[IGSREPORT-28784] Wk 2216 IGLOS Final Orbits
acc
acc at igs.org
Fri Jul 15 10:45:00 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2216 (Jun 26, 2022 - Jul 02, 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 2.2216.
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:
igl2216[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2216 in the SP3 format.
igl22167.sum Combination Report for GPS Week 2216.
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 | -7.7 ns
1 | -5.5 ns
2 | -4.3 ns
3 | 0.6 ns
4 | 2.0 ns
5 | -1.5 ns
6 | 0.4 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ALL | R24
1 | ALL | R24
2 | ALL | R24
3 | ALL | R24
4 | ALL | R24
5 | ALL | R24
6 | ALL | R24
6 | EMX | R19
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 1.2216, 1a.2216).
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 2.2216.0-6)
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 3.2216.0-6).
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 2216 summary. (Jun 26, 2022 - Jul 02, 2022)
Table 1.2216.a GPS week : 2216 MJD: 59756.0-59762.0
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| -1 0 4 6 -28 7 .11 23 18 | 31631 409 3756 10465
| 1 1 1 25 16 28 .03 | 6284 2353
emx n/a| -4 0 -15 31 10 -43 -.12 53 36 | -2492 482 3644 9417
| 2 1 1 38 26 62 .07 | 18193 1448
esx n/a| -1 0 1 10 17 0 -.13 32 22 | -11325 910 3696 13190
| 1 1 1 17 17 36 .04 | 14639 2054
gfz n/a| 0 0 6 -5 0 7 -.12 26 19 | 0 253 3490 9199
| 0 1 4 18 17 29 .05 | 0 2637
grg n/a| 4 0 -11 -18 23 13 .35 28 22 | -2131 344 3682 9609
| 1 1 1 9 18 23 .04 | 3716 2210
iac n/a| -1 0 2 5 -17 -11 -.20 27 26 | 408 -427 3677 10815
| 1 2 5 21 38 81 .07 | 3793 900
Table 1.2216.b GPS week : 2216 MJD: 59756.0-59762.0
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 | 22 20 20 20 21 21 22 |
R02 | 9 8 8 8 9 9 8 |
R03 | 8 9 9 9 9 8 8 |
R04 | 10 10 11 9 8 10 10 |
R05 | 7 10 10 8 8 9 10 |
R07 | 10 10 9 8 10 11 9 |
R08 | 11 10 9 10 12 10 7 |
R09 | 7 12 8 9 8 7 7 |
R11 | 11 9 9 11 11 8 11 |
R12 | 9 9 7 6 7 8 8 |
R13 | 17 16 18 18 16 19 16 |
R14 | 9 10 9 8 8 8 9 |
R15 | 10 8 10 7 7 7 5 |
R17 | 9 9 8 7 9 8 7 |
R18 | 9 10 10 8 8 8 8 |
R19 | 24 29 26 23 25 29 25 |
R20 | 23 23 27 24 25 21 24 |
R21 | 7 7 8 8 7 9 8 |
Table 1.2216.c GPS week : 2216 MJD: 59756.0-59762.0
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 2216 0 | 20 10 350 830 -1497 2238 80.9 1272 1272 | -7655 0
brd 2216 1 | 49 -27 364 2489 289 4271 81.5 1519 1519 | -5461 0
brd 2216 2 | 94 41 263 252 -1201 4051 84.1 1562 1562 | -4327 0
brd 2216 3 | -14 11 238 2352 -1653 267 81.4 1801 1801 | 581 0
brd 2216 4 | -19 9 254 -810 -3223 9934 80.7 1805 1805 | 1952 0
brd 2216 5 | 61 81 265 -474 1054 8243 82.5 1517 1517 | -1464 0
brd 2216 6 | 12 6 248 25 -825 3971 82.8 1452 1452 | 384 0
-------------+------------------------------------------------------------+----------------
brd 2216 mean| 29 19 283 666 -1008 4710 82.0 1561 1561 | -2284 0
brd 2216 sdev| 41 34 51 1307 1388 3336 1.2 189 189 | 3583 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 2.2216.0 GPS week: 2216 Day: 0 MJD: 59756
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 33 -29 10 .06 24 18 | 25031 -2788 3333 9806
emx n/a| -1 -1 -14 -5 52 -52 -.20 48 34 | -1228 -1859 3365 9499
esx n/a| -3 0 1 16 29 -16 -.12 32 18 | -17097 -1475 3357 12375
gfz n/a| 0 0 8 3 -7 0 -.15 31 19 | 0 -2621 3388 9286
grg n/a| 4 -3 -12 -22 5 20 .38 24 24 | -6374 -2302 3344 8924
iac n/a| -2 5 2 -19 11 2 -.08 25 24 | -4554 -1239 3335 10228
Table 2.2216.1 GPS week: 2216 Day: 1 MJD: 59757
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 -2 6 -12 -11 10 .13 24 19 | 24578 -837 3737 9355
emx n/a| -4 0 -17 -24 -19 56 -.22 55 38 | -21539 156 3695 8871
esx n/a| -2 1 0 19 13 45 -.14 29 22 | -24748 331 3653 12635
gfz n/a| 0 0 13 8 -22 46 -.08 31 19 | 0 -696 3721 8669
grg n/a| 5 -1 -14 -17 13 7 .35 31 21 | -5360 -819 3604 8506
iac n/a| -1 0 0 4 20 -147 -.20 26 24 | -3220 -1009 3630 9793
Table 2.2216.2 GPS week: 2216 Day: 2 MJD: 59758
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 -45 -41 .10 22 17 | 25547 2819 3635 8793
emx n/a| -2 0 -16 24 13 -117 -.09 53 36 | -22048 2165 3571 8316
esx n/a| -1 1 2 -21 49 11 -.07 30 20 | -27737 3756 3595 12032
gfz n/a| 0 3 10 -4 9 -13 -.07 29 25 | 0 3320 3580 8450
grg n/a| 5 0 -12 0 48 55 .35 31 24 | -5988 2977 3607 7886
iac n/a| 0 0 -5 34 -40 46 -.20 28 25 | -2810 942 3578 9143
Table 2.2216.3 GPS week: 2216 Day: 3 MJD: 59759
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 40 -29 16 .12 21 17 | 34141 2659 3350 12441
emx n/a| -5 -2 -13 84 -12 -61 -.07 53 36 | 7464 1453 3310 12016
esx n/a| 0 0 1 36 19 -60 -.09 33 24 | -7943 3112 3297 14713
gfz n/a| 1 -1 4 -31 28 -22 -.17 23 23 | 0 2057 3183 11529
grg n/a| 3 0 -8 -25 47 1 .39 27 24 | -457 2617 3276 11460
iac n/a| -1 3 0 7 -43 95 -.24 24 23 | 3995 -495 3274 12699
Table 2.2216.4 GPS week: 2216 Day: 4 MJD: 59760
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 2 10 -26 20 .14 25 18 | 36415 2960 4361 11005
emx n/a| -1 -2 -18 49 -5 5 -.04 52 36 | 25065 1939 4284 10525
esx n/a| 0 0 1 8 -5 4 -.20 30 22 | -9976 1984 4272 13066
gfz n/a| 1 0 5 -31 2 15 -.18 20 16 | 0 3112 4188 10392
grg n/a| 2 0 -12 -15 23 24 .35 26 20 | 397 2295 4271 10351
iac n/a| -3 0 4 -24 -68 -84 -.17 35 31 | 3884 -476 4263 11379
Table 2.2216.5 GPS week: 2216 Day: 5 MJD: 59761
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 3 -10 -5 -14 .09 20 15 | 37714 -605 3979 8691
emx n/a| -7 2 -14 26 6 -21 -.06 52 36 | -16377 -426 3886 8111
esx n/a| -1 1 4 9 9 37 -.15 35 25 | -8401 -337 3879 11920
gfz n/a| 2 0 1 -1 6 48 -.07 28 18 | 0 -3134 2998 7153
grg n/a| 4 -1 -10 -17 2 -17 .33 29 19 | -153 -724 3873 7802
iac n/a| 0 0 6 7 -35 -16 -.29 28 27 | 1793 634 3871 9024
Table 2.2216.6 GPS week: 2216 Day: 6 MJD: 59762
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 5 -26 -49 48 .15 24 22 | 37994 -1341 3902 13167
emx n/a| -6 0 -14 67 38 -111 -.16 60 37 | 11218 -48 3402 8585
esx n/a| -2 1 -1 6 8 -24 -.13 33 25 | 16626 -997 3820 15590
gfz n/a| 0 2 3 15 -20 -19 -.09 22 12 | 0 -262 3372 8915
grg n/a| 5 0 -10 -30 21 1 .27 27 19 | 3014 -1636 3805 12338
iac n/a| -2 -3 9 28 31 26 -.22 26 25 | 3772 -1352 3793 13445
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 3.2216.0 GPS week: 2216 Day: 0 MJD: 59756
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 395 54 66 66 60 21 18 22 | 96 52 62 99 67 66 66
R02 | 1848 16 33 9 25 12 25 8 | 79 46 67 88 70 69 70
R03 | 755 9 31 14 18 13 21 7 | 85 56 73 92 83 87 80
XR04M | 641 23 24 15 --- 17 18 9 | 82 42 73 --- 66 66 70
R05M | 1503 12 23 15 18 12 20 7 | 70 49 64 66 72 60 64
R07 | 2248 15 28 20 29 14 23 9 | 81 48 61 87 67 78 70
R08 | 1136 14 27 16 33 19 32 10 | 75 44 69 96 80 74 72
R09 | 1655 13 21 19 23 12 11 7 | 29 34 39 33 32 25 29
XR11 | 2610 --- 22 20 24 17 24 10 | --- 33 45 63 36 54 43
R12M | 430 16 32 14 18 13 25 8 | 116 98 110 115 114 113 111
R13M | 593 31 45 32 62 35 17 16 | 105 70 78 115 71 87 85
R14M | 806 16 40 22 14 13 18 9 | 56 46 68 65 49 62 56
R15 | 725 14 22 8 10 32 28 9 | 69 49 63 67 51 76 61
R17 | 827 20 24 11 14 13 30 8 | 32 32 28 30 33 45 31
R18 | 2051 16 27 14 19 12 28 8 | 26 31 27 37 27 32 26
R19 | 1301 41 129 40 17 53 32 24 | 48 60 44 59 49 41 44
R20 | 1298 38 64 80 51 38 34 23 | 43 59 53 40 36 41 38
R21 | 632 8 37 9 17 12 16 7 | 36 36 43 40 44 33 37
------+-----------------------------------------+-------------------------------------
RMS | 1271 24 48 32 31 24 25 |T 66 49 59 70 58 61 58
WRMS | 1271 18 34 18 19 24 24 |NE 58 44 51 63 51 55 51
MEDI | 827 16 28 15 19 13 23 |MD 70 46 62 66 51 62 61
Table 3.2216.1 GPS week: 2216 Day: 1 MJD: 59757
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 770 52 63 55 38 36 12 20 | 72 53 55 70 55 46 50
R02 | 2049 15 44 10 21 12 15 8 | 60 39 49 64 56 49 53
R03 | 1094 12 33 17 24 15 20 8 | 67 49 57 83 69 56 63
XR04M | 736 20 21 15 --- 27 17 10 | 64 34 64 --- 56 57 58
R05M | 794 21 32 21 23 23 22 10 | 64 47 64 76 68 61 62
R07 | 2312 10 44 16 26 12 24 9 | 55 43 57 75 68 68 60
R08 | 1492 11 38 18 27 17 27 9 | 59 43 55 78 58 71 60
R09 | 1527 18 25 24 36 16 35 11 | 45 51 52 46 43 29 40
XR11 | 3743 --- 20 18 19 18 14 9 | --- 35 30 33 21 27 24
R12M | 758 12 42 17 12 17 22 8 | 122 108 122 115 120 119 118
R13M | 696 33 43 28 36 41 33 15 | 72 39 59 68 54 76 60
R14M | 615 12 42 18 13 26 24 9 | 52 41 59 60 43 58 51
R15 | 795 16 21 9 15 18 20 7 | 57 45 56 58 47 50 51
R17 | 814 18 29 10 17 19 26 8 | 28 30 27 35 35 31 26
R18 | 3596 11 23 27 11 20 34 10 | 29 32 31 27 31 36 27
R19 | 1730 48 152 41 54 81 37 29 | 52 48 45 46 50 42 42
R20 | 1057 26 72 66 64 44 31 22 | 41 50 38 38 36 32 32
R21 | 773 11 35 12 11 8 15 6 | 39 39 44 46 44 27 38
------+-----------------------------------------+-------------------------------------
RMS | 1518 24 55 29 31 31 26 |T 57 45 53 59 53 51 50
WRMS | 1518 19 38 22 19 21 24 |NE 50 42 45 53 47 43 43
MEDI | 814 16 35 18 23 18 22 |MD 57 43 55 60 50 49 51
Table 3.2216.2 GPS week: 2216 Day: 2 MJD: 59758
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1126 50 54 52 42 43 18 20 | 73 25 59 74 49 52 51
R02 | 1564 7 40 9 24 15 15 8 | 53 33 54 69 56 51 53
R03 | 1128 7 35 19 19 15 23 8 | 74 60 65 88 79 79 74
XR04M | 1244 21 20 16 --- 21 25 10 | 58 30 52 --- 43 43 46
R05M | 773 16 24 24 20 17 28 9 | 46 43 65 63 54 44 51
R07 | 2470 11 35 22 15 17 26 9 | 64 37 46 61 60 65 55
R08 | 716 7 47 14 18 18 24 9 | 65 40 63 77 67 71 64
R09 | 2480 16 12 16 21 13 20 7 | 29 31 42 43 29 37 33
XR11 | 3725 --- 25 15 24 14 14 9 | --- 28 26 27 25 27 20
R12M | 1155 10 25 14 18 13 18 7 | 85 64 92 81 78 79 81
R13M | 560 36 56 31 30 29 59 17 | 73 41 53 77 57 98 66
R14M | 684 9 35 16 22 19 21 8 | 51 27 51 56 38 48 44
R15 | 735 18 22 12 12 13 42 9 | 59 51 48 52 47 45 46
R17 | 1041 16 25 14 13 14 26 8 | 23 21 21 26 31 22 20
R18 | 3493 20 22 23 28 19 21 10 | 27 29 22 34 28 26 22
R19 | 871 40 144 49 28 61 28 25 | 36 55 41 35 29 35 35
R20 | 1621 20 78 69 73 80 28 26 | 55 40 51 42 39 38 39
R21 | 1168 10 38 10 19 16 15 7 | 24 24 28 34 37 28 27
------+-----------------------------------------+-------------------------------------
RMS | 1562 22 53 30 29 31 28 |T 52 37 48 55 47 49 45
WRMS | 1562 17 36 20 25 24 25 |NE 48 36 43 50 44 44 41
MEDI | 1128 16 35 16 21 17 23 |MD 55 33 51 56 43 44 46
Table 3.2216.3 GPS week: 2216 Day: 3 MJD: 59759
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 729 55 62 56 29 33 33 20 | 76 30 54 58 46 41 45
R02 | 2110 10 46 9 18 16 15 8 | 57 27 57 67 57 62 56
R03 | 1082 11 33 21 15 15 32 9 | 74 58 64 82 89 96 78
XR04M | 1302 19 24 13 --- 14 16 8 | 48 27 36 --- 38 37 37
R05M | 795 14 26 17 12 18 26 8 | 54 50 58 50 65 31 50
R07 | 2555 13 27 22 9 17 20 7 | 71 53 51 66 69 74 64
R08 | 1322 11 35 22 14 16 33 9 | 72 52 60 89 78 89 75
R09 | 3491 13 21 26 16 14 24 8 | 21 28 30 25 16 32 19
XR11 | 4135 --- 11 22 16 22 32 11 | --- 59 58 66 63 62 59
R12M | 1934 12 25 10 11 13 10 5 | 89 86 91 90 98 83 89
R13M | 465 27 54 47 44 45 24 17 | 92 73 81 107 102 94 91
R14M | 775 14 36 15 14 18 14 7 | 56 33 63 56 44 55 51
R15 | 748 13 20 11 11 17 22 7 | 59 45 54 46 57 42 49
R17 | 998 10 31 8 12 16 20 7 | 21 18 24 24 29 21 20
R18 | 1440 13 21 28 16 18 13 8 | 21 20 34 23 27 20 21
R19 | 1209 28 120 63 31 39 37 22 | 33 44 26 31 27 33 24
R20 | 3041 32 117 64 47 57 20 24 | 26 49 32 28 30 31 23
R21 | 2396 7 28 12 11 23 24 7 | 26 20 30 29 30 33 25
------+-----------------------------------------+-------------------------------------
RMS | 1801 21 53 33 23 27 24 |T 52 42 50 55 53 52 48
WRMS | 1801 17 36 24 23 24 23 |NE 46 38 44 48 47 48 42
MEDI | 1302 13 28 21 15 17 22 |MD 56 44 54 56 46 41 49
Table 3.2216.4 GPS week: 2216 Day: 4 MJD: 59760
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 659 56 54 51 33 32 54 20 | 69 28 41 59 40 50 41
R02 | 3441 11 52 9 22 13 20 9 | 51 26 50 66 51 59 52
R03 | 799 8 37 14 22 15 25 8 | 62 44 54 74 57 70 61
XR04M | 1544 15 19 10 --- 15 25 8 | 72 58 69 --- 74 61 68
R05M | 1183 15 25 18 15 15 18 7 | 47 30 46 35 50 47 42
R07 | 2015 12 32 17 16 23 33 9 | 67 39 52 71 54 83 61
R08 | 1817 8 38 20 6 17 62 11 | 66 42 54 66 69 119 68
R09 | 3322 11 14 24 17 19 23 8 | 19 20 33 33 20 43 25
XR11 | 3920 --- 31 15 19 19 33 11 | --- 120 105 111 100 121 107
R12M | 1571 12 19 17 12 13 19 6 | 122 115 128 123 119 120 121
R13M | 684 31 38 26 30 38 58 16 | 131 131 133 131 119 160 129
R14M | 1019 13 30 20 12 13 21 7 | 59 40 71 63 65 55 60
R15 | 1142 9 19 10 15 16 21 6 | 54 46 58 57 60 68 57
R17 | 1162 7 39 17 7 17 38 9 | 19 16 20 22 29 35 19
R18 | 1103 11 24 28 18 12 15 8 | 21 24 23 19 24 18 19
R19 | 799 38 105 70 36 51 44 24 | 42 58 28 41 35 22 30
R20 | 2064 56 128 52 22 51 31 24 | 53 76 37 57 22 34 35
R21 | 2579 12 29 12 9 13 23 6 | 30 31 31 29 37 35 30
------+-----------------------------------------+-------------------------------------
RMS | 1804 25 52 30 20 26 35 |T 57 52 57 62 56 66 56
WRMS | 1804 18 36 22 16 20 31 |NE 46 43 45 54 46 58 46
MEDI | 1183 12 31 17 17 16 25 |MD 54 40 50 59 51 55 52
Table 3.2216.5 GPS week: 2216 Day: 5 MJD: 59761
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1014 38 64 69 44 32 42 21 | 63 44 32 69 41 77 49
R02 | 4031 15 38 10 17 17 26 8 | 45 25 38 44 41 46 39
R03 | 1051 10 36 12 17 14 19 7 | 104 96 100 106 98 101 100
XR04M | 1213 15 23 18 --- 22 25 10 | 88 120 91 --- 91 92 89
R05M | 790 17 24 16 28 19 15 8 | 40 28 42 37 44 34 34
R07 | 1161 12 35 30 25 23 32 11 | 86 76 70 89 72 99 80
R08 | 1307 9 37 17 24 18 33 9 | 80 76 77 98 83 94 83
R09 | 2068 10 21 21 20 12 13 7 | 21 30 27 33 25 28 24
XR11 | 4123 --- 22 14 17 15 17 8 | --- 170 178 174 174 173 174
R12M | 847 8 24 15 15 14 29 7 | 162 158 160 158 159 167 161
R13M | 852 34 48 50 41 49 40 19 | 215 213 197 209 216 218 212
R14M | 721 8 18 12 24 10 26 7 | 67 64 63 52 65 65 60
R15 | 1197 8 20 15 23 11 18 7 | 53 56 65 49 63 57 55
R17 | 755 9 31 12 13 15 33 8 | 22 23 24 26 28 27 22
R18 | 1269 10 34 22 14 8 21 7 | 23 19 21 27 26 23 21
R19 | 1303 42 145 65 36 71 25 28 | 43 40 37 45 39 35 35
R20 | 1355 27 72 68 54 45 24 21 | 38 65 44 38 40 29 33
R21 | 1165 7 29 12 11 23 35 9 | 31 33 31 33 36 40 30
------+-----------------------------------------+-------------------------------------
RMS | 1517 20 52 35 28 29 28 |T 69 74 72 75 74 78 72
WRMS | 1517 15 36 25 18 19 27 |NE 50 57 57 63 58 63 57
MEDI | 1165 10 31 16 23 17 25 |MD 53 56 44 49 44 57 49
Table 3.2216.6 GPS week: 2216 Day: 6 MJD: 59762
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1338 53 67 59 33 43 45 21 | 92 50 33 69 48 78 52
R02 | 3630 12 34 7 13 16 26 8 | 64 39 59 73 56 68 60
R03 | 1121 12 29 14 13 9 26 7 | 124 109 112 128 119 119 119
XR04M | 1155 18 --- 12 --- 11 24 9 | 186 --- 184 --- 183 176 182
R05M | 889 13 45 20 18 17 24 9 | 57 45 62 57 60 66 55
R07 | 819 14 38 23 15 15 21 9 | 100 87 83 99 87 106 93
R08 | 608 9 33 14 9 18 16 7 | 99 90 95 109 99 110 100
R09 | 1931 19 22 13 14 13 13 7 | 49 57 48 57 46 49 48
XR11 | 3494 --- 19 20 22 21 21 10 | --- 249 246 244 252 248 247
R12M | 836 11 19 20 14 16 21 7 | 162 156 168 163 162 161 162
R13M | 1155 42 52 31 31 39 16 16 | 351 331 350 354 339 352 346
R14M | 840 16 23 19 10 16 30 8 | 131 129 136 134 126 147 133
R15 | 699 7 15 10 14 12 10 5 | 80 76 83 83 75 80 79
R17 | 581 8 30 9 9 11 23 6 | 29 30 27 31 31 44 29
R18 | 1046 10 32 18 8 13 27 7 | 26 30 24 29 27 32 25
R19 | 2197 41 182 64 27 66 34 24 | 36 42 35 35 32 41 32
R20 | 1443 38 82 75 54 40 29 23 | 46 58 38 37 34 33 36
R21 | 587 7 35 11 9 17 29 8 | 33 30 28 28 32 42 29
------+-----------------------------------------+-------------------------------------
RMS | 1451 24 60 33 22 27 26 |T 97 94 100 101 100 108 101
WRMS | 1451 22 37 25 12 19 25 |NE 64 72 70 78 72 80 73
MEDI | 1046 13 33 18 14 16 24 |MD 80 58 62 73 60 78 60
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