[IGSREPORT-28556] Wk 2199 IGLOS Final Orbits
acc
acc at igs.org
Mon Mar 21 22:57:34 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2199 (Feb 27, 2022 - Mar 05, 2022)
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 2.2199.
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:
igl2199[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2199 in the SP3 format.
igl21997.sum Combination Report for GPS Week 2199.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | 3.0 ns
1 | -0.7 ns
2 | -0.8 ns
3 | 0.4 ns
4 | 1.7 ns
5 | -1.1 ns
6 | 0.7 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 1.2199, 1a.2199).
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 2.2199.0-6)
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 3.2199.0-6).
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 2199 summary. (Feb 27, 2022 - Mar 05, 2022)
Table 1.2199.a GPS week : 2199 MJD: 59637.0-59643.0
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 22 66 .15 28 22 | 39743 773 3302 8586
| 1 1 1 15 7 34 .05 | 1282 2694
emx n/a| 0 1 -15 -3 5 10 -.02 41 35 | -684 1113 3312 8553
| 2 1 2 22 38 34 .06 | 12701 2098
esx n/a| 0 0 -1 3 -24 -35 -.03 28 21 | 6169 55 3297 9001
| 1 1 1 25 4 18 .04 | 8433 2632
gfz n/a| 0 0 4 -15 5 -17 -.13 29 16 | 0 694 3261 8271
| 1 1 2 26 19 23 .06 | 0 2466
grg n/a| 3 -3 -6 -19 -10 36 .32 30 24 | -10 559 3298 8141
| 2 1 5 22 12 49 .07 | 379 2318
iac n/a| 0 1 2 29 20 -56 -.23 28 25 | 2126 505 3299 9154
| 1 3 2 29 32 117 .10 | 1135 1035
Table 1.2199.b GPS week : 2199 MJD: 59637.0-59643.0
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 | 17 19 21 21 21 16 16 |
R02 | 9 8 13 9 9 8 8 |
R03 | 9 9 9 10 10 9 10 |
R04 | 10 12 14 12 11 12 10 |
R05 | 11 7 10 10 9 12 11 |
R07 | 11 9 10 9 9 8 10 |
R08 | 9 12 9 12 10 8 10 |
R09 | 9 8 10 7 8 7 12 |
R11 | 7 9 9 8 10 8 7 |
R12 | 9 9 9 8 8 8 8 |
R13 | 13 20 13 14 16 18 11 |
R14 | 7 8 6 9 6 9 6 |
R15 | 6 5 9 6 9 7 8 |
R17 | 10 9 10 9 8 9 12 |
R18 | 10 9 10 10 8 8 8 |
R19 | 19 15 16 19 23 21 21 |
R20 | 31 28 25 27 28 32 30 |
R21 | 9 9 10 10 13 10 11 |
R22 | 24 24 22 22 22 21 26 |
R24 | 10 12 9 9 9 10 9 |
Table 1.2199.c GPS week : 2199 MJD: 59637.0-59643.0
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 2199 0 | -54 53 79 -1316 106 -770 80.1 1323 1323 | 2969 0
brd 2199 1 | 33 23 124 -1227 -602 1927 79.2 1390 1390 | -666 0
brd 2199 2 | -50 -10 164 -913 186 3877 81.7 1203 1203 | -806 0
brd 2199 3 | -62 -49 108 -1731 -1002 -516 82.1 1409 1409 | 446 0
brd 2199 4 | -24 11 89 -2252 -3161 -3464 77.9 1387 1387 | 1671 0
brd 2199 5 | 39 34 152 413 180 -5542 80.2 1243 1243 | -1054 0
brd 2199 6 | 107 -12 188 1333 -1518 -528 77.8 1277 1277 | 733 0
-------------+------------------------------------------------------------+----------------
brd 2199 mean| -1 7 129 -813 -830 -716 79.9 1318 1318 | 470 0
brd 2199 sdev| 63 34 40 1255 1219 3135 1.7 80 80 | 1471 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 2.2199.0 GPS week: 2199 Day: 0 MJD: 59637
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 4 12 11 51 .17 31 22 | 40312 5238 3704 7885
emx n/a| 0 1 -16 -36 10 15 -.12 41 34 | -7887 4103 3756 7935
esx n/a| -2 0 -2 31 -19 -64 -.04 27 21 | -2491 4843 3704 7307
gfz n/a| 0 0 8 -28 16 -48 -.03 33 17 | 0 4653 3748 7703
grg n/a| 3 -1 -6 -12 -15 -6 .31 28 21 | 331 4473 3705 7659
iac n/a| 2 0 4 32 -1 78 -.27 27 25 | 3917 1483 3731 8417
Table 2.2199.1 GPS week: 2199 Day: 1 MJD: 59638
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 8 4 21 58 .21 23 17 | 42306 -2195 3070 7998
emx n/a| -5 0 -14 -5 26 56 .02 46 41 | 2407 -1515 3069 7965
esx n/a| 0 -1 -2 29 -21 -26 .03 31 24 | 1007 -3000 3048 8112
gfz n/a| -1 0 1 34 8 -4 -.17 27 14 | 0 -2150 3002 7674
grg n/a| 6 -4 -12 -62 -6 18 .44 35 26 | 68 -1874 3064 7715
iac n/a| -1 5 4 -5 -26 -89 -.26 26 21 | 2423 -1233 3050 8549
Table 2.2199.2 GPS week: 2199 Day: 2 MJD: 59639
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 5 33 27 89 .15 23 17 | 39646 -1243 3016 8584
emx n/a| 0 1 -10 -3 -45 12 -.04 43 40 | 2558 -1241 3044 8435
esx n/a| 1 0 -2 10 -23 -35 -.01 28 20 | 792 -1833 3018 8087
gfz n/a| 0 0 1 -44 0 20 -.16 29 19 | 0 -1062 2985 8151
grg n/a| 5 -2 -2 -39 4 41 .37 29 27 | -438 -1164 3030 8013
iac n/a| -1 0 1 69 67 -113 -.30 28 27 | 765 406 3029 9246
Table 2.2199.3 GPS week: 2199 Day: 3 MJD: 59640
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 7 26 13 34 .19 28 23 | 38691 1258 3100 9093
emx n/a| 1 2 -18 -31 -36 28 .04 42 37 | 24283 1317 3132 9064
esx n/a| -2 -1 -1 9 -20 -50 -.02 28 18 | 9677 328 3092 11488
gfz n/a| -1 0 4 -31 28 -33 -.13 31 14 | 0 1014 3083 8594
grg n/a| 2 -1 0 -9 -27 77 .31 29 24 | -157 783 3103 8643
iac n/a| 1 -1 -1 36 57 -40 -.37 26 26 | 1378 1384 3095 9776
Table 2.2199.4 GPS week: 2199 Day: 4 MJD: 59641
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 19 30 24 .12 27 19 | 39665 2966 3275 8772
emx n/a| 1 0 -18 10 29 -43 -.01 39 31 | -2619 3219 3273 8792
esx n/a| 0 -3 0 2 -27 -15 -.04 32 22 | 61 1779 3275 6794
gfz n/a| -2 -1 2 -32 -8 -19 -.22 29 16 | 0 2997 3182 8544
grg n/a| 1 -2 0 -4 -11 -27 .32 28 22 | 64 2783 3260 8224
iac n/a| 0 4 5 2 20 66 -.12 28 24 | 3078 1546 3265 9423
Table 2.2199.5 GPS week: 2199 Day: 5 MJD: 59642
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 8 17 20 90 .09 31 26 | 38939 -1608 3447 8731
emx n/a| 1 5 -13 18 -9 -28 -.05 37 30 | -8360 448 3427 8621
esx n/a| 0 0 0 -42 -25 -43 -.10 27 18 | 14948 -1583 3451 10538
gfz n/a| 0 -1 4 -8 22 -35 -.12 29 15 | 0 -1367 3405 8507
grg n/a| 0 -4 -7 -2 4 36 .28 29 22 | -483 -1103 3452 8037
iac n/a| 0 4 3 8 7 -28 -.10 29 23 | 1076 -148 3449 9109
Table 2.2199.6 GPS week: 2199 Day: 6 MJD: 59643
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 8 -12 31 119 .10 30 27 | 38647 1001 3507 9045
emx n/a| 0 3 -15 21 60 32 .01 37 32 | -15175 1465 3489 9059
esx n/a| -1 1 0 -17 -30 -15 -.01 26 22 | 19190 -149 3495 10683
gfz n/a| 1 1 7 0 -26 -4 -.11 29 14 | 0 778 3422 8726
grg n/a| 2 -4 -14 -7 -23 118 .21 35 29 | 543 16 3475 8702
iac n/a| 0 -3 2 62 17 -265 -.15 29 31 | 2247 97 3478 9559
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 3.2199.0 GPS week: 2199 Day: 0 MJD: 59637
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 896 53 56 35 30 26 28 17 | 109 59 62 84 82 79 75
R02 | 1299 10 36 19 13 15 18 8 | 69 60 79 73 74 78 71
R03 | 1498 16 35 15 15 10 23 8 | 94 68 79 93 91 97 87
XR04 | 589 17 33 17 --- 20 14 10 | 109 84 96 --- 105 103 100
R05 | 1468 12 35 24 20 19 35 11 | 87 66 84 85 84 99 83
R07 | 1181 20 39 16 23 17 26 10 | 100 66 81 97 85 93 86
R08 | 1027 16 34 17 17 22 16 9 | 89 64 90 94 89 94 87
R09 | 633 17 15 10 21 28 21 8 | 50 55 52 48 56 56 50
XR11 | 2425 11 --- 14 14 13 17 7 | 47 --- 49 47 52 53 48
R12 | 967 24 18 21 15 16 24 9 | 58 56 61 60 40 52 52
R13 | 797 33 30 16 29 41 21 13 | 75 69 52 54 39 54 54
R14 | 501 7 10 16 17 12 18 6 | 46 43 50 38 48 51 45
R15 | 923 8 11 12 10 10 19 5 | 45 52 47 41 45 44 44
R17 | 718 16 37 12 13 19 36 10 | 56 35 43 55 49 65 49
R18 | 588 20 34 19 9 17 35 10 | 55 39 64 54 65 71 58
R19 | 3180 45 59 24 52 40 33 19 | 48 48 41 52 47 57 38
R20 | 1403 54 87 57 97 72 42 31 | 80 39 56 116 53 91 64
R21 | 1013 19 35 21 16 15 19 9 | 72 43 56 72 58 70 61
R22 | 2023 76 39 66 45 30 40 23 | 53 67 124 71 91 102 80
R24 | 1012 14 46 14 21 21 10 9 | 70 42 56 70 69 67 62
------+-----------------------------------------+-------------------------------------
RMS | 1323 31 41 27 33 28 27 |T 70 55 66 68 66 73 64
WRMS | 1323 22 34 21 17 21 25 |NE 70 55 66 68 66 73 64
MEDI | 1012 17 35 17 17 19 21 |MD 69 56 56 70 58 70 61
Table 3.2199.1 GPS week: 2199 Day: 1 MJD: 59638
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 856 47 64 53 17 35 31 19 | 76 43 57 40 37 72 49
R02 | 1725 7 27 17 13 22 22 7 | 42 35 47 28 50 34 37
R03 | 1288 9 38 19 15 22 23 9 | 59 41 48 61 62 69 56
XR04 | 1041 22 30 15 --- 22 31 12 | 68 51 62 --- 68 51 58
R05 | 1615 12 31 11 11 17 14 7 | 55 40 55 56 55 49 52
R07 | 1426 11 49 17 16 15 13 8 | 69 40 57 74 68 68 64
R08 | 548 14 42 26 33 12 25 11 | 59 37 62 82 61 51 58
R09 | 817 14 17 19 8 26 18 7 | 34 47 39 32 33 36 32
XR11 | 651 19 --- 16 17 18 19 9 | 27 --- 36 29 33 39 28
R12 | 1244 15 25 21 20 28 8 8 | 41 42 64 58 35 50 47
R13 | 612 33 51 18 23 86 38 19 | 51 71 47 40 23 49 38
R14 | 898 12 20 10 12 17 26 7 | 38 31 42 40 42 61 40
R15 | 1494 7 14 11 8 15 10 4 | 30 32 39 34 28 30 31
R17 | 746 5 43 16 22 21 20 9 | 32 21 32 50 42 48 36
R18 | 552 15 31 18 10 18 23 8 | 32 24 43 33 48 38 34
R19 | 2208 26 58 25 32 44 22 14 | 30 40 40 50 35 30 29
R20 | 2738 37 98 59 70 74 46 27 | 55 32 48 81 44 52 44
R21 | 600 16 39 20 13 16 17 8 | 45 25 31 39 44 40 37
R22 | 1575 48 45 73 53 19 50 23 | 36 50 63 43 44 51 33
R24 | 1658 16 55 21 24 26 26 12 | 46 27 37 54 57 52 43
------+-----------------------------------------+-------------------------------------
RMS | 1390 23 46 31 27 35 26 |T 46 38 47 48 45 48 42
WRMS | 1390 17 41 24 14 26 21 |NE 46 38 47 48 45 48 42
MEDI | 1041 15 39 18 17 21 22 |MD 42 40 47 43 44 49 38
Table 3.2199.2 GPS week: 2199 Day: 2 MJD: 59639
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 615 41 77 57 38 35 27 20 | 93 48 56 96 91 71 73
R02 | 1224 17 41 18 16 20 51 12 | 44 33 54 40 47 95 50
R03 | 532 14 38 15 12 30 13 9 | 68 41 47 52 84 49 57
XR04 | 1302 13 38 23 --- 32 33 13 | 75 50 63 --- 100 80 72
R05 | 1441 15 30 20 24 17 26 9 | 59 43 52 69 52 47 52
R07 | 1342 7 42 24 12 21 29 10 | 73 43 60 64 84 96 70
R08 | 1313 9 39 17 17 16 21 8 | 64 38 60 63 74 72 63
R09 | 1156 15 20 17 15 42 18 10 | 43 54 53 52 59 46 46
XR11 | 769 16 --- 18 15 21 21 9 | 33 --- 47 47 41 33 37
R12 | 1016 14 21 20 15 20 26 8 | 35 40 53 43 29 46 38
R13 | 1071 25 21 17 27 49 20 12 | 51 45 40 55 25 50 42
R14 | 835 7 19 9 12 15 16 5 | 31 32 32 38 30 41 32
R15 | 1727 8 17 15 21 13 37 9 | 33 37 28 25 36 58 32
R17 | 675 9 35 18 20 27 24 9 | 42 31 35 49 53 48 40
R18 | 895 16 26 16 15 33 22 9 | 40 31 45 36 63 37 39
R19 | 1510 42 56 22 39 26 28 16 | 38 50 36 37 39 35 27
R20 | 1011 31 79 59 81 49 30 25 | 60 28 51 92 63 61 54
R21 | 1120 19 34 17 21 24 16 9 | 49 37 44 54 43 42 43
R22 | 865 52 58 54 35 27 53 21 | 41 52 95 74 58 80 62
R24 | 2124 14 49 14 7 15 20 9 | 64 40 56 51 65 52 55
------+-----------------------------------------+-------------------------------------
RMS | 1202 23 43 28 29 29 28 |T 51 40 50 54 56 56 49
WRMS | 1202 17 40 20 19 27 27 |NE 51 40 50 54 56 56 49
MEDI | 1071 15 38 18 17 24 24 |MD 44 40 51 52 53 49 46
Table 3.2199.3 GPS week: 2199 Day: 3 MJD: 59640
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 662 42 75 57 38 40 28 21 | 103 43 55 97 96 67 72
R02 | 2036 11 40 15 13 15 26 9 | 50 26 57 59 52 69 52
R03 | 1106 9 42 15 14 22 31 10 | 73 44 66 65 82 86 69
XR04 | 1443 18 38 12 --- 26 25 11 | 75 43 66 --- 98 70 71
R05 | 1614 13 39 20 14 22 25 9 | 67 36 62 68 77 55 60
R07 | 1466 17 26 12 16 19 24 8 | 73 46 58 71 66 59 62
R08 | 1303 15 36 27 21 20 38 12 | 64 43 61 69 80 90 67
R09 | 719 16 12 10 14 17 19 6 | 24 24 23 22 28 27 19
XR11 | 677 15 --- 14 10 19 20 8 | 20 --- 42 33 35 41 32
R12 | 1131 21 13 11 15 14 22 7 | 33 45 45 41 40 52 40
R13 | 1307 30 17 32 22 48 22 13 | 57 63 57 69 38 59 53
R14 | 1458 9 13 11 10 26 32 8 | 36 33 29 30 31 54 30
R15 | 1414 12 13 9 11 16 14 5 | 41 41 29 30 30 39 33
R17 | 640 14 34 14 13 17 27 9 | 48 33 35 44 46 49 40
R18 | 1706 14 32 15 14 34 17 9 | 46 41 55 47 69 52 49
R19 | 1159 46 60 28 55 33 18 18 | 53 47 37 55 36 24 29
R20 | 1611 60 61 64 81 60 24 27 | 75 38 50 83 32 50 44
R21 | 748 14 39 19 12 12 28 9 | 55 27 36 51 56 65 48
R22 | 1796 55 71 39 53 39 41 22 | 67 53 114 138 104 106 94
R24 | 2182 18 45 12 17 12 16 9 | 63 34 51 60 64 55 54
------+-----------------------------------------+-------------------------------------
RMS | 1408 28 42 28 31 29 26 |T 56 40 51 59 58 58 50
WRMS | 1408 23 37 18 14 24 26 |NE 56 40 51 59 58 58 50
MEDI | 1307 15 38 15 14 20 24 |MD 55 41 51 59 52 55 49
Table 3.2199.4 GPS week: 2199 Day: 4 MJD: 59641
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1115 45 55 68 25 34 38 20 | 86 54 61 78 92 54 65
R02 | 3344 12 37 17 14 9 28 9 | 56 41 68 62 62 66 57
R03 | 1678 14 37 19 18 12 27 9 | 76 48 68 78 67 77 68
XR04 | 1654 15 32 16 --- 19 28 11 | 93 77 87 --- 85 92 85
R05 | 1119 11 29 18 12 24 18 8 | 71 64 71 75 89 60 70
R07 | 1657 20 26 14 9 16 28 8 | 79 59 63 69 69 62 65
R08 | 838 15 24 19 21 30 13 9 | 66 52 63 50 80 51 59
R09 | 818 14 20 13 14 14 24 7 | 61 72 51 54 62 57 57
R11 | 768 9 21 14 15 38 28 10 | 52 20 47 49 58 57 49
R12 | 1009 16 13 19 14 13 23 7 | 43 40 44 45 41 49 41
R13 | 731 37 28 33 35 43 28 15 | 43 52 59 59 42 36 45
R14 | 1355 11 17 14 13 13 15 6 | 41 38 43 40 37 38 37
R15 | 989 13 12 15 11 28 30 8 | 39 41 34 36 37 46 34
R17 | 690 15 29 12 16 11 25 8 | 46 34 41 41 46 48 40
R18 | 1332 12 26 13 20 21 14 8 | 56 39 52 45 59 53 48
R19 | 1430 43 84 47 54 29 42 22 | 63 62 44 76 72 60 53
R20 | 810 57 70 71 78 54 20 27 | 82 48 54 86 56 52 56
R21 | 756 12 41 21 14 24 45 12 | 55 44 48 54 49 76 51
R22 | 1281 50 56 54 44 45 39 21 | 69 69 109 93 107 102 85
R24 | 1947 15 32 14 20 14 25 9 | 59 49 59 64 61 58 56
------+-----------------------------------------+-------------------------------------
RMS | 1386 27 39 32 29 28 28 |T 61 50 58 60 63 59 56
WRMS | 1386 19 31 22 16 22 24 |NE 61 50 58 60 63 59 56
MEDI | 1115 15 29 17 16 21 27 |MD 59 48 54 59 61 57 56
Table 3.2199.5 GPS week: 2199 Day: 5 MJD: 59642
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1438 42 45 50 25 23 21 16 | 78 48 54 71 65 51 56
R02 | 2328 10 25 14 16 19 16 7 | 45 33 50 42 55 45 44
R03 | 1697 14 36 13 12 13 32 9 | 66 46 58 60 65 62 58
XR04 | 1981 12 36 13 --- 22 35 12 | 70 53 66 --- 76 70 65
R05 | 1362 20 27 35 14 28 20 11 | 63 51 84 67 51 59 60
R07 | 526 12 32 11 7 21 17 7 | 74 53 67 72 80 69 69
R08 | 1182 11 32 14 19 11 15 8 | 66 48 68 69 65 65 63
R09 | 846 12 17 10 13 14 19 6 | 40 52 48 43 49 45 45
R11 | 985 11 17 14 18 14 26 7 | 40 25 44 54 39 31 40
R12 | 1061 16 14 11 13 13 29 7 | 37 33 47 45 35 42 38
R13 | 870 35 26 27 42 63 28 18 | 44 38 33 40 49 39 35
R14 | 784 15 15 14 19 11 33 8 | 27 24 40 43 34 39 31
R15 | 1033 16 14 12 10 20 16 6 | 30 28 35 34 25 40 30
R17 | 929 19 29 16 17 11 30 9 | 45 39 34 42 43 52 39
R18 | 719 10 30 11 12 16 20 7 | 42 35 40 43 43 47 39
R19 | 1048 55 76 40 41 19 39 20 | 63 34 35 50 47 46 37
R20 | 1265 63 78 62 77 82 63 32 | 72 61 53 75 41 80 50
R21 | 648 21 34 15 20 24 23 10 | 49 36 48 52 46 50 44
R22 | 1296 74 33 48 46 22 40 21 | 41 66 87 70 77 84 67
R24 | 1999 19 35 13 23 21 25 10 | 48 44 45 52 45 49 43
------+-----------------------------------------+-------------------------------------
RMS | 1242 31 37 27 29 29 29 |T 52 42 51 53 51 53 47
WRMS | 1242 26 30 18 15 22 23 |NE 52 42 51 53 51 53 47
MEDI | 1048 16 30 14 18 19 25 |MD 45 39 48 52 47 49 44
Table 3.2199.6 GPS week: 2199 Day: 6 MJD: 59643
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1424 46 43 45 22 20 23 16 | 102 46 52 86 73 77 69
R02 | 2629 9 24 22 12 13 26 8 | 47 38 61 52 51 47 48
R03 | 1276 11 30 16 16 26 30 9 | 80 47 64 78 85 69 70
XR04 | 1299 9 30 16 --- 27 23 10 | 81 58 75 --- 93 78 76
R05 | 1241 22 31 30 21 26 12 11 | 64 45 83 84 58 71 68
R07 | 1147 9 34 17 11 26 28 9 | 92 67 80 88 97 103 86
R08 | 763 12 39 9 14 26 26 9 | 78 49 81 75 94 89 77
R09 | 722 10 21 17 18 21 55 11 | 55 62 55 56 59 75 56
R11 | 780 10 18 9 14 21 18 6 | 45 23 46 51 51 38 45
R12 | 1817 16 21 9 16 14 22 7 | 57 58 58 60 47 46 53
R13 | 1181 18 30 15 18 48 17 11 | 68 57 70 69 55 60 62
R14 | 565 11 15 8 18 7 14 5 | 47 46 54 52 50 46 48
R15 | 1155 17 15 11 10 16 35 8 | 51 49 51 47 54 59 48
R17 | 1106 13 34 12 11 51 34 12 | 75 65 64 65 67 82 66
R18 | 1457 9 33 13 11 17 18 7 | 57 44 59 50 61 55 53
R19 | 1096 56 67 35 32 39 49 20 | 67 52 39 51 45 46 39
R20 | 1696 49 74 62 90 69 29 29 | 89 56 48 106 45 86 61
R21 | 631 15 37 22 19 33 24 11 | 72 45 62 72 65 71 63
R22 | 1192 80 37 46 56 75 37 26 | 68 96 136 104 143 118 105
R24 | 483 16 36 10 10 22 18 8 | 65 39 56 64 63 47 55
------+-----------------------------------------+-------------------------------------
RMS | 1276 30 37 26 29 35 29 |T 68 52 64 68 67 68 62
WRMS | 1276 27 32 22 14 29 31 |NE 68 52 64 68 67 68 62
MEDI | 1155 13 31 16 16 26 24 |MD 67 49 59 65 59 69 61
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