[IGSREPORT-25834] Wk 1992 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 2 05:14:40 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1992 (Mar 11, 2018 - Mar 17, 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 2.1992.
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:
igl1992[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1992 in the SP3 format.
igl19927.sum Combination Report for GPS Week 1992.
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 | -7.0 ns
1 | -7.5 ns
2 | -5.8 ns
3 | -6.6 ns
4 | -7.6 ns
5 | -6.9 ns
6 | -8.3 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
----+--------+---------------
4 | GFZ | R08
6 | GFZ | R08
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 1.1992, 1a.1992).
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 2.1992.0-6)
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 3.1992.0-6).
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 1992 summary. (Mar 11, 2018 - Mar 17, 2018)
Table 1.1992.a GPS week : 1992 MJD: 58188.0-58194.0
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 -17 -7 23 .11 26 28 | 77378 -2257 11049 268110
| 1 0 2 18 21 28 .02 | 181901 5656
cof n/a| 0 0 1 -2 16 18 .08 29 30 | 77364 -2242 11047 268112
| 1 0 2 20 14 35 .05 | 181899 5650
emx n/a| 0 0 3 11 -37 -54 .00 24 24 | -4760 1079 3301 9119
| 0 1 2 28 19 53 .06 | 9847 1464
esx n/a| 0 0 -3 -8 29 9 .20 17 15 | -7173 -622 3318 11624
| 0 0 1 12 14 15 .01 | 12756 1634
gfz n/a| 0 -1 -5 16 40 0 .01 77 76 | 0 267 3322 9362
| 1 1 1 16 28 40 .03 | 0 1156
grg n/a| -1 0 13 -71 -10 59 -.41 29 25 | 60039 256 3288 150477
| 1 1 3 26 19 42 .04 | 177573 1290
iac n/a| 0 1 -6 35 -16 -30 .02 21 21 | 82378 -360 11062 267887
| 1 1 3 23 31 40 .04 | 176930 575
mcc n/a| -2 -2 -8 141 12 114 -.15 171 171 | --- --- --- ---
| 5 10 10 163 129 271 .19 | --- ---
Table 1.1992.b GPS week : 1992 MJD: 58188.0-58194.0
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 11 10 11 12 10 21 |
R02 | 7 7 10 7 7 7 7 |
R03 | 7 10 6 7 6 7 8 |
R04 | 7 10 8 7 7 8 8 |
R05 | 11 11 11 9 12 13 11 |
R06 | 8 7 8 8 10 16 17 |
R07 | 9 8 9 8 7 8 7 |
R08 | 14 10 11 7 12 17 34 |
R09 | 8 6 6 8 8 7 7 |
R10 | 7 7 7 9 8 7 8 |
R11 | 9 7 9 10 8 8 6 |
R13 | 7 9 6 7 6 6 8 |
R14 | 9 9 9 9 9 8 8 |
R15 | 17 17 12 12 13 14 15 |
R16 | 13 15 16 14 13 14 14 |
R17 | 9 13 12 10 10 12 10 |
R18 | 9 7 8 8 8 6 8 |
R19 | 13 11 12 17 15 16 12 |
R20 | 14 17 16 17 12 14 14 |
R21 | 10 10 10 8 9 11 10 |
R22 | 11 11 11 10 10 11 12 |
R23 | 8 8 10 9 7 8 9 |
R24 | 17 15 20 16 15 16 14 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1992.c GPS week : 1992 MJD: 58188.0-58194.0
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 1992 0 | 15 -45 24 863 -1207 3145 84.9 1440 1440 | -7002 0
brd 1992 1 | 3 88 137 128 -2307 823 85.3 1360 1360 | -7531 0
brd 1992 2 | -36 -10 36 -168 -552 2954 86.1 1698 1698 | -5761 0
brd 1992 3 | 4 37 40 -177 809 2646 82.8 1495 1495 | -6559 0
brd 1992 4 | 4 -29 141 -277 980 2628 82.8 1600 1600 | -7640 0
brd 1992 5 | 4 49 114 -635 654 3734 85.4 1374 1374 | -6929 0
brd 1992 6 | 23 -5 57 432 416 4332 83.7 1342 1342 | -8346 0
-------------+------------------------------------------------------------+----------------
brd 1992 mean| 2 12 78 23 -172 2894 84.4 1472 1472 | -7109 0
brd 1992 sdev| 18 47 50 497 1231 1099 1.3 134 134 | 832 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 2.1992.0 GPS week: 1992 Day: 0 MJD: 58188
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 -1 0 7 -30 1 .14 29 31 | 133939 -2719 58080 827779
cof n/a| -1 0 0 16 20 10 .11 33 33 | 133922 -2691 58080 827777
emx n/a| 0 0 2 -51 -21 -56 .08 24 24 | -16729 91 3895 8867
esx n/a| 0 0 -2 -2 51 33 .19 17 14 | 4573 -419 3938 11159
gfz n/a| 0 -4 -7 -9 4 60 .03 23 23 | 0 -107 3976 8980
grg n/a| 1 0 13 -46 -51 -1 -.38 22 20 | -7068 268 3898 8580
iac n/a| 0 1 -8 65 16 -47 .00 19 20 | 141949 -1578 58143 828677
mcc n/a| 0 0 10 -51 6 -208 -.02 201 201 | --- --- --- ---
Table 2.1992.1 GPS week: 1992 Day: 1 MJD: 58189
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 -7 8 -6 .08 28 30 | -13620 -2714 3195 9882
cof n/a| 1 0 3 14 23 -42 .16 28 30 | -13636 -2682 3193 9881
emx n/a| -1 0 6 24 -8 -104 .07 24 24 | 3154 -1524 3152 9246
esx n/a| 0 0 -5 -18 38 10 .20 16 15 | -3924 -3464 3203 11513
gfz n/a| 1 -2 -5 20 72 12 -.01 25 29 | 0 -2068 3190 9726
grg n/a| 0 0 17 -105 6 36 -.42 30 25 | -6080 -2561 3165 9070
iac n/a| 0 3 -10 52 -72 18 -.04 20 20 | -6227 -131 3197 9283
mcc n/a| -5 16 -9 245 -162 258 -.28 215 215 | --- --- --- ---
Table 2.1992.2 GPS week: 1992 Day: 2 MJD: 58190
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 -31 -36 -11 .09 25 27 | -14206 1745 3004 10326
cof n/a| -1 1 0 -10 0 33 -.00 26 29 | -14216 1748 3000 10323
emx n/a| -1 2 5 14 -43 -132 -.00 30 30 | 993 2863 2985 9889
esx n/a| 1 0 -3 6 22 24 .19 15 14 | -21799 1087 3001 12324
gfz n/a| 2 -2 -6 0 82 11 .01 24 24 | 0 848 2990 10142
grg n/a| -2 -1 15 -69 -9 37 -.43 32 31 | -6238 1070 2999 8825
iac n/a| 0 0 -5 26 -40 28 .03 21 21 | -4630 -298 3003 9767
mcc n/a| -3 0 -16 21 -21 420 -.40 202 202 | --- --- --- ---
Table 2.1992.3 GPS week: 1992 Day: 3 MJD: 58191
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 2 -9 -11 55 .11 26 29 | -12632 1130 3363 9488
cof n/a| -1 0 3 15 13 36 .07 30 32 | -12650 1144 3365 9495
emx n/a| -1 0 3 21 -29 -50 -.05 25 25 | -4748 1899 3345 9144
esx n/a| 0 0 -1 -24 33 1 .18 16 16 | 1637 851 3363 11666
gfz n/a| 0 0 -4 22 20 -68 .05 22 22 | 0 999 3359 9055
grg n/a| 1 -1 8 -66 -13 130 -.48 31 26 | -7197 1082 3338 8717
iac n/a| 1 0 -6 37 0 -19 .06 21 22 | -4640 -452 3353 8802
mcc n/a| -6 -6 -8 17 118 301 -.20 186 186 | --- --- --- ---
Table 2.1992.4 GPS week: 1992 Day: 4 MJD: 58192
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 -7 -16 54 .12 24 27 | -11748 654 3269 9947
cof n/a| -2 1 -1 2 24 71 .09 27 29 | -11758 668 3268 9950
emx n/a| 0 -1 2 22 -37 -42 -.01 20 20 | 6389 681 3261 9522
esx n/a| 0 0 -5 -18 5 9 .22 18 15 | -19739 -91 3243 12096
gfz n/a| 0 0 -4 12 35 13 -.01 396 396 | 0 135 3266 9809
grg n/a| -1 2 15 -105 6 49 -.38 26 21 | -7790 313 3217 9152
iac n/a| 2 0 -6 54 8 -67 .08 22 22 | -6296 -208 3277 9523
mcc n/a| -9 -12 -20 324 -93 -310 .18 155 155 | --- --- --- ---
Table 2.1992.5 GPS week: 1992 Day: 5 MJD: 58193
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 3 -45 9 39 .12 27 27 | 470847 -14417 3062 999999
cof n/a| 2 -1 3 -25 -4 23 .04 31 30 | 470828 -14396 3063 999999
emx n/a| 0 0 0 21 -67 -29 -.07 24 24 | -19434 2038 3076 8499
esx n/a| 2 0 -3 4 25 -5 .18 17 14 | 8169 -171 3061 10925
gfz n/a| -1 0 -4 39 22 0 -.02 24 17 | 0 1465 3087 8680
grg n/a| -2 0 8 -37 -6 88 -.40 31 25 | 462735 1018 3057 999999
iac n/a| 0 2 0 7 -20 -59 .00 23 21 | 463689 216 3061 999999
mcc n/a| -2 -17 -17 355 228 152 -.13 103 103 | --- --- --- ---
Table 2.1992.6 GPS week: 1992 Day: 6 MJD: 58194
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 4 -30 21 29 .12 27 27 | -10933 517 3370 9354
cof n/a| -1 1 3 -34 38 -1 .11 30 28 | -10941 509 3365 9361
emx n/a| 0 0 3 27 -52 32 -.02 23 23 | -2948 1508 3393 8669
esx n/a| 0 0 -1 -5 25 -6 .21 17 14 | -19131 -2151 3423 11686
gfz n/a| 0 -1 -7 28 48 -31 .02 25 18 | 0 602 3392 9147
grg n/a| -3 0 12 -66 -3 75 -.36 30 26 | -8089 607 3344 8996
iac n/a| 1 2 -7 3 -8 -66 -.01 22 22 | -7194 -70 3403 9160
mcc n/a| 9 0 0 75 13 186 -.19 132 132 | --- --- --- ---
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 3.1992.0 GPS week: 1992 Day: 0 MJD: 58188
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1573 25 29 19 11 24 28 20 --- 9 | 51 46 49 57 54 69 53 --- 52
R02E | 2107 12 16 16 10 21 17 13 90 6 | 79 81 81 81 77 73 80 83 78
R03E | 852 17 25 18 8 16 20 12 94 6 | 58 62 54 61 62 64 60 90 59
R04E | 1142 13 15 18 8 21 18 11 --- 6 | 40 41 43 45 45 41 42 --- 41
R05E | 1857 15 28 27 28 31 27 18 --- 11 | 126 130 128 116 131 137 128 --- 125
R06E | 1238 14 15 23 20 17 16 13 --- 8 | 47 50 40 62 52 47 52 --- 49
R07E | 1106 19 19 24 11 24 20 15 406 8 | 58 60 51 53 59 60 61 85 54
XR08E | 722 27 29 --- 17 --- --- 13 --- 13 | 80 75 --- 58 --- --- 82 --- 72
R09M | 1339 23 14 24 15 16 13 11 --- 7 | 29 31 25 34 33 22 31 --- 27
R10 | 1766 9 12 9 17 10 19 14 --- 6 | 39 38 32 41 30 35 31 --- 33
R11 | 741 21 24 16 14 21 19 22 133 8 | 42 42 33 35 27 29 23 29 29
R13M | 3675 11 16 10 20 14 23 8 --- 7 | 35 37 33 42 22 26 33 --- 31
R14M | 628 37 39 19 8 25 11 15 --- 8 | 50 50 40 34 29 29 26 --- 31
R15M | 1651 64 69 35 34 25 27 42 --- 17 | 65 67 53 41 36 46 36 --- 39
R16M | 576 33 30 39 17 22 38 16 --- 12 | 28 29 26 40 32 25 29 --- 26
R17 | 742 20 23 23 10 31 12 16 --- 8 | 49 49 47 41 26 46 30 --- 37
R18 | 1327 21 23 13 13 29 23 22 --- 9 | 32 33 33 36 36 43 24 --- 32
R19 | 723 42 43 37 21 28 18 30 --- 13 | 53 52 41 30 24 42 21 --- 31
R20 | 744 51 75 25 14 26 43 20 --- 13 | 53 68 34 33 27 34 27 --- 27
R21 | 825 31 30 28 9 30 10 17 51 9 | 54 56 48 37 24 38 35 57 37
R22M | 717 34 35 24 14 24 22 26 --- 10 | 52 50 40 37 33 42 28 --- 35
R23M | 1160 19 15 19 22 19 14 14 --- 8 | 21 24 26 41 32 27 28 --- 29
XR24 | 1377 37 73 33 24 --- 41 38 --- 17 | 60 85 63 46 --- 34 36 --- 39
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 28 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1439 29 33 24 17 23 22 19 201 |T 52 54 46 47 42 45 42 68 43
WRMS | 1439 31 33 24 14 23 20 20 201 |NE 47 52 41 37 27 37 28 43 32
MEDI | 1142 21 25 23 14 24 19 15 94 |MD 51 50 40 41 33 41 31 83 35
Table 3.1992.1 GPS week: 1992 Day: 1 MJD: 58189
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1242 28 25 25 16 29 31 18 --- 10 | 43 46 40 51 58 53 58 --- 48
R02E | 2925 13 15 15 11 19 17 12 54 6 | 60 62 62 60 58 62 52 59 58
R03E | 1455 20 20 19 16 22 36 12 60 9 | 42 39 45 41 51 57 41 79 42
R04E | 882 15 19 27 11 27 30 18 --- 9 | 28 29 47 39 46 26 29 --- 33
R05E | 712 23 22 26 17 29 26 22 --- 10 | 102 109 96 98 95 91 80 --- 91
R06E | 741 15 19 16 19 11 19 14 --- 7 | 40 37 40 45 35 48 39 --- 39
R07E | 1348 18 13 17 12 21 18 18 453 7 | 48 45 51 49 56 46 49 60 48
XR08E | 1758 18 22 --- 16 19 --- 14 --- 9 | 57 61 --- 42 180 --- 64 --- 54
R09M | 1671 20 23 15 12 14 12 11 --- 6 | 28 32 26 27 30 23 25 --- 24
R10 | 617 16 14 18 11 28 12 8 --- 7 | 17 19 17 23 25 28 20 --- 17
R11 | 552 21 25 11 10 11 13 18 126 6 | 24 28 22 22 24 23 18 17 19
R13M | 1992 13 18 17 22 20 29 11 --- 8 | 26 29 30 34 28 33 23 --- 25
R14M | 872 32 37 16 8 26 16 18 --- 8 | 27 29 25 28 25 23 24 --- 23
R15M | 3010 56 57 32 20 33 41 40 --- 16 | 36 41 28 30 35 34 27 --- 24
R16M | 1282 38 50 50 27 17 39 23 --- 15 | 27 38 33 30 28 17 25 --- 21
R17 | 577 34 27 28 10 40 29 28 --- 12 | 25 26 30 21 24 31 17 --- 19
R18 | 798 14 10 19 12 20 15 15 --- 7 | 19 24 33 25 29 19 21 --- 21
R19 | 1410 39 29 25 13 22 19 30 --- 11 | 26 26 32 29 36 22 22 --- 23
R20 | 710 33 30 36 29 31 66 22 --- 16 | 39 41 28 37 30 37 28 --- 26
R21 | 511 30 31 19 16 30 22 14 59 9 | 30 34 29 31 31 30 27 40 26
R22M | 760 30 29 24 19 26 23 19 --- 10 | 26 26 27 29 26 38 24 --- 23
R23M | 991 15 20 13 18 23 19 14 --- 7 | 18 19 18 31 31 17 20 --- 20
R24 | 790 37 37 33 13 22 59 29 --- 14 | 34 39 29 29 35 30 21 --- 20
XR26 | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 31 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1360 28 28 24 16 25 30 20 215 |T 35 38 35 37 44 35 32 51 32
WRMS | 1360 30 30 24 15 29 25 20 215 |NE 26 29 27 27 29 27 22 28 22
MEDI | 882 21 23 19 16 22 22 18 60 |MD 28 34 30 31 31 30 25 59 24
Table 3.1992.2 GPS week: 1992 Day: 2 MJD: 58190
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1941 28 21 24 12 28 16 23 --- 9 | 56 57 52 60 62 61 52 --- 56
R02E | 3547 16 20 19 20 22 20 33 59 10 | 62 72 64 75 73 59 48 60 62
R03E | 1661 15 14 15 9 19 13 12 116 6 | 28 28 25 26 25 28 30 90 24
R04E | 1614 13 15 22 10 20 26 12 --- 7 | 20 24 24 22 28 30 23 --- 18
R05E | 1385 25 24 26 12 31 23 28 --- 10 | 53 56 53 51 54 53 39 --- 46
R06E | 1372 16 14 19 17 11 26 14 --- 8 | 35 39 35 46 36 44 36 --- 35
R07E | 757 16 12 22 15 24 24 16 411 8 | 35 33 30 33 40 27 31 72 28
XR08E | 728 25 22 31 14 24 --- 11 --- 10 | 28 30 20 30 204 --- 36 --- 33
R09M | 1419 10 16 11 10 18 9 18 --- 6 | 20 24 21 24 38 22 20 --- 21
R10 | 904 10 11 21 16 14 17 18 --- 7 | 27 25 23 33 31 24 21 --- 24
R11 | 640 25 25 24 9 25 12 21 118 8 | 29 30 29 24 23 17 14 25 19
R13M | 1541 11 11 11 10 20 20 10 --- 6 | 25 29 28 31 32 30 28 --- 26
R14M | 605 25 28 17 16 23 27 16 --- 9 | 32 35 25 33 23 23 20 --- 23
R15M | 4680 41 47 24 16 22 25 27 --- 11 | 46 50 35 36 33 30 30 --- 31
R16M | 706 26 34 62 19 22 56 21 --- 15 | 29 34 46 32 31 23 25 --- 25
R17 | 618 30 32 22 12 36 26 27 --- 11 | 31 32 28 27 16 33 14 --- 20
R18 | 641 12 8 14 10 25 17 25 --- 8 | 21 19 27 23 24 13 17 --- 17
R19 | 1693 43 51 24 18 27 14 24 --- 11 | 34 40 31 27 24 27 24 --- 24
R20 | 687 14 20 30 20 27 81 23 --- 16 | 20 38 20 37 41 35 19 --- 24
R21 | 570 30 30 24 12 33 14 17 68 9 | 32 33 33 28 26 29 26 30 26
R22M | 845 37 38 31 14 33 13 10 --- 11 | 32 35 27 29 31 23 24 --- 22
R23M | 1158 20 13 19 25 12 24 20 --- 9 | 18 29 24 40 34 27 21 --- 25
R24 | 1555 33 37 86 24 25 69 25 --- 20 | 49 60 56 40 25 28 31 --- 31
XR26 | ---- --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 32 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1697 25 26 30 15 24 32 21 202 |T 33 37 32 35 41 31 27 55 28
WRMS | 1697 27 29 30 14 24 31 21 202 |NE 30 34 30 29 26 25 22 27 24
MEDI | 1158 25 21 22 14 24 20 18 116 |MD 31 33 28 32 31 28 25 60 25
Table 3.1992.3 GPS week: 1992 Day: 3 MJD: 58191
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1765 30 22 29 13 23 23 23 --- 10 | 77 79 84 66 81 86 73 --- 77
R02E | 3536 15 14 16 12 21 21 12 96 7 | 69 68 68 69 59 68 77 133 67
R03E | 833 14 13 16 13 20 16 12 151 7 | 29 31 30 29 31 35 27 83 26
R04E | 1322 16 22 14 11 13 24 14 --- 6 | 23 24 28 29 35 46 32 --- 28
R05E | 2916 19 47 25 12 23 21 19 --- 9 | 77 94 76 77 83 95 73 --- 77
R06E | 1476 16 23 14 13 15 27 21 --- 8 | 43 45 37 45 39 51 41 --- 39
R07E | 794 18 12 14 16 16 26 12 341 7 | 27 28 22 31 33 37 29 88 26
R08E | 740 15 18 17 13 16 22 15 --- 7 | 38 39 22 27 236 31 42 --- 34
R09M | 1297 23 28 22 11 16 29 12 --- 8 | 14 18 18 21 25 24 16 --- 12
R10 | 1223 16 27 16 12 16 28 26 --- 8 | 32 45 32 33 31 34 21 --- 27
R11 | 711 28 29 21 9 22 19 31 125 10 | 32 32 26 22 19 25 14 28 18
R13M | 818 11 14 15 16 14 17 16 --- 6 | 24 25 27 38 25 39 29 --- 28
R14M | 553 26 27 20 9 25 18 15 --- 8 | 31 35 30 26 27 21 20 --- 23
R15M | 3017 42 41 26 14 26 17 34 --- 12 | 50 47 39 34 35 43 39 --- 36
R16M | 1434 22 49 34 24 15 61 11 --- 13 | 25 44 34 40 34 27 30 --- 27
R17 | 626 28 27 21 11 29 24 25 --- 10 | 43 41 42 41 34 40 23 --- 35
R18 | 518 16 19 14 11 18 12 26 --- 7 | 28 30 31 32 22 30 25 --- 26
R19 | 1154 59 59 28 25 41 27 34 --- 16 | 55 57 32 26 25 46 19 --- 27
R20 | 829 25 20 56 25 12 68 18 --- 16 | 41 42 48 40 37 23 22 --- 28
R21 | 703 24 25 20 10 22 14 20 99 8 | 38 42 35 35 31 28 25 59 30
R22M | 637 30 31 18 12 32 22 18 --- 10 | 37 38 31 32 23 34 21 --- 27
R23M | 683 13 12 10 22 15 32 21 --- 9 | 23 20 21 31 26 29 17 --- 18
R24 | 1267 30 46 47 23 32 57 29 --- 16 | 56 73 60 37 26 24 32 --- 36
XR26 | ---- --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 25 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1495 26 30 25 16 22 31 21 186 |T 39 43 37 37 44 39 32 78 33
WRMS | 1495 29 32 25 16 22 26 22 186 |NE 40 45 38 33 28 31 22 43 28
MEDI | 833 22 25 20 13 20 23 18 125 |MD 37 41 32 33 31 34 25 83 27
Table 3.1992.4 GPS week: 1992 Day: 4 MJD: 58192
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 1080 24 17 29 19 24 30 37 --- 12 | 100 106 94 99 101 122 75 --- 98
R02E | 4044 12 9 17 13 14 20 15 97 7 | 80 78 73 77 75 88 74 135 76
R03E | 1070 14 9 16 13 13 16 11 115 6 | 29 28 26 33 34 30 31 152 28
R04E | 885 12 12 16 15 14 25 14 --- 7 | 20 25 20 25 30 36 25 --- 21
R05E | 3212 22 22 26 26 24 33 22 --- 11 | 61 58 65 64 62 43 45 --- 54
R06E | 1510 17 16 16 28 12 29 23 --- 10 | 39 43 42 57 39 53 54 --- 44
R07E | 1860 18 17 15 12 20 23 8 284 7 | 26 26 26 30 36 35 27 77 26
R08E | 1742 13 25 30 25 1897 21 16 --- 11 | 28 31 26 39 9999 39 34 --- 29
R09M | 1072 24 25 16 10 18 28 7 --- 8 | 21 24 17 18 25 30 18 --- 16
R10 | 1474 19 15 14 11 26 16 11 --- 7 | 31 28 24 26 27 28 19 --- 21
R11 | 621 24 21 14 11 15 12 26 101 8 | 25 24 17 23 24 19 15 45 16
R13M | 1546 7 11 11 16 14 15 16 --- 6 | 19 22 19 26 21 19 16 --- 16
R14M | 620 21 16 22 15 16 14 22 --- 8 | 29 27 30 28 18 21 18 --- 21
R15M | 2519 37 40 29 23 35 20 23 --- 12 | 43 48 42 43 45 38 31 --- 35
R16M | 1446 20 20 23 26 19 52 15 --- 12 | 22 26 32 36 23 23 29 --- 21
R17 | 850 33 38 20 16 28 15 17 --- 9 | 38 42 28 23 19 29 24 --- 24
R18 | 557 17 21 11 16 27 12 21 --- 8 | 26 29 21 31 25 32 22 --- 23
R19 | 897 54 58 28 22 39 20 27 --- 14 | 44 47 33 26 25 36 19 --- 26
R20 | 745 14 50 24 26 17 38 31 --- 11 | 34 75 45 39 31 30 24 --- 24
R21 | 829 25 26 20 10 29 11 26 83 9 | 42 44 47 37 24 35 26 36 34
R22M | 551 28 32 23 6 29 12 29 --- 10 | 37 39 34 32 31 28 22 --- 29
R23M | 642 13 21 10 16 18 16 16 --- 6 | 19 26 22 26 20 19 24 --- 18
R24 | 1271 31 39 16 19 36 58 38 --- 15 | 53 59 33 32 30 37 40 --- 34
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 25 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1600 24 27 20 18 396 26 22 155 |T 37 41 35 37 34 37 30 89 31
WRMS | 1600 27 29 20 15 396 21 22 155 |NE 36 43 31 29 25 30 23 40 25
MEDI | 1072 20 21 17 16 20 20 17 101 |MD 31 31 30 32 27 32 25 77 25
Table 3.1992.5 GPS week: 1992 Day: 5 MJD: 58193
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01E | 692 30 34 23 12 28 20 21 --- 10 | 80 94 87 72 92 94 92 --- 86
R02E | 1577 18 16 16 9 19 15 11 59 6 | 75 77 81 70 71 66 73 66 72
R03E | 798 15 12 17 10 18 20 15 88 7 | 40 41 42 40 38 39 39 94 38
R04E | 1067 18 15 12 10 18 30 13 --- 7 | 25 29 32 26 34 33 24 --- 26
R05E | 3202 16 22 30 21 18 34 39 --- 12 | 94 96 101 89 89 104 71 --- 86
R06E | 1618 44 56 39 27 31 36 40 --- 16 | 62 87 64 87 72 89 81 --- 72
R07E | 1836 20 17 15 12 22 23 15 150 8 | 44 46 42 43 41 48 44 77 41
XR08E | 2752 22 28 --- 28 --- 41 28 --- 17 | 38 36 --- 43 --- 39 38 --- 35
R09M | 1073 12 16 14 17 12 24 14 --- 7 | 23 27 21 31 25 35 23 --- 23
R10 | 1229 11 18 13 20 12 14 9 --- 6 | 23 25 19 31 19 21 19 --- 21
R11 | 602 23 28 10 10 22 31 11 116 8 | 27 28 20 22 23 35 17 31 18
R13M | 1548 10 10 10 11 11 22 15 --- 6 | 19 23 21 20 25 16 16 --- 16
R14M | 484 23 21 16 9 27 21 12 --- 8 | 22 21 23 26 28 33 19 --- 22
R15M | 3085 40 42 30 22 30 26 31 --- 13 | 29 24 36 32 31 36 18 --- 25
R16M | 1259 12 25 38 11 22 63 18 --- 13 | 28 38 25 22 32 35 25 --- 22
R17 | 810 38 43 22 21 33 26 12 --- 11 | 27 29 21 25 18 31 22 --- 18
R18 | 604 15 21 16 6 12 24 11 --- 6 | 19 24 20 18 20 25 21 --- 17
R19 | 818 50 52 37 27 46 24 21 --- 15 | 20 24 22 26 33 23 17 --- 18
R20 | 547 39 51 25 20 21 49 25 --- 13 | 29 48 38 41 36 25 24 --- 27
R21 | 613 29 29 22 17 27 18 35 78 11 | 34 36 33 28 32 35 31 30 28
R22M | 531 31 27 23 11 22 14 33 --- 10 | 31 31 28 34 32 25 19 --- 27
R23M | 612 21 22 17 20 13 17 16 --- 8 | 19 20 23 30 36 25 20 --- 24
R24 | 852 26 35 36 25 29 64 30 --- 15 | 37 40 45 32 24 22 28 --- 22
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 24 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1373 27 31 24 17 24 31 23 103 |T 36 41 38 38 38 40 33 59 33
WRMS | 1373 27 30 24 14 17 25 21 103 |NE 27 31 27 27 25 27 22 30 21
MEDI | 852 22 25 17 17 22 24 15 88 |MD 29 31 28 31 32 35 24 66 25
Table 3.1992.6 GPS week: 1992 Day: 6 MJD: 58194
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
------+---------------------------------------------------+-----------------------------------------------
XR01E |12679 37 52 31 --- 47 40 50 --- 20 | 74 97 70 --- 82 84 57 --- 68
R02E | 1083 16 13 20 13 19 16 11 45 7 | 90 89 98 91 92 84 88 94 90
R03E | 1067 19 17 18 13 22 16 14 139 7 | 54 56 54 51 55 49 55 116 52
R04E | 929 15 9 15 10 23 24 16 --- 7 | 34 33 36 36 34 40 31 --- 33
R05E | 3880 21 37 26 20 19 27 31 --- 11 | 75 82 86 94 93 86 70 --- 82
R06E | 1661 37 40 51 29 33 42 35 --- 17 | 82 86 81 104 88 83 96 --- 86
R07E | 1693 18 14 16 14 12 20 18 185 7 | 54 55 50 55 50 54 66 101 53
XR08E | 3153 48 44 --- --- 443 35 55 --- 34 | 54 56 --- --- 698 40 101 --- 64
R09M | 1107 15 17 11 11 21 24 12 --- 7 | 29 30 32 40 46 33 32 --- 33
R10 | 1198 11 11 7 21 9 31 16 --- 7 | 39 37 28 40 28 36 25 --- 30
R11 | 584 17 20 10 16 12 17 11 142 6 | 41 41 26 34 27 29 29 37 28
R13M | 1095 8 14 10 17 19 19 23 --- 7 | 30 34 32 38 26 26 25 --- 28
R14M | 572 25 30 9 7 25 21 14 --- 7 | 47 50 36 32 29 27 25 --- 30
R15M | 1024 44 44 35 20 41 30 32 --- 15 | 60 62 53 37 39 45 22 --- 38
R16M | 984 22 21 42 16 13 53 20 --- 13 | 32 32 38 40 33 35 29 --- 31
R17 | 616 34 35 17 10 31 20 26 --- 10 | 55 55 44 33 21 45 28 --- 35
R18 | 622 24 26 15 10 20 19 23 --- 8 | 38 35 33 34 24 37 28 --- 30
R19 | 1729 37 32 24 20 27 35 19 --- 12 | 56 56 41 31 22 46 28 --- 32
R20 | 729 48 68 21 22 32 44 28 --- 14 | 47 63 28 42 38 33 29 --- 32
R21 | 821 27 32 20 8 35 16 24 104 10 | 55 58 52 38 32 48 37 61 40
R22M | 532 33 35 26 11 35 20 36 --- 12 | 60 56 57 43 43 47 33 --- 44
R23M | 922 22 22 13 29 12 20 16 --- 9 | 34 39 36 52 39 29 35 --- 37
R24 | 1145 26 24 10 24 25 65 21 --- 13 | 55 58 52 52 30 30 41 --- 41
XR26 | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 28 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1342 27 30 23 17 25 30 22 131 |T 51 54 48 48 72 46 43 81 44
WRMS | 1342 27 28 23 14 18 26 22 131 |NE 48 50 38 38 27 38 30 49 32
MEDI | 1067 24 26 17 16 23 24 20 139 |MD 54 56 41 40 38 40 31 94 35
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