[IGSREPORT-25808] Wk 1990 IGLOS Final Orbits
acc
acc at igs.org
Thu Mar 15 16:10:49 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1990 (Feb 25, 2018 - Mar 03, 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 2.1990.
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:
igl1990[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1990 in the SP3 format.
igl19907.sum Combination Report for GPS Week 1990.
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 | -7.9 ns
1 | -6.8 ns
2 | -5.3 ns
3 | -0.7 ns
4 | 1.1 ns
5 | -0.9 ns
6 | 0.8 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 1.1990, 1a.1990).
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 2.1990.0-6)
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 3.1990.0-6).
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 1990 summary. (Feb 25, 2018 - Mar 03, 2018)
Table 1.1990.a GPS week : 1990 MJD: 58174.0-58180.0
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 -4 -10 -5 40 .05 32 31 | -3306 -216 3365 9554
| 1 1 2 19 15 27 .03 | 3388 1875
cof n/a| 0 -1 -7 -23 0 21 .10 34 32 | -3312 -206 3365 9554
| 1 1 3 22 39 21 .05 | 3391 1881
emx n/a| 0 0 5 -7 -8 -41 .09 22 22 | -3435 954 3349 9081
| 1 1 1 27 6 34 .04 | 9933 933
esx n/a| 0 0 0 0 10 24 .14 17 17 | -8258 -1890 3358 11778
| 0 1 1 14 21 20 .02 | 11542 1703
gfz n/a| -1 -1 0 6 33 -5 .13 27 26 | 0 -185 3355 9531
| 1 1 2 21 25 35 .05 | 0 1903
grg n/a| 0 0 2 -51 10 4 -.36 28 25 | -2196 -1132 3364 8929
| 1 2 3 21 23 54 .03 | 3710 1918
iac n/a| 1 1 -4 54 -21 -29 -.14 23 23 | -1685 595 3360 8970
| 0 1 3 36 49 60 .05 | 3956 551
mcc n/a| 0 8 -17 104 21 9 -.47 186 186 | --- --- --- ---
| 7 3 10 87 101 516 .31 | --- ---
Table 1.1990.b GPS week : 1990 MJD: 58174.0-58180.0
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 | 12 12 11 15 16 11 12 |
R02 | 8 7 6 7 11 9 7 |
R03 | 10 9 8 9 10 11 9 |
R04 | 10 9 9 8 10 8 8 |
R05 | 13 13 13 14 14 15 13 |
R06 | 7 7 8 10 9 9 8 |
R07 | 9 10 10 9 15 13 14 |
R08 | 9 7 8 8 11 10 8 |
R09 | 8 8 7 6 8 6 7 |
R10 | 6 6 7 8 10 8 8 |
R11 | 8 10 8 6 8 8 10 |
R13 | 9 11 7 7 7 9 7 |
R14 | 9 8 9 11 9 8 10 |
R15 | 15 14 16 18 21 15 15 |
R16 | 12 13 11 13 18 17 12 |
R17 | 9 9 8 11 11 8 9 |
R18 | 8 8 10 8 9 10 11 |
R19 | 11 14 13 13 13 12 12 |
R20 | 13 15 15 10 14 16 12 |
R21 | 9 8 7 9 10 8 8 |
R22 | 9 8 8 9 9 10 10 |
R23 | 8 7 9 9 7 7 8 |
R24 | 18 19 15 17 16 20 17 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1990.c GPS week : 1990 MJD: 58174.0-58180.0
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 1990 0 | -15 25 -40 -616 102 -4146 83.1 1222 1222 | -7869 0
brd 1990 1 | -36 0 -45 505 -225 -4125 83.4 1162 1162 | -6772 0
brd 1990 2 | -93 -37 -44 91 -4 -2639 83.6 1422 1422 | -5251 0
brd 1990 3 | 2 -27 -53 259 115 -1602 83.8 1389 1389 | -678 0
brd 1990 4 | 24 68 0 -726 -2423 -2292 82.1 1453 1453 | 1083 0
brd 1990 5 | -21 26 70 -1415 -1884 -2969 82.8 1197 1197 | -913 0
brd 1990 6 | 66 53 142 -2777 -3089 -4338 82.3 1264 1264 | 766 0
-------------+------------------------------------------------------------+----------------
brd 1990 mean| -10 15 4 -668 -1058 -3158 83.0 1301 1301 | -2804 0
brd 1990 sdev| 50 39 74 1141 1366 1062 .7 117 117 | 3726 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 2.1990.0 GPS week: 1990 Day: 0 MJD: 58174
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 -6 4 8 44 .06 33 33 | -6964 -800 3616 9251
cof n/a| -2 -1 -9 -30 37 29 .08 33 33 | -6970 -786 3612 9246
emx n/a| 2 0 5 -41 -9 -44 .12 20 20 | 5937 1073 3605 8572
esx n/a| 0 0 0 6 4 53 .14 16 15 | -3411 -3387 3604 11131
gfz n/a| -1 -1 0 0 69 -26 .20 26 29 | 0 -990 3601 9153
grg n/a| 0 1 2 -55 32 -31 -.38 26 22 | -7308 -1062 3593 8268
iac n/a| 1 0 -6 112 -78 0 -.12 22 22 | -7243 844 3614 8633
mcc n/a| -4 8 -9 142 -98 79 -.31 186 186 | --- --- --- ---
Table 2.1990.1 GPS week: 1990 Day: 1 MJD: 58175
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 -39 -3 50 .04 33 32 | -6227 546 2918 9470
cof n/a| 0 0 -5 -27 -9 19 .09 36 33 | -6233 559 2923 9476
emx n/a| 0 -1 4 6 -8 0 .07 19 19 | -12421 1314 2902 8654
esx n/a| 0 3 0 28 0 35 .13 18 17 | -17679 -2081 2918 11647
gfz n/a| -1 -1 -1 15 18 -31 .20 26 24 | 0 23 2908 9406
grg n/a| 1 0 1 -59 50 -42 -.35 30 25 | -7061 556 2928 8746
iac n/a| 1 1 -2 9 -42 -28 -.11 22 22 | -5998 446 2917 8816
mcc n/a| 0 8 -12 -45 199 64 -.72 225 225 | --- --- --- ---
Table 2.1990.2 GPS week: 1990 Day: 2 MJD: 58176
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 1 -2 0 .04 32 31 | -5298 2009 3440 9111
cof n/a| 0 0 -13 -13 40 60 .05 35 33 | -5307 2022 3439 9112
emx n/a| -2 0 3 32 -22 -39 .06 20 20 | -16159 2271 3428 8638
esx n/a| 0 0 -2 -9 16 47 .14 16 15 | -25858 1594 3431 11452
gfz n/a| 0 0 -3 4 67 -58 .12 25 24 | 0 2918 3424 8997
grg n/a| 0 3 6 -54 6 -31 -.37 25 20 | -3400 -3493 3428 8526
iac n/a| 2 1 -1 34 -35 -14 -.10 23 23 | -4087 945 3427 8398
mcc n/a| 10 8 -7 179 49 584 .02 183 183 | --- --- --- ---
Table 2.1990.3 GPS week: 1990 Day: 3 MJD: 58177
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 -30 -29 34 .04 32 32 | 1880 -2545 3571 9900
cof n/a| -1 -2 -9 -43 -57 15 .09 35 35 | 1873 -2534 3580 9898
emx n/a| 0 -1 3 -12 -2 -21 .06 24 24 | 8244 -232 3561 9451
esx n/a| 0 0 1 0 -28 15 .14 15 17 | -5250 -2351 3576 11815
gfz n/a| 0 -2 5 8 21 40 .12 29 30 | 0 -1906 3537 9811
grg n/a| 0 3 -5 -75 0 89 -.37 26 24 | 786 -2799 3633 8929
iac n/a| 1 0 0 74 54 -101 -.11 23 23 | 1062 597 3575 9292
mcc n/a| 5 13 -21 139 98 -40 -.80 169 169 | --- --- --- ---
Table 2.1990.4 GPS week: 1990 Day: 4 MJD: 58178
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 0 -20 -21 90 .03 31 30 | 491 858 3629 10130
cof n/a| -2 -2 -2 -51 -29 28 .17 31 29 | 495 850 3627 10126
emx n/a| 0 -2 6 -36 -4 -17 .05 26 26 | 659 1300 3604 9676
esx n/a| 1 0 -1 -12 12 6 .19 19 19 | -4217 -2032 3617 12206
gfz n/a| -2 -3 1 0 11 13 .12 29 27 | 0 974 3615 10101
grg n/a| -1 0 4 -53 8 58 -.40 33 31 | 592 790 3619 9363
iac n/a| 2 4 -9 82 41 -120 -.24 26 27 | 2070 1242 3618 9692
mcc n/a| -4 10 -25 203 -43 -483 -.78 160 160 | --- --- --- ---
Table 2.1990.5 GPS week: 1990 Day: 5 MJD: 58179
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 -6 2 13 23 .12 30 29 | -2614 -2791 3101 9920
cof n/a| 0 -2 -6 -15 36 0 .16 34 32 | -2610 -2798 3104 9922
emx n/a| 0 2 8 15 -11 -98 .11 25 25 | -12314 -349 3094 9614
esx n/a| 0 0 -1 0 42 0 .14 17 17 | -11600 -3500 3096 12128
gfz n/a| -3 -1 0 -26 38 0 .11 29 26 | 0 -2775 3135 9995
grg n/a| -2 -1 3 -52 -16 29 -.34 26 25 | 667 -2849 3086 9811
iac n/a| 0 1 -5 44 -56 42 -.13 20 21 | 758 -499 3098 9362
mcc n/a| -12 4 -35 79 -26 -777 -.23 253 253 | --- --- --- ---
Table 2.1990.6 GPS week: 1990 Day: 6 MJD: 58180
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 -2 8 -7 40 .06 30 29 | -4414 1206 3282 9102
cof n/a| 0 0 -8 16 -22 -1 .08 32 30 | -4434 1242 3276 9100
emx n/a| -2 0 3 -20 -3 -73 .17 23 23 | 2003 1304 3254 8967
esx n/a| 0 0 0 -8 22 12 .12 17 16 | 10203 -1477 3266 12069
gfz n/a| 0 0 -1 44 7 25 .07 24 24 | 0 457 3269 9257
grg n/a| 0 0 3 -6 -6 -42 -.30 28 26 | 349 927 3265 8861
iac n/a| 1 0 -5 22 -36 13 -.18 21 21 | 1639 595 3272 8600
mcc n/a| 2 1 -11 34 -29 639 -.49 125 125 | --- --- --- ---
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 3.1990.0 GPS week: 1990 Day: 0 MJD: 58174
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 | 818 60 60 17 16 29 13 26 --- 11 | 77 76 44 43 44 44 49 --- 43
R02E | 784 18 18 15 15 23 20 11 59 7 | 106 102 100 110 92 91 99 138 100
R03E | 1251 38 38 21 11 30 21 19 128 9 | 66 67 49 43 34 46 36 66 42
R04E | 1165 37 37 14 13 22 19 30 --- 9 | 96 98 75 79 73 74 68 --- 75
R05E | 645 43 45 27 13 29 36 24 --- 12 | 84 83 74 64 64 73 63 --- 66
R06E | 703 14 15 18 12 18 14 17 --- 7 | 86 87 77 82 79 78 78 --- 78
R07E | 914 41 49 13 12 31 13 20 352 9 | 120 125 97 99 92 95 93 214 97
R08E | 2546 25 23 11 22 19 17 25 --- 9 | 77 76 57 64 56 64 62 --- 61
R09 | 1399 19 16 17 8 14 27 12 --- 7 | 40 38 39 37 45 43 40 --- 38
R10 | 988 15 17 11 11 26 13 9 --- 6 | 48 50 42 54 37 43 45 --- 44
R11 | 846 19 16 15 9 25 13 25 119 7 | 57 58 48 52 39 48 44 75 47
R13 | 1872 12 15 16 23 13 26 14 --- 8 | 47 51 45 60 43 33 48 --- 46
R14 | 692 37 33 17 9 33 16 16 --- 9 | 64 62 46 44 36 47 38 --- 42
R15 | 1876 63 56 25 17 28 33 42 --- 14 | 84 84 56 36 35 59 34 --- 43
R16 | 699 36 41 24 26 23 25 21 --- 11 | 45 53 43 59 44 32 53 --- 44
R17 | 475 33 38 19 10 27 9 25 --- 9 | 18 21 22 23 23 16 24 --- 18
R18 | 601 15 18 12 14 20 15 25 --- 7 | 17 20 18 18 24 17 14 --- 13
R19 | 614 43 38 20 20 25 16 29 --- 11 | 33 37 29 34 39 39 32 --- 31
R20 | 1919 20 18 25 19 36 48 13 --- 12 | 21 26 28 33 31 38 17 --- 20
R21 | 447 29 32 22 7 33 12 21 125 9 | 14 16 20 19 24 21 18 95 15
R22 | 441 33 37 18 11 30 15 22 --- 9 | 16 18 19 29 24 24 24 --- 20
R23 | 1905 8 12 10 18 23 23 17 --- 8 | 17 18 21 24 26 21 17 --- 15
R24 | 1267 33 26 46 21 31 68 26 --- 18 | 22 29 39 28 21 29 22 --- 20
XR26 | ---- --- --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- 37 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1222 33 33 20 16 26 26 22 186 |T 54 56 47 49 44 46 43 117 44
WRMS | 1222 33 33 20 15 29 22 22 186 |NE 36 38 34 36 32 34 31 85 30
MEDI | 846 33 32 17 13 26 17 21 125 |MD 48 53 44 43 39 43 38 95 42
Table 3.1990.1 GPS week: 1990 Day: 1 MJD: 58175
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 | 693 59 57 17 13 34 30 16 --- 12 | 48 47 33 42 48 35 37 --- 35
R02E | 1653 16 19 13 19 19 16 14 35 7 | 85 81 82 89 73 77 82 163 81
R03E | 1094 31 32 18 12 27 20 16 155 9 | 43 46 35 33 28 36 25 110 29
R04E | 722 34 37 19 12 24 21 17 --- 9 | 74 77 65 65 64 68 62 --- 64
R05E | 889 50 54 15 23 25 36 32 --- 13 | 69 76 50 62 46 48 54 --- 52
R06E | 1164 20 34 15 12 16 13 17 --- 6 | 65 72 53 55 53 55 53 --- 53
R07E | 715 48 44 15 10 30 16 17 441 10 | 98 98 81 86 77 85 80 272 82
R08E | 2037 25 23 11 13 18 11 14 --- 6 | 56 57 48 49 50 50 47 --- 48
R09 | 1657 19 22 14 17 20 25 14 --- 8 | 34 38 33 35 37 38 32 --- 31
R10 | 1535 13 15 10 12 16 15 15 --- 6 | 36 35 36 35 36 38 29 --- 33
R11 | 784 26 21 18 16 32 24 24 112 10 | 34 33 31 38 35 34 36 56 30
R13 | 1007 13 13 15 24 15 42 21 --- 10 | 33 32 38 41 37 33 35 --- 32
R14 | 867 34 38 14 11 26 11 18 --- 8 | 49 52 35 45 37 35 33 --- 37
R15 | 2122 65 63 27 20 37 18 30 --- 14 | 47 46 32 27 28 26 21 --- 24
R16 | 851 24 42 24 27 22 47 27 --- 13 | 42 50 43 50 34 32 45 --- 38
R17 | 504 28 31 13 11 21 17 31 --- 9 | 18 19 14 22 21 16 18 --- 14
R18 | 594 28 26 13 14 19 15 21 --- 8 | 18 23 19 29 23 26 19 --- 19
R19 | 631 51 65 28 22 29 12 45 --- 14 | 28 44 31 27 41 27 29 --- 27
R20 | 1562 21 19 30 26 17 66 18 --- 15 | 19 25 33 38 39 16 17 --- 21
R21 | 792 24 23 14 14 18 23 20 148 8 | 15 16 17 24 27 22 20 111 17
R22 | 462 26 22 11 13 25 18 17 --- 7 | 13 15 17 26 22 21 17 --- 17
R23 | 1334 12 17 7 14 14 26 12 --- 6 | 14 19 13 24 19 35 18 --- 16
R24 | 729 26 37 40 31 53 68 29 --- 19 | 28 41 34 34 32 20 24 --- 20
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 20 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1162 33 36 19 18 26 30 22 225 |T 42 45 37 42 39 37 35 142 35
WRMS | 1162 32 33 19 17 24 25 22 225 |NE 28 32 28 33 31 27 25 83 24
MEDI | 867 26 31 15 14 22 20 17 148 |MD 36 44 34 38 37 35 29 111 30
Table 3.1990.2 GPS week: 1990 Day: 2 MJD: 58176
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 | 642 52 56 23 8 26 16 21 --- 10 | 62 66 32 34 33 36 37 --- 34
R02E | 3023 16 22 13 13 17 11 10 288 6 | 118 119 109 114 113 104 104 80 109
R03E | 1680 33 35 17 11 27 10 16 161 8 | 56 59 37 44 30 30 30 95 35
R04E | 658 26 28 18 14 23 25 15 --- 8 | 71 77 59 73 54 78 58 --- 64
R05E | 863 44 47 23 14 34 27 42 --- 13 | 74 74 50 57 50 74 56 --- 54
R06E | 1290 19 20 21 15 13 19 11 --- 7 | 79 78 63 74 71 62 68 --- 67
R07E | 716 43 46 16 11 25 22 16 179 9 | 105 107 84 76 67 88 69 123 78
R08E | 1075 25 27 13 11 25 16 20 --- 7 | 73 74 58 61 54 58 70 --- 60
R09 | 2136 24 28 13 12 21 13 16 --- 7 | 29 31 28 31 38 27 28 --- 27
R10 | 1312 10 15 13 16 19 17 17 --- 7 | 43 48 39 47 40 33 39 --- 38
R11 | 657 15 16 15 11 18 26 21 114 8 | 42 42 43 43 43 54 32 72 40
R13 | 1842 9 10 7 18 20 14 14 --- 6 | 37 38 31 40 28 33 32 --- 32
R14 | 1265 41 40 12 11 19 9 30 --- 9 | 86 90 80 84 83 80 79 --- 80
R15 | 3473 67 68 28 25 44 28 36 --- 16 | 62 67 38 34 39 49 26 --- 32
R16 | 587 19 40 16 25 17 40 19 --- 11 | 50 72 46 54 40 37 41 --- 41
R17 | 557 30 28 14 7 31 17 17 --- 8 | 18 21 21 21 28 16 24 --- 19
R18 | 677 23 22 20 26 31 11 21 --- 10 | 17 16 13 26 25 18 17 --- 17
R19 | 798 48 43 25 21 33 20 38 --- 13 | 36 35 37 35 46 35 29 --- 33
R20 | 1311 20 18 42 14 21 60 22 --- 15 | 36 44 34 35 37 45 25 --- 29
R21 | 962 24 30 9 9 17 16 18 114 6 | 19 19 23 23 28 23 18 105 20
R22 | 519 17 22 11 11 27 22 25 --- 8 | 23 20 29 29 39 23 21 --- 24
R23 | 720 12 18 22 22 24 15 14 --- 9 | 23 21 27 26 20 31 16 --- 20
R24 | 789 41 47 31 19 24 53 35 --- 15 | 36 44 30 28 23 33 24 --- 18
XR26 | ---- --- --- --- --- --- --- 3 --- 0 | --- --- --- --- --- --- 41 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1421 32 35 20 16 25 25 23 183 |T 51 54 43 47 44 46 41 95 42
WRMS | 1421 31 33 20 15 24 20 23 183 |NE 37 40 34 37 37 35 30 88 32
MEDI | 863 24 28 16 14 24 17 18 161 |MD 43 48 37 40 39 36 32 95 34
Table 3.1990.3 GPS week: 1990 Day: 3 MJD: 58177
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 | 589 54 59 33 18 35 37 29 --- 14 | 66 70 59 52 53 69 59 --- 52
R02E | 2274 23 23 12 10 20 16 13 275 6 | 92 92 77 78 72 76 79 106 78
R03E | 2400 33 30 20 10 24 24 15 122 9 | 58 58 44 38 31 51 36 59 38
R04E | 762 27 27 16 10 24 17 14 --- 7 | 82 82 69 73 56 76 71 --- 70
R05E | 1915 34 37 24 16 43 43 36 --- 14 | 63 69 53 61 60 72 60 --- 56
R06E | 1795 15 20 25 22 17 24 23 --- 9 | 72 80 67 84 69 79 70 --- 72
R07E | 667 39 42 17 10 20 26 18 125 9 | 94 95 67 67 65 80 66 116 69
R08E | 698 25 25 16 10 23 13 19 --- 7 | 62 59 49 51 45 54 50 --- 49
R09 | 2162 15 19 14 7 15 16 16 --- 6 | 28 32 28 34 41 36 25 --- 29
R10 | 1828 16 17 19 20 21 14 18 --- 8 | 41 40 38 57 35 51 53 --- 46
R11 | 550 17 23 12 9 20 11 13 178 6 | 44 48 33 41 37 45 43 55 38
R13 | 1715 18 18 14 11 22 17 14 --- 7 | 36 38 33 39 34 41 37 --- 34
R14 | 797 39 37 17 9 28 15 35 --- 10 | 63 64 48 39 30 47 29 --- 38
R15 | 2302 71 79 40 21 37 26 43 --- 17 | 71 78 50 33 28 52 24 --- 30
R16 | 492 9 32 47 23 20 40 16 --- 13 | 55 74 49 59 43 50 43 --- 49
R17 | 618 33 41 19 11 41 24 28 --- 11 | 19 21 18 35 43 28 25 --- 25
R18 | 636 22 27 17 11 22 22 21 --- 8 | 18 22 20 22 22 28 21 --- 18
R19 | 1166 44 46 27 18 48 21 19 --- 12 | 26 28 37 29 37 28 25 --- 26
R20 | 1269 14 24 25 13 26 38 18 --- 10 | 29 46 43 34 39 25 27 --- 30
R21 | 1009 30 31 15 10 26 13 30 68 9 | 19 23 20 24 31 22 23 72 20
R22 | 701 31 32 19 10 27 18 12 --- 8 | 18 27 22 26 27 37 21 --- 21
R23 | 1220 11 17 20 24 24 17 11 --- 8 | 19 28 24 23 24 30 17 --- 18
R24 | 707 35 42 35 25 45 58 33 --- 17 | 36 46 29 29 32 25 22 --- 19
XR26 | ---- --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- 34 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1389 32 35 24 15 29 26 23 169 |T 48 53 42 44 41 47 40 81 40
WRMS | 1389 32 35 24 17 30 24 23 169 |NE 34 41 32 34 33 36 29 63 29
MEDI | 1009 27 30 19 11 24 21 18 125 |MD 44 48 43 39 37 47 34 72 35
Table 3.1990.4 GPS week: 1990 Day: 4 MJD: 58178
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 | 894 45 43 25 17 29 58 43 --- 16 | 60 68 63 72 72 75 54 --- 59
R02E | 1606 26 33 15 14 31 35 27 212 10 | 146 148 134 137 134 124 136 96 134
R03E | 1864 35 46 17 11 28 25 21 92 10 | 56 62 42 45 43 59 40 41 43
R04E | 1043 33 29 15 10 24 30 22 --- 9 | 99 99 89 91 86 107 92 --- 92
R05E | 2317 32 36 19 21 40 47 32 --- 14 | 75 85 56 74 71 79 76 --- 67
R06E | 1393 17 26 20 21 12 26 14 --- 8 | 87 93 81 96 89 78 90 --- 86
R07E | 1020 49 37 20 15 35 29 45 106 14 | 143 158 143 149 143 148 110 105 137
R08E | 620 27 27 18 16 25 38 25 --- 11 | 85 87 75 78 77 84 97 --- 79
R09 | 1944 15 18 15 12 18 31 12 --- 7 | 42 43 46 47 49 51 43 --- 44
R10 | 1509 19 17 19 27 14 29 9 --- 9 | 45 44 46 67 55 46 47 --- 51
R11 | 791 19 21 14 13 21 16 18 248 7 | 49 49 44 48 40 41 48 90 44
R13 | 3039 14 14 13 20 18 13 12 --- 7 | 42 39 40 53 42 42 45 --- 44
R14 | 627 31 27 13 10 31 12 18 --- 8 | 72 70 68 72 60 65 66 --- 67
R15 | 2647 67 65 46 26 54 44 50 --- 21 | 69 70 64 46 53 60 45 --- 47
R16 | 657 14 19 64 37 21 42 28 --- 17 | 58 62 39 72 57 56 55 --- 53
R17 | 792 29 24 21 11 39 24 21 --- 10 | 32 34 31 31 34 32 25 --- 28
R18 | 1200 22 21 19 8 22 12 26 --- 8 | 31 29 31 37 37 32 27 --- 30
R19 | 646 42 31 29 20 32 21 27 --- 12 | 43 44 41 44 58 44 38 --- 42
R20 | 891 39 41 36 10 32 49 27 --- 14 | 34 46 46 38 43 40 35 --- 35
R21 | 1002 32 33 24 10 33 19 18 36 10 | 32 33 37 39 38 34 30 39 32
R22 | 581 17 20 17 18 23 20 27 --- 9 | 31 33 31 42 37 32 21 --- 29
R23 | 1741 12 20 13 20 16 9 14 --- 7 | 33 38 29 35 32 31 25 --- 29
R24 | 664 19 21 33 27 36 63 22 --- 15 | 33 41 47 38 40 37 33 --- 33
XR26 | ---- --- --- --- --- --- --- 11 --- 0 | --- --- --- --- --- --- 28 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1452 31 31 26 19 29 33 26 160 |T 60 64 57 63 60 60 54 74 55
WRMS | 1452 30 29 26 19 27 31 27 160 |NE 43 45 42 47 45 42 38 64 40
MEDI | 1020 27 27 19 16 28 29 22 106 |MD 49 49 46 48 53 51 45 90 44
Table 3.1990.5 GPS week: 1990 Day: 5 MJD: 58179
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 | 770 46 48 22 11 32 15 18 --- 10 | 57 66 45 45 53 57 44 --- 45
R02E | 952 21 25 21 12 20 31 17 387 9 | 168 170 169 172 173 160 161 103 166
R03E | 930 34 38 19 12 27 29 30 101 11 | 62 64 51 48 46 55 43 46 46
R04E | 555 30 29 17 9 23 20 10 --- 8 | 125 124 112 113 105 123 112 --- 114
R05E | 1815 27 17 30 27 40 42 30 --- 14 | 57 53 56 54 61 59 57 --- 51
R06E | 969 19 15 26 21 17 16 15 --- 9 | 70 72 73 68 66 58 69 --- 65
R07E | 710 42 46 34 14 26 41 23 149 13 | 110 129 107 113 108 118 92 123 104
R08E | 706 20 36 21 17 21 23 27 --- 9 | 69 83 62 72 60 66 58 --- 62
R09 | 1691 15 12 16 13 12 14 11 --- 6 | 30 29 28 34 34 36 33 --- 31
R10 | 933 9 10 13 25 13 19 19 --- 8 | 36 36 34 44 34 30 30 --- 32
R11 | 784 17 23 15 17 27 11 21 356 8 | 41 47 40 42 41 38 33 166 37
R13 | 2387 17 12 11 15 29 22 20 --- 8 | 37 40 34 42 36 51 36 --- 37
R14 | 802 32 32 14 7 27 12 15 --- 7 | 54 53 45 42 41 43 54 --- 45
R15 | 2609 52 60 25 22 33 38 38 --- 15 | 49 55 37 36 32 48 40 --- 35
R16 | 905 17 29 64 35 15 44 14 --- 16 | 39 60 43 55 37 27 34 --- 36
R17 | 578 30 35 15 7 20 15 22 --- 8 | 19 22 15 18 22 18 19 --- 15
R18 | 1273 27 29 17 19 31 19 17 --- 9 | 19 26 16 18 24 19 18 --- 16
R19 | 796 46 48 30 15 34 18 16 --- 11 | 18 18 19 26 29 29 17 --- 19
R20 | 932 36 59 33 15 57 50 23 --- 15 | 26 60 36 28 39 27 35 --- 26
R21 | 684 27 23 14 12 33 12 14 101 8 | 17 20 15 23 25 24 25 50 18
R22 | 558 30 30 19 11 46 18 11 --- 10 | 18 20 22 19 34 31 23 --- 20
R23 | 1020 10 15 16 16 19 11 12 --- 6 | 16 20 16 24 26 20 19 --- 17
XR24 | 969 22 32 24 31 --- 78 18 --- 19 | 46 51 36 22 --- 33 21 --- 23
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 32 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1197 30 34 25 17 29 26 20 253 |T 51 57 48 50 51 50 46 97 45
WRMS | 1197 29 32 25 17 26 25 21 253 |NE 31 37 29 31 32 31 29 108 27
MEDI | 930 27 29 19 15 27 19 17 149 |MD 41 53 37 42 37 38 34 103 35
Table 3.1990.6 GPS week: 1990 Day: 6 MJD: 58180
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 | 886 43 54 21 12 25 38 24 --- 12 | 42 49 48 50 58 56 49 --- 47
R02E | 1546 19 24 19 12 16 11 13 80 6 | 220 217 210 215 206 198 207 256 209
R03E | 588 30 35 18 14 25 19 13 118 8 | 51 56 40 42 41 42 40 103 39
R04E | 874 31 31 14 13 23 19 13 --- 8 | 112 114 102 104 94 112 100 --- 103
R05E | 1077 27 47 24 20 34 45 25 --- 13 | 69 81 71 73 76 86 74 --- 71
R06E | 974 16 19 20 18 13 17 18 --- 8 | 78 83 72 81 75 69 73 --- 74
R07E | 884 43 35 33 14 26 29 42 --- 14 | 132 128 111 121 115 128 123 --- 119
R08E | 1251 28 27 15 11 23 14 15 --- 7 | 93 93 78 80 71 86 82 --- 80
R09 | 1639 14 16 17 7 19 19 13 --- 6 | 29 30 30 25 29 23 28 --- 25
R10 | 976 13 15 10 19 17 24 22 --- 8 | 54 54 49 65 58 47 47 --- 52
R11 | 867 23 23 21 19 23 15 24 196 9 | 54 58 45 50 35 39 34 200 41
R13 | 2638 11 16 10 18 16 18 10 --- 6 | 49 53 43 52 36 39 48 --- 44
R14 | 1689 38 48 20 12 29 13 15 --- 9 | 82 86 60 59 56 58 52 --- 58
R15 | 2666 60 50 30 24 25 33 31 --- 15 | 87 85 54 37 39 63 31 --- 44
R16 | 677 15 31 40 18 16 40 20 --- 12 | 57 58 43 68 52 47 51 --- 51
R17 | 602 24 27 16 11 29 10 21 --- 8 | 34 36 33 32 37 32 28 --- 30
R18 | 704 16 18 19 29 17 36 20 --- 11 | 30 33 32 43 41 39 27 --- 33
R19 | 528 41 37 23 19 27 26 20 --- 11 | 34 39 34 41 40 44 34 --- 35
R20 | 1385 41 24 34 14 27 36 10 --- 12 | 39 42 34 32 39 36 31 --- 29
R21 | 542 29 33 19 11 18 10 12 60 7 | 29 31 30 32 28 28 30 47 28
R22 | 591 23 29 19 12 33 20 20 --- 9 | 28 27 27 33 36 35 25 --- 28
R23 | 584 16 17 18 14 22 17 12 --- 7 | 27 30 28 32 38 40 31 --- 30
R24 | 1474 26 42 44 28 23 64 27 --- 16 | 51 70 50 34 33 38 32 --- 32
XR26 | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 39 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1263 30 32 23 17 24 28 21 125 |T 64 67 57 60 57 60 54 151 56
WRMS | 1263 29 30 23 16 24 26 21 125 |NE 45 48 39 42 39 40 35 123 37
MEDI | 886 26 29 19 14 23 19 18 80 |MD 51 56 45 50 41 44 39 103 42
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