[IGSREPORT-28569] Wk 2200 IGLOS Final Orbits
acc
acc at igs.org
Sun Mar 27 23:19:14 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2200 (Mar 06, 2022 - Mar 12, 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 2.2200.
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:
igl2200[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2200 in the SP3 format.
igl22007.sum Combination Report for GPS Week 2200.
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 | -0.6 ns
1 | 0.6 ns
2 | 0.9 ns
3 | -0.7 ns
4 | 0.9 ns
5 | -0.6 ns
6 | -7.4 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 1.2200, 1a.2200).
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 2.2200.0-6)
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 3.2200.0-6).
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 2200 summary. (Mar 06, 2022 - Mar 12, 2022)
Table 1.2200.a GPS week : 2200 MJD: 59644.0-59650.0
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 1 5 8 2 51 .16 27 18 | 36645 -82 3398 8686
| 1 1 1 22 18 33 .03 | 4538 1484
emx n/a| 1 1 -11 15 23 -13 -.01 36 32 | -225 605 3439 8721
| 2 2 2 32 20 58 .03 | 16672 1324
esx n/a| 0 0 1 -12 -26 -43 -.07 26 20 | 5547 -501 3393 9714
| 1 0 1 13 14 28 .06 | 6197 1458
gfz n/a| 0 1 5 -21 -2 -30 -.08 30 16 | 0 -200 3401 8398
| 1 1 1 20 15 27 .05 | 0 1343
grg n/a| 2 -2 -5 12 -8 4 .30 32 24 | -1042 -277 3392 8294
| 1 1 3 10 13 49 .11 | 2829 1195
iac n/a| -1 0 0 22 5 14 -.24 25 22 | 794 150 3400 9265
| 3 1 4 28 25 138 .10 | 3136 901
Table 1.2200.b GPS week : 2200 MJD: 59644.0-59650.0
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 17 17 17 19 19 19 |
R02 | 7 8 8 10 9 10 9 |
R03 | 8 10 9 9 8 11 8 |
R04 | 10 10 10 11 10 9 10 |
R05 | 10 7 7 8 10 8 13 |
R07 | 10 10 8 7 7 8 8 |
R08 | 11 9 10 7 9 10 9 |
R09 | 8 8 10 8 6 6 11 |
R11 | 11 10 8 11 10 10 9 |
R12 | 8 9 7 8 5 8 7 |
R13 | 14 14 20 15 14 13 19 |
R14 | 7 7 6 8 5 6 6 |
R15 | 7 8 6 9 8 7 8 |
R17 | 8 12 10 9 9 8 7 |
R18 | 9 9 8 10 8 9 7 |
R19 | 17 19 17 17 20 23 22 |
R20 | 29 28 25 24 25 23 21 |
R21 | 9 9 9 8 8 9 8 |
R22 | 28 27 25 22 24 23 22 |
R24 | 10 10 12 10 9 9 8 |
Table 1.2200.c GPS week : 2200 MJD: 59644.0-59650.0
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 2200 0 | 7 39 147 -1164 298 600 79.8 1689 1689 | -595 0
brd 2200 1 | 20 -8 155 -456 1320 4247 78.3 1701 1701 | 637 0
brd 2200 2 | 72 52 110 -386 849 3075 81.2 1620 1620 | 922 0
brd 2200 3 | -17 27 119 -795 148 2563 81.9 1686 1686 | -696 0
brd 2200 4 | -34 12 4 1027 501 5238 82.2 1734 1734 | 936 0
brd 2200 5 | 22 -65 34 78 1621 -1576 79.9 1636 1636 | -594 0
brd 2200 6 | 81 -10 65 165 1541 -1562 80.3 1252 1252 | -7437 0
-------------+------------------------------------------------------------+----------------
brd 2200 mean| 21 6 90 -218 897 1797 80.5 1616 1616 | -975 0
brd 2200 sdev| 42 39 57 718 604 2712 1.4 165 165 | 2943 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 2.2200.0 GPS week: 2200 Day: 0 MJD: 59644
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 6 12 0 33 .13 25 16 | 39156 -1640 3571 9254
emx n/a| 2 3 -11 23 5 -28 -.03 37 34 | 7888 -1178 3627 9431
esx n/a| -1 0 0 -20 -9 -63 .01 25 22 | 12722 -990 3576 9450
gfz n/a| 0 1 3 -18 -16 -69 -.00 32 15 | 0 -1187 3559 9192
grg n/a| 3 -3 -5 4 -17 -36 .11 35 25 | -52 -1003 3583 9148
iac n/a| 2 0 1 66 -23 214 -.35 31 30 | 1816 99 3591 9931
Table 2.2200.1 GPS week: 2200 Day: 1 MJD: 59645
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| 3 0 5 25 0 76 .21 32 22 | 37859 702 3386 8657
emx n/a| 0 0 -12 -36 29 -67 -.03 36 33 | -17468 777 3343 8640
esx n/a| -1 1 0 9 -26 -19 -.04 24 19 | 6288 773 3359 8618
gfz n/a| 2 1 5 0 -23 -23 -.12 32 18 | 0 987 3379 8176
grg n/a| 3 -2 -9 1 3 -10 .19 34 22 | 69 818 3362 8246
iac n/a| -4 0 5 -3 23 -7 -.06 25 22 | 2139 -336 3360 9229
Table 2.2200.2 GPS week: 2200 Day: 2 MJD: 59646
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 41 30 78 .12 28 20 | 40536 789 3048 7314
emx n/a| -2 1 -14 2 62 28 -.04 36 32 | 3358 1091 3114 7438
esx n/a| 0 0 2 -20 -41 -13 -.10 26 21 | 13538 732 3046 7600
gfz n/a| 0 0 6 -20 9 -24 -.12 28 20 | 0 1021 3036 6942
grg n/a| 1 -3 -7 13 -14 48 .32 29 20 | 473 561 3050 6823
iac n/a| 0 -2 5 -1 -32 -156 -.15 32 24 | 3308 -148 3044 7845
Table 2.2200.3 GPS week: 2200 Day: 3 MJD: 59647
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 4 16 22 62 .19 25 16 | 38726 -2333 3673 9363
emx n/a| 0 -1 -12 -6 35 55 .02 34 31 | 13986 -1006 3766 9336
esx n/a| 2 0 3 -10 -45 -34 -.18 27 20 | -3522 -2998 3679 11797
gfz n/a| -1 3 7 -29 5 0 -.06 30 17 | 0 -2131 3721 9058
grg n/a| 2 -2 -2 3 -2 -39 .38 27 22 | -314 -2495 3660 8978
iac n/a| -2 0 -6 29 -2 -52 -.32 23 20 | 1335 -1027 3695 9973
Table 2.2200.4 GPS week: 2200 Day: 4 MJD: 59648
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 4 -21 -1 77 .17 25 17 | 37531 1293 3593 8017
emx n/a| 3 2 -13 55 1 -43 .03 36 32 | 9040 1726 3651 8087
esx n/a| 0 0 2 -2 -19 -80 -.07 26 19 | 6456 699 3588 10040
gfz n/a| 0 1 6 -56 -9 -62 -.15 27 14 | 0 1353 3605 7583
grg n/a| 0 0 -1 17 -25 68 .35 35 25 | 460 810 3600 7875
iac n/a| 1 -3 -2 41 27 42 -.24 23 18 | 1841 1713 3603 8580
Table 2.2200.5 GPS week: 2200 Day: 5 MJD: 59649
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 -17 -6 44 .18 28 18 | 35805 -732 3235 8776
emx n/a| 4 4 -9 49 19 50 -.03 37 32 | 11342 434 3305 8882
esx n/a| 2 -1 3 -10 -10 -17 -.07 29 20 | 800 -1712 3238 10865
gfz n/a| 2 0 7 4 19 0 -.05 33 17 | 0 -1089 3241 8559
grg n/a| 3 -1 -11 30 -14 51 .41 28 23 | -531 -455 3251 8194
iac n/a| -5 2 0 -9 15 -109 -.32 21 18 | 1271 932 3244 9350
Table 2.2200.6 GPS week: 2200 Day: 6 MJD: 59650
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 -1 -23 -13 .14 27 19 | 26905 1346 3283 9424
emx n/a| 2 2 -7 17 12 -92 .03 38 31 | -29725 2393 3268 9234
esx n/a| 0 0 0 -32 -30 -73 -.07 28 19 | 2553 -14 3268 9633
gfz n/a| 0 1 4 -31 -5 -36 -.08 26 13 | 0 -360 3271 9277
grg n/a| 2 -5 -3 19 13 -47 .33 33 30 | -7404 -177 3244 8797
iac n/a| -1 0 -1 37 29 169 -.24 21 20 | -6150 -179 3268 9952
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 3.2200.0 GPS week: 2200 Day: 0 MJD: 59644
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1465 40 47 48 24 23 30 16 | 110 70 58 88 89 88 79
R02 | 1780 9 22 16 11 13 21 6 | 74 61 81 76 71 85 74
R03 | 918 8 28 16 9 20 30 8 | 98 75 86 95 104 101 92
XR04 | 1552 7 25 17 --- 25 29 10 | 94 74 81 --- 97 104 88
R05 | 1691 7 27 22 15 14 37 9 | 82 66 93 92 81 90 83
R07 | 1795 13 38 18 19 16 33 10 | 98 68 88 102 96 108 92
R08 | 1037 14 40 11 18 23 41 11 | 82 72 87 80 87 89 81
R09 | 675 8 20 9 19 19 26 7 | 38 39 36 43 34 58 38
XR11 | 943 15 --- 17 22 11 36 10 | 39 --- 40 45 40 52 38
R12 | 2932 9 21 18 14 9 29 7 | 78 79 79 71 81 82 76
R13 | 800 30 44 19 24 44 27 14 | 81 84 66 68 55 75 69
R14 | 570 9 11 14 13 14 30 7 | 54 50 56 57 52 54 52
R15 | 465 15 12 13 16 13 24 7 | 63 65 60 63 61 70 61
R17E | 1943 16 26 10 10 18 31 8 | 96 94 92 91 90 92 91
R18E | 3207 8 25 17 13 23 31 8 | 66 67 68 64 67 72 65
R19E | 2460 39 57 22 34 49 34 17 | 64 66 73 69 78 88 68
R20E | 2272 35 72 55 98 71 27 28 | 119 119 100 143 98 117 109
R21E | 661 13 35 13 9 17 24 8 | 113 118 112 111 118 108 112
R22E | 1136 68 54 49 63 91 43 28 | 42 66 88 72 118 72 62
R24E | 886 17 35 11 15 32 30 10 | 103 108 99 100 102 97 99
------+-----------------------------------------+-------------------------------------
RMS | 1689 25 37 25 32 35 31 |T 79 75 77 80 80 85 76
WRMS | 1689 16 34 22 15 25 30 |NE 76 66 70 73 72 81 71
MEDI | 1136 13 28 17 16 19 30 |MD 81 70 81 76 81 88 76
Table 3.2200.1 GPS week: 2200 Day: 1 MJD: 59645
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1498 57 38 44 28 26 16 17 | 90 68 56 60 58 66 61
R02 | 1533 10 28 19 14 15 22 8 | 67 60 66 68 64 74 65
R03 | 694 16 28 15 15 16 32 9 | 74 64 68 76 77 61 68
XR04 | 1608 19 23 14 --- 17 27 10 | 58 40 50 --- 51 58 50
R05 | 2137 12 26 14 11 16 17 7 | 64 56 72 67 66 75 65
R07 | 1869 15 44 18 21 17 19 10 | 77 63 75 84 83 84 76
R08 | 918 13 32 19 18 21 10 8 | 66 61 71 63 68 61 64
R09 | 1129 17 12 15 22 16 20 8 | 36 38 38 36 39 45 35
R11 | 1153 16 28 18 21 14 28 9 | 44 15 48 46 50 49 41
R12 | 2357 19 24 16 14 22 19 8 | 75 76 85 80 80 77 77
R13 | 623 25 39 12 26 55 26 14 | 71 79 62 63 53 74 66
R14 | 651 9 14 16 8 13 22 6 | 54 53 61 61 49 53 54
R15 | 747 13 15 8 9 12 31 7 | 62 67 68 65 67 61 62
R17E | 3010 15 31 13 13 31 41 11 | 62 72 62 68 75 75 65
R18E | 2851 17 31 15 15 20 18 8 | 92 100 96 94 93 109 96
R19E | 2841 61 43 23 39 55 25 18 | 53 61 58 64 65 68 55
R20E | 1728 53 71 48 91 75 25 28 | 90 105 76 115 66 77 80
R21E | 557 16 41 11 18 14 13 8 | 126 135 128 128 129 122 127
R22E | 1504 76 45 50 65 75 40 26 | 81 94 98 100 110 88 87
R24E | 792 16 42 16 22 13 24 10 | 173 179 176 173 172 161 171
------+-----------------------------------------+-------------------------------------
RMS | 1701 32 36 24 32 34 25 |T 75 74 75 79 75 76 73
WRMS | 1701 22 33 19 18 22 22 |NE 64 56 63 64 61 64 60
MEDI | 1498 16 31 16 18 17 22 |MD 67 64 68 68 66 74 65
Table 3.2200.2 GPS week: 2200 Day: 2 MJD: 59646
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1339 41 41 46 34 31 24 16 | 75 42 47 63 44 64 49
R02 | 1444 9 30 13 17 16 16 7 | 59 43 62 53 55 70 56
R03 | 1289 15 39 17 15 18 13 8 | 80 43 62 80 84 76 71
XR04 | 1223 19 30 15 --- 15 14 9 | 70 47 58 --- 66 64 60
R05 | 2040 8 26 15 18 10 15 7 | 54 37 61 70 54 48 53
R07 | 879 7 39 11 14 16 18 8 | 70 45 69 65 73 81 66
R08 | 1235 18 27 23 23 19 25 10 | 58 44 67 67 51 41 54
R09 | 2171 15 11 19 20 9 41 9 | 31 39 32 36 41 50 34
XR11 | 1078 15 --- 22 12 11 17 8 | 21 --- 43 29 21 22 24
R12 | 1561 17 14 9 13 17 17 6 | 53 44 46 49 36 48 44
R13 | 1050 38 36 33 33 68 45 19 | 54 62 43 50 29 62 42
R14 | 597 9 12 13 10 11 17 5 | 26 25 29 23 24 38 25
R15 | 961 8 18 14 13 12 18 6 | 44 49 47 44 38 42 42
R17E | 2956 10 36 11 16 21 35 9 | 43 44 43 49 46 39 41
R18E | 2674 11 22 24 18 14 18 8 | 36 44 43 40 41 41 38
R19E | 1223 45 46 24 34 50 22 17 | 60 59 48 59 70 58 51
R20E | 2276 34 68 57 73 59 29 24 | 100 89 98 116 86 94 91
R21E | 896 18 26 17 21 16 14 8 | 57 57 57 59 62 57 55
R22E | 1303 74 55 38 36 28 82 24 | 57 65 88 85 95 106 72
R24E | 806 17 50 15 18 17 43 12 | 91 100 93 90 92 82 89
------+-----------------------------------------+-------------------------------------
RMS | 1620 28 36 26 28 29 32 |T 56 51 56 59 55 59 52
WRMS | 1620 20 32 21 20 20 24 |NE 53 43 51 52 47 54 47
MEDI | 1235 15 30 17 18 16 18 |MD 57 44 48 59 51 57 51
Table 3.2200.3 GPS week: 2200 Day: 3 MJD: 59647
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 800 37 44 50 37 36 20 17 | 89 41 60 95 86 57 68
R02 | 3106 17 26 32 16 21 13 9 | 56 36 62 43 38 38 44
R03 | 1024 11 35 14 17 19 24 9 | 80 48 64 74 87 79 72
XR04 | 757 10 33 23 --- 16 23 10 | 80 55 70 --- 93 91 78
R05 | 2035 15 24 21 18 14 10 7 | 55 37 66 68 62 48 55
R07 | 728 6 28 16 13 17 14 7 | 69 46 59 76 84 74 69
R08 | 1682 11 23 16 10 15 16 7 | 61 42 71 64 62 60 60
R09 | 1523 21 19 14 20 12 18 8 | 16 24 29 35 19 34 23
XR11 | 1913 15 --- 16 17 28 28 11 | 12 --- 23 28 34 36 22
R12 | 1141 11 23 15 14 22 21 8 | 51 41 60 61 39 69 52
R13 | 823 27 14 27 31 58 20 14 | 59 54 56 70 21 61 51
R14 | 549 9 13 19 14 17 23 7 | 35 36 35 28 28 47 31
R15 | 1490 16 17 18 23 19 26 9 | 49 49 32 29 40 58 40
R17E | 2671 17 28 16 21 16 18 8 | 66 73 79 82 74 70 71
R18E | 1511 22 23 20 13 20 27 9 | 46 45 54 51 55 55 49
R19E | 1023 43 46 27 40 35 28 16 | 102 96 105 109 114 104 101
R20E | 3191 32 62 47 83 52 40 24 | 150 131 145 166 163 126 141
R21E | 1039 12 28 16 16 16 19 8 | 66 70 68 70 72 62 66
R22E | 1062 58 62 51 44 32 41 21 | 44 42 95 79 77 67 58
R24E | 1631 16 40 17 21 18 17 9 | 58 61 57 60 63 65 58
------+-----------------------------------------+-------------------------------------
RMS | 1686 25 34 27 30 27 23 |T 62 54 64 67 65 65 60
WRMS | 1686 16 31 20 17 22 20 |NE 54 42 52 55 53 57 51
MEDI | 1141 16 28 18 18 19 20 |MD 58 46 60 68 62 61 58
Table 3.2200.4 GPS week: 2200 Day: 4 MJD: 59648
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1057 42 59 54 27 46 16 18 | 88 32 60 86 92 56 64
R02 | 4164 10 28 24 19 15 20 8 | 54 35 62 57 43 46 48
R03 | 706 14 34 16 13 17 16 8 | 73 47 59 63 72 78 65
XR04 | 1065 7 29 19 --- 18 22 9 | 75 62 55 --- 86 85 71
R05 | 1916 18 24 22 23 32 18 10 | 59 43 65 64 86 50 58
R07 | 741 12 24 12 9 13 16 6 | 75 56 68 61 75 68 67
R08 | 2337 13 28 15 14 29 18 8 | 63 45 67 59 85 54 61
R09 | 667 11 9 12 14 15 12 5 | 27 32 37 41 31 30 31
XR11 | 1365 16 --- 22 9 20 23 9 | 13 --- 28 22 31 35 20
R12 | 1427 13 13 12 12 10 10 5 | 57 52 58 55 57 65 57
R13 | 547 23 28 34 28 47 26 13 | 65 74 53 77 48 78 64
R14 | 599 8 15 13 9 14 11 5 | 38 40 39 34 32 41 36
R15 | 648 18 12 14 20 22 17 8 | 55 47 46 51 43 54 47
R17E | 2658 12 29 17 10 20 25 8 | 46 44 48 44 52 57 46
R18E | 598 16 19 19 11 19 20 8 | 34 31 34 34 44 39 34
R19E | 994 47 58 18 47 64 22 19 | 80 71 79 91 93 88 77
R20E | 2668 42 63 47 60 76 55 25 | 135 135 129 126 115 142 123
R21E | 1428 15 28 14 11 15 21 8 | 99 102 94 103 108 115 102
R22E | 858 52 60 49 56 57 42 23 | 48 28 99 112 90 48 64
R24E | 1897 14 37 15 18 17 14 8 | 53 54 52 52 57 51 50
------+-----------------------------------------+-------------------------------------
RMS | 1733 25 36 26 27 35 23 |T 61 54 61 64 67 64 59
WRMS | 1733 17 32 19 14 25 18 |NE 57 47 53 55 60 56 53
MEDI | 1057 14 28 17 14 19 18 |MD 57 47 58 59 57 54 58
Table 3.2200.5 GPS week: 2200 Day: 5 MJD: 59649
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 940 39 63 63 15 31 35 19 | 87 48 57 70 81 88 68
R02 | 4402 9 30 24 27 16 19 9 | 57 47 62 53 46 52 50
R03 | 818 13 46 17 39 11 14 11 | 66 41 70 85 60 56 61
XR04 | 665 14 21 20 --- 16 16 8 | 78 62 82 --- 62 68 70
R05 | 2527 9 22 23 19 15 17 8 | 64 59 75 69 52 53 60
R07 | 743 16 28 12 22 10 15 7 | 72 65 71 77 74 72 70
R08 | 1127 19 28 14 21 27 20 9 | 62 46 52 44 60 47 51
R09 | 1127 15 13 7 14 19 11 6 | 23 33 26 32 36 38 29
XR11 | 1127 17 --- 18 10 16 25 9 | 17 --- 32 25 27 28 21
R12 | 1048 22 19 16 14 10 24 8 | 56 51 56 47 55 39 48
R13 | 712 29 27 29 32 39 18 13 | 57 56 70 57 52 57 56
R14 | 510 10 17 14 16 11 11 6 | 40 45 49 49 52 45 45
R15 | 796 9 20 8 17 18 13 6 | 45 43 46 53 49 51 46
R17E | 1337 15 28 19 11 17 15 8 | 57 55 56 55 58 62 55
R18E | 1018 11 24 19 28 23 16 9 | 38 37 46 42 50 46 41
R19E | 1538 52 71 37 76 36 37 23 | 67 57 51 91 63 62 55
R20E | 1913 60 55 41 52 64 25 22 | 93 90 82 110 105 88 89
R21E | 1504 19 28 14 12 19 19 8 | 105 117 101 107 112 99 104
R22E | 1299 53 52 58 64 51 32 23 | 46 44 82 92 63 48 49
R24E | 1555 10 37 18 21 15 19 9 | 51 50 55 54 55 51 50
------+-----------------------------------------+-------------------------------------
RMS | 1635 28 37 29 33 28 21 |T 59 55 61 63 60 57 55
WRMS | 1635 18 32 20 17 23 18 |NE 55 49 57 55 54 53 51
MEDI | 1127 15 28 18 21 17 18 |MD 57 50 56 55 55 52 51
Table 3.2200.6 GPS week: 2200 Day: 6 MJD: 59650
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1156 51 65 50 23 31 18 18 | 116 62 63 94 91 85 81
R02 | 1813 13 30 17 11 29 21 9 | 74 55 81 74 80 75 72
R03 | 556 7 30 13 11 21 15 7 | 92 66 85 100 103 87 88
XR04 | 748 22 25 17 --- 15 20 10 | 99 74 92 --- 94 86 88
R05 | 2206 19 24 27 22 40 31 12 | 79 68 103 99 67 91 84
R07 | 700 9 29 19 12 14 13 7 | 97 75 83 99 100 98 92
R08 | 1396 21 25 17 24 24 14 9 | 80 58 77 69 72 67 70
R09 | 723 10 10 26 25 33 27 10 | 29 43 29 33 50 56 36
R11 | 720 14 16 14 20 17 26 8 | 20 22 25 27 32 37 25
R12 | 835 19 10 16 11 11 16 6 | 72 69 74 68 64 65 67
R13 | 765 41 42 36 34 77 23 19 | 87 75 68 84 63 81 75
R14 | 575 11 17 15 14 12 11 6 | 51 49 57 56 53 55 53
R15 | 735 10 18 11 13 25 21 7 | 60 57 65 69 53 68 61
R17E | 735 7 28 11 10 15 18 7 | 61 59 64 62 59 61 59
R18E | 708 10 19 17 14 20 12 7 | 44 42 48 42 53 39 42
R19E | 1376 39 87 38 49 42 33 21 | 69 66 63 87 89 73 69
R20E | 2061 54 53 48 45 55 25 21 | 97 107 99 101 94 91 90
R21E | 1483 11 34 11 14 14 13 7 | 140 141 139 143 146 135 140
R22E | 2076 54 52 56 53 39 29 21 | 49 56 116 77 91 73 68
R24E | 795 11 31 14 15 13 18 7 | 58 59 57 57 59 57 55
------+-----------------------------------------+-------------------------------------
RMS | 1252 27 38 28 26 33 21 |T 73 65 74 75 75 74 70
WRMS | 1252 19 31 19 13 30 20 |NE 73 59 69 72 70 73 68
MEDI | 765 13 28 17 15 21 18 |MD 72 59 68 74 67 73 69
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