[IGSREPORT-30153] Wk 2336 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 1 03:11:08 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2336 (Oct 13, 2024 - Oct 19, 2024)
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 2.2336.
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:
igl2336[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2336 in the SP3 format.
igl23367.sum Combination Report for GPS Week 2336.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
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 | 6.6 ns
1 | 4.3 ns
2 | 6.2 ns
3 | 6.8 ns
4 | 4.6 ns
5 | 7.6 ns
6 | 6.8 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 1.2336, 1a.2336).
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 2.2336.0-6)
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 3.2336.0-6).
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 2336 summary. (Oct 13, 2024 - Oct 19, 2024)
Table 1.2336.a GPS week : 2336 MJD: 60596.0-60602.0
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 3 -7 1 39 .12 21 19 | -1866 -840 3794 14426
| 1 1 1 15 9 28 .03 | 1527 1697
esa n/a| 0 0 -1 -30 -17 3 -.06 27 21 | 11352 -993 3187 7744
| 1 1 1 8 19 31 .05 | 3779 1767
gfz n/a| 0 0 3 42 11 -14 .04 20 15 | 0 -877 3212 7194
| 0 1 1 11 13 21 .08 | 0 1784
grg n/a| 0 0 -1 -28 -11 -26 .31 25 20 | 4085 -813 3854 14105
| 1 1 1 18 20 75 .04 | 2485 1600
iac n/a| 1 0 -6 24 33 -8 -.14 18 16 | 6529 -550 3775 13715
| 1 1 2 22 27 74 .09 | 2220 880
jgx n/a| 0 0 3 -20 -37 31 -.24 24 23 | 2614 -1018 3153 7228
| 1 1 2 10 13 19 .03 | 1446 1872
Table 1.2336.b GPS week : 2336 MJD: 60596.0-60602.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 14 12 15 12 14 14 16 |
R02 | 8 7 9 7 7 8 8 |
R03 | 7 7 7 6 6 6 7 |
R04 | 7 7 6 7 7 6 5 |
R05 | 4 7 9 6 7 6 7 |
R07 | 6 7 7 6 7 7 7 |
R08 | 8 7 7 7 8 7 5 |
R09 | 7 8 9 9 7 7 7 |
R11 | 5 6 6 6 6 6 6 |
R12 | 8 6 8 8 8 7 7 |
R14 | 9 7 7 8 8 7 7 |
R15 | 7 8 7 7 9 9 7 |
R16 | 9 8 9 8 8 9 10 |
R17 | 7 8 8 7 6 7 6 |
R18 | 7 8 8 7 8 8 8 |
R19 | 24 24 26 22 23 21 25 |
R20 | 20 17 19 17 17 14 19 |
R21 | 7 8 10 8 9 9 7 |
R22 | 6 8 7 7 7 10 8 |
R24 | 9 7 7 8 7 8 9 |
R25 | 9 10 15 12 11 15 10 |
R26 | 21 26 24 33 37 41 28 |
Table 1.2336.c GPS week : 2336 MJD: 60596.0-60602.0
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 2336 0 | 6 36 163 -587 2052 -732 81.9 1825 1825 | 6639 0
brd 2336 1 | 29 -31 105 837 1797 -2873 81.9 2402 2402 | 4258 0
brd 2336 2 | -22 -56 124 -2872 2349 -2835 81.0 1882 1882 | 6222 0
brd 2336 3 | 6 116 173 -683 289 -504 80.8 1657 1657 | 6801 0
brd 2336 4 | -43 9 182 1523 1042 -453 82.4 1892 1892 | 4633 0
brd 2336 5 | 10 23 196 -65 3461 6601 80.6 2234 2234 | 7615 0
brd 2336 6 | -51 -53 71 -297 -508 8638 80.8 2288 2288 | 6763 0
-------------+------------------------------------------------------------+----------------
brd 2336 mean| -9 6 145 -306 1497 1120 81.3 2025 2025 | 6133 0
brd 2336 sdev| 30 60 45 1385 1333 4595 .7 279 279 | 1229 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 2.2336.0 GPS week: 2336 Day: 0 MJD: 60596
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 -2 -14 -15 .07 23 20 | -2196 -125 4653 19831
esa n/a| 0 -1 0 -22 -44 -41 -.08 27 21 | 17000 -412 3572 7738
gfz n/a| 0 2 1 56 18 -41 -.06 22 16 | 0 -1135 3538 7050
grg n/a| 0 0 -1 -5 -43 -3 .34 24 19 | 3086 -760 4705 19928
iac n/a| 0 -1 -5 0 63 59 -.05 15 12 | 5008 -3 4630 18752
jgx n/a| 0 0 4 -20 -19 34 -.20 27 27 | 4785 -1419 3520 7109
Table 2.2336.1 GPS week: 2336 Day: 1 MJD: 60597
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 3 -26 -5 49 .07 19 15 | -3221 -1833 3993 18270
esa n/a| 1 -1 -1 -28 -42 43 -.13 27 22 | 9995 -1662 3189 10056
gfz n/a| 2 0 4 46 2 -7 .05 19 16 | 0 -1883 3238 7722
grg n/a| -2 0 0 -44 0 126 .29 26 21 | 1461 -2029 4077 18566
iac n/a| 0 0 -9 9 48 -158 -.07 16 15 | 4008 -900 3958 17315
jgx n/a| -2 -1 8 -9 -51 52 -.27 27 27 | 2043 -1998 3240 7652
Table 2.2336.2 GPS week: 2336 Day: 2 MJD: 60598
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 -7 7 60 .12 19 18 | -4218 1279 3941 18432
esa n/a| -2 0 -4 -30 -15 40 -.08 29 20 | 10768 186 3032 7935
gfz n/a| 0 2 0 41 32 14 .18 20 13 | 0 1275 2999 7713
grg n/a| 0 -1 -1 -47 16 -80 .32 26 23 | 1436 1976 4066 18580
iac n/a| 3 2 -5 55 -19 -29 -.25 23 21 | 4537 618 3909 17381
jgx n/a| 0 0 3 -14 -19 60 -.26 25 23 | 1607 1629 2918 7698
Table 2.2336.3 GPS week: 2336 Day: 3 MJD: 60599
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 2 -14 -3 21 .14 16 16 | -789 -263 4016 14716
esa n/a| -1 2 -1 -17 6 -10 .02 32 27 | 13622 -655 3426 6612
gfz n/a| 0 1 5 50 8 -9 .06 19 16 | 0 -1167 3486 6935
grg n/a| 1 -1 -2 -45 8 -54 .30 24 20 | 4383 -680 4090 14725
iac n/a| 1 -1 -7 19 25 56 -.27 17 15 | 7246 -65 4002 13818
jgx n/a| 0 -3 2 -7 -44 23 -.25 21 21 | 4089 -1540 3358 7202
Table 2.2336.4 GPS week: 2336 Day: 4 MJD: 60600
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 2 -22 9 45 .16 21 20 | -959 -3561 2695 8044
esa n/a| 0 0 1 -34 -14 13 -.06 27 25 | 6782 -3674 2691 8097
gfz n/a| 0 0 5 40 12 -21 -.06 18 12 | 0 -2827 2710 7426
grg n/a| 2 0 -2 -11 -24 -48 .38 24 19 | 5900 -2682 2717 6889
iac n/a| 0 -1 -8 18 40 7 -.13 19 16 | 7116 -944 2693 8065
jgx n/a| 1 0 2 -28 -44 4 -.26 26 25 | 911 -2724 2646 7374
Table 2.2336.5 GPS week: 2336 Day: 5 MJD: 60601
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 18 13 48 .11 24 19 | 264 -2019 3024 7116
esa n/a| 1 0 -2 -42 -7 3 -.08 23 18 | 14158 -2431 3021 6282
gfz n/a| 1 -1 2 20 -10 3 .08 18 17 | 0 -2273 3069 6309
grg n/a| 2 0 -4 -13 -16 -105 .25 23 17 | 8416 -1897 3080 5925
iac n/a| 0 0 -2 14 56 23 -.05 17 16 | 10457 -2119 3019 7075
jgx n/a| -1 2 4 -24 -49 24 -.24 20 19 | 3255 -2693 2941 6383
Table 2.2336.6 GPS week: 2336 Day: 6 MJD: 60602
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 -3 3 1 5 66 .14 26 21 | -1948 638 4239 14578
esa n/a| 0 -2 -1 -39 -5 -24 .01 23 17 | 7141 1692 3380 7491
gfz n/a| 0 0 2 45 14 -40 .04 21 16 | 0 1871 3444 7209
grg n/a| 1 2 -1 -28 -17 -17 .29 26 22 | 3913 381 4244 14125
iac n/a| 2 0 -7 56 22 -22 -.13 19 17 | 7336 -441 4217 13605
jgx n/a| -2 0 0 -36 -32 21 -.23 20 20 | 1609 1614 3450 7184
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 3.2336.0 GPS week: 2336 Day: 0 MJD: 60596
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1028 37 27 21 34 15 54 14 | 44 39 40 44 45 46 41
R02 | 719 8 22 22 20 10 18 7 | 31 40 39 31 33 17 30
R03 | 1006 10 10 16 19 6 23 6 | 36 44 45 48 43 38 41
R04 | 845 20 16 13 11 8 17 6 | 38 45 38 35 35 30 35
R05 | 1492 8 13 8 9 9 9 4 | 31 40 34 35 33 29 31
R07 | 2548 11 14 14 9 7 22 5 | 36 44 46 39 38 32 37
R08 | 995 20 15 18 16 18 14 7 | 37 43 47 41 52 36 42
R09E | 3311 15 14 20 13 11 20 7 | 70 73 80 75 76 60 74
R11E | 1163 12 11 8 11 7 11 4 | 51 61 59 58 58 59 57
R12E | 1174 14 11 14 24 17 20 7 | 149 150 151 152 143 150 148
R14E | 3281 8 32 15 23 19 11 8 | 94 95 94 96 96 90 93
R15E | 3809 8 21 14 20 13 15 7 | 73 81 80 70 77 76 75
R16E | 1048 10 30 22 22 12 18 8 | 98 92 93 100 95 93 94
R17 | 527 9 17 27 11 9 19 7 | 71 68 81 75 68 60 70
R18 | 467 16 25 17 10 15 11 7 | 54 71 61 59 62 54 58
R19 | 1415 60 69 27 70 26 69 24 | 89 67 106 106 99 66 87
R20 | 1092 49 54 63 33 28 42 20 | 88 69 82 85 81 70 76
R21 | 1528 10 21 10 8 17 27 7 | 76 70 70 79 71 61 70
R22 | 2383 11 14 14 8 12 17 5 | 52 56 57 60 44 46 51
R24 | 1352 27 20 17 16 13 21 8 | 65 63 56 57 58 48 56
XR25 | 9595 12 15 --- --- 11 --- 8 | 39 45 --- --- 35 --- 38
XR26 |45305 20 --- --- 32 33 --- 20 | 133 --- --- 127 147 --- 135
------+-----------------------------------------+-------------------------------------
RMS | 1825 23 27 22 24 15 27 |T 66 64 67 70 67 58 65
WRMS | 1825 20 21 16 19 12 27 |NE 57 53 57 61 59 45 56
MEDI | 1174 12 17 16 16 12 18 |MD 54 63 59 60 58 54 57
Table 3.2336.1 GPS week: 2336 Day: 1 MJD: 60597
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1750 26 17 30 32 17 43 12 | 41 44 42 48 44 62 43
R02 | 685 16 20 10 15 15 12 6 | 32 37 30 31 31 30 29
R03 | 799 14 20 17 9 12 20 7 | 36 52 50 43 37 37 40
R04 | 1553 10 13 16 13 13 25 6 | 37 45 49 39 32 36 38
R05 | 901 12 13 10 13 13 27 6 | 32 38 39 42 24 33 32
R07 | 2813 9 16 13 17 12 22 6 | 37 39 38 43 30 32 34
R08 | 1370 10 12 13 13 19 23 7 | 34 36 42 43 36 37 35
R09E | 3965 15 14 18 24 16 17 7 | 79 79 78 87 68 66 76
R11E | 1033 15 19 12 14 10 10 6 | 61 70 66 73 59 68 64
R12E | 1384 12 10 17 15 11 15 6 | 81 78 75 79 83 76 78
R14E | 3224 10 18 16 21 10 14 6 | 95 104 101 108 86 97 97
R15E | 1586 12 20 16 20 22 13 8 | 66 62 63 75 59 68 63
R16E | 856 12 26 21 21 13 7 7 | 66 76 66 66 65 67 66
R17 | 760 8 22 19 19 11 30 8 | 47 43 48 59 45 37 45
R18 | 596 12 18 14 22 13 31 8 | 44 46 49 52 35 36 42
R19 | 877 48 75 37 63 37 68 23 | 53 45 75 55 55 51 53
R20 | 6391 39 54 31 56 13 31 17 | 70 66 68 73 57 56 60
R21 | 728 7 22 6 29 10 33 8 | 54 54 49 63 43 51 50
R22 | 4451 11 25 17 16 18 18 7 | 40 39 46 50 34 25 36
R24 | 1722 15 18 10 14 20 16 7 | 51 50 48 50 40 52 45
XR25 |11619 12 15 --- --- 13 --- 9 | 45 49 --- --- 42 --- 46
XR26 |40466 30 --- --- 35 42 --- 26 | 87 --- --- 88 89 --- 86
------+-----------------------------------------+-------------------------------------
RMS | 2402 19 27 19 26 16 27 |T 54 54 56 60 49 50 52
WRMS | 2402 15 22 16 21 15 27 |NE 46 45 48 51 42 41 44
MEDI | 1384 12 18 16 19 13 20 |MD 47 49 49 55 43 51 45
Table 3.2336.2 GPS week: 2336 Day: 2 MJD: 60598
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1610 35 12 19 38 26 53 15 | 43 45 51 43 52 33 40
XR02 | 1696 13 14 12 20 25 --- 8 | 28 34 32 37 35 --- 29
R03 | 1552 11 20 11 13 11 19 6 | 35 39 35 30 31 31 31
R04 | 1958 16 12 10 8 16 15 6 | 34 36 34 31 32 29 31
R05 | 890 11 16 27 11 28 20 9 | 32 36 38 34 25 27 27
R07 | 1442 13 18 14 11 17 12 6 | 31 31 40 32 32 34 30
R08 | 1556 18 12 13 10 21 12 6 | 32 40 40 30 36 34 32
R09E | 1830 15 24 18 24 17 14 8 | 53 59 65 56 53 42 54
R11E | 1668 12 10 11 12 18 14 6 | 50 53 51 45 51 59 51
R12E | 1249 14 16 16 13 31 13 8 | 95 97 104 97 96 92 96
R14E | 1844 10 20 14 23 15 12 7 | 69 76 71 65 71 66 67
R15E | 1873 11 14 14 20 16 16 6 | 98 110 103 102 88 105 99
R16E | 747 11 24 24 21 22 11 8 | 47 62 59 60 48 47 51
R17 | 1148 8 19 13 17 27 15 7 | 69 72 72 70 74 66 69
R18 | 853 10 19 8 10 19 31 8 | 43 49 46 44 48 37 42
R19 | 634 38 82 42 75 40 62 25 | 64 43 86 78 72 54 63
R20 | 3485 45 63 41 31 31 28 18 | 75 45 61 62 62 56 56
R21 | 931 12 23 18 27 33 17 10 | 58 45 45 66 59 50 51
R22 | 4531 17 18 6 26 11 12 7 | 59 61 64 64 57 56 59
R24 | 1400 7 15 20 17 20 10 7 | 46 51 60 48 46 44 47
XR25 |18391 14 20 --- --- 28 --- 14 | 32 29 --- --- 38 --- 27
XR26 |26314 17 --- --- 33 49 --- 24 | 134 --- --- 109 134 --- 125
------+-----------------------------------------+-------------------------------------
RMS | 1881 19 29 20 26 23 25 |T 55 53 57 57 56 50 53
WRMS | 1881 18 20 13 23 21 23 |NE 50 43 50 51 52 42 47
MEDI | 1556 13 18 14 20 21 15 |MD 47 45 51 56 51 47 51
Table 3.2336.3 GPS week: 2336 Day: 3 MJD: 60599
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1641 32 23 20 33 18 32 12 | 42 43 34 39 30 36 34
XR02 | 1445 11 15 13 16 11 --- 6 | 26 30 32 42 27 --- 28
R03 | 2236 14 16 12 7 14 17 6 | 37 42 37 44 51 43 41
R04 | 1249 14 15 15 6 13 19 6 | 35 38 36 30 29 28 31
R05 | 950 14 13 12 9 10 22 6 | 31 39 34 34 35 26 31
R07 | 905 6 13 13 11 21 14 6 | 32 33 31 29 31 29 29
R08 | 704 16 12 18 15 17 17 7 | 28 30 38 29 37 35 30
XR09E |12367 12 14 19 23 20 --- 9 | 25 31 37 33 38 --- 28
R11E | 2174 15 12 14 12 13 14 6 | 27 39 40 28 30 34 31
R12E | 817 14 13 22 12 21 17 7 | 154 150 156 144 145 152 150
R14E | 2593 12 18 11 28 16 11 7 | 45 46 37 50 40 33 39
R15E | 2269 12 15 10 14 16 18 6 | 57 65 62 53 61 56 57
R16E | 1675 11 30 22 20 14 14 8 | 81 77 87 75 77 81 78
R17 | 775 9 13 21 20 10 13 6 | 50 45 52 36 37 38 42
R18 | 714 14 21 9 14 14 23 7 | 40 53 44 51 43 41 43
R19 | 808 23 93 40 65 35 41 22 | 83 48 103 106 76 70 79
R20 | 1908 30 66 35 37 24 29 16 | 70 40 76 68 64 52 61
R21 | 1034 11 22 15 18 20 15 7 | 54 47 48 58 64 48 52
R22 | 3140 13 13 12 18 11 20 6 | 30 39 37 39 31 40 33
R24 | 1234 12 23 17 22 13 17 7 | 45 53 45 55 40 34 42
XR25 |16521 15 18 --- --- 19 --- 12 | 30 29 --- --- 36 --- 29
XR26 |36857 36 --- --- 37 60 --- 33 | 88 --- --- 78 78 --- 77
------+-----------------------------------------+-------------------------------------
RMS | 1656 16 32 19 24 17 21 |T 50 48 53 53 50 48 48
WRMS | 1656 16 27 16 20 15 21 |NE 45 40 46 49 44 40 42
MEDI | 1445 14 15 15 18 16 17 |MD 40 42 38 44 38 38 39
Table 3.2336.4 GPS week: 2336 Day: 4 MJD: 60600
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1775 39 12 27 29 22 50 14 | 43 33 37 41 31 41 33
XR02 | 1283 16 13 13 17 12 --- 7 | 27 32 34 31 30 --- 28
R03 | 2211 12 17 8 11 11 15 5 | 34 32 39 38 35 35 34
R04 | 1563 20 15 13 12 9 22 7 | 38 34 31 39 37 31 33
R05 | 816 20 17 12 20 9 15 7 | 40 35 24 32 30 29 28
R07 | 1477 11 15 17 14 13 19 6 | 34 34 48 33 37 27 34
R08 | 702 22 14 19 15 12 24 8 | 30 36 44 40 40 28 35
XR09E |15838 16 10 10 15 16 --- 7 | 54 51 57 60 52 --- 53
R11E | 3775 15 13 7 14 12 16 5 | 46 53 56 50 48 57 50
R12E | 2552 20 16 9 17 24 15 8 | 127 128 128 123 105 121 121
R14E | 1268 11 14 16 30 16 16 8 | 64 61 63 66 62 64 62
R15E | 3893 12 14 10 34 25 22 9 | 71 69 66 94 61 74 70
R16E | 1963 12 15 18 20 21 12 7 | 56 47 56 67 44 55 52
R17 | 894 12 16 15 13 14 13 6 | 45 51 50 47 37 42 44
R18 | 797 13 29 13 22 12 16 8 | 43 56 47 45 41 39 43
R19 | 1061 42 74 30 60 33 62 22 | 84 49 87 95 83 68 76
R20 | 1078 34 59 40 24 32 34 17 | 68 34 79 79 62 52 60
R21 | 1022 15 23 20 13 13 26 8 | 53 50 60 50 49 43 49
R22 | 1663 18 10 14 14 14 16 6 | 60 58 63 53 53 55 56
R24 | 1282 12 22 13 13 14 23 7 | 48 51 42 47 49 34 43
XR25 |14309 14 18 --- --- 13 --- 10 | 26 36 --- --- 39 --- 32
XR26 |74410 57 --- --- 39 55 --- 36 | 180 --- --- 138 144 --- 150
------+-----------------------------------------+-------------------------------------
RMS | 1891 21 27 18 24 19 26 |T 57 49 55 60 53 49 53
WRMS | 1891 20 25 12 19 16 25 |NE 53 41 48 53 49 40 48
MEDI | 1477 15 15 13 17 14 16 |MD 46 49 50 50 44 42 44
Table 3.2336.5 GPS week: 2336 Day: 5 MJD: 60601
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1614 45 25 13 33 12 39 13 | 30 36 26 24 26 31 25
XR02 | 1255 8 13 20 14 20 --- 8 | 18 31 27 22 23 --- 19
R03 | 1268 11 16 12 16 15 8 6 | 23 35 36 35 33 39 31
R04 | 2450 9 20 12 11 13 10 5 | 22 38 26 21 23 24 22
R05 | 1412 13 13 15 14 10 17 6 | 21 22 16 23 19 16 15
R07 | 1487 7 16 11 13 19 18 6 | 28 40 32 23 41 24 29
R08 | 964 19 13 17 11 8 15 6 | 22 33 30 31 26 25 26
R09E | 1112 13 8 13 11 21 14 6 | 56 53 55 57 58 71 55
R11E | 4072 15 11 11 14 13 12 5 | 38 41 38 46 40 41 39
R12E | 3831 12 14 16 20 16 17 7 | 123 126 131 127 131 128 127
R14E | 1219 11 14 17 21 18 12 7 | 63 67 73 64 67 60 65
R15E | 4766 18 17 11 30 16 18 8 | 52 48 44 55 45 51 46
R16E | 3373 11 19 14 29 16 21 8 | 119 117 123 117 113 122 117
R17 | 788 14 15 16 15 14 14 6 | 37 33 25 43 33 30 30
R18 | 723 20 20 16 11 15 17 7 | 37 42 32 42 43 35 37
R19 | 981 62 59 37 59 23 39 21 | 62 44 70 54 50 50 51
R20 | 1416 42 49 26 19 23 20 14 | 60 40 68 43 53 52 48
R21 | 695 14 21 20 24 19 20 9 | 40 37 47 48 31 32 35
R22 | 2237 16 15 28 14 31 8 9 | 65 73 74 67 55 72 65
R24 | 1314 16 17 19 12 13 23 7 | 48 49 44 43 52 39 44
XR25 |16682 17 21 --- --- 22 --- 14 | 20 24 --- --- 40 --- 24
XR26 |65633 43 --- --- 56 68 --- 41 | 169 --- --- 160 188 --- 173
------+-----------------------------------------+-------------------------------------
RMS | 2233 24 23 18 23 17 20 |T 52 49 50 54 54 49 51
WRMS | 2233 19 18 17 17 16 19 |NE 43 38 39 45 46 36 42
MEDI | 1412 14 16 16 15 16 17 |MD 38 40 38 43 41 39 37
Table 3.2336.6 GPS week: 2336 Day: 6 MJD: 60602
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 988 41 30 21 45 24 46 16 | 56 45 47 44 43 40 40
R02 | 1146 8 19 8 12 24 19 7 | 32 41 36 39 35 22 32
R03 | 1108 15 12 16 21 21 8 7 | 39 47 47 48 48 41 44
R04 | 1944 10 11 12 13 10 10 5 | 39 42 40 37 35 34 37
R05 | 1258 9 15 17 10 9 22 6 | 35 37 37 34 30 28 31
R07 | 1095 16 14 13 24 11 7 6 | 43 41 42 40 43 37 39
R08 | 757 11 8 13 14 13 10 5 | 35 40 47 42 45 37 40
R09E | 1066 18 8 18 15 18 12 7 | 82 79 80 84 85 79 80
R11E | 1746 16 10 13 10 15 8 5 | 60 63 62 59 63 64 61
R12E | 2041 11 14 11 15 19 13 6 | 115 116 116 114 107 109 112
R14E | 2272 10 17 14 21 15 13 7 | 103 106 106 110 111 104 106
R15E | 4827 11 12 13 18 19 18 7 | 69 71 77 80 72 70 72
R16E | 5829 11 28 21 28 24 18 10 | 114 116 110 103 112 103 108
R17 | 1245 14 10 12 16 9 17 6 | 66 54 64 66 55 51 58
R18 | 851 15 19 12 20 20 19 8 | 59 71 61 61 61 51 59
R19 | 1323 69 70 50 61 29 43 24 | 95 74 116 105 100 69 90
R20 | 3060 62 30 48 50 32 19 18 | 98 59 95 86 78 77 78
R21 | 843 13 23 13 15 10 9 6 | 78 68 79 80 76 69 74
R22 | 2768 16 13 17 15 15 20 7 | 66 71 75 75 62 73 69
R24 | 1224 27 17 25 13 11 18 8 | 72 71 64 61 64 57 63
XR25 |15448 11 15 --- --- 12 --- 9 | 30 33 --- --- 32 --- 29
XR26 |35886 38 --- --- 29 47 --- 28 | 184 --- --- 163 189 --- 178
------+-----------------------------------------+-------------------------------------
RMS | 2288 26 23 21 26 19 20 |T 71 64 70 72 70 60 68
WRMS | 2288 21 17 16 22 17 20 |NE 64 52 60 65 62 49 60
MEDI | 1258 14 15 13 16 15 17 |MD 66 63 64 66 62 57 61
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