[IGSREPORT-26929] Wk 2078 IGLOS Final Orbits
acc
acc at igs.org
Sun Nov 24 02:45:49 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2078 (Nov 03, 2019 - Nov 09, 2019)
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 2.2078.
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:
igl2078[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2078 in the SP3 format.
igl20787.sum Combination Report for GPS Week 2078.
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 | -11.2 ns
1 | -11.4 ns
2 | -11.7 ns
3 | -11.8 ns
4 | -11.0 ns
5 | 1.1 ns
6 | 0.0 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 1.2078, 1a.2078).
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 2.2078.0-6)
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 3.2078.0-6).
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 2078 summary. (Nov 03, 2019 - Nov 09, 2019)
Table 1.2078.a GPS week : 2078 MJD: 58790.0-58796.0
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 0 13 15 39 .08 18 15 | 14824 59 3034 7535
| 0 1 0 12 7 23 .03 | 7670 1081
cof n/a| 0 0 1 20 26 33 .09 21 17 | 14822 51 3033 7535
| 1 1 1 13 24 29 .04 | 7667 1068
emx n/a| 0 0 -1 -29 -10 19 .01 24 24 | -10315 -210 3063 7624
| 1 1 3 27 15 53 .05 | 10583 810
esx n/a| 0 1 2 47 -11 -13 .14 22 19 | -1764 -892 3035 9784
| 1 1 1 17 17 29 .04 | 10846 1317
gfz n/a| 0 0 0 11 -16 -18 .21 27 22 | 0 -10 3025 7483
| 1 1 2 15 14 34 .04 | 0 845
grg n/a| 1 1 -4 -69 -11 -9 -.37 25 22 | -7971 -209 3031 6818
| 1 0 1 10 12 34 .04 | 5717 1026
iac n/a| 0 -1 2 9 20 -21 -.07 24 22 | -6629 -521 3039 7703
| 0 1 3 23 20 65 .04 | 6119 554
mcc n/a| -1 1 21 46 30 946 -.10 157 157 | --- --- --- ---
| 17 8 20 116 112 1054 .16 | --- ---
Table 1.2078.b GPS week : 2078 MJD: 58790.0-58796.0
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 | 18 20 18 18 16 13 14 |
R02 | 6 5 6 5 5 7 5 |
R03 | 5 6 5 6 6 7 7 |
R05 | 8 8 9 9 10 11 9 |
R07 | 8 7 7 6 6 6 6 |
R08 | 9 7 7 7 7 7 8 |
R09 | 7 7 8 6 6 8 8 |
R11 | 9 9 7 7 7 6 6 |
R12 | 15 13 12 12 12 13 12 |
R13 | 6 11 9 6 7 7 8 |
R14 | 6 8 8 9 8 8 9 |
R15 | 14 14 11 12 13 13 11 |
R16 | 15 17 13 15 11 11 12 |
R17 | 7 7 7 6 9 7 7 |
R18 | 6 6 6 6 10 8 8 |
R19 | 23 20 19 17 21 18 21 |
R20 | 12 14 13 10 12 11 10 |
R21 | 8 9 8 8 9 8 8 |
R22 | 7 7 8 8 9 8 8 |
R23 | 8 9 10 9 13 9 8 |
R24 | 12 13 18 10 12 14 13 |
R26 | 11 17 17 24 40 40 41 |
Table 1.2078.c GPS week : 2078 MJD: 58790.0-58796.0
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 2078 0 | 33 -40 107 -149 1329 -1583 83.4 1583 1583 | -11241 0
brd 2078 1 | -1 4 179 -245 146 -4702 84.8 1356 1356 | -11385 0
brd 2078 2 | -29 8 107 -362 -1500 -2580 84.2 1263 1263 | -11675 0
brd 2078 3 | 51 -22 54 -1534 -416 -457 81.7 1330 1330 | -11758 0
brd 2078 4 | -35 -35 17 -315 546 -48 82.3 1247 1247 | -10985 0
brd 2078 5 | 73 47 116 935 835 -848 82.6 1376 1376 | 1091 0
brd 2078 6 | 85 -72 169 815 -429 -927 81.2 1408 1408 | 2 0
-------------+------------------------------------------------------------+----------------
brd 2078 mean| 25 -15 107 -122 73 -1592 82.9 1366 1366 | -7993 0
brd 2078 sdev| 48 39 57 826 944 1597 1.3 111 111 | 5847 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 2.2078.0 GPS week: 2078 Day: 0 MJD: 58790
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 35 8 23 .05 17 14 | 10091 1191 3292 8137
cof n/a| 0 0 2 43 54 -16 .09 21 17 | 10082 1183 3296 8142
emx n/a| 0 0 3 -43 15 -17 .07 24 24 | -17300 -50 3296 8275
esx n/a| 0 0 3 46 -9 17 .17 26 20 | -218 -689 3290 9986
gfz n/a| -1 0 1 -1 -15 -69 .25 34 27 | 0 -173 3280 8105
grg n/a| 0 1 -4 -55 -16 -44 -.37 22 21 | -11545 139 3282 7426
iac n/a| 0 0 -2 19 -10 89 -.03 25 24 | -10462 508 3289 8288
mcc n/a| 0 -4 40 231 -80 552 -.39 185 185 | --- --- --- ---
Table 2.2078.1 GPS week: 2078 Day: 1 MJD: 58791
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 1 20 18 41 .07 18 16 | 11308 -1314 3225 7099
cof n/a| 0 1 1 35 14 56 .06 20 17 | 11296 -1321 3223 7103
emx n/a| 1 -1 0 -77 0 74 -.01 24 24 | -19266 -1101 3212 7163
esx n/a| 0 3 3 37 -11 0 .07 27 22 | -1677 396 3220 8686
gfz n/a| 0 -2 -2 36 -29 -21 .24 27 23 | 0 25 3208 7083
grg n/a| 0 0 -4 -52 -7 1 -.36 29 22 | -10776 -1330 3220 6560
iac n/a| 0 0 -2 39 30 -102 -.07 25 23 | -9800 -568 3224 7255
mcc n/a| 0 -3 34 -59 182 621 -.13 187 187 | --- --- --- ---
Table 2.2078.2 GPS week: 2078 Day: 2 MJD: 58792
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 1 10 10 47 .06 17 13 | 9936 -748 2694 6881
cof n/a| -2 1 0 10 26 40 .03 21 17 | 9933 -745 2693 6883
emx n/a| 0 1 0 -32 -22 82 .03 24 24 | -17040 -978 2878 7087
esx n/a| 2 1 0 39 -3 -56 .11 24 21 | 5191 -2109 2705 9428
gfz n/a| 1 0 -2 4 -26 2 .21 28 23 | 0 -857 2704 6781
grg n/a| 0 2 -6 -74 5 -67 -.30 26 21 | -11165 -1081 2684 6279
iac n/a| -1 -2 4 31 14 -75 -.09 23 22 | -10609 -375 2711 7044
mcc n/a| 15 -4 -6 191 3 154 -.16 132 132 | --- --- --- ---
Table 2.2078.3 GPS week: 2078 Day: 3 MJD: 58793
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 -1 -3 20 12 .07 19 16 | 9868 -112 3276 7952
cof n/a| -2 -1 0 10 32 14 .07 18 16 | 9872 -121 3273 7948
emx n/a| 1 -1 -2 9 -31 51 .06 22 22 | -18721 191 3271 8021
esx n/a| 0 3 3 41 16 -8 .16 20 18 | -21276 -1832 3273 9952
gfz n/a| 0 0 1 25 -17 -26 .15 24 15 | 0 -535 3274 7769
grg n/a| 0 1 -8 -77 -5 -3 -.41 24 25 | -11476 -430 3282 7017
iac n/a| 0 -2 3 -13 5 -37 -.02 22 20 | -10244 -572 3289 8262
mcc n/a| 9 -6 21 29 50 312 .00 117 117 | --- --- --- ---
Table 2.2078.4 GPS week: 2078 Day: 4 MJD: 58794
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 5 20 27 .10 20 16 | 10544 1100 2981 8421
cof n/a| 0 -1 1 18 59 32 .10 21 19 | 10562 1059 2978 8413
emx n/a| 2 -1 -4 -8 -11 23 .02 28 28 | -8350 1043 2985 8515
esx n/a| -2 1 1 85 -21 -53 .15 22 19 | -9806 565 2992 10509
gfz n/a| 0 0 0 -1 -22 -39 .22 24 18 | 0 1139 2986 8245
grg n/a| 0 1 -3 -79 -33 29 -.35 25 22 | -11615 1308 2984 7497
iac n/a| -2 0 3 -26 39 25 -.13 23 21 | -9925 -446 2996 8630
mcc n/a| 1 12 25 -15 7 584 .09 105 105 | --- --- --- ---
Table 2.2078.5 GPS week: 2078 Day: 5 MJD: 58795
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 10 3 37 .10 19 15 | 25249 1165 3087 7599
cof n/a| 0 0 0 16 -2 32 .13 24 17 | 25256 1148 3078 7590
emx n/a| 1 0 -5 -18 -9 -19 -.03 25 25 | 4405 340 3103 7568
esx n/a| -1 1 3 35 -4 13 .16 17 16 | 11581 110 3069 10598
gfz n/a| 0 -2 3 -1 -20 42 .17 25 23 | 0 1136 3045 7618
grg n/a| 2 0 -4 -73 -9 0 -.39 23 20 | 513 905 3074 6871
iac n/a| 0 0 4 13 13 -53 -.06 25 24 | 2530 -891 3074 7632
mcc n/a| 3 4 40 -49 -115 1177 -.00 118 118 | --- --- --- ---
Table 2.2078.6 GPS week: 2078 Day: 6 MJD: 58796
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 16 23 86 .12 19 17 | 26774 -869 2689 6660
cof n/a| 0 1 2 8 1 76 .13 24 18 | 26758 -845 2692 6667
emx n/a| 0 0 -3 -34 -11 -59 -.05 22 22 | 4065 -917 2701 6740
esx n/a| -2 1 0 44 -42 -10 .16 19 18 | 3855 -2688 2696 9334
gfz n/a| 0 -1 3 14 13 -19 .24 26 22 | 0 -806 2682 6785
grg n/a| 2 0 -3 -74 -16 20 -.41 24 21 | 262 -980 2694 6082
iac n/a| 0 -2 3 3 47 2 -.10 22 21 | 2106 -1305 2692 6811
mcc n/a| -37 14 -6 0 164 3227 -.09 256 256 | --- --- --- ---
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 3.2078.0 GPS week: 2078 Day: 0 MJD: 58790
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 | 748 38 46 46 60 37 15 28 --- 18 | 95 99 88 53 76 73 50 --- 69
R02 | 1005 9 12 8 18 15 13 14 68 5 | 55 58 51 44 60 56 43 66 50
R03 | 632 6 9 10 9 23 8 12 144 5 | 60 62 55 51 67 60 51 44 56
R05 | 1029 20 26 13 19 17 14 22 --- 8 | 52 51 48 30 35 37 31 --- 38
R07 | 930 9 8 9 20 12 22 30 151 8 | 67 65 64 58 64 78 48 146 63
R08 | 1569 10 10 13 15 38 12 24 --- 8 | 64 65 60 68 85 73 54 --- 66
R09 | 2127 8 10 12 16 17 21 9 --- 6 | 50 51 49 50 60 61 52 --- 52
R11 | 1431 12 14 17 14 38 16 28 311 9 | 67 69 48 55 86 54 35 146 56
R12 | 548 18 41 24 41 48 31 40 --- 14 | 79 96 47 42 102 83 34 --- 62
R13 | 2808 6 11 9 12 19 18 10 --- 5 | 49 52 47 59 60 34 48 --- 48
R14 | 1161 12 14 18 16 13 10 15 --- 6 | 59 61 38 50 56 52 37 --- 49
R15 | 764 11 17 22 30 34 37 45 --- 13 | 83 88 66 59 102 101 43 --- 74
R16 | 636 21 18 34 37 47 40 18 --- 14 | 65 66 45 66 74 88 57 --- 63
R17E | 1942 15 9 19 11 18 11 15 --- 6 | 54 53 55 53 59 47 57 --- 52
R18E | 1347 9 12 20 10 13 13 15 --- 6 | 37 41 42 38 40 40 38 --- 38
R19E | 581 38 34 53 46 91 36 52 --- 23 | 47 74 56 83 96 73 70 --- 58
R20E | 976 18 13 34 27 31 18 30 --- 11 | 51 54 63 63 58 65 56 --- 55
R21E | 2740 12 18 26 15 21 15 16 162 7 | 22 25 27 33 28 30 36 42 26
R22E | 774 10 18 24 12 19 8 15 --- 6 | 73 79 68 84 86 73 85 --- 76
R23E | 2935 11 20 13 21 29 16 21 --- 8 | 89 90 92 95 87 96 97 --- 91
R24E | 2350 20 28 25 27 27 36 19 --- 11 | 89 95 87 108 93 100 92 --- 92
XR26E | ---- 9 36 --- --- --- --- 13 --- 10 | 39 41 --- --- --- --- 32 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1582 17 21 24 26 34 22 25 185 |T 61 65 56 59 70 65 52 88 57
WRMS | 1582 14 17 24 20 27 21 24 185 |NE 65 67 54 52 71 65 44 100 57
MEDI | 1029 11 14 19 18 23 16 18 151 |MD 59 62 55 55 67 65 48 66 56
Table 3.2078.1 GPS week: 2078 Day: 1 MJD: 58791
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 | 600 36 27 49 71 27 24 36 --- 19 | 70 62 70 59 61 52 32 --- 52
R02 | 1361 8 11 8 14 11 13 12 92 5 | 38 34 36 32 36 39 33 55 34
R03 | 672 8 10 7 23 15 11 9 159 6 | 41 41 39 29 47 42 38 59 38
R05 | 1191 19 16 17 17 18 11 20 --- 8 | 34 37 29 41 40 34 26 --- 29
R07 | 800 11 13 13 25 12 18 13 188 7 | 47 48 45 34 40 50 33 134 39
R08 | 1687 8 14 17 13 26 15 15 --- 7 | 46 48 41 46 62 48 37 --- 45
R09 | 1988 8 15 14 19 18 21 14 --- 7 | 37 44 39 31 44 48 35 --- 37
R11 | 1295 15 14 16 13 28 13 29 273 9 | 48 47 37 37 57 37 23 140 39
R12 | 508 23 15 24 30 41 20 37 --- 13 | 55 42 38 35 62 49 25 --- 41
R13 | 1994 13 10 12 19 25 49 11 --- 10 | 37 34 32 42 51 24 29 --- 31
R14 | 759 15 16 19 13 12 19 20 --- 7 | 38 36 32 31 39 43 24 --- 33
R15 | 1073 18 19 19 29 31 30 49 --- 13 | 58 56 45 41 67 63 27 --- 48
R16 | 687 28 34 33 40 30 69 21 --- 17 | 43 46 27 50 55 98 43 --- 48
R17E | 1860 13 12 18 9 22 19 12 --- 7 | 38 40 39 38 45 34 33 --- 36
R18E | 1087 9 14 14 16 17 17 10 --- 6 | 22 22 27 31 24 33 21 --- 23
R19E | 1151 30 41 41 43 64 49 37 --- 19 | 41 65 47 48 61 71 56 --- 45
R20E | 1129 17 23 41 23 22 37 36 --- 13 | 37 43 55 31 44 41 35 --- 34
R21E | 1639 13 18 27 13 23 19 16 175 8 | 18 22 23 28 23 16 22 73 18
R22E | 914 12 18 21 12 17 16 18 --- 7 | 46 48 47 55 51 55 47 --- 49
R23E | 2621 17 24 17 22 26 15 20 --- 8 | 63 71 61 70 61 64 63 --- 61
R24E | 1146 27 26 26 18 27 34 41 --- 13 | 66 70 63 65 68 68 53 --- 60
XR26E | ---- 13 58 --- --- --- --- 20 --- 16 | 28 36 --- --- --- --- 25 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1355 18 20 24 27 27 29 25 187 |T 43 45 41 41 49 48 34 92 39
WRMS | 1355 16 17 24 22 23 22 23 187 |NE 45 44 39 39 50 48 31 97 39
MEDI | 1146 13 16 18 19 23 19 20 175 |MD 41 43 39 38 51 48 33 73 38
Table 3.2078.2 GPS week: 2078 Day: 2 MJD: 58792
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 | 610 32 38 41 63 16 29 39 --- 17 | 79 87 78 53 69 78 41 --- 62
R02 | 1283 10 9 10 15 18 12 13 121 5 | 46 54 47 56 66 50 42 115 49
R03 | 582 9 13 7 13 10 9 9 87 4 | 50 51 53 42 56 50 47 83 49
R05 | 828 9 10 15 27 20 15 26 --- 8 | 34 38 40 39 53 36 28 --- 35
R07 | 800 14 13 10 17 17 15 12 198 6 | 60 60 54 52 46 56 45 143 51
R08 | 1072 5 10 14 13 9 20 24 --- 6 | 57 60 49 58 56 64 54 --- 55
R09 | 1966 13 9 13 15 26 21 12 --- 7 | 31 29 31 34 39 29 32 --- 30
R11 | 1385 13 15 15 11 13 15 20 157 6 | 53 51 40 38 44 44 31 79 41
R12 | 532 17 32 25 24 34 25 34 --- 11 | 58 70 38 37 69 56 29 --- 47
R13 | 2424 9 14 14 24 14 35 10 --- 8 | 44 46 35 59 47 21 44 --- 41
R14 | 515 12 18 20 18 11 18 25 --- 8 | 44 48 34 36 44 44 31 --- 37
R15 | 872 16 24 22 22 25 30 35 --- 11 | 64 71 53 43 69 71 41 --- 55
R16 | 870 17 26 33 35 24 45 21 --- 13 | 46 47 34 53 58 74 44 --- 48
R17E | 711 10 11 21 9 14 16 14 --- 6 | 49 52 53 56 64 55 54 --- 54
R18E | 629 13 16 13 15 10 18 14 --- 6 | 25 25 27 31 28 29 31 --- 25
R19E | 1284 38 23 41 28 63 58 23 --- 19 | 39 52 44 40 74 75 57 --- 41
R20E | 842 18 26 35 28 29 32 27 --- 12 | 31 32 47 37 46 45 33 --- 31
R21E | 895 14 24 30 12 16 12 18 35 8 | 26 28 31 30 33 28 35 67 28
R22E | 1204 13 17 23 10 19 14 21 --- 7 | 35 32 38 33 40 28 40 --- 33
R23E | 2329 17 24 18 17 38 25 19 --- 10 | 52 56 50 58 44 61 49 --- 50
R24E | 1997 25 31 42 30 70 29 29 --- 17 | 52 70 65 60 100 58 51 --- 56
XR26E | ---- 13 31 --- --- --- --- 21 --- 16 | 29 35 --- --- --- --- 19 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1263 17 21 24 24 28 26 23 132 |T 45 49 44 45 54 50 39 97 42
WRMS | 1263 13 17 24 21 23 21 22 132 |NE 51 54 45 46 55 51 39 105 46
MEDI | 872 13 17 20 17 18 20 21 121 |MD 46 51 44 42 53 50 41 83 41
Table 3.2078.3 GPS week: 2078 Day: 3 MJD: 58793
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 | 1082 43 37 49 42 34 19 39 --- 17 | 92 87 85 47 73 70 46 --- 67
R02 | 463 10 12 14 14 8 12 11 120 5 | 48 48 49 40 47 43 39 63 43
R03 | 582 6 8 9 15 11 21 18 77 6 | 57 59 54 48 50 69 43 60 52
R05 | 674 18 17 27 15 17 18 20 --- 8 | 41 39 48 34 40 32 28 --- 34
R07 | 1046 10 11 11 9 14 19 16 172 6 | 53 54 50 52 56 63 41 87 51
R08 | 700 7 12 12 12 18 18 22 --- 6 | 59 61 54 60 60 70 45 --- 56
R09 | 2788 10 14 12 11 18 12 13 --- 5 | 25 28 23 26 26 24 29 --- 22
R11 | 1750 16 19 16 10 11 17 22 125 7 | 60 60 44 45 52 54 35 53 48
R12 | 612 21 15 23 25 32 27 34 --- 12 | 68 59 43 48 81 71 40 --- 56
R13 | 1260 11 13 11 14 12 18 14 --- 6 | 51 53 37 51 42 30 44 --- 42
R14 | 744 16 17 20 23 26 17 21 --- 9 | 51 48 32 44 62 44 29 --- 41
R15 | 847 22 21 17 24 33 17 37 --- 11 | 67 64 46 45 79 57 35 --- 53
R16 | 1152 20 21 22 37 22 57 29 --- 14 | 48 59 47 64 56 81 48 --- 54
R17E | 1160 13 11 18 10 14 14 8 --- 5 | 44 45 45 39 47 48 39 --- 42
R18E | 599 14 12 13 12 10 15 11 --- 5 | 26 32 29 33 30 34 33 --- 29
R19E | 1435 40 21 32 25 53 42 35 --- 17 | 43 44 42 51 76 64 57 --- 47
R20E | 1340 15 25 26 18 24 36 15 --- 10 | 25 36 39 33 34 41 25 --- 25
R21E | 843 12 23 26 14 22 17 11 48 7 | 24 30 29 32 26 26 27 33 25
R22E | 1057 16 13 24 17 22 16 11 --- 8 | 40 42 41 52 49 42 44 --- 43
R23E | 1765 16 15 18 16 24 30 12 --- 9 | 43 48 39 48 46 58 44 --- 43
R24E | 2737 17 25 25 14 36 23 21 --- 10 | 35 36 42 40 58 32 37 --- 36
XR26E | ---- 21 57 --- --- --- --- 27 --- 24 | 50 52 --- --- --- --- 21 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1330 19 18 22 20 24 24 22 117 |T 47 49 43 44 51 50 37 59 43
WRMS | 1330 16 16 22 18 15 25 20 117 |NE 55 55 47 46 55 54 38 65 47
MEDI | 1057 16 15 18 15 22 18 18 120 |MD 48 48 43 45 50 48 39 60 43
Table 3.2078.4 GPS week: 2078 Day: 4 MJD: 58794
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 | 571 34 30 54 41 16 22 33 --- 15 | 71 69 74 40 60 50 36 --- 52
R02 | 768 9 12 16 12 10 13 12 128 5 | 46 49 45 41 41 42 35 27 40
R03 | 783 10 10 15 13 10 18 17 76 6 | 54 53 49 47 51 61 36 57 48
R05 | 717 24 24 29 24 22 16 12 --- 10 | 45 44 53 35 35 35 30 --- 34
R07 | 627 11 11 8 13 14 9 18 140 5 | 52 53 55 63 64 54 40 60 53
R08 | 1684 11 15 12 13 9 20 19 --- 6 | 51 48 48 47 48 56 44 --- 48
R09 | 3237 14 17 15 13 15 10 11 --- 6 | 35 35 20 33 39 36 33 --- 31
R11 | 762 13 23 18 7 17 13 23 89 7 | 56 62 47 48 58 45 30 58 47
R12 | 728 19 31 23 27 31 25 31 --- 11 | 67 75 44 42 71 65 35 --- 53
R13 | 1013 11 17 16 21 12 15 11 --- 6 | 46 48 34 51 32 37 38 --- 39
R14 | 788 17 19 19 21 14 14 20 --- 8 | 47 50 32 47 48 32 32 --- 39
R15 | 640 19 25 19 23 34 24 44 --- 12 | 64 70 43 46 75 59 37 --- 52
R16 | 1125 19 20 24 19 24 37 27 --- 11 | 47 44 36 57 55 58 34 --- 46
R17E | 1149 11 7 21 26 16 20 17 --- 8 | 49 49 52 66 50 46 45 --- 50
R18E | 1517 11 11 21 33 19 20 16 --- 9 | 23 25 29 43 30 33 34 --- 27
R19E | 1229 49 38 49 37 61 46 32 --- 21 | 42 51 44 49 81 66 58 --- 47
R20E | 1180 13 15 49 18 21 29 22 --- 11 | 30 33 37 38 33 39 32 --- 30
R21E | 1325 9 10 30 12 20 32 16 73 9 | 46 51 43 46 50 56 48 53 45
R22E | 1664 14 19 27 13 26 20 14 --- 8 | 41 43 41 50 52 47 44 --- 44
R23E | 936 26 35 33 8 27 48 16 --- 12 | 45 71 50 56 72 76 52 --- 54
R24E | 735 18 26 37 21 33 23 30 --- 12 | 53 55 58 56 71 42 50 --- 51
XR26E | ---- 34 51 --- --- --- --- 46 --- 40 | 63 39 --- --- --- --- 26 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1247 20 21 28 22 24 25 23 105 |T 48 50 44 47 53 49 38 51 44
WRMS | 1247 16 19 28 19 18 22 21 105 |NE 52 53 44 45 52 48 35 50 44
MEDI | 936 14 19 21 19 19 20 18 89 |MD 47 49 44 47 51 47 36 57 46
Table 3.2078.5 GPS week: 2078 Day: 5 MJD: 58795
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 | 1635 30 35 44 27 13 23 23 --- 12 | 72 76 72 57 65 45 56 --- 58
R02 | 977 7 11 17 11 13 18 21 157 6 | 37 38 45 34 30 46 25 60 35
R03 | 1135 8 11 12 11 16 19 22 69 6 | 50 51 50 50 50 57 39 103 48
R05 | 1123 23 32 32 29 11 24 19 --- 11 | 45 49 53 28 34 33 36 --- 32
R07 | 665 9 12 13 13 14 13 14 123 5 | 48 50 51 45 49 48 39 93 46
R08 | 941 10 15 11 15 14 10 27 --- 6 | 54 63 53 52 55 55 62 --- 53
R09 | 3334 17 19 10 21 26 14 15 --- 8 | 38 43 35 46 40 35 41 --- 38
R11 | 663 14 14 14 4 10 8 20 101 5 | 46 45 36 39 34 35 29 77 36
R12 | 568 25 18 34 21 36 23 35 --- 12 | 65 57 35 39 68 52 36 --- 47
R13 | 1216 10 11 10 14 11 25 11 --- 6 | 39 41 31 45 36 20 35 --- 34
R14 | 1342 13 17 29 13 18 10 22 --- 8 | 42 45 30 40 47 30 28 --- 35
R15 | 697 19 20 23 26 34 19 47 --- 12 | 54 55 45 34 61 49 31 --- 43
R16 | 1298 23 30 24 17 24 31 25 --- 10 | 48 52 33 41 55 30 29 --- 37
R17E | 1322 10 18 16 15 14 11 20 --- 6 | 47 46 50 47 49 49 49 --- 47
R18E | 1266 11 14 17 9 14 25 22 --- 7 | 34 32 38 46 32 50 46 --- 39
R19E | 1783 42 46 32 19 59 46 28 --- 17 | 42 85 47 58 76 77 55 --- 52
R20E | 1197 16 15 41 15 20 21 27 --- 10 | 46 50 50 52 44 46 53 --- 46
R21E | 937 12 15 24 10 24 10 17 122 7 | 27 29 34 29 33 24 33 75 26
R22E | 1837 14 8 25 11 25 19 12 --- 8 | 52 53 57 46 53 57 50 --- 50
R23E | 1048 12 45 18 13 21 30 16 --- 8 | 70 87 63 70 74 84 71 --- 70
R24E | 1269 25 32 31 16 40 39 42 --- 14 | 54 57 63 57 66 74 59 --- 57
XR26E | ---- 31 46 --- --- --- --- 50 --- 40 | 48 39 --- --- --- --- 28 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1376 19 24 25 17 25 23 25 118 |T 48 51 46 45 50 47 42 81 43
WRMS | 1376 15 17 25 16 23 20 24 118 |NE 49 51 43 42 48 41 37 83 41
MEDI | 1197 14 17 23 15 18 19 22 122 |MD 47 50 47 46 49 48 39 77 43
Table 3.2078.6 GPS week: 2078 Day: 6 MJD: 58796
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 | 2011 25 32 40 25 35 31 31 --- 14 | 99 100 96 82 99 70 73 --- 83
R02 | 998 9 10 13 9 11 8 14 237 4 | 57 58 55 53 51 56 44 170 52
R03 | 820 12 12 9 16 12 9 23 374 6 | 69 69 62 60 66 64 49 179 61
R05 | 1580 23 21 23 19 17 14 18 --- 8 | 57 55 59 36 41 39 30 --- 42
R07 | 630 10 10 14 16 21 11 10 241 6 | 66 66 67 56 57 65 54 294 60
R08 | 577 21 14 19 15 21 10 16 --- 8 | 67 76 69 78 84 82 83 --- 75
R09 | 3351 18 15 15 15 22 12 23 --- 8 | 48 48 47 42 50 45 53 --- 45
R11 | 1082 13 17 14 8 9 13 15 249 5 | 62 66 50 50 60 49 37 148 51
R12 | 589 24 34 24 21 31 25 35 --- 12 | 86 91 51 48 88 83 41 --- 64
R13 | 2354 15 17 14 18 14 22 14 --- 7 | 58 58 47 65 49 34 49 --- 50
R14 | 876 16 14 31 15 17 20 17 --- 9 | 61 61 33 52 66 62 45 --- 51
R15 | 639 21 18 21 23 19 22 36 --- 11 | 78 79 58 48 83 78 41 --- 62
R16 | 617 24 39 22 28 25 38 17 --- 12 | 64 76 47 63 56 61 50 --- 54
R17E | 691 15 10 18 10 11 14 20 --- 6 | 57 58 60 57 54 51 57 --- 55
R18E | 2056 6 9 17 11 26 28 14 --- 8 | 36 36 44 41 30 48 37 --- 37
R19E | 1032 42 61 32 31 69 57 40 --- 20 | 53 69 69 60 101 86 73 --- 63
R20E | 886 13 20 32 19 26 24 20 --- 10 | 52 50 55 57 49 55 51 --- 51
R21E | 704 14 15 25 12 24 12 14 111 7 | 26 27 31 27 32 20 28 114 24
R22E | 1149 13 18 20 12 28 12 16 --- 7 | 68 73 70 74 77 62 64 --- 68
R23E | 1081 18 16 16 10 19 24 15 --- 7 | 83 94 77 89 87 89 77 --- 83
R24E | 1814 22 25 20 30 34 36 22 --- 12 | 83 90 85 89 87 88 76 --- 82
XR26E | ---- 37 75 --- --- --- --- 44 --- 41 | 68 71 --- --- --- --- 55 --- 51
------+---------------------------------------------------+-----------------------------------------------
RMS | 1408 19 24 22 19 26 24 22 256 |T 63 66 58 58 65 61 53 181 57
WRMS | 1408 17 18 22 18 22 21 21 256 |NE 67 69 57 56 65 60 49 197 57
MEDI | 998 16 17 20 16 21 20 17 241 |MD 62 66 58 57 60 62 50 170 54
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