[IGSREPORT-25953] Wk 2002 IGLOS Final Orbits
acc
acc at igs.org
Thu Jun 7 06:20:30 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2002 (May 20, 2018 - May 26, 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 2.2002.
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:
igl2002[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2002 in the SP3 format.
igl20027.sum Combination Report for GPS Week 2002.
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 | 5.0 ns
1 | 1.8 ns
2 | 6.2 ns
3 | 6.7 ns
4 | 7.0 ns
5 | 6.3 ns
6 | 4.2 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | GRG | R05
3 | GRG | R05
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 1.2002, 1a.2002).
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 2.2002.0-6)
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 3.2002.0-6).
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 2002 summary. (May 20, 2018 - May 26, 2018)
Table 1.2002.a GPS week : 2002 MJD: 58258.0-58264.0
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 32 -15 23 .05 23 23 | 4876 -592 3417 10210
| 0 1 0 17 9 27 .05 | 1462 1917
cof n/a| 0 0 0 17 -6 29 .04 26 25 | 4876 -597 3419 10212
| 0 1 1 18 19 27 .04 | 1466 1924
emx n/a| -1 0 3 -2 -1 -4 -.03 23 23 | 4452 -66 3373 9678
| 0 0 2 18 28 20 .03 | 10420 1359
esx n/a| 0 0 -1 -6 0 15 .18 15 13 | 3405 -433 3396 11709
| 0 0 1 11 12 35 .03 | 9295 2247
gfz n/a| 0 1 0 8 24 17 .00 23 17 | 0 -475 3398 9931
| 1 1 1 27 25 29 .05 | 0 1754
grg n/a| 2 0 0 -70 0 -9 -.33 36 26 | 5479 -525 3402 9659
| 1 1 3 19 35 71 .01 | 1453 1710
iac n/a| 1 0 0 9 -1 -30 -.02 19 18 | 6462 -570 4197 10545
| 1 0 1 36 30 62 .04 | 1944 867
mcc n/a| -2 -2 -10 30 -30 133 -.39 136 136 | --- --- --- ---
| 8 5 13 102 95 618 .17 | --- ---
Table 1.2002.b GPS week : 2002 MJD: 58258.0-58264.0
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 | 16 15 15 18 15 14 15 |
R02 | 8 7 6 6 6 7 5 |
R03 | 7 7 6 7 6 6 8 |
R04 | 7 6 6 6 6 6 5 |
R05 | 17 17 22 15 20 19 20 |
R07 | 6 6 7 7 7 6 6 |
R08 | 9 8 8 6 6 8 8 |
R09 | 6 8 7 7 6 7 5 |
R10 | 8 8 9 8 7 8 8 |
R11 | 10 8 8 9 7 8 7 |
R13 | 7 8 9 9 8 9 9 |
R14 | 7 8 9 10 10 9 9 |
R15 | 14 16 14 14 15 15 14 |
R16 | 16 14 15 16 14 15 17 |
R17 | 7 7 7 7 6 7 7 |
R18 | 7 6 7 7 6 6 6 |
R19 | 10 11 13 11 11 10 11 |
R20 | 11 10 10 10 13 13 10 |
R21 | 8 7 7 7 8 8 10 |
R22 | 9 9 7 7 8 7 9 |
R23 | 8 9 8 10 9 10 11 |
R24 | 11 12 13 13 13 13 13 |
R26 | 0 0 0 24 24 23 12 |
Table 1.2002.c GPS week : 2002 MJD: 58258.0-58264.0
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 2002 0 | -47 -42 167 807 -314 3399 84.5 1538 1538 | 4976 0
brd 2002 1 | 82 -72 208 1695 1475 2683 82.9 1500 1500 | 1783 0
brd 2002 2 | 3 46 95 -259 1503 844 85.2 1647 1647 | 6203 0
brd 2002 3 | -39 77 116 -585 -584 499 85.5 1460 1460 | 6651 0
brd 2002 4 | -13 48 123 -596 -588 -357 84.9 1517 1517 | 6985 0
brd 2002 5 | 99 -39 96 712 851 146 83.2 1400 1400 | 6328 0
brd 2002 6 | 9 -6 90 292 -19 2638 85.4 1476 1476 | 4227 0
-------------+------------------------------------------------------------+----------------
brd 2002 mean| 13 1 128 295 331 1407 84.5 1505 1505 | 5307 0
brd 2002 sdev| 56 56 44 844 928 1469 1.0 76 76 | 1833 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 2.2002.0 GPS week: 2002 Day: 0 MJD: 58258
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 0 32 -12 -5 -.01 23 23 | 3086 1503 3234 10000
cof n/a| 0 2 1 10 -14 20 -.01 26 25 | 3074 1510 3236 10007
emx n/a| -1 0 1 2 2 -18 -.03 20 20 | -8136 1320 3251 9601
esx n/a| 0 -1 -1 8 4 8 .14 14 12 | 5182 1090 3249 12497
gfz n/a| 0 2 -2 42 34 14 -.00 24 18 | 0 897 3255 9763
grg n/a| 3 0 4 -59 36 81 -.35 33 29 | 4535 1010 3230 9442
iac n/a| 2 -2 2 -44 -7 -35 -.02 21 21 | 4327 253 3784 11889
mcc n/a| 4 -6 -19 31 -50 -67 -.45 149 149 | --- --- --- ---
Table 2.2002.1 GPS week: 2002 Day: 1 MJD: 58259
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 0 37 -3 63 .12 23 23 | 2749 -1992 3263 10196
cof n/a| 0 0 0 48 1 81 .06 23 24 | 2747 -1991 3264 10198
emx n/a| -1 0 4 -10 -31 16 .01 22 22 | 2547 -631 3270 9633
esx n/a| -1 0 0 -13 -9 32 .18 15 12 | -6494 -1124 3252 12287
gfz n/a| 0 3 1 10 13 44 -.06 24 18 | 0 -1542 3278 10228
grg n/a| 1 0 -2 -48 9 -31 -.31 28 23 | 2713 -1915 3267 9295
iac n/a| 2 -1 0 20 8 -81 -.03 18 18 | 5031 -1002 3611 9683
mcc n/a| 8 -4 -10 -46 149 -909 -.63 167 167 | --- --- --- ---
Table 2.2002.2 GPS week: 2002 Day: 2 MJD: 58260
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 0 41 -20 47 .10 22 22 | 4596 -1428 3694 9642
cof n/a| 0 0 3 21 -11 20 .11 24 25 | 4594 -1426 3688 9642
emx n/a| -1 0 1 -25 -24 0 -.00 23 23 | 16437 -1501 3445 9006
esx n/a| 0 0 -3 3 1 11 .22 16 14 | 4041 -1072 3663 7531
gfz n/a| 0 1 0 8 -18 15 .01 21 18 | 0 -764 3651 9254
grg n/a| 2 0 0 -63 14 -63 -.34 29 23 | 6331 -1005 3689 8691
iac n/a| 0 -1 0 22 21 -42 -.00 17 17 | 6177 -244 4972 10196
mcc n/a| 2 2 -19 -143 -46 413 -.43 120 120 | --- --- --- ---
Table 2.2002.3 GPS week: 2002 Day: 3 MJD: 58261
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 0 59 -27 -3 .03 24 25 | 6228 -1074 3576 9750
cof n/a| 1 1 0 14 -17 15 .06 25 27 | 6228 -1087 3583 9749
emx n/a| -2 0 7 -14 -31 0 -.04 24 22 | 1861 -520 3507 9216
esx n/a| 0 0 -2 -3 0 -30 .21 17 13 | 7754 -326 3503 12249
gfz n/a| 0 0 0 -18 17 0 .01 21 17 | 0 -280 3515 9303
grg n/a| 0 -2 -3 -65 10 -66 -.33 42 32 | 7026 -870 3493 9060
iac n/a| 1 0 0 14 28 89 .00 18 17 | 9361 -2283 4602 9360
mcc n/a| 0 -9 -20 1 15 750 -.17 99 99 | --- --- --- ---
Table 2.2002.4 GPS week: 2002 Day: 4 MJD: 58262
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 7 -15 18 .07 24 23 | 5619 781 3634 10325
cof n/a| 0 -1 0 -11 -7 -6 .05 26 26 | 5613 781 3633 10327
emx n/a| -1 -1 1 3 3 -22 -.02 23 23 | -8688 1280 3629 9776
esx n/a| -1 0 1 -21 -21 -21 .17 14 12 | 19385 1084 3620 12124
gfz n/a| -2 0 0 -31 17 -31 -.06 23 15 | 0 758 3617 10035
grg n/a| 4 1 1 -59 12 106 -.34 35 21 | 6440 900 3637 9935
iac n/a| 3 0 -1 69 -1 8 .00 20 18 | 7100 149 3909 10835
mcc n/a| -7 4 -21 145 -43 812 -.15 105 105 | --- --- --- ---
Table 2.2002.5 GPS week: 2002 Day: 5 MJD: 58263
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 0 17 -26 40 .07 25 25 | 6394 1543 3384 10806
cof n/a| 0 1 0 10 32 35 .01 26 26 | 6396 1534 3389 10809
emx n/a| -1 1 1 33 41 22 -.01 22 22 | 13382 1331 3372 10231
esx n/a| 0 0 0 -16 19 29 .14 15 13 | -8502 2059 3366 12505
gfz n/a| 0 0 -1 5 61 20 .07 23 17 | 0 1326 3368 10532
grg n/a| 2 0 3 -96 -7 -41 -.32 39 26 | 5533 1404 3374 10612
iac n/a| 0 0 -1 7 -65 -92 .00 18 16 | 8511 -270 4266 10359
mcc n/a| -16 -1 3 111 -163 280 -.43 143 143 | --- --- --- ---
Table 2.2002.6 GPS week: 2002 Day: 6 MJD: 58264
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 1 30 -4 1 -.01 24 24 | 5466 -3481 3138 10752
cof n/a| 0 1 0 27 -28 39 .02 30 26 | 5483 -3506 3146 10758
emx n/a| 0 0 6 -8 26 -32 -.09 27 28 | 13764 -1747 3143 10283
esx n/a| 0 0 -3 0 0 75 .18 15 12 | 2469 -4744 3121 12774
gfz n/a| 1 1 -1 41 43 57 .05 23 16 | 0 -3725 3108 10407
grg n/a| 1 2 -2 -99 -75 -48 -.33 42 31 | 5777 -3202 3129 10580
iac n/a| 0 -1 1 -23 6 -60 -.11 19 17 | 4733 -599 4240 11498
mcc n/a| -9 -2 10 111 -78 -343 -.48 171 171 | --- --- --- ---
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 3.2002.0 GPS week: 2002 Day: 0 MJD: 58258
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 | 1383 30 20 17 28 28 71 37 --- 15 | 40 61 47 72 77 57 53 --- 55
R02 | 845 18 22 19 8 15 29 24 122 8 | 39 44 31 34 31 35 28 58 30
R03 | 1262 13 13 16 12 11 16 24 83 7 | 53 52 52 53 48 56 40 35 49
R04 | 1585 8 13 17 13 15 22 19 --- 7 | 55 55 50 51 59 67 47 --- 52
XR05 |32853 21 38 --- --- 21 --- 28 --- 17 | 40 60 --- --- 50 --- 48 --- 38
R07 | 759 9 10 14 9 10 20 17 239 5 | 63 62 61 62 61 73 55 75 60
R08 | 782 23 19 17 18 24 15 13 --- 8 | 52 52 49 49 56 57 42 --- 48
R09 | 2356 11 13 12 6 16 18 18 --- 5 | 38 40 37 33 38 32 39 --- 34
R10 | 1881 15 16 15 14 23 18 18 --- 7 | 54 57 46 56 34 47 50 --- 48
R11 | 1588 26 36 12 10 34 37 19 155 10 | 70 75 48 55 33 59 42 49 49
R13 | 2126 9 13 15 9 16 30 19 --- 7 | 65 65 56 67 55 75 54 --- 61
R14 | 1722 26 21 11 9 23 11 11 --- 7 | 92 93 79 87 82 86 84 --- 85
R15 | 2798 50 53 20 13 39 41 24 --- 13 | 86 86 52 45 29 60 34 --- 47
R16 | 503 29 55 41 14 39 75 29 --- 16 | 79 98 55 77 59 104 70 --- 68
R17E | 1478 15 11 15 9 17 23 17 --- 6 | 51 53 51 55 55 57 55 --- 53
R18E | 1117 12 14 17 14 13 25 15 --- 7 | 37 39 39 47 40 42 44 --- 41
R19E | 2237 29 35 27 15 28 22 19 --- 10 | 49 52 51 56 61 50 53 --- 51
R20E | 954 32 31 24 15 23 30 23 --- 10 | 90 95 106 100 109 112 100 --- 101
R21E | 1420 21 21 16 8 22 25 13 90 7 | 89 91 92 92 101 94 90 41 92
R22E | 635 18 19 28 9 24 19 19 --- 8 | 25 25 30 25 31 22 23 --- 22
R23E | 854 21 17 17 15 12 24 14 --- 7 | 42 47 43 48 45 55 49 --- 44
R24E | 1431 26 27 23 18 30 37 26 --- 11 | 37 46 27 39 34 46 34 --- 30
XR26E | 4580 --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 63 --- 63
------+---------------------------------------------------+-----------------------------------------------
RMS | 1537 23 26 20 14 24 33 21 149 |T 56 61 52 57 54 61 52 51 53
WRMS | 1537 23 25 20 12 18 29 21 149 |NE 59 64 51 57 50 62 49 54 51
MEDI | 1431 21 19 17 13 22 24 19 122 |MD 52 55 50 55 50 57 49 49 49
Table 3.2002.1 GPS week: 2002 Day: 1 MJD: 58259
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 | 1211 24 31 29 31 32 44 33 --- 14 | 40 38 40 53 65 53 51 --- 44
R02 | 959 20 20 17 11 19 18 15 153 7 | 35 35 35 42 40 31 33 99 34
R03 | 793 19 18 21 13 14 13 17 101 7 | 43 42 47 38 31 39 27 56 35
R04 | 1665 15 12 16 7 15 16 15 --- 6 | 41 40 42 41 38 40 32 --- 38
XR05 | 1099 15 27 --- --- 34 >>>> 22 --- 17 | 54 60 --- --- 55 9999 33 --- 44
R07 | 854 13 11 14 10 16 21 13 263 6 | 47 48 46 44 50 51 43 129 44
R08 | 1004 12 15 20 15 14 18 25 --- 8 | 46 49 47 49 52 44 35 --- 43
R09 | 2197 18 18 19 8 18 25 17 --- 7 | 30 31 34 27 33 23 29 --- 26
R10 | 1174 14 17 13 19 23 21 16 --- 8 | 42 46 36 45 34 48 40 --- 39
R11 | 2019 29 31 14 8 27 11 15 171 8 | 58 58 49 48 34 41 37 42 43
R13 | 1699 10 14 17 9 24 36 8 --- 8 | 50 56 44 50 46 71 44 --- 48
R14 | 896 27 32 14 14 22 22 12 --- 8 | 73 76 66 71 72 76 76 --- 71
R15 | 2272 52 49 23 29 47 37 22 --- 15 | 56 51 37 43 33 34 27 --- 34
R16 | 906 19 24 45 18 26 57 21 --- 14 | 52 56 52 55 52 55 51 --- 50
R17E | 1463 18 10 16 8 21 21 9 --- 7 | 52 51 55 55 62 59 51 --- 53
R18E | 1064 11 11 19 12 13 17 13 --- 6 | 37 40 39 37 40 38 37 --- 36
R19E | 3514 33 20 27 13 26 29 15 --- 10 | 48 42 48 51 56 56 44 --- 47
R20E | 1085 27 33 21 16 28 31 18 --- 10 | 83 87 89 93 94 88 88 --- 87
R21E | 956 17 20 15 8 24 15 11 87 6 | 97 102 101 102 108 92 98 37 99
R22E | 856 20 17 22 14 24 20 21 --- 8 | 27 31 35 39 46 35 23 --- 30
R23E | 836 22 26 22 14 18 28 13 --- 8 | 48 45 51 49 50 43 44 --- 45
R24E | 765 23 18 26 21 28 39 28 --- 12 | 27 27 25 29 32 36 31 --- 18
XR26E | 4705 --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 68 --- 69
------+---------------------------------------------------+-----------------------------------------------
RMS | 1499 23 23 22 15 24 28 18 167 |T 49 50 48 50 51 50 45 72 46
WRMS | 1499 23 24 22 12 18 23 18 167 |NE 47 49 44 46 45 46 39 81 42
MEDI | 1085 19 18 19 13 23 21 15 153 |MD 47 46 46 48 46 44 40 56 44
Table 3.2002.2 GPS week: 2002 Day: 2 MJD: 58260
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 | 849 21 40 37 29 15 67 20 --- 14 | 38 64 39 33 34 75 32 --- 31
R02 | 1698 10 12 12 7 20 17 15 117 6 | 36 31 29 30 26 43 37 136 31
R03 | 752 11 11 13 12 16 15 16 88 6 | 47 48 46 44 42 47 41 62 43
R04 | 885 15 18 14 9 10 15 12 --- 5 | 48 50 46 42 43 36 39 --- 41
XR05 | 931 24 30 --- 23 32 105 29 --- 22 | 42 56 --- 56 59 9999 58 --- 47
R07 | 725 12 17 18 9 11 14 21 144 6 | 53 58 54 44 52 51 42 147 47
R08 | 1251 16 15 13 24 9 21 18 --- 8 | 46 49 44 58 40 37 35 --- 42
R09 | 2832 12 19 14 14 19 11 14 --- 6 | 31 34 26 28 37 32 27 --- 27
R10 | 2046 11 13 23 14 29 33 15 --- 9 | 40 36 36 44 24 63 41 --- 38
R11 | 1638 27 31 15 9 24 12 11 154 7 | 54 55 36 41 32 40 34 79 37
R13 | 850 10 20 18 14 19 41 18 --- 9 | 47 53 43 53 38 71 38 --- 45
R14 | 765 28 30 16 11 26 15 13 --- 8 | 67 69 53 59 47 58 56 --- 55
R15 | 1380 52 50 20 25 29 23 29 --- 14 | 66 68 44 41 36 44 35 --- 40
R16 | 1430 24 25 52 19 19 57 21 --- 14 | 58 48 52 53 59 57 62 --- 53
R17E | 1065 18 18 17 8 18 19 17 --- 7 | 44 43 38 43 49 35 39 --- 39
R18E | 1250 6 11 22 14 18 18 15 --- 7 | 37 35 40 40 37 32 35 --- 35
R19E | 4302 29 19 37 25 27 22 25 --- 12 | 36 35 45 43 51 40 49 --- 40
R20E | 791 24 24 17 16 29 29 21 --- 10 | 53 53 46 59 63 49 54 --- 51
R21E | 871 18 22 14 10 21 19 9 77 6 | 49 51 49 40 45 44 46 55 44
R22E | 1109 19 21 14 14 22 12 13 --- 7 | 26 29 28 31 37 28 26 --- 27
R23E | 1061 19 23 22 16 19 24 10 --- 8 | 48 48 47 51 52 54 46 --- 48
R24E | 2189 31 32 29 19 30 45 16 --- 12 | 33 38 34 36 43 53 33 --- 31
XR26E | 5209 --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 38 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1646 22 24 23 16 21 29 17 120 |T 45 47 41 44 43 47 41 95 40
WRMS | 1646 22 25 23 14 18 23 17 120 |NE 48 51 42 44 40 50 41 106 41
MEDI | 1109 18 20 17 14 19 19 16 117 |MD 46 48 44 43 42 44 39 79 40
Table 3.2002.3 GPS week: 2002 Day: 3 MJD: 58261
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 | 858 28 21 51 41 19 63 36 --- 18 | 49 42 27 38 40 65 45 --- 29
R02 | 1065 12 20 13 11 12 13 12 87 5 | 33 41 41 32 32 34 33 73 32
R03 | 1088 11 16 15 12 14 29 17 80 7 | 48 49 54 46 51 71 47 39 50
R04 | 478 14 20 12 11 9 19 14 --- 6 | 49 52 47 38 46 34 41 --- 41
R05 | 820 35 24 47 26 24 136 16 --- 15 | 41 39 24 47 59 9999 52 --- 43
R07 | 916 10 11 16 11 17 13 22 121 7 | 55 54 60 62 65 49 43 87 55
R08 | 1184 15 20 7 13 8 17 13 --- 5 | 50 57 55 58 56 45 48 --- 52
R09 | 3066 15 11 12 10 17 20 13 --- 6 | 22 19 18 20 22 21 27 --- 17
R10 | 1151 19 17 19 14 17 24 10 --- 7 | 44 45 39 57 44 65 46 --- 47
R11 | 1333 27 27 17 14 26 13 11 115 8 | 54 54 31 46 30 38 41 56 39
R13 | 1116 19 19 19 18 27 26 13 --- 9 | 48 44 40 51 34 35 40 --- 39
R14 | 786 26 30 20 14 27 24 16 --- 9 | 51 52 31 35 26 47 36 --- 32
R15 | 867 52 60 21 12 34 39 22 --- 13 | 72 79 39 45 32 63 30 --- 42
R16 | 1333 28 41 42 22 24 61 35 --- 15 | 59 61 30 52 47 52 51 --- 42
R17E | 767 14 11 20 6 17 16 17 --- 7 | 33 31 32 32 36 34 35 --- 32
R18E | 1174 10 15 16 11 18 21 10 --- 6 | 25 27 30 29 30 24 26 --- 26
R19E | 3417 32 19 25 23 25 30 17 --- 11 | 39 48 49 47 48 39 35 --- 37
R20E | 990 24 23 22 17 26 17 21 --- 9 | 32 32 28 30 34 24 28 --- 24
R21E | 828 13 11 23 12 18 18 12 83 7 | 38 35 36 39 46 38 40 38 37
R22E | 649 19 22 15 6 25 14 11 --- 7 | 22 27 30 28 41 30 30 --- 27
R23E | 1939 24 21 22 20 17 32 18 --- 9 | 29 39 35 38 34 54 32 --- 32
R24E | 2070 24 41 21 22 26 59 14 --- 12 | 31 50 24 40 30 56 28 --- 28
XR26E |13596 25 66 --- --- --- --- 21 --- 23 | 50 71 --- --- --- --- 33 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1460 24 25 24 17 21 42 18 99 |T 42 45 36 41 40 43 37 58 36
WRMS | 1460 25 27 22 13 17 32 17 99 |NE 48 49 38 44 41 47 41 63 40
MEDI | 1088 19 20 19 13 18 21 16 87 |MD 44 45 32 39 36 39 36 56 37
Table 3.2002.4 GPS week: 2002 Day: 4 MJD: 58262
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 | 781 18 24 57 14 16 49 29 --- 14 | 44 58 28 46 52 68 50 --- 41
R02 | 1339 12 13 17 12 14 10 12 87 6 | 41 41 45 35 34 30 35 35 35
R03 | 1624 11 14 16 12 14 16 15 88 6 | 46 47 51 59 47 56 40 17 49
R04 | 900 16 13 12 10 16 13 14 --- 6 | 48 46 46 42 35 47 40 --- 41
R05 | 757 43 56 28 27 41 99 31 --- 19 | 35 52 35 38 49 9999 30 --- 32
R07 | 903 10 8 19 9 11 15 26 126 7 | 53 53 58 53 55 58 44 62 51
R08 | 818 15 12 10 10 8 16 16 --- 5 | 55 56 57 65 57 65 53 --- 58
R09 | 2914 13 19 10 11 13 16 11 --- 5 | 33 36 30 31 41 19 34 --- 30
R10 | 908 12 16 13 15 19 17 13 --- 6 | 45 47 42 46 37 35 35 --- 39
R11 | 1690 23 31 14 6 19 11 14 124 6 | 51 59 44 44 36 35 32 55 40
R13 | 1651 9 19 21 12 21 30 19 --- 8 | 46 52 33 53 36 61 48 --- 44
R14 | 645 24 25 24 14 33 27 15 --- 10 | 66 68 58 65 62 78 59 --- 62
R15 | 3187 56 59 20 12 37 40 27 --- 14 | 71 73 35 42 31 69 31 --- 39
R16 | 1272 29 32 33 16 35 59 22 --- 14 | 67 79 68 63 60 70 53 --- 59
R17E | 1302 13 14 13 9 16 20 9 --- 5 | 44 44 42 43 49 30 40 --- 40
R18E | 708 9 16 13 9 11 18 14 --- 5 | 42 43 43 40 41 30 35 --- 37
R19E | 2015 32 28 27 9 17 33 33 --- 11 | 39 36 48 47 48 63 50 --- 44
R20E | 1150 28 23 29 23 31 33 28 --- 12 | 60 61 57 76 73 61 61 --- 62
R21E | 1233 13 8 22 14 20 16 16 94 7 | 52 55 64 52 60 61 58 38 55
R22E | 972 19 23 17 14 16 28 14 --- 7 | 35 39 41 39 42 47 28 --- 35
R23E | 1086 21 18 19 16 15 41 17 --- 9 | 50 57 52 56 54 75 47 --- 52
R24E | 2089 33 29 27 23 41 36 21 --- 13 | 26 33 24 48 66 38 27 --- 31
XR26E | 5823 25 109 --- --- --- --- 22 --- 23 | 31 93 --- --- --- --- 40 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1516 24 26 23 14 23 35 20 105 |T 46 53 45 49 48 52 42 41 44
WRMS | 1516 23 26 23 12 15 21 18 105 |NE 50 54 45 48 45 53 41 42 44
MEDI | 1233 18 19 19 12 16 20 16 94 |MD 46 52 44 46 48 58 40 38 41
Table 3.2002.5 GPS week: 2002 Day: 5 MJD: 58263
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 | 707 16 30 54 15 20 39 30 --- 13 | 42 42 36 58 56 55 53 --- 45
R02 | 983 12 16 19 15 14 15 13 140 6 | 31 38 33 37 35 40 35 57 32
R03 | 727 15 15 11 9 15 26 12 96 6 | 42 44 38 39 36 54 34 29 37
R04 | 826 10 11 14 8 10 13 17 --- 5 | 46 45 45 52 45 42 37 --- 44
R05 | 646 42 30 33 23 38 92 35 --- 18 | 29 37 25 52 47 9999 41 --- 38
R07 | 764 7 11 12 8 12 11 19 189 5 | 45 45 48 49 54 45 38 82 45
R08 | 805 16 18 10 11 16 38 16 --- 7 | 40 41 46 42 39 71 53 --- 45
R09 | 2348 14 14 18 16 15 11 11 --- 6 | 21 21 24 24 27 22 20 --- 19
R10 | 913 19 16 13 22 19 16 14 --- 8 | 39 39 32 44 33 28 28 --- 32
R11 | 1517 27 23 13 6 25 18 9 171 7 | 42 41 31 30 27 29 28 74 28
R13 | 1397 24 27 20 15 21 10 20 --- 8 | 40 41 37 50 36 40 43 --- 40
R14 | 682 28 28 18 13 31 17 10 --- 8 | 59 63 51 56 54 58 51 --- 53
R15 | 2036 53 57 20 20 34 50 24 --- 14 | 58 64 38 48 31 65 33 --- 41
R16 | 1167 21 26 29 19 35 79 22 --- 14 | 64 71 63 68 58 73 51 --- 58
R17E | 1214 16 16 12 12 17 26 18 --- 7 | 34 36 39 37 43 54 33 --- 36
R18E | 1436 8 14 17 9 15 27 11 --- 6 | 29 32 34 32 34 28 33 --- 30
R19E | 1382 35 30 26 11 22 34 11 --- 10 | 30 36 38 39 49 61 42 --- 38
R20E | 877 30 29 30 13 30 60 22 --- 13 | 75 79 84 90 96 108 83 --- 85
R21E | 961 17 19 14 14 19 22 17 94 7 | 53 59 53 57 61 61 57 28 55
R22E | 670 16 15 20 8 18 22 15 --- 7 | 38 46 48 47 54 38 41 --- 43
R23E | 1029 20 30 23 13 15 59 10 --- 10 | 38 49 44 42 41 70 43 --- 40
R24E | 3680 37 51 23 28 28 28 22 --- 12 | 33 53 26 34 36 25 19 --- 22
XR26E | 6300 25 73 --- --- --- --- 20 --- 22 | 35 105 --- --- --- --- 47 --- 52
------+---------------------------------------------------+-----------------------------------------------
RMS | 1399 25 26 22 15 23 39 18 143 |T 41 49 41 46 45 50 41 54 41
WRMS | 1399 25 26 22 13 17 26 16 143 |NE 42 45 39 46 41 47 38 60 39
MEDI | 983 19 23 18 13 19 26 17 140 |MD 40 44 38 44 41 54 41 57 40
Table 3.2002.6 GPS week: 2002 Day: 6 MJD: 58264
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 | 704 32 39 59 21 30 48 22 --- 15 | 49 55 39 66 65 66 58 --- 53
R02 | 991 7 11 14 10 12 25 8 214 5 | 46 45 50 42 46 56 45 50 44
R03 | 825 17 17 20 18 9 26 14 61 7 | 58 56 56 51 53 68 44 68 51
R04 | 985 13 13 8 5 14 14 9 --- 4 | 59 57 54 53 51 53 49 --- 52
R05 | 1195 30 33 60 26 18 104 42 --- 20 | 26 26 29 38 45 9999 57 --- 38
R07 | 590 10 13 15 8 21 18 14 235 6 | 63 65 68 61 74 62 54 110 62
R08 | 963 17 18 14 6 27 25 14 --- 7 | 57 56 60 57 57 73 56 --- 57
R09 | 2015 10 12 12 8 11 15 10 --- 4 | 33 33 34 28 34 25 33 --- 29
R10 | 856 20 22 12 11 28 19 10 --- 7 | 52 54 38 52 36 47 43 --- 44
R11 | 1116 18 16 16 11 18 20 16 186 7 | 57 58 43 49 35 50 38 116 44
R13 | 3434 21 19 22 16 21 30 9 --- 8 | 56 60 53 63 49 78 56 --- 57
R14 | 898 26 28 16 13 26 18 14 --- 8 | 74 76 59 67 57 70 63 --- 63
R15 | 2289 51 53 23 12 40 47 20 --- 14 | 88 90 47 50 36 84 41 --- 51
R16 | 1412 40 60 47 15 42 69 25 --- 16 | 86 103 65 74 64 84 70 --- 69
R17E | 1048 14 9 16 11 15 27 10 --- 6 | 43 43 48 45 49 56 39 --- 44
R18E | 1639 9 13 16 9 16 23 12 --- 6 | 37 37 42 39 38 44 38 --- 38
R19E | 1195 32 26 23 13 18 51 15 --- 10 | 46 45 59 56 58 81 62 --- 55
R20E | 909 20 16 29 18 20 34 23 --- 10 | 82 79 89 82 81 89 88 --- 82
R21E | 1388 23 22 24 19 18 35 25 86 10 | 68 66 76 65 69 72 68 108 67
R22E | 1534 17 30 17 13 20 20 26 --- 8 | 28 50 34 30 38 39 31 --- 30
R23E | 981 17 57 23 18 20 63 14 --- 10 | 46 76 44 49 46 80 48 --- 46
R24E | 2212 27 45 35 21 24 60 19 --- 13 | 35 54 22 38 32 62 27 --- 26
XR26E | 5447 13 73 --- --- --- --- 10 --- 12 | 32 69 --- --- --- --- 60 --- 62
------+---------------------------------------------------+-----------------------------------------------
RMS | 1475 24 30 27 15 23 42 19 171 |T 53 58 50 52 50 63 50 90 50
WRMS | 1475 24 26 28 12 16 31 17 171 |NE 57 59 49 53 50 62 50 86 51
MEDI | 1116 18 22 17 13 20 26 14 186 |MD 52 56 48 51 49 66 49 108 51
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