[IGSREPORT-29351] Wk 2263 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 9 07:05:00 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2263 (May 21, 2023 - May 27, 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 2.2263.
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:
igl2263[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2263 in the SP3 format.
igl22637.sum Combination Report for GPS Week 2263.
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. 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.
3. 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).
4. 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
5. 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 | -0.9 ns
1 | -0.8 ns
2 | -11.4 ns
3 | -0.0 ns
4 | -0.2 ns
5 | -14.3 ns
6 | -15.6 ns
6. 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
----+--------+---------------
1 | ESA | R20
2 | 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 1.2263, 1a.2263).
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 2.2263.0-6)
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 3.2263.0-6).
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 2263 summary. (May 21, 2023 - May 27, 2023)
Table 1.2263.a GPS week : 2263 MJD: 60085.0-60091.0
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 0 7 -18 29 .07 20 16 | 29746 -768 3827 13272
| 0 0 1 11 15 10 .02 | 10409 1058
esa n/a| 0 0 0 -11 1 -13 -.15 44 25 | -5020 -345 3744 13002
| 1 0 2 16 16 22 .03 | 11807 1372
gfz n/a| 0 0 1 16 -2 -15 -.17 24 15 | 0 -1156 3016 8587
| 1 1 2 13 19 29 .08 | 0 1093
grg n/a| 2 0 -2 -22 27 -19 .24 26 20 | -5737 -1182 3023 8132
| 1 0 2 23 22 42 .03 | 7228 1004
iac n/a| -1 0 -3 -4 23 -30 -.21 29 29 | -2836 108 3681 12938
| 2 2 4 23 44 92 .05 | 8897 805
Table 1.2263.b GPS week : 2263 MJD: 60085.0-60091.0
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 | 20 20 19 24 23 25 27 |
R02 | 7 7 6 5 6 10 8 |
R03 | 7 9 7 8 8 6 11 |
R04 | 8 10 7 10 7 11 12 |
R05 | 11 10 6 6 10 10 10 |
R07 | 7 7 8 8 8 9 8 |
R08 | 9 7 6 8 6 7 7 |
R09 | 14 10 11 14 11 10 11 |
R11 | 10 7 9 10 8 9 8 |
R12 | 11 7 6 7 20 10 8 |
R13 | 26 23 32 26 21 17 24 |
R14 | 15 7 6 7 7 7 8 |
R15 | 14 10 7 8 9 7 9 |
R16 | 23 22 24 25 20 22 25 |
R17 | 7 5 7 7 6 5 7 |
R18 | 9 6 9 7 9 7 9 |
R19 | 27 27 25 24 21 26 27 |
R20 | 39 24 24 43 41 22 43 |
R21 | 9 8 7 7 7 7 7 |
R22 | 9 11 8 9 9 8 9 |
R24 | 11 12 11 11 7 10 10 |
R25 | 14 13 13 13 14 0 10 |
Table 1.2263.c GPS week : 2263 MJD: 60085.0-60091.0
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 2263 0 | 29 10 89 34 266 1625 81.8 2041 2041 | -912 0
brd 2263 1 | -42 -13 136 -262 -349 851 82.0 1776 1776 | -819 0
brd 2263 2 | 59 -16 241 -562 -516 1903 82.0 1775 1775 | -11366 0
brd 2263 3 | 129 10 219 -1682 -1606 2692 83.7 1689 1689 | -42 0
brd 2263 4 | -58 -7 162 -855 -372 36 82.3 1610 1610 | -196 0
brd 2263 5 | -64 -31 262 -1443 643 2511 81.1 1682 1682 | -14279 0
brd 2263 6 | -55 -15 248 -357 2552 183 81.1 1658 1658 | -15616 0
-------------+------------------------------------------------------------+----------------
brd 2263 mean| 0 -9 194 -732 88 1400 82.0 1747 1747 | -6175 0
brd 2263 sdev| 75 15 65 632 1294 1068 .9 143 143 | 7205 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 2.2263.0 GPS week: 2263 Day: 0 MJD: 60085
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 7 -33 37 .07 19 16 | 37386 -1505 2955 9062
esa n/a| -1 0 -1 -4 -4 -39 -.21 42 31 | -3931 -1412 2888 7759
gfz n/a| 0 1 0 20 -3 -12 -.07 26 15 | 0 -2075 2909 8302
grg n/a| 1 0 0 -37 68 -27 .18 29 21 | 31 -2193 2949 7748
iac n/a| -1 0 -10 8 23 -34 -.14 27 25 | 890 -525 2895 8983
Table 2.2263.1 GPS week: 2263 Day: 1 MJD: 60086
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 0 17 -16 27 .06 17 15 | 36051 -1900 3206 9657
esa n/a| -1 0 -3 -22 -27 -22 -.11 52 28 | 3157 -2022 3192 8889
gfz n/a| 0 1 0 30 18 -71 -.13 22 12 | 0 -2132 3229 9014
grg n/a| 2 0 0 -31 15 65 .24 22 20 | 147 -2269 3236 8496
iac n/a| 2 1 -5 4 84 -62 -.20 23 20 | 1292 25 3181 9613
Table 2.2263.2 GPS week: 2263 Day: 2 MJD: 60087
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 -1 15 -34 38 .09 23 17 | 22350 -1135 3286 9279
esa n/a| 0 0 0 -5 -5 -20 -.14 50 23 | -12236 -642 3241 7710
gfz n/a| 0 0 0 15 -5 -4 -.20 23 12 | 0 -1607 3260 8863
grg n/a| 3 0 0 -19 40 -17 .20 22 15 | -11139 -1199 3301 8383
iac n/a| 0 2 -8 -35 45 -30 -.17 26 23 | -10144 281 3221 9272
Table 2.2263.3 GPS week: 2263 Day: 3 MJD: 60088
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 13 -9 23 .07 20 18 | 35578 -503 4346 9857
esa n/a| 1 -2 2 -2 -1 15 -.15 40 24 | -8319 813 4201 7899
gfz n/a| 0 0 1 17 -4 2 -.23 24 15 | 0 483 2904 9072
grg n/a| 1 -1 -4 -46 0 -54 .24 30 21 | -293 585 2859 8670
iac n/a| -5 -3 -1 -16 27 78 -.24 23 22 | 4047 -443 4186 10317
Table 2.2263.4 GPS week: 2263 Day: 4 MJD: 60089
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 0 15 -14 28 .05 15 12 | 42109 1358 7218 38025
esa n/a| 0 0 3 13 15 -29 -.14 39 23 | 17045 2008 6907 37206
gfz n/a| 3 0 -1 -3 -11 0 -.24 24 14 | 0 -41 3017 8528
grg n/a| 0 0 -4 -38 35 -34 .24 30 20 | 3 -613 3033 8023
iac n/a| -1 0 1 36 41 -48 -.20 38 54 | 9384 1777 6527 34597
Table 2.2263.5 GPS week: 2263 Day: 5 MJD: 60090
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 -1 -10 -29 9 .10 19 15 | 18855 -1129 3077 7933
esa n/a| -1 0 0 -33 13 18 -.15 45 27 | -16441 -953 3073 13279
gfz n/a| -1 0 0 33 23 13 -.24 25 16 | 0 -2124 3066 7887
grg n/a| 3 0 -1 -11 19 -62 .28 21 19 | -13489 -1727 3057 7506
iac n/a| 0 -3 2 -17 0 -192 -.24 35 33 | -12000 -496 3062 8523
Table 2.2263.6 GPS week: 2263 Day: 6 MJD: 60091
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 -2 -7 9 37 .07 25 21 | 15896 -562 2707 9097
esa n/a| -3 0 0 -26 18 -14 -.17 38 22 | -14415 -209 2709 8278
gfz n/a| 1 -1 6 4 -33 -35 -.06 26 18 | 0 -602 2733 8443
grg n/a| 4 1 -3 23 16 -8 .27 28 24 | -15421 -864 2728 8099
iac n/a| -3 -3 0 -14 -60 77 -.30 33 30 | -13323 137 2695 9265
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 3.2263.0 GPS week: 2263 Day: 0 MJD: 60085
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 561 34 48 27 28 23 19 | 104 53 84 79 78 83
R02 | 644 9 13 13 14 19 7 | 70 64 71 72 69 69
R03 | 1535 9 15 9 12 18 6 | 75 73 81 81 78 77
R04 | 714 10 15 7 19 26 7 | 76 73 70 71 58 72
R05 | 793 14 21 18 21 21 10 | 67 78 77 64 70 69
R07 | 925 9 9 14 12 43 6 | 84 77 78 89 108 81
R08 | 991 12 18 14 16 22 8 | 77 87 87 82 91 82
R09 | 3604 19 41 16 24 25 14 | 43 52 38 44 51 40
R11 | 2984 14 18 16 20 14 9 | 21 26 33 25 24 22
R12 | 1130 11 18 15 27 23 10 | 351 355 352 350 350 351
R13 | 967 28 61 61 26 39 26 | 58 57 110 64 50 65
R14 | 3515 20 16 14 42 22 14 | 46 53 57 86 54 57
R15 | 1517 13 19 15 44 21 14 | 48 53 46 78 63 52
R16 | 1453 22 31 56 42 28 23 | 44 45 58 58 53 47
R17 | 602 7 12 15 7 34 6 | 25 23 32 28 36 26
R18 | 611 12 25 14 12 35 9 | 23 31 32 32 31 25
R19 | 528 45 62 29 52 26 26 | 43 37 53 49 43 39
R20 | 5188 23 138 45 53 32 38 | 86 29 84 89 79 76
R21 | 1526 10 25 13 17 27 9 | 46 44 49 56 54 47
XR22 | 3401 --- 18 5 13 19 9 | --- 210 205 195 198 203
R24 | 2483 20 21 19 16 25 11 | 36 32 27 37 34 30
XR25 |16419 8 20 --- --- 37 13 | 35 26 --- --- 31 30
------+------------------------------------+--------------------------------
RMS | 2041 19 42 26 29 27 |T 69 71 82 82 77 74
WRMS | 2041 16 31 15 21 25 |NE 69 71 82 82 77 74
MEDI | 1130 13 19 15 20 25 |MD 48 53 70 71 54 57
Table 3.2263.1 GPS week: 2263 Day: 1 MJD: 60086
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 504 30 51 24 30 29 19 | 69 47 53 73 46 60
R02 | 596 11 8 14 14 27 7 | 45 44 36 51 54 42
R03 | 863 12 18 8 20 11 8 | 44 38 51 64 45 48
R04 | 506 23 12 12 14 13 9 | 49 35 34 42 36 39
R05 | 610 15 19 11 24 15 10 | 45 52 34 38 42 39
R07 | 870 4 15 14 13 22 7 | 62 51 68 70 66 63
R08 | 754 11 10 11 12 18 6 | 58 61 68 65 67 62
R09 | 3077 16 17 19 13 21 9 | 31 34 42 33 39 33
R11 | 3020 11 9 12 11 18 6 | 15 21 27 25 29 20
R12 | 2102 9 13 10 15 17 7 | 246 250 244 242 250 245
R13 | 948 20 59 45 34 38 23 | 61 45 68 65 41 53
R14 | 3738 7 9 12 14 17 6 | 44 45 46 43 44 43
R15 | 1710 15 17 17 18 12 9 | 40 50 56 51 48 47
R16 | 2458 24 32 58 29 22 22 | 43 49 48 46 42 41
R17 | 734 9 6 10 7 41 4 | 22 22 21 26 31 21
R18 | 582 9 15 7 11 15 6 | 21 18 22 28 17 21
R19 | 581 32 78 27 45 22 26 | 35 33 41 30 36 27
R20 | 2976 26 195 33 42 25 24 | 46 59 44 32 44 40
R21 | 1304 10 21 11 14 33 8 | 35 39 39 43 38 37
XR22 | 4350 --- 22 15 8 20 11 | --- 185 182 170 180 178
R24 | 1077 18 35 15 12 14 12 | 29 27 28 32 24 25
XR25 |18085 9 16 --- --- 52 12 | 37 21 --- --- 27 29
------+------------------------------------+--------------------------------
RMS | 1776 17 52 22 22 23 |T 51 55 59 60 56 55
WRMS | 1776 15 28 12 20 20 |NE 51 55 59 60 56 55
MEDI | 948 12 17 14 14 20 |MD 44 44 44 43 42 40
Table 3.2263.2 GPS week: 2263 Day: 2 MJD: 60087
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 855 32 57 14 16 42 19 | 79 39 82 71 46 65
R02 | 757 9 10 7 10 17 5 | 59 55 57 63 55 58
R03 | 778 12 10 12 12 19 6 | 50 61 52 62 60 55
R04 | 469 18 5 15 7 23 7 | 51 46 43 55 34 47
R05 | 744 11 6 9 9 20 5 | 45 40 44 46 38 43
R07 | 1095 12 14 17 9 32 7 | 68 64 79 66 87 69
R08 | 685 7 12 7 10 23 5 | 69 67 73 73 82 70
R09 | 3818 22 20 16 13 14 10 | 18 34 32 25 25 24
R11 | 2531 14 14 20 12 21 9 | 39 35 45 46 37 40
R12 | 3022 9 13 8 12 17 6 | 386 387 392 387 397 388
R13 | 845 58 35 55 62 50 31 | 69 40 72 52 64 43
R14 | 3055 10 12 10 9 10 6 | 42 50 45 50 35 45
R15 | 1044 13 10 11 12 11 6 | 42 44 40 44 38 40
R16 | 2883 25 31 62 30 26 23 | 35 41 45 35 35 34
R17 | 700 12 9 13 12 38 7 | 21 22 21 24 31 20
R18 | 635 13 20 10 14 16 8 | 22 23 19 25 20 20
R19 | 772 46 55 27 40 39 24 | 51 33 40 29 52 34
R20 | 1829 33 195 30 38 25 24 | 57 37 70 57 51 65
R21 | 994 6 19 9 10 21 7 | 36 43 35 38 39 36
XR22 | 4452 --- 15 9 10 23 8 | --- 156 147 145 146 149
R24 | 1798 17 28 13 17 20 11 | 25 26 26 33 26 24
XR25 |16516 11 14 --- --- 33 13 | 22 25 --- --- 20 21
------+------------------------------------+--------------------------------
RMS | 1774 23 50 23 22 26 |T 61 62 69 67 64 63
WRMS | 1774 17 23 12 15 23 |NE 61 62 69 67 64 63
MEDI | 994 13 14 13 12 21 |MD 45 40 45 50 38 43
Table 3.2263.3 GPS week: 2263 Day: 3 MJD: 60088
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1137 41 61 28 30 29 23 | 91 34 63 64 54 65
R02 | 750 7 14 6 9 15 5 | 62 54 62 63 61 60
R03 | 1350 14 11 6 19 17 7 | 49 64 57 71 60 58
R04 | 750 18 14 18 12 22 9 | 47 48 39 40 30 41
R05 | 973 8 7 10 12 16 5 | 43 41 37 47 38 41
R07 | 696 9 21 12 13 23 8 | 64 69 77 72 81 70
R08 | 924 8 13 15 16 29 7 | 63 66 74 59 83 65
R09 | 4400 23 20 28 20 21 13 | 21 39 45 27 38 26
R11 | 2028 13 11 17 24 13 10 | 25 32 38 20 32 26
R12 | 2360 7 16 10 16 27 7 | 217 218 222 225 231 220
R13 | 883 45 39 41 51 30 25 | 68 31 47 43 54 41
R14 | 2580 8 12 11 15 16 6 | 50 56 56 53 57 52
R15 | 1511 9 13 17 17 14 8 | 50 43 55 44 47 47
R16 | 2226 28 41 63 29 33 24 | 51 53 58 44 55 48
R17 | 614 7 15 11 13 14 6 | 29 24 29 26 29 26
R18 | 621 10 16 8 14 24 7 | 25 28 25 23 26 22
R19 | 650 31 48 20 62 26 23 | 45 44 38 63 45 40
R20 | 1843 20 141 40 80 27 42 | 82 48 88 110 80 74
R21 | 775 6 19 13 12 24 7 | 31 25 31 33 29 29
XR22 | 3369 --- 12 9 16 31 9 | --- 95 96 92 98 94
R24 | 1279 10 27 17 21 32 10 | 33 32 27 44 40 31
XR25 |16282 9 19 --- --- 33 13 | 26 21 --- --- 28 25
------+------------------------------------+--------------------------------
RMS | 1689 20 40 24 30 23 |T 55 52 60 60 58 54
WRMS | 1689 18 24 15 21 22 |NE 55 52 60 60 58 54
MEDI | 1137 10 16 15 16 24 |MD 49 43 55 47 47 41
Table 3.2263.4 GPS week: 2263 Day: 4 MJD: 60089
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1408 31 59 34 37 30 23 | 81 40 87 54 54 68
R02 | 635 6 10 9 14 13 5 | 59 58 58 46 63 55
R03 | 899 9 9 15 17 21 7 | 52 49 48 62 66 51
R04 | 726 12 6 13 9 29 6 | 50 51 51 52 33 50
R05 | 1024 16 14 25 10 17 10 | 36 41 34 34 30 33
R07 | 826 7 19 11 18 16 8 | 59 50 56 72 63 58
R08 | 783 9 10 7 13 26 5 | 56 63 60 60 74 58
R09 | 4524 14 25 18 16 23 10 | 24 40 37 23 35 27
R11 | 1643 7 10 19 18 22 8 | 27 29 42 28 25 29
R12 | 1294 21 20 21 65 132 20 | 571 566 571 543 537 564
R13 | 1044 28 53 33 34 23 21 | 68 39 70 44 61 54
R14 | 2809 7 12 14 17 19 7 | 50 55 46 63 63 52
R15 | 1493 11 16 15 19 11 8 | 52 49 56 48 51 50
R16 | 1713 21 31 57 23 23 20 | 52 54 57 51 55 51
R17 | 811 7 10 11 9 24 5 | 27 27 31 30 36 28
R18 | 609 16 14 17 13 21 9 | 25 30 33 29 30 25
R19 | 791 19 48 19 54 21 20 | 40 52 48 46 33 42
R20 | 1721 16 132 51 73 46 40 | 66 52 83 83 74 63
R21 | 812 6 14 11 18 18 7 | 38 39 41 47 46 40
XR22 | 2272 --- 15 10 11 30 8 | --- 136 120 129 139 128
R24 | 1218 9 13 16 8 32 7 | 32 30 39 35 40 32
XR25 |11282 9 20 --- --- 26 14 | 41 35 --- --- 27 36
------+------------------------------------+--------------------------------
RMS | 1609 15 39 24 30 38 |T 71 72 79 75 74 72
WRMS | 1609 12 23 14 20 54 |NE 71 72 79 75 74 72
MEDI | 1044 11 14 16 17 23 |MD 50 49 51 48 51 50
Table 3.2263.5 GPS week: 2263 Day: 5 MJD: 60090
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1353 46 59 30 29 32 25 | 73 26 48 56 59 50
R02 | 771 8 12 27 16 27 9 | 49 45 67 45 69 49
R03 | 745 5 11 10 11 15 5 | 43 43 44 47 41 43
R04 | 627 13 14 29 13 21 10 | 47 46 24 50 48 39
R05 | 1213 14 16 22 13 38 9 | 37 40 24 36 32 32
R07 | 1184 10 17 23 10 16 9 | 45 33 52 46 45 43
R08 | 776 12 12 9 12 24 6 | 47 44 51 55 63 49
R09 | 3996 15 25 17 10 24 10 | 23 37 30 22 40 24
R11 | 1651 15 13 16 13 23 8 | 23 29 26 17 22 20
R12 | 1769 8 22 12 25 105 10 | 418 430 421 415 377 420
R13 | 951 24 38 25 26 36 16 | 50 42 48 45 56 39
R14 | 3099 10 14 9 15 25 7 | 40 48 41 57 62 45
R15 | 983 9 12 13 14 23 7 | 44 43 32 47 55 40
R16 | 1503 21 25 65 25 29 21 | 41 39 49 36 40 36
R17 | 1190 10 7 6 9 27 5 | 20 18 23 26 20 20
R18 | 600 12 15 12 10 20 7 | 20 23 29 26 24 22
R19 | 546 31 47 33 62 30 25 | 28 30 36 27 34 24
R20 | 3125 31 173 34 24 28 21 | 50 71 65 38 43 54
R21 | 624 10 14 14 10 35 6 | 41 39 42 40 44 40
XR22 | 2261 --- 12 14 8 40 8 | --- 77 76 74 59 75
R24 | 1380 15 16 22 15 25 10 | 25 24 29 31 21 22
XR25 |14887 2 --- --- --- 26 0 | 26 --- --- --- 26 29
------+------------------------------------+--------------------------------
RMS | 1681 19 45 25 21 35 |T 56 58 59 58 58 55
WRMS | 1681 15 27 16 19 33 |NE 56 58 59 58 58 55
MEDI | 1190 12 15 17 13 26 |MD 41 40 42 45 43 39
Table 3.2263.6 GPS week: 2263 Day: 6 MJD: 60091
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 958 53 71 24 26 51 26 | 101 44 69 76 92 70
R02 | 957 13 12 19 9 19 8 | 70 67 86 75 80 74
R03 | 804 19 10 27 12 20 11 | 68 70 87 73 74 73
R04 | 670 11 13 25 28 18 12 | 66 57 71 58 55 61
R05 | 1935 20 11 20 12 40 10 | 56 52 43 57 47 51
R07 | 702 9 6 18 15 25 7 | 64 64 65 73 72 65
R08 | 998 12 7 12 16 28 7 | 66 72 82 78 85 74
R09 | 3034 16 20 12 23 19 10 | 29 43 36 24 44 28
R11 | 1793 15 10 9 15 18 7 | 29 34 33 25 27 28
R12 | 2139 11 13 13 14 24 7 | 363 366 368 361 376 364
R13 | 814 20 58 52 28 46 24 | 81 53 114 74 68 77
R14 | 1796 12 16 14 15 38 8 | 62 74 68 76 88 68
R15 | 782 15 13 9 20 44 8 | 73 67 72 67 91 69
R16 | 1152 27 37 67 29 31 25 | 66 62 95 57 73 68
R17 | 1868 8 11 12 14 17 6 | 33 29 37 35 42 32
R18 | 714 13 11 18 19 23 9 | 31 33 37 32 30 30
R19 | 680 55 45 15 60 16 27 | 50 48 61 51 52 48
R20 | 3032 50 121 36 77 77 42 | 88 56 107 99 101 82
R21 | 654 8 15 14 8 18 6 | 55 48 58 55 60 53
XR22 | 2402 --- 17 12 10 33 9 | --- 121 122 114 109 117
R24 | 3141 10 24 19 12 24 10 | 42 35 49 46 50 41
XR25 |13264 7 12 --- --- 13 9 | 36 29 --- --- 36 35
------+------------------------------------+--------------------------------
RMS | 1657 25 38 26 28 33 |T 72 69 83 76 79 73
WRMS | 1657 21 22 18 24 30 |NE 72 69 83 76 79 73
MEDI | 998 13 13 18 15 24 |MD 64 53 69 67 68 65
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