[IGSREPORT-27009] Wk 2084 IGLOS Final Orbits
acc
acc at igs.org
Sat Jan 4 15:33:35 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2084 (Dec 15, 2019 - Dec 21, 2019)
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 2.2084.
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:
igl2084[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2084 in the SP3 format.
igl20847.sum Combination Report for GPS Week 2084.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 | -4.5 ns
1 | -4.0 ns
2 | -3.7 ns
3 | -3.9 ns
4 | -5.5 ns
5 | -5.0 ns
6 | -4.3 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 1.2084, 1a.2084).
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 2.2084.0-6)
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 3.2084.0-6).
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 2084 summary. (Dec 15, 2019 - Dec 21, 2019)
Table 1.2084.a GPS week : 2084 MJD: 58832.0-58838.0
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 0 -4 15 49 .00 29 26 | 20080 -400 2913 7784
| 0 1 1 15 20 13 .03 | 753 845
cof n/a| 0 0 0 -2 0 40 .00 31 27 | 20068 -389 2914 7786
| 0 0 0 25 18 15 .06 | 759 848
emx n/a| 1 0 -10 29 32 -10 -.02 27 27 | -5456 -540 2911 7953
| 1 1 1 29 29 32 .03 | 4527 800
esx n/a| 0 0 1 -7 -25 -24 .05 20 18 | -6423 -1704 2899 9693
| 1 0 0 18 17 24 .03 | 8474 1631
gfz n/a| -1 0 1 -28 -24 -20 .09 29 18 | 0 -310 2917 7762
| 1 1 1 15 14 31 .04 | 0 1013
iac n/a| 0 0 6 9 9 14 -.15 25 21 | -2668 -298 2907 7970
| 1 1 2 19 24 58 .04 | 424 474
mcc n/a| 6 2 8 94 30 312 -.31 221 221 | --- --- --- ---
| 9 10 20 100 120 248 .30 | --- ---
Table 1.2084.b GPS week : 2084 MJD: 58832.0-58838.0
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 | 19 19 19 17 17 18 19 |
R02 | 5 5 5 7 7 5 7 |
R03 | 7 8 7 8 7 6 6 |
R05 | 11 11 9 10 8 8 9 |
R07 | 8 8 6 9 9 7 7 |
R08 | 8 8 8 7 9 9 10 |
R09 | 11 11 13 7 6 6 6 |
R11 | 8 7 8 6 6 7 9 |
R12 | 7 7 10 9 8 9 10 |
R13 | 9 10 9 8 10 9 10 |
R14 | 9 9 8 9 8 8 9 |
R15 | 8 8 9 8 8 9 10 |
R16 | 14 15 11 14 11 18 14 |
R17 | 12 11 12 11 13 12 11 |
R18 | 9 7 8 7 6 7 10 |
R19 | 37 36 35 33 37 32 32 |
R20 | 14 19 22 20 17 16 17 |
R21 | 12 11 12 13 13 11 12 |
R22 | 13 28 15 11 13 11 12 |
R23 | 9 11 11 12 11 10 10 |
R26 | 27 23 24 29 15 16 12 |
Table 1.2084.c GPS week : 2084 MJD: 58832.0-58838.0
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 2084 0 | 0 -15 112 -1073 -88 2695 84.1 1642 1642 | -4465 0
brd 2084 1 | 12 28 27 526 3065 2200 83.3 1551 1551 | -3972 0
brd 2084 2 | 1 -18 0 1634 373 3914 83.1 1504 1504 | -3711 0
brd 2084 3 | -54 54 64 -392 4 4789 83.8 1686 1686 | -3864 0
brd 2084 4 | -11 17 120 129 1550 4459 83.1 1692 1692 | -5485 0
brd 2084 5 | -9 89 46 -1231 -660 2508 82.2 1659 1659 | -5022 0
brd 2084 6 | -76 30 128 -88 -1082 -1882 80.3 1595 1595 | -4278 0
-------------+------------------------------------------------------------+----------------
brd 2084 mean| -19 26 71 -70 451 2668 82.8 1618 1618 | -4399 0
brd 2084 sdev| 32 38 50 979 1421 2243 1.3 71 71 | 649 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 2.2084.0 GPS week: 2084 Day: 0 MJD: 58832
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 1 -10 -17 58 .01 29 26 | 19330 -631 3101 8765
cof n/a| 0 -1 0 -46 -1 70 -.09 29 26 | 19317 -625 3100 8765
emx n/a| 1 -1 -9 30 36 19 .01 22 22 | 2084 517 3087 8863
esx n/a| 0 1 1 -26 -4 -15 .04 23 21 | -13604 -3714 3078 10697
gfz n/a| 0 0 3 -28 -11 -32 .13 33 19 | 0 -500 3095 8786
iac n/a| 0 0 2 0 -19 -19 -.08 25 22 | -2658 -411 3085 8949
mcc n/a| 7 -8 13 51 69 -17 -.57 198 198 | --- --- --- ---
Table 2.2084.1 GPS week: 2084 Day: 1 MJD: 58833
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 -5 33 68 .04 32 28 | 19799 590 2615 7518
cof n/a| 1 0 0 12 2 26 .02 36 31 | 19786 594 2611 7508
emx n/a| 0 -2 -11 22 21 16 -.06 24 24 | -7476 -20 2625 7647
esx n/a| 0 1 1 -22 -39 -61 .04 20 17 | 7175 -1594 2540 9393
gfz n/a| 0 1 1 -1 -27 -65 .05 29 14 | 0 659 2621 7555
iac n/a| -2 0 9 6 16 123 -.10 29 25 | -2637 636 2610 7637
mcc n/a| -6 2 20 38 96 543 -.30 190 190 | --- --- --- ---
Table 2.2084.2 GPS week: 2084 Day: 2 MJD: 58834
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 -4 3 27 -.00 32 26 | 20425 -73 2788 7179
cof n/a| 0 0 0 -3 -11 42 .10 33 28 | 20416 -42 2790 7184
emx n/a| 2 -1 -12 48 42 14 .02 28 29 | -9322 -159 2772 7341
esx n/a| -2 0 1 6 -26 -8 .07 20 17 | -12981 -2005 2797 9267
gfz n/a| 0 0 0 -18 -9 -6 .05 29 17 | 0 -93 2792 7187
iac n/a| 1 1 7 -7 17 -33 -.17 28 23 | -2031 -358 2793 7310
mcc n/a| 1 -1 22 -1 -111 618 -.09 194 194 | --- --- --- ---
Table 2.2084.3 GPS week: 2084 Day: 3 MJD: 58835
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 3 54 .05 26 23 | 20945 718 2962 7589
cof n/a| 0 0 -1 -7 -28 23 .02 27 23 | 20938 721 2964 7600
emx n/a| 1 -1 -10 45 86 -39 -.03 28 29 | -10236 -130 2977 7709
esx n/a| -1 0 0 3 -46 -24 .05 19 18 | -3769 961 2954 9569
gfz n/a| -3 0 0 -39 -48 -28 .05 30 16 | 0 1259 2968 7556
iac n/a| 1 2 7 17 -7 19 -.17 24 21 | -2355 -94 2956 7716
mcc n/a| 12 23 35 19 -26 260 -.22 267 267 | --- --- --- ---
Table 2.2084.4 GPS week: 2084 Day: 4 MJD: 58836
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 0 4 38 46 .00 27 24 | 21070 -1533 2877 7692
cof n/a| 0 0 0 1 29 45 .04 29 25 | 21071 -1554 2877 7696
emx n/a| 3 1 -11 2 37 -57 -.05 31 31 | -2638 -1423 2864 7887
esx n/a| 0 0 2 -20 -39 -22 .11 20 18 | -12381 -2922 2889 9466
gfz n/a| -1 2 2 -32 -34 -34 .08 31 21 | 0 -1614 2883 7526
iac n/a| -2 -1 4 30 21 27 -.18 22 18 | -2777 -664 2888 7905
mcc n/a| 20 0 5 81 247 79 -.81 199 199 | --- --- --- ---
Table 2.2084.5 GPS week: 2084 Day: 5 MJD: 58837
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 -24 13 55 -.04 30 26 | 19151 -1078 3089 8477
cof n/a| 0 -1 0 38 0 32 -.02 31 29 | 19132 -1057 3096 8482
emx n/a| 2 0 -9 70 1 -33 -.06 27 27 | -8156 -927 3099 8687
esx n/a| 1 0 0 22 -17 10 .03 18 16 | 2473 -2547 3087 10110
gfz n/a| -2 0 -1 -48 -28 37 .15 28 18 | 0 -1237 3117 8424
iac n/a| -1 1 7 -16 49 -51 -.19 21 18 | -3404 -829 3077 8715
mcc n/a| 15 0 -18 231 6 187 -.28 217 217 | --- --- --- ---
Table 2.2084.6 GPS week: 2084 Day: 6 MJD: 58838
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 0 23 35 37 -.03 30 27 | 19844 -798 2961 7269
cof n/a| 1 -1 0 -13 16 40 -.05 31 27 | 19821 -764 2960 7271
emx n/a| 2 1 -7 -16 -1 8 .00 27 27 | -2450 -1641 2953 7543
esx n/a| 1 -1 2 -14 -4 -48 .03 20 20 | -11880 -113 2954 9354
gfz n/a| -2 -1 2 -29 -11 -9 .13 27 17 | 0 -649 2946 7302
iac n/a| -1 0 5 36 -14 38 -.15 23 19 | -2818 -372 2945 7558
mcc n/a| -2 0 -18 243 -68 517 .10 281 281 | --- --- --- ---
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 3.2084.0 GPS week: 2084 Day: 0 MJD: 58832
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac mcc IGL | cod cof emx esx gfz iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 846 41 46 37 46 33 19 --- 18 | 92 102 90 51 58 53 --- 65
R02 | 1098 9 17 11 9 8 14 278 5 | 57 61 55 53 49 44 161 51
R03 | 1362 12 12 13 14 15 16 98 7 | 64 64 68 61 59 49 49 59
R05 | 1050 22 21 24 22 16 25 --- 11 | 61 67 68 59 61 43 --- 56
R07 | 919 19 16 12 8 13 25 192 8 | 75 76 77 72 76 65 184 72
R08 | 833 18 20 8 19 16 14 --- 7 | 70 77 70 79 63 61 --- 68
R09E | 4002 21 13 22 13 15 34 --- 11 | 35 39 36 45 46 50 --- 39
R11E | 1875 9 10 16 11 22 18 244 8 | 43 42 37 41 46 49 69 41
R12E | 786 12 14 15 14 16 12 --- 7 | 35 34 30 33 38 31 --- 31
R13E | 4460 14 20 21 17 17 17 --- 9 | 63 65 62 63 63 61 --- 61
R14E | 688 14 9 14 24 20 16 --- 9 | 81 79 71 89 83 82 --- 80
R15E | 658 12 14 19 10 20 13 --- 8 | 73 75 69 74 75 80 --- 73
R16E | 712 19 21 26 21 40 28 --- 14 | 47 55 47 61 70 51 --- 51
R17 | 808 30 32 18 18 26 28 --- 12 | 85 87 58 60 83 51 --- 65
R18 | 588 10 15 16 24 12 19 --- 8 | 70 76 67 78 72 62 --- 69
R19 | 1280 78 81 56 51 114 61 --- 37 | 115 115 54 81 138 46 --- 71
R20 | 707 42 39 24 16 17 32 --- 13 | 96 90 62 60 81 51 --- 66
R21 | 1019 33 31 18 17 21 24 115 11 | 88 87 64 64 83 51 97 68
R22 | 1021 37 24 16 24 24 23 --- 12 | 398 409 407 248 406 399 --- 403
R23 | 881 22 20 10 22 16 16 --- 9 | 65 65 63 87 74 79 --- 73
XR26 | ---- 26 60 --- --- --- 26 --- 26 | 38 64 --- --- --- 41 --- 35
------+----------------------------------------------+------------------------------------------
RMS | 1641 29 29 22 23 32 25 198 |T 83 87 77 72 86 71 112 76
WRMS | 1641 26 26 22 21 19 22 198 |NE 98 102 92 81 100 78 122 87
MEDI | 881 19 20 16 17 17 19 192 |MD 70 75 63 61 70 51 97 65
Table 3.2084.1 GPS week: 2084 Day: 1 MJD: 58833
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac mcc IGL | cod cof emx esx gfz iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1633 59 59 36 37 32 18 --- 19 | 62 63 50 39 29 36 --- 39
R02 | 674 9 8 11 8 8 9 246 4 | 37 32 35 40 40 32 99 36
R03 | 1479 10 15 9 14 10 26 84 7 | 41 45 46 56 51 27 54 44
R05 | 1103 27 35 26 17 16 26 --- 11 | 42 51 40 36 38 22 --- 32
R07 | 466 12 12 16 9 16 24 218 7 | 54 56 59 59 67 44 90 56
R08 | 909 17 19 15 16 10 24 --- 8 | 52 50 49 51 50 35 --- 47
R09E | 4227 23 16 13 11 19 38 --- 10 | 67 59 60 62 64 25 --- 53
R11E | 2208 9 7 19 8 14 10 227 6 | 46 45 41 44 46 47 50 44
R12E | 577 16 15 18 8 10 20 --- 7 | 41 41 48 50 53 47 --- 47
R13E | 2799 17 16 27 16 14 16 --- 9 | 63 64 59 68 67 65 --- 64
R14E | 838 15 18 18 19 18 16 --- 9 | 65 73 64 75 70 62 --- 67
R15E | 580 16 15 21 8 18 14 --- 8 | 62 64 59 67 70 65 --- 64
R16E | 775 25 24 39 19 36 22 --- 14 | 41 52 39 50 68 43 --- 43
R17 | 1232 33 29 18 16 18 26 --- 11 | 46 46 36 34 37 29 --- 34
R18 | 864 14 10 16 11 15 13 --- 7 | 42 36 35 38 32 39 --- 35
R19 | 919 87 101 47 55 94 68 --- 35 | 68 81 34 64 80 25 --- 42
R20 | 928 43 67 37 18 32 55 --- 18 | 65 84 47 45 59 28 --- 45
R21 | 982 27 27 17 11 18 36 119 11 | 49 50 32 40 49 30 58 39
XR22 | 932 53 50 40 --- 41 57 --- 27 | 495 545 558 --- 552 528 --- 536
R23 | 788 26 34 20 21 22 17 --- 11 | 53 52 49 58 63 58 --- 55
XR26 | ---- 19 46 --- --- --- 25 --- 22 | 28 43 --- --- --- 29 --- 25
------+----------------------------------------------+------------------------------------------
RMS | 1550 32 36 24 20 29 29 190 |T 72 77 72 51 79 62 70 68
WRMS | 1550 28 31 24 17 14 25 190 |NE 81 88 82 46 88 68 75 76
MEDI | 919 19 19 18 16 18 24 218 |MD 52 52 47 50 53 36 58 44
Table 3.2084.2 GPS week: 2084 Day: 2 MJD: 58834
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac mcc IGL | cod cof emx esx gfz iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 788 53 67 37 37 34 16 --- 18 | 75 90 66 52 45 53 --- 52
R02 | 597 9 10 11 9 10 12 155 5 | 46 49 50 48 45 46 44 46
R03 | 553 8 12 13 14 12 17 70 6 | 58 53 58 60 44 44 40 52
R05 | 854 25 18 20 13 15 19 --- 9 | 50 51 49 39 40 39 --- 40
R07 | 668 11 9 11 10 14 13 308 6 | 58 58 61 58 72 57 139 60
R08 | 1060 17 21 15 11 14 20 --- 7 | 65 67 62 57 57 54 --- 57
R09E | 4444 17 19 23 15 26 43 --- 13 | 64 66 64 68 70 36 --- 59
R11E | 2286 7 10 20 12 12 19 219 7 | 46 45 45 44 42 50 52 44
R12E | 962 22 21 24 10 20 18 --- 9 | 50 49 57 53 46 51 --- 49
R13E | 2051 13 12 22 12 23 18 --- 9 | 81 84 79 89 91 86 --- 84
R14E | 1223 18 14 19 16 12 12 --- 8 | 76 77 75 82 80 79 --- 78
R15E | 644 15 25 23 12 23 16 --- 9 | 72 74 69 73 69 75 --- 71
R16E | 663 15 19 25 14 25 29 --- 11 | 63 65 59 68 70 68 --- 63
R17 | 1611 31 41 17 19 25 25 --- 11 | 60 67 39 34 56 36 --- 42
R18 | 894 20 15 19 13 15 13 --- 8 | 52 51 47 56 55 56 --- 52
R19 | 1535 83 91 66 51 89 64 --- 35 | 83 84 66 64 92 46 --- 54
R20 | 969 43 30 55 23 42 51 --- 21 | 84 73 53 53 83 38 --- 58
R21 | 820 26 30 18 15 27 33 125 12 | 63 67 47 50 60 37 40 49
R22 | 1132 53 25 22 17 22 31 --- 15 | 406 380 378 510 374 388 --- 385
R23 | 731 27 29 27 24 11 11 --- 11 | 48 48 46 64 57 59 --- 54
XR26 | ---- 23 37 --- --- --- 23 --- 23 | 33 54 --- --- --- 49 --- 38
------+----------------------------------------------+------------------------------------------
RMS | 1504 32 32 28 20 29 28 194 |T 77 78 73 81 77 68 63 70
WRMS | 1504 26 28 29 17 17 23 194 |NE 84 85 78 88 83 71 65 74
MEDI | 894 20 21 20 14 20 19 155 |MD 63 66 58 57 57 51 44 54
Table 3.2084.3 GPS week: 2084 Day: 3 MJD: 58835
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac mcc IGL | cod cof emx esx gfz iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 650 37 33 43 37 26 16 --- 16 | 69 66 73 34 46 40 --- 47
R02 | 894 12 17 13 9 13 18 116 6 | 38 42 40 35 38 26 71 32
R03 | 710 9 11 17 14 18 21 70 8 | 52 58 55 60 54 41 51 51
R05 | 514 17 21 24 16 13 24 --- 9 | 47 48 49 35 44 23 --- 36
R07 | 494 15 13 26 15 23 15 506 9 | 48 47 55 41 38 43 360 42
R08 | 1805 10 16 16 11 20 12 --- 7 | 56 60 57 55 53 46 --- 52
R09E | 5041 12 16 13 9 17 19 --- 7 | 27 31 33 38 37 26 --- 30
R11E | 920 8 8 20 11 10 10 250 6 | 45 42 40 43 45 38 60 41
R12E | 684 15 14 27 13 15 13 --- 8 | 54 55 68 67 63 62 --- 61
R13E | 3067 17 14 20 15 13 18 --- 8 | 64 61 52 59 64 55 --- 57
R14E | 2083 19 20 22 15 22 9 --- 9 | 69 67 63 72 81 72 --- 70
R15E | 962 15 18 21 11 14 14 --- 7 | 59 64 61 60 64 58 --- 59
R16E | 850 18 18 30 23 29 35 --- 13 | 37 48 27 54 54 41 --- 38
R17 | 1853 33 26 19 15 11 21 --- 11 | 65 60 40 38 49 33 --- 44
R18 | 600 7 10 17 9 16 14 --- 6 | 44 46 40 44 46 38 --- 41
R19 | 1636 78 73 67 35 84 59 --- 32 | 79 76 57 28 91 18 --- 42
R20 | 815 28 46 48 24 67 29 --- 20 | 79 95 50 44 108 41 --- 59
R21 | 504 27 26 19 20 34 29 141 13 | 68 65 44 43 68 36 57 50
R22 | 1262 24 26 18 11 15 35 --- 11 | 184 186 186 122 185 180 --- 180
R23 | 480 19 24 22 33 19 8 --- 11 | 42 35 42 67 41 51 --- 49
XR26 | ---- 29 42 --- --- --- 28 --- 29 | 20 47 --- --- --- 42 --- 24
------+----------------------------------------------+------------------------------------------
RMS | 1686 26 27 28 19 30 24 267 |T 59 61 56 51 63 48 119 52
WRMS | 1686 23 23 29 18 16 21 267 |NE 63 66 60 49 66 47 134 53
MEDI | 850 17 18 20 15 17 18 141 |MD 54 58 50 44 53 41 60 47
Table 3.2084.4 GPS week: 2084 Day: 4 MJD: 58836
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac mcc IGL | cod cof emx esx gfz iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 854 40 38 42 34 22 27 --- 16 | 64 63 63 54 55 40 --- 49
R02 | 699 14 11 18 13 10 10 120 6 | 34 35 41 33 29 26 39 29
R03 | 605 13 14 18 12 13 14 134 7 | 47 41 49 48 47 44 75 45
R05 | 664 11 19 26 12 15 11 --- 7 | 44 55 52 47 50 45 --- 45
R07 | 747 18 17 21 13 24 12 239 8 | 53 52 57 46 54 43 222 48
R08 | 1004 14 12 18 20 18 15 --- 8 | 48 54 45 51 58 54 --- 49
R09E | 4874 9 13 12 10 13 15 --- 6 | 25 25 29 27 35 30 --- 28
R11E | 642 10 11 21 9 15 6 282 6 | 26 30 20 34 38 28 63 28
R12E | 1216 16 15 22 9 22 12 --- 8 | 31 36 32 38 42 30 --- 32
R13E | 2114 14 16 31 14 21 18 --- 9 | 74 77 55 77 75 69 --- 70
R14E | 2083 12 11 27 12 12 11 --- 7 | 73 71 64 73 74 78 --- 72
R15E | 2145 13 15 20 13 19 15 --- 8 | 61 62 64 66 62 65 --- 63
R16E | 1006 17 19 27 19 17 22 --- 10 | 40 47 37 57 50 45 --- 44
R17 | 1652 26 29 21 19 37 28 --- 13 | 59 61 43 41 73 29 --- 46
R18 | 1419 10 12 17 7 7 14 --- 5 | 48 50 44 50 55 43 --- 47
R19 | 1967 80 95 77 49 105 55 --- 36 | 73 89 55 43 107 22 --- 42
R20 | 682 37 32 57 16 19 30 --- 16 | 65 54 30 43 50 36 --- 42
R21 | 489 24 23 21 21 37 24 170 13 | 60 60 40 42 76 36 61 48
R22 | 1911 30 28 18 17 26 30 --- 12 | 340 340 334 282 340 343 --- 339
R23 | 797 18 18 23 30 18 12 --- 11 | 54 56 53 77 59 56 --- 60
XR26 | ---- 16 110 --- --- --- 12 --- 14 | 29 88 --- --- --- 35 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 1692 27 29 31 20 31 22 199 |T 64 68 60 61 71 57 92 59
WRMS | 1692 24 25 31 18 21 18 199 |NE 72 78 69 65 81 60 99 65
MEDI | 1004 16 17 21 13 18 15 170 |MD 53 55 45 47 55 43 63 46
Table 3.2084.5 GPS week: 2084 Day: 5 MJD: 58837
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac mcc IGL | cod cof emx esx gfz iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 626 51 52 37 36 29 22 --- 18 | 58 75 53 53 66 39 --- 48
R02 | 1537 8 12 11 10 8 8 166 4 | 34 33 36 31 42 34 76 34
R03 | 723 14 15 13 11 13 10 170 6 | 41 43 42 37 45 42 59 39
R05 | 662 17 15 17 14 16 12 --- 7 | 40 37 37 52 55 38 --- 43
R07 | 428 14 23 13 9 8 21 301 7 | 55 60 47 59 54 38 129 49
R08 | 562 19 25 15 18 18 19 --- 9 | 42 38 43 48 45 33 --- 41
R09E | 3900 9 12 12 6 16 14 --- 6 | 42 45 43 46 52 47 --- 45
R11E | 909 9 17 19 13 10 15 231 7 | 50 50 53 54 49 45 50 49
R12E | 1094 15 15 28 11 20 10 --- 8 | 36 36 31 37 42 35 --- 34
R13E | 1234 17 16 18 14 21 14 --- 8 | 75 74 81 78 78 66 --- 74
R14E | 1628 8 8 22 12 13 16 --- 7 | 80 83 82 88 84 78 --- 82
R15E | 2920 20 12 24 16 10 16 --- 8 | 89 92 85 100 100 90 --- 92
R16E | 1163 18 24 31 22 65 30 --- 18 | 49 62 48 51 100 59 --- 57
R17 | 1357 33 35 18 15 24 29 --- 12 | 49 49 37 35 44 29 --- 36
R18 | 1888 15 19 17 15 8 12 --- 7 | 44 47 39 44 42 41 --- 42
R19 | 2382 92 83 67 35 68 54 --- 31 | 76 73 38 48 57 26 --- 39
R20 | 1005 33 47 47 16 35 26 --- 16 | 51 55 34 35 50 33 --- 37
R21 | 455 28 35 19 17 20 20 189 10 | 49 56 30 42 46 35 68 39
R22 | 2387 28 37 19 15 20 21 --- 10 | 233 229 236 226 231 224 --- 232
R23 | 1247 14 18 12 24 25 13 --- 9 | 52 62 50 59 50 56 --- 52
XR26 | ---- 17 100 --- --- --- 14 --- 15 | 18 111 --- --- --- 34 --- 25
------+----------------------------------------------+------------------------------------------
RMS | 1659 30 31 27 18 28 21 217 |T 60 67 57 61 66 53 76 56
WRMS | 1659 26 29 27 16 18 18 217 |NE 60 69 55 59 63 50 83 54
MEDI | 1163 17 19 18 15 18 16 189 |MD 49 56 43 48 50 39 68 43
Table 3.2084.6 GPS week: 2084 Day: 6 MJD: 58838
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz iac mcc IGL | cod cof emx esx gfz iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 936 51 44 45 34 26 29 --- 18 | 80 85 83 64 62 49 --- 62
R02 | 1718 12 17 11 19 8 16 228 7 | 46 50 50 48 51 45 132 46
R03 | 1055 10 13 14 10 12 16 247 6 | 55 56 63 62 59 49 76 57
R05 | 783 26 21 21 13 14 14 --- 9 | 49 56 50 48 48 38 --- 44
R07 | 609 17 15 16 13 9 11 406 6 | 73 73 68 63 69 54 129 64
R08 | 517 22 16 16 28 16 16 --- 10 | 59 62 63 82 73 55 --- 66
R09E | 3159 13 12 14 6 13 13 --- 6 | 34 34 36 33 40 44 --- 36
R11E | 559 11 9 23 17 12 17 249 8 | 62 61 60 71 63 72 65 65
R12E | 1469 17 20 27 19 14 22 --- 10 | 37 39 30 39 41 37 --- 34
R13E | 2187 16 15 24 11 27 14 --- 9 | 94 94 92 94 98 90 --- 92
R14E | 889 15 10 23 14 19 12 --- 8 | 107 108 104 112 117 108 --- 109
R15E | 1994 16 18 23 19 20 14 --- 9 | 102 103 98 105 106 108 --- 103
R16E | 1533 23 29 31 15 33 33 --- 14 | 69 70 56 65 61 66 --- 60
R17 | 995 25 28 21 10 27 26 --- 11 | 81 84 53 55 81 45 --- 61
R18 | 1110 20 24 25 21 15 10 --- 9 | 59 61 54 71 60 58 --- 60
R19 | 1823 90 93 58 39 72 59 --- 32 | 110 117 43 46 120 29 --- 56
R20 | 1500 33 44 38 20 44 25 --- 16 | 88 91 50 56 91 44 --- 63
R21 | 666 32 28 19 23 23 24 232 12 | 83 80 54 52 82 44 98 61
R22 | 3024 29 22 24 17 25 23 --- 12 | 324 324 323 276 320 315 --- 321
R23 | 1717 22 25 19 25 20 14 --- 10 | 56 56 61 86 65 74 --- 68
XR26 | ---- 12 39 --- --- --- 12 --- 12 | 31 56 --- --- --- 49 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1595 30 31 27 20 27 23 281 |T 80 83 74 76 85 70 100 74
WRMS | 1595 27 27 27 20 17 19 281 |NE 85 89 78 77 90 67 108 76
MEDI | 1110 20 21 23 17 19 16 247 |MD 69 70 56 63 65 49 98 61
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