[IGSREPORT-30122] Wk 2333 IGLOS Final Orbits
acc
acc at igs.org
Sun Oct 13 22:50:01 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2333 (Sep 22, 2024 - Sep 28, 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 2.2333.
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:
igl2333[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2333 in the SP3 format.
igl23337.sum Combination Report for GPS Week 2333.
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 | 8.3 ns
1 | 6.7 ns
2 | 4.8 ns
3 | 7.6 ns
4 | 7.7 ns
5 | 7.3 ns
6 | 7.7 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 1.2333, 1a.2333).
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 2.2333.0-6)
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 3.2333.0-6).
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 2333 summary. (Sep 22, 2024 - Sep 28, 2024)
Table 1.2333.a GPS week : 2333 MJD: 60575.0-60581.0
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 4 3 2 59 .17 21 17 | -2044 -1086 3928 17171
| 0 1 1 12 16 25 .03 | 1461 2275
esa n/a| 0 0 0 -23 -7 17 -.08 20 17 | 10687 -965 3267 7341
| 1 0 1 11 15 16 .04 | 4922 2429
gfz n/a| 0 0 3 45 6 -20 -.04 21 14 | 0 -702 3319 8095
| 1 0 1 10 8 16 .05 | 0 2252
grg n/a| 0 0 2 -17 -4 -45 .31 22 19 | 4270 -1085 4055 17433
| 1 1 1 16 13 35 .03 | 1101 2322
iac n/a| 0 0 -4 17 9 -7 -.16 18 17 | 6955 -953 3898 16306
| 0 0 1 13 18 36 .05 | 988 1290
jgx n/a| 0 0 -6 -52 -10 12 -.16 24 23 | 2924 -655 3317 8185
| 1 0 2 6 22 30 .06 | 1305 2214
Table 1.2333.b GPS week : 2333 MJD: 60575.0-60581.0
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 13 12 14 13 12 13 |
R02 | 8 5 5 7 6 5 6 |
R03 | 6 5 5 7 5 8 6 |
R04 | 6 6 7 6 5 6 6 |
R05 | 5 6 7 5 6 6 5 |
R07 | 8 6 6 7 6 6 7 |
R08 | 7 7 7 7 8 7 7 |
R09 | 7 7 6 6 9 6 7 |
R11 | 7 6 8 8 8 7 7 |
R12 | 6 7 8 8 5 6 7 |
R14 | 6 7 7 8 6 5 6 |
R15 | 7 8 7 8 6 7 7 |
R16 | 6 10 7 8 8 8 7 |
R17 | 7 7 7 7 9 6 8 |
R18 | 7 8 8 8 7 7 7 |
R19 | 24 21 20 19 20 23 22 |
R20 | 20 18 16 19 18 18 22 |
R21 | 7 8 9 7 8 8 10 |
R22 | 7 7 6 7 6 6 6 |
R24 | 8 7 6 7 7 8 7 |
R25 | 9 8 15 12 12 9 12 |
R26 | 35 35 29 30 29 30 23 |
Table 1.2333.c GPS week : 2333 MJD: 60575.0-60581.0
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 2333 0 | -98 -49 185 -747 -1020 -6519 80.8 1747 1747 | 8255 0
brd 2333 1 | -81 18 91 -3606 -569 -5728 79.3 1842 1842 | 6722 0
brd 2333 2 | 70 18 178 -1484 1124 -9307 79.6 1947 1947 | 4785 0
brd 2333 3 | -35 104 171 58 1615 -5891 78.9 1779 1779 | 7631 0
brd 2333 4 | 78 136 146 533 747 1243 81.4 1591 1591 | 7685 0
brd 2333 5 | -10 119 238 1611 1719 -1600 82.2 1428 1428 | 7307 0
brd 2333 6 | -34 60 147 -903 518 -883 81.7 1356 1356 | 7713 0
-------------+------------------------------------------------------------+----------------
brd 2333 mean| -16 58 165 -648 590 -4097 80.6 1670 1670 | 7156 0
brd 2333 sdev| 68 66 45 1659 1047 3740 1.3 218 218 | 1144 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 2.2333.0 GPS week: 2333 Day: 0 MJD: 60575
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 5 6 44 .14 21 16 | -1844 -917 4138 19595
esa n/a| -1 0 1 -20 2 0 -.03 19 15 | 18197 -1717 3159 8698
gfz n/a| -1 0 6 51 16 -33 .02 22 16 | 0 -795 3233 8863
grg n/a| 3 1 -1 -31 0 9 .30 24 19 | 4894 -1125 4276 19685
iac n/a| 0 -1 -4 -3 21 -6 -.22 21 19 | 7559 -226 4093 18753
jgx n/a| -1 0 -2 -49 -50 16 -.21 23 23 | 4307 -644 3228 8981
Table 2.2333.1 GPS week: 2333 Day: 1 MJD: 60576
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 7 -11 55 .20 19 17 | -3665 996 4075 16389
esa n/a| -1 0 0 -8 3 31 -.12 21 17 | 8798 1093 3561 7987
gfz n/a| 0 2 3 38 6 -43 .01 21 15 | 0 1026 3631 8112
grg n/a| 1 -1 2 -8 -14 -20 .31 22 18 | 2874 1274 4173 16279
iac n/a| 0 0 -4 7 21 -45 -.09 18 16 | 6312 135 4052 15469
jgx n/a| 0 0 -7 -58 -6 64 -.20 24 24 | 1414 1165 3618 8078
Table 2.2333.2 GPS week: 2333 Day: 2 MJD: 60577
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 7 26 89 .20 20 16 | -3236 -3484 4304 16233
esa n/a| 1 1 0 -7 -5 35 -.13 20 18 | 2417 -2876 3623 7891
gfz n/a| 1 0 1 32 9 -23 .01 23 18 | 0 -2723 3705 7081
grg n/a| 0 0 2 -11 -24 -86 .26 19 15 | 3287 -3073 4418 16287
iac n/a| 0 0 -4 13 2 -12 -.17 16 16 | 5441 -2632 4276 15234
jgx n/a| -2 0 -7 -58 -4 13 -.18 22 22 | 1666 -2772 3691 7072
Table 2.2333.3 GPS week: 2333 Day: 3 MJD: 60578
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 6 -11 16 60 .18 22 17 | -3320 -2321 3889 20473
esa n/a| 1 -1 0 -28 0 8 -.08 19 16 | 8547 -2559 2972 7018
gfz n/a| 0 0 2 53 -6 3 -.08 22 14 | 0 -1932 2998 7633
grg n/a| 0 0 2 0 19 -63 .32 21 19 | 4239 -2512 4251 22729
iac n/a| 0 0 -3 27 -20 -13 -.12 17 17 | 6117 -1977 3842 19756
jgx n/a| -1 0 -5 -40 2 27 -.14 23 21 | 2760 -1893 3013 7801
Table 2.2333.4 GPS week: 2333 Day: 4 MJD: 60579
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 -13 2 98 .15 21 16 | -1776 2829 3458 15079
esa n/a| 1 0 -1 -23 -39 13 -.06 19 15 | 11085 3630 3094 6134
gfz n/a| 1 1 1 46 -1 -18 -.10 20 15 | 0 3504 3147 8357
grg n/a| 0 0 4 -15 -9 -56 .37 22 19 | 3473 2924 3520 14780
iac n/a| -1 0 -1 18 30 -5 -.24 18 18 | 7426 941 3432 14289
jgx n/a| 0 1 -10 -55 -13 -36 -.15 23 24 | 2096 3380 3144 8481
Table 2.2333.5 GPS week: 2333 Day: 5 MJD: 60580
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -2 7 16 -2 25 .14 21 19 | 254 -3023 3782 16335
esa n/a| 0 0 -1 -32 -14 -4 -.09 22 19 | 11726 -2626 3376 6943
gfz n/a| 0 0 1 34 3 -23 -.09 19 12 | 0 -2627 3428 8399
grg n/a| 0 -1 1 -8 -3 -78 .32 21 17 | 5547 -3032 3848 16210
iac n/a| 0 0 -3 39 -9 66 -.14 16 15 | 8006 -1851 3765 15440
jgx n/a| 1 0 -7 -55 22 3 -.04 25 25 | 4787 -2481 3419 8627
Table 2.2333.6 GPS week: 2333 Day: 6 MJD: 60581
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 5 15 -22 45 .17 22 16 | -723 -1685 3856 16096
esa n/a| 0 -1 -1 -40 -1 35 -.05 22 20 | 14039 -1702 3085 6716
gfz n/a| 1 0 5 61 15 -2 -.07 20 11 | 0 -1372 3093 8223
grg n/a| 0 1 2 -47 0 -21 .32 24 26 | 5577 -2056 3899 16061
iac n/a| 0 0 -5 18 19 -35 -.14 18 16 | 7829 -1062 3829 15207
jgx n/a| 0 0 -7 -50 -21 0 -.16 25 25 | 3444 -1343 3109 8258
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 3.2333.0 GPS week: 2333 Day: 0 MJD: 60575
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1736 26 10 20 34 19 45 12 | 67 60 62 55 65 56 59
R02 | 2499 7 10 15 14 29 21 7 | 39 46 40 37 50 39 40
R03 | 921 11 9 12 8 20 16 6 | 51 49 50 56 58 47 51
R04 | 1327 19 11 13 14 14 8 6 | 53 50 53 45 53 49 50
R05 | 1926 9 8 8 10 14 12 4 | 52 53 48 48 51 44 49
R07 | 1593 10 21 11 27 11 15 7 | 46 47 50 53 47 40 45
R08 | 2140 15 13 22 17 8 12 7 | 42 43 50 50 49 45 45
R09 | 1515 17 10 14 13 21 14 6 | 63 64 68 60 65 62 63
R11 | 1310 13 14 16 19 16 14 7 | 35 41 40 43 41 39 38
R12 | 1617 8 12 17 13 13 20 6 | 70 68 70 74 68 50 66
R14 | 2734 11 13 15 18 12 10 6 | 80 78 69 83 77 64 74
R15 | 2027 10 18 12 16 18 18 7 | 70 56 69 70 66 57 63
R16 | 1184 15 14 9 17 8 11 5 | 77 72 71 71 78 71 72
R17 | 901 13 15 9 17 17 18 6 | 80 64 71 75 75 54 69
R18 | 965 19 14 9 12 11 18 6 | 61 76 75 68 75 63 69
R19 | 1673 31 49 60 71 54 54 24 | 85 58 118 60 97 61 75
R20 | 1838 65 39 49 23 40 35 20 | 80 53 79 56 53 44 53
R21 | 709 7 12 13 18 15 28 7 | 86 76 87 93 92 65 83
R22 | 3056 16 12 8 14 17 18 6 | 53 56 57 60 54 57 54
R24 | 985 11 20 18 26 13 17 8 | 71 78 77 76 75 63 72
XR25 |14571 15 11 --- --- 11 --- 9 | 30 40 --- --- 39 --- 35
XR26 | 9354 35 --- --- 36 70 --- 35 | 31 --- --- 29 61 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1747 21 19 22 24 21 23 |T 60 58 65 60 63 53 57
WRMS | 1747 16 15 16 19 19 23 |NE 60 58 65 60 63 53 57
MEDI | 1617 13 13 13 17 15 17 |MD 61 56 68 60 61 54 54
Table 3.2333.1 GPS week: 2333 Day: 1 MJD: 60576
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 3209 30 21 19 36 23 38 12 | 34 44 32 35 42 33 34
R02 | 2188 8 8 10 13 17 10 5 | 18 22 20 19 26 20 19
R03 | 1149 8 8 9 15 11 14 5 | 24 22 23 23 27 18 21
R04 | 1035 12 11 15 17 10 16 6 | 29 29 39 23 29 19 26
R05 | 1020 9 11 10 18 13 13 5 | 26 27 23 22 27 20 22
R07 | 1525 17 12 11 14 14 12 6 | 27 27 31 28 24 28 25
R08 | 1799 13 15 20 23 11 15 7 | 22 20 33 38 22 21 23
R09 | 1595 14 11 19 14 11 18 6 | 43 47 48 43 48 41 43
R11 | 2042 16 12 13 16 9 14 6 | 29 33 29 28 28 26 27
R12 | 902 12 10 18 15 12 18 6 | 42 43 44 53 40 35 41
R14 | 2380 11 11 12 16 23 20 7 | 72 73 73 75 87 61 73
R15 | 1722 13 22 13 24 13 21 8 | 58 45 63 74 64 42 57
R16 | 1339 11 21 19 20 26 31 10 | 77 91 94 70 85 80 81
R17 | 1329 16 16 11 15 11 21 6 | 51 39 36 43 42 36 39
R18 | 773 20 15 13 21 22 18 8 | 39 48 42 40 53 42 42
R19 | 2519 33 49 42 55 44 59 21 | 62 47 52 34 58 36 41
R20 | 1612 44 49 50 21 24 35 17 | 49 41 73 51 33 37 40
R21 | 1005 10 23 21 12 11 23 7 | 47 44 59 52 45 36 46
R22 | 3414 19 11 17 16 15 18 7 | 33 36 40 42 40 39 35
R24 | 1347 13 15 19 17 10 20 7 | 46 48 57 53 47 40 47
XR25 |10538 12 12 --- --- 10 --- 8 | 17 23 --- --- 22 --- 18
XR26 |10514 31 --- --- 44 64 --- 34 | 25 --- --- 33 38 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1841 19 21 21 22 18 24 |T 39 40 45 41 42 35 37
WRMS | 1841 17 17 15 18 16 24 |NE 39 40 45 41 42 35 37
MEDI | 1595 13 12 15 17 13 18 |MD 34 41 40 40 40 36 35
Table 3.2333.2 GPS week: 2333 Day: 2 MJD: 60577
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2739 28 27 20 31 19 34 12 | 41 51 40 39 48 47 40
R02 | 850 6 14 16 7 10 14 5 | 31 37 40 30 28 30 30
R03 | 875 9 14 10 7 11 11 4 | 36 35 38 37 39 32 34
R04 | 1496 7 16 13 12 21 15 6 | 38 33 40 36 48 34 37
R05 | 644 5 18 15 14 16 20 7 | 32 38 35 34 40 34 33
R07 | 1704 7 8 20 14 10 12 5 | 35 34 39 30 36 35 33
R08 | 943 21 17 20 10 14 9 7 | 34 37 46 42 42 40 39
R09 | 954 12 14 12 11 14 16 6 | 80 82 84 79 77 84 80
R11 | 3565 16 13 23 18 18 16 8 | 62 63 72 71 66 67 65
R12 | 995 12 12 24 20 13 20 7 | 68 66 85 77 65 55 68
R14 | 1592 13 10 22 12 18 14 6 | 83 84 81 84 87 70 81
R15 | 920 15 21 14 15 15 18 7 | 63 45 54 69 62 53 57
R16 | 2042 13 23 12 14 15 15 7 | 111 110 110 114 110 102 109
R17 | 1292 10 22 22 16 8 17 7 | 64 48 73 71 55 50 59
R18 | 759 21 20 13 20 15 19 8 | 51 57 59 55 57 53 54
R19 | 2481 49 42 49 51 27 43 19 | 75 52 85 47 59 48 55
R20 | 1427 42 35 50 20 15 42 15 | 62 36 67 45 50 35 44
R21 | 715 8 17 21 15 19 30 8 | 64 58 76 67 71 43 63
R22 | 4969 17 10 10 15 9 16 6 | 47 47 53 58 52 45 49
R24 | 1608 11 12 15 15 15 17 6 | 54 59 50 61 64 50 56
XR25 |12077 27 15 --- --- 17 --- 14 | 27 41 --- --- 40 --- 31
XR26 |14589 23 --- --- 39 52 --- 28 | 32 --- --- 39 41 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1947 20 20 23 19 16 22 |T 54 53 61 56 56 50 52
WRMS | 1947 16 18 18 15 16 22 |NE 54 53 61 56 56 50 52
MEDI | 1427 13 16 16 15 15 16 |MD 51 48 54 55 52 47 49
Table 3.2333.3 GPS week: 2333 Day: 3 MJD: 60578
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 793 39 20 16 34 19 48 13 | 46 46 43 34 43 35 38
R02 | 1086 10 17 20 14 16 12 7 | 31 38 28 33 35 28 29
R03 | 1124 10 18 8 16 18 15 6 | 38 44 40 44 38 40 38
R04 | 1413 11 13 13 17 6 14 5 | 37 43 44 35 40 48 39
R05 | 816 6 12 10 8 13 15 5 | 36 39 38 33 40 31 35
R07 | 2057 11 10 9 15 21 21 7 | 43 41 40 34 49 32 39
R08 | 872 18 9 10 11 20 12 6 | 34 38 41 39 45 32 37
R09 | 1130 13 9 17 10 14 10 5 | 50 59 62 55 56 55 55
R11 | 3906 21 10 17 27 10 12 7 | 38 41 51 41 42 44 40
R12 | 680 10 20 16 11 17 27 8 | 53 55 61 58 56 37 52
R14 | 1973 17 13 19 15 22 8 7 | 92 105 111 100 91 100 99
R15 | 483 20 13 16 20 11 17 7 | 69 54 51 68 50 48 55
R16 | 1930 16 22 17 13 21 19 8 | 81 60 64 73 85 60 69
R17 | 1096 11 22 12 10 15 21 7 | 65 57 65 66 63 47 59
R18 | 927 15 16 18 21 15 20 8 | 58 63 51 78 61 50 59
R19 | 1302 35 46 60 44 14 37 18 | 75 50 99 59 68 56 64
R20 | 1618 55 25 47 46 24 44 18 | 64 28 52 45 37 37 30
R21 | 651 7 20 12 13 21 18 7 | 71 62 73 75 81 60 69
R22 | 4266 17 15 9 15 17 9 6 | 30 40 38 44 29 39 34
R24 | 1636 19 19 13 14 11 19 7 | 55 64 53 53 54 52 53
XR25 |14329 20 8 --- --- 20 --- 12 | 30 31 --- --- 47 --- 34
XR26 |11605 39 --- --- 31 52 --- 30 | 27 --- --- 39 42 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1778 22 19 22 21 17 23 |T 51 50 55 52 52 46 48
WRMS | 1778 17 16 14 19 17 21 |NE 51 50 55 52 52 46 48
MEDI | 1130 16 16 16 15 17 17 |MD 46 46 51 45 47 44 39
Table 3.2333.4 GPS week: 2333 Day: 4 MJD: 60579
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 649 35 17 16 30 14 46 12 | 44 37 40 35 36 28 34
R02 | 1033 7 10 18 14 16 14 6 | 35 39 37 37 34 40 34
R03 | 2177 13 10 12 17 7 11 5 | 38 37 31 37 35 37 34
R04 | 735 11 11 12 10 10 14 5 | 38 39 39 33 32 32 34
R05 | 881 9 18 18 11 9 14 6 | 38 44 43 37 35 41 37
R07 | 1212 8 15 14 10 12 17 5 | 40 42 40 31 35 35 36
R08 | 878 16 16 18 24 12 19 8 | 34 35 40 34 40 42 35
R09 | 1935 12 15 28 14 30 10 9 | 87 88 87 87 90 84 85
R11 | 2879 19 17 8 25 16 12 7 | 64 68 67 74 76 69 69
R12 | 1024 9 12 12 12 7 16 5 | 56 53 46 53 47 48 49
R14 | 1064 10 13 14 16 15 15 6 | 63 72 75 75 66 61 68
R15 | 723 14 11 12 20 7 12 6 | 59 50 57 65 53 45 54
R16 | 1494 14 20 14 12 20 21 7 | 128 115 116 125 128 129 122
R17 | 639 8 21 15 18 21 29 8 | 56 51 57 72 62 45 56
R18 | 967 21 11 12 16 12 19 7 | 52 61 65 72 60 44 59
R19 | 1640 42 43 45 57 24 52 19 | 75 68 96 77 80 48 70
R20 | 1699 54 32 38 31 41 37 18 | 54 41 65 42 44 35 37
R21 | 875 10 16 17 12 25 15 7 | 60 53 39 53 69 50 53
R22 | 3887 11 14 16 16 13 11 6 | 40 45 40 54 43 48 43
R24 | 1036 14 16 13 12 13 16 6 | 54 47 50 56 43 35 47
XR25 | 6911 22 12 --- --- 14 --- 11 | 27 38 --- --- 39 --- 33
XR26 | 8930 38 --- --- 26 49 --- 28 | 50 --- --- 70 64 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 1591 21 19 20 22 18 23 |T 54 53 56 58 55 49 52
WRMS | 1591 16 15 15 19 18 24 |NE 54 53 56 58 55 49 52
MEDI | 1036 13 15 14 16 14 15 |MD 52 47 46 54 44 44 47
Table 3.2333.5 GPS week: 2333 Day: 5 MJD: 60580
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1239 30 28 12 30 14 39 11 | 30 25 35 23 31 36 28
R02 | 1347 11 12 9 11 13 13 5 | 32 33 33 31 28 28 29
R03 | 1663 10 20 14 20 17 19 7 | 31 25 26 40 37 20 28
R04 | 1354 15 13 12 6 12 23 6 | 33 29 35 33 29 22 28
R05 | 785 16 19 6 6 18 13 6 | 25 34 27 28 28 27 25
R07 | 1124 13 12 15 5 13 20 6 | 23 36 30 29 25 32 27
R08 | 1381 13 12 13 19 9 18 6 | 25 33 24 30 23 26 24
R09 | 1990 15 8 14 11 12 9 5 | 79 79 78 73 84 79 78
R11 | 1890 14 17 12 19 12 16 6 | 53 55 56 51 48 49 51
R12 | 1567 9 15 10 15 12 20 6 | 45 48 37 49 45 29 41
R14 | 1658 7 10 9 14 11 14 5 | 93 94 94 89 82 90 89
R15 | 825 13 26 13 13 13 19 7 | 63 47 53 62 58 47 54
R16 | 1623 15 24 14 18 17 16 7 | 92 100 101 93 90 87 93
R17 | 636 8 18 10 8 15 22 6 | 52 41 52 56 56 43 50
R18 | 681 10 27 13 11 11 15 6 | 51 57 46 50 45 41 46
R19 | 1299 54 49 56 59 22 66 23 | 64 57 82 64 53 51 58
R20 | 1540 47 30 42 40 36 39 18 | 49 48 49 53 37 57 42
R21 | 1237 9 26 16 15 14 24 7 | 61 57 69 70 65 55 63
R22 | 2452 13 19 13 13 11 10 6 | 49 51 54 61 45 51 50
R24 | 726 13 19 13 14 22 21 7 | 53 49 44 56 64 41 50
XR25 | 8607 14 15 --- --- 10 --- 9 | 41 36 --- --- 37 --- 36
XR26 |11077 33 --- --- 39 49 --- 29 | 51 --- --- 33 31 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1428 21 22 19 21 16 25 |T 49 49 51 51 47 45 46
WRMS | 1428 19 19 12 17 15 25 |NE 49 49 51 51 47 45 46
MEDI | 1354 13 19 13 14 13 19 |MD 49 48 46 51 45 41 42
Table 3.2333.6 GPS week: 2333 Day: 6 MJD: 60581
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 580 34 18 18 31 21 46 12 | 59 51 57 47 49 55 50
R02 | 1298 10 18 13 20 6 7 5 | 41 46 38 37 37 38 38
R03 | 720 10 12 10 17 6 25 6 | 48 58 53 56 53 43 51
R04 | 1879 12 13 10 10 12 18 5 | 49 45 44 44 47 40 44
R05 | 709 10 12 6 9 9 12 4 | 43 41 39 41 37 38 38
R07 | 1355 8 16 14 9 14 24 6 | 45 49 49 42 44 39 43
R08 | 816 12 13 13 13 20 16 6 | 43 46 51 50 57 40 47
R09 | 2842 18 10 14 20 19 9 7 | 97 101 102 90 104 99 98
R11 | 1452 13 16 10 25 13 11 6 | 67 69 68 62 64 62 65
R12 | 2005 10 13 12 17 16 19 6 | 52 42 52 46 55 32 46
R14 | 990 12 10 13 16 10 11 5 | 85 82 78 86 75 76 79
R15 | 457 18 17 15 12 13 18 7 | 80 55 69 75 61 55 65
R16 | 1454 15 21 9 15 13 19 7 | 100 95 97 102 99 94 97
R17 | 704 9 23 10 18 19 29 8 | 80 65 73 83 85 68 75
R18 | 778 11 18 14 15 10 22 6 | 69 79 79 74 73 66 73
R19 | 1660 49 60 48 58 24 52 22 | 95 63 108 77 84 68 79
R20 | 672 58 36 58 48 43 44 22 | 93 66 71 61 49 54 57
R21 | 1296 8 27 11 28 16 33 9 | 90 78 93 106 98 69 89
R22 | 1628 13 15 9 13 15 7 5 | 53 56 58 61 51 55 54
R24 | 1248 7 21 18 13 16 13 7 | 79 78 74 81 87 74 78
XR25 |12367 21 17 --- --- 12 --- 12 | 49 44 --- --- 42 --- 42
XR26 |11455 27 --- --- 28 37 --- 22 | 34 --- --- 46 59 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1356 22 22 20 24 18 25 |T 65 62 67 65 64 58 61
WRMS | 1356 16 20 11 26 16 25 |NE 65 62 67 65 64 58 61
MEDI | 1296 12 17 13 17 14 18 |MD 59 58 68 61 57 55 54
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