[IGSREPORT-29500] Wk 2277 IGLOS Final Orbits
acc
acc at igs.org
Mon Sep 18 11:17:04 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2277 (Aug 27, 2023 - Sep 02, 2023)
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 2.2277.
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:
igl2277[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2277 in the SP3 format.
igl22777.sum Combination Report for GPS Week 2277.
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).
The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | 0.2 ns
1 | 0.4 ns
2 | -0.1 ns
3 | 1.3 ns
4 | 0.2 ns
5 | -10.4 ns
6 | 0.7 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 1.2277, 1a.2277).
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 2.2277.0-6)
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 3.2277.0-6).
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 2277 summary. (Aug 27, 2023 - Sep 02, 2023)
Table 1.2277.a GPS week : 2277 MJD: 60183.0-60189.0
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 0 -30 34 -.02 16 12 | 28043 235 3426 9754
| 0 0 1 13 14 6 .05 | 4336 1289
esa n/a| 0 0 1 -15 27 0 -.20 31 22 | -3050 1449 3418 7303
| 1 1 1 13 14 22 .02 | 8308 1548
gfz n/a| -1 0 -3 25 10 3 -.11 24 14 | 0 522 3489 8729
| 1 1 2 12 14 38 .06 | 0 1052
grg n/a| 3 0 -4 -7 22 -64 .37 25 20 | -1741 524 3497 8255
| 2 1 2 20 18 31 .03 | 4019 1131
iac n/a| 1 1 -16 -16 -22 -27 -3.11 49 46 | 1327 -393 3410 9211
| 1 2 3 32 24 102 .12 | 4324 1511
jgx n/a| 1 1 2 2 -6 44 -.27 31 31 | 27893 143 3503 8838
| 2 1 1 13 32 77 .05 | 4276 1492
Table 1.2277.b GPS week : 2277 MJD: 60183.0-60189.0
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 | 27 25 22 22 21 24 24 |
R02 | 6 9 7 7 8 6 10 |
R03 | 8 7 8 12 6 6 8 |
R04 | 7 9 7 7 10 7 8 |
R05 | 9 7 8 9 7 7 7 |
R07 | 10 9 9 11 10 7 10 |
R08 | 9 8 7 12 11 10 7 |
R09 | 7 6 11 8 10 8 10 |
R11 | 6 8 7 10 8 8 6 |
R12 | 6 9 8 9 8 8 6 |
R13 | 16 14 19 20 18 17 19 |
R14 | 8 7 6 10 7 6 7 |
R15 | 8 8 7 8 9 11 7 |
R16 | 10 9 12 15 9 8 10 |
R17 | 9 9 10 10 10 9 10 |
R18 | 8 7 7 9 8 9 10 |
R19 | 21 25 24 26 22 21 24 |
R20 | 36 34 38 33 32 34 31 |
R21 | 9 8 8 10 10 10 11 |
R22 | 6 6 8 7 7 9 11 |
R24 | 12 12 11 10 11 11 13 |
R25 | 21 11 14 14 16 18 13 |
Table 1.2277.c GPS week : 2277 MJD: 60183.0-60189.0
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 2277 0 | 1 8 148 -1160 -2862 4616 78.6 1539 1539 | 170 0
brd 2277 1 | 40 26 139 -1012 -1894 7220 79.0 1648 1648 | 441 0
brd 2277 2 | 95 13 81 -1464 1933 8327 78.9 1615 1615 | -65 0
brd 2277 3 | 41 -24 94 -2077 945 5258 77.5 8574 8574 | 1298 0
brd 2277 4 | -21 -60 118 -1048 1256 2957 79.1 1239 1239 | 197 0
brd 2277 5 | -11 -28 117 854 2087 780 77.9 1213 1213 | -10352 0
brd 2277 6 | 68 -40 102 689 3406 1657 79.5 1214 1214 | 670 0
-------------+------------------------------------------------------------+----------------
brd 2277 mean| 30 -15 114 -745 695 4402 78.6 2434 2434 | -1091 0
brd 2277 sdev| 43 32 23 1098 2256 2794 .7 2714 2714 | 4107 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 2.2277.0 GPS week: 2277 Day: 0 MJD: 60183
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 16 -41 32 -.03 14 11 | 30216 -1196 3010 9525
esa n/a| 0 -1 2 -26 16 4 -.18 34 21 | -146 27 3000 7220
gfz n/a| 0 1 -2 41 24 -15 -.05 23 12 | 0 -480 3003 8271
grg n/a| 0 -3 -4 -34 57 -77 .36 26 19 | 98 -137 3024 7574
iac n/a| -1 1 -22 21 0 45 -2.93 53 49 | 3995 -1296 2992 8831
jgx n/a| -1 2 2 -5 34 28 -.29 27 27 | 30149 -944 3028 8349
Table 2.2277.1 GPS week: 2277 Day: 1 MJD: 60184
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 1 2 5 -16 33 -.09 16 13 | 28467 692 3155 9202
esa n/a| 0 0 2 -23 6 16 -.18 33 21 | 4611 1250 3142 6588
gfz n/a| 0 1 -5 38 20 -7 -.07 21 14 | 0 475 3205 8019
grg n/a| 6 -2 -3 -10 3 -56 .35 22 16 | -12 474 3230 7569
iac n/a| 2 2 -20 34 -25 -44 -3.05 51 45 | 2918 -247 3121 8600
jgx n/a| 0 2 1 24 -16 100 -.22 38 38 | 28881 805 3150 7988
Table 2.2277.2 GPS week: 2277 Day: 2 MJD: 60185
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 2 -4 -30 24 -.05 14 11 | 30204 -1651 3515 10458
esa n/a| -1 2 1 -13 25 -3 -.21 33 22 | -733 -898 3507 6905
gfz n/a| -2 -1 -3 20 28 -65 -.09 26 14 | 0 -1078 3589 9468
grg n/a| 5 2 -5 18 23 -31 .36 25 19 | 200 -1415 3560 9000
iac n/a| 3 3 -16 -33 5 -125 -3.30 50 46 | 3346 -2344 3512 10016
jgx n/a| 3 0 1 0 -34 80 -.18 35 35 | 29874 -2354 3647 9715
Table 2.2277.3 GPS week: 2277 Day: 3 MJD: 60186
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 2 12 -18 33 -.02 17 13 | 29393 1909 4122 12656
esa n/a| -2 -1 4 -26 21 -29 -.23 31 25 | 5584 3670 4119 9290
gfz n/a| -1 0 -1 9 -3 11 -.11 26 14 | 0 1913 4369 12180
grg n/a| 7 0 -8 -16 11 -35 .37 25 20 | -808 1982 4366 11884
iac n/a| 0 3 -12 -31 -69 158 -3.17 50 50 | 1840 1737 4125 12157
jgx n/a| 3 1 2 11 -7 156 -.26 30 30 | 28484 1880 4355 12376
Table 2.2277.4 GPS week: 2277 Day: 4 MJD: 60187
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 6 -23 -33 44 .03 17 13 | 28913 762 3580 8901
esa n/a| 0 -1 0 11 31 -27 -.19 27 21 | -4376 1796 3575 6276
gfz n/a| -2 1 -5 30 13 13 -.06 20 13 | 0 559 3578 7893
grg n/a| 3 0 -4 19 12 -47 .39 29 27 | -610 688 3631 7503
iac n/a| 3 -3 -15 -52 -28 -107 -3.03 50 49 | 1406 1205 3557 8429
jgx n/a| 3 0 3 10 -51 30 -.28 29 29 | 28181 -45 3627 8128
Table 2.2277.5 GPS week: 2277 Day: 5 MJD: 60188
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 3 1 -15 39 .02 14 11 | 18376 -89 3082 8427
esa n/a| -1 0 0 -21 51 28 -.18 28 24 | -18689 1528 3081 7170
gfz n/a| -2 -1 -6 26 -4 41 -.18 24 14 | 0 693 3110 7301
grg n/a| 1 -1 0 -25 15 -121 .42 27 21 | -10818 407 3076 6776
iac n/a| 0 5 -12 -13 -20 -10 -3.09 48 45 | -8215 -54 3065 7908
jgx n/a| 1 2 0 -11 -6 -1 -.27 27 27 | 18490 -35 3130 7190
Table 2.2277.6 GPS week: 2277 Day: 6 MJD: 60189
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 -8 -53 32 .03 17 13 | 30732 1224 3523 9114
esa n/a| 0 0 2 -11 37 16 -.20 28 23 | -7607 2772 3506 7676
gfz n/a| 1 1 0 11 -3 47 -.19 28 18 | 0 1577 3571 7977
grg n/a| 1 0 -4 -2 32 -81 .32 21 17 | -240 1674 3594 7480
iac n/a| 2 1 -14 -37 -19 -106 -3.19 43 42 | 4004 -1756 3501 8538
jgx n/a| 1 0 2 -11 36 -83 -.35 33 32 | 31197 1699 3587 8124
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 3.2277.0 GPS week: 2277 Day: 0 MJD: 60183
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 720 23 97 24 33 84 36 27 | 137 58 139 132 172 105 120
R02 | 688 7 15 10 10 65 22 6 | 75 68 87 83 128 62 78
R03 | 1250 6 21 10 19 56 13 8 | 95 79 95 103 132 80 93
R04 | 984 9 15 12 15 58 21 7 | 91 84 89 95 128 79 89
R05 | 1001 11 21 12 20 49 22 9 | 95 83 98 94 119 79 92
R07 | 1420 9 15 16 29 79 21 10 | 90 75 95 82 144 68 86
R08 | 1775 7 14 21 20 62 22 9 | 82 76 98 82 133 68 84
R09 | 815 10 9 15 11 46 18 6 | 47 48 48 48 49 47 47
R11 | 702 8 8 10 15 49 19 6 | 58 64 62 59 58 60 60
R12 | 1513 8 9 10 14 35 16 6 | 50 52 54 56 74 49 52
R13 | 1044 11 32 23 48 48 56 16 | 69 65 75 60 93 65 66
R14 | 798 9 9 12 19 48 9 7 | 49 52 54 45 83 49 49
R15 | 906 12 15 10 19 56 18 8 | 61 62 62 74 107 73 63
R16 | 769 19 20 12 16 40 10 10 | 66 54 54 45 93 57 54
R17E | 1106 11 14 15 23 30 --- 9 | 78 78 81 89 78 --- 80
R18E | 1034 9 15 11 21 32 18 8 | 52 51 51 68 62 54 53
R19E | 2403 31 41 43 30 55 34 21 | 79 114 108 77 81 86 86
R20E | 1811 22 93 71 67 70 63 35 | 101 135 139 105 113 120 106
R21E | 1541 14 19 12 16 32 14 8 | 99 95 100 105 96 99 99
R22E | 2944 10 9 10 13 46 14 6 | 45 45 49 51 45 42 46
R24E | 3321 14 21 22 24 35 11 11 | 132 123 128 134 128 124 129
XR25E |16273 13 32 --- --- 53 --- 21 | 21 32 --- --- 23 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 1538 14 34 23 26 53 27 |T 76 72 84 80 97 73 75
WRMS | 1538 11 21 12 19 49 27 |NE 76 65 79 75 108 67 73
MEDI | 1044 10 15 12 19 49 18 |MD 75 65 87 82 93 68 78
Table 3.2277.1 GPS week: 2277 Day: 1 MJD: 60184
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 633 21 88 26 22 64 26 24 | 93 45 105 95 123 82 86
R02 | 570 11 14 18 14 81 21 8 | 51 50 68 60 119 44 56
R03 | 956 11 15 9 10 57 19 6 | 62 52 54 55 92 47 56
R04 | 1009 11 12 19 18 61 21 9 | 60 52 55 66 87 51 57
R05 | 1024 6 22 7 12 51 28 7 | 63 51 65 72 93 49 62
R07 | 1238 13 17 14 18 56 38 9 | 64 54 68 59 104 39 61
R08 | 989 12 8 16 15 61 23 7 | 58 57 58 53 100 45 55
R09 | 851 7 12 9 10 55 22 5 | 36 37 36 35 47 37 35
R11 | 678 17 12 15 8 44 19 8 | 42 45 41 37 42 45 40
R12 | 1124 5 13 17 23 36 19 9 | 35 38 29 43 69 39 34
R13 | 676 25 33 18 20 47 53 14 | 59 43 35 53 81 69 45
R14 | 625 11 8 13 10 37 16 6 | 36 46 51 42 67 44 43
R15 | 1166 9 10 13 17 43 17 7 | 42 49 43 51 81 39 45
R16 | 552 18 17 9 14 36 17 8 | 50 46 44 38 83 52 42
R17E | 993 12 16 10 21 31 --- 8 | 47 49 48 51 42 --- 46
R18E | 1283 7 14 8 15 30 21 6 | 37 42 42 36 34 38 38
R19E | 2356 29 49 53 41 29 68 25 | 64 63 69 79 66 83 61
R20E | 3361 39 91 54 54 79 114 33 | 75 100 84 72 89 80 68
R21E | 959 9 21 8 16 28 23 8 | 62 60 61 68 55 67 61
R22E | 3522 10 11 9 11 51 13 6 | 21 21 28 29 27 19 23
R24E | 3605 16 19 16 26 40 18 11 | 92 92 86 92 91 82 88
XR25E |18779 7 15 --- --- 49 --- 11 | 24 24 --- --- 26 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1647 16 33 21 22 51 38 |T 53 50 55 56 73 52 51
WRMS | 1647 13 21 14 16 45 38 |NE 53 47 53 54 84 48 51
MEDI | 993 11 15 14 16 47 21 |MD 51 49 54 53 81 45 46
Table 3.2277.2 GPS week: 2277 Day: 2 MJD: 60185
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 565 20 75 25 26 52 47 21 | 104 48 101 103 121 69 92
R02 | 693 7 12 11 18 66 18 6 | 64 58 66 53 111 55 61
R03 | 983 6 20 12 21 66 30 8 | 75 64 82 68 123 56 73
R04 | 1131 8 12 14 15 57 35 7 | 75 74 68 68 105 61 71
R05 | 1097 7 14 10 22 38 36 7 | 71 67 75 89 91 56 74
R07 | 959 10 25 10 18 46 33 9 | 77 59 71 70 101 53 70
R08 | 1096 4 19 13 14 57 35 7 | 67 51 67 67 108 55 63
R09 | 1015 18 20 19 13 63 18 10 | 28 45 50 42 30 38 37
R11 | 749 10 15 12 9 57 19 6 | 51 53 57 52 51 56 52
R12 | 789 7 19 13 18 36 19 8 | 36 34 43 45 78 34 38
R13 | 1357 22 46 29 40 40 36 19 | 68 45 35 61 81 55 53
R14 | 711 6 9 10 18 43 14 6 | 34 40 32 47 74 37 36
R15 | 1750 7 9 11 17 40 22 6 | 46 51 51 52 84 41 48
R16 | 622 21 13 16 25 33 23 11 | 53 46 44 37 84 34 44
R17E | 2176 7 18 10 30 33 --- 9 | 36 36 33 58 27 --- 37
R18E | 1224 9 14 11 18 37 22 7 | 22 26 27 27 20 26 22
R19E | 1664 22 50 59 31 56 53 23 | 64 71 107 93 64 74 76
R20E | 2719 29 95 81 62 72 93 37 | 96 138 141 101 116 121 107
R21E | 1059 10 13 13 18 31 22 7 | 78 74 77 84 61 71 78
R22E | 3263 12 10 16 13 47 19 7 | 25 29 30 31 20 30 26
R24E | 3490 12 22 17 29 40 23 11 | 53 58 53 49 46 54 51
XR25E |16830 8 21 --- --- 57 --- 13 | 25 34 --- --- 31 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1614 14 33 26 25 50 35 |T 56 54 62 61 73 53 56
WRMS | 1614 11 22 14 19 46 35 |NE 60 52 60 61 88 50 58
MEDI | 1096 9 18 13 18 46 23 |MD 53 51 57 58 78 55 52
Table 3.2277.3 GPS week: 2277 Day: 3 MJD: 60186
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 628 27 70 19 17 56 36 21 | 108 46 99 101 134 72 90
R02 | 715 8 9 14 12 66 25 6 | 67 67 73 66 121 56 68
R03 | 616 11 19 29 18 57 20 11 | 76 71 103 80 122 70 81
R04 | 1480 9 9 12 17 46 25 7 | 73 67 75 63 99 63 69
R05 | 1004 12 12 18 16 41 20 8 | 78 77 69 89 105 76 77
R07 | 925 10 32 11 21 49 31 11 | 82 64 89 100 119 66 83
R08 | 1128 13 27 28 15 57 25 12 | 78 64 106 96 133 70 85
R09 | 611 10 16 13 17 56 25 8 | 25 23 29 24 36 29 22
R11 | 737 11 21 18 17 54 17 9 | 25 23 39 27 33 36 24
R12 | 579 12 12 18 21 38 28 9 | 34 39 39 38 79 30 35
R13 | 1597 23 42 28 43 42 37 19 | 57 35 41 40 79 40 43
R14 | 637 9 14 22 20 36 17 9 | 36 35 27 42 72 33 32
R15 | 2021 12 14 11 16 35 18 7 | 50 65 54 61 83 61 55
R16 | 491 18 24 23 35 40 18 14 | 55 74 74 38 98 57 56
R17E | 1920 11 21 11 25 29 --- 9 | 47 46 44 49 45 --- 44
R18E | 1645 10 17 13 19 37 18 8 | 27 34 31 30 26 28 26
R19E | 2322 29 45 69 20 87 66 25 | 83 88 85 84 100 86 76
R20E |38858 39 75 60 56 66 55 32 | 65 69 83 49 50 52 57
R21E | 1015 9 19 12 28 42 21 10 | 73 78 80 72 80 75 73
R22E | 1386 11 9 11 15 52 16 6 | 19 26 23 33 23 27 22
R24E | 1994 16 20 14 20 34 20 10 | 48 59 44 49 42 52 47
XR25E |16108 9 19 --- --- 59 --- 13 | 20 31 --- --- 32 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 8574 17 31 26 25 50 30 |T 55 53 62 58 77 53 54
WRMS | 8574 13 25 14 20 50 30 |NE 60 53 65 61 93 54 58
MEDI | 1015 11 19 18 19 46 21 |MD 55 59 69 49 79 56 55
Table 3.2277.4 GPS week: 2277 Day: 4 MJD: 60187
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 827 34 62 11 25 53 31 21 | 113 67 93 102 129 75 93
R02 | 973 12 12 14 16 59 32 7 | 75 70 75 79 120 57 74
R03 | 538 6 8 9 17 60 30 5 | 77 74 79 71 118 57 75
R04 | 1103 11 8 14 32 47 20 9 | 80 81 88 64 106 74 79
R05 | 1119 11 15 13 11 62 17 7 | 80 77 90 93 129 76 84
R07 | 1089 9 25 8 29 40 23 10 | 79 70 85 107 107 76 83
R08 | 1089 15 18 11 34 69 15 11 | 72 80 83 109 132 79 82
R09 | 801 12 9 15 28 48 20 9 | 36 39 45 38 42 31 37
R11 | 643 16 13 12 8 53 21 7 | 57 58 59 62 57 61 57
R12 | 1192 8 13 10 24 36 24 7 | 43 51 45 50 84 53 45
R13 | 1606 27 29 16 53 34 52 17 | 46 46 36 39 77 37 36
R14 | 774 11 11 11 15 33 13 6 | 42 39 35 43 76 37 38
R15 | 2016 7 11 12 28 42 12 8 | 58 56 53 75 94 62 58
R16 | 587 15 20 11 15 43 14 9 | 56 73 64 53 86 65 60
R17E | 1827 9 20 14 28 34 --- 10 | 51 64 58 47 53 --- 54
R18E | 1487 12 14 15 17 40 15 8 | 59 62 66 56 63 63 60
R19E | 2059 31 43 43 35 83 59 22 | 52 66 52 43 52 64 46
R20E | 1169 35 66 59 65 56 53 32 | 87 109 105 87 118 98 90
R21E | 731 13 18 19 17 34 20 9 | 84 85 89 81 79 87 84
R22E | 1223 12 10 11 15 50 19 7 | 40 41 46 46 44 37 42
R24E | 1476 9 25 14 30 35 34 11 | 78 73 80 75 78 67 75
XR25 |16858 11 20 --- --- 55 --- 15 | 14 33 --- --- 18 --- 20
------+-----------------------------------------+-------------------------------------
RMS | 1238 17 27 20 29 50 29 |T 62 64 67 67 84 62 62
WRMS | 1238 13 21 13 27 49 29 |NE 65 62 66 70 96 60 64
MEDI | 1103 12 15 13 25 47 20 |MD 58 66 66 64 79 63 60
Table 3.2277.5 GPS week: 2277 Day: 5 MJD: 60188
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 581 17 80 20 36 60 23 23 | 87 46 98 102 115 78 82
R02 | 795 5 16 11 12 54 20 6 | 69 54 73 62 99 54 65
R03 | 641 7 15 8 11 50 24 5 | 68 59 65 65 96 50 64
R04 | 527 8 18 10 11 51 20 6 | 68 69 65 69 97 62 67
R05 | 847 6 15 13 19 47 13 7 | 69 72 68 82 100 73 71
R07 | 1045 10 19 8 12 37 26 7 | 69 58 68 65 88 56 65
R08 | 1946 15 21 16 18 64 11 10 | 54 62 71 73 107 62 61
R09 | 694 9 10 19 14 54 9 7 | 35 44 41 39 41 42 37
R11 | 874 12 16 13 12 48 17 7 | 44 46 37 45 43 41 42
R12 | 826 9 16 11 21 40 10 8 | 29 31 37 41 73 31 31
R13 | 2183 10 33 30 43 33 83 16 | 30 26 47 31 67 38 30
R14 | 744 9 11 8 14 48 13 6 | 30 29 27 31 77 25 27
R15 | 1713 11 20 18 27 51 12 10 | 43 31 34 54 90 42 38
R16 | 485 13 15 15 15 43 10 8 | 51 55 54 55 86 47 51
R17E | 961 8 17 15 23 29 --- 8 | 56 49 54 64 47 --- 54
R18E | 1354 9 18 16 17 36 18 8 | 53 53 58 51 54 54 53
R19E | 887 24 39 43 41 67 22 20 | 59 89 89 73 73 80 68
R20E | 1814 38 59 75 66 60 49 33 | 58 81 118 68 67 62 66
R21E | 875 11 14 18 24 31 20 9 | 76 76 79 95 84 81 79
R22E | 1428 15 10 21 12 46 11 9 | 22 25 45 28 22 26 26
R24E | 1888 8 21 17 32 37 13 11 | 47 43 44 56 44 41 44
XR25 |23274 11 26 --- --- 54 --- 17 | 37 41 --- --- 32 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1212 14 28 24 27 48 27 |T 52 51 60 59 72 52 52
WRMS | 1212 11 24 14 21 45 27 |NE 53 48 56 58 84 50 52
MEDI | 875 10 17 16 18 48 17 |MD 53 49 58 62 73 50 53
Table 3.2277.6 GPS week: 2277 Day: 6 MJD: 60189
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1181 27 70 24 36 50 31 23 | 124 55 114 135 155 97 109
R02 | 742 11 23 22 15 48 18 10 | 89 79 109 101 140 84 94
R03 | 602 10 17 13 12 43 17 7 | 91 75 90 92 123 77 88
R04 | 519 13 18 13 12 41 31 8 | 91 81 82 82 112 75 84
R05 | 863 7 10 15 14 41 21 6 | 93 88 92 94 115 79 91
R07 | 755 7 23 24 14 57 23 10 | 107 90 122 109 147 92 107
R08 | 2431 8 12 9 17 39 22 7 | 86 85 95 105 131 86 92
R09 | 901 11 14 23 17 55 19 9 | 44 44 48 48 49 52 44
R11 | 748 8 14 9 11 52 12 6 | 59 67 62 59 58 63 60
R12 | 937 7 13 10 13 33 16 6 | 47 46 47 47 73 44 45
R13 | 686 28 37 32 33 43 52 18 | 64 40 50 51 91 48 50
R14 | 662 9 8 9 16 32 13 6 | 50 47 49 48 80 43 48
R15 | 749 8 18 7 10 35 16 6 | 65 57 58 69 86 58 62
R16 | 523 11 24 19 16 40 17 10 | 70 60 68 70 100 74 66
R17E | 1511 9 20 15 20 29 --- 9 | 92 87 99 104 93 --- 95
R18E | 1597 6 24 22 18 34 12 10 | 37 42 42 36 43 39 36
R19E | 966 36 40 59 32 52 56 24 | 73 104 106 101 81 112 87
R20E | 1587 38 59 76 35 45 95 30 | 107 99 128 100 104 118 102
R21E | 1056 12 18 23 20 34 12 10 | 119 117 129 135 122 128 124
R22E | 1567 17 9 27 18 48 12 11 | 38 40 49 43 42 41 40
R24E | 2296 18 27 17 29 35 25 13 | 88 88 82 91 89 90 85
XR25E |11597 9 17 --- --- 58 --- 13 | 21 28 --- --- 25 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 1213 17 28 28 21 43 33 |T 75 69 81 81 93 75 74
WRMS | 1213 13 23 18 17 42 32 |NE 77 65 77 79 104 69 74
MEDI | 901 10 18 19 17 41 18 |MD 73 67 82 91 91 75 84
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