[IGSREPORT-25520] Wk 1965 IGLOS Final Orbits
acc
acc at igs.org
Sun Sep 24 15:54:23 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1965 (Sep 03, 2017 - Sep 09, 2017)
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 2.1965.
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:
igl1965[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1965 in the SP3 format.
igl19657.sum Combination Report for GPS Week 1965.
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 | -1.4 ns
1 | 1.3 ns
2 | -2.1 ns
3 | -0.2 ns
4 | 0.5 ns
5 | -16.1 ns
6 | 0.6 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 | IAC | R09
1 | GRG | R09
1 | IAC | R09
2 | GRG | R09
3 | GRG | R09
4 | GRG | R09
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 1.1965, 1a.1965).
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 2.1965.0-6)
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 3.1965.0-6).
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 1965 summary. (Sep 03, 2017 - Sep 09, 2017)
Table 1.1965.a GPS week : 1965 MJD: 57999.0-58005.0
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 6 10 12 -60 .08 33 31 | 11222 -392 3244 10373
| 1 1 2 11 21 32 .05 | 5501 2024
cof n/a| 0 0 10 12 2 -37 .11 36 33 | 11223 -404 3245 10372
| 1 1 3 13 32 63 .05 | 5498 2041
emx n/a| -1 1 -4 26 -14 37 .08 25 25 | -2546 -863 3123 9261
| 1 1 1 12 40 51 .04 | 9138 1384
esx n/a| 0 0 -1 -3 31 -22 .17 15 15 | -1175 -728 3116 12016
| 1 1 1 16 17 36 .03 | 12606 2697
gfz n/a| 0 0 -5 6 42 18 .06 23 22 | 0 -672 3111 9719
| 1 0 3 14 21 45 .05 | 0 2100
grg n/a| 0 1 4 -77 -17 -41 -.41 33 29 | -2091 -521 3109 8934
| 1 2 4 24 21 79 .09 | 5847 2251
iac n/a| 1 0 2 38 -51 38 -.19 20 19 | -1735 -404 3693 10022
| 1 1 3 34 49 84 .04 | 5469 1450
mcc n/a| 0 1 45 37 -37 314 -.83 146 146 | --- --- --- ---
| 8 6 25 139 136 383 .16 | --- ---
Table 1.1965.b GPS week : 1965 MJD: 57999.0-58005.0
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 13 13 12 13 12 13 |
R02 | 8 9 9 8 9 8 8 |
R03 | 9 8 9 9 9 10 9 |
R04 | 9 7 7 7 8 12 12 |
R05 | 12 13 11 12 15 14 12 |
R06 | 10 9 10 7 9 9 9 |
R07 | 9 11 9 10 9 10 13 |
R08 | 8 8 9 8 9 8 9 |
R09 | 31 24 53 24 19 11 12 |
R10 | 7 8 7 8 8 7 7 |
R11 | 8 8 7 8 8 9 8 |
R13 | 7 7 10 7 8 8 8 |
R15 | 15 14 14 12 12 13 13 |
R16 | 18 16 12 12 11 14 16 |
R17 | 9 10 7 8 8 9 9 |
R18 | 9 9 9 10 8 7 7 |
R19 | 14 11 13 11 11 11 12 |
R20 | 13 11 11 13 15 16 14 |
R21 | 10 8 8 10 9 8 7 |
R22 | 8 11 11 9 9 8 8 |
R23 | 10 10 7 6 8 8 10 |
R24 | 18 15 15 16 15 11 15 |
R26 | 14 19 10 14 16 17 25 |
Table 1.1965.c GPS week : 1965 MJD: 57999.0-58005.0
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 1965 0 | -7 18 246 -418 -1752 2515 119.1 >>>>> >>>>> | -1426 0
brd 1965 1 | 11 -65 226 505 -1363 1456 102.1 >>>>> >>>>> | 1255 0
brd 1965 2 | -121 -37 286 -1198 -766 4556 116.5 >>>>> >>>>> | -2070 0
brd 1965 3 | -4 -106 299 800 -1456 -319 117.6 >>>>> >>>>> | -168 0
brd 1965 4 | 61 -57 366 698 193 -4752 116.9 >>>>> >>>>> | 512 0
brd 1965 5 | 4 -19 1371 -87 -1002 -741 130.8 >>>>> >>>>> | -16116 0
brd 1965 6 | -1 2 232 360 113 1036 99.6 >>>>> >>>>> | 595 0
-------------+------------------------------------------------------------+----------------
brd 1965 mean| -8 -38 432 94 -861 535 114.7 >>>>> >>>>> | -2488 0
brd 1965 sdev| 55 42 416 715 762 2929 10.7 5411 5411 | 6122 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 2.1965.0 GPS week: 1965 Day: 0 MJD: 57999
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 3 6 7 -8 -94 .13 37 32 | 11447 -1883 2921 11150
cof n/a| 0 1 8 -2 -36 4 .15 40 33 | 11468 -1941 2922 11147
emx n/a| 0 0 -3 28 -31 -50 .10 26 27 | 7193 -2461 2877 10087
esx n/a| 1 -2 1 -13 53 -12 .13 17 16 | -12052 -889 2872 13765
gfz n/a| 2 -1 -6 -4 53 97 .10 22 22 | 0 -2089 2883 10677
grg n/a| 0 1 5 -67 -14 -24 -.37 32 29 | -302 -2245 2873 9766
iac n/a| 1 1 1 56 -54 28 -.18 19 20 | -2567 594 3422 9996
mcc n/a| 8 2 4 159 -114 1047 -.81 109 109 | --- --- --- ---
Table 2.1965.1 GPS week: 1965 Day: 1 MJD: 58000
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 14 21 -15 .07 35 32 | 13576 2990 3578 10269
cof n/a| 0 -1 8 28 34 -11 .10 38 35 | 13565 3010 3575 10268
emx n/a| 0 2 -2 29 21 24 .08 23 23 | -12691 1217 3401 9776
esx n/a| 0 0 -1 -5 53 -34 .15 15 14 | -4385 1409 3407 12503
gfz n/a| 0 0 -10 13 42 5 -.01 25 23 | 0 2449 3407 10001
grg n/a| 0 1 9 -51 0 39 -.40 32 34 | -200 3090 3392 9333
iac n/a| 0 0 2 -12 -102 17 -.22 19 19 | 2546 459 3993 9457
mcc n/a| -7 7 19 44 -249 -37 -.76 118 118 | --- --- --- ---
Table 2.1965.2 GPS week: 1965 Day: 2 MJD: 58001
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 5 16 2 -102 .12 35 36 | 13184 -2957 3332 10721
cof n/a| 1 0 9 5 -32 -75 .15 35 37 | 13184 -2967 3339 10723
emx n/a| 0 2 -6 31 -49 10 .10 23 23 | 1715 -2755 3039 8096
esx n/a| 0 0 0 29 13 -28 .22 19 17 | -966 -2598 3046 10222
gfz n/a| 0 0 -1 0 26 -17 .13 23 22 | 0 -3597 3049 8640
grg n/a| 1 1 2 -66 -33 34 -.25 24 22 | 183 -3743 3045 7937
iac n/a| 2 0 0 17 27 44 -.14 17 17 | -1417 -3077 3902 12614
mcc n/a| -6 -12 42 26 122 230 -.75 117 117 | --- --- --- ---
Table 2.1965.3 GPS week: 1965 Day: 3 MJD: 58002
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 9 -2 2 -85 .11 33 33 | 13893 -513 3318 9301
cof n/a| -2 -3 13 21 9 -138 .15 38 37 | 13891 -519 3318 9296
emx n/a| -3 0 -3 41 -61 50 .13 25 24 | -7133 -918 3219 8599
esx n/a| 0 -2 -2 2 30 -93 .19 13 13 | 13114 942 3218 11159
gfz n/a| 0 0 -7 16 22 -28 -.02 24 25 | 0 -125 3193 8918
grg n/a| 0 5 -3 -104 -23 2 -.42 30 28 | 381 -322 3163 8243
iac n/a| 3 0 3 46 -6 136 -.13 17 17 | 1150 -427 3543 8254
mcc n/a| 13 3 65 95 63 610 -.85 141 141 | --- --- --- ---
Table 2.1965.4 GPS week: 1965 Day: 4 MJD: 58003
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| -4 0 10 31 12 -48 .04 32 31 | 14909 888 3236 10301
cof n/a| -1 -1 15 19 -13 -21 .03 36 33 | 14915 865 3241 10300
emx n/a| -3 0 -6 37 -4 93 .07 28 27 | -15481 65 3244 9463
esx n/a| 1 0 0 -4 12 19 .17 14 13 | 12667 450 3223 12026
gfz n/a| -3 0 -7 -1 86 58 .05 26 22 | 0 317 3244 9910
grg n/a| 0 2 3 -77 10 -46 -.40 47 28 | 241 664 3238 9180
iac n/a| 2 0 0 11 -93 -76 -.18 22 19 | 1946 158 3449 9347
mcc n/a| -5 6 72 -208 -138 78 -.59 189 189 | --- --- --- ---
Table 2.1965.5 GPS week: 1965 Day: 5 MJD: 58004
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| -3 -1 8 1 55 -39 .08 31 28 | -1011 -1770 3228 9628
cof n/a| -1 1 13 -5 52 52 .05 32 30 | -1004 -1798 3230 9628
emx n/a| 0 0 -2 6 51 100 .06 25 25 | 2989 -716 3069 8819
esx n/a| 0 -1 -1 -17 23 0 .17 13 12 | -21100 -5883 3048 11563
gfz n/a| 0 0 -2 30 29 26 .08 22 22 | 0 -2386 2999 9389
grg n/a| -2 1 4 -117 -52 -130 -.56 33 30 | -15338 -1678 3059 8455
iac n/a| 0 2 0 87 -92 -37 -.20 23 23 | -13424 -1570 4137 9489
mcc n/a| 1 0 48 -58 -27 61 -.95 188 188 | --- --- --- ---
Table 2.1965.6 GPS week: 1965 Day: 6 MJD: 58005
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 3 6 3 -40 -.00 30 27 | 12556 499 3101 11245
cof n/a| 2 0 5 22 2 -76 .14 35 27 | 12542 519 3096 11243
emx n/a| -1 3 -5 13 -28 31 .01 27 26 | 5586 -473 3018 9988
esx n/a| -1 1 -3 -13 35 -7 .20 17 16 | 4493 1468 3001 12875
gfz n/a| -1 -1 -3 -12 39 -11 .05 21 21 | 0 727 3003 10500
grg n/a| 0 -2 6 -56 -10 -165 -.45 31 28 | 396 587 2994 9630
iac n/a| 0 0 8 60 -37 153 -.24 22 21 | -380 1031 3410 11003
mcc n/a| -2 -1 63 205 86 212 -1.09 157 157 | --- --- --- ---
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 3.1965.0 GPS week: 1965 Day: 0 MJD: 57999
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
------+---------------------------------------------------+-----------------------------------------------
R01E |>>>>> 64 62 18 15 26 39 20 --- 12 | 75 74 45 44 45 38 38 --- 40
R02E |>>>>> 32 28 16 10 23 14 13 78 7 | 57 62 34 34 28 37 27 47 31
R03E |>>>>> 39 45 16 10 24 16 17 75 8 | 67 69 48 48 38 49 38 59 44
R04E |>>>>> 34 31 17 11 19 23 16 --- 8 | 68 66 48 48 38 48 38 --- 44
R05E |>>>>> 36 39 21 19 29 34 23 --- 11 | 58 57 43 40 33 35 44 --- 36
R06E |>>>>> 35 40 22 24 12 18 18 --- 9 | 38 45 40 66 49 44 52 --- 49
R07E |>>>>> 43 47 14 11 19 16 18 90 8 | 75 77 51 48 43 54 47 70 47
R08E |>>>>> 37 35 12 11 22 19 14 --- 8 | 61 63 35 40 34 45 39 --- 38
XR09 |>>>>> 49 66 44 --- 38 --- 201 --- 30 | 58 82 57 --- 41 --- 211 --- 40
R10 |>>>>> 24 31 20 10 14 15 10 --- 6 | 76 83 52 69 51 71 63 --- 62
R11 |>>>>> 30 37 21 13 22 16 9 182 8 | 72 74 49 61 36 49 47 116 50
R13 |>>>>> 24 16 15 14 11 16 17 --- 7 | 76 77 65 80 67 66 63 --- 69
R15 |>>>>> 69 86 32 14 35 23 32 --- 14 | 88 97 56 42 34 50 28 --- 41
R16 |>>>>> 35 48 62 28 24 55 21 --- 17 | 71 75 52 69 57 56 69 --- 60
R17 |>>>>> 25 23 18 12 26 25 13 --- 8 | 22 24 27 26 28 26 21 --- 23
R18 |>>>>> 20 17 26 18 13 28 14 --- 9 | 27 30 30 32 30 28 26 --- 27
R19 |>>>>> 39 35 28 17 26 51 24 --- 13 | 34 36 34 33 38 29 33 --- 30
R20 |>>>>> 21 28 27 25 13 50 21 --- 12 | 44 54 48 40 37 35 37 --- 37
R21 |>>>>> 42 39 30 12 27 15 11 83 10 | 22 23 21 35 35 40 29 53 29
R22 |>>>>> 36 28 17 8 16 17 18 --- 8 | 26 27 22 29 28 36 22 --- 25
R23 |>>>>> 13 18 27 27 8 33 7 --- 10 | 26 26 33 31 29 44 24 --- 27
R24 |>>>>> 33 35 41 27 28 67 38 --- 17 | 54 58 56 51 45 33 32 --- 39
XR26 | 2706 21 44 --- --- --- --- 9 --- 13 | 19 50 --- --- --- --- 26 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 37 40 26 17 22 32 19 109 |T 52 57 43 46 39 43 45 69 39
WRMS |>>>>> 32 33 27 16 22 29 20 109 |NE 47 54 43 46 39 43 48 84 38
MEDI |>>>>> 35 35 21 14 22 23 17 83 |MD 58 62 45 42 37 44 38 59 39
Table 3.1965.1 GPS week: 1965 Day: 1 MJD: 58000
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
------+---------------------------------------------------+-----------------------------------------------
R01E |>>>>> 68 68 26 12 32 25 24 --- 13 | 59 63 41 30 37 39 28 --- 29
R02E |>>>>> 38 46 19 7 21 17 24 80 9 | 39 48 32 30 32 33 27 59 27
R03E |>>>>> 35 35 18 12 21 17 13 108 8 | 48 44 41 34 31 41 34 41 34
R04E |>>>>> 29 31 11 7 25 16 8 --- 6 | 47 50 35 36 25 36 33 --- 32
R05E |>>>>> 34 41 22 14 37 47 28 --- 13 | 37 49 30 35 47 31 38 --- 30
R06E |>>>>> 29 26 20 20 15 21 12 --- 8 | 24 30 24 44 31 32 32 --- 31
R07E |>>>>> 45 44 20 16 28 23 20 99 10 | 61 59 44 40 36 42 37 79 37
R08E |>>>>> 36 35 16 9 25 18 12 --- 8 | 44 44 26 30 33 39 32 --- 29
XR09 |>>>>> 31 50 33 --- 34 4617 260 --- 23 | 26 46 53 --- 37 9999 242 --- 37
R10 |>>>>> 20 19 14 10 28 28 8 --- 7 | 53 52 40 48 37 47 43 --- 43
R11 |>>>>> 26 25 14 12 21 22 15 184 7 | 48 48 37 39 33 29 38 109 35
R13 |>>>>> 17 25 14 13 21 24 11 --- 7 | 52 56 54 59 48 51 50 --- 52
R15 |>>>>> 69 64 27 9 32 22 30 --- 13 | 62 60 38 30 21 37 22 --- 29
R16 |>>>>> 37 49 49 22 29 50 25 --- 15 | 51 66 43 54 41 44 53 --- 44
R17 |>>>>> 22 24 17 10 24 42 21 --- 10 | 20 24 17 22 19 29 18 --- 16
R18 |>>>>> 16 21 25 19 19 17 11 --- 8 | 19 22 17 20 23 19 16 --- 16
R19 |>>>>> 40 46 26 18 31 24 14 --- 10 | 27 29 24 24 28 21 25 --- 21
R20 |>>>>> 15 28 24 22 19 41 12 --- 10 | 36 27 36 38 33 26 23 --- 28
R21 |>>>>> 27 29 18 9 21 23 19 91 8 | 18 21 21 27 25 16 22 168 20
R22 |>>>>> 30 41 34 10 25 12 26 --- 10 | 17 23 22 29 25 21 26 --- 21
R23 |>>>>> 16 20 13 20 11 47 11 --- 9 | 16 21 20 24 21 47 20 --- 20
R24 |>>>>> 22 36 24 26 25 70 29 --- 15 | 40 55 38 55 50 34 37 --- 38
XR26 | 2618 26 48 --- --- --- --- 13 --- 18 | 17 46 --- --- --- --- 29 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 35 38 23 15 25 32 19 118 |T 37 42 33 35 32 34 40 91 30
WRMS |>>>>> 32 35 23 14 23 34 19 118 |NE 33 39 32 36 31 32 44 138 29
MEDI |>>>>> 29 35 20 12 25 23 15 99 |MD 39 46 35 34 32 34 32 79 29
Table 3.1965.2 GPS week: 1965 Day: 2 MJD: 58001
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
------+---------------------------------------------------+-----------------------------------------------
R01E |>>>>> 70 75 28 14 35 18 15 --- 13 | 62 64 37 31 38 29 26 --- 27
R02E |>>>>> 46 54 16 8 24 17 15 90 9 | 53 60 24 25 28 30 28 39 24
R03E |>>>>> 38 41 14 11 22 25 14 118 9 | 56 58 38 44 37 48 33 39 38
R04E |>>>>> 32 27 13 12 16 17 12 --- 7 | 67 64 44 54 45 58 41 --- 48
R05E |>>>>> 33 30 19 20 23 27 24 --- 10 | 45 40 43 43 39 53 39 --- 36
R06E |>>>>> 20 22 25 25 19 22 16 --- 9 | 33 42 27 56 45 34 45 --- 38
R07E |>>>>> 42 53 20 12 20 19 11 62 9 | 63 74 47 57 49 51 49 87 50
R08E |>>>>> 34 36 12 24 25 16 13 --- 9 | 53 54 37 46 34 35 33 --- 35
XR09 |>>>>> 87 114 80 --- 57 222 115 --- 53 | 58 67 59 --- 38 9999 129 --- 49
R10 |>>>>> 11 17 14 21 18 11 12 --- 7 | 48 55 43 61 37 41 41 --- 45
R11 |>>>>> 15 18 18 14 17 18 11 177 6 | 45 46 33 50 36 47 38 64 39
R13 |>>>>> 26 19 17 23 18 33 9 --- 9 | 66 66 59 76 67 57 59 --- 61
R15 |>>>>> 54 41 29 20 27 33 26 --- 13 | 65 58 46 29 32 61 27 --- 37
R16 |>>>>> 20 41 27 30 14 40 22 --- 12 | 66 75 51 72 60 47 58 --- 57
R17 |>>>>> 14 14 13 10 13 23 20 --- 7 | 14 19 19 24 33 24 17 --- 17
R18 |>>>>> 17 20 25 19 23 13 16 --- 8 | 19 22 22 27 26 27 18 --- 21
R19 |>>>>> 51 50 27 21 29 33 21 --- 13 | 26 28 32 30 27 35 24 --- 25
R20 |>>>>> 27 26 32 28 23 20 16 --- 11 | 25 51 27 43 38 30 21 --- 24
R21 |>>>>> 28 23 18 9 20 11 16 102 7 | 19 20 19 27 27 24 21 43 21
R22 |>>>>> 32 21 27 13 32 18 24 --- 10 | 19 24 19 21 29 23 21 --- 16
R23 |>>>>> 9 11 19 17 18 16 9 --- 7 | 21 25 28 34 31 24 19 --- 23
R24 |>>>>> 36 23 42 18 28 46 22 --- 14 | 35 37 32 29 32 25 20 --- 23
XR26 | 2330 14 34 --- --- --- --- 6 --- 9 | 17 36 --- --- --- --- 21 --- 18
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 35 35 23 19 23 24 17 116 |T 42 47 35 41 37 38 36 54 33
WRMS |>>>>> 36 37 23 17 22 22 17 116 |NE 36 41 34 40 36 35 35 53 31
MEDI |>>>>> 32 27 19 18 22 19 16 102 |MD 45 51 33 43 36 35 28 43 35
Table 3.1965.3 GPS week: 1965 Day: 3 MJD: 58002
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
------+---------------------------------------------------+-----------------------------------------------
R01E |>>>>> 55 50 27 14 37 16 13 --- 11 | 60 60 40 37 56 30 36 --- 35
R02E |>>>>> 41 46 16 11 23 12 10 127 8 | 45 50 20 31 34 18 22 47 22
R03E |>>>>> 44 44 14 11 28 21 12 115 9 | 53 51 27 32 39 22 29 44 27
R04E |>>>>> 32 40 15 10 18 16 11 --- 7 | 48 56 26 34 34 28 31 --- 30
R05E |>>>>> 34 27 13 17 27 52 24 --- 12 | 34 33 29 34 38 36 35 --- 27
R06E |>>>>> 14 17 20 17 8 13 16 --- 7 | 35 36 26 45 33 30 35 --- 34
R07E |>>>>> 45 45 25 9 26 25 12 39 9 | 59 59 40 37 39 37 36 81 35
R08E |>>>>> 34 40 19 9 17 18 14 --- 7 | 42 49 30 28 30 29 31 --- 26
XR09 |>>>>> 46 54 22 --- 45 213 47 --- 24 | 38 66 43 --- 41 457 59 --- 41
R10 |>>>>> 19 25 12 13 20 25 20 --- 8 | 65 69 58 66 51 66 50 --- 58
R11 |>>>>> 16 14 12 14 24 18 17 168 7 | 61 62 56 63 42 57 45 91 53
R13 |>>>>> 28 52 16 11 17 18 9 --- 7 | 74 97 51 66 53 55 61 --- 60
R15 |>>>>> 49 54 34 14 33 26 16 --- 12 | 75 78 57 36 26 47 39 --- 40
R16 |>>>>> 28 19 49 7 17 39 15 --- 11 | 89 84 73 66 58 65 65 --- 66
R17 |>>>>> 16 26 18 11 17 14 25 --- 7 | 31 34 27 34 33 36 25 --- 27
R18 |>>>>> 24 28 28 19 9 28 18 --- 9 | 30 33 31 27 30 29 26 --- 25
R19 |>>>>> 42 42 19 15 20 26 31 --- 11 | 33 38 37 40 43 34 36 --- 34
R20 |>>>>> 26 46 33 14 24 58 12 --- 12 | 33 36 34 39 36 57 36 --- 35
R21 |>>>>> 27 38 26 15 25 33 10 199 9 | 25 31 21 37 33 36 32 130 28
R22 |>>>>> 35 36 22 13 17 24 16 --- 9 | 29 30 24 35 34 27 26 --- 27
R23 |>>>>> 11 15 15 12 20 14 10 --- 6 | 26 28 26 38 35 34 25 --- 28
R24 |>>>>> 24 55 51 15 39 57 21 --- 15 | 50 62 52 51 49 42 40 --- 43
XR26 | 2302 19 34 --- --- --- --- 11 --- 14 | 12 43 --- --- --- --- 26 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 33 38 25 13 24 30 17 141 |T 45 51 37 41 39 57 36 78 35
WRMS |>>>>> 33 37 24 13 25 28 17 141 |NE 44 52 42 46 40 74 39 110 39
MEDI |>>>>> 28 40 19 13 20 24 15 127 |MD 42 50 31 37 36 36 35 81 34
Table 3.1965.4 GPS week: 1965 Day: 4 MJD: 58003
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
------+---------------------------------------------------+-----------------------------------------------
R01E |>>>>> 42 46 23 20 30 39 31 --- 13 | 44 48 43 47 48 44 44 --- 38
R02E |>>>>> 35 35 25 11 27 20 10 112 9 | 34 35 33 34 43 28 27 85 27
R03E |>>>>> 38 37 19 12 28 17 14 46 9 | 50 48 44 50 52 42 39 40 43
R04E |>>>>> 32 27 17 9 25 18 17 --- 8 | 59 56 40 44 42 46 33 --- 40
R05E |>>>>> 26 32 22 21 43 58 26 --- 14 | 38 45 36 37 56 55 54 --- 38
R06E |>>>>> 22 23 22 17 19 32 10 --- 9 | 34 37 27 41 26 48 28 --- 32
R07E |>>>>> 46 47 16 7 26 18 18 111 9 | 62 63 40 36 34 44 36 162 36
R08E |>>>>> 34 35 18 7 32 17 14 --- 8 | 42 45 33 30 44 34 33 --- 30
R09 |>>>>> 28 39 31 26 38 175 57 --- 18 | 39 40 40 37 42 528 71 --- 34
R10 |>>>>> 20 20 20 16 17 16 19 --- 8 | 62 68 56 75 65 70 52 --- 64
R11 |>>>>> 25 30 21 6 29 10 13 177 7 | 55 61 54 47 39 48 40 170 45
R13 |>>>>> 24 32 14 13 18 25 12 --- 7 | 79 83 63 75 64 70 56 --- 67
R15 |>>>>> 56 53 31 10 22 23 23 --- 11 | 67 71 55 45 37 51 40 --- 44
R16 |>>>>> 32 48 30 14 20 33 24 --- 10 | 84 102 71 74 60 74 58 --- 68
R17 |>>>>> 29 28 26 7 26 11 17 --- 8 | 27 32 27 32 30 24 25 --- 26
R18 |>>>>> 26 34 22 13 22 11 14 --- 7 | 36 38 29 36 33 32 27 --- 30
R19 |>>>>> 39 39 30 18 14 29 24 --- 11 | 36 36 36 39 43 39 33 --- 35
R20 |>>>>> 43 56 50 10 30 53 20 --- 14 | 45 50 51 43 46 30 29 --- 36
R21 |>>>>> 20 16 17 7 24 26 26 349 8 | 27 29 27 32 32 39 31 274 29
R22 |>>>>> 30 37 14 7 24 24 26 --- 9 | 29 32 26 34 44 44 27 --- 31
R23 |>>>>> 12 13 23 15 12 27 16 --- 8 | 33 34 31 41 39 43 24 --- 32
R24 |>>>>> 18 30 64 11 18 53 11 --- 14 | 39 59 54 50 43 39 33 --- 41
XR26 | 3759 23 155 --- --- --- --- 11 --- 16 | 24 175 --- --- --- --- 28 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 32 36 28 14 26 47 22 189 |T 45 55 41 44 43 66 37 146 38
WRMS |>>>>> 31 33 27 13 22 28 19 189 |NE 45 60 44 47 44 80 38 222 40
MEDI |>>>>> 29 35 22 11 24 24 17 112 |MD 39 48 40 41 43 44 33 162 36
Table 3.1965.5 GPS week: 1965 Day: 5 MJD: 58004
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
------+---------------------------------------------------+-----------------------------------------------
R01E |>>>>> 46 42 25 12 28 19 32 --- 11 | 82 80 73 85 88 74 75 --- 77
R02E |>>>>> 27 29 19 9 19 29 13 210 8 | 41 42 34 31 32 29 28 121 28
R03E |>>>>> 35 29 21 10 26 31 18 152 9 | 57 54 50 50 50 52 46 103 46
R04E |>>>>> 37 34 14 13 30 26 45 --- 12 | 70 75 71 71 76 84 67 --- 68
R05E |>>>>> 30 34 29 20 38 47 26 --- 13 | 55 62 45 59 63 41 59 --- 50
R06E |>>>>> 32 27 18 17 10 27 16 --- 8 | 43 47 43 58 45 53 42 --- 47
R07E |>>>>> 50 39 14 9 24 22 23 239 10 | 94 89 82 89 83 88 86 152 85
R08E |>>>>> 34 28 15 6 22 25 13 --- 8 | 52 42 35 33 31 38 36 --- 32
R09 |>>>>> 23 19 19 20 16 54 13 --- 11 | 26 25 27 20 31 383 36 --- 28
R10 |>>>>> 25 21 18 9 14 16 15 --- 6 | 44 44 56 49 52 50 46 --- 49
R11 |>>>>> 26 27 14 14 25 23 21 209 8 | 45 49 36 39 30 40 30 157 33
R13 |>>>>> 16 17 19 12 18 22 17 --- 7 | 51 53 55 45 48 48 39 --- 44
R15 |>>>>> 46 43 31 12 24 38 27 --- 12 | 52 51 48 43 37 36 36 --- 39
R16 |>>>>> 29 44 31 15 19 69 32 --- 14 | 72 88 56 62 66 61 54 --- 59
R17 |>>>>> 25 32 17 7 21 29 26 --- 8 | 22 29 24 20 25 30 14 --- 20
R18 |>>>>> 25 23 13 12 17 22 9 --- 7 | 23 33 33 31 27 22 17 --- 23
R19 |>>>>> 35 40 32 11 30 17 23 --- 10 | 27 33 29 24 34 26 18 --- 21
R20 |>>>>> 28 49 58 20 21 54 30 --- 15 | 33 55 66 44 35 20 23 --- 35
R21 |>>>>> 20 30 20 9 17 13 23 94 7 | 20 25 19 28 22 23 23 128 21
R22 |>>>>> 25 24 17 8 20 11 24 --- 7 | 22 30 18 24 19 23 23 --- 20
R23 |>>>>> 16 18 21 16 14 23 12 --- 7 | 35 40 35 40 43 39 31 --- 36
R24 |>>>>> 16 30 42 10 13 44 15 --- 10 | 55 76 63 51 34 44 24 --- 41
XR26 | 3502 20 466 --- --- --- --- 14 --- 16 | 16 398 --- --- --- --- 23 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 31 32 25 13 22 33 23 188 |T 45 66 45 45 44 59 38 132 40
WRMS |>>>>> 28 30 25 12 22 30 23 188 |NE 36 68 40 37 35 60 29 142 32
MEDI |>>>>> 27 30 19 12 20 25 21 209 |MD 44 49 43 43 35 40 36 128 36
Table 3.1965.6 GPS week: 1965 Day: 6 MJD: 58005
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
------+---------------------------------------------------+-----------------------------------------------
R01E |>>>>> 50 60 29 12 27 20 34 --- 13 | 123 129 117 100 90 102 84 --- 98
R02E |>>>>> 23 26 19 11 20 17 12 218 7 | 38 43 37 36 45 37 36 108 35
R03E |>>>>> 30 47 18 13 23 16 18 153 8 | 58 65 54 49 53 50 45 81 47
R04E |>>>>> 27 36 24 18 21 35 32 --- 11 | 85 93 79 78 73 90 54 --- 73
R05E |>>>>> 33 48 26 20 22 34 25 --- 11 | 48 66 37 40 55 52 58 --- 43
R06E |>>>>> 26 25 22 22 16 19 19 --- 9 | 36 42 41 48 47 40 42 --- 40
R07E |>>>>> 46 56 39 15 24 30 21 141 12 | 139 159 140 142 131 159 127 145 137
R08E |>>>>> 34 38 19 10 17 21 13 --- 8 | 69 75 60 63 60 66 64 --- 62
R09 |>>>>> 25 29 18 28 19 41 19 --- 11 | 50 49 46 35 52 392 53 --- 40
R10 |>>>>> 12 13 11 12 21 22 16 --- 7 | 92 92 85 89 76 93 81 --- 85
R11 |>>>>> 26 24 21 10 18 19 18 163 8 | 92 92 79 76 62 85 65 102 74
R13 |>>>>> 17 17 17 15 20 16 13 --- 7 | 93 98 80 88 75 86 73 --- 81
R15 |>>>>> 45 42 25 21 26 30 32 --- 13 | 106 103 82 69 56 77 56 --- 71
R16 |>>>>> 33 45 55 20 19 56 23 --- 15 | 106 112 82 99 82 90 82 --- 89
R17 |>>>>> 28 27 25 10 17 24 22 --- 9 | 37 39 40 34 32 35 34 --- 33
R18 |>>>>> 18 23 22 11 20 15 10 --- 7 | 44 48 47 45 42 44 39 --- 43
R19 |>>>>> 34 34 36 8 34 22 18 --- 11 | 45 47 53 43 51 49 44 --- 45
R20 |>>>>> 26 27 50 20 18 55 13 --- 14 | 46 59 55 56 55 55 42 --- 49
R21 |>>>>> 22 18 11 9 11 17 25 79 7 | 41 42 40 50 48 48 43 144 44
R22 |>>>>> 23 21 18 14 13 20 22 --- 8 | 40 44 38 44 41 46 40 --- 40
R23 |>>>>> 21 22 22 30 9 23 10 --- 9 | 46 50 45 56 53 50 41 --- 47
R24 |>>>>> 25 36 30 20 22 62 36 --- 14 | 59 64 72 52 49 51 42 --- 49
XR26 | 6275 27 146 --- --- --- --- 23 --- 24 | 37 153 --- --- --- --- 42 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 30 35 27 17 21 31 22 157 |T 66 76 64 63 60 81 55 116 59
WRMS |>>>>> 27 27 26 16 21 28 21 157 |NE 62 72 60 59 55 85 51 123 55
MEDI |>>>>> 26 29 22 14 20 22 19 153 |MD 50 65 54 52 53 52 45 108 47
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