[IGSREPORT-26966] Wk 2081 IGLOS Final Orbits
acc
acc at igs.org
Thu Dec 12 19:33:19 PST 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2081 (Nov 24, 2019 - Nov 30, 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 2.2081.
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:
igl2081[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2081 in the SP3 format.
igl20817.sum Combination Report for GPS Week 2081.
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 | 0.6 ns
1 | 0.3 ns
2 | -13.2 ns
3 | 1.2 ns
4 | 0.1 ns
5 | -11.5 ns
6 | -11.4 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 1.2081, 1a.2081).
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 2.2081.0-6)
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 3.2081.0-6).
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 2081 summary. (Nov 24, 2019 - Nov 30, 2019)
Table 1.2081.a GPS week : 2081 MJD: 58811.0-58817.0
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 2 32 9 31 .26 23 19 | 20806 -940 3016 7895
| 1 1 1 18 14 34 .07 | 8042 2266
cof n/a| 0 0 4 32 -3 39 .10 26 20 | 20784 -941 3016 7913
| 1 1 1 15 24 39 .07 | 8054 2265
emx n/a| 1 -1 -8 10 6 87 .14 26 26 | -7182 -770 2998 8028
| 1 0 3 14 22 34 .09 | 11511 1421
esx n/a| 0 1 1 13 -24 26 .11 23 19 | -4219 -2004 3022 9868
| 1 1 0 19 17 37 .07 | 10885 1714
gfz n/a| -1 0 0 -17 -19 3 -.09 31 21 | 0 -915 3016 7922
| 1 1 2 14 14 37 .11 | 0 2019
grg n/a| 2 0 0 -45 -2 -139 -.43 25 21 | -4493 -784 3020 7297
| 1 1 4 21 35 71 .18 | 6269 2163
iac n/a| -1 0 2 -3 42 -7 -.04 27 25 | -3042 -416 2997 8049
| 1 2 3 19 15 147 .08 | 7229 1022
mcc n/a| 5 -6 0 98 52 79 -.40 260 260 | --- --- --- ---
| 11 5 25 100 143 1043 .44 | --- ---
Table 1.2081.b GPS week : 2081 MJD: 58811.0-58817.0
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 | 14 16 24 22 18 15 17 |
R02 | 5 7 8 7 6 7 6 |
R03 | 6 6 8 7 7 6 7 |
R05 | 11 9 12 13 11 10 8 |
R07 | 7 7 7 7 6 7 9 |
R08 | 9 11 6 9 9 8 9 |
R09 | 8 7 6 8 8 8 7 |
R11 | 6 7 7 7 8 12 7 |
R12 | 10 8 9 10 11 16 11 |
R13 | 9 8 8 9 9 8 7 |
R14 | 7 8 8 7 9 10 10 |
R15 | 9 10 10 10 10 11 11 |
R16 | 12 12 11 14 17 12 14 |
R17 | 10 11 10 11 9 10 9 |
R18 | 7 7 10 9 9 8 7 |
R19 | 25 26 24 22 29 30 27 |
R20 | 13 11 13 14 12 15 16 |
R21 | 10 11 12 13 11 8 8 |
R22 | 54 12 15 15 12 10 7 |
R23 | 10 10 17 13 10 10 10 |
R26 | 19 18 24 51 13 19 22 |
Table 1.2081.c GPS week : 2081 MJD: 58811.0-58817.0
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 2081 0 | -22 67 132 -310 917 1157 83.0 1684 1684 | 646 0
brd 2081 1 | -43 56 114 -512 -914 -676 82.8 1635 1635 | 302 0
brd 2081 2 | -61 18 80 -640 -355 -1651 80.4 1615 1615 | -13217 0
brd 2081 3 | -26 -39 125 -1321 -329 369 81.7 1619 1619 | 1208 0
brd 2081 4 | 100 1 112 -1220 -369 -387 82.2 1755 1755 | 122 0
brd 2081 5 | -40 1 43 -161 -332 -3716 83.1 2033 2033 | -11468 0
brd 2081 6 | 61 12 39 -797 1129 -342 82.5 2201 2201 | -11355 0
-------------+------------------------------------------------------------+----------------
brd 2081 mean| -4 16 92 -708 -36 -749 82.2 1791 1791 | -4823 0
brd 2081 sdev| 60 35 38 436 755 1570 .9 232 232 | 6761 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 2.2081.0 GPS week: 2081 Day: 0 MJD: 58811
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 3 39 -4 14 .17 20 18 | 27775 1054 2749 7610
cof n/a| 2 -1 3 55 -29 13 .18 23 19 | 27758 1083 2752 7618
emx n/a| 1 0 -4 18 -9 54 -.01 25 22 | 4209 402 2758 7800
esx n/a| -1 3 1 16 -23 24 .12 20 16 | -12792 18 2756 9866
gfz n/a| 0 -1 1 -12 -22 47 .06 30 22 | 0 394 2751 7762
grg n/a| 3 2 -5 -40 19 -213 -.35 25 19 | -185 1267 2743 6948
iac n/a| -4 -2 3 -8 63 121 -.08 24 21 | 2531 299 2755 7827
mcc n/a| 0 1 44 -97 -27 614 -1.22 243 243 | --- --- --- ---
Table 2.2081.1 GPS week: 2081 Day: 1 MJD: 58812
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 4 28 -13 34 .16 23 19 | 28700 -1130 2978 8566
cof n/a| 1 0 2 20 -39 54 .07 27 20 | 28694 -1144 2977 8603
emx n/a| 4 0 -5 33 41 59 .09 24 24 | 8409 -1187 2986 8710
esx n/a| -1 2 0 15 -30 86 .13 21 16 | -8847 -2767 3004 10205
gfz n/a| -1 -1 -2 6 -22 41 -.04 31 22 | 0 -1024 2981 8688
grg n/a| 2 0 2 -77 -45 -226 -.31 23 21 | 753 -1208 2995 7890
iac n/a| -3 -2 0 -24 44 -18 -.18 24 22 | 2951 -256 2995 8789
mcc n/a| -3 -17 -6 72 55 -1373 -.15 320 320 | --- --- --- ---
Table 2.2081.2 GPS week: 2081 Day: 2 MJD: 58813
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 -3 3 13 10 96 .31 24 16 | 12442 -3682 3235 9338
cof n/a| 0 -4 2 34 32 100 -.02 26 18 | 12389 -3672 3231 9341
emx n/a| 0 -2 -9 -1 9 133 .12 27 27 | -16404 -2821 3237 9475
esx n/a| -1 0 2 30 3 58 .04 24 20 | 6785 -3688 3234 10771
gfz n/a| 0 0 0 -22 -5 40 -.02 31 20 | 0 -3648 3229 9197
grg n/a| 4 1 -5 -58 -53 -124 -.50 24 23 | -11707 -3433 3229 9074
iac n/a| -3 1 7 2 48 -262 -.00 32 32 | -12022 -1613 3223 9433
mcc n/a| 18 -5 21 228 -195 -1210 -.56 262 262 | --- --- --- ---
Table 2.2081.3 GPS week: 2081 Day: 3 MJD: 58814
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 30 21 47 .34 22 17 | 25279 2308 2981 6992
cof n/a| -1 -1 6 18 7 36 .14 27 17 | 25254 2290 2976 7033
emx n/a| 0 0 -5 7 8 58 .12 29 28 | -14288 681 2976 7209
esx n/a| 0 0 2 15 -46 -29 .17 24 20 | -2695 226 2970 8997
gfz n/a| 0 0 0 -9 -14 -39 -.03 26 17 | 0 2383 2976 7182
grg n/a| 1 1 0 -23 42 -169 -.78 28 23 | 23 2495 2970 6689
iac n/a| -2 3 0 -33 14 179 .07 32 29 | 2162 1138 2974 7209
mcc n/a| 16 -3 -23 113 -3 -165 -.25 269 269 | --- --- --- ---
Table 2.2081.4 GPS week: 2081 Day: 4 MJD: 58815
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 19 12 4 .21 21 18 | 27042 -3483 3143 7156
cof n/a| 0 1 4 41 -2 13 .11 25 20 | 27040 -3503 3148 7179
emx n/a| 1 -2 -11 -8 -30 125 .25 25 25 | 173 -2265 2981 7077
esx n/a| 2 0 0 37 -14 8 .21 26 21 | 12599 -4148 3145 9441
gfz n/a| -2 -1 0 -31 -1 -20 -.10 31 22 | 0 -2737 3154 7301
grg n/a| 1 -1 4 -14 10 -144 -.50 30 24 | 1441 -2733 3149 6463
iac n/a| -1 0 1 15 47 -18 -.04 30 25 | 3249 -1744 2992 7075
mcc n/a| 18 -7 -27 88 130 1406 -.58 231 231 | --- --- --- ---
Table 2.2081.5 GPS week: 2081 Day: 5 MJD: 58816
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 1 70 30 -8 .31 23 20 | 12614 -1883 2909 7669
cof n/a| 0 -1 3 45 -3 -15 .17 26 22 | 12586 -1867 2903 7665
emx n/a| 1 0 -10 1 21 69 .19 27 27 | -22120 -854 2920 7793
esx n/a| -2 2 0 -19 -42 10 -.00 26 21 | -5987 -1333 2919 9665
gfz n/a| -3 0 5 -38 -26 -27 -.29 36 21 | 0 -1627 2908 7515
grg n/a| 1 -1 -3 -46 -4 -65 -.26 24 19 | -10484 -1960 2930 6784
iac n/a| 0 0 4 18 31 54 .02 27 25 | -10386 -619 2915 7927
mcc n/a| -6 -7 -7 162 193 528 .17 276 276 | --- --- --- ---
Table 2.2081.6 GPS week: 2081 Day: 6 MJD: 58817
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 24 9 34 .27 26 22 | 11790 235 3123 7938
cof n/a| -1 0 4 13 9 70 .07 28 24 | 11773 220 3126 7952
emx n/a| 2 -1 -14 20 4 109 .23 26 27 | -10259 650 3133 8135
esx n/a| 0 0 1 -2 -19 24 .09 22 17 | -18597 -2337 3127 10135
gfz n/a| 0 2 3 -12 -45 -17 -.18 33 24 | 0 -151 3119 7811
grg n/a| 1 2 4 -55 15 -32 -.31 23 19 | -11292 81 3124 7234
iac n/a| 0 -2 0 4 46 -105 -.09 23 22 | -9781 -120 3131 8084
mcc n/a| -3 -6 1 122 217 756 -.21 220 220 | --- --- --- ---
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 3.2081.0 GPS week: 2081 Day: 0 MJD: 58811
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 759 22 20 44 26 28 40 21 --- 14 | 48 47 55 51 56 52 42 --- 44
R02 | 1335 8 14 6 8 13 14 16 327 5 | 35 37 37 33 33 37 42 353 34
R03M | 1468 6 9 10 11 18 9 16 123 5 | 38 37 40 42 38 40 40 116 38
R05 | 609 27 25 32 29 21 15 17 --- 11 | 31 37 40 41 37 30 25 --- 28
R07 | 506 11 11 9 18 16 22 17 391 7 | 42 42 41 45 42 50 31 283 39
R08M | 2157 22 9 11 24 16 18 21 --- 8 | 40 46 45 60 54 49 39 --- 46
R09M | 4422 14 16 17 16 19 17 16 --- 7 | 87 87 89 84 81 83 97 --- 86
R11E | 729 17 21 14 7 14 15 14 113 6 | 65 68 53 58 59 51 51 173 55
R12E | 504 27 33 24 12 23 14 21 --- 9 | 101 104 74 81 95 81 74 --- 83
R13E | 3689 14 15 15 21 18 29 13 --- 8 | 60 61 51 70 56 52 63 --- 57
R14E | 1333 16 13 18 20 17 11 14 --- 7 | 68 63 56 70 74 59 60 --- 63
R15E | 1269 21 22 19 8 18 10 31 --- 8 | 85 82 67 72 83 73 79 --- 75
R16E | 367 17 28 24 26 35 31 19 --- 11 | 70 74 70 71 64 72 73 --- 66
R17E | 1522 18 13 22 20 31 16 24 --- 9 | 139 140 136 134 142 131 131 --- 134
R18E | 829 13 13 18 17 11 9 13 --- 6 | 70 68 68 69 71 71 77 --- 70
R19E | 1296 39 47 50 38 90 56 64 --- 25 | 73 81 61 64 116 60 59 --- 56
R20E | 866 22 33 40 18 33 33 30 --- 13 | 188 187 187 191 184 177 176 --- 183
R21E | 838 17 24 22 15 28 21 25 91 9 | 59 61 52 53 67 57 54 111 55
XR22E | ---- 46 42 --- --- 64 --- --- --- 54 | 218 218 --- --- 245 --- --- --- 224
R23E | 673 23 31 16 18 25 32 15 --- 10 | 99 99 101 102 103 112 100 --- 101
XR26E | ---- 18 36 --- --- --- --- 18 --- 18 | 78 71 --- --- --- --- 70 --- 74
------+---------------------------------------------------+-----------------------------------------------
RMS | 1683 20 23 25 20 30 25 24 243 |T 80 81 69 73 85 70 69 207 76
WRMS | 1683 18 19 22 16 22 19 21 243 |NE 36 38 39 39 37 39 32 318 33
MEDI | 866 18 21 18 18 19 17 17 123 |MD 70 68 56 69 67 59 60 173 63
Table 3.2081.1 GPS week: 2081 Day: 1 MJD: 58812
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 1269 33 44 47 36 29 29 26 --- 15 | 29 52 35 56 53 51 34 --- 37
R02 | 1541 14 18 10 14 14 20 14 323 6 | 17 21 17 27 21 22 24 340 16
R03M | 626 14 21 7 8 21 19 9 104 6 | 23 29 19 29 21 29 20 89 20
R05 | 940 15 23 18 12 20 27 22 --- 8 | 27 32 19 30 40 21 17 --- 20
R07 | 822 16 13 17 17 14 10 12 408 6 | 22 24 25 27 23 21 15 403 19
R08M | 529 23 26 19 29 26 16 28 --- 10 | 24 38 34 52 52 42 25 --- 34
R09M | 3136 14 18 17 10 18 14 17 --- 6 | 63 65 59 67 65 60 70 --- 63
R11E | 500 18 12 13 11 10 18 11 438 6 | 45 40 36 42 38 35 33 182 37
R12E | 368 23 19 22 10 12 20 20 --- 8 | 78 73 63 68 67 73 63 --- 67
R13E | 3636 20 20 17 21 20 18 11 --- 8 | 38 41 39 52 39 52 44 --- 42
R14E | 1297 16 15 22 12 22 19 13 --- 8 | 50 51 46 55 61 60 48 --- 51
R15E | 2192 25 17 21 15 18 23 23 --- 9 | 72 73 65 64 67 73 65 --- 66
R16E | 497 14 28 16 27 40 27 24 --- 11 | 44 50 41 49 43 45 45 --- 39
R17E | 1620 24 20 24 22 22 24 33 --- 11 | 122 122 121 121 119 116 107 --- 117
R18E | 1540 17 20 18 11 17 14 18 --- 7 | 62 61 62 66 69 69 64 --- 64
R19E | 2741 53 62 51 45 93 43 54 --- 25 | 77 87 44 47 109 60 40 --- 49
R20E | 555 24 28 27 12 30 32 23 --- 11 | 157 156 156 158 156 158 163 --- 157
R21E | 1100 25 26 24 14 26 22 29 196 10 | 65 69 57 60 72 63 58 153 60
XR22E | ---- 10 16 --- --- 14 --- --- --- 12 | 221 222 --- --- 223 --- --- --- 222
R23E | 608 21 30 20 24 28 25 16 --- 10 | 85 86 87 91 87 87 89 --- 86
XR26E | ---- 18 49 --- --- --- --- 17 --- 17 | 63 85 --- --- --- --- 62 --- 61
------+---------------------------------------------------+-----------------------------------------------
RMS | 1635 23 27 24 21 31 23 24 320 |T 65 70 53 61 71 59 54 233 63
WRMS | 1635 19 20 24 16 22 21 22 320 |NE 22 25 20 28 28 21 18 371 18
MEDI | 1100 18 20 19 14 20 20 18 323 |MD 62 61 44 55 61 60 45 182 51
Table 3.2081.2 GPS week: 2081 Day: 2 MJD: 58813
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 675 51 54 69 53 62 34 38 --- 23 | 44 91 54 82 90 78 42 --- 55
R02 | 926 17 13 10 15 20 22 12 226 7 | 26 29 34 38 30 43 32 218 30
R03M | 612 8 15 13 16 17 25 18 117 7 | 28 30 32 24 24 34 25 61 23
R05 | 778 26 21 22 21 39 19 33 --- 12 | 33 34 33 39 54 33 30 --- 30
R07 | 1680 12 21 13 12 18 15 18 297 6 | 33 41 31 37 47 47 23 220 33
R08M | 1002 13 15 14 10 13 10 13 --- 5 | 32 32 37 31 31 37 26 --- 30
R09M | 2690 13 9 13 11 15 16 16 --- 6 | 53 53 56 50 55 48 62 --- 52
R11E | 858 17 19 15 11 11 15 21 407 7 | 54 56 49 54 51 53 45 117 49
R12E | 539 16 18 24 14 19 25 26 --- 9 | 69 66 57 57 65 76 55 --- 62
R13E | 2711 12 19 15 22 16 14 18 --- 7 | 41 38 42 58 44 42 60 --- 46
R14E | 1037 11 16 26 17 16 17 19 --- 8 | 53 61 40 59 53 51 47 --- 49
R15E | 2479 25 33 21 19 17 22 31 --- 10 | 72 80 49 49 64 68 55 --- 58
R16E | 913 18 28 21 24 26 30 27 --- 11 | 62 62 58 71 62 70 70 --- 61
R17E | 1521 16 20 24 10 17 19 40 --- 9 | 89 90 91 88 94 97 86 --- 89
R18E | 1712 13 17 21 19 19 26 30 --- 9 | 86 85 80 80 82 96 102 --- 85
R19E | 3386 58 50 52 51 63 39 52 --- 23 | 71 75 62 61 84 63 44 --- 52
R20E | 921 20 31 33 15 52 27 23 --- 13 | 119 121 129 127 133 132 116 --- 123
R21E | 1410 16 26 22 18 35 21 48 153 12 | 71 79 66 73 86 74 57 85 68
XR22E | ---- 12 17 --- --- 17 --- --- --- 15 | 183 185 --- --- 180 --- --- --- 182
R23E | 427 14 21 20 34 38 40 68 --- 16 | 101 103 103 109 104 125 73 --- 100
XR26E | ---- 17 68 --- --- --- --- 31 --- 23 | 47 83 --- --- --- --- 86 --- 58
------+---------------------------------------------------+-----------------------------------------------
RMS | 1614 24 26 27 24 31 24 32 262 |T 65 71 58 62 71 66 56 140 63
WRMS | 1614 16 18 27 20 20 23 32 262 |NE 30 34 32 38 43 41 28 219 31
MEDI | 1002 16 20 21 17 18 22 26 226 |MD 54 66 54 58 62 63 55 117 55
Table 3.2081.3 GPS week: 2081 Day: 3 MJD: 58814
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 637 41 54 72 51 52 39 31 --- 22 | 32 78 41 76 78 53 38 --- 48
R02 | 1140 10 8 11 17 21 14 22 379 7 | 27 30 33 36 42 34 38 352 30
R03M | 532 11 14 12 17 11 16 25 144 7 | 27 32 29 39 36 34 25 63 29
R05 | 470 24 30 35 28 36 17 30 --- 13 | 26 46 34 56 58 46 38 --- 37
R07 | 619 9 20 11 15 15 17 19 214 6 | 33 39 29 35 41 37 28 109 30
R08M | 2604 13 11 16 22 13 17 29 --- 8 | 34 31 43 35 32 37 34 --- 32
R09M | 2523 16 15 12 7 17 27 19 --- 7 | 50 50 54 52 54 58 60 --- 52
R11E | 1400 13 12 20 9 14 20 21 365 7 | 65 64 53 60 60 56 50 82 56
R12E | 708 19 16 30 20 18 22 24 --- 10 | 89 87 74 84 92 89 66 --- 82
R13E | 1474 20 19 20 19 12 19 21 --- 8 | 54 58 57 68 55 68 62 --- 59
R14E | 1292 16 12 20 14 17 16 16 --- 7 | 66 64 55 66 62 57 52 --- 59
R15E | 1660 28 25 24 14 14 18 30 --- 10 | 71 70 59 51 62 54 42 --- 55
R16E | 522 21 28 25 16 35 44 44 --- 14 | 72 80 85 93 84 101 72 --- 80
R17E | 2818 15 19 25 17 18 33 35 --- 10 | 70 73 69 66 70 72 60 --- 65
R18E | 948 14 16 23 14 17 29 18 --- 8 | 73 74 69 81 79 83 80 --- 75
R19E | 3562 46 65 46 52 45 53 45 --- 21 | 71 92 66 59 85 61 63 --- 54
R20E | 1639 25 28 36 14 25 19 61 --- 14 | 98 107 109 98 96 98 104 --- 96
R21E | 458 21 18 26 24 31 30 44 132 13 | 82 85 81 83 99 92 68 87 81
XR22E |10190 16 17 --- --- 16 30 --- --- 14 | 196 197 --- --- 202 46 --- --- 199
R23E | 528 20 17 18 27 34 34 34 --- 12 | 91 99 97 98 93 108 73 --- 92
XR26E | ---- 39 54 --- --- --- --- 66 --- 50 | 64 78 --- --- --- --- 76 --- 56
------+---------------------------------------------------+-----------------------------------------------
RMS | 1618 22 27 29 24 26 28 32 269 |T 66 73 59 65 74 64 56 138 65
WRMS | 1618 17 17 28 20 17 23 29 269 |NE 28 38 32 42 47 39 34 230 32
MEDI | 1140 19 18 23 17 17 20 29 214 |MD 66 73 57 66 62 57 60 87 56
Table 3.2081.4 GPS week: 2081 Day: 4 MJD: 58815
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 1822 30 27 50 52 39 35 22 --- 17 | 43 49 54 63 70 59 53 --- 51
R02 | 576 10 12 10 20 19 8 10 --- 6 | 30 31 30 37 33 29 31 --- 28
R03M | 808 10 18 11 19 17 24 11 202 7 | 32 40 27 45 32 32 31 83 31
R05 | 527 21 14 18 26 37 17 24 --- 11 | 29 39 43 53 56 39 41 --- 37
R07 | 662 10 15 13 9 17 11 20 195 6 | 34 39 28 41 39 38 33 167 33
R08M | 2902 17 14 12 24 15 15 32 --- 9 | 35 44 37 56 48 40 27 --- 38
R09M | 2753 14 9 10 13 25 22 24 --- 8 | 73 72 75 72 76 75 80 --- 73
R11E | 2219 11 11 18 9 12 26 25 331 7 | 66 63 64 63 68 71 52 131 62
R12E | 1090 24 37 32 11 17 32 28 --- 11 | 131 141 114 126 123 146 115 --- 124
R13E | 2879 16 13 17 21 18 22 19 --- 8 | 61 61 60 71 75 71 68 --- 65
R14E | 639 9 15 22 14 15 35 19 --- 9 | 66 69 59 63 65 91 61 --- 65
R15E | 743 22 20 24 8 17 28 27 --- 9 | 71 70 53 58 57 77 52 --- 59
R16E | 745 28 52 31 25 49 37 55 --- 16 | 132 136 145 142 132 144 133 --- 134
R17E | 2700 22 30 20 12 19 13 26 --- 8 | 90 91 89 87 93 92 80 --- 87
R18E | 765 13 14 18 23 19 29 11 --- 8 | 73 74 71 84 72 85 77 --- 75
R19E | 2913 47 46 53 63 87 69 71 --- 28 | 80 80 49 64 106 87 62 --- 57
R20E | 2013 22 23 27 17 26 35 28 --- 11 | 117 114 118 116 118 128 119 --- 117
R21E | 682 17 13 24 25 22 30 24 159 10 | 71 72 59 59 73 83 64 133 66
XR22E | 1738 15 23 --- 23 19 29 --- --- 12 | 174 174 --- 33 163 42 --- --- 170
R23E | 824 18 29 19 30 26 18 19 --- 10 | 84 81 83 93 82 98 86 --- 86
XR26E | ---- 11 40 --- --- --- --- 15 --- 13 | 70 57 --- --- --- --- 78 --- 72
------+---------------------------------------------------+-----------------------------------------------
RMS | 1755 21 25 25 26 31 30 30 231 |T 74 76 66 71 79 76 67 128 72
WRMS | 1755 18 20 25 21 22 24 25 231 |NE 31 36 33 43 42 35 35 167 32
MEDI | 824 17 18 19 20 19 26 24 195 |MD 71 70 59 63 72 75 62 131 65
Table 3.2081.5 GPS week: 2081 Day: 5 MJD: 58816
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 1344 30 27 43 41 21 40 16 --- 15 | 24 30 33 40 36 27 23 --- 21
R02 | 721 12 15 19 18 20 8 11 417 6 | 18 24 21 38 35 26 19 340 22
R03M | 716 11 15 14 12 21 11 11 102 6 | 16 17 20 28 33 21 26 49 19
R05 | 649 13 24 20 32 28 20 12 --- 9 | 17 34 29 44 49 20 25 --- 24
R07 | 1939 14 18 19 18 16 18 11 165 7 | 19 22 21 25 26 17 18 123 15
R08M | 2421 14 12 10 13 21 21 24 --- 8 | 18 20 21 27 22 19 18 --- 17
R09M | 3891 12 14 13 13 30 17 24 --- 8 | 73 76 72 75 73 80 86 --- 75
R11E | 2854 16 17 20 12 17 28 45 393 11 | 121 124 116 125 121 124 109 196 117
R12E | 1299 42 39 33 16 39 44 25 --- 15 | 182 183 168 169 188 176 165 --- 172
R13E | 3312 10 9 20 17 21 18 12 --- 7 | 87 85 83 93 92 85 93 --- 87
R14E | 903 18 18 27 19 20 20 30 --- 10 | 176 180 182 179 179 183 173 --- 177
R15E | 699 19 28 27 16 36 23 30 --- 11 | 99 106 93 96 115 100 80 --- 95
R16E | 809 22 33 31 32 32 21 22 --- 12 | 145 149 144 157 146 150 147 --- 147
R17E | 2045 22 25 23 17 23 18 30 --- 10 | 74 77 74 73 80 76 71 --- 73
R18E | 1220 12 13 18 22 16 13 23 --- 8 | 57 59 57 62 62 59 58 --- 58
R19E | 3511 52 58 55 62 117 39 64 --- 29 | 68 78 26 59 116 59 30 --- 43
R20E | 1936 23 30 36 31 31 40 28 --- 14 | 116 124 112 121 114 106 114 --- 111
R21E | 839 22 27 20 15 17 11 18 125 8 | 42 46 31 31 40 28 33 124 32
R22E | 1884 24 18 28 22 16 20 24 --- 10 | 157 157 22 24 154 19 19 --- 155
R23E | 2421 19 23 22 27 32 10 19 --- 10 | 55 54 57 56 57 55 47 --- 52
XR26E | ---- 18 32 --- --- --- --- 19 --- 19 | 93 104 --- --- --- --- 98 --- 93
------+---------------------------------------------------+-----------------------------------------------
RMS | 2033 23 26 27 26 36 24 27 276 |T 78 83 69 76 86 71 69 166 76
WRMS | 2033 20 22 27 21 21 19 25 276 |NE 18 26 23 35 36 21 20 231 20
MEDI | 1344 18 23 20 18 21 20 23 165 |MD 73 77 57 59 73 59 58 124 73
Table 3.2081.6 GPS week: 2081 Day: 6 MJD: 58817
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
------+---------------------------------------------------+-----------------------------------------------
R01M | 563 41 39 48 37 36 34 17 --- 16 | 43 56 39 56 71 54 41 --- 48
R02 | 1456 12 13 9 8 13 14 16 166 5 | 27 28 30 31 34 34 30 114 28
R03M | 2225 12 18 17 16 22 7 21 84 7 | 25 30 26 36 42 29 24 89 26
R05 | 938 19 35 10 16 26 13 19 --- 7 | 22 52 28 43 51 39 21 --- 31
R07 | 1862 16 12 16 13 31 28 8 211 9 | 29 32 27 34 48 41 27 241 28
R08M | 875 15 27 9 14 9 28 28 --- 8 | 34 40 33 32 29 45 24 --- 30
R09M | 5023 14 12 16 8 16 13 22 --- 6 | 103 105 105 103 100 102 116 --- 104
R11E | 2677 16 16 20 11 14 11 20 374 7 | 149 150 158 151 153 159 153 191 153
R12E | 1888 31 17 29 22 29 15 22 --- 11 | 207 209 191 202 206 203 183 --- 198
R13E | 2502 11 14 22 10 23 11 10 --- 6 | 71 74 67 76 83 76 71 --- 72
R14E | 1689 15 11 29 16 24 18 22 --- 9 | 130 134 125 144 140 134 130 --- 133
R15E | 700 12 22 27 13 23 31 28 --- 10 | 107 111 107 105 108 114 110 --- 106
R16E | 749 24 22 31 29 45 36 26 --- 14 | 122 123 122 120 128 128 127 --- 122
R17E | 2662 22 20 20 16 23 13 24 --- 8 | 83 83 81 78 85 83 79 --- 80
R18E | 1807 8 8 20 16 19 10 14 --- 6 | 75 75 69 80 78 77 78 --- 75
R19E | 1140 73 84 54 52 101 44 41 --- 27 | 67 76 27 66 90 53 47 --- 41
R20E | 2648 27 30 41 35 32 42 37 --- 16 | 149 155 143 154 147 145 145 --- 145
R21E | 826 26 23 18 10 16 10 22 150 8 | 71 74 55 59 69 61 54 99 60
R22E | 2230 25 25 19 13 14 12 11 --- 7 | 181 184 17 20 177 26 17 --- 178
R23E | 3729 21 17 15 23 30 12 23 --- 9 | 71 72 73 83 70 79 71 --- 73
XR26E | ---- 23 40 --- --- --- --- 19 --- 21 | 111 117 --- --- --- --- 103 --- 107
------+---------------------------------------------------+-----------------------------------------------
RMS | 2200 26 28 26 22 33 23 23 219 |T 89 94 76 83 95 84 78 146 87
WRMS | 2200 22 24 27 17 24 19 22 219 |NE 26 37 28 36 44 38 26 177 29
MEDI | 1807 19 20 20 16 23 13 22 166 |MD 75 76 67 76 83 76 71 114 75
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