[IGSREPORT-24380] Wk 1890 IGLOS Final Orbits
IGS ACC
acc at igs.org
Sat Apr 16 00:12:48 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1890 (Mar 27, 2016 - Apr 02, 2016)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1890.
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:
igl1890[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1890 in the SP3 format.
igl18907.sum Combination Report for GPS Week 1890.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -8.3 ns
1 | -5.5 ns
2 | -3.7 ns
3 | -9.2 ns
4 | -8.1 ns
5 | -8.5 ns
6 | -7.0 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 1.1890, 1a.1890).
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 2.1890.0-6)
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 3.1890.0-6).
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 1890 summary. (Mar 27, 2016 - Apr 02, 2016)
Table 1.1890.a GPS week : 1890 MJD: 57474.0-57480.0
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 6 0 -20 6 .25 28 27 | --- --- --- ---
| 2 2 2 45 26 31 .04 | --- ---
cof n/a| -1 0 6 10 -13 -4 .27 32 30 | --- --- --- ---
| 1 2 3 32 39 39 .06 | --- ---
emx n/a| 0 -1 3 -36 -55 -60 .19 26 25 | -10869 68 3611 7592
| 1 1 2 22 24 39 .05 | 6768 495
esx n/a| 0 0 0 11 27 27 -.11 20 18 | -11561 -717 3617 8875
| 1 1 1 19 21 25 .03 | 5492 938
gfz n/a| 0 0 3 47 89 38 .02 22 20 | 0 -783 3556 7246
| 1 1 1 20 23 37 .05 | 0 1095
grg n/a| -2 0 5 -4 13 -1 -.31 39 36 | -427461 -735 4136 616754
| 1 1 2 32 28 39 .09 | 2703 1114
iac n/a| 1 0 -8 -11 -27 -26 -.05 18 18 | -6176 -804 3620 7385
| 1 0 1 30 26 34 .12 | 1981 613
mcc n/a| 0 6 -35 141 5 245 -.38 163 163 | --- --- --- ---
| 13 20 22 123 171 1011 .57 | --- ---
Table 1.1890.b GPS week : 1890 MJD: 57474.0-57480.0
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 | 16 13 14 13 16 11 13 |
R02 | 9 9 7 6 8 8 7 |
R03 | 8 12 9 8 9 9 9 |
R04 | 8 10 9 8 8 9 9 |
R05 | 11 13 15 13 14 14 14 |
R06 | 9 11 10 10 7 7 7 |
R07 | 12 13 9 9 8 7 9 |
R08 | 12 8 12 10 8 9 10 |
R09 | 9 8 7 7 7 8 10 |
R10 | 9 9 9 10 8 7 10 |
R13 | 10 9 11 10 11 10 10 |
R14 | 14 13 11 12 16 17 15 |
R15 | 18 12 15 12 14 12 12 |
R16 | 14 15 13 14 18 18 17 |
R17 | 9 11 11 13 9 9 9 |
R18 | 8 8 9 9 7 7 10 |
R19 | 9 8 9 9 11 10 9 |
R20 | 16 15 14 14 11 13 14 |
R21 | 9 7 8 8 9 10 9 |
R22 | 9 7 9 10 9 11 8 |
R23 | 8 8 8 8 10 9 8 |
R24 | 18 14 15 19 16 12 18 |
R26 | 38 30 51 38 26 31 56 |
Table 1.1890.c GPS week : 1890 MJD: 57474.0-57480.0
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 1890 0 | -14 66 150 -463 -1650 6012 86.9 1476 1476 | -8310 0
brd 1890 1 | 53 25 107 424 -628 5271 84.5 1623 1623 | -5494 0
brd 1890 2 | -53 -63 183 36 555 3313 84.3 1805 1805 | -3706 0
brd 1890 3 | 91 -8 117 258 9 4365 87.1 1929 1929 | -9199 0
brd 1890 4 | 11 -16 181 -189 1135 3830 87.1 1931 1931 | -8066 0
brd 1890 5 | -27 97 242 -124 0 842 84.9 1936 1936 | -8539 0
brd 1890 6 | -16 22 102 -965 1877 1138 84.8 1354 1354 | -6996 0
-------------+------------------------------------------------------------+----------------
brd 1890 mean| 6 17 154 -146 185 3538 85.7 1721 1721 | -7187 0
brd 1890 sdev| 50 53 50 464 1154 1956 1.3 239 239 | 1954 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 2.1890.0 GPS week: 1890 Day: 0 MJD: 57474
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 37 -57 25 .23 30 28 | --- --- --- ---
cof n/a| -4 -2 0 27 -27 34 .24 35 31 | --- --- --- ---
emx n/a| 1 0 6 -56 -34 -64 .29 27 30 | -5527 300 3119 6577
esx n/a| -1 -1 2 43 45 47 -.14 20 19 | -4675 -1664 3095 7856
gfz n/a| 1 1 1 81 111 31 .08 28 20 | 0 121 3103 6329
grg n/a| -2 0 9 45 50 -43 -.43 39 34 | -429564 -52 3141 616579
iac n/a| 0 0 -9 -52 -39 -28 -.16 18 18 | -7655 -658 3134 6439
mcc n/a| 28 -2 -49 154 116 -423 -.30 145 145 | --- --- --- ---
Table 2.1890.1 GPS week: 1890 Day: 1 MJD: 57475
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 4 27 -30 57 .21 26 22 | --- --- --- ---
cof n/a| -2 0 3 35 -45 15 .25 29 26 | --- --- --- ---
emx n/a| 0 0 6 -22 -53 -111 .18 22 22 | -8757 860 3270 7783
esx n/a| 0 -2 0 21 50 -9 -.11 23 20 | -12140 918 3221 9082
gfz n/a| 4 -1 3 48 78 51 .06 21 18 | 0 467 3219 7161
grg n/a| -1 1 2 0 35 -3 -.36 36 34 | -425171 675 3276 616622
iac n/a| -1 0 -9 -32 -28 -14 -.17 20 20 | -3910 -1222 3279 7507
mcc n/a| -6 9 -53 79 17 -1730 -1.40 217 217 | --- --- --- ---
Table 2.1890.2 GPS week: 1890 Day: 2 MJD: 57476
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 10 46 -1 -15 .24 27 27 | --- --- --- ---
cof n/a| 0 0 10 61 47 -15 .23 28 27 | --- --- --- ---
emx n/a| 0 -1 3 -58 -62 18 .22 25 25 | -3675 -385 4064 7908
esx n/a| -1 1 0 6 27 68 -.13 19 16 | -12095 -993 4106 9353
gfz n/a| 0 0 2 60 84 94 .03 25 36 | 0 -1253 4042 7518
grg n/a| -4 -1 5 14 29 -33 -.23 37 34 | -422631 -1611 4066 616572
iac n/a| 3 0 -9 -29 -30 -99 -.16 18 18 | -3004 -1255 4070 7651
mcc n/a| 0 35 -37 7 -208 515 -.93 156 156 | --- --- --- ---
Table 2.1890.3 GPS week: 1890 Day: 3 MJD: 57477
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 7 26 -18 -42 .32 30 28 | --- --- --- ---
cof n/a| -1 0 9 9 -40 -60 .37 36 35 | --- --- --- ---
emx n/a| 2 -4 1 -58 -21 -62 .16 30 27 | -22947 451 3168 7638
esx n/a| 0 -1 -1 -7 45 28 -.06 20 18 | -20771 -1516 3204 8705
gfz n/a| -1 0 3 49 132 8 .05 20 19 | 0 -1275 3168 7515
grg n/a| -1 0 4 10 -23 -37 -.20 38 41 | -427111 -798 3181 618052
iac n/a| 2 2 -8 -1 -74 -6 -.06 15 15 | -7258 -776 3181 7395
mcc n/a| -11 30 -50 198 -184 703 -.03 125 125 | --- --- --- ---
Table 2.1890.4 GPS week: 1890 Day: 4 MJD: 57478
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 7 -69 -24 -1 .26 30 30 | --- --- --- ---
cof n/a| 0 2 9 -18 0 -45 .31 34 30 | --- --- --- ---
emx n/a| -1 -2 2 -1 -67 -79 .15 25 24 | -13197 -332 4149 7316
esx n/a| -2 1 0 -10 12 10 -.07 21 18 | -6997 -1062 4168 8126
gfz n/a| 0 -1 3 40 79 10 .02 20 14 | 0 89 3912 7186
grg n/a| -1 -1 4 -38 -5 59 -.37 43 42 | -428435 -1548 5937 616970
iac n/a| 2 1 -7 -10 -16 -5 -.05 17 17 | -7948 433 4146 7177
mcc n/a| -4 -24 -48 186 215 450 -.19 144 144 | --- --- --- ---
Table 2.1890.5 GPS week: 1890 Day: 5 MJD: 57479
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 2 7 -27 24 5 .29 29 28 | --- --- --- ---
cof n/a| -2 3 6 -25 26 -6 .28 36 33 | --- --- --- ---
emx n/a| 0 -1 4 -29 -52 -66 .15 24 23 | -15394 -461 4068 8760
esx n/a| -2 0 -2 3 -8 28 -.10 19 17 | -15777 -908 4114 10066
gfz n/a| 0 2 3 16 70 77 -.03 21 17 | 0 -2671 4004 8239
grg n/a| -3 2 4 -47 -17 32 -.37 40 34 | -429927 -2232 5924 615603
iac n/a| 1 0 -6 38 -16 -30 .09 17 17 | -7519 -780 4073 8494
mcc n/a| -1 -1 3 356 -91 1092 -.06 265 265 | --- --- --- ---
Table 2.1890.6 GPS week: 1890 Day: 6 MJD: 57480
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| -5 2 6 -41 -38 19 .21 26 24 | --- --- --- ---
cof n/a| -1 3 7 -17 -54 43 .20 29 27 | --- --- --- ---
emx n/a| -3 1 0 -28 -97 -58 .16 27 27 | -6589 44 3442 7163
esx n/a| 1 0 -1 24 16 18 -.15 20 18 | -8472 200 3412 8938
gfz n/a| 2 0 6 35 69 -3 -.05 22 18 | 0 -960 3450 6774
grg n/a| -3 0 4 -14 27 15 -.22 39 35 | -429388 415 3428 616880
iac n/a| 2 0 -7 8 13 2 .12 19 19 | -5940 -1376 3460 7035
mcc n/a| 1 0 -9 7 176 1113 .22 92 92 | --- --- --- ---
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 3.1890.0 GPS week: 1890 Day: 0 MJD: 57474
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 | 2540 56 52 28 23 42 35 33 --- 16 | 116 120 125 144 152 142 118 --- 129
R02E | 1788 22 30 20 14 21 29 14 --- 8 | 47 49 42 47 50 53 38 --- 41
R03E | 1254 26 30 17 14 25 24 9 194 8 | 206 206 217 208 215 200 204 308 208
R04E | 1170 25 31 17 11 19 25 10 --- 7 | 138 138 143 134 139 128 138 --- 137
R05E | 1229 33 38 28 18 28 33 19 --- 11 | 45 48 38 37 54 49 45 --- 37
R06E | 980 24 29 21 15 19 20 21 --- 9 | 41 44 43 38 45 41 37 --- 37
R07E | 1273 30 35 30 24 18 35 24 77 11 | 93 96 90 111 100 121 76 43 94
R08E | 1163 30 34 28 15 25 29 28 --- 11 | 36 34 34 32 34 47 52 --- 33
R09 | 2345 24 28 21 17 21 31 14 --- 9 | 20 28 20 32 37 23 20 --- 21
R10 | 1173 20 25 21 21 15 26 14 --- 8 | 45 47 25 44 30 23 33 --- 32
R13 | 632 41 44 17 16 23 33 10 --- 10 | 43 49 22 29 32 28 18 --- 20
R14 | 1399 39 46 39 26 20 31 27 --- 13 | 34 45 29 52 42 21 38 --- 33
R15 | 2560 38 41 31 19 79 21 22 --- 17 | 51 53 30 30 54 18 19 --- 23
XR16 | 1760 22 40 42 --- 18 39 20 --- 14 | 40 59 39 --- 36 36 45 --- 34
XR17 | 1676 20 23 13 --- 22 24 10 --- 8 | 64 68 59 --- 52 43 45 --- 50
R18 | 1095 13 16 13 16 14 38 9 --- 7 | 56 58 55 60 50 29 39 --- 47
R19 | 722 28 25 19 17 16 39 15 --- 9 | 64 63 58 59 49 39 33 --- 47
R20 | 897 18 52 40 28 19 87 15 --- 15 | 56 75 56 58 54 30 31 --- 44
R21 | 1004 21 20 16 17 20 21 19 140 8 | 77 77 72 70 67 58 51 61 63
R22 | 1207 21 23 11 20 11 41 13 --- 8 | 73 73 66 67 57 40 46 --- 57
R23 | 1631 8 13 17 25 11 24 13 --- 7 | 24 27 24 47 33 14 18 --- 25
R24 | 1428 36 45 58 34 23 76 10 --- 17 | 64 64 58 53 40 22 36 --- 43
XR26 | ---- 56 1107 --- --- --- --- 25 --- 37 | 49 9999 --- --- --- --- 35 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1475 30 35 27 20 28 39 18 145 |T 64 69 61 67 64 54 52 137 55
WRMS | 1475 28 31 30 19 20 34 18 145 |NE 50 56 43 50 45 30 33 61 37
MEDI | 1229 25 31 21 17 20 31 15 140 |MD 51 58 43 52 50 39 38 61 41
Table 3.1890.1 GPS week: 1890 Day: 1 MJD: 57475
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 | 2354 40 38 31 23 26 49 13 --- 13 | 140 141 150 165 154 161 156 --- 152
R02E | 3318 24 20 21 17 23 25 11 --- 9 | 41 39 37 31 40 43 36 --- 34
R03E | 952 35 29 19 16 24 33 34 313 12 | 160 169 179 175 174 185 157 457 168
R04E | 1572 22 33 18 16 24 22 24 --- 9 | 102 104 111 109 118 109 106 --- 107
R05E | 750 28 31 21 28 27 42 32 --- 13 | 68 66 65 79 68 73 49 --- 61
R06E | 1928 29 24 27 32 14 28 17 --- 11 | 45 44 58 46 46 56 38 --- 41
R07E | 1695 36 39 18 20 26 29 40 181 13 | 103 107 107 110 108 113 76 58 97
R08E | 1190 30 30 15 17 18 24 9 --- 8 | 33 34 18 23 31 28 20 --- 19
R09 | 2558 20 16 17 17 17 26 8 --- 7 | 16 19 11 27 28 23 16 --- 16
R10 | 1540 16 21 10 24 16 30 23 --- 9 | 30 31 26 37 23 23 26 --- 23
R13 | 1422 38 42 14 14 22 21 9 --- 9 | 30 34 19 18 27 23 14 --- 15
R14 | 757 20 25 29 37 17 57 17 --- 13 | 29 31 31 49 36 34 31 --- 27
R15 | 1789 34 33 24 14 34 31 17 --- 11 | 38 38 28 26 46 22 16 --- 21
XR16 | 936 18 20 46 --- 19 42 18 --- 15 | 32 30 42 --- 31 29 27 --- 27
XR17 | 788 27 27 21 --- 21 25 17 --- 11 | 47 48 45 --- 33 23 19 --- 30
R18 | 620 15 13 16 11 9 36 14 --- 7 | 41 43 43 38 38 20 24 --- 33
R19 | 682 23 32 16 17 14 24 13 --- 7 | 37 46 37 38 34 32 26 --- 31
R20 | 1395 24 44 39 28 25 65 21 --- 14 | 32 55 57 38 39 23 19 --- 29
R21 | 1113 15 10 12 16 16 15 13 106 6 | 58 57 53 59 54 66 52 102 54
R22 | 829 20 25 13 11 16 26 12 --- 7 | 44 47 38 41 40 32 33 --- 37
R23 | 1945 8 12 17 25 11 37 10 --- 8 | 17 20 18 30 23 22 17 --- 16
R24 | 982 16 25 37 40 15 58 16 --- 13 | 48 58 61 71 45 26 34 --- 44
XR26 | ---- 37 1191 --- --- --- --- 25 --- 30 | 60 885 --- --- --- --- 16 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1623 26 29 22 23 21 36 20 217 |T 54 93 56 60 56 53 43 205 48
WRMS | 1623 22 26 22 20 18 34 20 217 |NE 37 96 36 39 35 28 24 102 28
MEDI | 1190 24 27 18 17 18 29 17 181 |MD 41 46 42 38 39 29 27 102 31
Table 3.1890.2 GPS week: 1890 Day: 2 MJD: 57476
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 | 1439 40 34 34 20 28 45 25 --- 13 | 86 86 83 82 83 86 67 --- 75
R02E | 3545 14 20 16 14 13 23 14 --- 6 | 34 39 29 35 34 37 23 --- 28
R03E | 878 29 22 19 11 25 29 16 206 9 | 77 86 81 80 84 91 77 278 78
R04E | 816 23 21 25 16 22 19 18 --- 9 | 72 74 84 74 85 84 62 --- 73
R05E | 909 33 34 23 31 46 38 27 --- 14 | 65 70 62 49 79 68 63 --- 55
R06E | 1959 23 31 24 22 16 23 20 --- 9 | 38 41 33 49 43 36 39 --- 36
R07E | 2996 34 39 22 13 20 26 10 119 9 | 60 60 35 51 49 61 41 51 44
R08E | 1718 32 32 25 21 33 37 19 --- 12 | 40 42 22 43 48 40 25 --- 30
R09 | 2178 14 17 16 15 10 22 12 --- 6 | 15 21 14 26 27 22 13 --- 16
R10 | 1239 7 24 22 26 9 42 11 --- 9 | 33 41 33 53 39 23 33 --- 34
R13 | 788 46 38 19 15 20 41 12 --- 11 | 44 42 26 23 29 33 16 --- 18
R14 | 650 29 34 20 27 16 33 18 --- 10 | 24 31 40 47 37 35 34 --- 27
R15 | 4059 40 36 21 17 54 40 25 --- 15 | 45 44 42 33 44 31 17 --- 26
XR16 | 703 21 32 34 --- 16 45 19 --- 13 | 28 42 45 --- 40 25 35 --- 32
XR17 | 668 25 30 26 --- 20 32 14 --- 11 | 55 60 54 --- 38 20 30 --- 37
R18 | 630 19 23 22 17 17 25 24 --- 9 | 45 48 39 36 40 29 17 --- 29
R19 | 1872 19 16 25 11 19 30 11 --- 8 | 45 41 53 33 41 49 30 --- 36
R20 | 812 32 34 22 19 25 69 23 --- 13 | 74 79 61 59 58 32 27 --- 48
R21 | 816 18 20 16 13 12 36 14 126 7 | 51 54 42 47 39 42 39 98 40
R22 | 570 26 19 24 13 23 20 16 --- 9 | 55 52 55 51 47 49 29 --- 43
R23 | 1573 17 19 15 22 20 29 11 --- 8 | 20 20 21 33 37 20 15 --- 21
R24 | 804 14 24 55 19 18 64 23 --- 15 | 47 48 59 49 43 34 29 --- 40
XR26 | ---- 67 2118 --- --- --- --- 37 --- 50 | 86 9999 --- --- --- --- 46 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1805 27 28 25 19 25 37 18 155 |T 49 50 46 47 48 43 35 142 39
WRMS | 1805 27 26 25 16 36 34 18 155 |NE 44 44 41 40 39 31 27 98 32
MEDI | 878 25 30 22 17 20 32 18 126 |MD 45 44 42 47 41 35 30 98 36
Table 3.1890.3 GPS week: 1890 Day: 3 MJD: 57477
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 | 1234 44 42 26 21 27 40 20 --- 12 | 104 114 102 112 114 123 106 --- 108
R02E | 2751 20 27 19 11 15 17 7 --- 6 | 34 40 30 34 37 35 28 --- 29
R03E | 1655 19 29 24 14 16 32 11 117 8 | 86 83 101 87 89 93 95 187 91
R04E | 2035 24 26 20 16 20 21 10 --- 8 | 101 98 103 103 104 98 110 --- 103
R05E | 859 30 37 29 19 33 50 23 --- 13 | 60 68 66 68 76 61 65 --- 60
R06E | 2024 24 38 40 12 22 17 17 --- 9 | 38 52 56 45 55 47 37 --- 42
R07E | 3407 29 35 25 13 18 24 13 141 8 | 55 57 68 65 61 56 52 51 57
R08E | 1655 46 51 21 17 17 25 11 --- 10 | 44 50 27 30 38 32 19 --- 23
R09 | 2047 19 25 18 13 16 31 10 --- 7 | 19 27 26 32 37 43 16 --- 24
R10 | 1226 22 24 25 22 27 31 9 --- 9 | 34 39 25 44 33 42 34 --- 31
R13 | 677 39 56 21 20 16 38 13 --- 10 | 40 54 33 29 29 24 16 --- 19
R14 | 810 25 34 41 27 10 53 19 --- 12 | 28 40 37 41 29 24 25 --- 25
R15 | 4716 40 50 21 23 28 43 14 --- 11 | 52 61 41 31 38 24 26 --- 25
XR16 | 796 24 29 33 --- 16 52 21 --- 13 | 41 50 72 --- 32 36 46 --- 41
XR17 | 734 22 26 21 --- 21 58 13 --- 12 | 62 64 58 --- 67 30 38 --- 47
R18 | 724 20 22 14 19 16 43 18 --- 9 | 54 53 47 51 51 22 25 --- 38
R19 | 2556 26 27 30 18 12 21 13 --- 8 | 52 52 52 40 47 28 29 --- 37
R20 | 1063 37 64 32 35 24 54 15 --- 13 | 78 105 52 67 54 38 43 --- 51
R21 | 590 21 26 16 21 13 16 16 113 7 | 73 76 72 78 69 59 51 66 64
R22 | 563 32 33 33 17 23 29 10 --- 10 | 60 60 63 49 36 31 34 --- 40
R23 | 865 16 21 16 20 17 17 12 --- 7 | 16 20 28 35 29 20 23 --- 21
R24 | 779 33 18 76 18 23 84 26 --- 18 | 38 43 74 38 51 22 26 --- 31
XR26 | ---- 65 180 --- --- --- --- 21 --- 38 | 41 371 --- --- --- --- 63 --- 47
------+---------------------------------------------------+-----------------------------------------------
RMS | 1929 30 36 30 20 20 38 15 125 |T 52 72 56 53 53 44 43 101 45
WRMS | 1929 28 35 27 18 19 41 15 125 |NE 45 74 48 44 43 31 33 66 36
MEDI | 1063 25 29 24 18 17 31 13 117 |MD 52 54 52 44 47 35 34 66 40
Table 3.1890.4 GPS week: 1890 Day: 4 MJD: 57478
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 | 2183 44 46 26 37 28 57 31 --- 15 | 87 98 87 112 101 99 72 --- 87
R02E | 2530 26 29 15 13 21 24 10 --- 7 | 38 41 29 29 34 34 25 --- 26
R03E | 3384 24 25 21 17 18 27 13 94 8 | 56 57 60 55 53 64 55 104 54
R04E | 3088 22 26 17 11 18 37 13 --- 8 | 49 51 58 51 44 72 42 --- 47
R05E | 782 27 37 29 31 24 60 25 --- 13 | 47 51 58 42 58 63 51 --- 44
R06E | 1918 17 17 22 14 15 26 8 --- 7 | 39 37 34 38 46 54 48 --- 40
R07E | 2909 25 25 24 16 16 21 9 223 8 | 32 37 38 35 35 39 31 57 30
R08E | 1885 32 35 13 12 17 29 12 --- 8 | 38 41 21 27 32 32 19 --- 22
R09 | 1967 20 20 17 14 14 28 11 --- 7 | 14 18 19 23 23 25 13 --- 15
R10 | 832 13 16 22 23 6 31 12 --- 7 | 27 25 25 33 26 32 18 --- 21
R13 | 617 45 40 11 21 25 31 20 --- 11 | 41 36 22 29 24 26 15 --- 17
R14 | 1073 44 32 46 32 20 70 23 --- 16 | 40 54 45 49 37 26 26 --- 28
R15 | 3377 52 51 17 23 36 51 15 --- 13 | 55 55 28 23 35 19 23 --- 20
XR16 | 1516 42 49 47 --- 17 49 28 --- 17 | 37 41 52 --- 25 32 37 --- 30
XR17 | 739 20 22 18 --- 14 21 15 --- 8 | 51 52 51 --- 39 53 30 --- 39
R18 | 726 16 21 16 16 10 25 10 --- 6 | 43 49 38 36 39 26 29 --- 33
R19 | 1698 26 27 27 14 26 42 17 --- 10 | 50 52 49 43 34 17 26 --- 33
R20 | 1518 30 26 24 17 16 63 15 --- 11 | 63 62 57 42 40 31 35 --- 41
R21 | 486 19 16 18 12 14 45 16 64 8 | 50 47 50 47 45 36 29 28 39
R22 | 573 26 32 19 19 11 36 16 --- 8 | 57 64 48 53 42 25 30 --- 40
R23 | 970 26 25 22 29 14 29 18 --- 10 | 15 23 30 46 39 14 20 --- 26
R24 | 1164 22 74 57 21 24 75 19 --- 15 | 34 65 77 43 40 26 24 --- 34
XR26 | ---- 40 81 --- --- --- --- 15 --- 25 | 50 260 --- --- --- --- 51 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1930 30 34 25 21 20 43 17 144 |T 44 57 44 42 40 38 32 63 35
WRMS | 1930 30 30 24 18 14 42 17 144 |NE 41 60 42 38 34 27 27 28 30
MEDI | 1516 26 27 21 17 17 31 15 94 |MD 43 51 45 42 39 32 29 57 33
Table 3.1890.5 GPS week: 1890 Day: 5 MJD: 57479
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 | 1698 37 47 29 17 27 32 16 --- 11 | 62 68 67 72 84 82 66 --- 69
R02E | 2172 25 35 23 14 20 23 7 --- 8 | 38 44 24 35 40 39 31 --- 31
R03E | 3957 30 39 20 11 26 21 9 96 8 | 78 82 80 79 87 86 80 151 80
R04E | 3412 34 42 21 12 16 38 11 --- 9 | 80 86 78 74 78 71 77 --- 75
R05E | 956 31 31 21 26 34 35 35 --- 13 | 63 66 57 73 86 72 54 --- 61
R06E | 1449 20 17 15 15 17 25 11 --- 7 | 36 38 38 36 39 46 30 --- 33
R07E | 1992 21 23 21 10 18 22 10 407 7 | 50 56 58 52 56 57 46 146 51
R08E | 2830 23 32 27 17 20 22 9 --- 8 | 28 35 26 27 35 31 18 --- 21
R09 | 2011 24 33 21 14 12 37 9 --- 8 | 12 22 20 26 22 28 16 --- 16
R10 | 743 17 12 17 15 18 19 9 --- 7 | 28 29 24 24 23 23 23 --- 19
R13 | 709 35 45 14 20 17 34 15 --- 9 | 37 44 25 29 22 21 15 --- 17
R14 | 736 49 61 36 40 26 74 21 --- 17 | 30 49 48 58 29 41 31 --- 29
R15 | 3226 39 56 21 17 28 55 18 --- 12 | 42 57 29 31 34 23 21 --- 20
XR16 | 1838 30 34 51 --- 18 55 24 --- 17 | 31 37 49 --- 40 37 28 --- 30
XR17 | 646 21 16 20 --- 20 19 13 --- 9 | 42 33 41 --- 37 38 25 --- 31
R18 | 919 17 17 18 10 15 12 15 --- 6 | 37 36 35 30 27 35 24 --- 27
R19 | 1875 32 30 27 11 13 28 26 --- 10 | 49 47 45 35 37 19 17 --- 30
R20 | 1277 25 14 28 23 25 70 19 --- 13 | 41 33 33 51 43 26 24 --- 34
R21 | 553 26 31 26 19 17 40 14 189 9 | 63 67 60 60 63 63 52 63 56
R22 | 574 27 29 24 14 15 47 25 --- 10 | 41 43 39 35 37 16 15 --- 26
R23 | 578 20 19 19 23 11 29 19 --- 9 | 16 19 34 32 26 21 10 --- 19
R24 | 1414 18 55 35 18 22 65 16 --- 12 | 26 78 51 38 44 26 36 --- 32
XR26 | ---- 47 123 --- --- --- --- 20 --- 31 | 37 98 --- --- --- --- 37 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1935 29 36 24 19 21 40 17 265 |T 42 50 43 44 44 40 33 120 36
WRMS | 1935 28 33 23 17 17 34 17 265 |NE 35 46 38 37 34 29 24 63 27
MEDI | 1414 26 32 21 15 18 32 15 189 |MD 38 44 39 35 37 35 28 146 30
Table 3.1890.6 GPS week: 1890 Day: 6 MJD: 57480
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 | 1616 31 45 42 28 27 28 19 --- 13 | 78 85 84 97 99 98 82 --- 86
R02E | 1285 20 26 17 13 16 21 6 --- 7 | 45 50 43 42 45 46 40 --- 40
R03E | 1968 24 32 20 16 20 24 12 82 8 | 77 80 77 83 84 77 77 83 78
R04E | 1229 28 35 22 9 21 23 21 --- 9 | 58 55 50 54 52 52 62 --- 52
R05E | 1217 27 32 45 18 38 42 18 --- 14 | 52 59 44 46 72 46 48 --- 45
R06E | 634 16 20 20 14 15 21 11 --- 7 | 31 31 31 41 39 39 42 --- 35
R07E | 1364 21 15 20 14 21 27 13 125 8 | 53 51 59 50 56 57 51 168 51
R08E | 1981 21 22 25 23 15 37 17 --- 10 | 28 28 25 31 33 32 26 --- 23
R09 | 1981 27 14 24 19 10 42 17 --- 10 | 22 18 21 32 30 30 18 --- 21
R10 | 1659 16 23 18 18 23 46 18 --- 10 | 37 37 38 43 23 36 34 --- 31
R13 | 523 29 35 28 13 24 29 10 --- 9 | 40 41 27 25 25 21 21 --- 20
R14 | 843 34 39 33 30 27 32 35 --- 14 | 40 52 43 67 51 26 36 --- 39
R15 | 2525 36 34 21 19 26 37 20 --- 11 | 53 52 30 35 31 24 23 --- 26
XR16 | 1059 20 28 28 --- 25 80 19 --- 16 | 31 35 32 --- 27 31 41 --- 27
XR17 | 686 17 23 18 --- 16 24 14 --- 8 | 64 68 63 --- 51 40 42 --- 50
R18 | 644 18 22 24 15 17 38 21 --- 9 | 55 58 53 45 48 33 29 --- 40
R19 | 1332 28 38 14 14 11 21 27 --- 9 | 68 75 55 49 51 38 28 --- 45
R20 | 1037 25 30 30 21 25 76 22 --- 14 | 54 57 68 64 67 39 40 --- 52
R21 | 570 18 22 18 11 19 43 11 56 8 | 75 77 69 68 62 48 55 89 62
R22 | 772 25 21 19 18 10 19 12 --- 7 | 69 67 66 51 49 37 38 --- 49
R23 | 547 11 14 15 23 15 30 15 --- 8 | 22 20 30 42 31 21 19 --- 25
R24 | 894 37 30 49 38 33 77 26 --- 18 | 78 68 70 69 45 42 42 --- 54
XR26 | ---- 73 226 --- --- --- --- 43 --- 56 | 64 212 --- --- --- --- 45 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1353 26 29 27 20 22 39 19 92 |T 51 59 49 51 48 41 40 113 42
WRMS | 1353 24 27 27 18 18 35 19 92 |NE 51 62 47 49 42 33 34 89 37
MEDI | 1059 25 28 21 18 20 30 18 82 |MD 53 55 44 46 48 38 40 89 40
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