[IGSREPORT-29816] Wk 2306 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 8 02:15:53 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2306 (Mar 17, 2024 - Mar 23, 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 2.2306.
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:
igl2306[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2306 in the SP3 format.
igl23067.sum Combination Report for GPS Week 2306.
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 | 6.5 ns
1 | 3.9 ns
2 | 2.5 ns
3 | 5.2 ns
4 | 3.0 ns
5 | 6.0 ns
6 | -13.7 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 | R26
1 | ALL | R26
2 | ALL | R26
3 | ALL | R26
4 | ALL | R26
5 | ALL | R26
6 | ALL | R26
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 1.2306, 1a.2306).
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 2.2306.0-6)
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 3.2306.0-6).
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 2306 summary. (Mar 17, 2024 - Mar 23, 2024)
Table 1.2306.a GPS week : 2306 MJD: 60386.0-60392.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -10 -30 29 .17 22 16 | -1262 182 3484 8290
| 0 0 1 13 23 24 .03 | 6296 1679
esa n/a| 0 -1 2 -32 -3 -22 -.05 24 18 | -2890 -90 3480 7727
| 1 1 1 18 15 29 .05 | 11053 1719
gfz n/a| 2 1 -2 30 1 -39 .01 27 17 | 0 70 3474 7679
| 1 1 2 14 14 25 .07 | 0 1438
grg n/a| 0 -1 5 -25 -10 31 .26 25 19 | 1776 61 3521 7297
| 1 1 2 37 17 41 .06 | 6302 1576
iac n/a| 0 0 -2 11 11 -12 -.19 18 16 | 3586 32 3484 8344
| 1 1 2 12 17 29 .06 | 6456 1127
jgx n/a| -1 0 0 29 35 27 -.08 27 26 | 1244 451 3275 7671
| 1 1 2 16 25 41 .02 | 7056 1117
Table 1.2306.b GPS week : 2306 MJD: 60386.0-60392.0
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 | 10 14 13 15 13 11 10 |
R02 | 6 6 7 7 6 6 7 |
R03 | 7 7 5 6 7 7 7 |
R04 | 6 5 6 5 6 7 8 |
R05 | 6 6 6 8 5 8 10 |
R07 | 9 8 7 6 7 6 6 |
R08 | 7 7 7 7 9 7 7 |
R09 | 8 9 7 8 9 10 10 |
R11 | 6 8 7 7 7 8 6 |
R12 | 7 8 8 9 7 7 8 |
R13 | 18 15 13 13 14 15 14 |
R14 | 8 6 7 9 8 7 8 |
R15 | 7 8 7 8 9 7 7 |
R16 | 8 9 11 8 9 11 8 |
R17 | 10 8 7 10 7 8 8 |
R18 | 10 7 8 8 10 9 7 |
R19 | 18 18 22 19 18 18 20 |
R20 | 27 23 25 25 22 28 29 |
R21 | 11 9 8 8 11 9 8 |
R22 | 8 11 9 8 10 10 12 |
R24 | 10 7 9 10 8 9 7 |
R25 | 10 11 16 12 14 12 12 |
Table 1.2306.c GPS week : 2306 MJD: 60386.0-60392.0
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 2306 0 | -25 25 111 -1569 1447 3261 78.7 2442 2442 | 6543 0
brd 2306 1 | 28 -6 135 -625 1512 9094 79.8 2334 2334 | 3874 0
brd 2306 2 | 119 57 102 1843 964 8353 81.6 2685 2685 | 2500 0
brd 2306 3 | -8 23 124 2226 -1675 6648 82.0 2351 2351 | 5163 0
brd 2306 4 | -73 -48 56 1306 -1791 4099 80.7 2508 2508 | 2982 0
brd 2306 5 | 52 49 59 442 -2531 5250 80.7 2158 2158 | 6046 0
brd 2306 6 | 65 80 -21 -1044 -1228 9012 80.0 1988 1988 | -13667 0
-------------+------------------------------------------------------------+----------------
brd 2306 mean| 22 25 81 368 -471 6531 80.5 2352 2352 | 1920 0
brd 2306 sdev| 64 43 54 1485 1716 2391 1.1 228 228 | 7037 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 2.2306.0 GPS week: 2306 Day: 0 MJD: 60386
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 -3 -6 -59 24 .12 20 16 | 1421 -209 3341 8138
esa n/a| 0 -1 0 -20 -5 -16 -.08 23 15 | 1574 183 3356 7594
gfz n/a| 1 0 0 27 7 4 .10 22 14 | 0 506 3360 7628
grg n/a| 0 -1 0 -24 -7 -34 .16 23 17 | 6134 561 3348 7182
iac n/a| 0 0 2 6 43 22 -.21 21 18 | 7577 172 3333 8154
jgx n/a| -1 1 1 11 3 -47 -.10 31 31 | 3299 662 3405 7890
Table 2.2306.1 GPS week: 2306 Day: 1 MJD: 60387
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 -36 -45 34 .14 20 15 | -1613 2658 3162 7737
esa n/a| 1 1 1 -17 -2 -5 -.10 22 16 | 2782 2435 3155 6862
gfz n/a| 4 3 0 47 3 -40 .02 24 13 | 0 1331 2941 6881
grg n/a| 2 0 5 6 14 39 .27 25 19 | 2583 2176 3221 6521
iac n/a| -1 -2 -3 0 -4 -19 -.19 20 16 | 4965 728 3167 7753
jgx n/a| -3 0 2 23 86 33 -.12 27 27 | 1295 2683 3166 7068
Table 2.2306.2 GPS week: 2306 Day: 2 MJD: 60388
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 4 -34 10 .17 20 14 | -290 -616 3049 7228
esa n/a| 1 1 2 -5 -2 4 -.08 23 15 | 7674 -1128 3061 6665
gfz n/a| 3 3 0 36 -6 -19 -.07 30 17 | 0 -638 3089 6410
grg n/a| 0 1 4 -5 -15 42 .23 32 20 | 2640 -820 3098 5838
iac n/a| 0 -3 -4 3 23 -39 -.09 19 15 | 4509 -1090 3059 7332
jgx n/a| 0 -1 -1 19 29 43 -.08 22 21 | 3113 -734 3197 6542
Table 2.2306.3 GPS week: 2306 Day: 3 MJD: 60389
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -8 -43 44 .18 22 17 | 2783 -392 3297 7636
esa n/a| -1 -2 3 -49 -2 -27 -.00 29 21 | -17047 -772 3281 7929
gfz n/a| 2 0 -1 31 0 -60 .01 27 19 | 0 -95 3312 7063
grg n/a| 0 0 4 -53 -12 -9 .24 23 18 | 5330 -678 3297 6562
iac n/a| 1 0 -4 19 16 -6 -.16 18 15 | 6989 36 3274 7775
jgx n/a| 0 0 -1 31 45 68 -.09 25 21 | 5582 -301 3331 7224
Table 2.2306.4 GPS week: 2306 Day: 4 MJD: 60390
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -20 -32 45 .20 25 18 | -320 -813 3233 9123
esa n/a| 1 -1 1 -42 3 9 -.03 21 17 | 360 -1195 3212 7618
gfz n/a| 0 1 -3 25 27 -64 -.03 27 20 | 0 -787 3235 8685
grg n/a| 0 -2 6 13 -7 31 .36 23 17 | 3053 -826 3243 8398
iac n/a| -1 0 -2 6 3 -38 -.19 15 13 | 4376 -1182 3240 9223
jgx n/a| 0 0 -3 16 26 68 -.08 28 26 | 2776 404 2990 8721
Table 2.2306.5 GPS week: 2306 Day: 5 MJD: 60391
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 -2 7 58 .19 21 16 | 4023 2402 3600 8315
esa n/a| 1 -2 0 -52 19 -55 .03 28 19 | 4670 1984 3585 7590
gfz n/a| 2 0 -5 1 0 -61 .09 31 21 | 0 2253 3638 7500
grg n/a| -1 0 8 -95 -43 67 .28 25 20 | 4856 2019 3636 7099
iac n/a| 0 0 -1 36 -5 -36 -.30 17 16 | 7410 2059 3601 8245
jgx n/a| -3 -1 -2 48 22 29 -.08 26 26 | 6844 668 3373 7953
Table 2.2306.6 GPS week: 2306 Day: 6 MJD: 60392
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -4 -7 -13 .18 23 17 | -14843 -1755 4712 9858
esa n/a| 1 -1 4 -42 -32 -66 -.07 25 20 | -20246 -2143 4713 9833
gfz n/a| 1 1 -6 38 -20 -32 -.05 29 17 | 0 -2077 4749 9589
grg n/a| 0 -3 6 -20 -3 83 .29 25 20 | -12158 -1999 4810 9482
iac n/a| 0 0 -1 9 6 30 -.20 18 16 | -10719 -499 4715 9928
jgx n/a| -2 -1 0 54 32 -4 -.04 30 32 | -14199 -219 3466 8302
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 3.2306.0 GPS week: 2306 Day: 0 MJD: 60386
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1235 30 21 19 20 22 18 10 | 78 49 68 70 58 63 63
R02 | 692 10 10 12 9 13 20 5 | 44 45 43 39 42 35 40
R03 | 3157 12 16 12 7 19 16 6 | 62 62 51 60 66 55 59
R04 | 721 14 10 13 15 8 11 5 | 60 56 55 59 57 51 56
R05 | 1682 11 10 11 9 13 20 5 | 54 67 62 56 59 52 58
R07 | 1167 22 24 13 17 13 28 8 | 59 64 58 70 56 48 58
R08 | 2532 19 9 11 15 13 26 7 | 43 38 42 46 43 37 40
R09 | 1510 15 20 13 26 14 11 7 | 64 69 65 72 61 65 64
R11 | 1659 12 15 7 20 13 15 6 | 37 35 38 48 42 29 37
R12 | 1784 15 20 9 24 10 8 7 | 71 85 68 61 69 68 70
XR13 | 1386 20 44 49 27 22 --- 17 | 120 87 142 122 108 --- 114
R14 | 571 8 19 15 16 15 28 7 | 91 104 98 86 93 79 92
R15 | 1448 13 17 14 14 11 16 6 | 99 102 87 100 89 88 94
R16 | 1553 18 21 12 12 13 21 7 | 97 99 99 89 85 82 91
XR17 | 1043 14 22 12 33 15 --- 10 | 67 54 61 68 61 --- 59
R18 | 676 15 11 16 29 34 15 9 | 50 61 54 67 67 47 55
R19E | 3216 37 31 52 31 31 54 17 | 221 231 219 242 236 236 227
R20E | 7352 44 72 56 49 49 94 27 | 73 113 95 85 73 102 78
R21 | 1030 14 17 28 29 22 34 11 | 68 65 72 63 69 58 63
R22E | 2786 13 8 15 27 15 17 7 | 151 157 159 145 155 50 153
R24 | 1864 24 12 19 28 19 19 9 | 59 45 53 52 49 45 47
XR25E |11759 15 12 --- --- 12 --- 9 | 78 74 --- --- 81 --- 77
------+-----------------------------------------+-------------------------------------
RMS | 2442 20 23 22 23 21 31 |T 79 80 80 80 78 67 77
WRMS | 2442 15 15 14 17 18 31 |NE 67 65 67 68 65 56 64
MEDI | 1510 15 17 13 20 14 19 |MD 67 65 65 68 66 55 63
Table 3.2306.1 GPS week: 2306 Day: 1 MJD: 60387
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1330 40 25 23 22 32 31 13 | 47 44 44 36 30 51 36
R02 | 832 9 11 9 17 17 12 5 | 36 38 38 38 29 37 34
XR03 | 3086 11 18 --- 16 10 11 6 | 45 54 --- 39 50 45 46
R04 | 579 12 10 11 9 13 12 5 | 47 60 52 54 52 53 52
R05 | 1005 14 8 20 8 12 12 6 | 50 54 45 47 51 47 48
R07 | 1230 13 14 10 26 16 19 7 | 46 54 53 56 42 44 48
R08 | 2717 14 12 13 21 17 20 7 | 35 39 35 41 41 36 36
R09 | 2231 16 22 16 18 20 20 8 | 54 58 56 54 51 62 53
R11 | 1350 12 10 24 20 13 22 7 | 38 37 57 53 39 33 41
R12 | 1371 16 27 10 13 13 21 7 | 67 74 57 56 59 49 60
XR13 | 767 35 32 34 23 20 --- 15 | 104 86 105 108 94 --- 97
R14 | 993 8 16 9 12 9 15 5 | 80 80 73 74 81 69 76
R15 | 1260 13 18 19 18 11 26 8 | 77 87 87 79 84 74 81
R16 | 738 17 25 22 20 13 21 9 | 78 87 91 88 81 77 82
XR17 | 1059 14 14 13 18 16 --- 7 | 52 45 48 53 47 --- 47
R18 | 983 8 15 14 21 15 14 6 | 41 42 40 53 54 39 43
R19E | 2025 31 26 57 53 36 36 18 | 195 203 199 221 213 204 203
R20E | 7586 42 62 55 27 39 72 23 | 97 111 119 81 86 88 90
R21 | 733 24 15 14 21 20 28 9 | 52 45 56 55 58 48 50
R22E | 3029 15 13 21 49 11 16 10 | 137 139 151 130 137 76 138
R24 | 1108 19 10 13 20 11 18 7 | 56 52 49 54 51 51 51
XR25E |10964 14 13 --- --- 18 --- 11 | 80 70 --- --- 88 --- 79
------+-----------------------------------------+-------------------------------------
RMS | 2334 20 22 24 25 20 27 |T 68 70 72 70 69 62 67
WRMS | 2334 15 16 13 19 16 27 |NE 55 57 58 57 55 50 54
MEDI | 1230 14 15 14 20 15 20 |MD 52 54 56 54 52 51 51
Table 3.2306.2 GPS week: 2306 Day: 2 MJD: 60388
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1626 29 30 18 34 24 31 12 | 53 62 50 45 38 50 45
R02 | 723 13 23 12 21 10 16 7 | 30 43 28 30 29 27 28
R03 | 2047 9 8 16 12 9 11 5 | 44 39 48 46 45 35 41
R04 | 835 14 12 19 10 7 11 5 | 44 41 52 42 41 41 41
R05 | 2178 9 12 20 7 10 12 5 | 39 45 55 41 39 40 41
R07 | 1236 16 15 16 19 12 13 6 | 49 44 42 53 41 42 43
R08 | 1350 13 11 16 12 17 15 6 | 38 36 38 39 35 31 34
R09 | 2594 14 15 14 21 17 15 7 | 59 56 62 49 56 66 57
R11 | 2982 14 16 15 25 12 14 7 | 25 38 34 35 30 29 29
R12 | 1653 15 28 9 22 13 19 8 | 59 69 53 47 42 40 51
XR13 | 1429 20 34 37 16 17 --- 13 | 96 72 104 95 79 --- 85
R14 | 839 14 16 13 17 14 22 7 | 76 90 83 74 82 79 80
R15 | 787 9 18 17 16 7 24 7 | 77 80 85 80 80 65 77
R16 | 764 19 26 40 15 20 25 11 | 77 64 97 77 64 63 70
XR17 | 1139 13 11 15 21 11 --- 7 | 53 47 58 50 50 --- 50
R18 | 687 12 20 18 28 10 14 7 | 45 59 53 52 52 41 48
R19E | 2393 43 30 69 82 35 39 22 | 148 148 157 182 136 153 146
R20E | 9046 38 58 79 76 44 42 24 | 69 104 100 131 70 77 76
R21 | 767 15 17 13 18 14 29 8 | 41 39 36 39 41 23 34
R22E | 3360 13 9 25 31 25 16 9 | 137 140 138 141 147 115 139
R24 | 813 21 9 21 25 12 25 8 | 46 31 38 37 31 30 31
XR25E | 8022 22 19 --- --- 23 --- 15 | 58 71 --- --- 66 --- 62
------+-----------------------------------------+-------------------------------------
RMS | 2685 20 23 30 32 19 22 |T 61 64 67 65 58 55 59
WRMS | 2685 14 15 17 20 15 21 |NE 52 53 56 51 48 43 49
MEDI | 1350 14 16 17 21 13 16 |MD 53 56 53 49 45 41 48
Table 3.2306.3 GPS week: 2306 Day: 3 MJD: 60389
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1311 40 47 26 44 15 23 15 | 61 46 45 70 38 44 46
R02 | 769 16 27 16 6 11 17 7 | 30 39 26 23 21 25 23
R03 | 1228 8 15 7 14 17 14 6 | 44 46 40 45 40 39 40
R04 | 553 11 13 11 9 9 9 4 | 40 33 35 39 39 35 36
R05 | 2022 21 18 12 17 13 21 7 | 34 40 43 53 45 35 39
R07 | 1338 13 10 22 15 11 11 6 | 44 38 29 44 43 39 39
R08 | 1413 12 10 19 16 18 13 7 | 35 43 34 44 51 43 41
R09 | 1861 13 15 18 25 17 11 7 | 45 53 48 36 61 44 46
R11 | 3714 13 19 13 12 19 12 6 | 20 33 28 25 28 27 22
R12 | 1564 17 40 18 16 12 14 9 | 52 70 35 38 35 34 41
R13 | 1284 25 38 37 26 14 33 13 | 87 46 102 69 76 38 72
R14 | 1611 11 28 14 11 23 20 8 | 68 80 70 66 50 60 63
R15 | 839 20 27 16 20 11 17 8 | 80 80 59 54 64 58 64
R16 | 782 11 21 29 12 8 23 8 | 85 68 92 84 84 67 80
XR17 | 1352 16 16 20 30 13 --- 9 | 44 34 48 36 39 --- 36
R18 | 663 11 21 14 21 10 21 7 | 32 43 38 37 41 30 33
R19E | 1607 50 44 47 47 27 34 18 | 92 82 101 82 87 90 84
R20E | 7402 43 68 68 33 49 67 24 | 70 86 99 59 55 91 65
R21 | 778 18 17 13 15 12 26 7 | 40 23 29 40 41 28 31
R22E | 3722 15 13 16 30 14 18 8 | 82 86 91 111 79 64 86
R24 | 974 16 14 35 26 13 27 10 | 39 28 51 31 36 27 31
XR25E | 8361 16 18 --- --- 17 --- 12 | 47 54 --- --- 65 --- 55
------+-----------------------------------------+-------------------------------------
RMS | 2350 22 29 27 23 18 25 |T 53 52 54 51 50 45 48
WRMS | 2350 17 21 19 18 15 21 |NE 48 46 47 46 46 39 43
MEDI | 1338 16 18 18 17 13 18 |MD 44 46 45 44 43 39 41
Table 3.2306.4 GPS week: 2306 Day: 4 MJD: 60390
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 778 34 24 33 39 21 20 12 | 51 40 40 55 26 50 38
R02 | 699 13 13 19 11 10 17 6 | 35 35 30 28 23 29 27
R03 | 829 13 18 17 15 11 13 6 | 38 35 30 36 32 35 32
R04 | 517 13 13 17 14 7 12 5 | 42 36 39 38 40 39 37
R05 | 1308 7 12 15 14 9 14 5 | 36 43 35 38 38 41 36
R07 | 751 7 8 17 12 10 30 6 | 45 50 54 48 51 41 46
R08 | 1124 10 9 32 19 11 32 8 | 36 38 61 35 45 29 38
R09 | 1277 17 20 23 29 18 13 9 | 59 67 69 60 69 68 63
R11 | 2887 14 9 17 20 11 18 6 | 31 43 52 49 38 35 39
R12 | 1563 8 26 12 10 14 12 7 | 59 75 52 61 51 57 57
XR13 | 802 25 32 29 40 18 --- 14 | 93 81 102 100 92 --- 91
R14 | 2710 11 20 19 11 16 20 7 | 76 91 89 81 71 76 79
R15 | 626 23 25 21 13 12 21 8 | 94 95 78 78 74 71 80
R16 | 1078 22 19 21 24 12 20 8 | 96 92 88 69 88 77 84
XR17 | 764 15 12 15 16 11 --- 7 | 46 45 45 50 44 --- 44
R18 | 562 9 21 26 37 11 21 9 | 39 44 51 51 44 35 39
R19E | 2315 48 28 53 43 24 48 17 | 130 135 128 135 127 124 125
R20E | 8858 68 47 52 25 26 68 21 | 66 66 65 61 49 65 51
R21 | 831 16 24 35 13 16 40 10 | 50 45 67 50 55 35 47
XR22E | 3440 18 15 26 22 17 --- 9 | 98 95 112 107 102 --- 101
R24 | 1195 16 13 20 21 10 28 8 | 43 39 36 45 33 40 35
XR25E |11996 17 24 --- --- 17 --- 13 | 55 44 --- --- 63 --- 54
------+-----------------------------------------+-------------------------------------
RMS | 2507 25 21 27 23 15 28 |T 59 60 63 60 57 52 56
WRMS | 2507 18 17 20 17 13 26 |NE 53 55 56 54 50 47 50
MEDI | 1078 15 19 21 19 12 20 |MD 50 45 54 51 49 41 46
Table 3.2306.5 GPS week: 2306 Day: 5 MJD: 60391
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 723 27 31 29 30 11 14 10 | 44 30 28 40 38 33 32
R02 | 1021 13 14 20 10 11 13 6 | 33 29 30 32 26 33 28
R03 | 550 9 17 22 16 16 12 7 | 39 40 35 38 39 34 36
R04 | 708 20 20 11 12 13 12 7 | 42 49 38 37 30 37 36
R05 | 949 16 18 11 27 9 14 7 | 31 35 33 27 21 32 26
R07 | 1336 9 15 13 17 10 14 5 | 47 41 38 45 43 40 41
R08 | 1678 9 11 15 15 11 22 6 | 34 31 39 42 38 27 34
R09 | 961 18 29 16 43 14 10 10 | 54 63 56 43 60 54 52
R11 | 1792 16 17 22 17 16 10 7 | 39 28 42 33 37 40 34
R12 | 1024 7 21 12 16 14 14 6 | 56 65 57 49 53 52 54
XR13 | 913 25 33 26 43 24 --- 15 | 91 70 73 83 83 --- 79
R14 | 3190 12 21 16 21 11 13 7 | 72 90 74 78 73 72 75
R15 | 1270 15 13 15 11 12 26 7 | 82 77 79 78 72 74 76
R16 | 1225 18 28 29 14 29 23 11 | 77 76 84 69 54 63 67
XR17 | 500 15 12 17 17 16 --- 8 | 50 44 45 51 45 --- 45
R18 | 870 11 21 21 24 11 26 8 | 41 49 44 46 44 43 41
R19E | 3698 24 32 39 45 34 56 17 | 104 128 126 135 126 110 119
R20E | 6404 59 79 98 47 30 59 28 | 66 104 111 61 61 55 61
R21 | 797 18 18 16 22 13 25 8 | 47 44 45 51 46 37 43
XR22E | 2081 21 14 15 25 19 --- 10 | 97 100 91 103 100 --- 98
R24 | 1185 11 20 29 22 15 25 9 | 51 48 50 50 43 47 45
XR25E |10727 18 19 --- --- 13 --- 11 | 41 57 --- --- 50 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 2158 21 28 31 25 17 26 |T 56 59 58 56 53 49 53
WRMS | 2158 16 19 21 20 16 26 |NE 51 50 49 49 46 44 46
MEDI | 1024 16 19 17 21 13 14 |MD 47 49 45 49 45 40 45
Table 3.2306.6 GPS week: 2306 Day: 6 MJD: 60392
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 758 17 26 27 30 18 13 9 | 60 48 54 59 49 62 53
R02 | 648 15 9 27 7 9 15 6 | 40 34 27 35 34 35 32
R03 | 775 9 13 24 13 13 15 6 | 47 49 42 52 58 46 49
R04 | 1716 21 16 10 11 18 17 7 | 54 44 45 48 41 45 44
R05 | 1131 25 25 22 24 15 19 9 | 46 55 49 48 40 40 43
R07 | 1837 11 14 12 20 10 14 6 | 57 54 50 58 52 53 53
R08 | 1338 6 17 16 22 12 23 7 | 44 43 38 54 45 39 42
R09 | 990 20 25 16 36 15 15 10 | 72 80 73 52 73 74 69
R11 | 1208 12 9 17 12 14 14 6 | 51 49 54 56 60 54 53
R12 | 875 10 24 18 16 16 12 7 | 86 99 84 72 74 76 80
R13 | 1262 28 32 41 24 18 38 13 | 131 101 135 123 117 46 116
R14 | 2593 8 26 17 17 14 20 7 | 101 121 106 104 96 90 102
R15 | 2506 10 12 18 19 10 18 6 | 114 119 110 110 102 98 108
R16 | 1248 23 14 11 14 14 18 7 | 114 106 114 101 98 94 103
XR17 | 633 14 16 21 17 13 --- 8 | 44 34 44 47 41 --- 39
R18 | 877 8 22 11 14 15 17 6 | 33 39 30 43 44 29 35
R19E | 3692 26 37 46 48 36 72 19 | 136 150 151 151 142 144 142
R20E | 5122 70 61 85 54 38 79 28 | 70 114 92 64 72 75 66
R21 | 862 16 12 17 24 11 22 7 | 37 30 37 36 35 28 31
XR22E | 953 17 16 21 39 18 --- 11 | 91 95 86 94 98 --- 92
R24 | 1836 9 14 20 15 10 19 6 | 27 27 21 40 26 36 26
XR25E | 6519 19 18 --- --- 14 --- 12 | 42 56 --- --- 53 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 1988 23 25 29 25 18 30 |T 68 70 68 68 65 61 64
WRMS | 1988 17 20 17 20 16 32 |NE 64 62 61 63 60 55 59
MEDI | 1208 15 16 18 19 14 18 |MD 54 54 54 56 53 53 53
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