[IGSREPORT-25712] Wk 1983 IGLOS Final Orbits
acc
acc at igs.org
Thu Jan 25 20:01:57 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1983 (Jan 07, 2018 - Jan 13, 2018)
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 2.1983.
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:
igl1983[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1983 in the SP3 format.
igl19837.sum Combination Report for GPS Week 1983.
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 | -5.3 ns
1 | -5.2 ns
2 | -4.5 ns
3 | -5.8 ns
4 | -5.5 ns
5 | -8.7 ns
6 | -6.8 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 1.1983, 1a.1983).
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 2.1983.0-6)
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 3.1983.0-6).
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 1983 summary. (Jan 07, 2018 - Jan 13, 2018)
Table 1.1983.a GPS week : 1983 MJD: 58125.0-58131.0
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 1 14 14 36 .10 30 30 | -11789 363 3188 9934
| 0 1 2 19 13 26 .02 | 871 1201
cof n/a| -1 0 0 12 10 44 .12 33 31 | -11796 373 3191 9933
| 0 1 2 12 20 29 .05 | 863 1199
emx n/a| 1 0 -7 11 27 -8 .06 21 21 | -5670 658 3176 9421
| 1 1 2 12 14 37 .03 | 10189 507
esx n/a| 0 0 1 -28 -1 -4 .12 17 15 | -7974 1083 3179 11951
| 1 0 1 17 14 23 .03 | 12496 2006
gfz n/a| -2 0 -5 -15 20 38 .05 23 21 | 0 864 3162 9612
| 1 1 1 20 26 21 .04 | 0 1392
grg n/a| 0 0 4 -42 -28 -75 -.38 27 25 | -6390 681 3228 8828
| 1 1 5 20 10 38 .05 | 939 1284
iac n/a| 1 0 4 68 -33 22 -.09 21 21 | -4819 -197 3181 9253
| 1 1 3 35 28 29 .03 | 1323 491
mcc n/a| 0 -1 18 136 51 798 -.36 179 179 | --- --- --- ---
| 4 9 7 65 119 509 .33 | --- ---
Table 1.1983.b GPS week : 1983 MJD: 58125.0-58131.0
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 | 11 9 9 7 8 9 9 |
R02 | 8 7 6 7 6 7 8 |
R03 | 8 8 7 5 6 7 10 |
R04 | 7 7 6 7 7 7 8 |
R05 | 15 13 20 15 14 16 15 |
R06 | 9 11 10 9 12 10 10 |
R07 | 7 8 7 10 10 9 7 |
R08 | 7 7 8 11 8 9 9 |
R09 | 7 7 6 8 8 7 8 |
R10 | 8 9 7 8 7 7 7 |
R11 | 8 6 7 8 6 7 8 |
R13 | 9 10 8 10 10 8 9 |
R14 | 9 8 7 8 11 10 11 |
R15 | 8 9 11 9 11 11 11 |
R16 | 12 10 11 15 13 13 12 |
R17 | 9 10 9 11 12 12 12 |
R18 | 7 6 8 8 7 8 10 |
R19 | 15 15 16 16 17 14 15 |
R20 | 13 12 12 12 12 14 17 |
R21 | 11 12 11 11 11 11 10 |
R22 | 10 11 12 11 12 13 12 |
R23 | 11 10 11 9 10 8 9 |
R24 | 13 18 16 16 14 12 13 |
R26 | 14 25 26 20 25 25 0 |
Table 1.1983.c GPS week : 1983 MJD: 58125.0-58131.0
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 1983 0 | -49 -29 61 1115 -572 -4694 84.2 2007 2007 | -5310 0
brd 1983 1 | -19 -27 140 1984 299 -5330 86.8 1891 1891 | -5206 0
brd 1983 2 | -14 -44 132 941 -614 -2959 83.7 1684 1684 | -4539 0
brd 1983 3 | 44 -22 115 -1419 -1446 -1655 84.1 1570 1570 | -5848 0
brd 1983 4 | 5 57 118 -973 109 -2543 84.8 1642 1642 | -5532 0
brd 1983 5 | -20 -28 135 673 333 -3548 84.0 1546 1546 | -8719 0
brd 1983 6 | -2 -34 128 1509 -385 -3969 83.6 1541 1541 | -6763 0
-------------+------------------------------------------------------------+----------------
brd 1983 mean| -8 -18 118 547 -325 -3528 84.4 1697 1697 | -5988 0
brd 1983 sdev| 29 34 26 1268 634 1265 1.1 182 182 | 1381 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 2.1983.0 GPS week: 1983 Day: 0 MJD: 58125
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 2 10 -2 17 .10 27 30 | -13332 339 2926 10055
cof n/a| 0 0 0 14 4 11 .14 32 33 | -13319 302 2926 10057
emx n/a| 0 -1 -9 25 16 -17 .12 22 22 | 4281 362 2905 9489
esx n/a| 1 0 1 -34 -8 -7 .10 16 14 | -6108 1731 2911 11721
gfz n/a| -2 0 -7 22 31 55 .03 22 18 | 0 985 2897 9727
grg n/a| -1 0 13 -40 -13 -62 -.30 24 25 | -5727 825 2963 8661
iac n/a| 1 1 -1 21 -28 42 -.04 22 20 | -3836 -101 2911 9401
mcc n/a| 4 3 26 62 -39 217 .10 136 136 | --- --- --- ---
Table 2.1983.1 GPS week: 1983 Day: 1 MJD: 58126
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 2 3 33 12 -3 .13 30 32 | -12408 391 3129 9559
cof n/a| -1 1 2 21 -31 24 .17 33 34 | -12422 410 3126 9559
emx n/a| 1 -2 -9 0 18 31 .03 21 21 | -2602 361 3121 9281
esx n/a| 0 0 1 -49 -30 13 .16 16 16 | 901 1082 3116 11592
gfz n/a| -2 -2 -4 -28 12 50 .02 22 22 | 0 856 3119 9305
grg n/a| 0 0 4 -50 -40 -92 -.45 24 26 | -5542 711 3174 8690
iac n/a| 1 1 2 118 14 22 -.10 19 19 | -3584 -308 3108 8827
mcc n/a| 6 8 16 144 -107 221 -.25 193 193 | --- --- --- ---
Table 2.1983.2 GPS week: 1983 Day: 2 MJD: 58127
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 4 -2 -1 46 .10 30 28 | -12179 1630 3409 10223
cof n/a| -2 0 3 -3 20 84 .10 33 29 | -12184 1636 3413 10226
emx n/a| -1 0 -8 3 56 48 .04 21 21 | 4294 612 3394 9371
esx n/a| 2 0 2 -14 0 -34 .16 18 16 | -12473 2160 3399 11714
gfz n/a| 0 -1 -4 -27 66 20 .05 24 20 | 0 2117 3400 9855
grg n/a| 0 -1 0 -61 -34 -125 -.40 27 24 | -5479 1535 3406 9370
iac n/a| 1 1 4 90 -78 52 -.08 21 21 | -4029 -34 3425 9489
mcc n/a| -4 -8 11 83 -2 396 -.36 274 274 | --- --- --- ---
Table 2.1983.3 GPS week: 1983 Day: 3 MJD: 58128
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 1 29 75 .09 30 28 | -11230 418 3122 9117
cof n/a| -1 -1 1 28 34 70 .04 34 31 | -11232 418 3127 9112
emx n/a| 1 -1 -3 -1 27 -24 .06 18 18 | -4409 770 3097 8577
esx n/a| 0 0 0 -34 3 1 .08 17 16 | 2698 2625 3110 10974
gfz n/a| -4 0 -7 -38 -21 21 .13 23 25 | 0 1118 3046 8852
grg n/a| -1 1 6 -11 -28 -62 -.38 31 27 | -6388 1214 3117 8075
iac n/a| 0 0 2 74 -46 -20 -.14 24 23 | -4097 -527 3121 8427
mcc n/a| -1 12 25 82 245 1269 -.85 149 149 | --- --- --- ---
Table 2.1983.4 GPS week: 1983 Day: 4 MJD: 58129
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 1 -9 12 60 .07 28 28 | -11105 1985 3119 10632
cof n/a| -1 0 1 3 12 27 .17 32 29 | -11120 2015 3120 10630
emx n/a| 2 0 -5 14 30 -1 .07 19 19 | -18404 1751 3105 10294
esx n/a| 1 0 3 -1 9 -20 .11 20 15 | -27352 3326 3107 13438
gfz n/a| -1 -1 -5 -26 7 6 .01 22 20 | 0 2786 3100 10340
grg n/a| -4 0 -1 -29 -26 -59 -.31 29 25 | -6884 2473 3228 9187
iac n/a| 1 1 6 86 -46 24 -.09 21 22 | -4860 689 3098 9864
mcc n/a| -7 -9 14 184 63 915 -.64 164 164 | --- --- --- ---
Table 2.1983.5 GPS week: 1983 Day: 5 MJD: 58130
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 -2 33 17 33 .13 30 30 | -11106 -1319 3157 9376
cof n/a| 0 -1 -4 21 18 22 .05 31 30 | -11125 -1292 3162 9377
emx n/a| 1 0 -9 28 12 -45 .03 20 20 | -21048 340 3152 8813
esx n/a| 0 0 -1 -43 3 34 .15 18 15 | 6337 -1595 3157 11822
gfz n/a| 0 0 -6 -1 30 62 .03 25 21 | 0 -789 3137 9015
grg n/a| 1 -1 8 -32 -17 -113 -.39 26 23 | -8128 -1121 3188 8003
iac n/a| 0 0 8 23 -36 49 -.09 21 22 | -6521 -910 3152 8770
mcc n/a| -1 -10 8 148 156 1393 -.03 164 164 | --- --- --- ---
Table 2.1983.6 GPS week: 1983 Day: 6 MJD: 58131
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 0 36 34 28 .09 33 32 | -11163 -897 3460 10576
cof n/a| 0 0 -2 0 14 69 .14 37 34 | -11176 -877 3463 10570
emx n/a| 1 2 -5 8 30 -52 .06 23 23 | -1802 414 3464 10126
esx n/a| -1 0 2 -18 13 -17 .09 17 15 | -19821 -1744 3458 12397
gfz n/a| -1 0 -3 -8 15 53 .08 23 20 | 0 -1023 3441 10191
grg n/a| 0 1 -1 -70 -41 -9 -.41 29 28 | -6588 -869 3524 9814
iac n/a| 3 -1 7 61 -15 -16 -.08 21 21 | -6811 -191 3457 9994
mcc n/a| -2 -6 24 247 47 1173 -.46 175 175 | --- --- --- ---
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 3.1983.0 GPS week: 1983 Day: 0 MJD: 58125
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 | 1007 22 36 30 32 15 19 13 --- 11 | 51 64 56 51 58 43 41 --- 47
R02 | 901 15 15 16 13 16 30 16 138 8 | 43 46 46 38 47 36 29 63 38
R03 | 1230 22 24 21 6 14 25 16 92 7 | 63 65 65 53 54 48 52 50 54
R04 | 827 11 18 17 9 13 16 24 --- 7 | 69 70 65 62 60 66 54 --- 61
R05 | 1418 31 55 30 23 23 48 45 --- 15 | 45 54 55 50 43 37 38 --- 42
R06 | 1544 26 32 21 17 23 16 8 --- 8 | 42 44 44 60 57 46 48 --- 49
R07 | 989 10 7 14 10 16 23 14 214 6 | 66 65 69 61 64 45 55 141 59
R08 | 1806 13 13 11 7 16 25 23 --- 7 | 51 50 55 54 52 38 58 --- 51
R09E | 4175 13 18 17 8 17 23 16 --- 7 | 36 38 26 39 45 51 39 --- 37
R10E | 1152 13 15 25 14 15 21 16 --- 8 | 57 60 58 58 50 53 60 --- 55
R11E | 1688 12 11 11 16 17 26 20 124 8 | 40 39 39 45 39 35 44 119 38
R13E | 4681 17 22 19 19 19 15 23 --- 8 | 159 160 157 171 170 160 152 --- 162
XR14E | 1947 14 18 18 18 21 --- 17 --- 9 | 40 40 40 47 46 --- 43 --- 41
R15E | 3110 19 12 15 15 25 16 18 --- 8 | 50 48 45 50 47 46 46 --- 45
R16E | 2606 20 24 30 21 27 36 22 --- 11 | 55 64 58 58 68 57 59 --- 56
R17 | 1430 40 44 15 5 22 18 16 --- 9 | 77 79 47 49 36 47 42 --- 47
R18 | 1087 13 16 9 13 16 21 11 --- 6 | 60 62 44 61 45 47 54 --- 51
R19 | 2291 63 59 22 15 43 20 23 --- 14 | 96 97 59 62 60 64 50 --- 60
R20 | 913 42 60 29 18 29 28 22 --- 12 | 87 97 52 66 50 63 42 --- 56
R21 | 725 40 42 23 9 27 22 20 59 10 | 89 88 64 65 43 58 53 82 60
R22 | 844 39 42 19 10 23 18 27 --- 10 | 89 87 60 60 41 52 43 --- 55
R23 | 1224 21 30 26 27 17 21 19 --- 10 | 49 46 47 75 50 48 56 --- 54
R24 | 1979 24 21 31 23 29 24 34 --- 12 | 64 62 60 80 44 54 54 --- 61
XR26 | ---- 15 83 --- --- --- --- 12 --- 14 | 26 78 --- --- --- --- 48 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 2007 27 32 22 16 22 24 22 136 |T 62 66 57 61 55 54 52 91 54
WRMS | 2007 30 33 22 14 18 25 20 136 |NE 62 67 55 59 50 49 48 84 52
MEDI | 1418 19 22 19 15 19 21 18 124 |MD 55 62 55 58 50 48 48 82 51
Table 3.1983.1 GPS week: 1983 Day: 1 MJD: 58126
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 | 1014 18 17 27 12 16 14 24 --- 8 | 35 44 53 47 49 49 30 --- 42
R02 | 822 15 22 17 7 22 18 8 223 6 | 36 38 37 37 42 28 36 79 33
R03 | 1369 14 16 13 15 13 26 22 121 8 | 53 52 48 50 52 38 39 28 45
R04 | 1127 13 13 12 15 8 28 12 --- 7 | 50 51 45 44 42 59 45 --- 45
R05 | 887 44 55 21 20 30 36 32 --- 13 | 33 35 43 47 31 51 30 --- 36
R06 | 2594 26 27 21 28 20 38 10 --- 11 | 37 37 32 53 47 38 45 --- 40
R07 | 699 19 19 22 17 11 22 11 317 7 | 54 52 53 46 41 31 38 173 42
R08 | 2480 19 18 17 6 12 29 12 --- 7 | 40 41 40 32 33 23 32 --- 31
R09E | 4586 20 20 14 7 16 19 21 --- 7 | 20 23 15 23 24 31 27 --- 19
R10E | 952 20 21 17 23 21 13 19 --- 8 | 50 52 42 63 52 47 48 --- 49
R11E | 2205 11 13 15 12 16 13 14 105 6 | 54 55 50 54 53 49 46 108 50
R13E | 2889 13 32 28 19 17 16 31 --- 10 | 109 118 115 107 112 118 89 --- 106
XR14E | 2393 16 12 17 13 18 --- 18 --- 8 | 44 42 46 49 49 --- 47 --- 45
R15E | 2706 21 23 17 13 27 21 16 --- 8 | 39 44 36 44 49 38 43 --- 39
R16E | 1953 27 39 27 15 14 21 21 --- 9 | 62 61 63 62 64 60 72 --- 62
R17 | 877 44 46 20 8 30 22 13 --- 10 | 53 55 41 35 31 32 34 --- 33
R18 | 611 18 17 13 11 18 13 12 --- 6 | 40 40 28 36 34 32 33 --- 32
R19 | 1866 69 74 28 20 33 24 23 --- 14 | 66 70 46 43 45 53 42 --- 45
R20 | 1267 45 38 27 20 31 29 16 --- 12 | 58 52 32 45 38 33 29 --- 35
R21 | 958 43 44 26 16 32 29 16 103 11 | 54 59 49 53 33 44 43 46 43
R22 | 1364 40 35 20 11 31 25 20 --- 10 | 51 47 40 38 25 40 32 --- 34
R23 | 873 17 13 21 26 19 22 19 --- 9 | 36 42 31 53 52 38 31 --- 38
XR24 | 740 33 48 32 39 --- 38 32 --- 17 | 48 65 38 70 --- 45 40 --- 46
XR26 | ---- 32 87 --- --- --- --- 19 --- 24 | 36 67 --- --- --- --- 39 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1890 30 33 21 16 22 24 19 193 |T 48 51 44 49 45 44 41 86 42
WRMS | 1890 32 34 21 16 22 26 19 193 |NE 45 49 41 45 39 39 36 81 38
MEDI | 1267 20 22 20 15 18 22 18 121 |MD 48 51 42 47 42 38 39 79 40
Table 3.1983.2 GPS week: 1983 Day: 2 MJD: 58127
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 | 765 17 25 20 14 20 20 25 --- 8 | 37 30 45 43 41 47 26 --- 37
R02 | 843 5 7 14 7 6 15 23 270 6 | 38 38 45 43 44 48 30 154 40
R03 | 1805 19 23 16 10 9 21 13 149 6 | 54 60 57 53 60 67 55 47 56
R04 | 1069 15 17 13 10 6 16 10 --- 5 | 59 57 59 50 51 48 44 --- 51
R05 | 559 57 23 39 34 42 57 37 --- 19 | 42 58 37 57 55 33 31 --- 37
R06 | 2545 24 23 21 24 12 28 15 --- 9 | 45 47 40 61 53 48 50 --- 49
R07 | 687 18 26 16 7 11 23 15 474 7 | 64 71 63 55 58 46 58 303 56
R08 | 1698 20 27 18 15 19 20 15 --- 8 | 45 56 45 54 46 48 44 --- 46
R09E | 4001 12 14 13 10 17 8 17 --- 6 | 23 25 18 28 34 26 29 --- 24
R10E | 1833 13 27 18 15 17 19 11 --- 7 | 45 51 44 46 40 42 41 --- 41
R11E | 1645 14 18 17 13 17 18 13 187 7 | 43 41 46 43 39 49 44 117 42
R13E | 2324 16 16 14 19 12 21 17 --- 7 | 65 66 67 75 65 62 67 --- 66
XR14E | 1337 19 16 12 12 15 --- 15 --- 7 | 45 47 38 47 42 --- 44 --- 42
R15E | 1309 28 33 21 10 28 33 23 --- 10 | 46 52 42 53 48 62 49 --- 46
R16E | 2631 24 53 28 22 21 27 25 --- 11 | 51 63 46 62 59 49 42 --- 48
R17 | 668 36 37 17 11 24 16 21 --- 9 | 62 64 43 47 36 37 36 --- 41
R18 | 558 22 26 12 18 26 18 14 --- 8 | 48 52 33 48 35 32 43 --- 38
R19 | 900 70 69 29 16 34 29 35 --- 16 | 75 77 37 43 25 57 31 --- 39
R20 | 1658 33 52 24 11 36 30 24 --- 11 | 54 67 39 41 34 53 35 --- 37
R21 | 792 43 41 23 10 35 15 22 144 11 | 64 61 46 44 29 36 35 80 39
R22 | 1642 46 45 23 11 36 21 18 --- 11 | 68 67 45 39 27 33 34 --- 37
R23 | 562 18 16 18 31 19 30 20 --- 11 | 41 41 39 65 45 34 50 --- 44
R24 | 1566 27 32 29 32 37 58 24 --- 16 | 65 69 74 80 77 39 45 --- 60
XR26 | ---- 32 52 --- --- --- --- 20 --- 25 | 30 68 --- --- --- --- 39 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1684 30 33 21 18 24 27 21 274 |T 50 55 45 51 45 45 41 140 43
WRMS | 1684 28 29 21 16 20 24 21 274 |NE 52 57 46 51 44 44 40 146 43
MEDI | 1337 20 26 18 13 19 21 18 187 |MD 46 57 45 48 44 47 42 117 41
Table 3.1983.3 GPS week: 1983 Day: 3 MJD: 58128
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 | 682 20 32 17 9 13 25 11 --- 7 | 48 63 37 46 43 36 44 --- 40
R02 | 797 12 20 18 15 13 14 19 93 7 | 39 48 42 34 41 46 28 135 36
R03 | 1654 12 11 15 9 8 9 7 147 4 | 49 50 57 50 54 53 52 37 52
R04 | 1043 12 13 15 11 18 21 10 --- 6 | 42 52 50 59 67 38 48 --- 51
R05 | 1242 52 63 13 12 26 56 39 --- 14 | 43 41 45 32 47 31 35 --- 32
R06 | 1049 14 19 14 26 10 21 17 --- 8 | 37 39 42 58 46 34 38 --- 42
R07 | 684 24 18 22 13 14 38 24 136 10 | 61 54 58 53 41 32 33 226 46
R08 | 760 19 17 14 24 19 48 14 --- 10 | 52 58 58 69 59 29 50 --- 53
R09E | 4483 14 13 17 12 20 22 19 --- 7 | 22 24 19 28 37 30 35 --- 25
R10E | 892 10 22 22 17 17 20 14 --- 8 | 43 52 44 52 44 45 49 --- 45
R11E | 819 12 17 19 16 22 21 10 211 7 | 37 38 34 39 31 39 41 56 34
R13E | 1199 17 13 22 19 19 39 18 --- 10 | 56 56 57 56 54 63 55 --- 52
XR14E | 1846 16 19 16 13 19 --- 16 --- 8 | 38 39 32 37 38 --- 39 --- 33
R15E | 2295 27 14 14 13 24 30 20 --- 9 | 44 43 35 38 42 43 34 --- 35
R16E | 2404 30 52 28 30 35 33 43 --- 15 | 72 74 57 71 69 65 89 --- 66
R17 | 827 38 36 21 11 25 27 22 --- 10 | 69 67 49 41 35 41 34 --- 41
R18 | 809 20 21 16 16 28 16 11 --- 8 | 51 52 41 51 32 35 40 --- 40
R19 | 811 69 78 20 13 30 33 39 --- 15 | 83 87 48 56 52 58 30 --- 47
R20 | 1324 27 21 26 12 22 36 31 --- 11 | 56 55 33 37 33 58 38 --- 34
R21 | 494 46 49 19 13 26 17 22 131 10 | 72 74 44 43 28 47 35 110 41
R22 | 948 43 48 14 9 36 22 18 --- 11 | 70 73 42 43 23 47 35 --- 39
R23 | 837 17 21 14 27 17 17 17 --- 8 | 36 36 41 64 38 40 56 --- 46
R24 | 2439 36 36 16 28 31 56 47 --- 16 | 74 71 52 74 57 43 53 --- 54
XR26 | ---- 23 46 --- --- --- --- 16 --- 19 | 22 41 --- --- --- --- 36 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1569 30 34 18 17 23 31 24 149 |T 50 53 44 49 43 43 42 112 42
WRMS | 1569 28 31 18 16 25 27 23 149 |NE 53 56 46 50 43 41 40 127 42
MEDI | 948 20 21 17 13 20 22 18 136 |MD 48 52 44 50 42 41 38 110 41
Table 3.1983.4 GPS week: 1983 Day: 4 MJD: 58129
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 | 574 26 31 15 16 19 16 12 --- 8 | 54 54 44 36 49 43 45 --- 41
R02 | 1254 12 11 14 15 11 12 17 184 6 | 45 42 44 36 46 43 39 87 41
R03 | 2263 7 9 11 6 11 17 20 145 5 | 59 61 63 62 64 82 58 34 63
R04 | 798 11 11 23 11 16 10 14 --- 7 | 66 66 67 54 58 65 59 --- 60
R05 | 1532 34 46 26 24 15 56 32 --- 14 | 47 63 57 46 66 36 44 --- 47
R06 | 891 22 25 23 33 15 41 16 --- 11 | 43 43 42 66 49 28 48 --- 45
R07 | 856 22 27 22 11 18 33 24 99 9 | 62 63 59 51 40 42 52 175 49
R08 | 1089 11 12 13 12 15 22 25 --- 7 | 50 50 51 49 51 40 36 --- 45
R09E | 4032 14 22 14 8 16 23 22 --- 7 | 25 31 24 27 38 36 28 --- 26
R10E | 1241 9 11 13 15 16 18 15 --- 6 | 42 47 40 46 46 42 45 --- 42
R11E | 1472 14 17 12 13 16 18 10 245 6 | 44 49 46 48 45 49 44 57 45
R13E | 876 17 33 30 23 19 21 19 --- 10 | 70 82 73 83 78 74 66 --- 73
XR14E | 968 16 18 22 20 23 --- 21 --- 10 | 46 48 44 51 49 --- 52 --- 45
R15E | 2950 29 21 22 14 31 28 23 --- 10 | 44 41 50 52 49 57 48 --- 46
R16E | 3179 29 54 18 31 23 39 31 --- 12 | 94 112 107 121 116 110 90 --- 105
R17 | 843 42 41 22 10 35 19 16 --- 11 | 66 63 50 42 37 38 32 --- 41
R18 | 1329 24 25 12 14 18 24 6 --- 7 | 52 52 35 48 44 30 43 --- 40
R19 | 853 60 53 21 32 34 44 31 --- 16 | 60 60 37 50 38 46 31 --- 36
R20 | 1076 34 36 15 19 30 31 28 --- 11 | 53 43 40 44 35 41 40 --- 38
R21 | 946 41 40 18 11 31 24 20 104 11 | 68 66 55 49 46 43 39 56 47
R22 | 606 48 39 18 11 31 24 19 --- 11 | 68 65 42 46 37 58 38 --- 44
R23 | 558 19 19 15 32 14 29 14 --- 9 | 38 35 37 57 39 37 49 --- 40
R24 | 1035 27 54 30 29 23 44 30 --- 13 | 78 90 84 90 71 65 71 --- 75
XR26 | ---- 29 59 --- --- --- --- 20 --- 24 | 41 55 --- --- --- --- 39 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1641 28 32 19 20 22 29 21 164 |T 54 57 51 54 51 50 47 81 48
WRMS | 1641 28 29 19 15 20 25 22 164 |NE 55 57 50 51 48 46 44 88 46
MEDI | 1035 22 25 18 15 18 24 20 145 |MD 52 54 46 49 46 43 44 57 45
Table 3.1983.5 GPS week: 1983 Day: 5 MJD: 58130
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 | 732 31 41 15 10 11 19 26 --- 8 | 47 58 28 39 35 38 24 --- 31
R02 | 1136 10 15 17 10 10 24 17 236 7 | 33 36 32 34 33 27 25 70 29
R03 | 2580 14 12 13 10 12 21 15 145 6 | 48 49 43 56 58 43 43 31 48
R04 | 716 11 12 16 11 9 13 27 --- 7 | 54 54 48 60 57 57 46 --- 52
R05 | 987 33 27 32 24 28 61 33 --- 16 | 37 32 48 36 36 39 36 --- 36
R06 | 798 38 29 20 21 20 26 14 --- 10 | 34 38 42 57 59 53 39 --- 45
R07 | 829 18 20 17 8 17 35 18 117 8 | 47 48 45 47 49 28 32 114 39
R08 | 1243 15 17 13 22 13 18 27 --- 8 | 42 44 39 52 34 37 31 --- 38
R09E | 4051 17 19 13 10 20 18 20 --- 7 | 25 28 22 21 27 37 24 --- 22
R10E | 900 11 14 15 11 14 20 15 --- 6 | 42 41 42 41 39 39 43 --- 39
R11E | 614 17 18 17 12 12 21 17 163 7 | 62 63 58 64 58 59 53 65 58
R13E | 2014 16 19 23 14 18 18 16 --- 8 | 98 96 103 99 100 97 105 --- 99
XR14E | 1464 16 22 21 19 26 --- 17 --- 10 | 41 41 47 54 53 --- 48 --- 47
R15E | 2489 30 29 22 20 33 18 20 --- 10 | 42 41 35 52 50 45 46 --- 42
R16E | 2625 18 36 25 23 31 24 40 --- 12 | 141 136 124 127 149 142 136 --- 133
R17 | 505 40 42 24 12 42 22 14 --- 11 | 48 49 34 36 27 31 23 --- 29
R18 | 1167 20 21 19 17 26 18 9 --- 8 | 43 43 41 50 33 42 46 --- 42
R19 | 610 62 61 20 22 38 23 20 --- 14 | 67 69 64 69 74 69 61 --- 64
R20 | 1176 46 52 22 30 31 31 26 --- 13 | 61 67 44 55 37 48 35 --- 43
R21 | 818 39 37 25 14 33 22 17 131 11 | 57 57 51 44 33 39 35 48 40
R22 | 424 51 50 21 16 30 27 26 --- 12 | 59 59 37 31 27 47 27 --- 33
R23 | 582 19 18 17 18 15 20 15 --- 7 | 31 32 32 43 31 35 42 --- 35
R24 | 665 22 33 26 26 38 30 14 --- 12 | 40 47 40 46 33 38 42 --- 35
XR26 | ---- 30 40 --- --- --- --- 21 --- 25 | 66 75 --- --- --- --- 52 --- 53
------+---------------------------------------------------+-----------------------------------------------
RMS | 1546 30 31 20 18 25 26 21 164 |T 52 54 47 52 49 49 45 65 47
WRMS | 1546 30 30 20 15 21 23 22 164 |NE 47 50 41 47 41 41 37 65 40
MEDI | 900 19 22 20 16 20 21 17 145 |MD 47 48 42 50 37 39 42 65 40
Table 3.1983.6 GPS week: 1983 Day: 6 MJD: 58131
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 | 573 38 36 18 10 14 20 22 --- 9 | 63 62 40 37 38 47 30 --- 38
R02 | 1204 20 23 24 9 6 30 12 197 8 | 47 50 49 36 37 35 30 61 37
R03 | 2214 23 26 26 8 17 39 16 174 9 | 68 69 64 61 65 52 53 41 59
R04 | 626 19 21 19 12 10 27 12 --- 7 | 72 76 65 71 71 68 59 --- 66
R05 | 752 34 33 36 25 23 45 35 --- 14 | 45 67 68 57 53 51 38 --- 50
R06 | 916 36 44 17 25 17 28 15 --- 10 | 43 43 45 69 54 60 48 --- 52
R07 | 730 15 17 18 14 12 17 19 172 7 | 66 68 69 57 59 60 45 90 56
R08 | 1135 16 18 18 16 10 34 17 --- 8 | 59 60 60 68 62 69 49 --- 60
R09E | 3794 13 15 16 8 16 26 25 --- 8 | 34 36 29 36 43 31 36 --- 33
R10E | 1128 9 19 16 14 12 21 16 --- 6 | 47 55 42 53 43 45 47 --- 45
R11E | 705 16 18 17 14 16 23 17 168 7 | 72 74 73 66 69 71 61 80 67
R13E | 1163 17 19 24 16 18 19 17 --- 8 | 114 117 117 121 125 117 125 --- 120
XR14E | 1007 22 15 23 23 20 --- 14 --- 10 | 43 46 43 61 51 --- 55 --- 49
R15E | 3997 32 29 18 13 42 28 14 --- 11 | 47 49 37 47 63 44 47 --- 43
R16E | 1516 23 25 27 19 31 24 27 --- 11 | 143 155 152 154 161 150 152 --- 151
R17 | 657 41 42 29 12 29 23 25 --- 11 | 76 76 49 43 27 48 32 --- 41
R18 | 834 26 27 28 22 23 13 18 --- 10 | 63 63 48 63 40 47 53 --- 51
R19 | 547 63 67 27 18 36 37 28 --- 15 | 88 88 60 70 72 67 50 --- 61
R20 | 1170 68 89 23 31 29 45 34 --- 17 | 91 110 52 50 46 58 45 --- 51
R21 | 609 37 35 23 12 28 15 18 163 10 | 84 83 62 66 46 63 48 90 59
R22 | 590 53 52 25 10 31 16 21 --- 12 | 89 88 61 51 35 49 43 --- 50
R23 | 763 21 24 21 19 15 23 13 --- 8 | 41 40 40 63 41 46 54 --- 47
R24 | 1436 30 27 29 12 24 54 21 --- 12 | 69 69 62 60 41 45 52 --- 52
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 47 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1541 33 37 23 17 23 29 21 175 |T 68 71 60 63 58 60 54 72 57
WRMS | 1541 32 34 23 15 20 28 21 175 |NE 66 69 55 57 49 54 45 70 51
MEDI | 916 23 26 23 14 18 24 17 172 |MD 66 68 60 61 51 51 48 80 51
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