[IGSREPORT-28829] Wk 2218 IGLOS Final Orbits
acc
acc at igs.org
Mon Aug 8 06:52:22 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2218 (Jul 10, 2022 - Jul 16, 2022)
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 2.2218.
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:
igl2218[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2218 in the SP3 format.
igl22187.sum Combination Report for GPS Week 2218.
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.
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 | -0.8 ns
1 | 1.1 ns
2 | 0.2 ns
3 | -1.2 ns
4 | 0.9 ns
5 | -0.3 ns
6 | -0.2 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | EMX | R19
2 | EMX | R19
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 1.2218, 1a.2218).
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 2.2218.0-6)
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 3.2218.0-6).
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 2218 summary. (Jul 10, 2022 - Jul 16, 2022)
Table 1.2218.a GPS week : 2218 MJD: 59770.0-59776.0
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 -1 5 -2 -31 12 .13 22 16 | 1198017 11134 287985 292063
| 1 0 1 17 8 9 .03 | 2025594 32557
emx n/a| -2 -1 -5 0 -17 -8 -.14 47 32 | -6725 -59 3043 8415
| 1 1 5 23 23 17 .05 | 11602 1377
esx n/a| 0 1 0 12 12 12 -.09 26 20 | -4406 372 2915 11242
| 1 0 1 11 18 18 .02 | 6702 1846
gfz n/a| 0 0 1 -10 9 18 -.11 25 17 | 0 -473 3039 8169
| 1 2 3 23 14 19 .04 | 0 1605
grg n/a| 4 0 -3 -28 41 4 .34 29 23 | 681686 -904 3139 149553
| 2 2 5 30 14 47 .08 | 1803202 2077
iac n/a| 0 2 -5 6 -8 -14 -.22 30 28 | 1138452 9753 145656 292297
| 2 3 8 40 59 126 .06 | 1993770 28999
Table 1.2218.b GPS week : 2218 MJD: 59770.0-59776.0
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 | 18 19 21 18 20 18 17 |
R02 | 9 8 8 9 9 11 11 |
R03 | 8 8 10 10 8 9 9 |
R04 | 9 9 10 11 12 9 9 |
R05 | 11 10 8 8 9 9 8 |
R07 | 8 8 10 9 8 8 12 |
R08 | 9 10 9 10 9 7 8 |
R09 | 7 7 7 10 6 8 7 |
R11 | 13 11 15 13 12 11 12 |
R12 | 7 8 8 9 7 6 8 |
R13 | 16 14 12 17 13 17 15 |
R14 | 7 5 7 7 8 7 8 |
R15 | 5 8 7 7 7 6 7 |
R17 | 7 6 7 8 7 8 7 |
R18 | 9 7 9 19 20 18 10 |
R19 | 25 27 17 27 26 25 29 |
R20 | 24 24 24 21 24 23 22 |
R21 | 9 10 9 6 7 7 9 |
R24 | 10 9 11 9 12 11 11 |
Table 1.2218.c GPS week : 2218 MJD: 59770.0-59776.0
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 2218 0 | 17 10 137 -1401 224 10840 80.5 1746 1746 | -759 0
brd 2218 1 | -41 51 83 -1140 431 5876 80.7 1597 1597 | 1076 0
brd 2218 2 | 9 -88 319 695 2264 5699 80.5 1479 1479 | 221 0
brd 2218 3 | 16 -53 168 -28 1424 8504 79.5 1899 1899 | -1168 0
brd 2218 4 | -6 -17 103 474 -628 9334 80.3 1599 1599 | 873 0
brd 2218 5 | 27 -58 220 2017 -400 4164 83.0 1501 1501 | -329 0
brd 2218 6 | 59 55 160 -193 -341 6226 82.9 1445 1445 | -232 0
-------------+------------------------------------------------------------+----------------
brd 2218 mean| 11 -14 170 60 424 7234 81.1 1609 1609 | -45 0
brd 2218 sdev| 31 56 79 1158 1064 2368 1.4 162 162 | 822 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 2.2218.0 GPS week: 2218 Day: 0 MJD: 59770
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 4 12 -39 13 .12 25 18 | 36050 -2238 2884 8351
emx n/a| -4 -3 -10 21 -27 -10 -.13 54 32 | -10888 -939 2833 7965
esx n/a| 0 0 0 14 -4 35 -.09 27 22 | -13074 -1496 2821 11292
gfz n/a| 0 0 4 -42 -1 31 -.15 28 19 | 0 -2007 2810 7901
grg n/a| 6 -1 -7 -40 20 35 .35 29 20 | 152 -2022 2845 7336
iac n/a| 0 1 2 42 31 -107 -.16 21 20 | 1528 -568 2840 8796
Table 2.2218.1 GPS week: 2218 Day: 1 MJD: 59771
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 4 8 -30 15 .10 25 18 | 35706 2063 2987 8998
emx n/a| -2 -4 -4 14 19 14 -.12 46 32 | 8435 824 2987 8777
esx n/a| -1 1 -1 11 51 35 -.08 26 21 | -11147 2205 2939 10618
gfz n/a| -1 -1 1 9 18 26 -.08 22 15 | 0 1355 2962 8589
grg n/a| 3 0 -7 -79 53 47 .40 29 26 | 135 1496 2937 8284
iac n/a| 4 6 3 36 -124 -126 -.21 27 25 | 2766 734 2939 9282
Table 2.2218.2 GPS week: 2218 Day: 2 MJD: 59772
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 6 -4 -31 0 .15 20 14 | 37382 -30 3310 8632
emx n/a| 0 0 0 9 -11 -18 -.22 36 33 | 3466 -179 3281 8463
esx n/a| -3 1 1 17 10 -13 -.09 27 19 | 6689 -438 3065 11237
gfz n/a| 0 1 1 1 15 2 -.17 20 14 | 0 153 3297 8095
grg n/a| 5 -3 -12 -18 54 -50 .40 24 21 | 76 -224 3233 7674
iac n/a| 2 0 0 -51 -45 200 -.26 32 31 | 3516 -2088 3219 8857
Table 2.2218.3 GPS week: 2218 Day: 3 MJD: 59773
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 4 -39 -30 0 .11 22 16 | 37249 -2044 4005 9683
emx n/a| -3 0 -8 -21 -40 -26 -.16 47 32 | -14410 -1748 3715 9193
esx n/a| 0 1 0 18 2 -2 -.10 25 25 | -6767 -1907 3160 11684
gfz n/a| 0 -2 2 3 -7 36 -.11 25 15 | 0 -2794 3681 9058
grg n/a| 6 1 -2 -6 47 -2 .36 33 22 | 755 -3773 3168 8286
iac n/a| 0 0 -7 4 35 -60 -.24 29 28 | 1956 -1252 3842 9820
Table 2.2218.4 GPS week: 2218 Day: 4 MJD: 59774
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 4 11 -31 20 .14 19 13 | 3394231 84853 999999 999999
emx n/a| -2 -2 -14 -44 -38 -16 -.08 52 34 | -20931 2519 2985 7501
esx n/a| 0 0 -2 -10 17 14 -.08 25 17 | -1951 3086 2987 9803
gfz n/a| 0 -1 2 11 21 -15 -.06 27 17 | 0 1465 3010 7551
grg n/a| 2 3 4 -29 48 30 .27 35 20 | -238 1746 3026 7236
iac n/a| -1 1 -10 52 22 -82 -.16 31 30 | 3184193 75471 999999 999999
Table 2.2218.5 GPS week: 2218 Day: 5 MJD: 59775
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 6 -5 -44 14 .19 22 16 | 4810146 -3633 999999 999999
emx n/a| -1 -1 -4 5 7 17 -.16 48 32 | 3513 -339 2745 8542
esx n/a| 0 1 3 25 0 16 -.05 24 18 | -3931 967 2723 11699
gfz n/a| 1 2 1 -11 26 15 -.12 26 22 | 0 -540 2767 7812
grg n/a| 2 -1 1 -41 43 40 .19 29 32 | 4770965 -2685 4017 999999
iac n/a| -1 -1 -20 0 -14 -53 -.20 31 28 | 4773272 -2755 4024 999999
Table 2.2218.6 GPS week: 2218 Day: 6 MJD: 59776
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 -2 6 2 -16 22 .09 23 17 | 35361 -1033 2714 8784
emx n/a| 0 -2 0 8 -30 -20 -.10 45 31 | -16265 -555 2756 8465
esx n/a| 1 1 0 10 12 0 -.11 26 19 | -664 189 2710 12363
gfz n/a| 0 1 -6 -44 -7 33 -.10 27 19 | 0 -949 2746 8180
grg n/a| 1 0 -2 18 23 -71 .37 26 22 | -41 -867 2751 8059
iac n/a| -1 5 -3 -37 33 126 -.32 36 35 | 1934 -1268 2731 9328
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 3.2218.0 GPS week: 2218 Day: 0 MJD: 59770
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1169 41 46 36 56 39 21 18 | 76 62 53 81 60 65 59
R02E | 1894 12 26 11 9 20 28 8 | 82 60 82 83 86 81 79
R03E | 766 9 33 15 16 14 17 7 | 75 50 61 78 68 75 68
XR04E | 1670 21 27 13 --- 12 18 9 | 95 84 82 --- 87 79 84
R05E | 1371 24 31 19 20 17 28 10 | 46 28 42 45 44 46 37
R07E | 678 15 26 17 17 17 17 8 | 65 44 52 72 56 64 59
R08E | 1743 8 31 12 25 22 19 8 | 60 40 52 76 71 59 59
R09 | 2159 15 15 14 20 13 17 7 | 50 39 42 52 43 48 43
XR11 | 2583 --- 20 20 15 32 30 12 | --- 36 51 39 58 41 42
R12 | 2419 9 18 17 19 16 15 7 | 64 64 72 71 55 72 66
R13 | 864 34 42 32 30 52 20 16 | 81 40 43 67 48 52 55
R14 | 828 11 12 18 10 12 21 6 | 39 32 49 44 39 31 38
R15 | 864 7 13 10 12 11 14 5 | 63 55 61 65 59 69 62
R17 | 840 11 30 8 19 9 12 6 | 42 33 37 39 42 46 38
R18 | 2318 18 34 20 13 19 18 9 | 33 33 22 40 35 37 36
R19 | 2629 50 175 62 22 66 26 24 | 63 45 31 60 64 67 54
R20 | 1439 50 70 61 68 41 25 23 | 79 67 47 90 73 67 64
R21 | 884 12 25 11 19 17 28 8 | 46 39 41 42 46 52 41
R24 | 3513 20 49 8 15 27 16 10 | 45 42 41 43 45 40 39
------+-----------------------------------------+-------------------------------------
RMS | 1745 25 54 27 28 29 21 |T 61 47 50 60 56 57 53
WRMS | 1745 18 32 22 19 20 20 |NE 55 43 44 54 50 51 48
MEDI | 1439 15 30 17 19 17 19 |MD 63 42 49 60 56 59 55
Table 3.2218.1 GPS week: 2218 Day: 1 MJD: 59771
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 822 47 49 36 44 47 34 19 | 63 54 52 57 58 58 50
R02E | 1700 9 28 11 23 19 21 8 | 68 57 68 78 67 62 67
R03E | 802 13 33 11 12 17 26 8 | 66 50 53 59 71 47 57
XR04E | 1152 15 29 14 --- 16 21 9 | 87 78 87 --- 83 80 82
R05E | 1517 20 34 23 13 21 24 9 | 42 31 50 47 41 48 40
R07E | 1004 15 25 14 15 14 24 7 | 53 40 44 45 52 57 46
R08E | 1157 9 36 15 22 15 29 9 | 43 36 43 59 50 60 47
R09 | 1039 13 25 11 12 15 21 7 | 57 46 57 65 55 54 55
XR11 | 2714 --- 31 12 13 31 27 11 | --- 41 53 39 85 37 49
R12 | 2603 11 15 21 7 28 22 8 | 56 54 66 62 52 54 55
R13 | 917 30 50 21 19 43 27 13 | 60 64 41 45 40 53 45
R14 | 766 6 10 12 9 13 14 5 | 40 42 43 42 39 36 39
R15 | 925 8 14 16 10 14 31 7 | 55 53 52 55 53 65 53
R17 | 1184 10 25 7 12 13 16 6 | 36 37 39 41 42 38 38
R18 | 2068 12 26 20 8 12 15 7 | 32 31 23 35 31 39 33
R19 | 1535 51 128 56 25 61 48 26 | 45 61 37 51 44 53 39
R20 | 1182 52 62 61 49 49 37 23 | 48 51 47 42 39 37 40
R21 | 899 10 32 10 23 21 29 9 | 44 50 44 38 58 42 42
R24 | 3753 20 44 8 11 24 20 9 | 42 38 39 38 39 43 37
------+-----------------------------------------+-------------------------------------
RMS | 1596 25 46 26 22 29 27 |T 52 48 49 49 52 50 48
WRMS | 1596 18 32 21 15 26 25 |NE 46 47 45 46 48 45 43
MEDI | 1157 13 31 14 13 19 24 |MD 48 50 47 45 52 53 46
Table 3.2218.2 GPS week: 2218 Day: 2 MJD: 59772
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 518 54 52 45 46 42 31 20 | 79 62 51 65 51 52 53
R02E | 2161 16 28 14 16 17 20 8 | 78 54 69 55 66 73 65
R03E | 725 9 37 18 15 19 37 9 | 65 49 58 65 58 84 60
XR04E | 1417 13 32 11 --- 14 32 9 | 49 30 40 --- 45 34 39
R05E | 879 9 34 16 13 16 28 8 | 40 30 40 43 44 41 38
R07E | 629 12 30 16 21 19 39 9 | 52 36 44 56 49 47 46
R08E | 1465 10 39 14 13 16 37 9 | 47 35 43 54 55 76 48
R09 | 619 11 17 7 17 14 26 6 | 30 36 30 35 29 50 31
XR11 | 1475 --- 18 19 18 44 47 15 | --- 35 31 37 25 57 24
R12 | 2928 12 23 18 15 16 25 7 | 56 52 58 58 52 55 53
R13 | 926 17 22 16 19 40 39 11 | 60 73 55 65 44 52 55
R14 | 776 8 12 21 11 14 18 6 | 33 33 45 25 29 49 32
R15 | 755 11 16 7 6 13 34 6 | 55 53 54 53 49 58 51
R17 | 987 9 27 10 5 20 31 7 | 27 26 23 24 31 48 25
R18 | 1608 11 29 20 14 19 26 8 | 27 22 18 20 36 33 24
XR19 | 5126 21 160 --- 20 37 47 17 | 46 54 --- 43 73 56 49
R20 | 2031 40 71 80 39 44 40 24 | 44 70 43 48 53 55 38
R21 | 659 9 38 12 11 14 35 8 | 38 28 35 38 44 49 36
R24 | 2664 14 49 10 15 26 34 10 | 29 28 27 26 33 43 25
------+-----------------------------------------+-------------------------------------
RMS | 1479 20 36 27 20 24 32 |T 47 42 42 45 45 53 41
WRMS | 1479 14 33 19 14 21 31 |NE 40 42 38 39 41 50 36
MEDI | 987 11 30 16 15 19 34 |MD 46 36 43 43 45 52 39
Table 3.2218.3 GPS week: 2218 Day: 3 MJD: 59773
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 748 47 42 41 34 36 37 18 | 75 78 78 77 79 84 71
R02E | 4259 14 30 11 15 17 30 8 | 96 77 92 93 83 105 91
R03E | 754 10 36 12 16 22 37 9 | 80 61 70 74 74 96 75
XR04E | 1726 18 28 16 --- 20 31 11 | 73 61 74 --- 68 70 68
R05E | 897 13 36 13 17 20 20 8 | 48 42 51 54 56 51 49
R07E | 846 18 27 13 18 16 28 8 | 68 44 56 63 63 66 59
R08E | 2090 9 37 19 20 13 36 10 | 61 54 55 70 71 87 63
R09 | 680 15 18 18 18 12 40 9 | 50 45 42 57 52 64 49
XR11 | 1269 --- 39 13 20 37 23 12 | --- 48 45 48 47 51 42
R12 | 2595 16 18 15 10 13 39 8 | 62 54 60 57 55 51 55
R13 | 714 23 42 36 37 60 27 16 | 66 56 51 61 69 79 58
R14 | 702 8 19 16 11 22 15 6 | 60 59 65 62 50 59 58
R15 | 789 15 14 14 12 15 19 6 | 72 64 65 63 58 57 63
R17 | 1391 14 30 7 12 21 24 7 | 56 56 59 57 63 60 57
XR18 | 3957 24 23 --- 37 --- 41 19 | 53 48 --- 59 --- 55 47
R19 | 850 42 125 53 49 76 30 27 | 72 63 58 70 54 73 61
R20 | 4253 31 76 49 50 50 28 20 | 68 65 59 76 59 66 60
R21 | 734 14 25 9 7 14 19 6 | 56 53 56 54 58 65 55
R24 | 1557 13 41 11 11 25 19 8 | 58 54 64 57 64 58 58
------+-----------------------------------------+-------------------------------------
RMS | 1899 22 47 25 25 33 29 |T 65 56 61 64 62 68 59
WRMS | 1899 16 32 25 15 22 28 |NE 61 55 56 60 57 61 55
MEDI | 897 15 30 14 17 20 28 |MD 62 56 59 61 59 65 58
Table 3.2218.4 GPS week: 2218 Day: 4 MJD: 59774
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 893 45 46 41 48 58 33 20 | 93 82 83 88 99 85 82
R02E | 3901 14 32 14 21 23 20 8 | 78 61 76 76 85 70 74
R03E | 1095 9 30 15 14 20 26 7 | 65 47 55 68 70 72 62
XR04E | 2538 14 33 13 --- 26 40 11 | 60 48 50 --- 52 58 51
R05E | 1129 13 36 13 14 33 28 9 | 40 38 46 45 58 58 43
R07E | 1164 11 31 17 15 16 28 8 | 51 33 40 56 63 63 50
R08E | 1413 9 34 16 20 28 25 8 | 53 40 50 66 69 52 53
R09 | 1010 12 17 9 12 12 25 6 | 17 21 22 25 17 29 17
XR11 | 1035 --- 29 8 17 23 41 11 | --- 29 47 33 60 58 42
R12 | 1889 11 22 10 15 12 28 7 | 66 65 67 75 61 69 66
R13 | 908 20 35 23 28 34 41 12 | 61 47 49 64 66 51 53
R14 | 738 12 29 13 15 18 26 7 | 38 29 43 39 29 43 35
R15 | 858 12 24 10 14 19 28 7 | 52 50 51 57 53 46 50
R17 | 2027 9 29 11 13 12 21 6 | 25 21 22 24 30 26 21
XR18 | 6765 13 --- --- --- --- 29 19 | 32 --- --- --- --- 55 32
R19 | 1238 35 141 50 42 65 43 25 | 35 40 35 36 41 40 30
R20 | 1877 19 88 54 62 79 35 24 | 59 72 62 65 36 55 53
R21 | 759 11 33 14 7 10 24 7 | 24 22 20 22 24 34 21
R24 | 1610 11 51 13 13 21 53 11 | 31 35 33 35 43 70 34
------+-----------------------------------------+-------------------------------------
RMS | 1598 19 52 25 27 35 31 |T 48 43 47 51 53 54 45
WRMS | 1598 13 34 17 17 20 30 |NE 40 39 41 43 41 48 37
MEDI | 1164 12 32 13 15 21 28 |MD 51 40 47 56 53 55 50
Table 3.2218.5 GPS week: 2218 Day: 5 MJD: 59775
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 578 36 39 41 44 44 38 18 | 116 114 124 124 114 126 116
R02E | 4205 16 32 14 27 13 44 10 | 75 68 83 85 83 64 75
R03E | 939 13 30 14 28 19 19 8 | 82 72 80 85 75 71 77
XR04E | 2179 12 35 11 --- 17 21 8 | 59 54 58 --- 62 52 56
R05E | 1012 15 31 15 18 18 29 8 | 38 34 45 44 41 43 37
R07E | 821 11 39 13 16 13 28 8 | 68 58 73 63 68 76 67
R08E | 955 10 32 12 13 15 23 7 | 44 32 40 47 50 50 42
R09 | 1374 12 20 9 28 20 19 8 | 11 17 18 35 19 32 16
XR11 | 1028 --- 20 20 9 30 22 10 | --- 26 28 26 42 26 26
R12 | 1191 12 19 11 12 8 22 6 | 61 64 60 57 58 36 55
R13 | 871 39 25 29 31 46 50 16 | 48 51 48 53 53 68 47
R14 | 1099 8 18 15 14 17 22 7 | 41 38 49 40 47 39 40
R15 | 1030 10 12 7 15 19 18 6 | 50 53 50 60 43 48 50
R17 | 1693 7 37 9 12 10 31 7 | 26 26 28 24 35 50 27
XR18 | 2628 21 --- --- --- 32 20 17 | 28 --- --- --- 44 24 24
R19 | 1211 46 122 61 48 22 40 25 | 44 43 30 56 25 40 34
R20 | 1042 29 94 35 47 77 34 23 | 34 56 45 47 33 38 33
R21 | 1005 9 29 11 8 16 19 6 | 28 25 25 29 41 32 28
R24 | 1320 16 54 17 13 17 38 11 | 27 27 29 24 33 43 24
------+-----------------------------------------+-------------------------------------
RMS | 1500 22 48 24 26 29 31 |T 48 47 50 52 50 50 46
WRMS | 1500 16 32 18 22 32 28 |NE 36 38 37 41 39 39 33
MEDI | 1042 12 31 14 16 18 23 |MD 44 43 45 47 44 43 40
Table 3.2218.6 GPS week: 2218 Day: 6 MJD: 59776
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 874 38 46 27 44 37 31 16 | 99 106 101 91 107 104 97
R02E | 3150 9 27 17 16 25 56 11 | 99 90 103 91 95 93 94
R03E | 910 13 28 13 25 18 27 9 | 75 56 65 81 71 75 69
XR04E | 2156 13 30 14 --- 17 20 9 | 62 61 57 --- 64 63 59
R05E | 1051 18 29 13 13 14 24 7 | 57 34 54 54 53 57 51
R07E | 916 14 41 18 43 21 27 12 | 92 69 84 105 92 96 89
R08E | 1737 13 29 12 12 15 30 7 | 66 48 65 72 74 76 66
R09 | 893 13 13 12 19 13 28 7 | 25 26 29 32 27 26 24
XR11 | 1762 --- 30 9 17 34 28 11 | --- 31 37 33 50 44 37
R12 | 849 14 12 13 8 13 40 7 | 76 75 84 78 77 62 75
R13 | 1552 31 16 36 33 37 26 14 | 77 61 53 65 66 61 62
R14 | 1088 12 16 11 11 22 31 7 | 47 45 60 50 55 47 49
R15 | 1584 12 14 10 14 17 32 7 | 73 68 73 75 65 53 68
R17 | 1673 9 26 14 11 13 31 7 | 30 21 31 34 39 46 30
XR18 | 1069 11 21 --- 15 12 40 9 | 27 28 --- 20 28 42 24
R19 | 980 43 114 69 58 48 61 28 | 66 53 39 76 50 77 50
R20 | 1020 51 84 47 28 47 43 22 | 73 54 57 81 58 58 57
R21 | 1556 7 28 14 11 15 44 8 | 38 42 34 41 40 51 36
R24 | 1440 16 56 14 18 17 22 10 | 37 22 40 44 42 43 35
------+-----------------------------------------+-------------------------------------
RMS | 1445 23 45 26 27 26 36 |T 62 52 59 62 60 61 56
WRMS | 1445 17 31 19 19 22 35 |NE 51 43 48 52 49 50 45
MEDI | 1088 13 28 14 16 17 31 |MD 66 53 57 65 58 58 57
More information about the IGSREPORT
mailing list