[IGSREPORT-30306] Wk 2350 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 7 00:48:59 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2350 (Jan 19, 2025 - Jan 25, 2025)
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 2.2350.
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:
igl2350[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2350 in the SP3 format.
igl23507.sum Combination Report for GPS Week 2350.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | 5.3 ns
1 | -0.4 ns
2 | 1.2 ns
3 | 6.1 ns
4 | 1.8 ns
5 | 1.9 ns
6 | 6.1 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 1.2350, 1a.2350).
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 2.2350.0-6)
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 3.2350.0-6).
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 2350 summary. (Jan 19, 2025 - Jan 25, 2025)
Table 1.2350.a GPS week : 2350 MJD: 60694.0-60700.0
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 4 -3 2 66 .19 22 18 | 2671 299 3366 9077
| 0 0 1 12 11 14 .05 | 1216 2636
esa n/a| 0 0 -1 -20 -11 -8 -.21 27 22 | 3183 -210 3341 7984
| 1 2 1 15 13 38 .06 | 7004 2617
gfz n/a| 0 0 2 12 16 -14 -.01 24 16 | 0 119 3343 7940
| 1 1 1 15 16 28 .07 | 0 2492
grg n/a| 2 0 0 -21 -21 0 .38 26 19 | 2372 119 3333 8512
| 1 1 5 22 17 52 .04 | 1911 2378
iac n/a| 0 0 -3 20 23 -8 -.19 19 19 | 3651 170 3324 8969
| 1 1 2 15 27 39 .12 | 2338 1031
jgx n/a| 0 0 0 -1 -20 -42 -.14 23 23 | 4433 143 3290 8059
| 1 1 1 17 16 22 .04 | 1257 3088
Table 1.2350.b GPS week : 2350 MJD: 60694.0-60700.0
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 | 18 17 17 15 15 17 16 |
R02 | 6 7 6 7 5 6 9 |
R03 | 8 7 7 7 7 7 8 |
R04 | 8 10 9 8 7 8 8 |
R05 | 8 8 8 8 8 7 7 |
R06 | --- --- 0 0 47 40 51 |
R07 | 8 7 7 8 7 8 10 |
R08 | 10 8 7 8 8 9 8 |
R09 | 5 7 7 5 6 6 7 |
R11 | 8 8 7 6 7 7 6 |
R12 | 9 7 6 7 9 7 8 |
R14 | 6 6 4 6 8 5 6 |
R15 | 8 6 6 7 8 8 8 |
R16 | 10 8 8 7 8 8 7 |
R17 | 13 17 10 8 8 6 8 |
R18 | 9 10 12 9 7 6 6 |
R19 | 23 22 21 17 17 17 13 |
R20 | 23 24 22 22 31 29 19 |
R21 | 7 10 17 7 6 7 7 |
R22 | 7 7 8 18 6 7 7 |
R24 | 17 16 8 8 7 7 8 |
R26 | 32 31 --- --- --- --- --- |
Table 1.2350.c GPS week : 2350 MJD: 60694.0-60700.0
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 2350 0 | 116 41 25 -1269 -1083 -11940 76.7 2054 2054 | 5325 0
brd 2350 1 | 20 46 27 -1579 -2581 -7837 76.8 2417 2417 | -448 0
brd 2350 2 | 0 12 -29 -1182 -3182 -4134 79.1 2339 2339 | 1208 0
brd 2350 3 | 9 16 37 -305 714 -2037 82.0 1958 1958 | 6065 0
brd 2350 4 | 20 -70 45 13 1489 436 79.2 1805 1805 | 1750 0
brd 2350 5 | 86 21 176 1430 3638 4734 77.5 1879 1879 | 1879 0
brd 2350 6 | -40 -1 164 -1289 3442 6903 79.0 1740 1740 | 6125 0
-------------+------------------------------------------------------------+----------------
brd 2350 mean| 30 9 63 -597 348 -1982 78.6 2027 2027 | 3129 0
brd 2350 sdev| 53 38 76 1064 2736 6682 1.9 260 260 | 2657 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 2.2350.0 GPS week: 2350 Day: 0 MJD: 60694
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 5 -21 15 75 .23 21 17 | 4429 2841 3405 10358
esa n/a| 0 -3 -1 -7 -27 -21 -.26 30 25 | 14280 3010 3442 10426
gfz n/a| 0 1 2 18 18 -6 -.04 25 21 | 0 2962 3436 7598
grg n/a| 0 0 5 -25 -6 39 .36 21 17 | 2019 2799 3400 9956
iac n/a| -1 1 -6 13 40 -41 -.35 25 26 | 5088 559 3404 9759
jgx n/a| -1 0 0 19 -3 -54 -.12 22 22 | 5982 4147 3431 7945
Table 2.2350.1 GPS week: 2350 Day: 1 MJD: 60695
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 0 8 92 .22 19 15 | 2307 -3321 3232 11338
esa n/a| -1 1 -3 -20 -16 -66 -.12 29 24 | 11572 -4084 3261 7242
gfz n/a| -1 0 2 1 5 -56 -.06 27 14 | 0 -3400 3277 7934
grg n/a| 3 -2 3 -42 -6 36 .38 26 19 | -827 -3224 3235 11118
iac n/a| 0 2 -4 44 0 46 -.33 21 21 | 230 -1463 3229 10640
jgx n/a| -2 -1 1 -6 -18 -75 -.06 21 21 | 4469 -4696 2941 8050
Table 2.2350.2 GPS week: 2350 Day: 2 MJD: 60696
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 -17 60 .18 23 19 | 1740 -1925 3307 7392
esa n/a| 2 -1 -1 -29 2 -33 -.20 30 22 | -2586 -1785 3321 6976
gfz n/a| 1 0 3 3 23 -2 -.08 25 16 | 0 -1978 3308 7422
grg n/a| 1 -1 2 -9 -12 -45 .35 30 19 | 2089 -1811 3312 6984
iac n/a| -1 2 -4 26 7 6 -.09 20 20 | 1825 -28 3299 7829
jgx n/a| -2 0 -1 -3 -2 -52 -.14 21 21 | 2976 -1889 3297 7512
Table 2.2350.3 GPS week: 2350 Day: 3 MJD: 60697
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -1 5 -6 1 53 .12 23 21 | 3072 3422 3645 10463
esa n/a| -1 2 0 -29 -25 -23 -.29 26 22 | 246 1879 3334 9420
gfz n/a| 0 3 0 -10 -6 -18 .06 23 16 | 0 2666 3336 9460
grg n/a| 2 -1 0 18 -43 -9 .32 27 22 | 4481 2668 3346 9014
iac n/a| 0 0 -1 -2 63 -3 -.05 18 19 | 6004 2002 3318 9570
jgx n/a| 0 1 2 -8 -14 -34 -.19 23 24 | 4987 2772 3330 9431
Table 2.2350.4 GPS week: 2350 Day: 4 MJD: 60698
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 -1 5 0 1 73 .14 25 19 | 1209 -252 3598 9859
esa n/a| 0 2 0 4 10 30 -.25 24 19 | -560 -363 3679 8963
gfz n/a| 1 0 1 23 45 17 -.08 29 19 | 0 28 3674 9393
grg n/a| 2 0 0 -12 -44 -87 .44 25 18 | 1632 -228 3678 9215
iac n/a| 0 0 -3 21 -11 7 -.09 19 15 | 2916 331 3601 10080
jgx n/a| 0 0 0 24 -19 -11 -.13 24 24 | 3641 -156 3660 9471
Table 2.2350.5 GPS week: 2350 Day: 5 MJD: 60699
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 18 14 61 .26 22 18 | 1894 -1188 3418 7508
esa n/a| 2 0 -1 -18 -15 41 -.17 28 20 | 2845 -2165 3338 6519
gfz n/a| 0 0 3 19 22 12 .08 22 13 | 0 -1433 3359 7088
grg n/a| 3 -1 -10 -27 -9 8 .40 33 21 | 2291 -1292 3344 6803
iac n/a| 2 0 1 10 17 -78 -.16 15 13 | 2850 -120 3432 7809
jgx n/a| 0 2 0 -24 -36 -17 -.16 24 24 | 3071 -1391 3362 7235
Table 2.2350.6 GPS week: 2350 Day: 6 MJD: 60700
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 4 -10 -7 49 .15 19 16 | 4046 2517 2961 6625
esa n/a| 0 1 -3 -42 -5 10 -.19 27 22 | -3514 2035 3014 6347
gfz n/a| -1 1 2 33 4 -47 .04 20 14 | 0 1994 3012 6686
grg n/a| 4 1 -1 -49 -30 59 .42 21 17 | 4920 1924 3016 6496
iac n/a| -1 -1 -3 30 47 2 -.28 16 16 | 6649 -87 2985 7101
jgx n/a| 1 -1 3 -13 -49 -48 -.15 23 23 | 5907 2214 3013 6770
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 3.2350.0 GPS week: 2350 Day: 0 MJD: 60694
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1713 44 71 38 17 20 33 17 | 142 69 133 111 98 83 105
R02 | 2465 9 12 8 20 8 18 6 | 95 94 99 111 95 83 96
R03 | 1630 9 21 13 20 13 25 8 | 110 101 110 122 108 85 105
R04 | 2846 15 23 12 20 15 16 7 | 111 103 109 115 97 89 103
R05 | 2799 16 18 16 19 26 12 8 | 101 100 94 101 87 83 93
R07 | 1189 11 24 12 18 22 21 8 | 114 105 115 115 115 95 109
R08 | 2169 20 19 11 27 18 30 10 | 111 108 111 122 115 93 109
R09 | 1111 12 12 12 11 9 6 4 | 29 28 31 28 24 28 26
R11 | 1228 9 13 20 23 19 18 8 | 33 39 44 47 36 35 35
R12 | 1071 20 14 29 15 24 12 9 | 36 36 43 31 33 34 31
R14 | 932 9 9 21 11 14 10 5 | 39 41 50 41 42 34 39
R15 | 1255 15 15 23 11 20 21 8 | 45 48 53 34 42 34 39
R16 | 1321 27 26 23 7 18 28 10 | 52 65 59 48 50 44 48
XR17E | 1391 17 22 28 40 16 --- 13 | 101 106 107 95 99 --- 98
R18E | 705 11 18 26 25 16 13 8 | 47 50 47 62 49 46 48
XR19E | 2724 52 71 35 33 34 --- 23 | 94 53 82 87 50 --- 65
R20E | 4490 39 77 67 37 27 46 22 | 76 47 104 72 54 46 58
R21E | 682 19 15 15 15 11 17 7 | 65 65 71 72 67 68 67
R22E | 3504 17 14 21 17 11 8 6 | 58 61 66 65 55 59 59
R24E | 853 25 25 28 30 75 16 17 | 184 201 205 178 180 193 186
XR26 |>>>>> 30 --- --- 36 64 --- 32 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 2054 21 30 25 21 25 22 |T 82 76 86 82 74 68 75
WRMS | 2054 17 25 21 17 26 22 |NE 78 72 80 78 72 63 72
MEDI | 1391 17 18 21 20 18 17 |MD 76 65 82 72 55 59 65
Table 3.2350.1 GPS week: 2350 Day: 1 MJD: 60695
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1697 42 61 46 19 20 29 17 | 97 49 100 76 65 61 74
R02 | 1653 6 19 16 21 14 17 7 | 65 73 62 80 55 54 63
R03 | 1264 10 17 8 17 12 22 6 | 76 65 70 80 73 59 70
R04 | 3082 14 26 16 27 15 26 9 | 75 73 75 81 65 53 68
R05 | 2983 11 23 8 19 22 18 8 | 93 102 89 80 77 93 88
R07 | 782 7 16 14 14 19 15 6 | 73 65 65 75 83 67 71
R08 | 2760 14 18 13 20 16 21 7 | 73 76 75 81 81 64 74
R09 | 1296 12 17 16 10 17 21 7 | 16 20 17 26 19 31 18
R11 | 883 17 20 15 26 18 14 8 | 14 20 19 30 21 21 15
R12 | 652 14 17 18 6 20 14 7 | 16 27 35 27 33 26 23
R14 | 1780 8 16 20 14 15 9 6 | 22 35 34 20 25 24 24
R15 | 1476 16 15 14 10 10 14 6 | 22 36 25 16 19 19 20
R16 | 898 18 20 21 13 16 19 8 | 28 49 43 23 27 33 30
XR17E | 1472 28 16 19 62 24 --- 16 | 104 101 102 133 96 --- 103
R18E | 624 10 18 34 30 14 19 9 | 37 39 42 55 38 34 37
XR19E | 1512 53 61 33 21 36 --- 21 | 74 35 62 77 43 --- 54
R20E | 7036 46 72 79 46 23 42 23 | 63 52 86 41 40 43 45
R21E | 587 9 19 19 35 18 23 9 | 71 77 80 87 68 74 73
R22E | 3307 18 19 9 15 13 10 6 | 40 42 43 46 43 40 40
R24E | 1036 15 27 15 63 53 21 16 | 116 114 122 136 129 111 117
XR26 |>>>>> 30 --- --- 37 57 --- 30 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 2416 19 29 27 26 21 21 |T 58 57 62 63 55 50 55
WRMS | 2416 15 24 14 19 21 21 |NE 51 53 54 53 49 46 49
MEDI | 1476 14 19 16 20 18 19 |MD 65 49 62 75 43 43 54
Table 3.2350.2 GPS week: 2350 Day: 2 MJD: 60696
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1945 37 54 54 12 18 32 16 | 114 58 131 94 79 70 90
R02 | 792 9 13 14 17 13 15 6 | 67 77 80 79 67 58 69
R03 | 815 19 14 13 16 11 20 7 | 88 74 77 84 68 62 74
R04 | 2658 17 20 10 33 11 20 8 | 88 76 76 97 67 63 75
R05 | 3375 8 18 15 27 16 16 7 | 103 105 94 117 92 88 97
XR06 | 4707 4 --- --- --- --- --- 0 | --- --- --- --- --- --- 0
R07 | 1333 8 21 16 19 11 18 7 | 91 86 97 94 92 78 88
R08 | 2136 9 17 13 20 16 13 6 | 85 79 79 89 91 73 82
R09 | 1208 10 16 28 12 9 16 7 | 21 25 36 25 25 25 22
R11 | 899 7 17 18 20 13 7 6 | 27 30 32 31 28 24 25
R12 | 702 10 14 9 12 15 16 6 | 27 25 28 32 30 24 24
R14 | 1966 10 5 7 11 11 9 4 | 31 26 28 24 27 27 25
R15 | 893 21 17 9 9 12 12 6 | 33 35 29 31 28 23 27
R16 | 901 21 22 21 9 13 14 7 | 41 53 51 35 34 37 39
R17E | 2555 24 18 17 34 22 13 9 | 51 58 55 62 49 43 51
R18E | 597 8 17 15 55 28 18 11 | 62 61 66 100 61 62 64
R19E | 961 61 62 39 33 33 45 21 | 76 42 70 48 48 51 44
R20E | 7246 44 77 58 33 25 42 21 | 58 55 68 53 49 38 41
R21E | 665 18 20 23 81 44 19 17 | 73 70 79 106 75 65 69
R22E | 1445 14 13 13 31 19 15 8 | 72 76 86 98 67 78 76
R24E | 2907 13 23 16 22 14 14 7 | 80 73 79 87 77 74 76
------+-----------------------------------------+-------------------------------------
RMS | 2339 23 30 25 30 20 21 |T 64 59 67 69 57 53 57
WRMS | 2339 19 22 16 19 20 21 |NE 62 57 64 64 56 50 56
MEDI | 1333 13 17 15 20 14 16 |MD 67 58 70 79 61 58 64
Table 3.2350.3 GPS week: 2350 Day: 3 MJD: 60697
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2232 37 54 29 30 15 34 15 | 127 65 120 127 96 83 102
R02 | 706 5 16 18 16 13 15 6 | 84 88 89 84 90 75 84
R03 | 686 16 17 18 14 14 19 7 | 94 83 96 94 73 70 84
R04 | 1691 10 24 17 17 13 24 8 | 95 86 96 96 96 72 89
R05 | 2467 12 13 29 21 9 19 8 | 116 110 130 112 108 102 112
XR06 | 2119 4 --- --- --- --- --- 0 | --- --- --- --- --- --- 0
R07 | 870 10 18 16 25 7 24 7 | 95 92 93 88 88 75 87
R08 | 1839 18 15 13 29 10 22 8 | 96 94 96 100 99 85 94
R09 | 1387 13 9 13 6 13 12 5 | 16 22 32 21 29 16 20
R11 | 1114 11 6 11 18 12 14 5 | 24 23 26 29 26 28 24
R12 | 1155 23 13 14 19 9 15 7 | 27 32 32 19 24 25 22
R14 | 663 6 12 17 8 11 22 6 | 31 34 41 34 37 26 32
R15 | 721 24 17 15 11 8 10 6 | 33 21 29 20 22 16 21
R16 | 830 25 21 14 9 10 11 7 | 37 46 37 30 27 30 31
R17E | 2421 11 18 17 19 21 22 8 | 60 60 67 63 57 34 59
R18E | 747 12 18 19 32 16 13 8 | 33 33 35 49 36 31 32
R19E | 1248 54 43 34 31 22 39 17 | 73 52 71 57 51 36 52
R20E | 4811 54 64 57 35 15 57 21 | 70 54 79 47 53 42 47
R21E | 712 11 19 21 17 10 14 7 | 64 61 59 75 63 64 62
R22E | 1560 12 12 23 76 56 11 18 | 71 72 77 115 69 69 70
R24E | 4171 15 23 16 19 16 16 8 | 99 110 111 102 101 98 102
------+-----------------------------------------+-------------------------------------
RMS | 1957 23 26 23 27 18 23 |T 67 61 70 68 62 53 61
WRMS | 1957 21 22 16 22 19 24 |NE 67 61 70 65 62 54 61
MEDI | 1248 12 17 17 19 13 16 |MD 70 60 71 63 57 42 59
Table 3.2350.4 GPS week: 2350 Day: 4 MJD: 60698
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2090 49 45 37 14 18 28 15 | 115 53 102 83 73 77 81
R02 | 650 7 17 14 11 7 12 5 | 82 87 81 87 82 73 81
R03 | 652 10 17 15 17 6 21 6 | 91 79 95 90 84 70 84
R04 | 1144 13 20 10 17 10 16 6 | 83 80 78 89 81 71 79
R05 | 2232 20 15 16 14 15 21 7 | 76 62 73 72 50 49 61
XR06 | 1438 58 --- --- --- 37 --- 46 | --- --- --- --- --- --- 0
R07 | 1209 13 14 14 18 10 24 7 | 93 91 83 82 84 69 82
R08 | 1548 13 20 12 22 13 21 7 | 86 96 93 98 95 79 90
R09 | 1473 12 16 19 11 6 10 5 | 16 26 18 20 18 18 15
R11 | 1128 14 12 20 19 13 17 7 | 22 36 36 27 29 27 26
R12 | 1096 27 16 18 27 14 15 9 | 28 30 32 31 21 24 22
R14 | 598 8 13 23 17 16 20 7 | 30 24 36 25 36 22 27
R15 | 894 26 23 13 13 11 21 8 | 37 31 28 32 30 21 27
R16 | 1199 21 25 16 8 14 7 7 | 38 50 38 39 32 46 37
R17E | 1834 15 12 19 23 15 13 7 | 60 62 67 56 61 37 60
R18E | 695 8 15 23 16 13 12 6 | 36 40 42 37 40 38 36
R19E | 1055 47 34 29 68 16 21 17 | 92 114 116 125 101 113 107
R20E | 3218 61 57 100 54 62 77 31 | 104 126 146 109 76 112 97
R21E | 729 16 17 12 16 10 14 6 | 53 49 51 49 52 47 49
R22E | 1350 12 12 11 15 16 13 6 | 65 68 69 62 66 69 65
R24E | 4988 14 18 16 19 15 15 7 | 46 62 60 44 48 54 50
------+-----------------------------------------+-------------------------------------
RMS | 1805 25 24 29 25 19 24 |T 62 63 67 62 57 55 58
WRMS | 1805 19 19 19 18 15 24 |NE 61 57 61 59 55 49 54
MEDI | 1199 14 17 16 17 14 16 |MD 60 62 67 56 52 49 60
Table 3.2350.5 GPS week: 2350 Day: 5 MJD: 60699
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1448 51 50 35 35 14 35 16 | 99 57 86 60 73 50 70
R02 | 626 10 14 13 21 6 10 5 | 71 74 74 70 71 64 70
R03 | 2261 11 21 12 17 12 17 6 | 80 71 82 85 90 76 80
R04 | 471 15 18 18 19 15 25 8 | 77 71 82 70 87 63 75
R05 | 1443 17 10 17 19 7 21 7 | 77 70 81 67 71 59 70
XR06 | 2114 50 --- --- --- 30 --- 39 | --- --- --- --- --- --- 0
R07 | 1484 8 17 21 25 11 21 8 | 85 79 97 97 80 72 83
R08 | 1323 24 22 15 21 16 20 8 | 78 83 85 90 93 77 84
R09 | 1446 17 16 13 10 11 10 6 | 31 33 39 35 36 33 33
R11 | 609 12 16 10 21 16 14 6 | 22 32 27 32 30 20 24
R12 | 692 20 11 8 25 10 16 6 | 23 23 18 19 13 20 16
R14 | 922 14 15 10 10 10 10 5 | 19 32 31 29 28 32 27
R15 | 1086 18 23 13 20 16 19 8 | 30 30 24 43 34 19 27
R16 | 1723 19 17 9 19 19 12 7 | 34 45 36 46 26 48 35
R17E | 1876 13 15 10 19 10 11 5 | 60 61 63 57 61 28 59
R18E | 748 12 17 18 15 10 10 6 | 24 29 29 31 32 27 26
R19E | 1533 38 25 35 74 24 28 16 | 112 91 115 124 96 84 101
R20E | 3526 45 86 63 94 32 70 28 | 117 116 127 114 87 95 98
R21E | 1406 13 21 7 16 11 18 6 | 46 47 48 48 49 44 45
R22E | 1570 15 15 16 21 11 14 6 | 41 45 41 45 41 39 40
R24E | 5047 12 15 12 25 18 16 7 | 88 91 89 99 91 89 89
------+-----------------------------------------+-------------------------------------
RMS | 1878 22 28 22 33 15 24 |T 60 59 63 63 59 51 57
WRMS | 1878 18 20 13 21 13 24 |NE 55 53 58 57 56 48 53
MEDI | 1446 15 17 13 20 12 16 |MD 60 57 63 57 61 48 59
Table 3.2350.6 GPS week: 2350 Day: 6 MJD: 60700
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1277 43 59 20 26 13 37 15 | 153 82 137 122 118 96 118
R02 | 806 8 23 30 21 18 12 9 | 99 110 85 99 105 88 96
R03 | 2518 11 20 13 21 18 22 8 | 119 103 113 121 112 94 110
R04 | 1214 9 18 22 20 14 20 8 | 111 104 115 122 115 100 111
R05 | 613 17 16 13 14 13 22 7 | 106 96 104 104 100 81 98
XR06 | 2156 54 --- --- --- 47 --- 50 | --- --- --- --- --- --- 0
R07 | 2343 8 28 19 16 22 36 10 | 121 106 128 120 120 91 115
R08 | 1214 20 16 17 15 15 23 8 | 116 111 127 114 117 101 114
R09 | 1254 12 15 8 13 14 26 7 | 34 32 38 37 43 38 35
R11 | 756 11 13 14 12 13 18 6 | 23 30 35 31 22 37 26
R12 | 625 21 18 19 15 14 11 7 | 31 36 33 26 28 25 26
R14 | 2121 10 13 11 12 14 15 5 | 36 42 45 38 46 37 39
R15 | 1315 18 15 17 15 21 21 8 | 45 41 47 40 49 29 40
R16 | 1792 20 19 11 11 18 16 7 | 53 52 53 53 47 42 48
R17E | 2092 19 24 14 20 13 13 7 | 66 61 66 77 65 36 65
R18E | 1133 16 23 12 12 10 9 6 | 30 36 33 37 33 33 31
R19E | 1677 26 27 27 30 21 39 12 | 62 64 65 62 60 72 58
R20E | 2168 30 62 47 47 20 44 18 | 69 72 102 65 61 52 64
R21E | 1124 14 16 17 16 14 13 6 | 54 49 48 55 56 54 51
R22E | 1536 17 12 15 17 16 9 6 | 48 47 52 56 48 47 48
R24E | 3779 11 26 12 23 16 17 8 | 78 78 83 85 78 83 79
------+-----------------------------------------+-------------------------------------
RMS | 1739 19 27 20 21 16 23 |T 72 67 75 73 71 61 68
WRMS | 1739 16 22 14 17 16 23 |NE 80 72 81 79 78 66 75
MEDI | 1315 17 18 15 16 15 18 |MD 62 61 65 62 60 52 58
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