[IGSREPORT-25930] Wk 2000 IGLOS Final Orbits
acc
acc at igs.org
Mon May 28 05:03:13 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2000 (May 06, 2018 - May 12, 2018)
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 2.2000.
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:
igl2000[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2000 in the SP3 format.
igl20007.sum Combination Report for GPS Week 2000.
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 | 7.0 ns
1 | 7.9 ns
2 | 7.1 ns
3 | 6.7 ns
4 | 5.0 ns
5 | 7.7 ns
6 | 6.6 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 1.2000, 1a.2000).
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 2.2000.0-6)
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 3.2000.0-6).
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 2000 summary. (May 06, 2018 - May 12, 2018)
Table 1.2000.a GPS week : 2000 MJD: 58244.0-58250.0
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 5 44 4 16 .09 32 29 | 5675 -13 3289 10318
| 1 1 2 22 19 16 .03 | 782 1372
cof n/a| 0 0 8 22 7 13 .13 34 30 | 5671 -5 3290 10320
| 1 1 3 15 24 28 .06 | 781 1380
emx n/a| -1 0 0 -3 -22 -2 .08 23 23 | 6329 526 3302 9734
| 1 1 2 15 15 49 .03 | 8425 1026
esx n/a| 0 0 -2 1 -20 -26 .12 15 14 | -1966 86 3290 12217
| 0 0 0 13 17 33 .03 | 5202 1879
gfz n/a| 0 0 -9 18 35 13 .02 28 26 | 0 49 3288 10019
| 1 2 4 16 32 38 .05 | 0 1464
grg n/a| 1 0 9 -67 4 40 -.39 35 30 | 6872 -42 3310 9675
| 1 2 6 20 17 43 .13 | 745 1430
iac n/a| 0 0 0 6 34 6 -.10 21 21 | 8219 -465 3304 9682
| 1 1 3 37 57 70 .04 | 554 848
mcc n/a| 2 0 9 75 33 -9 -.17 192 192 | --- --- --- ---
| 8 6 6 104 142 323 .35 | --- ---
Table 1.2000.b GPS week : 2000 MJD: 58244.0-58250.0
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 | 17 19 23 15 17 14 14 |
R02 | 6 6 10 8 6 7 8 |
R03 | 10 8 9 10 10 11 10 |
R04 | 8 9 8 9 8 9 10 |
R07 | 12 13 11 10 9 7 7 |
R08 | 9 10 7 8 8 8 7 |
R09 | 9 7 7 9 6 7 7 |
R10 | 9 8 10 8 7 7 8 |
R11 | 8 9 9 8 7 7 8 |
R13 | 9 9 11 10 7 8 8 |
R14 | 10 10 13 8 10 10 8 |
R15 | 14 14 18 17 16 18 14 |
R16 | 17 16 19 17 16 19 18 |
R17 | 10 8 10 8 7 8 8 |
R18 | 8 11 10 9 7 6 6 |
R19 | 12 12 14 15 12 10 11 |
R20 | 12 12 16 14 12 13 12 |
R21 | 9 9 10 8 10 9 8 |
R22 | 8 11 15 11 7 11 9 |
R23 | 11 12 11 10 10 8 11 |
R24 | 14 14 15 14 12 13 12 |
R26 | 0 0 --- 0 0 0 0 |
Table 1.2000.c GPS week : 2000 MJD: 58244.0-58250.0
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 2000 0 | 223 -930 -673 -49580 -3815 -834 84.3 >>>>> >>>>> | 6982 0
brd 2000 1 | 771 10210 -15 3570 -8425 -34870 37.1 >>>>> >>>>> | 7892 0
brd 2000 2 |-2964 -229 164 -3563 2299 189000 75.9 >>>>> >>>>> | 7110 0
brd 2000 3 | 3787 98 362 -109 -15310 -36470 156.3 >>>>> >>>>> | 6692 0
brd 2000 4 | -178 -74 643 1263 -1278 2666 92.1 >>>>> >>>>> | 4994 0
brd 2000 5 |-5568 788 -306 -241 -1092 11970 41.1 >>>>> >>>>> | 7705 0
brd 2000 6 | 143 257 -1961 -4157 -4108 2017 85.5 >>>>> >>>>> | 6575 0
-------------+------------------------------------------------------------+----------------
brd 2000 mean| -540 1445 -255 -7545 -4532 19068 81.8 >>>>> >>>>> | 6850 0
brd 2000 sdev| 2965 3899 866 18726 5789 77327 39.5 38474 38474 | 952 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 2.2000.0 GPS week: 2000 Day: 0 MJD: 58244
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 2 11 -24 -9 .13 34 33 | 4600 -660 3107 10243
cof n/a| 0 -2 9 36 1 55 .13 36 34 | 4607 -675 3105 10242
emx n/a| -3 0 0 11 -26 -21 .02 25 25 | -3116 -638 3108 9938
esx n/a| -1 -1 -2 8 -14 -38 .12 15 12 | 1845 -2092 3107 11991
gfz n/a| -1 4 -16 41 40 15 -.06 28 27 | 0 -194 3098 9994
grg n/a| 1 3 13 -76 20 20 -.30 35 28 | 7538 -1057 3174 9749
iac n/a| 3 1 1 -10 36 70 -.14 20 20 | 8830 -1356 3106 9601
mcc n/a| -2 8 16 -109 -5 488 .35 316 316 | --- --- --- ---
Table 2.2000.1 GPS week: 2000 Day: 1 MJD: 58245
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 54 20 33 .12 36 33 | 5065 835 3194 9041
cof n/a| 1 2 13 17 -21 17 .13 41 37 | 5036 889 3198 9046
emx n/a| 0 -3 1 -27 -10 65 .10 25 25 | -2654 1131 3196 8353
esx n/a| 0 0 -2 -8 -29 -50 .11 14 15 | 2149 830 3173 11122
gfz n/a| -1 -1 -12 28 38 -21 .02 28 28 | 0 1007 3158 8638
grg n/a| 0 5 20 -45 8 86 -.56 40 35 | 6906 804 3200 7715
iac n/a| 0 0 -4 31 60 -39 -.09 21 21 | 8683 478 3176 8184
mcc n/a| -4 4 16 24 191 88 -.47 233 233 | --- --- --- ---
Table 2.2000.2 GPS week: 2000 Day: 2 MJD: 58246
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 18 16 21 .12 33 27 | 5572 2550 3180 9586
cof n/a| 0 1 7 1 50 8 .24 34 27 | 5574 2558 3172 9584
emx n/a| -1 0 2 5 -17 32 .10 20 19 | 14877 2240 3192 9087
esx n/a| 0 0 -2 -4 -13 -73 .07 17 17 | -5166 2987 3184 12063
gfz n/a| 2 0 -7 -10 77 -10 .07 33 36 | 0 2580 3189 9264
grg n/a| 1 -2 1 -50 5 63 -.58 36 31 | 7511 2555 3194 8453
mcc n/a| -8 -2 5 82 -40 -489 -.58 160 160 | --- --- --- ---
Table 2.2000.3 GPS week: 2000 Day: 3 MJD: 58247
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 0 10 58 15 -4 .06 34 31 | 6129 -36 3387 11216
cof n/a| -1 0 10 46 -14 7 .15 33 32 | 6128 -40 3391 11221
emx n/a| 0 0 0 -11 -16 37 .07 23 23 | 2511 1183 3405 10675
esx n/a| 0 0 -3 -12 -38 -40 .09 15 15 | -8823 -81 3398 12838
gfz n/a| 0 -1 -5 10 53 -16 .08 25 24 | 0 -666 3418 10977
grg n/a| 0 0 12 -91 -7 37 -.31 34 29 | 5459 153 3263 10947
iac n/a| 0 0 0 34 24 35 -.10 23 24 | 7664 -589 3390 10448
mcc n/a| 13 -10 11 115 165 -264 -.39 143 143 | --- --- --- ---
Table 2.2000.4 GPS week: 2000 Day: 4 MJD: 58248
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 7 59 16 22 .04 31 29 | 7048 -1776 3400 10690
cof n/a| 0 -1 5 15 4 23 .06 35 30 | 7043 -1762 3401 10691
emx n/a| -1 0 -2 -10 -16 -6 .09 22 22 | 3380 -368 3406 10192
esx n/a| 0 0 -1 8 4 5 .13 13 12 | 5470 -2274 3402 12265
gfz n/a| 0 1 -11 11 56 90 -.01 27 22 | 0 -2102 3394 10434
grg n/a| 0 0 9 -45 24 61 -.30 37 34 | 6338 -1846 3478 10427
iac n/a| 0 -1 1 -14 -46 -83 -.13 20 21 | 7492 -252 3396 9975
mcc n/a| 1 -4 0 39 -202 -69 -.26 140 140 | --- --- --- ---
Table 2.2000.5 GPS week: 2000 Day: 5 MJD: 58249
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 3 36 7 31 .09 29 24 | 5506 -590 3441 9998
cof n/a| 1 1 2 29 3 23 .11 32 26 | 5531 -636 3440 10000
emx n/a| -3 1 -3 15 -55 -55 .11 23 23 | 17899 151 3468 9338
esx n/a| 0 1 -1 25 -44 23 .16 16 15 | -6089 1430 3445 12066
gfz n/a| 0 0 -4 28 -18 12 .06 26 22 | 0 -517 3448 9648
grg n/a| 1 0 8 -89 -28 59 -.32 33 30 | 7255 -731 3477 9842
iac n/a| 0 0 0 -50 125 -37 -.12 20 20 | 8114 424 3442 9202
mcc n/a| 10 -7 4 164 148 -75 .19 160 160 | --- --- --- ---
Table 2.2000.6 GPS week: 2000 Day: 6 MJD: 58250
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 68 -21 22 .08 26 25 | 5807 -414 3320 11457
cof n/a| 0 1 8 10 29 -38 .07 28 26 | 5782 -374 3324 11461
emx n/a| 0 0 0 -10 -12 -66 .11 21 21 | 11406 -13 3339 10560
esx n/a| 0 0 -3 -8 -6 -11 .13 15 13 | -3154 -197 3323 13174
gfz n/a| 0 0 -7 21 3 20 -.01 26 24 | 0 239 3317 11183
grg n/a| 4 0 3 -71 5 -45 -.38 28 25 | 7103 -177 3389 10597
iac n/a| 0 0 4 47 8 93 -.03 22 22 | 8535 -1499 3319 10687
mcc n/a| 8 3 10 209 -25 252 -.02 194 194 | --- --- --- ---
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 3.2000.0 GPS week: 2000 Day: 0 MJD: 58244
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 |>>>>> 64 60 38 16 27 54 32 --- 16 | 72 76 33 50 47 60 37 --- 38
R02 |>>>>> 19 11 16 7 20 13 10 135 6 | 51 51 38 46 34 52 36 84 41
R03 |>>>>> 27 25 31 16 32 22 15 116 10 | 74 75 66 55 38 77 42 29 55
R04 |>>>>> 24 23 27 9 21 15 17 --- 8 | 67 70 64 52 41 60 41 --- 53
R07 |>>>>> 35 31 24 14 33 40 27 668 12 | 69 70 58 46 46 79 34 156 49
R08 |>>>>> 16 14 25 10 32 14 20 --- 8 | 64 65 62 52 37 65 38 --- 51
XR09 |>>>>> 23 24 14 16 23 --- 17 --- 9 | 27 27 21 38 39 --- 22 --- 28
R10 |>>>>> 14 15 19 18 31 23 15 --- 9 | 47 49 36 52 32 47 29 --- 41
R11 |>>>>> 28 30 12 8 31 15 15 85 7 | 56 56 38 41 26 33 26 75 36
R13 |>>>>> 14 23 21 9 35 28 19 --- 9 | 49 55 45 52 39 58 35 --- 45
R14 |>>>>> 35 26 14 12 32 20 23 --- 9 | 84 76 62 66 51 74 55 --- 64
R15 |>>>>> 51 50 17 21 36 45 24 --- 13 | 76 78 44 42 33 64 24 --- 42
R16 | ---- 34 51 51 18 27 72 26 --- 17 | 77 76 50 68 54 68 53 --- 59
R17E |>>>>> 38 42 18 13 26 37 14 --- 10 | 106 109 111 112 112 106 95 --- 108
R18E |>>>>> 13 13 20 10 18 31 12 --- 7 | 114 116 112 115 117 121 114 --- 114
R19E |>>>>> 56 54 23 19 22 21 19 --- 11 | 53 56 50 58 61 51 45 --- 51
R20E | ---- 29 36 21 21 21 41 27 --- 11 | 52 60 53 58 54 48 46 --- 51
R21E | ---- 31 26 16 7 25 30 21 125 9 | 46 47 43 41 48 48 46 70 42
R22E |>>>>> 37 38 16 6 22 15 12 --- 7 | 52 54 48 48 53 50 42 --- 48
R23E |>>>>> 37 41 32 20 16 17 16 --- 10 | 53 51 52 57 52 54 49 --- 51
R24E |>>>>> 25 47 29 20 35 63 22 --- 14 | 51 58 56 56 51 69 45 --- 48
XR26E | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 69 --- 68
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 34 36 25 15 28 35 20 316 |T 63 65 54 57 50 64 46 82 53
WRMS |>>>>> 33 34 25 12 27 28 20 316 |NE 62 63 47 50 39 61 36 86 46
MEDI |>>>>> 29 30 21 14 27 23 17 125 |MD 56 60 50 52 47 60 42 75 49
Table 3.2000.1 GPS week: 2000 Day: 1 MJD: 58245
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 |>>>>> 83 103 32 24 53 56 20 --- 18 | 56 80 25 45 64 40 33 --- 30
R02 |>>>>> 14 28 11 7 17 18 12 126 5 | 40 53 35 36 33 41 37 56 34
R03 |>>>>> 25 26 23 10 15 23 19 152 8 | 53 54 46 41 41 53 35 20 41
R04 |>>>>> 26 30 28 10 24 20 20 --- 9 | 49 52 49 46 31 43 40 --- 40
R07 |>>>>> 35 41 28 14 32 50 29 467 12 | 49 58 43 29 26 66 31 72 31
R08 |>>>>> 29 30 27 8 16 27 27 --- 9 | 41 47 44 34 34 36 34 --- 33
XR09 | ---- 15 16 12 9 19 --- 14 --- 6 | 19 22 14 19 23 --- 21 --- 16
R10 |>>>>> 10 16 16 15 23 27 16 --- 7 | 31 36 27 43 30 40 27 --- 32
R11 |>>>>> 23 33 13 13 36 22 15 94 8 | 32 37 25 36 21 29 20 53 26
R13 |>>>>> 13 20 26 12 30 27 16 --- 9 | 36 36 38 33 33 28 24 --- 30
R14 |>>>>> 32 52 19 12 34 23 25 --- 10 | 52 65 50 48 46 54 49 --- 45
R15 |>>>>> 55 63 20 21 34 39 23 --- 13 | 49 56 33 31 30 32 23 --- 28
R16 |>>>>> 37 32 47 10 25 68 29 --- 15 | 45 42 41 37 36 32 33 --- 33
R17E |>>>>> 35 29 19 8 22 24 13 --- 8 | 130 131 125 126 121 127 108 --- 125
R18E |>>>>> 21 12 22 11 27 43 27 --- 10 | 134 147 147 147 149 153 144 --- 142
R19E |>>>>> 55 50 23 14 21 32 19 --- 11 | 43 43 33 31 33 37 37 --- 30
R20E |>>>>> 19 21 26 17 28 50 26 --- 11 | 41 48 39 40 53 43 48 --- 39
R21E | ---- 27 29 17 8 24 38 15 67 8 | 59 55 50 46 53 49 57 62 48
R22E | ---- 41 31 19 14 26 32 26 --- 10 | 66 67 59 60 60 63 66 --- 59
R23E |>>>>> 37 44 34 19 13 35 18 --- 11 | 52 54 50 55 58 65 62 --- 52
R24E |>>>>> 30 25 31 12 23 83 16 --- 14 | 48 64 39 49 47 100 44 --- 46
XR26E | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 105 --- 105
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 36 41 25 14 28 40 21 232 |T 53 59 48 49 48 56 49 52 48
WRMS |>>>>> 33 37 25 15 28 35 21 232 |NE 42 49 36 36 34 41 31 50 32
MEDI |>>>>> 29 30 23 12 24 32 19 126 |MD 49 54 41 41 36 43 37 56 34
Table 3.2000.2 GPS week: 2000 Day: 2 MJD: 58246
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg mcc IGL | cod cof emx esx gfz grg mcc IGL
------+----------------------------------------------+------------------------------------------
R01 |>>>>> 78 61 25 33 48 53 --- 22 | 62 52 33 48 62 44 --- 30
R02 |>>>>> 19 17 12 8 43 15 134 9 | 45 47 41 38 27 39 45 35
R03 |>>>>> 20 17 15 13 27 16 156 8 | 59 58 56 43 41 52 39 49
R04 |>>>>> 18 19 9 9 25 19 --- 7 | 64 63 60 60 52 64 --- 60
R07 | ---- 23 22 13 20 25 34 254 11 | 61 58 51 35 42 71 90 48
R08 |>>>>> 9 15 8 13 12 21 --- 6 | 53 58 51 48 51 60 --- 51
XR09 | ---- 13 20 12 9 18 --- --- 7 | 29 29 27 24 31 --- --- 24
R10 | ---- 14 12 12 14 27 40 --- 10 | 42 39 32 43 31 65 --- 40
R11 |>>>>> 25 20 12 8 33 17 121 9 | 43 37 29 29 28 38 58 30
R13 | ---- 12 12 20 19 29 29 --- 11 | 40 38 39 46 34 50 --- 41
R14 |>>>>> 28 20 19 18 47 22 --- 12 | 61 54 48 63 46 64 --- 55
R15 |>>>>> 51 58 21 20 59 43 --- 18 | 61 66 38 30 21 60 --- 37
R16 |>>>>> 32 51 36 18 39 71 --- 19 | 58 75 38 42 49 65 --- 42
R17E |>>>>> 27 30 18 13 19 19 --- 9 | 82 83 85 80 80 83 --- 80
R18E |>>>>> 19 16 23 16 13 26 --- 10 | 85 85 89 82 84 79 --- 82
R19E |>>>>> 45 57 18 15 36 33 --- 13 | 59 73 62 57 69 76 --- 57
R20E |>>>>> 27 32 24 20 37 60 --- 16 | 52 61 54 58 62 68 --- 53
R21E |>>>>> 27 24 17 13 19 22 79 9 | 60 62 64 61 61 66 62 60
R22E |>>>>> 58 60 23 15 25 34 --- 15 | 125 125 120 123 116 130 --- 120
R23E | ---- 20 20 22 22 17 22 --- 10 | 48 54 50 58 55 48 --- 50
R24E | ---- 26 25 24 22 28 54 --- 15 | 35 46 42 55 52 61 --- 43
------+----------------------------------------------+------------------------------------------
RMS |>>>>> 33 34 20 17 33 36 160 |T 58 60 52 53 52 64 58 51
WRMS |>>>>> 27 27 19 17 36 31 160 |NE 52 51 41 42 39 56 58 41
MEDI |>>>>> 25 20 18 15 27 26 134 |MD 59 58 50 48 51 64 58 49
Table 3.2000.3 GPS week: 2000 Day: 3 MJD: 58247
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 |>>>>> 49 52 27 22 16 64 20 --- 14 | 51 53 28 21 34 55 18 --- 15
R02 |>>>>> 21 17 10 13 18 22 19 116 7 | 43 40 30 29 24 42 23 42 27
R03 |>>>>> 19 21 14 9 31 37 24 139 9 | 57 61 50 43 25 71 28 33 41
R04 |>>>>> 18 23 16 9 29 28 21 --- 8 | 56 57 43 43 30 65 38 --- 41
R07 |>>>>> 31 33 26 17 21 27 22 161 10 | 59 61 50 29 23 57 29 200 35
R08 |>>>>> 12 12 15 14 15 32 11 --- 7 | 61 56 58 47 44 76 53 --- 52
XR09 |>>>>> 21 21 20 12 16 --- 19 --- 8 | 14 13 19 17 26 --- 24 --- 14
R10 |>>>>> 17 18 7 14 19 27 25 --- 8 | 37 39 25 37 29 44 23 --- 29
R11 |>>>>> 25 35 13 12 24 15 11 167 7 | 44 53 29 40 31 37 30 74 33
R13 |>>>>> 14 23 18 15 24 20 32 --- 9 | 40 48 35 50 29 50 40 --- 39
R14 |>>>>> 32 33 14 11 29 15 11 --- 8 | 55 58 42 45 27 47 41 --- 40
R15 |>>>>> 68 63 33 22 45 33 26 --- 16 | 64 63 36 35 25 47 26 --- 32
R16 |>>>>> 54 51 40 13 37 68 23 --- 17 | 72 72 40 48 28 60 34 --- 40
R17E | ---- 20 25 22 9 20 20 23 --- 8 | 106 110 102 110 103 109 127 --- 106
R18E |>>>>> 18 13 25 15 16 22 17 --- 8 | 131 130 132 132 138 130 112 --- 130
R19E |>>>>> 53 49 26 9 22 56 35 --- 14 | 43 48 49 46 50 65 54 --- 44
R20E |>>>>> 29 34 28 22 32 38 41 --- 14 | 49 59 55 57 66 56 62 --- 52
R21E |>>>>> 27 22 17 10 20 25 14 127 8 | 42 44 40 44 46 45 37 74 40
R22E | ---- 51 28 20 12 18 23 18 --- 10 | 50 50 46 40 52 43 63 --- 42
R23E | ---- 22 25 28 17 12 14 26 --- 9 | 49 52 38 48 39 48 51 --- 44
R24E | ---- 29 31 34 28 30 35 26 --- 13 | 35 39 45 46 39 43 35 --- 34
XR26E | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 88 --- 86
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 34 33 23 15 25 34 23 143 |T 55 57 47 47 43 59 47 84 46
WRMS |>>>>> 31 32 23 15 24 29 24 143 |NE 50 51 37 37 28 54 31 87 33
MEDI |>>>>> 25 25 20 13 21 27 21 139 |MD 50 53 42 44 31 50 37 74 40
Table 3.2000.4 GPS week: 2000 Day: 4 MJD: 58248
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 |>>>>> 58 39 44 28 30 56 20 --- 17 | 40 36 37 36 42 33 23 --- 21
R02 |>>>>> 15 12 13 7 11 24 16 82 6 | 42 44 39 40 33 57 31 48 38
R03 |>>>>> 22 23 19 8 32 42 27 85 10 | 56 56 43 43 28 70 27 52 40
R04 |>>>>> 25 24 15 3 32 18 12 --- 7 | 58 59 55 46 43 57 34 --- 47
R07 |>>>>> 27 31 22 9 20 16 27 169 9 | 54 56 49 36 37 41 27 76 38
R08 |>>>>> 24 24 17 10 25 22 16 --- 8 | 50 51 44 38 30 48 36 --- 38
XR09 |>>>>> 17 17 15 9 15 --- 10 --- 6 | 21 24 19 22 29 --- 25 --- 21
R10 |>>>>> 22 21 9 10 26 30 12 --- 7 | 34 34 30 33 26 32 27 --- 28
R11 | ---- 21 21 13 12 19 21 12 191 6 | 43 40 32 41 39 25 31 53 34
R13 |>>>>> 15 17 15 11 23 25 16 --- 7 | 41 38 42 39 33 43 34 --- 37
R14 |>>>>> 28 31 12 9 38 30 22 --- 9 | 55 55 40 45 33 61 39 --- 43
R15 |>>>>> 55 58 24 18 36 63 33 --- 15 | 57 63 41 34 28 69 20 --- 32
R16 |>>>>> 36 76 37 13 46 77 14 --- 15 | 57 94 44 49 35 61 40 --- 42
R17E |>>>>> 23 27 13 8 22 18 12 --- 6 | 50 54 45 45 46 51 48 --- 46
R18E | ---- 13 15 19 9 18 24 12 --- 6 | 89 89 88 88 84 87 79 --- 86
R19E |>>>>> 49 58 25 12 22 34 26 --- 11 | 41 46 49 45 46 48 35 --- 41
R20E |>>>>> 35 30 27 13 33 41 30 --- 12 | 53 59 47 51 50 45 45 --- 45
R21E |>>>>> 31 31 16 14 27 38 18 140 9 | 39 41 34 36 39 41 32 124 33
R22E |>>>>> 28 33 16 6 18 13 14 --- 6 | 33 36 34 31 39 26 30 --- 30
R23E | ---- 26 35 23 19 16 31 18 --- 9 | 33 35 29 43 40 36 35 --- 33
R24E | ---- 28 31 29 20 24 40 28 --- 12 | 37 40 33 49 48 48 36 --- 36
XR26E | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 37 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 31 35 22 13 27 37 20 140 |T 46 50 41 42 39 48 35 70 38
WRMS |>>>>> 29 30 22 12 22 34 21 140 |NE 46 50 39 38 33 49 30 57 35
MEDI |>>>>> 26 30 17 10 24 30 16 140 |MD 43 46 41 41 39 48 34 53 37
Table 3.2000.5 GPS week: 2000 Day: 5 MJD: 58249
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 |>>>>> 47 60 29 31 30 29 25 --- 14 | 55 72 54 52 52 43 31 --- 44
R02 |>>>>> 15 20 11 11 16 27 17 83 7 | 50 53 43 46 39 63 30 56 42
R03 |>>>>> 18 19 20 16 12 38 37 91 11 | 55 62 51 66 56 80 35 22 54
R04 |>>>>> 26 27 23 9 23 20 23 --- 9 | 56 58 49 43 44 63 36 --- 45
R07 |>>>>> 19 15 14 7 16 22 21 242 7 | 53 51 46 47 44 47 40 60 44
R08 |>>>>> 21 22 18 15 22 19 12 --- 7 | 53 52 45 42 37 51 47 --- 44
XR09 |>>>>> 18 18 14 8 22 --- 8 --- 6 | 18 22 21 24 28 --- 25 --- 21
R10 |>>>>> 12 16 10 13 26 14 16 --- 6 | 30 36 30 40 38 30 25 --- 30
R11 |>>>>> 16 26 11 9 29 16 10 205 6 | 36 43 37 43 35 37 29 73 34
R13 | ---- 14 16 16 15 24 21 12 --- 7 | 39 41 37 39 29 36 39 --- 34
R14 |>>>>> 36 34 13 10 35 16 19 --- 9 | 45 44 30 29 24 27 31 --- 27
R15 |>>>>> 58 55 25 18 53 62 30 --- 17 | 46 47 32 25 28 56 21 --- 24
R16 |>>>>> 30 37 59 20 36 82 17 --- 19 | 55 58 39 51 33 66 44 --- 43
R17E | ---- 26 28 18 15 17 22 11 --- 8 | 55 51 48 56 51 40 57 --- 50
R18E |>>>>> 11 11 17 11 18 16 11 --- 6 | 90 92 89 93 94 91 83 --- 90
R19E | ---- 41 43 20 12 23 19 17 --- 9 | 45 45 39 43 46 48 48 --- 41
XR20E |>>>>> 26 37 27 18 24 --- 31 --- 12 | 53 59 50 55 53 --- 47 --- 48
R21E |>>>>> 30 29 27 11 20 23 16 108 9 | 33 33 28 29 29 31 29 72 27
R22E |>>>>> 30 36 20 15 29 34 23 --- 10 | 30 33 26 30 33 34 23 --- 24
R23E |>>>>> 20 26 19 19 13 21 12 --- 8 | 33 30 32 38 30 33 36 --- 31
R24E | ---- 32 31 23 25 24 40 26 --- 12 | 41 49 44 52 51 59 48 --- 42
XR26E | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 40 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 29 32 23 16 26 33 20 160 |T 46 49 41 44 41 49 38 56 39
WRMS |>>>>> 24 26 23 15 22 30 20 160 |NE 45 49 39 42 37 49 33 52 37
MEDI |>>>>> 26 27 19 15 23 22 17 108 |MD 46 49 39 43 38 47 36 60 41
Table 3.2000.6 GPS week: 2000 Day: 6 MJD: 58250
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 |>>>>> 39 43 19 34 29 31 24 --- 13 | 53 75 52 82 76 46 48 --- 57
R02 |>>>>> 25 25 15 14 12 18 15 154 7 | 59 60 52 42 38 51 42 106 44
R03 |>>>>> 15 15 17 7 20 36 31 129 9 | 77 78 72 66 54 93 44 42 66
R04 |>>>>> 24 29 23 10 14 10 38 --- 9 | 75 77 71 58 53 68 36 --- 59
R07 |>>>>> 15 17 11 11 14 14 21 297 6 | 66 66 60 57 47 69 45 151 56
R08 |>>>>> 18 21 22 8 18 8 13 --- 6 | 65 65 60 53 47 64 49 --- 55
XR09 |>>>>> 18 24 13 7 17 --- 14 --- 6 | 27 30 23 24 26 --- 25 --- 22
R10 |>>>>> 12 14 10 17 35 20 11 --- 8 | 44 46 39 53 41 45 31 --- 41
R11 |>>>>> 23 21 13 14 29 8 13 195 7 | 55 57 46 55 38 43 37 100 46
R13 |>>>>> 16 22 14 12 26 19 16 --- 7 | 59 60 51 57 49 59 44 --- 51
R14 | ---- 29 28 11 11 28 16 16 --- 8 | 64 66 49 47 31 48 40 --- 45
R15 |>>>>> 51 46 12 14 41 46 20 --- 13 | 72 76 47 40 43 76 30 --- 44
R16 |>>>>> 20 35 39 15 48 68 39 --- 17 | 76 88 46 65 39 99 58 --- 60
R17E | ---- 22 20 16 11 19 17 20 --- 7 | 44 44 45 48 54 53 42 --- 45
R18E | ---- 10 13 15 9 17 18 9 --- 5 | 98 99 96 98 102 95 95 --- 97
R19E |>>>>> 41 48 23 17 26 26 18 --- 11 | 34 39 50 52 65 60 49 --- 49
XR20E | ---- 29 42 23 13 24 --- 30 --- 11 | 44 53 49 46 52 --- 44 --- 43
R21E |>>>>> 22 28 20 12 26 20 12 148 8 | 42 45 44 47 56 35 36 77 42
R22E |>>>>> 28 31 21 7 24 15 23 --- 8 | 30 31 37 29 43 32 28 --- 30
R23E |>>>>> 24 23 35 19 17 27 15 --- 10 | 31 37 34 37 31 38 37 --- 31
R24E |>>>>> 24 30 28 19 24 36 34 --- 12 | 31 48 35 35 36 43 38 --- 28
XR26E | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 54 --- 58
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 26 28 21 15 26 28 22 194 |T 54 59 50 51 48 58 43 95 48
WRMS |>>>>> 25 26 21 13 24 25 22 194 |NE 60 64 51 53 44 63 40 99 49
MEDI |>>>>> 23 25 17 12 24 19 16 154 |MD 55 60 49 52 47 53 42 100 45
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