[IGSREPORT-25796] Wk 1989 IGLOS Final Orbits
acc
acc at igs.org
Thu Mar 8 22:08:15 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1989 (Feb 18, 2018 - Feb 24, 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 2.1989.
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:
igl1989[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1989 in the SP3 format.
igl19897.sum Combination Report for GPS Week 1989.
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 | 0.2 ns
1 | 1.1 ns
2 | -8.4 ns
3 | -7.1 ns
4 | -7.5 ns
5 | -8.9 ns
6 | -7.5 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 1.1989, 1a.1989).
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 2.1989.0-6)
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 3.1989.0-6).
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 1989 summary. (Feb 18, 2018 - Feb 24, 2018)
Table 1.1989.a GPS week : 1989 MJD: 58167.0-58173.0
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 -7 -14 1 36 .09 37 35 | -640 -481 3370 9944
| 0 0 1 38 24 31 .02 | 3810 1502
cof n/a| 0 0 -10 -13 21 26 .11 39 37 | -647 -470 3371 9944
| 1 1 2 39 28 41 .04 | 3813 1497
emx n/a| 0 0 2 5 16 -2 .11 23 23 | -13644 317 3353 9393
| 1 0 2 20 12 42 .03 | 6805 1376
esx n/a| 0 0 0 -4 4 19 .12 18 16 | -8820 -1519 3358 12203
| 0 0 1 14 13 40 .03 | 8517 1515
gfz n/a| -1 0 3 3 30 3 .18 27 25 | 0 -459 3349 9893
| 1 1 3 24 16 18 .06 | 0 1678
grg n/a| 0 0 2 -78 -12 -34 -.37 30 27 | -5250 -311 3358 9264
| 1 1 3 17 22 61 .02 | 3676 1679
iac n/a| 1 0 -2 64 -25 -31 -.16 20 21 | -4357 111 3355 9388
| 0 1 2 40 25 34 .05 | 3898 1224
mcc n/a| 1 2 22 99 31 231 -.34 230 230 | --- --- --- ---
| 4 8 37 188 84 524 .49 | --- ---
Table 1.1989.b GPS week : 1989 MJD: 58167.0-58173.0
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 13 14 11 12 13 12 |
R02 | 8 7 9 8 8 7 7 |
R03 | 10 9 9 10 10 10 9 |
R04 | 10 10 9 11 9 9 8 |
R05 | 11 14 13 16 12 14 13 |
R06 | 8 8 10 9 8 8 8 |
R07 | 11 10 11 10 10 11 8 |
R08 | 8 9 9 8 8 10 9 |
R09 | 8 6 6 6 7 8 7 |
R10 | 7 10 8 9 9 7 8 |
R11 | 11 12 7 8 7 7 7 |
R13 | 7 9 9 7 8 11 9 |
R14 | 9 9 10 11 8 10 10 |
R15 | 15 16 18 19 15 16 18 |
R16 | 16 13 14 14 12 13 13 |
R17 | 9 9 9 9 9 9 10 |
R18 | 7 8 8 6 9 8 9 |
R19 | 12 14 12 13 11 11 11 |
R20 | 12 15 19 19 17 16 17 |
R21 | 10 8 10 11 12 11 9 |
R22 | 11 9 9 10 12 10 10 |
R23 | 10 8 8 9 7 10 9 |
R24 | 24 19 14 16 13 20 18 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1989.c GPS week : 1989 MJD: 58167.0-58173.0
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 1989 0 | -20 7 -52 261 -696 100 82.0 1082 1082 | 242 0
brd 1989 1 | -4 -42 -11 -276 -1016 -966 83.0 1277 1277 | 1097 0
brd 1989 2 | 9 45 -51 -990 -1626 -726 83.5 1388 1388 | -8409 0
brd 1989 3 | -8 -27 -54 -1218 -2147 -1076 84.9 1274 1274 | -7055 0
brd 1989 4 | 7 62 -43 -1630 -677 -3180 83.4 1219 1219 | -7494 0
brd 1989 5 | -40 -62 -40 -1062 702 -3304 83.4 1083 1083 | -8904 0
brd 1989 6 | 7 68 -75 -375 556 -3906 84.1 1242 1242 | -7493 0
-------------+------------------------------------------------------------+----------------
brd 1989 mean| -7 7 -46 -755 -700 -1865 83.5 1223 1223 | -5430 0
brd 1989 sdev| 18 52 19 650 1048 1557 .9 109 109 | 4220 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 2.1989.0 GPS week: 1989 Day: 0 MJD: 58167
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 -7 -19 19 80 .09 40 39 | 3509 -114 3296 10241
cof n/a| 1 0 -10 12 71 4 .10 42 39 | 3504 -115 3295 10243
emx n/a| 0 0 1 29 30 -81 .07 25 25 | -9091 912 3241 9676
esx n/a| 0 0 2 -19 21 43 .13 18 16 | -17142 -1445 3258 12866
gfz n/a| 0 0 5 0 32 18 .23 29 26 | 0 -128 3248 10209
grg n/a| 0 1 2 -73 -3 30 -.38 31 27 | 226 -107 3238 9388
iac n/a| 0 0 -1 72 -47 -19 -.22 20 20 | 295 -159 3246 9639
mcc n/a| -2 2 -44 -120 -85 893 -.99 205 205 | --- --- --- ---
Table 2.1989.1 GPS week: 1989 Day: 1 MJD: 58168
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 -7 -3 16 -6 .09 37 35 | 6126 1339 3185 9378
cof n/a| 0 1 -11 -25 41 39 .05 40 37 | 6124 1338 3181 9381
emx n/a| 0 -1 1 16 22 -25 .10 20 20 | -14147 2152 3181 8976
esx n/a| 0 2 0 -10 -13 77 .16 19 17 | -4423 1337 3178 11997
gfz n/a| -1 2 7 10 29 0 .15 29 25 | 0 1331 3177 9337
grg n/a| 2 0 2 -94 -21 -11 -.41 27 23 | 33 2022 3181 8716
iac n/a| 1 1 -3 79 -4 -52 -.15 23 23 | 2252 953 3194 8906
mcc n/a| 5 1 43 47 -30 -504 -.30 239 239 | --- --- --- ---
Table 2.1989.2 GPS week: 1989 Day: 2 MJD: 58169
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 -91 -41 36 .13 37 38 | -2624 -2126 3288 10331
cof n/a| 0 -2 -11 -88 -18 -21 .16 37 37 | -2644 -2098 3291 10332
emx n/a| 0 0 0 -20 2 -5 .09 23 23 | -11680 -901 3274 9955
esx n/a| 0 0 0 -16 -2 -49 .10 19 18 | -4189 -2606 3274 12253
gfz n/a| -2 -1 7 -31 1 -34 .12 28 27 | 0 -1999 3262 10217
grg n/a| 0 -1 -3 -73 -21 33 -.35 28 25 | -7264 -2194 3280 9468
iac n/a| 1 0 1 125 -7 32 -.09 20 20 | -6572 -1271 3284 9895
mcc n/a| 2 -7 54 394 -1 -16 -.45 197 197 | --- --- --- ---
Table 2.1989.3 GPS week: 1989 Day: 3 MJD: 58170
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 8 -2 57 .09 37 38 | -2791 646 3022 9988
cof n/a| -2 -2 -6 -1 25 102 .08 41 40 | -2798 654 3024 9986
emx n/a| 1 -1 0 -7 19 7 .15 26 26 | -10465 1351 3007 9349
esx n/a| 1 1 0 20 21 -2 .07 17 16 | -11034 -886 3011 12389
gfz n/a| -2 -1 0 30 56 11 .18 29 24 | 0 1021 3007 9987
grg n/a| -2 -1 8 -63 20 -30 -.35 33 28 | -7357 794 3013 9099
iac n/a| 1 0 -1 -1 -64 -32 -.12 19 19 | -6011 755 2999 9468
mcc n/a| 5 -5 60 204 11 630 -.14 265 265 | --- --- --- ---
Table 2.1989.4 GPS week: 1989 Day: 4 MJD: 58171
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 -6 -21 32 54 .07 35 33 | -2545 180 3388 10272
cof n/a| 0 0 -10 -9 14 -2 .12 35 32 | -2556 206 3390 10273
emx n/a| -1 -1 5 16 2 1 .12 21 21 | -28230 742 3375 9651
esx n/a| 0 0 -3 6 4 18 .12 16 16 | -12396 -1609 3384 12059
gfz n/a| 0 -3 4 12 35 0 .28 28 29 | 0 371 3383 10219
grg n/a| 0 1 4 -77 -1 -75 -.36 29 26 | -7570 370 3375 9712
iac n/a| 1 1 -2 26 -9 -21 -.23 19 19 | -6777 302 3370 9680
mcc n/a| 6 14 35 -89 147 727 -.62 289 289 | --- --- --- ---
Table 2.1989.5 GPS week: 1989 Day: 5 MJD: 58172
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 -9 31 -13 32 .05 36 34 | -2892 -2863 3880 9723
cof n/a| 0 2 -12 -20 13 48 .10 40 36 | -2895 -2855 3882 9724
emx n/a| 0 0 4 21 31 33 .11 24 24 | -13744 -1841 3881 9079
esx n/a| -1 0 0 -6 0 3 .09 17 16 | -18416 -3481 3881 12067
gfz n/a| -3 0 1 -28 39 22 .10 23 21 | 0 -3348 3857 9675
grg n/a| 0 3 2 -110 -51 -47 -.37 33 30 | -7376 -2804 3886 9458
iac n/a| 2 2 -4 80 -43 -52 -.15 23 23 | -6906 -1609 3873 9155
mcc n/a| -3 0 6 246 133 -194 -.49 203 203 | --- --- --- ---
Table 2.1989.6 GPS week: 1989 Day: 6 MJD: 58173
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 -9 -3 2 -2 .09 36 31 | -3263 -434 3534 9677
cof n/a| 0 1 -12 37 4 16 .14 40 35 | -3266 -423 3538 9675
emx n/a| -1 0 4 -16 8 49 .12 22 22 | -8152 -193 3517 9066
esx n/a| 1 0 0 -8 -3 43 .12 18 15 | 5859 -1944 3524 11790
gfz n/a| -2 -1 1 27 19 7 .22 24 21 | 0 -465 3509 9610
grg n/a| 0 0 0 -59 -8 -139 -.38 31 28 | -7442 -262 3534 9007
iac n/a| 1 1 -4 67 -3 -75 -.18 22 22 | -6780 1811 3519 8974
mcc n/a| -2 14 0 12 47 86 .59 214 214 | --- --- --- ---
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 3.1989.0 GPS week: 1989 Day: 0 MJD: 58167
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 | 551 66 67 27 15 30 42 22 --- 14 | 89 93 44 46 44 59 39 --- 43
R02 | 1147 25 26 19 14 25 19 14 168 8 | 111 113 99 104 90 102 98 106 99
R03 | 1439 41 45 19 14 28 21 16 106 9 | 116 120 87 92 81 94 83 65 88
R04 | 599 41 47 13 15 24 27 25 --- 10 | 159 162 132 149 142 128 133 --- 138
R05 | 685 57 59 15 20 22 16 19 --- 10 | 88 90 48 55 57 54 52 --- 53
R06 | 1356 26 33 17 11 22 31 8 --- 8 | 89 97 76 85 67 77 77 --- 77
R07 | 1154 48 52 26 7 38 19 11 345 10 | 99 100 76 68 57 58 60 281 65
R08 | 508 33 29 11 12 27 15 19 --- 8 | 91 94 72 80 62 77 68 --- 73
R09 | 1552 24 23 15 17 14 14 17 --- 7 | 27 28 20 27 27 22 27 --- 21
R10 | 1027 17 13 18 14 15 15 14 --- 7 | 58 56 48 64 44 47 56 --- 52
R11 | 523 38 28 18 19 30 30 23 176 11 | 311 311 306 313 314 305 290 194 305
R13 | 1556 13 14 15 19 11 16 10 --- 6 | 56 56 43 66 50 48 52 --- 51
R14 | 509 35 35 16 13 27 17 22 --- 9 | 70 70 49 53 40 58 39 --- 48
R15 | 1543 75 70 25 12 31 33 30 --- 14 | 92 90 45 26 36 54 24 --- 33
R16 | 565 48 64 29 34 30 46 24 --- 15 | 50 59 56 77 53 52 65 --- 58
R17 | 697 23 19 14 12 41 20 18 --- 9 | 21 22 19 23 33 20 19 --- 18
R18 | 1030 18 16 11 14 22 20 12 --- 7 | 16 20 19 24 17 25 14 --- 17
R19 | 954 46 49 33 26 31 18 15 --- 12 | 28 32 25 21 31 17 19 --- 17
R20 | 1848 18 28 43 12 15 44 12 --- 12 | 31 53 59 27 38 28 25 --- 27
R21 | 680 39 38 18 7 36 19 21 147 10 | 20 21 20 18 22 17 18 115 16
R22 | 649 37 36 18 11 44 19 27 --- 11 | 22 25 21 20 30 20 19 --- 17
R23 | 939 18 24 11 27 21 34 18 --- 10 | 16 22 17 32 30 37 22 --- 22
R24 | 1482 49 61 72 32 40 81 31 --- 23 | 45 61 59 39 26 22 17 --- 29
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 43 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1081 40 42 25 18 28 31 20 205 |T 74 78 62 65 60 61 56 152 58
WRMS | 1081 39 39 25 16 26 27 20 205 |NE 74 78 62 65 60 61 56 152 58
MEDI | 954 37 35 18 14 27 20 18 168 |MD 58 61 48 53 44 52 39 115 43
Table 3.1989.1 GPS week: 1989 Day: 1 MJD: 58168
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 | 501 67 88 21 12 37 26 20 --- 13 | 74 92 41 40 37 48 36 --- 38
R02 | 1589 24 27 13 12 19 15 10 227 6 | 118 119 109 114 113 116 118 120 114
R03 | 1294 42 35 15 15 30 15 15 130 9 | 110 106 100 93 91 105 95 58 97
R04 | 562 34 40 16 13 29 21 23 --- 9 | 151 156 136 157 151 142 144 --- 145
R05 | 924 47 55 18 14 41 32 40 --- 13 | 83 98 74 96 83 83 64 --- 78
R06 | 1027 19 31 17 18 17 20 20 --- 8 | 87 94 80 93 83 84 72 --- 82
R07 | 2025 47 42 16 13 30 19 21 165 10 | 98 95 86 90 90 77 77 171 84
R08 | 629 32 36 12 12 25 20 21 --- 8 | 91 97 92 93 81 95 76 --- 87
R09 | 1520 22 26 15 11 15 16 8 --- 6 | 26 28 27 20 26 19 21 --- 20
R10 | 913 11 15 21 27 20 26 12 --- 9 | 45 46 45 57 37 27 43 --- 41
R11 | 846 30 27 14 16 23 25 42 434 11 | 349 361 346 356 357 353 328 123 348
R13 | 674 13 23 16 26 19 25 17 --- 9 | 37 44 37 49 38 30 39 --- 36
R14 | 560 36 40 11 13 25 20 19 --- 8 | 58 58 41 52 38 59 44 --- 47
R15 | 3285 74 76 22 22 32 31 39 --- 15 | 61 61 37 39 37 50 34 --- 35
R16 | 714 36 37 13 30 29 43 19 --- 12 | 43 53 60 62 51 44 52 --- 51
R17 | 821 24 31 14 15 23 17 25 --- 8 | 21 25 22 28 26 18 19 --- 18
R18 | 868 21 25 9 17 29 20 10 --- 7 | 20 27 19 30 25 29 21 --- 21
R19 | 1276 49 47 30 22 54 15 17 --- 13 | 21 24 24 27 28 18 19 --- 17
R20 | 1530 20 19 42 23 36 41 21 --- 14 | 37 50 52 54 64 28 32 --- 38
R21 | 743 24 27 12 9 21 18 21 48 7 | 16 20 20 25 40 16 22 84 19
R22 | 1324 28 33 11 16 26 16 25 --- 8 | 17 18 22 20 23 25 18 --- 17
R23 | 1488 13 13 11 23 16 18 13 --- 7 | 17 20 21 31 24 25 20 --- 22
R24 | 686 45 42 42 37 31 62 22 --- 18 | 40 37 36 46 30 21 18 --- 23
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 38 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1277 37 40 20 19 29 27 23 239 |T 70 75 66 72 68 65 60 111 63
WRMS | 1277 35 37 20 17 25 23 23 239 |NE 70 75 66 72 68 65 60 111 63
MEDI | 913 30 33 15 16 26 20 20 165 |MD 45 53 41 52 38 44 38 120 38
Table 3.1989.2 GPS week: 1989 Day: 2 MJD: 58169
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 | 526 70 64 25 11 40 24 14 --- 13 | 70 64 40 28 35 31 23 --- 25
R02 | 1753 28 25 14 17 21 17 20 191 8 | 119 122 113 126 107 112 107 60 113
R03 | 1566 38 44 18 11 20 25 12 67 8 | 89 95 72 66 57 71 58 36 65
R04 | 714 37 27 17 13 19 17 22 --- 9 | 122 113 102 104 96 104 80 --- 98
R05 | 599 46 42 21 20 36 31 28 --- 13 | 84 96 68 70 66 72 65 --- 65
R06 | 1176 17 26 18 15 22 23 27 --- 9 | 83 81 82 87 82 77 78 --- 80
R07 | 1691 53 58 21 10 25 20 15 310 10 | 90 96 80 66 68 48 50 204 63
R08 | 679 38 40 18 11 30 16 17 --- 9 | 75 80 62 57 44 61 42 --- 53
R09 | 2968 16 19 15 13 17 13 10 --- 6 | 15 15 20 18 25 13 19 --- 14
R10 | 1169 11 16 17 21 19 20 13 --- 8 | 39 44 36 53 31 35 47 --- 40
R11 | 815 22 23 14 9 24 15 12 236 7 | 177 174 177 171 167 165 171 108 171
R13 | 717 13 19 19 18 22 21 21 --- 8 | 39 46 34 42 28 25 48 --- 35
R14 | 487 37 36 21 12 34 20 19 --- 10 | 46 47 34 35 28 34 24 --- 28
R15 | 3832 75 71 32 28 44 41 35 --- 18 | 70 68 46 41 48 57 35 --- 38
R16 | 745 23 23 34 31 16 51 15 --- 14 | 55 70 45 67 51 46 50 --- 50
R17 | 845 38 34 20 17 20 16 16 --- 9 | 18 26 19 33 17 25 16 --- 19
R18 | 546 25 24 18 22 17 14 7 --- 7 | 20 24 19 44 31 30 23 --- 25
R19 | 849 46 47 24 13 31 18 31 --- 12 | 23 26 19 25 21 20 23 --- 16
R20 | 880 24 29 53 28 34 70 21 --- 19 | 25 35 61 38 35 39 18 --- 24
R21 | 647 27 25 17 16 40 18 14 32 9 | 19 27 23 21 32 26 28 53 21
R22 | 1373 30 25 17 16 23 17 20 --- 8 | 19 22 25 24 33 24 20 --- 20
R23 | 728 7 11 14 26 15 18 12 --- 8 | 19 22 20 24 27 17 19 --- 17
R24 | 877 36 41 19 25 38 46 22 --- 13 | 37 44 44 29 27 19 16 --- 21
XR26 | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 36 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1388 37 37 23 19 28 28 20 197 |T 58 62 53 55 50 50 45 92 47
WRMS | 1388 38 37 23 18 27 25 20 197 |NE 58 62 53 55 50 50 45 92 47
MEDI | 845 30 27 18 16 23 20 16 191 |MD 46 47 44 42 35 35 35 60 35
Table 3.1989.3 GPS week: 1989 Day: 3 MJD: 58170
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 | 893 56 64 20 10 26 28 18 --- 11 | 71 75 27 38 31 24 25 --- 29
R02 | 1487 25 29 20 8 28 11 15 116 7 | 116 118 105 109 101 110 114 66 109
R03 | 901 44 42 23 10 28 16 15 154 9 | 123 122 106 112 113 122 115 37 113
R04 | 656 38 44 16 14 28 38 17 --- 10 | 145 145 122 130 111 117 135 --- 127
R05 | 1014 42 43 23 24 36 65 30 --- 16 | 100 93 93 100 89 81 94 --- 91
R06 | 1304 22 22 17 14 20 33 18 --- 9 | 101 106 105 113 97 125 107 --- 108
R07 | 1321 49 47 18 10 32 15 13 454 9 | 122 123 106 106 107 92 103 272 104
R08 | 672 28 34 19 11 18 25 15 --- 8 | 119 123 107 112 111 118 100 --- 109
R09 | 3473 17 19 16 7 15 23 10 --- 6 | 20 19 17 22 25 28 22 --- 17
R10 | 956 12 19 17 21 29 26 8 --- 8 | 38 35 32 52 41 40 38 --- 39
R11 | 1510 25 25 11 13 28 20 14 324 7 | 130 133 125 121 116 104 114 129 118
R13 | 714 17 18 16 15 12 15 16 --- 7 | 47 44 39 51 38 44 36 --- 41
R14 | 523 40 37 22 17 32 17 20 --- 10 | 62 60 48 55 47 48 35 --- 45
R15 | 2539 81 86 41 27 50 30 35 --- 18 | 73 76 44 18 32 38 28 --- 22
R16 | 468 26 31 31 34 14 42 22 --- 13 | 67 76 52 74 56 54 62 --- 60
R17 | 803 30 35 14 15 21 15 23 --- 8 | 20 19 16 17 15 16 11 --- 11
R18 | 509 14 17 12 9 17 21 13 --- 6 | 17 19 15 20 17 28 15 --- 14
R19 | 1200 50 52 27 17 41 28 24 --- 13 | 18 19 22 29 34 20 23 --- 19
R20 | 980 37 36 63 17 40 66 22 --- 18 | 24 32 50 39 44 32 26 --- 32
R21 | 787 37 49 28 14 47 15 10 55 11 | 18 23 19 25 33 19 20 33 16
R22 | 813 40 37 24 13 22 26 13 --- 9 | 20 22 20 20 25 27 21 --- 18
R23 | 633 13 16 16 24 19 18 15 --- 8 | 17 21 16 29 30 28 14 --- 18
R24 | 684 27 51 36 26 34 73 15 --- 16 | 30 40 44 40 40 24 14 --- 26
XR26 | ---- --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 45 --- 45
------+---------------------------------------------------+-----------------------------------------------
RMS | 1274 37 41 26 17 29 33 19 265 |T 65 67 57 62 58 58 54 107 55
WRMS | 1274 38 40 26 16 24 28 19 265 |NE 65 67 57 62 58 58 54 107 55
MEDI | 893 30 36 20 14 28 25 15 154 |MD 62 60 44 51 41 40 35 66 39
Table 3.1989.4 GPS week: 1989 Day: 4 MJD: 58171
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 | 960 56 50 19 17 33 29 20 --- 12 | 61 56 30 33 40 28 28 --- 28
R02 | 861 23 25 16 11 24 25 15 147 8 | 89 90 81 91 78 92 85 134 85
R03 | 522 45 45 17 13 24 30 17 105 10 | 81 79 56 67 57 34 57 36 57
R04 | 857 42 43 17 9 31 16 10 --- 9 | 87 89 65 67 62 68 61 --- 65
R05 | 1721 36 34 18 16 24 37 28 --- 11 | 86 87 79 82 81 70 77 --- 76
R06 | 2466 17 23 21 17 19 23 11 --- 8 | 66 66 61 82 62 71 79 --- 71
R07 | 2112 44 40 20 13 29 20 17 463 10 | 80 77 61 58 53 56 58 406 57
R08 | 859 29 26 12 14 23 9 15 --- 7 | 78 76 58 67 57 57 58 --- 60
R09 | 1654 22 25 11 13 11 13 15 --- 6 | 17 22 10 18 22 16 18 --- 12
R10 | 652 11 12 17 24 15 24 12 --- 8 | 38 33 43 49 36 31 34 --- 37
R11 | 1685 17 15 10 12 19 15 15 407 6 | 184 183 183 189 188 186 182 177 185
R13 | 1170 16 13 19 20 21 13 14 --- 8 | 35 40 29 42 39 36 40 --- 34
R14 | 526 31 29 15 12 19 15 19 --- 8 | 53 53 37 44 36 44 30 --- 38
R15 | 2145 76 73 24 19 32 25 35 --- 15 | 76 76 40 45 37 46 39 --- 40
R16 | 656 16 33 37 18 19 41 20 --- 12 | 55 71 42 60 49 55 45 --- 49
R17 | 580 33 32 9 10 36 16 16 --- 8 | 17 16 16 18 21 16 17 --- 14
R18 | 907 19 21 12 12 25 33 17 --- 8 | 17 21 16 18 24 39 16 --- 16
R19 | 653 46 38 25 23 27 14 16 --- 11 | 17 26 16 27 19 17 17 --- 14
R20 | 749 33 50 40 16 59 62 21 --- 17 | 28 52 35 25 46 23 33 --- 25
R21 | 946 33 31 16 17 42 23 28 77 11 | 15 15 20 24 32 24 18 40 15
R22 | 682 39 42 25 12 42 24 21 --- 11 | 15 16 19 20 29 20 17 --- 14
R23 | 637 13 20 16 19 9 21 12 --- 7 | 18 29 20 25 23 19 13 --- 16
R24 | 809 17 21 28 14 19 64 16 --- 13 | 35 44 45 31 26 19 15 --- 25
XR26 | ---- --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 34 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1219 35 35 21 16 28 29 19 289 |T 54 57 46 51 48 46 44 158 44
WRMS | 1219 33 32 21 16 29 26 19 289 |NE 54 57 46 51 48 46 44 158 44
MEDI | 859 31 31 17 14 24 23 16 147 |MD 53 53 40 44 39 36 34 134 36
Table 3.1989.5 GPS week: 1989 Day: 5 MJD: 58172
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 | 584 64 66 26 12 32 27 21 --- 13 | 62 65 41 39 43 33 31 --- 34
R02 | 980 28 26 12 9 16 21 11 119 7 | 64 62 54 53 45 48 48 73 50
R03 | 573 49 53 17 10 23 23 18 75 10 | 90 90 73 73 76 65 74 69 72
R04 | 1432 40 35 17 7 26 17 12 --- 8 | 89 89 71 71 70 78 69 --- 72
R05 | 1003 38 67 24 19 35 45 29 --- 13 | 88 107 85 84 79 88 89 --- 82
R06 | 1377 13 23 20 17 18 16 14 --- 7 | 91 94 90 95 95 95 100 --- 93
R07 | 1776 41 46 16 10 28 27 24 409 10 | 116 122 101 106 102 93 83 355 99
R08 | 1080 29 27 16 14 27 28 22 --- 9 | 112 110 102 102 93 102 100 --- 100
R09 | 1324 21 20 14 17 17 20 13 --- 7 | 21 21 18 18 22 28 24 --- 17
R10 | 871 11 19 10 12 11 23 19 --- 6 | 42 48 38 46 49 39 43 --- 41
R11 | 556 21 21 12 14 18 11 12 128 6 | 103 102 101 112 109 106 107 227 106
R13 | 896 17 15 19 34 14 33 10 --- 10 | 38 40 35 68 44 41 48 --- 46
R14 | 625 37 40 15 16 25 25 21 --- 10 | 51 53 36 40 35 42 34 --- 36
R15 | 1519 76 74 22 19 24 33 38 --- 15 | 64 62 39 29 46 36 26 --- 33
R16 | 624 14 21 36 22 20 36 31 --- 12 | 38 43 38 45 37 41 41 --- 36
R17 | 739 29 38 10 12 23 25 18 --- 8 | 13 21 17 23 22 24 14 --- 13
R18 | 715 21 23 12 14 14 21 19 --- 7 | 13 14 16 18 17 20 15 --- 12
R19 | 905 42 50 23 15 21 20 23 --- 10 | 22 26 23 26 29 28 21 --- 21
R20 | 1904 34 24 53 14 21 61 16 --- 16 | 30 25 33 29 33 27 24 --- 20
R21 | 1104 41 43 26 10 29 23 24 56 11 | 14 18 22 21 22 29 20 30 17
R22 | 763 28 27 20 19 25 26 21 --- 10 | 14 16 18 26 25 21 14 --- 14
R23 | 817 15 15 24 23 21 31 19 --- 10 | 15 17 20 23 27 44 30 --- 21
R24 | 1164 43 57 43 26 18 79 45 --- 19 | 58 77 40 34 40 31 19 --- 23
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 22 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1082 36 40 24 17 23 33 23 203 |T 54 57 48 51 50 50 45 150 45
WRMS | 1082 34 36 24 16 21 30 23 203 |NE 54 57 48 51 50 50 45 150 45
MEDI | 905 29 27 19 14 21 25 19 119 |MD 51 53 38 40 43 41 31 73 34
Table 3.1989.6 GPS week: 1989 Day: 6 MJD: 58173
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 | 521 64 74 22 7 31 25 20 --- 12 | 77 85 37 34 34 39 27 --- 32
R02 | 1034 22 30 14 10 18 19 11 96 6 | 69 74 50 59 44 56 48 65 52
R03 | 826 44 47 19 8 22 19 14 220 9 | 95 96 62 67 69 67 58 54 65
R04 | 1474 34 43 15 8 22 24 10 --- 8 | 92 97 66 65 52 71 58 --- 64
R05 | 650 51 48 28 11 24 31 34 --- 13 | 97 100 93 81 72 82 78 --- 79
R06 | 766 18 16 19 16 17 12 17 --- 7 | 92 93 76 91 82 94 94 --- 87
R07 | 1189 40 36 11 10 23 16 16 384 8 | 124 124 100 100 92 99 86 344 97
R08 | 2274 28 33 20 13 22 21 18 --- 8 | 107 109 89 94 78 94 82 --- 88
R09 | 1696 22 25 16 8 24 18 11 --- 7 | 23 25 16 17 25 22 20 --- 16
R10 | 667 16 20 10 15 23 21 16 --- 7 | 60 60 52 65 48 50 58 --- 55
R11 | 556 23 29 13 12 12 8 18 132 6 | 169 171 160 173 171 167 166 208 167
R13 | 1620 9 10 14 26 16 25 15 --- 8 | 50 49 45 68 46 39 54 --- 51
R14 | 652 38 40 16 19 30 19 21 --- 10 | 79 82 53 62 41 52 44 --- 52
R15 | 2501 71 79 30 18 45 43 47 --- 18 | 96 100 54 38 51 67 27 --- 43
R16 | 610 36 47 29 29 19 35 16 --- 12 | 45 48 47 73 50 43 54 --- 52
R17 | 627 37 31 22 15 22 17 24 --- 9 | 20 22 23 22 25 20 16 --- 16
R18 | 508 19 22 14 21 13 31 18 --- 9 | 16 20 16 22 18 38 19 --- 15
R19 | 1014 37 37 24 18 23 18 33 --- 11 | 25 27 25 42 33 23 16 --- 24
R20 | 2038 22 36 39 32 35 63 22 --- 17 | 25 33 27 43 29 22 22 --- 22
R21 | 538 33 34 21 10 16 15 28 83 9 | 17 17 15 24 18 18 22 30 16
R22 | 579 35 42 18 9 33 18 24 --- 9 | 18 21 15 19 26 21 17 --- 15
R23 | 1046 15 18 17 28 17 20 13 --- 9 | 15 20 18 29 28 28 19 --- 21
R24 | 1677 41 42 34 22 28 83 20 --- 18 | 43 39 41 29 25 33 22 --- 23
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 41 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1242 36 40 22 18 24 31 22 214 |T 63 65 51 57 50 54 47 140 49
WRMS | 1242 31 35 22 15 21 28 22 214 |NE 63 65 51 57 50 54 47 140 49
MEDI | 826 34 36 19 15 22 20 18 132 |MD 60 60 47 59 44 43 41 65 43
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