[IGSREPORT-29725] Wk 2298 IGLOS Final Orbits
acc
acc at igs.org
Mon Feb 12 00:16:01 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2298 (Jan 21, 2024 - Jan 27, 2024)
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 2.2298.
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:
igl2298[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2298 in the SP3 format.
igl22987.sum Combination Report for GPS Week 2298.
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).
The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | -4.2 ns
1 | -5.1 ns
2 | -8.8 ns
3 | -6.4 ns
4 | -6.8 ns
5 | -6.6 ns
6 | -10.7 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | COD | R26
0 | ESA | R26
0 | GFZ | R26
0 | GRG | R26
0 | IAC | R26
0 | JGX | R26
2 | COD | R26
2 | ESA | R26
2 | GFZ | R26
2 | GRG | R26
2 | IAC | R26
2 | JGX | R26
3 | COD | R26
3 | ESA | R26
3 | GFZ | R26
3 | GRG | R26
3 | IAC | R26
3 | JGX | R26
4 | COD | R26
4 | ESA | R26
4 | GFZ | R26
4 | GRG | R26
4 | IAC | R26
4 | JGX | R26
5 | COD | R26
5 | ESA | R26
5 | GFZ | R26
5 | GRG | R26
5 | IAC | R26
5 | JGX | R26
6 | COD | R26
6 | ESA | R26
6 | GFZ | R26
6 | GRG | R26
6 | IAC | R26
6 | JGX | R26
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 1.2298, 1a.2298).
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 2.2298.0-6)
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 3.2298.0-6).
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 2298 summary. (Jan 21, 2024 - Jan 27, 2024)
Table 1.2298.a GPS week : 2298 MJD: 60330.0-60336.0
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 4 -10 49 .14 25 20 | 14239 691 3298 8119
| 0 0 1 9 19 19 .07 | 1492 1027
esa n/a| 0 0 0 -25 -11 -28 -.19 34 22 | -8569 667 3299 7521
| 1 0 1 13 8 14 .05 | 4252 1133
gfz n/a| 0 0 1 41 12 -8 -.03 26 15 | 0 993 3346 7209
| 0 0 1 13 15 21 .08 | 0 881
grg n/a| 1 -3 -4 8 0 10 .34 32 28 | -7524 856 3344 6810
| 1 0 2 29 13 37 .09 | 2006 1030
iac n/a| 0 0 -4 11 44 -18 -.19 25 23 | -5534 -55 3300 8129
| 1 2 1 25 20 64 .09 | 2345 578
jgx n/a| 0 0 -5 -44 15 -28 -.23 29 28 | 17434 931 3221 7313
| 1 1 2 30 14 46 .02 | 1370 1031
Table 1.2298.b GPS week : 2298 MJD: 60330.0-60336.0
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 17 17 18 22 20 22 |
R02 | 7 7 7 8 11 7 18 |
R03 | 7 8 7 8 9 13 13 |
R04 | 7 8 9 9 10 7 20 |
R05 | 6 7 6 9 8 7 18 |
R07 | 6 8 10 6 10 10 13 |
R08 | 7 9 9 10 9 9 14 |
R09 | 8 5 6 7 6 7 11 |
R11 | 9 8 7 7 11 7 7 |
R12 | 9 9 6 8 10 8 6 |
R13 | 17 20 22 21 20 24 22 |
R14 | 6 8 6 6 6 6 6 |
R15 | 8 8 7 7 9 11 10 |
R16 | 7 9 7 8 10 11 11 |
R17 | 10 11 9 11 10 8 11 |
R18 | 8 7 7 10 9 11 9 |
R19 | 20 19 19 19 16 24 28 |
R20 | 39 45 43 41 37 38 39 |
R21 | 8 10 10 10 12 11 11 |
R22 | 9 9 10 9 8 8 10 |
R24 | 12 10 10 11 11 12 12 |
R25 | 13 14 16 11 17 19 16 |
R26 | --- 17 --- --- --- --- --- |
Table 1.2298.c GPS week : 2298 MJD: 60330.0-60336.0
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 2298 0 | 106 42 8 1206 3355 4903 80.8 1429 1429 | -4229 0
brd 2298 1 | -3 -44 37 1464 1470 -763 78.0 1694 1694 | -5076 0
brd 2298 2 | 44 -55 3 1553 863 -7989 79.0 1605 1605 | -8817 0
brd 2298 3 | 63 12 108 755 -200 -7833 79.7 1557 1557 | -6377 0
brd 2298 4 | -3 72 84 16 1426 -3251 80.1 1485 1485 | -6769 0
brd 2298 5 | -114 -4 -19 -795 -678 -5121 79.0 1688 1688 | -6549 0
brd 2298 6 | 67 -21 -51 -1345 -758 -6833 78.3 1602 1602 | -10689 0
-------------+------------------------------------------------------------+----------------
brd 2298 mean| 22 0 24 407 782 -3841 79.3 1580 1580 | -6929 0
brd 2298 sdev| 72 46 56 1144 1471 4654 1.0 98 98 | 2194 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 2.2298.0 GPS week: 2298 Day: 0 MJD: 60330
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 11 -23 76 .09 23 18 | 13577 1935 3683 8485
esa n/a| 0 0 0 -43 0 -18 -.11 36 24 | -10543 2526 3678 8328
gfz n/a| 0 0 3 45 19 -15 -.06 24 13 | 0 2159 3745 7371
grg n/a| 2 -3 -4 -13 0 35 .25 27 22 | -5445 2459 3717 7150
iac n/a| 0 -2 -2 17 64 61 -.19 19 18 | -1727 -606 3686 8456
jgx n/a| -2 2 -4 -43 9 -67 -.23 26 27 | 17045 2614 3776 7752
Table 2.2298.1 GPS week: 2298 Day: 1 MJD: 60331
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 7 -22 52 .08 23 19 | 13613 739 3722 8129
esa n/a| -1 0 1 -18 -21 -28 -.21 35 23 | -9328 798 3743 7310
gfz n/a| 0 0 1 60 14 -28 -.03 29 14 | 0 595 3735 7101
grg n/a| 2 -2 -1 12 -6 61 .27 30 30 | -5588 537 3752 6703
iac n/a| -1 -1 -5 10 45 0 -.15 24 22 | -4580 -161 3736 8013
jgx n/a| 1 1 -2 -81 22 -100 -.25 28 28 | 17380 1086 3579 7057
Table 2.2298.2 GPS week: 2298 Day: 2 MJD: 60332
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 13 -29 64 .12 24 19 | 11741 1305 3434 7931
esa n/a| 0 -1 1 -36 -3 -41 -.23 32 19 | -7662 606 3427 7729
gfz n/a| -1 1 0 46 20 27 -.08 25 15 | 0 1416 3485 7203
grg n/a| 2 -2 -2 -13 8 -8 .35 30 34 | -9570 1420 3523 6650
iac n/a| -1 1 -4 53 8 -120 -.13 25 21 | -7269 657 3435 8014
jgx n/a| -1 0 -6 -32 18 -30 -.25 30 30 | 15556 492 3383 7472
Table 2.2298.3 GPS week: 2298 Day: 3 MJD: 60333
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 0 -13 25 .18 21 18 | 15069 -524 3329 7896
esa n/a| 0 0 0 0 -3 -42 -.23 33 23 | -4625 -1153 3336 7803
gfz n/a| 1 0 1 47 -9 -20 .06 30 14 | 0 -273 3409 7313
grg n/a| 0 -3 -1 7 25 51 .32 27 21 | -6482 -443 3403 7169
iac n/a| 2 0 -5 18 64 -80 -.25 25 21 | -5055 -985 3335 7984
jgx n/a| -1 1 -7 -69 -4 -10 -.26 30 26 | 17727 398 3193 7581
Table 2.2298.4 GPS week: 2298 Day: 4 MJD: 60334
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 4 9 26 33 .06 28 24 | 15603 471 2903 6701
esa n/a| 0 -1 0 -25 -21 -22 -.16 28 20 | -7476 635 2889 5591
gfz n/a| 0 0 1 36 -1 17 .08 24 17 | 0 1195 2947 5612
grg n/a| 2 -4 -3 46 -9 -31 .29 31 25 | -7154 771 2973 5535
iac n/a| -2 0 -4 20 59 0 -.11 23 22 | -5262 186 2893 6624
jgx n/a| 0 0 -3 -27 18 -35 -.19 30 28 | 19398 -242 2691 5648
Table 2.2298.5 GPS week: 2298 Day: 5 MJD: 60335
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 6 -15 -9 60 .19 27 22 | 16148 1634 3202 8147
esa n/a| -1 -2 1 -24 -17 -39 -.27 34 19 | -3802 1309 3214 7379
gfz n/a| 1 0 0 40 8 -22 -.17 24 16 | 0 1741 3259 7251
grg n/a| 1 -2 -9 -28 2 -19 .53 32 23 | -7639 1512 3242 6760
iac n/a| -1 1 -4 -8 26 -30 -.12 26 24 | -5538 435 3206 8204
jgx n/a| 0 0 -5 7 5 44 -.23 31 29 | 18818 1985 3257 7134
Table 2.2298.6 GPS week: 2298 Day: 6 MJD: 60336
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 8 2 1 32 .26 27 21 | 13924 -719 2813 9549
esa n/a| 3 0 -3 -28 -11 -3 -.15 40 28 | -16553 -46 2809 8513
gfz n/a| 0 0 4 17 36 -16 -.04 30 16 | 0 119 2842 8617
grg n/a| -2 -2 -6 45 -14 -16 .33 44 44 | -10791 -264 2804 7705
iac n/a| -2 5 -1 -29 43 39 -.36 31 31 | -9313 88 2815 9609
jgx n/a| 0 2 -7 -63 41 -2 -.22 30 28 | 16116 184 2672 8550
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 3.2298.0 GPS week: 2298 Day: 0 MJD: 60330
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1749 20 53 44 14 24 27 17 | 66 87 83 71 79 76 70
XR02 | 663 9 14 10 12 17 --- 6 | 62 71 64 70 58 --- 65
R03E | 933 13 18 13 16 20 12 7 | 105 113 101 112 98 114 107
R04E | 1258 9 18 13 14 17 16 7 | 52 56 56 52 54 52 52
R05E | 1886 10 11 12 13 22 12 6 | 53 48 54 52 61 48 50
R07E | 622 10 13 11 13 16 13 6 | 65 56 58 69 61 56 60
R08E | 2495 8 15 16 18 11 14 7 | 59 60 58 55 56 55 56
R09 | 614 12 15 13 25 16 16 8 | 31 31 32 35 26 34 31
R11 | 1727 10 14 16 21 16 25 9 | 32 31 33 35 28 37 30
R12 | 614 22 8 12 21 15 23 9 | 37 29 35 31 28 34 31
R13 | 802 28 15 14 46 10 53 17 | 45 35 41 38 34 30 35
R14 | 1603 8 17 10 12 24 15 6 | 38 41 37 32 42 38 36
R15 | 601 16 16 13 11 15 19 7 | 39 43 43 39 42 30 37
R16 | 1057 14 12 12 9 17 18 6 | 47 48 48 48 54 41 45
XR17 | 978 8 28 13 16 15 --- 9 | 69 58 70 75 68 --- 67
R18 | 818 12 20 11 17 21 18 8 | 73 78 71 80 68 72 73
R19 | 2064 38 51 20 53 23 40 20 | 75 39 77 75 65 58 62
R20 | 1537 66 121 76 61 31 55 39 | 128 57 135 90 90 64 87
R21 | 596 17 21 8 14 13 19 8 | 87 71 85 84 83 73 79
R22 | 2246 15 8 10 30 18 20 9 | 39 48 42 55 37 46 42
R24 | 1401 19 25 15 29 24 27 11 | 103 83 105 95 90 77 92
XR25 |12321 11 14 --- --- 23 --- 12 | 35 37 --- --- 30 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1428 23 36 24 27 19 26 |T 60 55 63 61 57 54 56
WRMS | 1428 18 24 13 22 18 27 |NE 58 50 61 59 53 48 52
MEDI | 1057 12 15 13 16 17 19 |MD 53 48 58 55 58 52 52
Table 3.2298.1 GPS week: 2298 Day: 1 MJD: 60331
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1379 20 42 48 18 37 34 17 | 65 51 83 64 62 55 58
XR02 | 764 10 13 14 14 11 --- 7 | 44 40 44 46 44 --- 42
R03E | 1078 12 19 19 12 25 10 7 | 80 82 74 78 80 80 78
R04E | 1928 9 18 13 14 20 18 7 | 39 38 42 36 39 32 36
R05E | 1259 11 13 12 13 18 16 6 | 54 51 51 57 58 52 52
R07E | 924 13 14 14 18 21 17 7 | 71 71 66 81 62 68 70
R08E | 1245 17 20 15 21 25 17 9 | 45 47 50 48 48 38 43
R09 | 743 8 8 11 13 18 11 5 | 30 28 33 35 38 22 29
R11 | 2315 10 12 21 19 10 17 8 | 17 23 32 28 20 15 19
R12 | 727 26 8 8 14 23 26 9 | 27 19 24 17 27 26 19
R13 | 1287 34 11 15 62 26 56 20 | 22 25 27 29 25 38 22
R14 | 1423 12 12 8 22 15 23 8 | 28 28 25 32 26 21 24
R15 | 1103 15 11 22 11 16 15 8 | 27 41 45 39 31 36 34
R16 | 501 25 23 12 7 21 13 9 | 36 42 34 34 33 33 33
XR17 | 1580 21 19 9 20 19 --- 10 | 108 106 100 104 105 --- 103
R18 | 1261 8 13 13 13 20 19 6 | 86 91 88 87 79 91 88
R19 | 4529 27 45 46 36 33 35 19 | 59 71 74 65 51 53 60
R20 | 2201 65 127 90 83 41 70 44 | 92 96 116 76 86 56 77
R21 | 681 16 18 15 24 25 27 10 | 77 71 74 81 70 62 72
R22 | 2025 14 14 18 26 19 15 9 | 42 40 40 56 39 41 39
R24 | 800 22 15 12 30 27 18 10 | 71 67 65 59 68 66 64
XR25 |16243 12 16 --- --- 22 --- 14 | 33 31 --- --- 39 --- 30
XR26 |20378 17 --- --- 17 105 --- 17 | 30 --- --- 30 27 --- 6
------+-----------------------------------------+-------------------------------------
RMS | 1694 23 35 29 30 24 28 |T 51 52 56 53 50 46 47
WRMS | 1694 19 23 14 30 22 28 |NE 48 51 54 51 47 43 44
MEDI | 1261 15 14 14 18 21 18 |MD 44 42 50 48 44 41 42
Table 3.2298.2 GPS week: 2298 Day: 2 MJD: 60332
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 748 44 28 38 12 54 34 17 | 62 50 82 57 55 48 55
XR02 | 1852 8 14 11 12 21 --- 6 | 51 50 52 57 57 --- 51
R03E | 733 12 11 10 16 14 15 6 | 69 60 70 63 65 64 64
R04E | 1037 20 20 17 13 19 21 9 | 33 41 44 39 40 31 35
R05E | 938 11 14 11 11 26 10 5 | 51 54 51 49 46 45 49
R07E | 2189 14 21 26 16 20 20 10 | 43 47 55 51 41 40 45
R08E | 1097 19 16 11 15 16 27 9 | 41 40 40 46 41 35 38
R09 | 603 9 11 13 11 30 17 6 | 19 27 24 17 21 24 18
R11 | 1877 11 9 10 20 19 18 7 | 16 19 22 21 23 22 16
R12 | 559 11 15 10 7 18 11 5 | 25 17 31 29 34 31 24
R13 | 1123 39 27 22 43 16 74 21 | 34 37 31 30 44 43 26
R14 | 1380 12 12 11 12 16 10 5 | 29 28 33 31 32 25 28
R15 | 1168 15 14 8 12 18 16 6 | 27 23 25 27 28 20 23
R16 | 507 13 16 11 12 13 11 6 | 32 37 38 34 33 37 34
XR17 | 1340 16 21 12 12 16 --- 9 | 70 73 70 68 75 --- 69
R18 | 968 9 20 8 11 14 19 7 | 43 49 40 43 36 38 41
R19 | 3397 26 33 31 54 26 45 19 | 79 87 83 87 62 78 78
R20 | 3434 62 114 79 93 44 66 42 | 110 114 152 68 107 102 101
R21 | 581 21 16 17 13 28 28 9 | 74 63 68 71 79 67 67
R22 | 2244 19 14 13 31 22 14 9 | 72 68 78 51 55 71 66
R24 | 1103 15 25 24 13 22 15 9 | 97 88 107 100 96 95 97
XR25 |14771 15 16 --- --- 28 --- 16 | 34 47 --- --- 31 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1604 24 32 25 30 25 30 |T 50 50 56 48 49 48 48
WRMS | 1604 19 19 15 34 21 30 |NE 50 51 56 47 49 50 48
MEDI | 1103 15 16 12 13 19 18 |MD 43 47 51 46 41 40 41
Table 3.2298.3 GPS week: 2298 Day: 3 MJD: 60333
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 2152 45 35 25 23 47 40 17 | 108 118 109 117 104 121 110
XR02 | 1593 13 10 11 18 20 --- 8 | 84 81 93 89 81 --- 86
R03E | 688 11 18 11 19 21 13 7 | 107 114 100 120 107 111 109
R04E | 1557 16 19 14 16 16 22 8 | 29 34 40 42 30 30 32
R05E | 860 17 15 25 11 20 13 8 | 61 56 52 58 59 54 55
R07E | 1991 10 12 16 13 12 11 6 | 72 62 70 74 65 58 66
R08E | 1341 22 17 17 15 16 26 10 | 67 59 68 74 61 57 64
R09 | 1162 14 19 13 11 21 11 7 | 20 28 20 23 20 26 19
R11 | 596 15 13 13 11 20 8 6 | 27 21 26 30 27 25 23
R12 | 751 18 11 9 16 23 22 8 | 32 31 29 30 33 33 28
R13 | 817 26 14 28 57 24 64 20 | 37 37 49 29 50 41 35
R14 | 1088 7 10 13 10 17 18 6 | 30 37 41 38 36 34 34
R15 | 1479 16 9 22 12 35 8 7 | 38 36 31 36 39 39 33
R16 | 547 17 10 21 13 18 15 7 | 35 37 38 38 41 39 34
XR17 | 1590 14 25 17 21 21 --- 11 | 81 73 79 76 71 --- 76
R18 | 1154 14 15 19 21 16 26 9 | 72 73 81 84 73 72 74
R19 | 2470 22 39 35 43 32 48 19 | 73 55 70 83 73 66 64
R20 | 3447 42 120 97 67 43 63 41 | 96 75 125 97 86 64 72
R21 | 702 17 19 18 14 23 28 9 | 56 40 55 54 57 45 47
R22 | 2272 18 10 14 22 23 20 9 | 49 60 57 79 50 54 58
R24 | 676 15 18 31 16 18 25 10 | 60 54 62 66 60 46 55
XR25 |15588 10 12 --- --- 28 --- 11 | 39 34 --- --- 33 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1557 21 33 30 27 25 30 |T 57 55 61 62 56 53 55
WRMS | 1557 18 23 14 21 21 26 |NE 51 48 57 56 51 44 48
MEDI | 1162 16 15 17 16 21 22 |MD 56 54 57 58 57 46 55
Table 3.2298.4 GPS week: 2298 Day: 4 MJD: 60334
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1630 56 30 28 69 28 24 21 | 117 118 109 154 111 108 115
XR02 | 1287 17 11 18 28 17 --- 11 | 46 47 39 71 43 --- 47
R03E | 886 14 14 17 22 14 17 8 | 59 65 69 71 60 61 63
R04E | 1971 8 17 21 20 19 24 9 | 34 40 54 50 35 33 38
R05E | 932 16 11 18 14 12 16 7 | 50 52 64 60 46 49 53
R07E | 1346 17 19 19 19 30 24 10 | 38 43 44 43 44 43 39
R08E | 1819 20 16 13 20 14 16 8 | 43 45 46 41 42 40 41
R09 | 1506 12 10 8 14 15 10 5 | 28 25 21 27 24 34 25
R11 | 580 18 16 18 39 10 9 10 | 21 25 30 34 22 20 20
R12 | 746 7 13 22 21 21 26 9 | 20 29 33 16 20 19 21
R13 | 1389 44 19 19 39 31 65 19 | 25 30 37 28 47 39 27
R14 | 860 7 6 14 14 27 18 6 | 27 25 33 20 34 22 24
R15 | 976 24 13 17 13 16 21 9 | 34 27 28 30 32 21 25
R16 | 1168 29 9 22 20 13 12 10 | 36 38 46 49 38 34 38
XR17 | 1075 19 19 10 16 16 --- 9 | 66 55 55 64 51 --- 58
R18 | 766 13 16 10 25 25 26 9 | 54 56 58 70 50 53 56
R19 | 1111 36 37 29 33 37 24 16 | 76 69 86 75 68 50 69
R20 | 2691 62 93 67 64 37 71 36 | 91 49 88 93 72 56 58
R21 | 1219 20 23 21 26 11 27 11 | 70 70 76 72 63 65 69
R22 | 3085 17 13 8 23 16 19 8 | 79 79 76 85 68 70 76
R24 | 584 18 17 18 25 31 30 11 | 103 103 99 97 87 112 101
XR25 |14862 16 16 --- --- 25 --- 16 | 59 56 --- --- 56 --- 55
------+-----------------------------------------+-------------------------------------
RMS | 1484 28 28 24 31 23 30 |T 52 52 56 58 49 48 50
WRMS | 1484 24 20 17 25 22 28 |NE 51 48 53 54 47 45 48
MEDI | 1168 17 16 18 22 17 24 |MD 46 47 54 50 46 43 47
Table 3.2298.5 GPS week: 2298 Day: 5 MJD: 60335
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 730 42 44 23 50 34 35 19 | 127 127 125 135 126 129 124
XR02 | 939 8 12 11 15 14 --- 6 | 82 80 72 86 77 --- 78
R03E | 950 18 26 13 45 23 17 12 | 123 134 123 131 125 119 123
R04E | 2150 12 13 14 19 16 14 7 | 56 50 62 63 60 45 54
R05E | 2338 10 12 11 18 21 17 7 | 57 50 51 61 50 52 52
R07E | 1572 15 14 20 25 34 20 9 | 81 78 74 90 63 80 78
R08E | 2221 15 17 14 21 23 19 8 | 47 45 37 44 44 49 42
R09 | 1416 17 13 7 12 13 20 7 | 13 20 13 17 13 32 15
R11 | 683 14 14 10 21 14 11 7 | 22 29 25 29 27 38 23
R12 | 588 21 19 8 15 19 12 8 | 16 32 23 19 14 21 16
R13 | 2618 42 19 24 67 36 70 23 | 27 37 31 19 25 31 22
R14 | 907 9 6 10 14 16 19 6 | 18 18 22 21 24 27 19
R15 | 484 19 11 16 15 27 37 10 | 21 24 29 21 33 29 19
R16 | 1016 21 17 20 16 13 30 10 | 20 30 36 21 20 23 20
XR17 | 1482 16 13 11 18 24 --- 8 | 122 115 120 118 113 --- 119
R18 | 799 9 22 21 32 21 21 11 | 84 89 87 92 81 84 84
R19 | 774 47 66 35 46 40 34 23 | 96 81 102 67 76 91 83
R20 | 3479 70 103 72 56 48 61 37 | 82 59 78 50 66 69 58
R21 | 1469 14 23 26 23 22 20 11 | 39 29 43 40 39 33 33
R22 | 2737 15 8 13 19 18 18 7 | 66 79 78 95 67 70 76
R24 | 664 22 23 21 18 21 32 11 | 102 105 102 97 98 99 100
XR25 |17410 18 20 --- --- 35 --- 19 | 55 43 --- --- 29 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1688 27 34 24 32 26 31 |T 60 61 63 64 58 59 58
WRMS | 1688 22 19 16 23 24 29 |NE 53 54 57 56 51 49 50
MEDI | 1016 16 17 14 19 21 20 |MD 56 50 62 61 60 49 52
Table 3.2298.6 GPS week: 2298 Day: 6 MJD: 60336
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 809 36 57 47 21 54 41 21 | 93 86 99 100 92 92 87
XR02 | 945 15 26 16 62 29 --- 18 | 132 129 140 167 128 --- 137
R03E | 692 9 19 18 54 42 26 13 | 109 110 111 122 119 103 108
R04E | 1920 26 34 22 86 50 17 19 | 44 57 59 96 51 45 46
R05E | 3847 13 25 20 85 48 14 17 | 47 45 49 110 46 46 50
R07E | 2436 18 19 17 52 25 17 12 | 63 66 63 82 55 61 61
R08E | 2029 17 26 12 59 34 17 13 | 69 51 64 103 59 60 64
R09 | 996 10 18 24 14 15 31 10 | 15 21 27 29 15 33 18
R11 | 693 11 9 13 24 11 13 7 | 27 32 32 36 32 33 29
R12 | 751 10 15 8 14 18 13 6 | 30 34 31 30 31 33 29
R13 | 1980 36 16 27 64 41 60 21 | 43 37 41 32 39 34 33
R14 | 704 12 11 9 17 10 13 6 | 34 39 40 33 32 35 35
R15 | 651 14 19 17 12 13 27 9 | 37 46 40 33 41 37 35
R16 | 873 23 17 23 13 15 27 11 | 40 55 57 40 45 41 42
XR17 | 1806 18 21 15 24 20 --- 11 | 95 81 85 81 81 --- 85
R18 | 587 9 23 13 23 29 19 8 | 61 70 66 63 59 51 60
R19 | 1001 59 68 51 31 39 56 27 | 106 67 104 78 77 72 77
R20 | 1024 61 123 82 66 30 43 39 | 111 55 119 70 84 67 68
R21 | 1032 12 24 25 18 19 22 10 | 59 45 65 57 58 43 52
R22 | 2540 22 19 10 23 11 20 9 | 68 75 71 87 66 72 72
R24 | 1237 26 27 20 21 20 26 12 | 95 96 94 90 88 89 91
XR25 |12288 13 17 --- --- 20 --- 15 | 45 40 --- --- 34 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1602 27 40 30 44 31 30 |T 66 60 69 74 62 55 59
WRMS | 1602 21 28 16 44 31 28 |NE 64 57 67 64 60 49 56
MEDI | 1001 15 19 18 24 20 22 |MD 61 55 64 78 58 46 52
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