[IGSREPORT-28871] Wk 2222 IGLOS Final Orbits
acc
acc at igs.org
Sun Aug 28 23:05:07 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2222 (Aug 07, 2022 - Aug 13, 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 2.2222.
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:
igl2222[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2222 in the SP3 format.
igl22227.sum Combination Report for GPS Week 2222.
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 | -2.1 ns
1 | -4.9 ns
2 | -5.3 ns
3 | -5.8 ns
4 | -2.9 ns
5 | -5.8 ns
6 | -5.9 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 1.2222, 1a.2222).
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 2.2222.0-6)
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 3.2222.0-6).
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 2222 summary. (Aug 07, 2022 - Aug 13, 2022)
Table 1.2222.a GPS week : 2222 MJD: 59798.0-59804.0
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 0 -21 -50 31 .09 26 19 | 24400 -229 3057 8642
| 1 1 1 14 18 29 .04 | 2362 2526
emx n/a| -2 2 8 28 0 -9 -.11 44 30 | -10814 -393 3078 8507
| 0 1 5 26 32 49 .07 | 9458 1771
esx n/a| 0 0 3 17 29 15 -.13 27 23 | -6331 546 3052 11662
| 0 1 1 13 7 28 .04 | 9380 2502
gfz n/a| 0 0 0 -4 0 30 -.06 24 16 | 0 -361 3102 8505
| 1 0 2 19 12 27 .08 | 0 2600
grg n/a| 1 -2 -7 6 19 -34 .41 24 21 | -4579 -383 3055 8153
| 1 1 2 13 12 69 .03 | 2144 2649
iac n/a| 0 0 3 -28 -24 -34 -.27 29 27 | -1843 -641 3104 10004
| 3 2 3 32 21 100 .15 | 1426 597
Table 1.2222.b GPS week : 2222 MJD: 59798.0-59804.0
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 | 20 20 17 16 18 16 19 |
R02 | 7 7 7 7 7 10 6 |
R03 | 8 6 7 8 8 9 10 |
R04 | 8 8 8 11 10 10 8 |
R05 | 7 9 8 8 8 9 9 |
R07 | 7 7 7 8 9 8 9 |
R08 | 7 9 7 7 9 7 7 |
R09 | 6 8 8 9 9 8 11 |
R11 | 8 8 7 8 9 9 9 |
R12 | 7 7 10 8 8 9 8 |
R13 | 17 12 15 17 12 14 15 |
R14 | 7 7 6 6 7 7 8 |
R15 | 6 7 7 8 8 7 8 |
R17 | 6 7 8 11 8 9 9 |
R18 | 8 10 10 13 9 10 9 |
R19 | 22 24 27 32 31 28 27 |
R20 | 22 23 24 22 25 28 27 |
R21 | 7 8 11 10 9 12 8 |
R24 | 10 11 10 8 10 12 11 |
R25 | --- --- 0 0 0 0 0 |
Table 1.2222.c GPS week : 2222 MJD: 59798.0-59804.0
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 2222 0 | 15 -21 62 291 65 4163 84.8 1717 1717 | -2061 0
brd 2222 1 | 36 12 103 1024 1049 4514 83.3 1580 1580 | -4852 0
brd 2222 2 | -14 -30 100 1127 -658 859 80.8 1241 1241 | -5334 0
brd 2222 3 | -55 17 113 521 -787 701 79.4 1478 1478 | -5751 0
brd 2222 4 | 44 -8 27 1394 372 1464 82.0 1566 1566 | -2884 0
brd 2222 5 | 41 -44 135 -1244 1864 1886 83.1 1654 1654 | -5804 0
brd 2222 6 | 15 24 172 -284 66 6875 82.8 1494 1494 | -5878 0
-------------+------------------------------------------------------------+----------------
brd 2222 mean| 12 -7 102 404 281 2923 82.3 1532 1532 | -4652 0
brd 2222 sdev| 36 26 47 922 932 2312 1.8 153 153 | 1548 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 2.2222.0 GPS week: 2222 Day: 0 MJD: 59798
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 -16 -26 27 .04 21 15 | 28689 -3737 2693 7725
emx n/a| -2 2 0 37 29 -25 -.15 44 32 | -12379 -2175 2723 7617
esx n/a| 0 0 3 18 29 24 -.13 26 21 | -11390 -2977 2712 11242
gfz n/a| 0 0 0 12 -18 43 -.08 23 13 | 0 -4340 2750 7409
grg n/a| 1 0 -2 -7 12 35 .40 23 19 | -42 -4103 2687 7236
iac n/a| 0 -1 0 -22 0 -114 -.22 24 21 | 40 -653 2704 8417
Table 2.2222.1 GPS week: 2222 Day: 1 MJD: 59799
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 -1 -19 -46 29 .15 23 17 | 21826 439 3115 8381
emx n/a| -1 1 1 44 52 -51 -.16 40 29 | -8831 602 3120 7830
esx n/a| 0 -1 3 9 36 -6 -.15 27 23 | -10555 996 3090 11747
gfz n/a| 1 0 5 23 0 59 -.20 20 14 | 0 120 3133 7937
grg n/a| 0 0 -8 -1 2 0 .39 22 18 | -5096 262 3112 7766
iac n/a| 0 -1 5 -49 -37 -132 -.00 29 26 | -3212 -670 3098 9125
Table 2.2222.2 GPS week: 2222 Day: 2 MJD: 59800
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 -21 -33 37 .07 24 17 | 23925 -397 2840 9155
emx n/a| -1 0 7 27 -3 33 -.03 42 29 | -19634 -237 2883 8993
esx n/a| 0 1 3 2 28 14 -.12 25 21 | -19354 537 2839 12719
gfz n/a| 0 0 -1 -9 18 38 -.02 25 17 | 0 -11 2888 9163
grg n/a| 2 -1 -12 17 20 11 .43 26 20 | -5061 -402 2820 8677
iac n/a| 3 -2 8 -39 -29 -127 -.32 27 24 | -1368 -335 2996 10553
Table 2.2222.3 GPS week: 2222 Day: 3 MJD: 59801
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -1 -4 -60 -6 .03 28 23 | 22358 -3144 3242 8679
emx n/a| 0 0 9 72 -20 -79 -.05 44 31 | -1752 -2345 3266 8688
esx n/a| -1 0 3 28 16 -33 -.16 28 24 | 4910 -2258 3254 11836
gfz n/a| 0 0 -1 -19 4 -17 -.01 23 19 | 0 -2702 3318 8682
grg n/a| 1 -2 -8 16 9 28 .37 25 22 | -4243 -3387 3239 8166
iac n/a| 5 -1 5 -38 3 94 -.27 30 29 | -3530 -1244 3247 9377
Table 2.2222.4 GPS week: 2222 Day: 4 MJD: 59802
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 2 1 -18 -78 72 .13 30 23 | 23098 3550 3662 8223
emx n/a| -1 2 14 10 -36 -17 -.07 45 27 | 731 2851 3659 8264
esx n/a| -1 0 3 0 39 14 -.18 26 27 | -5158 4406 3634 10193
gfz n/a| 1 0 -1 -18 9 25 -.11 25 16 | 0 3881 3709 8150
grg n/a| 0 -3 -7 -11 23 -70 .41 24 21 | -4927 3699 3676 7793
iac n/a| 1 0 0 33 -19 -26 -.23 27 27 | -331 464 3673 10399
Table 2.2222.5 GPS week: 2222 Day: 5 MJD: 59803
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 -19 -66 60 .10 28 18 | 25169 1315 3177 8529
emx n/a| -3 3 13 -10 2 63 -.21 45 29 | -7900 -922 3203 8502
esx n/a| -1 -1 4 29 25 44 -.14 27 25 | 6930 1839 3165 10849
gfz n/a| -2 0 -3 -26 -2 55 .02 28 17 | 0 540 3239 8588
grg n/a| 3 -5 -5 8 35 -114 .45 23 23 | -6474 883 3189 8068
iac n/a| -1 3 -1 -15 -32 -39 -.48 31 31 | -1510 -1315 3226 10442
Table 2.2222.6 GPS week: 2222 Day: 6 MJD: 59804
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 0 -51 -41 -2 .09 27 20 | 25741 371 2675 9803
emx n/a| -2 2 10 21 -30 7 -.12 47 33 | -25938 -529 2697 9656
esx n/a| 0 -2 1 33 28 50 -.06 27 20 | -9705 1279 2675 13048
gfz n/a| 1 -1 0 10 -14 6 -.03 22 16 | 0 -19 2682 9609
grg n/a| 4 -2 -7 23 33 -129 .45 26 22 | -6214 367 2664 9366
iac n/a| -4 1 5 -68 -56 103 -.36 34 31 | -2993 -740 2790 11715
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 3.2222.0 GPS week: 2222 Day: 0 MJD: 59798
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 628 39 57 51 48 22 49 20 | 104 113 146 132 110 116 116
R02E | 2624 8 25 15 15 10 16 6 | 42 33 40 43 49 43 41
R03E | 1942 12 29 15 20 9 26 8 | 85 84 82 86 87 89 84
XR04E | 1162 9 31 12 --- 10 17 7 | 77 83 83 --- 79 79 79
R05E | 1517 11 29 13 18 12 12 6 | 96 90 97 101 96 103 97
R07E | 2001 11 27 21 8 12 19 7 | 105 107 100 101 105 111 104
R08E | 2160 11 31 11 15 10 10 6 | 96 102 105 106 100 96 100
R09 | 1558 12 22 11 9 14 18 6 | 17 27 21 22 27 25 17
R11 | 940 10 17 12 15 18 28 7 | 23 35 25 30 28 28 25
R12 | 1057 13 24 10 13 12 20 6 | 20 21 25 25 15 30 19
R13 | 2731 34 40 40 32 49 32 17 | 40 45 42 37 36 48 36
R14 | 1304 11 11 12 15 13 29 7 | 23 23 27 27 27 40 25
R15 | 719 10 10 15 14 10 21 6 | 32 33 25 33 30 39 29
R17 | 1116 9 26 13 10 10 13 5 | 71 53 63 62 70 60 64
R18 | 1160 12 26 26 10 18 13 8 | 50 52 68 49 53 46 51
R19 | 1040 36 103 59 47 39 23 22 | 115 37 46 107 100 77 78
R20 | 1195 47 95 42 40 53 22 21 | 95 48 54 89 74 73 68
R21 | 730 13 24 9 16 19 15 7 | 86 69 82 80 85 69 78
R24 | 3361 12 58 12 9 16 27 10 | 75 49 73 73 83 79 72
------+-----------------------------------------+-------------------------------------
RMS | 1717 21 44 26 23 23 24 |T 65 58 63 66 66 65 62
WRMS | 1717 15 32 21 13 19 21 |NE 53 41 45 52 52 51 46
MEDI | 1195 12 27 13 15 13 20 |MD 75 49 63 62 74 69 68
Table 3.2222.1 GPS week: 2222 Day: 1 MJD: 59799
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 617 45 57 56 36 27 50 20 | 83 85 99 98 88 91 85
R02E | 2023 10 26 18 12 11 16 6 | 60 47 63 66 61 53 58
R03E | 1859 13 27 11 10 8 14 6 | 62 64 66 67 67 65 64
XR04E | 625 13 --- 12 --- 10 21 8 | 71 --- 70 --- 70 60 67
R05E | 2221 23 24 19 13 11 24 8 | 63 58 69 69 66 77 65
R07E | 1416 10 24 14 13 11 24 7 | 93 92 98 91 99 108 95
R08E | 1017 13 36 19 14 17 28 9 | 68 62 59 68 64 79 65
R09 | 1349 20 19 11 14 12 24 7 | 19 29 24 25 18 28 18
R11 | 898 14 13 13 9 20 32 8 | 20 26 30 25 22 41 23
R12 | 1196 11 14 16 13 16 19 6 | 15 17 27 21 20 21 15
R13 | 2310 23 20 19 27 33 25 11 | 28 29 27 21 22 33 21
R14 | 1695 12 12 13 13 16 28 7 | 20 16 19 22 18 40 18
R15 | 1308 11 8 17 15 13 22 6 | 19 17 19 26 18 31 17
R17 | 1561 15 26 11 12 13 16 6 | 43 37 41 32 50 35 38
R18 | 878 7 19 32 17 20 25 9 | 32 26 39 23 42 37 29
R19 | 1237 47 98 64 32 33 53 24 | 65 47 46 61 73 75 56
R20 | 1811 45 86 45 45 55 19 22 | 53 51 46 51 53 57 47
R21 | 833 17 20 13 15 14 31 8 | 46 40 44 34 51 47 41
R24 | 2511 13 52 15 11 20 34 11 | 41 32 44 45 55 65 44
------+-----------------------------------------+-------------------------------------
RMS | 1579 23 40 27 20 22 29 |T 47 43 48 46 50 54 45
WRMS | 1579 17 29 23 14 18 26 |NE 33 30 33 32 36 42 30
MEDI | 1349 13 24 16 13 16 24 |MD 46 37 44 34 53 53 44
Table 3.2222.2 GPS week: 2222 Day: 2 MJD: 59800
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 999 25 50 37 41 25 50 17 | 62 58 55 83 64 61 59
R02E | 1691 8 27 15 15 12 14 6 | 30 18 39 42 39 32 32
R03E | 1119 12 28 10 14 12 17 6 | 45 39 46 49 54 44 45
XR04E | 1025 12 28 14 --- 12 18 8 | 89 102 87 --- 91 85 87
R05E | 2181 16 30 15 13 15 18 7 | 48 45 41 47 51 50 45
R07E | 1137 10 25 12 12 15 18 6 | 51 56 52 57 60 52 53
R08E | 1195 9 26 12 15 13 23 7 | 46 46 46 49 52 53 47
R09 | 860 15 18 13 17 23 21 8 | 33 29 30 36 22 23 26
R11 | 809 9 14 13 14 17 21 6 | 21 25 32 33 20 29 23
R12 | 983 15 11 17 16 30 36 10 | 18 23 31 33 18 45 22
R13 | 747 24 28 21 36 50 30 14 | 39 34 37 32 21 48 29
R14 | 917 15 10 13 11 11 16 6 | 23 22 24 23 16 25 19
R15 | 846 10 15 15 17 14 15 6 | 23 22 21 29 24 30 22
R17 | 998 13 32 12 10 14 20 7 | 50 41 44 49 57 41 45
R18 | 847 8 17 30 20 19 26 9 | 38 36 49 26 56 27 35
R19 | 1649 51 113 66 60 38 32 27 | 86 49 44 106 82 76 68
R20 | 1810 62 81 46 40 57 35 24 | 82 43 47 67 53 56 52
R21 | 1013 22 24 15 15 20 39 10 | 80 66 70 74 75 49 67
R24 | 1384 13 47 17 12 25 19 10 | 56 43 56 59 65 58 54
XR25 |19508 --- --- --- --- --- 10 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1241 24 42 25 25 26 27 |T 48 41 44 49 48 46 43
WRMS | 1241 17 29 21 17 20 24 |NE 45 36 40 47 42 42 38
MEDI | 1013 13 27 15 15 17 20 |MD 46 41 44 47 53 48 45
Table 3.2222.3 GPS week: 2222 Day: 3 MJD: 59801
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1697 38 58 31 34 20 32 15 | 115 108 113 117 118 120 113
R02E | 3361 10 25 10 16 14 20 7 | 55 52 48 67 57 52 54
R03E | 645 12 33 13 15 15 25 8 | 47 39 48 55 53 57 48
XR04E | 679 17 25 19 --- 19 26 10 | 72 77 85 --- 81 62 75
R05E | 1201 13 29 19 11 16 20 8 | 35 29 33 37 47 46 35
R07E | 884 14 30 13 18 14 23 8 | 57 50 56 58 64 76 58
R08E | 1864 13 30 11 14 12 19 7 | 80 76 79 78 88 97 82
R09 | 1414 14 31 11 11 25 26 8 | 30 37 30 27 17 39 24
R11 | 1090 17 21 18 12 13 24 7 | 18 29 28 30 18 26 20
R12 | 477 14 19 13 9 23 25 7 | 20 23 23 19 18 27 17
R13 | 700 33 26 34 36 54 33 17 | 30 34 34 38 29 58 32
R14 | 624 11 16 10 7 9 22 5 | 18 20 30 27 26 38 22
R15 | 918 10 17 17 17 18 24 7 | 26 33 23 32 27 30 24
R17 | 777 22 28 14 17 16 47 11 | 62 39 49 56 56 40 47
R18 | 907 15 25 34 10 17 53 12 | 37 35 63 43 53 55 44
R19 | 2314 79 133 75 45 49 35 31 | 118 47 30 94 91 68 68
R20 | 2099 47 61 55 50 40 33 21 | 81 68 27 81 54 58 51
R21 | 792 18 32 13 19 19 29 9 | 69 54 54 69 73 43 60
R24 | 1429 19 34 11 10 17 21 8 | 68 45 61 62 72 58 61
XR25 |27897 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1477 28 44 28 23 25 30 |T 54 47 48 55 54 55 49
WRMS | 1477 23 31 24 19 22 29 |NE 48 38 37 48 44 45 39
MEDI | 918 15 29 14 15 17 25 |MD 55 39 48 55 54 55 48
Table 3.2222.4 GPS week: 2222 Day: 4 MJD: 59802
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 2360 46 50 30 37 32 44 17 | 95 106 103 87 106 104 94
R02E | 2010 12 26 8 13 14 25 7 | 35 32 29 34 36 24 29
R03E | 880 13 30 13 18 15 22 8 | 53 47 53 55 63 43 51
XR04E | 1252 15 29 12 --- 18 22 9 | 94 86 88 --- 99 87 91
R05E | 1661 20 29 17 12 14 19 8 | 53 56 56 55 54 60 53
R07E | 661 18 30 12 13 15 27 8 | 79 79 75 76 82 78 76
R08E | 1101 10 25 14 13 23 26 8 | 66 58 65 55 71 60 61
R09 | 2197 18 29 13 21 23 20 9 | 24 36 37 37 25 39 29
R11 | 2589 20 21 16 16 15 31 9 | 19 26 39 45 30 39 30
R12 | 661 17 11 18 16 20 24 8 | 17 15 33 27 14 29 18
R13 | 1290 24 33 28 15 33 24 12 | 27 34 24 31 23 33 21
R14 | 862 14 17 11 9 13 25 6 | 17 18 25 21 20 35 17
R15 | 970 14 16 13 12 13 35 8 | 22 22 24 23 22 46 21
R17 | 934 23 24 11 9 18 25 8 | 56 35 49 45 48 35 43
R18 | 1283 14 24 26 16 17 16 8 | 38 27 55 36 50 48 41
R19 | 2014 86 132 70 49 33 32 30 | 111 65 40 81 73 63 61
R20 | 1517 46 77 57 63 51 32 24 | 85 40 47 94 66 67 62
R21 | 920 17 33 9 20 18 23 8 | 70 56 66 72 66 57 63
R24 | 2073 24 29 10 18 25 28 10 | 71 54 60 63 60 53 58
XR25 |27450 --- --- --- --- --- 4 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1566 30 45 26 25 24 27 |T 54 46 50 52 53 52 48
WRMS | 1566 23 27 27 16 21 27 |NE 46 35 41 47 41 45 38
MEDI | 1283 18 29 13 16 18 25 |MD 53 40 49 45 54 48 51
Table 3.2222.5 GPS week: 2222 Day: 5 MJD: 59803
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1176 32 54 38 35 22 41 16 | 105 102 107 111 106 109 103
R02E | 1544 12 26 10 18 17 40 9 | 43 32 38 45 46 58 40
R03E | 635 16 28 13 26 15 17 8 | 70 70 66 80 73 66 69
XR04E | 1940 11 26 14 --- 14 31 9 | 77 72 81 --- 78 71 76
R05E | 1391 14 33 21 19 9 28 9 | 70 62 77 70 70 72 68
R07E | 922 12 27 13 20 17 24 8 | 91 94 90 95 92 88 90
R08E | 1457 9 26 12 17 18 10 7 | 78 74 71 75 85 81 76
R09 | 2309 14 19 12 17 17 27 7 | 22 17 28 35 20 36 22
R11 | 3099 16 30 17 19 15 22 8 | 14 23 23 24 18 28 11
R12 | 533 13 17 12 34 13 21 8 | 13 13 22 44 16 20 16
R13 | 2191 21 26 33 24 44 26 14 | 26 45 25 23 24 38 23
R14 | 1194 9 15 10 12 18 29 7 | 10 10 19 19 13 29 10
R15 | 1016 12 13 10 13 13 28 6 | 16 17 24 22 15 34 15
R17 | 954 10 29 17 15 17 34 9 | 45 38 37 51 52 73 46
R18 | 1824 10 20 34 11 22 30 10 | 34 27 46 41 40 36 35
R19 | 2822 81 117 57 45 33 32 28 | 84 49 40 65 52 36 48
R20 | 1299 50 96 62 75 45 42 27 | 56 37 32 84 59 62 45
R21 | 1289 22 25 14 22 26 50 12 | 87 75 81 73 89 69 77
R24 | 1459 29 38 16 10 23 38 11 | 54 33 40 37 51 42 41
XR25 |27484 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1654 28 45 27 28 23 31 |T 52 46 49 55 52 55 47
WRMS | 1654 18 29 25 17 23 31 |NE 38 32 34 43 37 41 32
MEDI | 1391 14 26 14 19 17 28 |MD 54 38 40 45 52 58 45
Table 3.2222.6 GPS week: 2222 Day: 6 MJD: 59804
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 739 45 53 40 41 25 49 18 | 81 82 93 97 85 105 84
R02E | 1495 9 24 11 10 13 19 6 | 38 32 33 36 40 31 33
R03E | 626 19 26 18 14 16 42 9 | 80 87 86 84 87 95 84
XR04E | 2614 12 26 13 --- 14 20 8 | 90 92 93 --- 97 96 93
R05E | 1841 12 29 15 19 22 22 8 | 101 89 99 102 98 104 99
R07E | 1772 16 32 17 13 13 36 9 | 152 144 141 144 146 161 146
R08E | 1079 9 28 14 12 16 20 7 | 75 73 72 77 78 80 75
R09 | 2230 21 11 13 17 33 35 10 | 26 26 28 30 27 44 24
R11 | 2604 22 30 24 16 9 22 9 | 18 30 33 30 24 28 21
R12 | 588 18 23 16 15 16 23 8 | 21 25 32 32 28 23 21
R13 | 1643 25 54 26 20 41 43 15 | 31 37 31 35 30 54 30
R14 | 870 15 11 13 11 21 28 7 | 27 25 29 30 32 26 26
R15 | 1195 8 11 11 14 20 36 8 | 31 29 33 37 26 51 30
R17 | 973 21 25 13 10 22 34 9 | 80 59 66 67 73 70 68
R18 | 1804 7 22 24 15 18 34 9 | 58 50 74 56 61 67 58
R19 | 1476 71 109 59 27 55 51 27 | 123 59 63 106 95 87 80
R20 | 1226 43 109 62 55 48 47 26 | 105 56 48 118 85 90 77
R21 | 1519 11 30 11 13 12 28 7 | 103 82 95 97 98 80 93
R24 | 1454 25 55 9 12 23 24 11 | 86 58 72 75 80 71 74
XR25 |17669 --- --- --- --- --- 10 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1494 27 47 27 22 26 34 |T 69 59 64 69 67 71 64
WRMS | 1494 20 33 20 16 22 31 |NE 59 44 50 59 54 57 50
MEDI | 1476 18 28 15 14 20 28 |MD 80 58 66 67 78 71 74
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