[IGSREPORT-24330] Wk 1887 IGLOS Final Orbits
IGS ACC
acc at igs.org
Fri Mar 25 17:36:04 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1887 (Mar 06, 2016 - Mar 12, 2016)
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 2.1887.
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:
igl1887[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1887 in the SP3 format.
igl18877.sum Combination Report for GPS Week 1887.
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
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 | -6.5 ns
1 | -8.2 ns
2 | -10.4 ns
3 | -8.7 ns
4 | -10.0 ns
5 | -9.3 ns
6 | -11.0 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
----+--------+---------------
3 | GRG | R17
6 | GRG | R24
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 1.1887, 1a.1887).
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 2.1887.0-6)
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 3.1887.0-6).
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 1887 summary. (Mar 06, 2016 - Mar 12, 2016)
Table 1.1887.a GPS week : 1887 MJD: 57453.0-57459.0
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 -7 47 -27 44 .22 39 37 | --- --- --- ---
| 1 1 1 43 23 69 .03 | --- ---
cof n/a| 0 0 -11 61 0 14 .15 43 39 | --- --- --- ---
| 2 1 3 33 38 41 .09 | --- ---
emx n/a| 1 -1 4 -11 -40 -85 .24 28 29 | -9253 68 3714 6973
| 2 1 3 16 19 36 .02 | 5964 831
esx n/a| 0 0 -2 -32 10 24 -.05 21 19 | -10118 -1603 3756 8132
| 0 1 1 12 22 39 .06 | 4103 1605
gfz n/a| 0 0 3 53 68 59 .15 22 19 | 0 -964 3647 6603
| 2 1 2 14 35 37 .08 | 0 1587
grg n/a| -2 1 7 -40 17 -10 -.39 52 38 | -446087 -1101 4446 624983
| 2 2 3 30 31 48 .05 | 11631 2008
iac n/a| 0 1 -2 -14 -25 -26 -.13 17 17 | -8339 -487 3725 6785
| 0 1 2 12 34 70 .04 | 1797 803
mcc n/a| 0 -2 -23 16 67 -115 -.44 130 130 | --- --- --- ---
| 13 6 13 142 192 736 .70 | --- ---
Table 1.1887.b GPS week : 1887 MJD: 57453.0-57459.0
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 | 13 11 14 13 12 15 15 |
R02 | 8 8 8 10 10 8 7 |
R03 | 11 10 10 10 11 9 11 |
R04 | 10 10 10 9 10 9 10 |
R05 | 16 15 13 18 14 13 16 |
R06 | 9 9 9 10 9 8 10 |
R07 | 12 10 9 11 13 12 10 |
R08 | 10 10 10 10 12 11 10 |
R09 | 6 7 8 9 8 7 9 |
R10 | 8 7 9 11 8 9 10 |
R13 | 15 9 10 9 10 10 11 |
R14 | 14 16 16 18 13 13 14 |
R15 | 11 13 13 15 13 11 11 |
R16 | --- --- --- 0 0 0 51 |
R17 | 9 10 11 11 11 13 11 |
R18 | 10 9 8 9 14 10 7 |
R19 | 8 9 9 8 9 9 7 |
R20 | 15 16 15 15 12 23 18 |
R21 | 12 8 10 11 12 8 10 |
R22 | 11 11 9 9 10 9 10 |
R23 | 8 9 9 9 8 8 9 |
R24 | 13 16 15 17 20 19 18 |
R26 | 31 59 51 61 24 68 0 |
Table 1.1887.c GPS week : 1887 MJD: 57453.0-57459.0
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 1887 0 | 0 6 -16 -1286 -154 -2563 81.8 1340 1340 | -6456 0
brd 1887 1 | -20 4 36 -1608 653 -4698 82.0 1617 1617 | -8188 0
brd 1887 2 | 37 55 -27 -664 124 -5304 83.3 1271 1271 | -10440 0
brd 1887 3 | -4 47 -31 448 1118 -4165 84.8 1228 1228 | -8731 0
brd 1887 4 | 0 0 -22 -359 -811 -4094 80.8 1638 1638 | -10039 0
brd 1887 5 | 2 -21 -64 -950 -840 -3733 82.1 1836 1836 | -9342 0
brd 1887 6 | 39 47 -3 -97 -307 -3279 84.5 1548 1548 | -11042 0
-------------+------------------------------------------------------------+----------------
brd 1887 mean| 7 19 -18 -645 -30 -3976 82.8 1496 1496 | -9176 0
brd 1887 sdev| 22 29 30 708 726 901 1.5 223 223 | 1550 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 2.1887.0 GPS week: 1887 Day: 0 MJD: 57453
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 -5 -7 3 -83 .19 40 35 | --- --- --- ---
cof n/a| 0 0 -6 4 60 -23 .17 43 38 | --- --- --- ---
emx n/a| -1 0 4 -1 -44 -152 .23 30 30 | -12915 900 3588 6874
esx n/a| -1 0 -1 -36 3 35 -.00 21 20 | -10137 -1680 3629 7578
gfz n/a| 2 -2 1 37 110 8 .22 21 15 | 0 -544 3453 6510
grg n/a| -1 0 2 -29 -4 -62 -.46 46 37 | -447950 71 3584 625414
iac n/a| 0 1 0 -2 -54 53 -.11 15 15 | -5376 -530 3618 6953
mcc n/a| -8 0 -22 42 -156 -710 -.07 107 107 | --- --- --- ---
Table 2.1887.1 GPS week: 1887 Day: 1 MJD: 57454
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 -10 105 -17 54 .21 40 37 | --- --- --- ---
cof n/a| -3 -1 -14 98 -21 25 .29 42 38 | --- --- --- ---
emx n/a| 0 -4 3 -18 -53 -74 .26 30 32 | -4784 -262 3672 6315
esx n/a| 1 -1 -2 -6 -2 11 .01 20 18 | -5518 -3105 3733 7701
gfz n/a| -2 0 6 44 31 79 .11 23 23 | 0 -955 3686 6230
grg n/a| -2 0 11 -68 -28 14 -.44 40 35 | -447870 -1257 3676 624872
iac n/a| 1 3 -3 -10 21 -17 -.09 13 13 | -6579 -328 3684 6240
mcc n/a| 9 -5 -11 57 18 -316 -.27 87 87 | --- --- --- ---
Table 2.1887.2 GPS week: 1887 Day: 2 MJD: 57455
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 -8 4 -14 -3 .20 40 39 | --- --- --- ---
cof n/a| 0 2 -16 54 20 -11 .00 45 41 | --- --- --- ---
emx n/a| 0 -3 4 -34 -66 -79 .25 21 22 | -17749 -768 3184 7113
esx n/a| 0 0 -2 -46 24 25 -.06 20 19 | -15064 -3672 3237 7691
gfz n/a| 1 1 3 46 102 20 .09 23 19 | 0 -3050 3173 6588
grg n/a| -2 5 9 7 45 38 -.39 41 40 | -451536 -2911 3208 624291
iac n/a| 0 1 -4 -1 -45 18 -.09 18 18 | -9604 -854 3209 6741
mcc n/a| -9 -8 -21 188 82 319 .07 87 87 | --- --- --- ---
Table 2.1887.3 GPS week: 1887 Day: 3 MJD: 57456
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 3 -8 39 -36 99 .28 41 40 | --- --- --- ---
cof n/a| -2 3 -11 104 -39 -45 .15 47 43 | --- --- --- ---
emx n/a| 5 -2 3 -27 -37 -68 .26 25 23 | -9752 1345 3890 5709
esx n/a| 0 -2 -3 -34 -10 -41 -.13 23 21 | -12226 897 3909 7571
gfz n/a| -3 0 6 73 50 37 .02 25 18 | 0 1180 3760 5763
grg n/a| 0 3 6 -73 55 -34 -.34 47 44 | -452215 1762 3914 623889
iac n/a| 0 3 -1 -7 9 25 -.17 18 18 | -7946 -444 3842 5801
mcc n/a| 6 -3 -18 150 109 -1218 .02 103 103 | --- --- --- ---
Table 2.1887.4 GPS week: 1887 Day: 4 MJD: 57457
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 -7 31 -25 120 .24 40 36 | --- --- --- ---
cof n/a| 1 0 -11 47 24 64 .06 43 38 | --- --- --- ---
emx n/a| 0 0 0 -13 -19 -31 .25 27 27 | -12432 -69 4032 8639
esx n/a| 0 1 -1 -27 -13 37 -.12 20 21 | -13936 -495 4064 9823
gfz n/a| 1 0 0 50 20 107 .22 21 19 | 0 461 4047 7976
grg n/a| -4 1 11 -42 -2 7 -.41 39 37 | -451630 -678 4064 623028
iac n/a| 0 0 0 -21 1 -133 -.17 20 20 | -9398 -1858 4056 8112
mcc n/a| 1 -5 -8 11 459 -119 .07 144 144 | --- --- --- ---
Table 2.1887.5 GPS week: 1887 Day: 5 MJD: 57458
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 -7 97 -30 39 .21 37 38 | --- --- --- ---
cof n/a| 1 0 -13 59 -1 55 .18 41 41 | --- --- --- ---
emx n/a| 2 -1 6 6 -10 -87 .21 34 40 | -7634 248 3647 6049
esx n/a| -1 0 -1 -40 23 15 -.01 19 19 | -4093 -736 3647 7358
gfz n/a| 1 -1 5 74 67 82 .20 23 21 | 0 -889 3621 5518
grg n/a| -5 0 8 -13 12 -78 -.35 46 36 | -451381 -343 8109 625755
iac n/a| 1 0 -4 -34 -62 -18 -.11 15 15 | -9131 842 3654 5537
mcc n/a| 22 -7 -32 -116 -25 1053 -1.46 199 199 | --- --- --- ---
Table 2.1887.6 GPS week: 1887 Day: 6 MJD: 57459
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 -8 64 -71 83 .22 37 33 | --- --- --- ---
cof n/a| -3 0 -9 59 -47 36 .17 42 35 | --- --- --- ---
emx n/a| 3 -2 9 8 -52 -105 .23 27 28 | 489 -914 3985 8114
esx n/a| 0 0 -4 -34 48 90 -.04 21 20 | -9857 -2433 4077 9207
gfz n/a| -1 0 3 49 93 83 .19 22 19 | 0 -2953 3794 7637
grg n/a| -4 2 5 -65 45 44 -.33 101 36 | -420027 -4354 4569 627635
iac n/a| 0 0 -5 -24 -47 -112 -.18 18 18 | -10341 -238 4012 8117
mcc n/a| -15 10 -48 -218 -15 184 -1.46 181 181 | --- --- --- ---
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 3.1887.0 GPS week: 1887 Day: 0 MJD: 57453
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 672 73 59 20 19 27 37 19 --- 13 | 75 72 24 45 45 19 22 --- 28
R02 | 1002 32 32 16 14 20 24 6 --- 7 | 110 112 103 100 98 86 101 --- 99
R03 | 1194 58 63 17 10 29 28 8 36 10 | 115 117 91 84 82 72 90 95 86
R04 | 836 45 52 22 15 23 32 10 --- 9 | 102 108 77 73 70 68 75 --- 73
R05 | 724 44 31 49 24 22 79 21 --- 15 | 96 92 85 86 87 74 83 --- 82
R06 | 722 16 23 29 25 12 33 12 --- 9 | 103 108 105 122 104 97 111 --- 108
R07 | 886 53 58 35 13 27 28 12 177 11 | 116 119 101 92 84 81 86 101 89
R08 | 623 51 52 20 24 14 33 11 --- 10 | 125 128 99 102 99 92 97 --- 99
R09 | 2435 18 20 18 14 9 24 8 --- 6 | 20 23 18 31 30 24 20 --- 21
R10 | 1578 21 16 22 22 16 28 9 --- 8 | 56 56 39 55 37 39 40 --- 42
R13 | 1314 33 26 27 19 17 107 13 --- 14 | 48 46 34 42 37 38 30 --- 33
R14 | 1130 28 26 46 28 22 39 31 --- 14 | 49 49 72 67 63 35 57 --- 54
R15 | 2591 45 57 16 24 33 29 11 --- 11 | 66 73 35 42 39 31 33 --- 32
XR17 | 863 36 37 17 --- 12 33 10 --- 9 | 72 72 59 --- 47 150 45 --- 49
R18 | 933 30 27 27 15 21 49 7 --- 9 | 51 50 52 43 28 27 29 --- 34
R19 | 586 30 34 23 8 19 26 8 --- 7 | 56 57 48 36 33 26 25 --- 33
R20 | 1168 41 71 46 32 22 65 23 --- 15 | 71 93 52 58 43 30 32 --- 41
R21 | 2292 36 39 21 33 22 33 19 45 11 | 60 62 50 61 45 28 34 33 43
R22 | 712 42 48 33 18 24 24 21 --- 11 | 64 70 66 53 47 31 27 --- 42
R23 | 1074 11 16 18 23 13 29 14 --- 8 | 20 22 22 32 28 15 15 --- 17
R24 | 1574 33 40 44 19 13 71 14 --- 13 | 41 43 39 38 33 46 21 --- 27
XR26 | ---- 65 205 --- --- --- --- 14 --- 31 | 58 211 --- --- --- --- 46 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1340 40 43 30 21 21 46 15 107 |T 71 81 60 63 56 52 50 76 53
WRMS | 1340 35 38 30 20 15 37 15 107 |NE 71 81 60 63 56 52 50 76 53
MEDI | 1002 36 37 22 19 21 33 12 45 |MD 64 72 52 55 45 38 34 95 42
Table 3.1887.1 GPS week: 1887 Day: 1 MJD: 57454
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 531 70 78 17 17 25 27 10 --- 11 | 58 67 24 35 26 29 25 --- 24
R02 | 1010 32 36 17 13 23 28 7 --- 7 | 93 93 86 77 79 69 79 --- 78
R03 | 906 45 53 21 14 23 41 5 60 9 | 91 93 72 69 71 62 69 83 68
R04 | 1542 52 53 19 8 32 26 8 --- 9 | 82 79 54 55 59 47 57 --- 55
R05 | 1185 43 58 43 21 32 58 23 --- 14 | 78 86 79 68 64 59 69 --- 65
R06 | 958 17 21 24 20 21 24 13 --- 8 | 81 87 84 87 80 72 80 --- 80
R07 | 649 49 45 20 17 22 30 13 126 9 | 91 91 77 70 69 67 74 65 71
R08 | 818 48 50 17 17 24 32 9 --- 9 | 93 93 80 78 71 74 72 --- 74
R09 | 1995 14 18 16 15 13 30 10 --- 6 | 17 21 18 28 25 24 15 --- 16
R10 | 1340 19 20 19 16 12 18 12 --- 6 | 39 38 32 30 27 23 27 --- 26
R13 | 2023 31 40 24 16 24 28 9 --- 8 | 40 46 35 29 30 39 28 --- 24
R14 | 2515 30 24 59 32 31 39 22 --- 15 | 46 50 51 47 57 27 42 --- 37
R15 | 4024 54 50 24 21 37 44 13 --- 12 | 55 54 27 33 33 23 23 --- 23
XR17 | 740 42 45 17 --- 18 22 13 --- 10 | 51 50 41 --- 50 195 48 --- 45
R18 | 605 26 26 20 16 20 44 11 --- 9 | 33 34 31 35 31 18 20 --- 24
R19 | 1463 42 45 24 16 16 25 12 --- 9 | 35 38 21 27 17 14 15 --- 16
R20 | 961 54 32 55 19 20 81 15 --- 16 | 51 31 56 25 21 26 18 --- 20
R21 | 2370 24 23 20 18 14 39 8 57 8 | 37 34 32 33 32 17 31 31 28
R22 | 749 35 35 23 26 16 35 17 --- 10 | 43 41 39 44 26 17 18 --- 27
R23 | 923 19 22 19 26 19 23 13 --- 8 | 18 24 20 30 23 16 10 --- 14
R24 | 1227 41 46 56 27 22 67 20 --- 15 | 38 43 48 30 32 25 16 --- 19
XR26 | ---- 134 1319 --- --- --- --- 25 --- 58 | 77 9999 --- --- --- --- 83 --- 79
------+---------------------------------------------------+-----------------------------------------------
RMS | 1616 40 42 30 20 23 40 13 87 |T 56 56 47 46 43 44 41 59 41
WRMS | 1616 37 38 32 18 23 35 13 87 |NE 56 56 47 46 43 44 41 59 41
MEDI | 1010 41 40 20 17 22 30 12 60 |MD 51 50 41 35 32 27 28 65 27
Table 3.1887.2 GPS week: 1887 Day: 2 MJD: 57455
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 604 77 86 21 22 23 36 20 --- 13 | 68 78 22 30 19 37 26 --- 19
R02 | 843 34 35 15 12 16 25 12 --- 7 | 108 112 99 92 97 86 91 --- 93
R03 | 997 49 45 16 17 18 38 13 69 10 | 106 104 79 86 77 96 83 109 83
R04 | 1433 47 48 19 17 23 29 16 --- 10 | 101 102 71 76 77 65 86 --- 76
R05 | 1224 46 45 23 23 26 54 27 --- 13 | 98 100 101 93 78 61 88 --- 85
R06 | 693 16 17 20 20 20 29 18 --- 9 | 82 83 78 86 81 78 89 --- 81
R07 | 585 44 51 13 12 23 26 13 102 8 | 87 92 73 75 74 59 69 147 71
R08 | 679 47 48 16 17 22 40 12 --- 10 | 108 110 91 93 93 106 95 --- 93
R09 | 1502 17 13 16 14 17 37 8 --- 7 | 17 20 24 35 29 40 18 --- 23
R10 | 1001 25 21 18 22 15 32 18 --- 9 | 42 43 33 41 40 23 28 --- 30
R13 | 1417 36 35 22 19 17 47 10 --- 10 | 45 47 29 35 30 44 30 --- 28
R14 | 2731 27 39 34 35 33 53 31 --- 15 | 54 72 54 65 46 31 66 --- 49
R15 | 1732 58 74 16 24 37 40 14 --- 12 | 61 76 27 33 43 21 28 --- 25
XR17 | 870 41 38 15 --- 14 26 20 --- 10 | 63 59 49 --- 52 301 48 --- 48
R18 | 515 22 29 18 12 14 19 22 --- 8 | 40 42 37 39 42 38 21 --- 33
R19 | 1775 35 34 10 18 16 37 14 --- 8 | 52 47 37 36 26 22 24 --- 29
R20 | 674 52 61 33 31 27 58 18 --- 14 | 60 71 60 42 30 33 20 --- 31
R21 | 1891 36 40 16 17 15 49 13 87 9 | 48 48 36 44 37 34 26 84 32
R22 | 608 23 31 16 17 17 43 12 --- 8 | 46 50 42 48 44 30 35 --- 39
R23 | 706 13 13 12 23 22 17 22 --- 9 | 17 20 25 35 29 26 15 --- 21
R24 | 1147 40 48 40 19 32 64 22 --- 15 | 42 48 43 31 30 22 17 --- 21
XR26 | ---- 98 391 --- --- --- --- 26 --- 51 | 111 410 --- --- --- --- 83 --- 84
------+---------------------------------------------------+-----------------------------------------------
RMS | 1270 40 45 21 20 23 41 18 87 |T 66 83 52 55 51 59 49 113 49
WRMS | 1270 39 41 22 19 19 40 18 87 |NE 66 83 52 55 51 59 49 113 49
MEDI | 997 36 39 16 18 20 37 16 87 |MD 60 71 43 42 43 38 30 109 33
Table 3.1887.3 GPS week: 1887 Day: 3 MJD: 57456
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 754 73 76 30 19 22 35 15 --- 13 | 74 82 24 43 38 26 27 --- 29
R02 | 1190 28 35 16 30 17 36 13 --- 10 | 96 95 91 102 76 64 84 --- 86
R03 | 1089 42 47 22 10 21 31 13 70 9 | 98 102 92 82 80 70 89 96 85
R04 | 986 44 48 19 9 20 24 11 --- 8 | 89 91 70 68 63 73 70 --- 68
R05 | 1341 48 55 30 24 27 114 21 --- 18 | 98 104 75 78 73 111 87 --- 79
R06 | 1485 17 21 20 22 20 37 17 --- 9 | 82 82 73 93 75 77 88 --- 81
R07 | 830 61 59 14 11 28 28 11 72 10 | 102 99 65 68 61 66 66 103 66
R08 | 678 43 52 14 14 26 35 13 --- 9 | 107 112 96 93 82 88 91 --- 90
XR09 | 1003 18 30 --- 23 10 29 12 --- 8 | 26 39 --- 41 31 42 26 --- 31
R10 | 1043 25 37 33 20 23 27 19 --- 10 | 48 58 37 44 36 34 42 --- 37
R13 | 672 41 46 10 19 21 24 11 --- 8 | 51 59 36 40 38 41 32 --- 33
R14 | 2759 37 31 52 37 24 29 39 --- 17 | 49 77 64 86 67 56 67 --- 62
R15 | 2078 58 57 21 25 51 46 16 --- 15 | 64 67 34 48 53 39 34 --- 34
XR16 | ---- 9 2238 --- --- --- --- --- --- 0 | 84 9999 --- --- --- --- --- --- 80
XR17 | 605 36 39 18 --- 16 1376 15 --- 11 | 67 70 60 --- 47 9999 54 --- 54
R18 | 516 31 27 17 19 26 31 12 --- 9 | 52 49 45 48 33 42 31 --- 37
R19 | 1367 29 32 11 13 20 27 11 --- 7 | 55 56 46 42 31 39 39 --- 38
R20 | 772 41 81 22 38 31 61 24 --- 15 | 61 99 42 56 38 31 30 --- 34
R21 | 515 41 44 21 11 22 49 13 147 10 | 56 59 45 38 35 41 30 76 35
R22 | 951 40 37 21 14 10 27 14 --- 8 | 58 57 47 36 40 22 26 --- 34
R23 | 758 9 21 15 28 16 33 13 --- 8 | 22 27 25 40 30 20 22 --- 23
R24 | 1173 24 25 41 34 25 85 30 --- 17 | 43 47 58 54 26 38 21 --- 32
XR26 | ---- 118 396 --- --- --- --- 31 --- 61 | 67 399 --- --- --- --- 74 --- 54
------+---------------------------------------------------+-----------------------------------------------
RMS | 1227 41 47 25 23 25 47 18 103 |T 67 87 56 60 50 51 51 91 52
WRMS | 1227 40 43 23 21 18 44 18 103 |NE 67 87 56 60 50 51 51 91 52
MEDI | 986 40 44 20 19 22 33 13 72 |MD 64 70 47 48 40 41 39 96 38
Table 3.1887.4 GPS week: 1887 Day: 4 MJD: 57457
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 715 66 61 20 14 20 37 18 --- 12 | 66 67 36 34 31 18 27 --- 27
R02 | 1190 25 27 20 14 21 32 22 --- 9 | 124 129 124 117 110 91 109 --- 112
R03 | 1261 40 46 24 12 27 30 15 155 10 | 115 118 98 94 96 93 97 86 95
R04 | 921 44 51 13 17 17 30 18 --- 9 | 100 100 77 82 78 69 79 --- 78
R05 | 1076 59 68 35 19 19 41 31 --- 14 | 105 108 93 92 93 102 90 --- 90
R06 | 823 17 22 23 20 9 23 24 --- 9 | 90 103 89 98 93 76 94 --- 90
R07 | 789 64 72 21 15 25 40 22 147 13 | 95 101 70 71 66 54 69 81 66
R08 | 651 51 49 15 20 25 31 21 --- 11 | 106 101 87 94 86 90 93 --- 89
R09 | 1006 28 21 25 17 13 18 11 --- 8 | 30 31 26 33 36 19 24 --- 24
R10 | 899 30 20 21 18 12 26 11 --- 8 | 50 46 37 49 45 37 37 --- 40
R13 | 664 49 54 24 15 17 31 11 --- 10 | 49 55 34 26 28 33 22 --- 22
R14 | 2617 29 42 32 25 29 34 24 --- 12 | 49 53 42 58 51 41 65 --- 49
R15 | 5082 36 37 37 23 25 37 22 --- 12 | 52 53 36 42 41 31 29 --- 30
XR16 | ---- 9 41 --- --- --- --- --- --- 0 | 48 459 --- --- --- --- --- --- 47
XR17 | 756 29 35 26 --- 21 20 13 --- 10 | 63 67 67 --- 43 405 52 --- 52
R18 | 623 24 33 35 26 24 61 17 --- 13 | 41 50 54 50 25 27 31 --- 32
R19 | 858 30 31 19 16 19 22 21 --- 9 | 46 46 39 40 38 29 22 --- 32
R20 | 927 25 21 41 17 16 52 14 --- 12 | 29 29 25 29 32 58 25 --- 25
R21 | 974 34 34 24 25 19 34 24 127 11 | 72 73 68 67 57 58 50 43 58
R22 | 997 45 51 21 12 20 30 14 --- 9 | 52 57 36 26 16 17 21 --- 22
R23 | 2568 10 15 12 20 13 37 18 --- 8 | 21 26 23 29 24 25 17 --- 18
R24 | 950 33 43 46 39 36 87 31 --- 19 | 71 76 82 74 58 40 50 --- 60
XR26 | ---- 41 351 --- --- --- --- 14 --- 24 | 66 465 --- --- --- --- 55 --- 53
------+---------------------------------------------------+-----------------------------------------------
RMS | 1637 40 43 27 20 21 39 20 144 |T 66 104 59 60 54 67 52 70 52
WRMS | 1637 36 38 27 21 19 37 20 144 |NE 66 104 59 60 54 67 52 70 52
MEDI | 927 33 41 24 17 20 32 18 147 |MD 63 67 54 50 45 41 50 81 49
Table 3.1887.5 GPS week: 1887 Day: 5 MJD: 57458
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 543 71 73 47 16 32 44 13 --- 15 | 61 64 24 31 35 24 23 --- 22
R02 | 867 23 22 12 13 16 46 10 --- 8 | 119 114 115 116 109 108 103 --- 110
R03 | 1027 43 45 20 12 21 27 11 208 9 | 115 121 118 113 104 104 106 52 109
R04 | 784 43 51 14 16 20 27 11 --- 9 | 104 114 81 85 86 90 82 --- 84
R05 | 1203 51 44 29 20 25 36 22 --- 12 | 114 113 97 91 92 104 99 --- 94
R06 | 1282 13 23 18 16 19 23 16 --- 7 | 104 106 99 99 97 93 98 --- 98
R07 | 744 58 62 25 11 29 42 11 251 12 | 112 117 89 85 73 84 80 64 83
R08 | 925 49 51 16 12 32 35 8 --- 10 | 132 133 125 114 107 117 117 --- 116
R09 | 1534 21 21 15 15 16 18 14 --- 7 | 23 26 17 31 32 31 20 --- 21
R10 | 904 16 32 19 19 21 36 14 --- 8 | 47 61 38 44 43 45 40 --- 39
R13 | 487 41 50 19 17 16 39 11 --- 9 | 42 47 32 29 28 36 27 --- 25
R14 | 1073 31 42 39 30 25 26 22 --- 12 | 40 50 38 50 50 47 51 --- 43
R15 | 6542 45 41 26 21 26 33 15 --- 11 | 50 48 30 40 35 35 28 --- 29
XR16 | 7702 8 26 --- --- --- --- --- --- 0 | 38 299 --- --- --- --- --- --- 39
XR17 | 871 30 31 30 --- 17 54 13 --- 13 | 45 41 50 --- 45 237 45 --- 41
R18 | 512 26 34 33 13 19 35 13 --- 9 | 36 36 55 35 28 34 28 --- 31
R19 | 664 23 26 24 18 25 24 13 --- 9 | 42 41 47 44 39 27 24 --- 33
R20 | 1017 29 29 78 24 19 142 22 --- 22 | 18 26 36 44 41 68 19 --- 27
R21 | 1204 20 25 15 15 22 29 12 110 8 | 60 58 58 60 57 68 58 88 57
R22 | 1841 25 31 10 21 13 42 15 --- 9 | 45 47 35 49 34 46 29 --- 36
R23 | 2114 21 24 26 11 22 24 15 --- 8 | 17 20 26 17 28 18 14 --- 12
R24 | 1338 37 42 84 39 24 54 22 --- 19 | 54 58 79 47 47 136 46 --- 47
XR26 | ---- 128 1859 --- --- --- --- 34 --- 68 | 111 9999 --- --- --- --- 58 --- 63
------+---------------------------------------------------+-----------------------------------------------
RMS | 1836 37 41 34 19 23 46 15 199 |T 66 79 61 61 57 73 54 68 54
WRMS | 1836 38 41 40 19 21 36 15 199 |NE 66 79 61 61 57 73 54 68 54
MEDI | 1017 30 34 24 16 21 35 13 208 |MD 50 58 50 47 45 68 45 64 41
Table 3.1887.6 GPS week: 1887 Day: 6 MJD: 57459
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 573 76 92 29 21 33 34 11 --- 14 | 76 84 25 24 41 21 26 --- 23
R02 | 1136 26 39 10 16 16 23 11 --- 7 | 131 135 122 124 116 104 113 --- 118
R03 | 777 48 53 11 10 26 45 13 177 11 | 133 134 114 110 104 107 110 72 109
R04 | 711 45 44 23 11 22 29 10 --- 9 | 114 115 82 86 83 88 91 --- 86
R05 | 995 50 51 39 28 32 56 22 --- 15 | 114 115 105 105 97 95 101 --- 98
R06 | 1777 17 16 22 23 19 31 21 --- 10 | 100 102 102 115 103 95 102 --- 103
R07 | 1286 53 57 19 12 19 30 15 208 10 | 144 148 121 109 104 106 105 91 109
R08 | 654 48 55 19 12 18 29 12 --- 9 | 145 148 127 122 122 125 123 --- 124
R09 | 2080 20 22 15 16 14 48 14 --- 9 | 20 24 17 31 32 46 19 --- 21
R10 | 1399 23 14 17 24 17 30 24 --- 10 | 58 54 43 57 41 31 44 --- 44
R13 | 618 39 33 23 20 20 40 16 --- 11 | 47 51 31 41 35 34 25 --- 27
R14 | 986 22 25 31 27 21 50 34 --- 14 | 63 67 59 76 64 56 79 --- 65
R15 | 4832 48 53 19 15 31 31 15 --- 11 | 67 68 33 37 37 28 30 --- 29
XR16 | 8654 54 64 --- --- --- 48 --- --- 51 | 42 325 --- --- --- 5 --- --- 23
XR17 | 1354 27 32 22 --- 15 40 13 --- 11 | 62 62 60 --- 46 166 45 --- 46
R18 | 475 20 20 19 12 18 21 8 --- 7 | 47 48 50 38 24 24 29 --- 33
R19 | 728 26 26 21 12 18 15 8 --- 7 | 53 52 53 40 26 33 33 --- 36
R20 | 851 25 50 61 24 19 77 21 --- 17 | 40 66 71 50 32 29 22 --- 33
R21 | 872 23 20 17 28 19 24 19 155 9 | 115 115 115 120 106 106 99 95 108
R22 | 1629 33 29 18 15 18 21 23 --- 9 | 63 63 59 55 48 41 27 --- 45
R23 | 738 9 13 11 30 14 15 22 --- 9 | 18 20 19 33 22 18 15 --- 14
R24 | 1587 29 42 52 43 24 422 23 --- 18 | 81 84 74 94 75 92 69 --- 76
XR26 | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 73 --- 86
------+---------------------------------------------------+-----------------------------------------------
RMS | 1548 37 42 27 21 22 101 18 181 |T 78 94 70 73 64 65 62 86 63
WRMS | 1548 33 35 28 20 19 36 18 181 |NE 78 94 70 73 64 65 62 86 63
MEDI | 986 27 33 19 16 19 31 15 177 |MD 63 68 60 57 48 46 45 91 46
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