[IGSREPORT-24140] Wk 1875 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Mon Jan 4 07:23:14 PST 2016
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1875 (Dec 13, 2015 - Dec 19, 2015)
Contact: igs.acc at noaa.gov
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 2.1875.
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:
igl1875[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1875 in the SP3 format.
igl18757.sum Combination Report for GPS Week 1875.
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 | 20.5 ns
1 | 19.4 ns
2 | 21.9 ns
3 | 25.2 ns
4 | 26.2 ns
5 | 25.4 ns
6 | 24.6 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
----+--------+---------------
2 | GRG | R16
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 1.1875, 1a.1875).
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 2.1875.0-6)
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 3.1875.0-6).
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 1875 summary. (Dec 13, 2015 - Dec 19, 2015)
Table 1.1875.a GPS week : 1875 MJD: 57369.0-57375.0
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 2 -15 -21 -87 .28 45 38 | --- --- --- ---
| 2 1 2 17 36 40 .07 | --- ---
cof n/a| -1 -1 2 4 -4 -87 .32 47 40 | --- --- --- ---
| 2 1 4 36 27 33 .05 | --- ---
emx n/a| 0 0 -3 -56 -98 -59 .24 28 29 | 24654 -368 4050 7556
| 1 1 3 32 20 27 .03 | 5141 916
esx n/a| 1 0 2 15 2 9 -.11 21 20 | 20315 -295 4105 8804
| 1 1 2 33 17 9 .05 | 8341 1787
gfz n/a| 0 0 -1 43 75 5 .09 23 19 | 0 -901 4018 7927
| 1 0 1 21 16 28 .05 | 0 1897
grg n/a| -3 1 8 -12 13 -36 -.36 42 35 | -584884 -579 4696 688634
| 1 1 3 22 21 26 .05 | 3359 3090
iac n/a| 0 0 -2 0 0 36 -.09 17 17 | 25420 -972 4107 8087
| 1 1 1 45 32 30 .04 | 2959 1148
Table 1.1875.b GPS week : 1875 MJD: 57369.0-57375.0
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 | 10 9 11 11 9 9 8 |
R02 | 8 8 8 7 8 7 8 |
R03 | 9 10 8 6 6 6 7 |
R04 | 6 10 9 7 7 7 8 |
R05 | 13 10 11 12 12 13 11 |
R06 | 8 5 8 9 9 9 8 |
R07 | 9 11 9 9 9 8 9 |
R08 | 10 8 8 10 10 9 8 |
R09 | 14 12 13 15 14 12 14 |
R10 | 9 8 8 7 8 7 9 |
R11 | 25 20 20 21 22 21 27 |
R12 | 25 25 19 21 19 20 21 |
R13 | 11 12 12 11 11 11 10 |
R14 | 19 12 12 14 13 15 15 |
R15 | 12 11 9 11 11 12 13 |
R16 | 11 9 10 9 8 9 10 |
R18 | 8 8 9 8 9 8 9 |
R19 | 10 17 21 11 9 8 11 |
R20 | 14 17 11 13 13 14 16 |
R21 | 11 9 10 10 10 11 9 |
R22 | 9 12 9 11 11 9 9 |
R23 | 10 10 9 9 10 10 8 |
R24 | 13 9 14 14 12 14 17 |
R26 | 20 30 30 28 43 46 31 |
R27 | 0 0 0 0 0 0 0 |
Table 1.1875.c GPS week : 1875 MJD: 57369.0-57375.0
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 1875 0 | 32 42 0 -485 -193 -132 85.3 1785 1785 | 20477 0
brd 1875 1 | 24 18 6 -649 -291 107 84.1 2388 2388 | 19398 0
brd 1875 2 | 45 3 -38 -226 711 1425 83.5 1927 1927 | 21921 0
brd 1875 3 | 0 32 -2 -327 615 2985 84.0 2036 2036 | 25164 0
brd 1875 4 | -27 -20 2 180 -539 2982 84.9 2064 2064 | 26246 0
brd 1875 5 | 33 -24 -67 -851 -673 1846 84.6 1725 1725 | 25398 0
brd 1875 6 | 0 30 -69 -768 -559 -540 83.5 1716 1716 | 24598 0
-------------+------------------------------------------------------------+----------------
brd 1875 mean| 15 11 -24 -446 -132 1239 84.3 1948 1948 | 23314 0
brd 1875 sdev| 25 26 33 357 568 1461 .7 239 239 | 2687 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 2.1875.0 GPS week: 1875 Day: 0 MJD: 57369
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 -22 -19 -111 .30 51 51 | --- --- --- ---
cof n/a| 0 -4 -2 19 -52 -91 .31 50 51 | --- --- --- ---
emx n/a| 0 -2 1 -74 -93 -68 .23 29 30 | 27906 -1058 4778 8778
esx n/a| 0 -3 0 12 2 15 -.09 19 18 | 22554 -1125 4770 9500
gfz n/a| 0 -1 -1 10 66 9 .08 27 21 | 0 -1236 4759 8614
grg n/a| -3 3 8 -25 47 -50 -.30 41 38 | -587881 -1364 4756 687603
iac n/a| 0 2 -2 18 19 56 -.05 20 20 | 22990 -2158 4772 8702
Table 2.1875.1 GPS week: 1875 Day: 1 MJD: 57370
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 3 -9 -44 -124 .30 48 37 | --- --- --- ---
cof n/a| 2 1 3 29 11 -96 .28 51 39 | --- --- --- ---
emx n/a| 0 0 -7 -24 -76 -28 .22 27 29 | 17030 -80 3736 6878
esx n/a| 3 -1 3 31 35 9 -.15 23 21 | 12246 -985 3724 7426
gfz n/a| 1 0 -1 43 74 14 .10 25 19 | 0 -1155 3644 6642
grg n/a| -4 0 9 -11 -6 -25 -.38 41 37 | -588640 -853 3753 688074
iac n/a| -1 0 -1 -19 -29 13 -.09 16 16 | 21265 -1158 3722 6781
Table 2.1875.2 GPS week: 1875 Day: 2 MJD: 57371
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| -4 -1 0 -8 -75 -67 .26 44 36 | --- --- --- ---
cof n/a| -2 -1 2 -4 -28 -103 .29 46 37 | --- --- --- ---
emx n/a| -2 -1 -4 -9 -129 -20 .26 27 27 | 26915 -923 3465 6902
esx n/a| 3 1 2 71 0 16 -.19 23 21 | 7100 -120 3484 8150
gfz n/a| 2 0 0 35 58 -13 .05 21 16 | 0 -1929 3452 6837
grg n/a| -2 2 2 -30 15 -6 -.32 69 34 | -586465 -2492 3467 689099
iac n/a| 0 0 -1 -60 34 15 -.06 15 15 | 23362 -1082 3484 6797
Table 2.1875.3 GPS week: 1875 Day: 3 MJD: 57372
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 1 -15 -45 -37 .40 41 33 | --- --- --- ---
cof n/a| -4 -3 -4 5 3 -34 .33 43 34 | --- --- --- ---
emx n/a| -1 0 -1 -41 -104 -88 .30 29 30 | 18162 931 4548 7022
esx n/a| 0 0 4 -5 6 12 -.08 21 20 | 18237 2539 4554 7491
gfz n/a| 0 1 -3 31 60 44 .01 23 15 | 0 1612 4344 6760
grg n/a| -2 0 5 -33 -12 -77 -.33 36 36 | -586774 5100 8707 687083
iac n/a| 2 1 -2 28 22 17 -.05 17 17 | 26228 498 4549 6873
Table 2.1875.4 GPS week: 1875 Day: 4 MJD: 57373
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 1 1 -47 33 -132 .29 43 32 | --- --- --- ---
cof n/a| -3 -1 4 -50 13 -132 .41 46 34 | --- --- --- ---
emx n/a| 0 0 0 -101 -88 -89 .22 30 29 | 25990 772 3667 7772
esx n/a| 0 0 2 -36 3 -11 -.07 20 21 | 30147 1513 4025 11750
gfz n/a| -1 -1 -1 43 73 0 .16 20 17 | 0 1340 4055 11703
grg n/a| -2 2 11 -26 26 -44 -.43 34 30 | -580705 1594 4018 689911
iac n/a| 2 0 -5 77 -32 91 -.14 16 16 | 29301 555 4026 11978
Table 2.1875.5 GPS week: 1875 Day: 5 MJD: 57374
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 3 -15 9 -106 .21 44 42 | --- --- --- ---
cof n/a| 0 -1 5 -25 29 -51 .26 48 47 | --- --- --- ---
emx n/a| 0 -2 -9 -66 -78 -53 .21 27 28 | 30975 -912 4316 8735
esx n/a| 0 0 5 20 -19 17 -.16 22 21 | 23967 -1162 4347 9667
gfz n/a| -1 0 0 64 101 26 .14 19 20 | 0 -1042 4135 8403
grg n/a| -4 2 9 12 23 -3 -.40 37 35 | -580672 -1592 4356 689615
iac n/a| 2 0 -4 -29 -38 12 -.11 17 17 | 28290 -1091 4355 8883
Table 2.1875.6 GPS week: 1875 Day: 6 MJD: 57375
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 8 11 -5 -34 .21 46 35 | --- --- --- ---
cof n/a| 0 0 5 58 -8 -105 .34 48 36 | --- --- --- ---
emx n/a| 0 0 -3 -79 -122 -66 .25 32 32 | 25602 -1310 3842 6811
esx n/a| 0 0 0 14 -13 8 -.05 19 16 | 27955 -2728 3833 7650
gfz n/a| -2 0 -5 75 95 -43 .07 24 21 | 0 -3902 3740 6530
grg n/a| -2 3 10 25 -2 -46 -.33 35 33 | -583053 -4447 3817 689055
iac n/a| 1 1 -2 -20 28 47 -.12 19 19 | 26508 -2372 3842 6596
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 3.1875.0 GPS week: 1875 Day: 0 MJD: 57369
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1354 36 43 29 13 18 27 23 10 | 56 56 59 40 34 43 25 37
R02 | 731 21 19 14 12 20 24 18 7 | 47 43 46 44 40 48 29 38
R03 | 728 13 18 11 19 19 42 11 8 | 56 58 51 54 49 44 45 47
R04 | 1523 19 32 18 9 10 20 12 6 | 60 71 50 48 44 33 40 44
R05 | 579 39 45 33 28 22 47 13 12 | 52 54 57 38 35 26 32 33
R06 | 1100 28 34 17 17 12 28 14 8 | 29 28 37 47 39 35 49 39
R07 | 704 34 31 26 9 10 26 18 8 | 67 68 72 52 51 41 35 48
R08 | 2160 24 23 12 13 23 29 26 9 | 66 64 54 51 56 45 37 47
R09 | 778 45 35 41 18 21 59 14 13 | 62 60 38 50 45 41 44 41
R10 | 1632 15 14 26 20 10 30 10 8 | 45 45 40 48 39 37 39 39
R11 | 1552 137 134 51 24 55 72 30 25 | 116 118 58 53 74 45 36 42
R12 | 1068 131 129 45 28 53 76 36 25 | 117 119 50 48 52 57 38 37
R13 | 724 54 43 17 19 20 34 14 10 | 74 73 42 51 42 32 38 40
R14 | 1325 54 48 58 31 25 75 23 18 | 57 63 58 70 54 40 50 51
R15 | 5339 33 34 21 17 41 18 23 11 | 67 70 47 52 47 38 41 44
R16 | 691 34 39 21 23 25 32 16 10 | 56 61 37 50 40 60 38 38
R18E | 1172 27 29 21 14 15 23 15 8 | 40 44 37 34 33 27 27 29
R19E | 1273 36 30 19 12 24 33 21 10 | 52 56 52 43 42 63 40 40
R20E | 1697 45 40 34 17 32 56 21 14 | 113 115 124 120 130 112 113 117
R21E | 590 31 32 25 17 27 33 17 10 | 35 37 32 32 40 35 25 25
R22E | 928 34 30 17 12 20 29 14 8 | 42 34 31 37 47 41 41 35
R23E | 3895 25 33 20 20 27 27 15 9 | 41 46 34 41 39 29 29 32
R24E | 990 25 24 33 22 29 29 28 12 | 44 55 49 46 46 33 39 38
XR26E | ---- 35 105 --- --- --- --- 11 19 | 45 129 --- --- --- --- 34 32
XR27 | ---- --- --- --- --- --- --- 3 0 | --- --- --- --- --- --- 85 86
------+----------------------------------------------+------------------------------------------
RMS | 1784 51 50 29 19 27 41 20 |T 59 65 50 49 48 43 41 43
WRMS | 1784 51 51 30 18 21 38 20 |NE 64 65 49 49 46 41 41 44
MEDI | 1100 34 33 21 17 22 30 16 |MD 56 58 49 48 44 41 38 39
Table 3.1875.1 GPS week: 1875 Day: 1 MJD: 57370
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 736 26 27 17 20 16 33 13 8 | 40 40 38 37 40 43 26 32
R02 | 735 14 18 21 16 14 24 14 7 | 29 31 37 34 27 16 19 24
R03 | 600 13 11 18 24 19 53 10 10 | 39 37 34 54 47 58 40 40
R04 | 962 29 24 28 19 20 24 17 10 | 51 49 41 41 33 22 28 32
R05 | 887 36 40 23 22 14 28 17 9 | 47 54 48 32 28 37 18 27
R06 | 1140 25 24 10 10 8 18 7 5 | 31 31 41 39 39 47 49 41
R07 | 609 35 40 31 13 13 24 26 11 | 48 51 48 29 25 22 18 25
R08 | 2382 29 25 19 18 10 23 7 7 | 43 41 40 26 22 18 24 25
R09 | 513 41 41 32 23 18 45 16 12 | 49 55 35 41 34 31 34 31
R10 | 1245 23 24 14 21 20 26 10 8 | 39 39 34 33 33 29 26 28
R11 | 1036 124 124 33 29 41 39 17 20 | 84 85 35 52 58 40 32 34
R12 | 848 123 136 66 36 53 55 24 25 | 82 95 48 60 70 45 35 37
R13 | 667 60 70 16 27 28 35 13 12 | 59 69 35 42 32 33 29 30
R14 | 1525 32 32 22 32 19 44 12 11 | 35 46 39 58 48 29 39 39
R15 | 9281 27 28 15 17 39 23 23 11 | 49 50 38 43 44 45 32 36
R16 | 827 27 36 18 28 16 22 9 8 | 43 49 38 47 35 87 32 34
R18E | 1192 31 31 18 15 13 28 12 8 | 40 37 26 28 29 35 26 25
R19E | 1173 31 27 22 24 16 111 14 17 | 52 52 44 43 51 95 44 47
R20E | 1267 54 37 35 24 46 69 23 17 | 73 68 65 69 74 72 58 60
R21E | 1073 33 27 17 15 27 27 12 9 | 36 31 26 27 38 37 27 26
R22E | 1580 34 51 35 23 25 27 15 11 | 38 51 41 34 38 29 23 26
R23E | 4345 32 36 28 24 13 24 18 10 | 38 43 39 37 32 35 39 33
R24E | 739 32 40 19 20 18 31 14 9 | 36 46 40 41 35 51 35 34
XR26E | ---- 60 105 --- --- --- --- 14 29 | 63 137 --- --- --- --- 34 36
XR27 | ---- --- --- --- --- --- --- 2 0 | --- --- --- --- --- --- 92 92
------+----------------------------------------------+------------------------------------------
RMS | 2388 48 51 27 23 25 41 16 |T 47 53 39 41 39 41 34 35
WRMS | 2388 37 39 29 21 19 37 16 |NE 48 51 39 41 38 37 33 35
MEDI | 1036 32 32 21 22 18 28 14 |MD 43 49 39 41 35 37 32 33
Table 3.1875.2 GPS week: 1875 Day: 2 MJD: 57371
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 644 43 43 30 28 25 16 14 11 | 45 51 43 42 45 30 16 27
R02 | 966 16 18 26 11 20 18 15 8 | 34 36 27 28 36 24 13 23
R03 | 545 10 19 12 27 14 29 14 8 | 49 55 48 63 56 53 37 48
R04 | 545 22 19 23 15 10 41 11 8 | 45 43 50 41 37 41 26 35
R05 | 784 26 32 23 21 12 60 19 11 | 43 49 50 43 31 35 27 31
R06 | 672 21 20 22 11 10 17 19 7 | 34 39 37 40 39 48 36 36
R07 | 624 33 34 25 12 12 29 16 9 | 60 61 50 37 36 21 36 37
R08 | 2290 27 30 18 18 13 27 15 8 | 55 57 54 47 33 40 28 37
R09 | 497 38 48 39 33 18 35 14 12 | 50 59 34 48 41 43 40 37
R10 | 1131 16 26 22 23 14 24 14 8 | 40 52 35 45 33 32 39 34
R11 | 1579 110 104 40 30 35 58 18 20 | 89 84 40 47 47 45 30 32
R12 | 681 100 97 40 38 36 40 21 19 | 84 84 33 68 57 35 33 38
R13 | 577 61 70 18 23 29 27 14 12 | 64 71 32 48 49 32 32 35
R14 | 2246 45 47 23 30 19 41 14 11 | 41 47 50 58 47 38 46 44
R15 | 6974 26 34 16 17 18 33 12 8 | 52 59 45 44 43 28 37 38
R16 | 764 26 28 23 24 18 254 14 10 | 42 41 45 52 42 174 33 38
R18E | 905 34 35 20 21 17 26 11 8 | 34 39 31 37 23 31 25 24
R19E | 919 29 31 24 28 14 147 13 20 | 48 49 42 37 41 131 30 33
R20E | 1331 31 34 26 28 22 35 20 11 | 57 61 59 65 52 55 52 51
R21E | 1016 38 41 23 18 24 29 11 10 | 45 49 32 31 40 35 30 30
R22E | 1070 36 31 18 16 25 29 10 9 | 39 36 34 32 42 33 30 30
R23E | 3357 32 49 16 25 18 23 14 9 | 40 51 33 55 44 37 35 37
R24E | 871 33 35 50 15 23 45 17 13 | 47 48 57 43 38 52 44 40
XR26E | ---- 57 544 --- --- --- --- 15 29 | 58 595 --- --- --- --- 28 28
XR27 | ---- --- --- --- --- --- --- 4 0 | --- --- --- --- --- --- 113 114
------+----------------------------------------------+------------------------------------------
RMS | 1926 44 46 27 23 21 69 15 |T 49 75 41 45 41 47 35 38
WRMS | 1926 36 37 27 21 16 34 15 |NE 51 55 42 46 42 44 36 40
MEDI | 905 32 34 23 23 18 29 14 |MD 45 51 42 44 41 37 33 36
Table 3.1875.3 GPS week: 1875 Day: 3 MJD: 57372
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 784 39 37 31 20 17 24 22 11 | 48 53 52 44 41 33 25 33
R02 | 804 20 16 18 10 17 16 11 6 | 41 38 29 31 31 44 27 29
R03 | 728 16 15 15 12 10 23 10 6 | 49 51 45 41 33 55 36 39
R04 | 586 19 24 13 15 12 19 16 7 | 48 53 43 43 42 33 26 36
R05 | 773 24 25 32 26 19 50 15 12 | 49 48 43 55 49 32 39 42
R06 | 835 13 19 21 32 12 20 16 9 | 41 48 34 56 40 26 40 38
R07 | 555 18 26 18 10 21 28 22 9 | 59 67 57 55 67 30 37 49
R08 | 2164 29 28 26 21 14 46 9 10 | 57 61 53 35 48 37 38 39
R09 | 628 26 30 52 30 19 47 21 14 | 53 52 43 59 48 46 43 43
R10 | 1362 8 23 24 20 11 20 11 7 | 42 33 42 50 38 43 43 41
R11 | 3109 112 118 36 23 29 59 28 21 | 98 102 49 44 45 41 34 34
R12 | 995 105 97 41 32 45 49 22 21 | 95 97 39 61 68 44 33 39
R13 | 682 41 34 13 19 26 45 7 10 | 55 51 37 41 32 49 37 34
R14 | 2605 30 30 30 26 29 48 24 13 | 45 59 55 63 51 36 45 45
R15 | 6863 21 19 17 20 28 44 14 10 | 50 49 47 50 52 37 40 41
R16 | 840 20 32 22 27 17 25 12 9 | 40 47 49 48 37 84 37 38
R18E | 639 27 27 18 14 16 22 12 7 | 35 40 31 27 25 28 26 22
R19E | 911 36 39 26 18 27 30 16 11 | 55 57 46 44 42 87 41 42
R20E | 1887 29 40 45 22 28 32 23 13 | 44 49 49 40 43 45 43 37
R21E | 968 32 31 31 15 18 27 12 9 | 45 45 31 30 31 38 27 27
R22E | 1723 38 43 28 11 27 30 15 10 | 44 50 27 30 38 32 22 25
R23E | 2989 28 27 16 18 23 20 13 8 | 41 39 38 49 48 32 43 39
R24E | 1145 38 48 44 21 23 54 16 13 | 45 58 52 49 47 55 39 40
XR26E | ---- 48 1255 --- --- --- --- 15 28 | 50 9999 --- --- --- --- 71 62
XR27 | ---- --- --- --- --- --- --- 3 0 | --- --- --- --- --- --- 153 153
------+----------------------------------------------+------------------------------------------
RMS | 2036 41 43 29 21 23 36 17 |T 51 54 43 45 43 42 41 42
WRMS | 2036 33 34 30 20 15 36 17 |NE 54 56 44 48 45 41 43 45
MEDI | 911 28 30 26 20 19 30 15 |MD 48 51 43 44 42 38 38 39
Table 3.1875.4 GPS week: 1875 Day: 4 MJD: 57373
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 1612 24 15 35 15 16 19 17 9 | 50 41 58 39 37 40 33 38
R02 | 611 18 22 25 11 12 28 10 7 | 48 51 50 37 37 28 41 37
R03 | 652 17 24 23 16 9 10 8 6 | 51 51 53 42 42 47 41 43
R04 | 907 14 17 12 18 19 20 13 7 | 50 57 49 54 50 39 36 44
R05 | 522 21 17 36 27 12 55 14 12 | 49 54 55 61 48 37 35 44
R06 | 1532 20 22 26 25 14 11 12 8 | 25 23 34 46 32 38 29 31
R07 | 1045 21 17 22 22 11 28 20 9 | 55 52 52 57 37 35 31 41
R08 | 1146 17 18 16 14 14 56 9 9 | 55 57 49 58 54 34 50 48
R09 | 462 22 32 50 34 21 42 19 14 | 41 51 40 55 44 45 44 40
R10 | 1972 16 24 19 23 13 21 13 7 | 36 45 37 45 36 30 33 34
R11 | 3015 128 136 40 21 32 47 19 22 | 96 106 46 44 48 43 34 34
R12 | 1064 110 121 29 24 32 43 19 19 | 89 100 42 45 47 41 33 35
R13 | 696 35 26 17 12 29 36 14 10 | 52 48 40 39 35 42 34 33
R14 | 1518 35 36 44 17 26 44 17 13 | 39 41 38 51 45 33 34 35
R15 | 7424 21 28 14 19 37 27 19 11 | 46 53 39 47 45 34 39 38
R16 | 586 16 19 18 19 19 21 11 7 | 43 46 43 47 39 41 37 37
R18E | 668 30 23 18 21 13 28 10 8 | 43 40 35 37 31 37 31 31
R19E | 781 32 35 20 16 16 31 16 9 | 48 56 36 43 42 42 40 37
R20E | 2413 32 41 49 21 29 26 19 13 | 48 60 52 42 50 38 44 40
R21E | 1027 39 39 24 16 14 26 16 9 | 58 56 36 37 40 41 31 35
R22E | 2354 40 44 35 12 13 28 17 10 | 41 44 35 36 30 44 30 30
R23E | 1259 23 32 18 24 11 36 18 9 | 37 39 30 52 34 34 36 34
R24E | 1030 26 31 44 19 17 36 15 11 | 53 55 55 50 46 52 40 43
XR26E | ---- 73 1067 --- --- --- --- 24 43 | 53 9999 --- --- --- --- 45 31
XR27 | ---- --- --- --- --- --- --- 8 0 | --- --- --- --- --- --- 71 72
------+----------------------------------------------+------------------------------------------
RMS | 2063 43 46 30 20 20 34 16 |T 50 53 43 46 41 38 38 38
WRMS | 2063 32 34 29 21 17 30 16 |NE 51 54 45 47 42 37 38 40
MEDI | 1045 23 26 24 19 16 28 16 |MD 48 51 42 45 42 39 36 37
Table 3.1875.5 GPS week: 1875 Day: 5 MJD: 57374
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 886 14 19 24 14 25 15 16 8 | 32 41 46 33 59 33 33 39
R02 | 622 19 19 18 11 15 21 12 7 | 44 41 38 27 41 34 32 34
R03 | 736 21 20 19 14 11 10 9 6 | 49 48 47 30 39 35 34 36
R04 | 503 14 21 21 14 10 23 11 6 | 42 48 45 33 40 50 46 39
R05 | 482 25 34 31 22 17 61 19 12 | 31 43 39 36 45 38 34 34
R06 | 1103 29 27 16 30 12 34 9 9 | 24 30 33 44 24 33 28 26
R07 | 940 10 11 12 22 7 32 15 7 | 43 39 48 56 43 33 40 43
R08 | 1010 20 17 14 28 9 47 8 9 | 43 38 39 56 40 23 38 38
R09 | 693 23 28 31 28 21 34 21 11 | 37 50 48 51 44 51 40 40
R10 | 2020 12 22 18 21 16 23 10 7 | 32 38 32 36 32 32 29 28
R11 | 2592 118 121 43 16 29 57 22 21 | 85 90 37 35 46 42 30 32
R12 | 874 119 131 36 18 35 37 18 20 | 91 99 36 41 47 35 30 33
R13 | 670 36 55 30 26 21 39 10 11 | 49 64 44 48 40 43 31 36
R14 | 1075 51 50 31 35 24 57 21 15 | 35 47 47 47 42 28 31 31
R15 | 5764 29 35 18 21 27 46 20 11 | 45 52 32 43 44 30 29 32
R16 | 538 14 24 22 28 16 33 7 9 | 36 45 35 47 35 41 30 31
R18E | 676 36 52 16 18 14 17 15 8 | 31 50 26 35 35 29 27 26
R19E | 1041 28 32 16 13 15 28 15 8 | 48 51 40 39 42 44 31 35
R20E | 1868 35 40 40 18 21 48 28 13 | 44 47 57 47 47 59 41 42
R21E | 872 42 37 26 17 20 24 18 10 | 49 49 31 36 33 39 29 29
R22E | 2347 33 29 24 16 13 33 11 9 | 36 34 25 29 26 41 21 22
R23E | 1448 27 27 23 23 9 31 25 10 | 31 33 28 27 20 24 31 22
R24E | 1597 29 34 45 27 27 47 21 14 | 44 48 39 44 29 43 37 31
XR26E | ---- 77 292 --- --- --- --- 28 46 | 103 377 --- --- --- --- 33 43
XR27 | ---- --- --- --- --- --- --- 4 0 | --- --- --- --- --- --- 64 64
------+----------------------------------------------+------------------------------------------
RMS | 1725 44 48 27 22 19 37 17 |T 46 62 38 40 38 37 33 34
WRMS | 1725 42 47 28 21 20 35 17 |NE 44 50 40 41 41 36 35 36
MEDI | 940 28 29 23 21 16 33 15 |MD 43 47 39 39 40 35 31 34
Table 3.1875.6 GPS week: 1875 Day: 6 MJD: 57375
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 891 21 16 19 12 20 16 15 7 | 59 61 68 55 46 47 43 50
R02 | 1232 15 21 15 13 18 31 13 7 | 61 65 54 55 51 50 47 51
R03 | 777 15 20 16 13 13 21 11 6 | 59 59 60 49 52 65 48 52
R04 | 843 25 25 27 14 14 13 9 7 | 54 55 55 44 38 34 38 41
R05 | 486 28 37 25 16 14 45 23 11 | 48 54 53 57 55 40 45 48
R06 | 754 27 30 13 13 17 26 13 7 | 26 28 41 50 52 36 45 41
R07 | 1568 15 18 16 13 17 38 16 8 | 65 67 70 70 68 32 54 60
R08 | 735 17 16 11 17 15 35 13 8 | 65 62 63 66 64 36 58 58
R09 | 553 19 23 38 27 33 42 25 13 | 47 54 37 56 43 39 45 38
R10 | 899 15 15 12 18 13 40 12 8 | 42 41 39 46 33 32 35 35
R11 | 2823 126 121 69 31 41 78 26 26 | 112 107 62 41 59 69 43 37
R12 | 663 125 130 34 18 31 44 27 21 | 118 125 42 47 61 53 39 41
R13 | 706 46 47 18 14 22 22 13 9 | 66 68 41 42 35 40 36 37
R14 | 815 47 54 29 33 33 39 24 14 | 50 54 41 58 41 39 43 40
R15 | 4902 38 31 18 18 43 30 22 12 | 61 56 37 50 48 33 43 41
R16 | 1392 18 22 25 21 25 30 9 9 | 48 52 51 54 44 32 42 43
R18E | 683 27 26 23 15 15 22 16 8 | 41 40 38 38 29 35 35 32
R19E | 1662 34 45 32 14 29 32 16 11 | 46 46 36 46 52 40 45 39
R20E | 2086 37 36 65 17 23 44 28 16 | 43 43 49 38 43 52 45 38
R21E | 745 39 44 25 10 18 25 13 9 | 44 50 36 26 33 34 34 28
R22E | 2465 33 35 22 10 26 28 10 9 | 44 47 41 35 39 42 29 31
R23E | 985 22 21 14 22 11 12 20 8 | 37 35 39 41 40 34 40 36
R24E | 2905 35 41 61 30 24 34 33 16 | 49 59 50 49 49 40 39 39
XR26E | ---- 49 139 --- --- --- --- 20 31 | 81 174 --- --- --- --- 34 35
XR27 | ---- --- --- --- --- --- --- 4 0 | --- --- --- --- --- --- 75 75
------+----------------------------------------------+------------------------------------------
RMS | 1716 46 48 32 19 24 35 19 |T 56 62 47 48 46 41 43 42
WRMS | 1716 35 36 32 16 21 33 19 |NE 61 63 50 52 49 42 45 46
MEDI | 891 27 30 23 16 20 31 16 |MD 49 54 42 49 46 39 43 40
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