[IGSREPORT-29861] Wk 2310 IGLOS Final Orbits
acc
acc at igs.org
Mon May 6 00:15:45 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2310 (Apr 14, 2024 - Apr 20, 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 2.2310.
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:
igl2310[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2310 in the SP3 format.
igl23107.sum Combination Report for GPS Week 2310.
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 | 1.0 ns
1 | 3.1 ns
2 | 5.3 ns
3 | 4.8 ns
4 | 2.0 ns
5 | 5.0 ns
6 | 4.2 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 | ESA | R20
1 | ESA | R20
2 | ESA | R20
3 | ESA | R20
4 | ESA | R20
5 | ESA | R20
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 1.2310, 1a.2310).
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 2.2310.0-6)
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 3.2310.0-6).
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 2310 summary. (Apr 14, 2024 - Apr 20, 2024)
Table 1.2310.a GPS week : 2310 MJD: 60414.0-60420.0
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 2 -13 -25 56 .07 18 15 | 3765 -922 3377 11812
| 1 0 1 20 21 17 .03 | 2135 1617
esa n/a| 0 0 3 -20 14 -51 -.05 42 22 | 2929 -296 3234 7160
| 1 1 1 13 17 12 .03 | 5105 1693
gfz n/a| 1 0 -2 14 3 -39 .06 22 16 | 0 -711 3244 7034
| 1 1 3 15 12 19 .06 | 0 1891
grg n/a| 0 0 3 7 5 65 .24 28 21 | 4500 -917 3394 11386
| 2 2 2 18 19 47 .04 | 3264 1818
iac n/a| 0 0 -6 -3 -7 -21 -.13 20 16 | 6592 -324 3405 12847
| 1 0 4 12 23 45 .05 | 2917 517
jgx n/a| 0 -1 -1 28 34 -17 -.16 30 26 | 5281 -481 3333 7414
| 1 2 2 27 26 33 .04 | 1299 1753
Table 1.2310.b GPS week : 2310 MJD: 60414.0-60420.0
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 | 12 11 11 11 12 10 14 |
R02 | 7 6 5 6 6 7 7 |
R03 | 6 7 5 8 6 9 7 |
R04 | 6 4 7 7 7 7 7 |
R05 | 7 6 7 7 6 7 7 |
R07 | 10 0 15 20 10 16 11 |
R08 | 8 9 8 6 7 7 6 |
R09 | 7 6 7 7 6 6 6 |
R11 | 6 6 6 6 6 5 7 |
R12 | 7 8 8 8 8 9 8 |
R13 | 18 16 17 17 21 16 14 |
R14 | 8 7 8 7 8 8 7 |
R15 | 7 7 7 9 8 8 7 |
R16 | 8 9 9 10 9 7 7 |
R17 | 8 11 10 8 8 9 8 |
R18 | 8 9 8 7 6 8 7 |
R19 | 23 22 20 17 19 18 19 |
R20 | 28 23 25 30 26 26 29 |
R21 | 9 8 7 9 9 11 9 |
R22 | 7 7 6 6 5 6 7 |
R24 | 9 10 10 8 10 9 10 |
R25 | 12 15 14 15 8 13 11 |
R26 | 25 25 32 37 31 29 35 |
Table 1.2310.c GPS week : 2310 MJD: 60414.0-60420.0
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 2310 0 | 6 72 236 37 2058 5918 81.9 1609 1609 | 1016 0
brd 2310 1 | -175 52 152 710 -203 6065 80.0 1936 1936 | 3113 0
brd 2310 2 | -24 63 71 -1609 -132 10540 80.6 2131 2131 | 5265 0
brd 2310 3 | 73 8 103 -2543 -1724 6502 78.9 1852 1852 | 4770 0
brd 2310 4 | 8 25 178 -2223 -147 2295 81.3 1714 1714 | 2040 0
brd 2310 5 | -16 -53 110 -840 157 3374 81.0 1543 1543 | 4957 0
brd 2310 6 | 46 -85 206 1413 2561 5925 78.1 1471 1471 | 4211 0
-------------+------------------------------------------------------------+----------------
brd 2310 mean| -11 11 151 -722 366 5802 80.3 1750 1750 | 3624 0
brd 2310 sdev| 79 60 59 1503 1467 2621 1.4 235 235 | 1617 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 2.2310.0 GPS week: 2310 Day: 0 MJD: 60414
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 2 21 -47 61 .09 19 17 | 1708 -1569 3610 8160
esa n/a| 2 -3 3 -41 -2 -37 -.03 48 24 | -2116 -533 3618 7506
gfz n/a| 1 -1 -6 7 -4 -49 .05 26 15 | 0 -850 3629 7551
grg n/a| -1 1 7 -3 20 19 .27 24 20 | -1929 -1337 3650 7911
iac n/a| -2 -1 -11 -17 -14 6 -.19 20 17 | 535 -275 3591 8176
jgx n/a| 0 2 0 -2 60 -22 -.21 31 31 | 6166 -718 3885 8251
Table 2.2310.1 GPS week: 2310 Day: 1 MJD: 60415
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 -4 -9 45 .06 15 14 | 6782 -2636 3642 13395
esa n/a| 1 0 4 -15 14 -43 -.04 46 23 | 1077 -1967 3423 7092
gfz n/a| 3 -3 -6 19 -7 -17 .07 21 15 | 0 -2886 3318 7061
grg n/a| -1 0 4 -19 7 8 .25 29 24 | 6145 -2392 3553 13374
iac n/a| -1 0 -8 18 14 -5 -.05 20 17 | 7270 -263 3693 14765
jgx n/a| 0 0 1 9 8 -18 -.22 29 31 | 7309 -2920 3325 7449
Table 2.2310.2 GPS week: 2310 Day: 2 MJD: 60416
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 1 -17 -2 73 .08 14 12 | 5834 -1908 3305 15014
esa n/a| 3 0 4 -15 46 -47 -.09 43 23 | 6750 -1818 2919 7790
gfz n/a| 2 1 0 1 0 -25 -.01 21 17 | 0 -1429 2948 6736
grg n/a| 0 -2 1 10 32 35 .24 24 19 | 8448 -2077 3352 14627
iac n/a| 0 0 -7 2 -36 -98 -.09 22 16 | 9237 -665 3374 16497
jgx n/a| 0 -2 -2 12 4 12 -.13 30 24 | 5815 -707 2964 7180
Table 2.2310.3 GPS week: 2310 Day: 3 MJD: 60417
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 0 -21 56 .08 19 15 | 3934 1853 3133 14496
esa n/a| 1 0 0 -38 -1 -71 -.02 42 22 | 9749 2293 3025 6299
gfz n/a| 2 1 -2 -7 19 -48 .11 19 13 | 0 2803 3019 6899
grg n/a| -2 -3 1 28 -9 56 .18 28 18 | 5427 2590 3133 13867
iac n/a| -1 1 0 -2 17 -30 -.17 19 16 | 8637 589 3166 16089
jgx n/a| 0 -3 -4 22 12 37 -.14 34 27 | 4334 2611 3066 7117
Table 2.2310.4 GPS week: 2310 Day: 4 MJD: 60418
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 0 -26 -61 28 .01 20 16 | 3734 -1834 3204 12993
esa n/a| 0 1 3 -18 10 -66 -.01 43 19 | 1676 -143 3038 6840
gfz n/a| 0 1 -3 37 -5 -67 .10 29 18 | 0 -1523 3069 6232
grg n/a| 2 -1 5 -2 0 118 .19 28 21 | 4426 -1950 3244 12491
iac n/a| 0 0 -3 -1 15 40 -.12 16 14 | 7017 -1123 3243 14624
jgx n/a| 0 -3 -4 61 69 -34 -.12 33 27 | 4277 -1465 3135 6475
Table 2.2310.5 GPS week: 2310 Day: 5 MJD: 60419
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 1 -39 -23 51 .08 19 18 | 3718 -1114 3261 10030
esa n/a| 0 -1 5 -7 29 -47 -.06 41 25 | 7240 -1548 3141 6337
gfz n/a| 1 0 0 24 0 -17 .11 18 12 | 0 -1802 3196 6527
grg n/a| 1 0 2 0 -25 99 .27 28 21 | 5809 -1774 3299 9441
iac n/a| -1 0 -7 -16 -18 -55 -.18 21 16 | 7847 -304 3304 11123
jgx n/a| 2 0 0 72 46 -32 -.17 32 25 | 5513 -968 3272 6819
Table 2.2310.6 GPS week: 2310 Day: 6 MJD: 60420
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 -14 79 .09 19 16 | 648 750 3487 8598
esa n/a| -1 0 4 -6 8 -43 -.06 34 20 | -3870 1642 3474 8261
gfz n/a| -1 0 0 16 21 -48 -.03 22 19 | 0 706 3532 8238
grg n/a| 3 2 0 33 10 119 .30 32 24 | 3176 516 3529 7997
iac n/a| 0 0 -9 -10 -33 -3 -.10 19 15 | 5602 -227 3468 8658
jgx n/a| 1 -1 0 22 36 -66 -.13 23 20 | 3553 796 3686 8608
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 3.2310.0 GPS week: 2310 Day: 0 MJD: 60414
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 437 32 30 21 34 18 26 12 | 63 48 53 69 57 62 56
R02 | 832 12 17 14 22 16 9 7 | 47 51 44 54 48 46 46
R03 | 2834 9 20 12 12 18 7 6 | 48 51 46 56 51 46 47
R04 | 1207 13 11 9 14 18 11 5 | 47 44 43 44 42 44 43
R05 | 911 13 16 17 13 18 10 6 | 39 38 40 35 33 36 35
XR07 |10881 19 --- 15 17 19 --- 10 | 8 --- 9 8 9 --- 5
R08 | 1310 16 10 15 17 20 20 7 | 44 51 56 45 56 49 49
R09E | 1793 11 9 14 22 11 16 6 | 57 60 65 70 62 59 61
R11E | 1459 13 15 15 12 8 13 6 | 29 37 42 34 32 29 33
R12E | 2611 14 21 13 18 17 13 7 | 64 63 65 65 61 57 61
XR13E | 2505 23 42 42 43 23 --- 17 | 97 109 120 104 89 --- 98
R14E | 1251 13 17 15 23 14 17 7 | 122 127 127 126 125 125 124
R15E | 1847 10 15 16 14 19 12 6 | 51 52 56 56 52 51 51
R16E | 2261 12 22 17 20 13 14 7 | 87 84 87 87 86 76 83
XR17 | 678 7 22 14 16 21 --- 8 | 48 39 56 51 61 --- 50
R18 | 1522 10 23 13 23 17 18 8 | 37 44 44 42 40 31 37
R19 | 1022 45 43 49 54 47 67 23 | 64 64 79 64 65 56 58
R20 | 1604 28 177 75 40 26 88 28 | 108 71 146 110 101 63 99
R21 | 1094 12 26 19 14 18 28 9 | 56 40 58 54 57 38 49
XR22 | 3563 13 16 8 11 16 --- 6 | 30 38 37 43 38 --- 34
R24 | 1306 20 28 21 12 14 21 9 | 55 41 60 61 64 44 52
XR25 |12536 18 18 --- --- 15 --- 12 | 35 31 --- --- 31 --- 30
XR26 | 9670 25 --- --- 27 48 --- 25 | 111 --- --- 106 125 --- 113
------+-----------------------------------------+-------------------------------------
RMS | 1609 19 48 26 24 20 31 |T 58 56 63 62 60 53 57
WRMS | 1609 17 24 15 20 17 31 |NE 52 46 55 56 54 46 50
MEDI | 1522 13 20 15 17 18 16 |MD 51 51 56 56 57 49 50
Table 3.2310.1 GPS week: 2310 Day: 1 MJD: 60415
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 769 23 18 21 41 17 24 10 | 37 41 22 42 29 33 30
R02 | 709 8 14 16 20 14 12 6 | 34 38 31 38 37 42 34
R03 | 2617 15 16 15 17 19 11 7 | 37 34 33 41 37 36 33
R04 | 1088 10 8 7 8 10 9 4 | 32 32 35 33 31 27 31
R05 | 1267 11 14 12 10 19 9 6 | 31 30 37 23 26 27 28
XR07 | ---- 3 --- --- --- --- --- 0 | 40 --- --- --- --- --- 44
R08 | 1562 8 11 20 26 22 26 8 | 33 32 43 38 38 27 33
R09E | 2153 13 8 15 23 12 8 6 | 26 35 37 45 31 32 31
R11E | 1041 12 11 11 21 9 15 6 | 33 34 37 32 36 35 32
R12E | 2025 10 15 12 20 27 15 7 | 54 55 59 59 55 53 54
XR13E | 1839 28 34 36 32 23 --- 15 | 81 92 102 80 85 --- 84
R14E | 955 8 21 11 26 9 11 6 | 108 112 107 118 110 108 109
R15E | 1974 9 19 12 28 14 12 7 | 58 59 63 68 57 57 58
R16E | 1194 15 32 20 21 14 13 9 | 75 72 79 77 74 69 72
XR17 | 656 13 31 16 14 32 --- 11 | 31 27 38 35 47 --- 33
R18 | 885 14 17 10 16 20 34 8 | 30 32 27 29 33 27 26
R19 | 740 29 48 36 76 36 70 21 | 76 75 72 81 63 68 67
R20 | 4443 29 172 53 37 30 75 23 | 66 76 84 59 47 38 58
R21 | 1152 14 20 17 14 14 22 7 | 37 29 31 36 26 31 30
R22 | 3821 12 12 17 23 19 13 7 | 47 55 52 46 46 34 48
R24 | 1110 10 38 18 18 21 19 9 | 27 32 35 39 38 29 29
XR25 |11075 19 11 --- --- 29 --- 15 | 34 30 --- --- 38 --- 29
XR26 |11767 28 --- --- 22 49 --- 25 | 97 --- --- 92 98 --- 96
------+-----------------------------------------+-------------------------------------
RMS | 1936 15 46 21 29 20 29 |T 48 48 51 52 49 42 47
WRMS | 1936 14 23 15 24 17 31 |NE 43 40 41 45 42 34 40
MEDI | 1194 13 17 16 21 19 13 |MD 37 35 37 42 38 34 33
Table 3.2310.2 GPS week: 2310 Day: 2 MJD: 60416
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 612 16 25 14 39 30 14 10 | 54 57 64 74 40 59 56
R02 | 1023 8 12 8 12 10 13 4 | 38 38 34 28 33 30 33
R03 | 2038 10 12 7 15 13 12 5 | 35 43 42 40 41 41 38
R04 | 647 17 15 8 10 17 18 6 | 31 33 29 28 21 28 26
R05 | 1304 9 15 20 13 21 17 7 | 27 27 30 33 30 29 25
XR07 | ---- 8 --- --- 23 --- --- 14 | 19 --- --- 36 --- --- 19
R08 | 2144 8 22 21 20 24 14 8 | 27 37 42 28 37 33 31
R09E | 3838 13 14 16 24 12 9 6 | 27 40 39 28 35 34 31
R11E | 1056 10 11 12 15 12 14 5 | 26 33 33 37 35 30 30
R12E | 874 17 12 11 23 13 24 7 | 84 78 69 76 72 69 74
XR13E | 1084 19 43 43 31 37 --- 17 | 49 63 68 59 51 --- 50
R14E | 1238 6 23 12 35 12 16 8 | 71 73 71 77 73 77 71
R15E | 1814 10 18 14 19 17 16 6 | 54 47 53 64 45 58 51
R16E | 897 11 25 17 27 17 22 8 | 48 59 51 55 43 56 48
XR17 | 844 12 29 19 12 22 --- 9 | 32 26 47 47 47 --- 37
R18 | 715 9 18 21 13 20 25 8 | 32 38 47 39 47 26 36
R19 | 1040 27 57 37 52 45 60 20 | 54 58 52 66 41 50 45
R20 | 4891 27 156 52 24 40 89 25 | 73 47 105 76 78 53 72
R21 | 1330 9 17 24 10 13 18 7 | 41 34 54 41 36 35 39
R22 | 4421 10 11 16 19 11 9 5 | 34 33 35 45 40 40 35
R24 | 612 10 25 15 19 30 31 9 | 37 26 35 47 50 24 34
XR25 | 6928 17 18 --- --- 24 --- 13 | 35 26 --- --- 26 --- 27
XR26 |14741 25 --- --- 39 70 --- 32 | 129 --- --- 124 130 --- 128
------+-----------------------------------------+-------------------------------------
RMS | 2131 14 43 21 24 22 30 |T 45 43 50 52 47 42 45
WRMS | 2131 12 23 17 19 16 24 |NE 43 37 47 50 46 37 42
MEDI | 1084 10 18 16 19 17 16 |MD 37 38 47 45 41 35 37
Table 3.2310.3 GPS week: 2310 Day: 3 MJD: 60417
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 832 30 27 18 35 12 25 11 | 63 41 50 56 55 50 51
R02 | 1377 6 14 12 14 10 16 5 | 50 45 50 40 52 53 48
R03 | 1876 8 17 13 14 26 21 7 | 49 45 53 54 64 42 50
R04 | 1200 11 11 12 16 17 20 6 | 43 42 47 45 35 34 39
R05 | 2089 15 15 13 14 16 11 6 | 43 46 42 43 32 35 38
XR07 | ---- 14 --- --- 26 --- --- 20 | 31 --- --- 25 --- --- 30
R08 | 1628 10 16 8 11 16 14 5 | 37 35 39 38 43 37 37
R09E | 2682 19 15 12 14 7 16 6 | 31 41 45 37 35 45 37
R11E | 895 13 7 11 16 10 14 5 | 37 41 47 38 36 41 39
R12E | 1157 12 12 11 29 19 16 7 | 77 75 74 93 71 75 75
R13E | 861 28 37 43 20 32 54 16 | 43 45 61 45 41 64 42
R14E | 1091 11 22 9 27 11 13 7 | 46 52 45 53 39 44 43
R15E | 2194 8 26 15 34 14 20 9 | 69 71 74 83 70 73 70
R16E | 1187 12 35 20 28 13 15 9 | 46 65 53 55 39 40 45
XR17 | 1352 7 26 12 13 15 --- 7 | 34 31 34 36 40 --- 33
R18 | 676 9 11 15 20 16 18 6 | 28 27 30 44 28 23 26
R19 | 749 50 31 27 52 31 25 16 | 50 34 54 50 43 50 42
R20 | 2371 32 160 37 69 26 113 29 | 77 74 81 109 60 40 64
R21 | 1464 15 14 14 19 17 37 9 | 41 31 36 43 30 31 32
R22 | 4902 11 14 11 15 17 13 6 | 26 29 34 33 35 24 28
R24 | 491 9 21 19 14 17 16 7 | 36 35 47 41 40 42 38
XR25 | 8457 22 12 --- --- 24 --- 15 | 30 26 --- --- 31 --- 22
XR26 |11103 38 --- --- 42 69 --- 37 | 58 --- --- 46 64 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 1851 19 42 19 28 19 34 |T 45 44 49 50 44 44 42
WRMS | 1851 15 22 13 18 16 27 |NE 43 38 45 46 43 38 39
MEDI | 1352 12 16 13 19 16 16 |MD 43 41 47 44 40 42 39
Table 3.2310.4 GPS week: 2310 Day: 4 MJD: 60418
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 686 28 21 20 25 27 28 11 | 67 54 58 62 71 56 60
R02 | 1540 12 9 7 16 16 18 6 | 44 52 52 43 59 49 49
R03 | 1338 13 8 14 17 11 20 6 | 55 53 55 56 57 52 54
R04 | 939 11 14 13 23 6 20 6 | 52 58 57 55 52 54 53
R05 | 1970 17 11 17 10 11 17 6 | 60 52 54 50 45 45 50
XR07 | ---- 6 --- --- 12 --- --- 9 | 45 --- --- 40 --- --- 44
R08 | 2324 16 20 15 14 10 20 7 | 47 53 58 54 51 63 52
R09E | 1074 13 9 17 16 10 11 5 | 33 38 47 36 37 35 36
R11E | 1509 14 10 13 10 9 16 5 | 46 46 49 41 41 46 43
R12E | 1639 17 10 19 23 14 19 7 | 80 80 88 92 86 81 83
R13E | 797 36 41 78 33 39 57 21 | 78 86 130 76 80 47 81
R14E | 873 9 26 13 29 12 11 8 | 91 99 91 95 88 91 91
R15E | 1966 12 16 18 36 12 14 8 | 80 80 86 83 73 76 78
R16E | 1468 10 25 20 34 10 13 8 | 77 79 79 74 74 70 74
XR17 | 1281 13 17 12 17 15 --- 7 | 33 38 34 38 34 --- 33
R18 | 960 12 12 22 13 7 16 6 | 33 32 43 40 29 38 33
R19 | 872 41 21 46 66 26 52 18 | 51 35 54 55 43 34 38
R20 | 1721 34 168 49 50 21 94 25 | 77 101 94 82 61 44 66
R21 | 1051 15 23 28 14 9 33 9 | 51 47 58 45 40 55 47
R22 | 4603 12 11 14 15 8 13 5 | 38 41 37 41 37 45 37
R24 | 739 15 23 34 22 13 29 10 | 41 28 52 47 33 34 35
XR25 | 9581 12 10 --- --- 10 --- 7 | 57 49 --- --- 44 --- 49
XR26 | 9102 46 --- --- 27 48 --- 31 | 146 --- --- 142 150 --- 148
------+-----------------------------------------+-------------------------------------
RMS | 1714 20 43 29 28 16 33 |T 60 57 63 61 58 53 58
WRMS | 1714 16 19 18 21 14 27 |NE 56 49 54 56 53 47 53
MEDI | 1338 13 16 17 17 11 19 |MD 52 52 55 54 51 49 50
Table 3.2310.5 GPS week: 2310 Day: 5 MJD: 60419
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1014 23 28 14 27 20 27 10 | 47 26 43 41 39 36 35
R02 | 1208 13 19 9 12 20 14 6 | 28 37 31 28 22 35 26
R03 | 884 21 17 14 24 13 24 8 | 27 47 41 38 26 42 33
R04 | 664 9 12 11 20 15 28 7 | 26 31 35 28 36 23 26
R05 | 1347 18 12 11 13 12 18 6 | 34 34 28 20 24 24 24
XR07 | ---- 13 --- --- 18 --- --- 15 | 23 --- --- 37 --- --- 29
R08 | 2071 17 17 8 17 17 16 6 | 24 31 27 38 27 34 27
R09E | 1806 15 10 12 14 11 15 6 | 55 54 62 54 54 50 54
R11E | 2252 12 12 8 11 12 12 5 | 23 33 30 26 27 29 27
R12E | 1670 17 20 18 22 20 19 8 | 88 86 93 82 79 76 83
R13E | 1027 21 26 31 33 48 45 15 | 60 74 67 64 57 49 63
R14E | 1064 8 24 10 29 10 13 7 | 83 79 80 91 88 80 82
R15E | 1424 16 15 11 31 20 16 8 | 55 57 59 70 49 62 56
R16E | 729 10 20 13 23 10 17 7 | 54 51 52 62 56 49 52
XR17 | 1055 10 21 15 17 19 --- 8 | 30 28 26 36 33 --- 28
R18 | 1135 14 22 12 21 22 21 8 | 27 41 29 31 37 37 31
R19 | 951 43 18 38 49 37 54 18 | 41 32 42 36 32 54 27
R20 | 1640 35 159 37 67 32 86 26 | 48 66 53 68 45 37 41
R21 | 1065 10 35 21 20 18 31 10 | 40 30 41 49 39 30 36
R22 | 3542 12 16 12 10 11 14 5 | 26 36 28 34 29 37 29
R24 | 966 11 23 17 17 18 30 8 | 33 33 33 41 32 32 32
XR25 |10556 16 16 --- --- 23 --- 13 | 27 25 --- --- 38 --- 26
XR26 | 8426 26 --- --- 37 56 --- 29 | 87 --- --- 75 99 --- 87
------+-----------------------------------------+-------------------------------------
RMS | 1542 19 41 18 28 21 32 |T 42 44 45 47 44 42 41
WRMS | 1542 18 25 12 21 16 25 |NE 35 35 35 40 37 35 33
MEDI | 1135 15 19 12 20 18 19 |MD 34 36 41 38 37 37 32
Table 3.2310.6 GPS week: 2310 Day: 6 MJD: 60420
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 894 28 47 26 28 24 26 13 | 79 58 65 77 78 71 70
R02 | 978 11 22 12 17 13 19 7 | 55 57 53 59 59 57 55
R03 | 857 11 14 19 20 13 9 6 | 58 60 62 68 63 61 61
R04 | 837 11 12 26 17 13 15 7 | 56 52 58 54 52 57 54
R05 | 1049 20 10 13 19 15 15 7 | 59 53 57 46 47 53 51
XR07 | 9210 7 --- --- 15 --- --- 10 | 42 --- --- 36 --- --- 42
R08 | 3175 11 12 12 10 16 17 6 | 46 54 59 53 58 52 53
R09E | 1474 12 9 17 21 13 9 6 | 46 50 51 46 52 47 48
R11E | 1338 11 10 23 15 14 10 6 | 40 46 48 47 45 44 43
R12E | 1025 15 13 18 23 16 16 7 | 95 100 95 120 106 97 101
XR13E | 1108 24 28 27 33 27 --- 13 | 113 122 122 118 119 --- 116
R14E | 1150 10 18 21 25 10 12 7 | 139 144 138 143 138 143 140
R15E | 935 11 13 16 28 17 11 7 | 70 71 72 84 79 73 73
R16E | 820 10 18 14 20 13 17 6 | 96 95 99 108 100 99 98
XR17 | 1509 7 18 15 17 19 --- 7 | 34 29 41 36 47 --- 37
R18 | 811 12 18 19 15 8 21 7 | 26 37 37 35 35 27 30
R19 | 844 41 29 39 72 23 49 19 | 53 53 71 59 54 53 51
R20 | 2374 45 122 40 86 37 53 29 | 86 64 96 110 73 46 70
R21 | 1217 11 28 22 21 14 22 8 | 51 30 52 57 49 32 43
R22 | 2798 12 11 18 21 19 14 7 | 22 26 27 36 30 30 25
R24 | 596 13 14 17 11 33 27 9 | 40 33 40 42 53 25 35
XR25 |11609 15 11 --- --- 17 --- 10 | 36 35 --- --- 36 --- 34
XR26 |10983 40 --- --- 47 59 --- 35 | 122 --- --- 116 136 --- 123
------+-----------------------------------------+-------------------------------------
RMS | 1470 19 34 22 32 19 23 |T 63 60 67 70 68 59 63
WRMS | 1470 16 20 19 24 15 20 |NE 54 45 55 58 58 47 52
MEDI | 1108 12 14 18 20 16 16 |MD 55 53 58 57 54 53 53
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