21 | 11 11 10 12 12 12 12 |
R22 | 10 10 10 11 11 12 12 |
R23 | 9 10 10 8 10 10 11 |
R24 | 14 15 15 16 18 18 19 |
R26 | 20 23 17 26 18 14 18 |
Table 1.1959.c GPS week : 1959 MJD: 57957.0-57963.0
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 1959 0 | -3 -31 98 730 -1575 4134 84.2 1601 1601 | -18726 0
brd 1959 1 | 23 6 123 -384 -1051 3600 82.1 1615 1615 | -21362 0
brd 1959 2 | 8 0 123 -632 -226 3537 83.8 1404 1404 | -22201 0
brd 1959 3 | -43 21 179 -786 255 6411 85.5 1550 1550 | -16687 0
brd 1959 4 | 32 10 89 318 -685 4245 83.6 1419 1419 | -19985 0
brd 1959 5 | -28 13 87 1053 971 -313 83.5 1395 1395 | -19735 0
brd 1959 6 | 0 -17 98 1104 598 -791 84.9 1661 1661 | 1400 0
-------------+------------------------------------------------------------+----------------
brd 1959 mean| -1 0 114 200 -244 2974 83.9 1520 1520 | -16756 0
brd 1959 sdev| 27 18 32 800 917 2597 1.1 112 112 | 8202 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 2.1959.0 GPS week: 1959 Day: 0 MJD: 57957
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 -71 -45 65 .10 30 29 | -11932 -685 2917 10884
cof n/a| 2 2 8 -51 -3 35 .16 36 32 | -11919 -723 2920 10887
emx n/a| -1 0 9 36 -15 14 .01 19 19 | -17049 26 2921 9974
esx n/a| 0 1 0 17 23 -24 .10 16 16 | -15277 -830 2916 12422
gfz n/a| -2 -2 -2 -35 26 25 .01 22 18 | 0 -696 2919 10369
grg n/a| 0 -3 -14 -47 7 -65 -.36 34 29 | -18393 -813 2869 9995
iac n/a| 0 0 -1 80 -5 10 -.02 26 26 | -17211 -321 2929 10029
mcc n/a| -1 -7 8 118 -15 -172 -.36 121 121 | --- --- --- ---
Table 2.1959.1 GPS week: 1959 Day: 1 MJD: 57958
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 2 7 -73 -28 33 .10 32 34 | -15455 1466 3297 11174
cof n/a| 0 1 9 -56 12 51 .11 36 38 | -15454 1455 3296 11175
emx n/a| 0 0 8 25 -11 -48 .04 21 21 | -20240 512 3302 10405
esx n/a| 0 0 0 -25 37 -35 .15 19 18 | -17618 -2604 3304 12929
gfz n/a| 0 0 -4 -19 41 35 .11 22 21 | 0 1352 3301 10841
grg n/a| -1 -2 -7 -71 26 40 -.36 29 28 | -21968 1308 3305 10546
iac n/a| 2 -2 -3 96 -52 8 -.03 21 22 | -20692 788 3294 10341
mcc n/a| -6 -3 -7 112 13 -232 .23 139 139 | --- --- --- ---
Table 2.1959.2 GPS week: 1959 Day: 2 MJD: 57959
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 -50 -7 52 .02 33 34 | -14391 -915 3232 10903
cof n/a| 0 2 4 -43 8 52 .07 35 35 | -14395 -937 3229 10903
emx n/a| 0 -1 8 12 -34 13 .04 19 19 | -16951 -1694 3240 10137
esx n/a| 0 0 -2 -13 4 -18 .16 17 15 | -10828 -132 3245 12948
gfz n/a| 0 1 -3 -12 47 48 .05 23 19 | 0 -565 3233 10440
grg n/a| 0 2 -8 -39 6 -36 -.43 32 30 | -21794 -673 3249 10171
iac n/a| -1 -1 0 42 -21 -17 -.02 18 18 | -21178 -489 3228 9958
mcc n/a| 0 -6 1 56 -63 -129 -.11 132 132 | --- --- --- ---
Table 2.1959.3 GPS week: 1959 Day: 3 MJD: 57960
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 -35 -10 66 .06 31 32 | -9817 3542 3095 10919
cof n/a| -1 1 0 15 7 87 .17 34 34 | -9798 3494 3091 10918
emx n/a| 0 0 11 19 -44 10 .04 20 20 | -38016 906 3110 9963
esx n/a| 1 0 -3 19 3 -52 .15 15 14 | -26122 644 3135 12597
gfz n/a| -1 -1 -3 -6 32 64 .09 24 22 | 0 2914 3139 10570
grg n/a| 0 0 0 -55 54 21 -.34 30 28 | -18368 3217 3099 10168
iac n/a| 0 0 -7 18 -20 15 -.11 18 18 | -16303 1241 3117 10015
mcc n/a| 13 17 -4 64 -14 -724 -.02 130 130 | --- --- --- ---
Table 2.1959.4 GPS week: 1959 Day: 4 MJD: 57961
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 -14 -9 30 .03 34 32 | -9069 -1796 3052 11916
cof n/a| 0 2 2 -14 26 56 .13 34 33 | -9069 -1803 3052 11917
emx n/a| 1 0 7 5 -31 16 .00 22 22 | -21861 -1294 3064 10962
esx n/a| -1 0 -2 23 15 50 .13 17 15 | -13594 -3005 3054 13895
gfz n/a| 0 -1 -4 -15 57 73 .14 22 19 | 0 -1416 3051 11446
grg n/a| 0 0 -5 -62 37 -112 -.43 33 30 | -19363 -1231 3072 10820
iac n/a| 0 -1 -1 16 -61 -62 -.15 18 18 | -17759 -664 3055 10862
mcc n/a| 10 7 6 32 29 -950 -.31 122 122 | --- --- --- ---
Table 2.1959.5 GPS week: 1959 Day: 5 MJD: 57962
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 -46 36 70 .08 34 35 | -10937 -1144 3319 10981
cof n/a| 2 5 3 -25 25 117 .11 38 37 | -10944 -1136 3321 10979
emx n/a| 0 -1 5 10 -45 9 .09 22 23 | -46104 -1340 3330 10335
esx n/a| 0 2 -1 10 26 -3 .10 16 14 | -34839 -3037 3321 13486
gfz n/a| 1 0 -2 -43 21 42 .06 24 20 | 0 -1896 3320 10579
grg n/a| -2 1 0 -76 8 -86 -.33 33 30 | -19308 -869 3328 10282
iac n/a| 0 -2 0 53 -28 -36 -.13 19 19 | -18828 -527 3336 10077
mcc n/a| -4 2 3 42 82 -1004 -.35 115 115 | --- --- --- ---
Table 2.1959.6 GPS week: 1959 Day: 6 MJD: 57963
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 5 -39 -8 72 .07 33 33 | 9706 2051 3189 10638
cof n/a| 1 0 7 -19 28 104 .15 37 36 | 9697 2042 3191 10640
emx n/a| 0 -1 4 14 -58 12 .05 22 21 | -1578 1033 3202 9740
esx n/a| 0 0 -2 7 53 38 .19 18 16 | -8312 -412 3208 12080
gfz n/a| -1 1 -6 -43 90 58 .07 28 25 | 0 2836 3239 10707
grg n/a| 0 -1 0 -31 29 -143 -.35 32 27 | 25 2623 3190 9430
iac n/a| 2 0 1 28 -53 -19 -.12 20 20 | 2087 1073 3205 9787
mcc n/a| 6 9 26 -43 -49 -583 -.42 109 109 | --- --- --- ---
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 3.1959.0 GPS week: 1959 Day: 0 MJD: 57957
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 | 998 28 39 20 23 14 18 13 --- 9 | 71 79 53 31 32 48 37 --- 40
R02 | 911 16 20 12 9 14 24 16 149 6 | 59 64 53 47 43 56 39 59 47
R03 | 1797 20 21 17 10 21 26 17 114 8 | 64 69 56 51 48 57 45 20 51
R04 | 1688 12 9 10 10 15 19 23 --- 6 | 62 61 55 56 55 42 48 --- 53
R05 | 1495 32 50 16 21 22 41 22 --- 11 | 59 64 51 59 60 41 39 --- 50
R06 | 1240 14 17 9 13 11 39 21 --- 8 | 23 26 32 38 35 14 31 --- 28
R07 | 1002 19 15 10 7 14 17 18 154 6 | 67 63 57 51 45 54 46 42 52
R08 | 800 13 18 15 8 24 42 25 --- 9 | 65 68 62 59 49 76 43 --- 57
R09E | 4883 16 18 17 12 15 18 18 --- 7 | 58 57 53 56 62 57 56 --- 56
R10E | 703 13 13 19 20 19 24 32 --- 9 | 40 43 37 41 41 48 48 --- 39
R11E | 2059 12 16 14 12 18 19 8 98 6 | 48 45 45 47 51 47 44 34 45
R13E | 1683 13 20 13 16 17 21 19 --- 7 | 29 34 28 39 31 28 36 --- 29
R15E | 1286 21 22 24 16 26 93 34 --- 17 | 113 112 103 112 110 172 101 --- 112
R16E | 1394 22 28 22 24 15 28 45 --- 12 | 45 65 56 59 54 61 57 --- 52
R17 | 608 45 51 22 9 24 25 25 --- 11 | 75 78 51 46 37 45 38 --- 45
R18 | 1251 28 30 11 12 20 21 17 --- 8 | 63 64 46 50 31 51 40 --- 44
R19 | 1271 67 65 30 20 44 24 31 --- 16 | 89 94 57 58 48 52 35 --- 51
R20 | 1247 61 81 42 13 29 51 23 --- 16 | 83 96 30 44 40 37 32 --- 37
R21 | 761 45 46 14 8 25 19 29 67 10 | 72 72 40 38 28 41 34 87 37
R22 | 829 42 44 14 8 27 23 20 --- 10 | 76 78 44 44 33 53 32 --- 43
R23 | 762 16 16 20 27 13 23 14 --- 9 | 33 36 34 57 42 28 45 --- 40
R24 | 1052 24 35 17 28 21 42 53 --- 14 | 52 58 49 58 44 47 58 --- 45
XR26 | ---- 21 195 --- --- --- --- 19 --- 20 | 36 158 --- --- --- --- 34 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1601 30 36 19 16 22 34 26 121 |T 60 68 49 51 46 52 44 48 47
WRMS | 1601 29 32 19 16 18 29 26 121 |NE 61 72 48 49 41 46 39 52 44
MEDI | 1240 21 22 16 12 19 24 21 114 |MD 62 64 51 50 43 48 40 42 45
Table 3.1959.1 GPS week: 1959 Day: 1 MJD: 57958
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 | 1284 31 43 23 19 20 23 30 --- 11 | 58 65 49 55 37 51 26 --- 42
R02 | 672 24 20 17 21 13 18 14 198 8 | 50 49 42 31 32 46 29 86 34
R03 | 1911 16 16 11 8 13 22 13 121 6 | 47 47 41 36 38 39 33 11 37
R04 | 1619 16 11 18 12 29 33 15 --- 9 | 42 40 38 35 33 59 39 --- 36
R05 | 1642 28 31 13 29 14 29 42 --- 12 | 48 57 48 62 60 45 27 --- 45
R06 | 904 19 23 24 12 22 15 25 --- 9 | 18 22 29 28 29 22 34 --- 24
R07 | 716 12 20 11 19 15 31 18 137 8 | 48 53 41 57 57 28 35 27 42
R08 | 918 15 17 11 22 8 21 23 --- 8 | 49 52 44 58 42 33 35 --- 42
R09E | 4728 21 22 29 12 18 25 14 --- 9 | 53 54 57 46 49 49 51 --- 46
R10E | 1076 12 17 23 13 17 17 12 --- 7 | 49 53 45 56 51 58 55 --- 50
R11E | 2195 13 12 12 9 21 14 13 143 6 | 46 48 38 44 42 41 46 54 40
R13E | 1288 18 15 15 13 17 19 14 --- 7 | 27 29 33 34 32 23 23 --- 27
R15E | 1397 23 20 19 23 22 69 19 --- 14 | 132 130 123 139 139 114 132 --- 128
R16E | 1700 27 29 30 23 20 21 22 --- 10 | 37 46 48 42 40 41 46 --- 37
R17 | 621 45 53 24 10 22 20 27 --- 11 | 52 56 43 37 32 39 30 --- 35
R18 | 880 33 39 18 15 26 18 15 --- 9 | 38 41 33 30 21 25 25 --- 25
R19 | 1300 63 68 24 24 36 38 28 --- 15 | 50 54 43 36 33 50 28 --- 34
R20 | 1486 71 81 37 14 28 26 28 --- 15 | 58 64 43 30 36 22 32 --- 26
R21 | 1189 47 53 15 12 28 20 17 61 10 | 43 50 31 31 30 29 27 65 27
R22 | 1195 46 51 12 10 25 23 18 --- 10 | 43 47 25 27 32 34 25 --- 26
R23 | 805 16 16 27 27 15 20 15 --- 9 | 22 22 22 35 29 25 29 --- 23
R24 | 863 18 28 29 39 29 50 17 --- 14 | 50 62 38 69 49 49 41 --- 45
XR26 | ---- 28 80 --- --- --- --- 18 --- 22 | 44 80 --- --- --- --- 36 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1615 32 36 21 19 22 29 21 139 |T 48 53 43 46 42 41 38 48 39
WRMS | 1615 34 38 21 18 21 28 22 139 |NE 44 50 38 41 36 37 31 47 34
MEDI | 1195 23 23 18 14 20 21 18 137 |MD 48 52 41 36 36 39 33 54 36
Table 3.1959.2 GPS week: 1959 Day: 2 MJD: 57959
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 | 1353 44 40 11 16 12 24 18 --- 9 | 69 63 41 40 35 45 39 --- 40
R02 | 619 19 22 16 19 21 24 15 227 8 | 50 54 47 53 23 31 29 132 38
R03 | 1410 15 17 16 11 13 39 11 115 8 | 48 52 50 42 41 35 45 13 41
R04 | 900 15 28 14 6 9 30 8 --- 6 | 42 53 42 36 34 31 37 --- 36
R05 | 1235 43 33 17 22 23 60 22 --- 13 | 41 34 36 34 32 53 26 --- 29
R06 | 863 30 35 29 24 20 12 19 --- 10 | 15 19 24 45 35 29 26 --- 25
R07 | 687 23 18 18 18 17 20 12 107 8 | 47 45 46 28 42 46 31 65 36
R08 | 478 11 13 12 9 15 28 10 --- 6 | 49 52 53 51 51 39 49 --- 48
R09E | 4448 18 20 11 20 16 24 18 --- 8 | 33 35 32 42 37 35 32 --- 32
R10E | 1086 25 26 24 12 10 23 13 --- 8 | 38 40 36 34 30 35 31 --- 30
R11E | 1098 15 17 21 15 19 16 12 97 7 | 39 42 45 40 35 30 35 85 36
R13E | 1212 15 18 13 15 18 35 18 --- 8 | 32 35 32 38 34 31 33 --- 31
R15E | 1051 26 30 20 23 24 29 29 --- 11 | 118 120 116 112 117 118 102 --- 110
R16E | 1836 31 23 22 21 16 23 22 --- 10 | 44 50 42 53 44 47 50 --- 43
R17 | 664 41 43 21 10 28 22 21 --- 10 | 62 64 48 48 40 32 33 --- 41
R18 | 782 30 32 16 15 29 16 20 --- 9 | 53 55 48 50 32 51 31 --- 41
R19 | 720 69 67 20 12 36 20 23 --- 13 | 69 67 42 40 31 44 25 --- 35
R20 | 972 55 76 23 18 27 41 22 --- 13 | 51 69 33 35 24 29 23 --- 25
R21 | 1241 42 41 20 11 32 15 16 30 10 | 50 47 32 30 19 25 29 60 26
R22 | 1158 45 45 18 9 26 15 17 --- 9 | 54 56 33 31 30 26 25 --- 29
R23 | 769 18 15 21 24 16 34 17 --- 10 | 26 30 30 51 45 32 36 --- 35
R24 | 1112 17 23 18 15 38 76 17 --- 14 | 59 63 67 60 58 65 65 --- 62
XR26 | ---- 24 109 --- --- --- --- 11 --- 16 | 33 109 --- --- --- --- 28 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1403 33 35 19 17 23 32 18 132 |T 48 54 44 45 39 41 37 71 39
WRMS | 1403 34 35 19 15 19 30 18 132 |NE 48 54 42 42 35 38 33 67 36
MEDI | 1051 25 28 18 15 19 24 17 107 |MD 48 52 42 40 35 35 32 65 36
Table 3.1959.3 GPS week: 1959 Day: 3 MJD: 57960
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 | 1573 47 48 9 16 17 22 15 --- 9 | 72 72 36 34 36 53 35 --- 39
R02 | 684 27 26 18 11 12 16 20 156 8 | 61 57 50 41 33 41 25 125 39
R03 | 1637 18 25 20 11 15 15 19 127 7 | 53 55 55 50 41 46 36 21 45
R04 | 1438 17 13 14 12 9 21 13 --- 6 | 46 41 40 38 41 44 33 --- 38
R05 | 879 37 42 14 18 33 49 18 --- 12 | 38 45 39 46 56 48 37 --- 40
R06 | 1203 14 15 15 14 18 19 12 --- 6 | 16 18 27 28 23 35 24 --- 21
R07 | 764 21 24 28 16 21 27 19 138 9 | 55 55 59 44 38 55 30 84 42
R08 | 666 18 18 17 14 17 20 12 --- 7 | 50 45 44 29 42 42 39 --- 36
R09E | 4858 16 21 27 10 17 34 15 --- 9 | 25 27 19 28 35 49 26 --- 25
R10E | 1214 10 15 16 12 12 12 14 --- 6 | 53 56 48 47 43 51 48 --- 46
R11E | 1114 11 7 14 16 23 16 14 144 7 | 32 33 31 35 23 33 36 104 29
R13E | 1035 18 23 17 14 16 23 24 --- 8 | 32 36 33 32 29 32 23 --- 27
R15E | 1228 25 35 22 25 32 24 18 --- 11 | 72 70 73 78 85 70 67 --- 72
R16E | 1696 22 34 22 27 20 27 23 --- 11 | 50 66 61 55 48 60 45 --- 48
R17 | 787 35 38 17 9 23 21 18 --- 9 | 62 65 42 40 32 47 32 --- 39
R18 | 688 26 26 15 11 39 18 17 --- 9 | 58 57 47 53 47 57 42 --- 47
R19 | 1296 64 64 26 12 34 26 26 --- 14 | 78 81 41 46 36 47 27 --- 40
R20 | 1090 50 42 25 13 26 27 21 --- 11 | 52 53 36 30 27 35 32 --- 25
R21 | 1123 43 49 23 8 35 35 21 65 12 | 52 58 34 31 23 38 21 29 27
R22 | 684 40 43 24 14 33 19 18 --- 10 | 55 57 39 37 30 33 22 --- 31
R23 | 804 12 16 16 17 11 28 13 --- 7 | 28 38 37 45 35 24 36 --- 34
R24 | 1943 29 52 31 19 30 79 17 --- 16 | 80 100 62 73 67 63 74 --- 67
XR26 | ---- 36 53 --- --- --- --- 17 --- 25 | 21 71 --- --- --- --- 30 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS | 1549 31 34 20 15 24 30 18 130 |T 49 54 43 42 39 45 35 72 38
WRMS | 1549 32 34 20 14 22 28 18 130 |NE 51 56 43 41 37 44 33 64 37
MEDI | 1114 25 26 17 14 20 22 18 138 |MD 52 56 40 40 36 46 33 84 39
Table 3.1959.4 GPS week: 1959 Day: 4 MJD: 57961
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 | 1183 52 52 24 27 18 27 15 --- 12 | 71 68 45 40 50 55 33 --- 41
R02 | 632 20 27 12 12 14 20 15 132 6 | 54 59 48 47 47 50 34 84 44
R03 | 1687 19 20 16 10 9 21 25 111 8 | 58 59 45 49 46 44 47 36 46
R04 | 1026 21 28 22 12 13 26 16 --- 8 | 46 49 45 40 32 32 35 --- 36
R05 | 521 44 37 21 26 26 58 18 --- 14 | 35 46 35 49 49 56 34 --- 39
R06 | 1106 13 15 14 10 11 47 16 --- 9 | 23 24 27 25 26 32 23 --- 19
R07 | 700 27 29 23 16 30 24 17 116 10 | 62 61 52 48 54 60 37 55 47
R08 | 1106 18 16 12 7 21 33 12 --- 7 | 47 50 46 45 40 66 46 --- 46
R09E | 4295 15 15 18 7 13 16 14 --- 6 | 30 31 36 35 32 29 30 --- 30
R10E | 1134 13 11 19 14 13 32 12 --- 8 | 42 43 38 44 40 36 46 --- 40
R11E | 901 12 13 14 18 16 27 11 146 7 | 30 27 28 33 26 32 22 53 24
R13E | 1804 20 21 18 15 16 23 9 --- 7 | 25 30 21 30 26 24 22 --- 21
R15E | 1487 21 22 21 16 21 38 28 --- 10 | 75 74 78 69 69 81 68 --- 70
R16E | 1299 30 32 16 29 29 24 27 --- 11 | 48 53 40 45 53 58 53 --- 44
R17 | 1156 36 34 11 10 18 9 17 --- 7 | 58 56 46 44 45 43 38 --- 43
R18 | 738 25 25 13 10 16 12 15 --- 6 | 55 54 52 46 48 50 44 --- 47
R19 | 890 70 70 22 23 37 22 22 --- 14 | 80 82 49 50 34 40 35 --- 44
R20 | 1060 48 37 38 19 37 40 17 --- 14 | 45 45 29 48 48 44 35 --- 32
R21 | 679 48 47 22 11 31 16 26 101 11 | 54 53 34 36 25 42 21 56 29
R22 | 564 47 47 14 12 32 13 22 --- 10 | 51 50 24 31 21 30 17 --- 23
R23 | 748 14 18 18 27 14 33 15 --- 9 | 36 38 35 44 37 27 37 --- 34
R24 | 1579 46 60 50 18 16 79 19 --- 17 | 84 95 49 58 46 44 47 --- 49
XR26 | ---- 25 47 --- --- --- --- 12 --- 17 | 30 50 --- --- --- --- 35 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1418 34 34 22 17 22 33 18 122 |T 49 52 41 43 40 44 36 56 38
WRMS | 1418 32 33 22 15 19 30 18 122 |NE 52 55 41 43 40 44 35 57 38
MEDI | 1060 25 28 18 14 16 24 16 116 |MD 48 50 40 44 40 43 35 55 40
Table 3.1959.5 GPS week: 1959 Day: 5 MJD: 57962
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 | 686 62 62 27 23 29 33 28 --- 14 | 58 59 42 34 29 55 31 --- 31
R02 | 670 26 31 11 17 15 23 13 114 7 | 53 55 42 32 43 54 31 54 38
R03 | 1715 11 19 6 16 13 11 19 104 6 | 53 59 46 56 47 44 38 35 46
R04 | 577 23 26 17 8 11 22 22 --- 7 | 45 49 35 39 35 25 30 --- 33
R05 | 669 28 26 16 21 20 27 20 --- 9 | 34 42 44 47 52 32 33 --- 37
R06 | 1533 17 19 21 18 18 60 17 --- 11 | 22 24 23 33 37 34 25 --- 23
R07 | 557 28 30 18 9 14 18 14 121 7 | 58 61 48 44 47 54 48 41 47
R08 | 1505 10 13 19 7 26 27 18 --- 8 | 43 45 45 37 40 53 33 --- 38
R09E | 4095 13 16 18 9 16 27 12 --- 7 | 46 48 44 45 50 51 46 --- 44
R10E | 1211 16 17 17 15 14 38 18 --- 9 | 76 77 67 65 65 78 72 --- 68
R11E | 694 8 12 14 10 16 12 11 138 5 | 44 49 47 45 42 40 42 38 43
R13E | 1316 19 25 19 15 18 24 9 --- 7 | 28 29 22 29 28 27 20 --- 22
R15E | 2410 25 25 15 12 19 28 14 --- 8 | 182 183 175 177 179 166 179 --- 177
R16E | 848 27 43 24 20 29 39 25 --- 12 | 55 63 48 56 56 40 53 --- 48
R17 | 1252 44 51 22 15 27 19 15 --- 10 | 51 54 28 36 35 39 34 --- 32
R18 | 1159 32 30 12 11 19 27 17 --- 8 | 49 45 31 35 34 46 29 --- 33
R19 | 656 67 65 27 19 20 23 23 --- 13 | 69 71 56 53 49 42 37 --- 47
R20 | 606 46 52 23 26 44 59 19 --- 15 | 44 50 46 45 39 52 29 --- 34
R21 | 689 46 50 24 7 32 22 23 92 11 | 54 55 46 35 28 35 30 56 35
R22 | 714 50 49 19 16 29 27 23 --- 11 | 49 49 31 39 37 42 22 --- 31
R23 | 762 9 17 20 24 25 19 19 --- 9 | 40 40 36 54 47 27 48 --- 41
R24 | 986 41 71 57 21 34 64 21 --- 18 | 62 86 57 43 74 47 47 --- 43
XR26 | ---- 18 52 --- --- --- --- 10 --- 13 | 59 82 --- --- --- --- 37 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1395 34 38 22 16 24 33 19 115 |T 55 59 48 49 49 49 43 44 45
WRMS | 1395 35 37 23 14 20 30 19 115 |NE 49 54 41 41 42 42 34 46 37
MEDI | 762 26 30 19 15 19 27 18 114 |MD 51 54 44 43 42 42 34 41 38
Table 3.1959.6 GPS week: 1959 Day: 6 MJD: 57963
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 | 903 42 55 26 21 51 43 27 --- 15 | 74 81 55 35 35 70 34 --- 41
R02 | 809 26 35 21 12 27 25 18 119 9 | 67 72 56 42 40 65 39 28 47
R03 | 1321 13 14 8 14 19 31 11 98 7 | 71 72 64 58 52 79 52 26 59
R04 | 813 16 20 16 12 15 15 19 --- 7 | 59 61 56 56 42 45 43 --- 49
R05 | 1183 35 35 37 31 24 67 17 --- 16 | 53 56 54 45 38 48 39 --- 38
R06 | 1718 27 27 22 17 10 31 21 --- 9 | 24 25 24 36 26 26 34 --- 25
R07 | 1479 21 19 20 15 23 20 13 149 8 | 65 64 59 44 38 61 38 64 47
R08 | 816 20 25 18 16 9 19 16 --- 7 | 60 64 50 47 47 66 44 --- 49
R09E | 3598 14 18 19 33 17 25 29 --- 11 | 53 55 46 61 58 58 56 --- 53
R10E | 1017 19 22 16 10 21 16 16 --- 7 | 54 57 52 55 54 50 57 --- 52
R11E | 848 12 12 15 14 17 25 9 90 7 | 52 51 49 52 47 50 50 58 48
R13E | 2047 19 28 14 12 12 30 8 --- 7 | 32 39 23 34 29 28 25 --- 25
R15E | 4544 18 15 14 16 22 32 15 --- 8 | 141 143 142 144 153 144 142 --- 143
R16E | 1495 14 26 28 21 35 37 26 --- 12 | 61 67 75 65 73 69 67 --- 64
R17 | 888 43 46 21 12 34 25 18 --- 11 | 72 76 44 47 42 47 38 --- 44
R18 | 783 38 44 15 10 31 18 14 --- 9 | 71 74 48 49 38 58 40 --- 47
R19 | 630 68 67 24 24 36 37 31 --- 16 | 108 110 65 71 59 68 48 --- 63
R20 | 861 52 62 39 14 46 48 24 --- 16 | 76 87 56 53 40 53 38 --- 46
R21 | 816 44 46 22 10 42 12 23 72 11 | 79 80 56 50 28 52 42 77 48
R22 | 938 50 58 20 12 33 21 22 --- 11 | 79 81 48 44 26 50 29 --- 42
R23 | 985 15 17 26 28 10 37 15 --- 10 | 33 35 44 51 37 37 37 --- 38
XR24 | 861 23 25 49 15 --- 70 20 --- 19 | 87 89 67 78 --- 68 70 --- 70
XR26 | ---- 23 130 --- --- --- --- 13 --- 18 | 43 105 --- --- --- --- 37 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1660 33 37 22 18 28 32 20 109 |T 65 71 56 55 47 58 47 50 51
WRMS | 1660 33 36 21 16 25 27 20 109 |NE 65 72 52 50 39 55 41 48 46
MEDI | 903 23 27 20 14 23 25 18 98 |MD 65 72 54 50 40 53 40 58 47
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