[IGSREPORT-29271] Wk 2255 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 17 02:02:05 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2255 (Mar 26, 2023 - Apr 01, 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 2.2255.
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:
igl2255[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2255 in the SP3 format.
igl22557.sum Combination Report for GPS Week 2255.
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 | -0.1 ns
1 | -0.1 ns
2 | -13.7 ns
3 | 0.7 ns
4 | -0.2 ns
5 | -0.3 ns
6 | -0.2 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
----+--------+---------------
0 | ESA | R22
1 | ESA | R22
2 | ESA | R22
3 | ESA | R22
4 | ESA | R22
5 | ESA | R22
6 | ESA | R22
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 1.2255, 1a.2255).
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 2.2255.0-6)
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 3.2255.0-6).
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 2255 summary. (Mar 26, 2023 - Apr 01, 2023)
Table 1.2255.a GPS week : 2255 MJD: 60029.0-60035.0
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 -1 -7 -30 35 .04 18 14 | 32976 -50 3382 8768
| 1 0 1 16 15 19 .05 | 5439 983
esa n/a| 0 -1 0 -6 31 -43 -.17 26 21 | 822 438 3353 8421
| 1 1 1 18 23 26 .02 | 6386 1063
gfz n/a| 0 1 0 13 -15 -25 -.06 27 16 | 0 -22 3330 8573
| 1 1 1 22 17 26 .05 | 0 1157
grg n/a| 0 -1 0 -12 27 41 .14 23 20 | -2027 -136 3344 8176
| 1 1 0 27 14 53 .04 | 5585 1169
iac n/a| -1 0 -5 -9 9 -42 -.31 31 27 | -88 25 3344 9138
| 1 1 3 35 32 82 .10 | 5055 682
Table 1.2255.b GPS week : 2255 MJD: 60029.0-60035.0
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 18 18 19 14 14 16 |
R02 | 12 10 8 10 8 6 8 |
R03 | 8 8 8 8 10 8 6 |
R04 | 8 8 10 8 8 8 7 |
R05 | 8 7 6 12 9 10 8 |
R07 | 9 8 7 7 5 8 11 |
R08 | 8 7 9 7 8 10 7 |
R09 | 11 8 8 12 8 11 10 |
R11 | 7 6 7 10 9 6 11 |
R12 | 12 12 13 10 11 8 12 |
R13 | 18 17 18 20 19 19 22 |
R14 | 11 9 10 10 11 10 8 |
R15 | 8 9 9 7 9 10 8 |
R16 | 22 22 23 22 24 24 22 |
R17 | 11 9 12 9 10 10 12 |
R18 | 12 10 9 10 9 9 9 |
R19 | 19 21 20 17 18 19 17 |
R20 | 35 33 28 31 30 27 32 |
R21 | 9 8 9 9 9 9 11 |
R22 | 11 10 12 9 12 9 13 |
R24 | 14 12 10 10 11 9 10 |
Table 1.2255.c GPS week : 2255 MJD: 60029.0-60035.0
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 2255 0 | -70 -52 219 -266 238 8224 82.6 1469 1469 | -127 0
brd 2255 1 | 42 3 168 -651 154 11030 79.5 1525 1525 | -142 0
brd 2255 2 | -4 -30 119 580 -1277 11750 81.0 1556 1556 | -13681 0
brd 2255 3 | -83 -14 149 558 -1665 6718 79.9 1711 1711 | 717 0
brd 2255 4 | 38 -47 108 2316 682 5506 80.6 1847 1847 | -162 0
brd 2255 5 | -25 -16 40 680 -349 4580 80.9 1364 1364 | -257 0
brd 2255 6 | 43 8 111 -1183 -164 3190 80.1 1579 1579 | -239 0
-------------+------------------------------------------------------------+----------------
brd 2255 mean| -8 -21 131 290 -339 7285 80.6 1578 1578 | -1984 0
brd 2255 sdev| 53 23 55 1138 845 3225 1.0 158 158 | 5168 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 2.2255.0 GPS week: 2255 Day: 0 MJD: 60029
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 -3 28 -44 46 .13 22 17 | 35261 -228 3186 8043
esa n/a| 0 -2 1 -3 14 -83 -.18 28 22 | 4115 -80 3179 7216
gfz n/a| 1 1 0 -6 -24 -39 -.12 29 16 | 0 -380 3160 7929
grg n/a| -1 0 0 -51 37 58 .12 22 18 | 112 -607 3150 7692
iac n/a| -1 0 -7 61 10 -54 -.30 31 25 | 2193 -389 3156 8536
Table 2.2255.1 GPS week: 2255 Day: 1 MJD: 60030
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 -11 -39 37 .00 20 15 | 34715 -1323 3763 9879
esa n/a| 0 0 1 -41 45 -1 -.20 26 19 | -1634 -861 3692 9044
gfz n/a| -1 2 0 30 -1 15 -.01 27 15 | 0 -1572 3683 9700
grg n/a| 1 -1 1 2 14 -32 .13 21 16 | 190 -1182 3673 9376
iac n/a| -2 0 -10 -16 41 -80 -.29 33 31 | 1617 -1172 3664 10228
Table 2.2255.2 GPS week: 2255 Day: 2 MJD: 60031
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 -17 -16 65 .03 21 16 | 20768 1149 3838 9679
esa n/a| 0 -2 -1 11 61 -41 -.14 25 19 | -10185 1802 3830 11988
gfz n/a| -1 2 2 7 -20 -55 -.06 24 11 | 0 1732 3728 9355
grg n/a| 0 0 0 -19 21 40 .13 22 19 | -14691 1507 3806 8791
iac n/a| -1 -4 -7 -46 -44 -62 -.36 33 24 | -11515 232 3812 9985
Table 2.2255.3 GPS week: 2255 Day: 3 MJD: 60032
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 -9 -33 31 .05 19 15 | 35920 1304 3478 8840
esa n/a| 1 -3 0 -12 54 -28 -.17 25 18 | 3231 1973 3411 8031
gfz n/a| 0 2 0 -14 -44 -47 -.03 25 20 | 0 1294 3404 8559
grg n/a| -1 0 1 33 23 64 .14 26 20 | -81 1553 3420 8166
iac n/a| -1 0 -2 -40 -18 -70 -.46 31 28 | 1944 1072 3408 9147
Table 2.2255.4 GPS week: 2255 Day: 4 MJD: 60033
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 -16 -20 28 .03 14 11 | 35989 -152 3039 9261
esa n/a| 2 -2 1 0 28 -39 -.16 25 19 | 9183 439 2979 8104
gfz n/a| -2 1 -2 32 -22 -38 .02 30 19 | 0 -9 2984 9037
grg n/a| 0 -1 0 -18 9 42 .08 26 21 | 16 -472 2999 8516
iac n/a| -1 0 -2 -9 38 77 -.39 30 28 | 2177 78 3001 9567
Table 2.2255.5 GPS week: 2255 Day: 5 MJD: 60034
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 -5 -10 0 -.00 14 12 | 34237 -123 3456 7981
esa n/a| 0 -1 2 11 -5 -68 -.16 28 28 | -3403 -232 3427 7438
gfz n/a| 0 0 -1 0 -3 -12 -.13 29 18 | 0 -560 3413 7879
grg n/a| 1 -3 0 -5 35 130 .18 20 19 | 170 -1128 3424 7560
iac n/a| -3 1 -4 1 37 55 -.18 27 27 | 1000 153 3418 8389
Table 2.2255.6 GPS week: 2255 Day: 6 MJD: 60035
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 0 -20 -51 36 .05 20 15 | 33944 -980 2918 7693
esa n/a| 1 0 -2 -10 23 -38 -.17 25 19 | 4447 31 2954 7129
gfz n/a| -1 -1 0 44 5 0 -.08 26 16 | 0 -659 2942 7553
grg n/a| 2 -2 0 -31 49 -12 .19 25 23 | 94 -623 2939 7134
iac n/a| 0 1 0 -18 3 -160 -.19 28 27 | 1964 202 2952 8114
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 3.2255.0 GPS week: 2255 Day: 0 MJD: 60029
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1197 42 38 21 30 30 19 | 90 82 68 77 76 76
R02 | 1126 22 18 21 18 23 11 | 43 51 47 49 33 44
R03 | 603 12 13 16 11 24 7 | 63 56 55 68 68 60
R04 | 821 14 20 11 9 12 8 | 67 59 68 74 64 66
R05 | 795 12 14 18 10 15 8 | 55 59 67 59 52 58
R07 | 744 12 12 16 18 22 8 | 75 79 77 88 78 79
R08 | 1144 14 16 10 14 31 8 | 60 72 61 69 55 65
R09 | 1708 15 23 18 19 17 11 | 41 45 45 38 44 39
R11 | 1623 12 11 12 14 26 7 | 26 29 32 29 37 27
R12 | 1512 12 25 14 26 20 11 | 49 64 55 44 49 49
R13 | 1364 23 37 33 28 34 17 | 86 55 92 75 90 75
R14 | 823 11 25 15 20 15 10 | 61 76 57 53 62 60
R15 | 1945 11 13 16 16 21 8 | 84 90 82 86 80 84
R16 | 2485 22 28 65 26 27 22 | 88 85 93 86 86 87
R17E | 1395 21 12 15 21 17 10 | 116 107 118 107 101 111
R18E | 1236 20 24 20 20 23 12 | 30 40 35 32 28 30
R19E | 1470 31 37 39 22 56 18 | 75 69 76 73 78 69
R20E | 2637 54 73 73 40 83 35 | 128 161 160 135 140 136
R21E | 1104 14 19 12 12 20 8 | 41 44 46 46 39 42
XR22E | 3283 --- 331 10 10 21 10 | --- 147 46 51 43 48
R24E | 1656 18 14 24 33 26 13 | 153 150 159 137 152 148
------+------------------------------------+--------------------------------
RMS | 1468 22 28 29 22 31 |T 71 77 73 70 69 69
WRMS | 1468 17 22 16 18 25 |NE 63 64 64 63 62 62
MEDI | 1364 14 20 16 19 23 |MD 63 69 67 69 64 65
Table 3.2255.1 GPS week: 2255 Day: 1 MJD: 60030
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1263 29 33 30 30 35 17 | 57 59 49 53 44 52
R02 | 931 14 23 12 14 33 9 | 27 48 35 32 23 32
R03 | 1012 17 9 17 10 15 8 | 38 33 38 28 34 32
R04 | 543 11 20 12 10 16 8 | 46 39 52 50 38 46
R05 | 1552 12 12 14 10 19 7 | 34 35 36 43 38 35
R07 | 1176 8 14 14 14 12 7 | 49 46 50 62 51 50
R08 | 911 9 14 13 11 24 6 | 43 52 43 43 32 44
R09 | 966 12 15 16 14 13 8 | 45 46 51 35 47 42
R11 | 2760 9 12 11 9 16 6 | 26 34 35 29 30 28
R12 | 1161 18 22 15 27 15 12 | 47 46 37 41 38 39
R13 | 2404 19 33 29 32 30 16 | 77 50 70 66 76 65
R14 | 1320 7 20 11 17 18 8 | 57 67 61 53 52 58
R15 | 1626 14 16 10 17 13 8 | 64 74 62 60 68 64
R16 | 1713 25 32 64 21 22 22 | 66 70 84 79 68 73
R17E | 1849 11 13 12 22 34 8 | 84 85 88 91 72 86
R18E | 1061 8 23 18 16 19 9 | 35 37 28 33 32 30
R19E | 1635 29 36 46 33 45 21 | 62 59 80 53 72 57
R20E | 2199 54 67 61 44 89 32 | 107 99 126 114 115 102
R21E | 1061 8 17 15 12 12 7 | 33 29 36 37 36 32
XR22E | 2956 --- 335 9 9 19 9 | --- 113 39 46 40 42
R24E | 1380 18 17 19 24 59 11 | 163 166 174 167 145 167
------+------------------------------------+--------------------------------
RMS | 1524 20 26 27 21 33 |T 58 61 60 57 54 56
WRMS | 1524 15 19 15 16 31 |NE 48 49 50 48 45 47
MEDI | 1320 12 20 15 16 19 |MD 47 50 50 50 44 46
Table 3.2255.2 GPS week: 2255 Day: 2 MJD: 60031
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1688 36 33 29 25 24 18 | 71 49 47 61 71 55
R02 | 787 15 12 12 15 32 8 | 38 41 42 42 23 39
R03 | 602 15 16 3 16 25 8 | 45 51 54 55 44 50
R04 | 530 18 21 15 13 22 10 | 54 49 36 49 51 45
R05 | 1508 10 12 11 10 14 6 | 46 39 52 52 41 46
R07 | 1417 13 11 10 12 12 6 | 59 49 56 51 49 53
R08 | 1304 5 15 13 23 19 9 | 47 51 45 42 37 45
R09 | 939 18 16 11 9 16 8 | 31 41 40 39 32 35
R11 | 2210 11 13 12 9 16 6 | 23 29 30 27 32 26
R12 | 1163 10 31 20 21 19 12 | 38 49 32 36 44 35
R13 | 2333 25 41 22 32 35 17 | 71 46 61 62 69 58
R14 | 1901 13 17 17 20 23 10 | 52 64 72 55 46 59
R15 | 799 13 13 17 18 24 9 | 73 71 56 71 61 66
R16 | 1175 22 29 63 31 25 23 | 76 75 81 63 76 73
R17E | 1014 15 19 24 21 19 11 | 74 70 79 69 56 71
R18E | 1140 11 16 13 20 23 9 | 35 33 34 30 29 31
R19E | 1957 26 34 40 38 45 20 | 49 61 55 49 55 45
R20E | 3119 51 57 44 35 104 27 | 90 106 105 83 103 89
R21E | 1246 15 14 11 17 20 8 | 34 35 32 37 35 32
XR22E | 2969 --- 326 11 12 26 12 | --- 127 32 48 38 40
R24E | 1639 17 19 10 19 20 9 | 92 98 106 101 99 98
------+------------------------------------+--------------------------------
RMS | 1556 21 25 24 22 33 |T 54 58 54 53 51 51
WRMS | 1556 16 19 11 19 24 |NE 51 50 50 50 48 48
MEDI | 1304 15 17 13 19 23 |MD 49 49 52 51 46 46
Table 3.2255.3 GPS week: 2255 Day: 3 MJD: 60032
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1489 27 34 32 40 26 19 | 77 46 51 72 77 60
R02 | 722 12 12 22 23 15 10 | 36 41 34 53 39 38
R03 | 517 9 14 12 19 22 8 | 48 52 48 64 48 52
R04 | 529 10 18 13 12 15 7 | 47 47 40 49 44 44
R05 | 831 23 20 16 19 20 11 | 43 53 46 36 38 42
R07 | 1042 7 12 13 12 19 6 | 62 61 57 55 59 58
R08 | 1633 11 12 15 12 17 7 | 55 44 49 50 56 49
R09 | 1369 19 20 21 24 25 12 | 21 29 32 31 29 21
R11 | 1227 15 13 25 11 19 10 | 19 26 44 27 33 27
R12 | 1025 12 21 12 20 25 9 | 38 50 43 39 53 40
R13 | 2082 24 43 26 39 33 19 | 74 36 69 76 79 62
R14 | 2024 13 18 19 20 12 10 | 44 49 34 46 34 41
R15 | 882 12 11 11 13 9 6 | 59 52 49 49 49 52
R16 | 913 26 37 57 24 25 21 | 64 51 59 60 53 55
R17E | 633 13 13 12 21 19 8 | 56 58 62 61 62 58
R18E | 1646 12 18 16 24 15 10 | 35 40 34 33 32 33
R19E | 2237 19 31 35 33 38 17 | 39 49 51 47 57 37
R20E | 1529 44 52 53 65 103 30 | 114 130 131 157 134 124
R21E | 946 14 15 11 20 18 8 | 33 30 35 44 28 33
XR22E | 3233 --- 356 8 9 29 9 | --- 141 31 33 34 31
R24E | 4998 16 24 14 13 21 10 | 107 107 99 94 100 101
------+------------------------------------+--------------------------------
RMS | 1711 19 25 25 26 31 |T 53 56 52 56 54 50
WRMS | 1711 15 18 20 20 28 |NE 49 45 46 50 49 45
MEDI | 1227 13 18 16 20 20 |MD 47 49 48 49 49 44
Table 3.2255.4 GPS week: 2255 Day: 4 MJD: 60033
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 939 21 31 24 23 20 14 | 74 54 66 63 65 66
R02 | 473 8 15 13 21 16 8 | 35 27 27 47 43 32
R03 | 657 11 10 24 24 16 9 | 44 47 42 60 46 45
R04 | 827 9 14 14 17 24 7 | 47 46 48 58 51 48
R05 | 640 12 17 14 22 17 9 | 38 48 41 32 34 38
R07 | 919 6 9 9 10 23 5 | 56 56 58 61 44 56
R08 | 776 7 12 24 11 13 8 | 50 52 45 47 45 48
R09 | 2272 10 12 13 16 26 7 | 36 46 52 55 37 44
R11 | 743 11 15 19 19 28 9 | 34 39 52 44 55 39
R12 | 891 7 22 21 27 14 10 | 49 60 54 45 52 50
R13 | 1952 17 51 32 27 36 18 | 85 48 100 93 88 78
R14 | 1183 10 21 26 24 13 11 | 50 51 34 36 49 42
R15 | 910 13 15 12 20 15 8 | 76 69 68 67 70 70
R16 | 1062 15 29 76 41 24 23 | 79 72 96 71 80 78
R17E | 1557 9 15 24 20 15 9 | 49 38 55 43 45 44
R18E | 1383 10 17 16 19 15 8 | 30 35 36 36 29 31
R19E | 1168 15 33 45 34 25 17 | 43 54 61 55 49 44
R20E | 2362 31 61 62 61 101 30 | 82 90 98 121 84 83
R21E | 872 10 11 16 26 14 9 | 32 28 40 41 29 32
XR22E | 3022 --- 338 11 11 30 11 | --- 113 41 46 30 42
R24E | 6196 15 23 17 21 24 10 | 55 44 47 56 51 49
------+------------------------------------+--------------------------------
RMS | 1846 14 25 30 26 30 |T 52 53 55 56 51 50
WRMS | 1846 11 19 19 21 28 |NE 53 51 55 55 54 52
MEDI | 939 10 17 19 21 20 |MD 49 48 52 55 49 45
Table 3.2255.5 GPS week: 2255 Day: 5 MJD: 60034
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 581 19 34 18 21 20 13 | 55 48 63 69 52 58
R02 | 583 8 13 11 12 19 6 | 40 37 43 36 47 38
R03 | 612 8 19 13 17 15 8 | 45 37 41 47 41 42
R04 | 523 11 10 13 16 19 7 | 43 46 44 53 51 46
R05 | 1312 17 20 13 18 14 10 | 40 41 35 36 36 36
R07 | 712 7 20 7 16 16 7 | 47 57 56 56 46 52
R08 | 797 11 21 16 19 20 9 | 43 40 47 55 37 45
R09 | 1987 14 10 28 20 19 11 | 31 31 58 22 27 32
R11 | 982 7 15 12 9 26 6 | 32 38 38 37 44 34
R12 | 1046 8 17 12 18 28 8 | 46 49 41 47 58 45
R13 | 549 17 53 33 25 27 18 | 79 48 84 72 80 70
R14 | 690 14 22 15 16 21 9 | 46 61 57 57 51 52
R15 | 1246 13 16 26 15 14 10 | 69 74 58 69 64 66
R16 | 1479 16 34 73 38 30 24 | 77 84 91 96 83 85
R17E | 1463 16 14 9 22 21 9 | 57 60 57 68 66 58
R18E | 1566 6 22 17 17 18 9 | 42 45 35 41 41 39
R19E | 777 18 36 51 23 48 18 | 53 51 80 53 77 52
R20E | 2256 26 68 63 30 66 27 | 159 168 169 128 137 152
R21E | 803 14 11 13 21 22 9 | 42 39 41 42 37 39
XR22E | 3183 --- 328 8 9 18 8 | --- 133 42 45 37 45
R24E | 3396 13 20 12 17 28 9 | 85 91 87 80 88 84
------+------------------------------------+--------------------------------
RMS | 1363 14 28 29 20 27 |T 56 60 60 57 57 55
WRMS | 1363 12 28 18 19 27 |NE 49 49 54 53 51 50
MEDI | 982 13 20 13 18 20 |MD 46 48 56 53 51 46
Table 3.2255.6 GPS week: 2255 Day: 6 MJD: 60035
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 609 33 15 34 16 23 15 | 82 63 60 68 73 68
R02 | 579 10 18 8 17 36 7 | 44 49 50 59 44 49
R03 | 654 8 14 11 9 23 6 | 60 57 59 63 71 59
R04 | 826 13 13 11 11 25 7 | 54 43 47 55 63 49
R05 | 1642 14 13 11 14 19 7 | 50 39 48 42 46 44
R07 | 730 13 11 26 23 14 11 | 68 67 74 73 71 69
R08 | 783 12 12 8 15 15 7 | 56 51 53 57 47 53
R09 | 2973 14 15 15 24 22 9 | 42 47 47 37 37 41
R11 | 1028 14 19 28 11 18 11 | 31 35 54 33 49 35
R12 | 1221 8 16 17 37 17 12 | 57 68 62 45 67 55
R13 | 518 23 49 34 43 28 22 | 101 52 101 89 103 85
R14 | 885 8 14 13 17 18 7 | 59 64 53 49 57 56
R15 | 846 11 12 13 17 29 7 | 84 82 75 87 77 81
R16 | 1650 27 30 62 27 23 22 | 101 107 106 106 104 103
R17E | 2411 20 16 15 31 50 12 | 90 96 99 96 90 93
R18E | 801 11 18 16 16 14 9 | 33 30 22 35 27 27
R19E | 498 23 30 34 28 35 16 | 91 82 96 89 78 85
R20E | 3733 52 68 48 48 65 32 | 114 121 124 125 109 111
R21E | 1458 16 16 22 24 18 11 | 39 40 43 44 37 39
XR22E | 3167 --- 347 12 13 20 12 | --- 167 32 36 31 32
R24E | 2348 10 14 19 25 20 10 | 78 78 84 75 75 77
------+------------------------------------+--------------------------------
RMS | 1578 20 25 26 25 28 |T 66 68 66 64 64 62
WRMS | 1578 15 19 16 23 27 |NE 63 58 63 61 64 60
MEDI | 885 13 16 16 17 22 |MD 59 63 59 59 67 56
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