Date: July 25th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5651 05 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 1657)
---------------------------------------

Vector Time (GMT): 2007/204/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -389498
02                 A    =         6726398
65  meter
 Y    =       -6651657
29  meter          E    =           
0009717
 Z    =        -932167
04                 I    =           51
33251
 XDOT =       4799
185026                 Wp   =           93
48149
 YDOT =      -1102
568288  meter/sec      RA   =          273
07661  deg
 ZDOT =       5914
739576                 TA   =          256
29715
                                          MA   =          256
40535
                                          Ha   =            189
752  n
mi
                                          Hp   =            178
986

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1277880
63                 X    =         -310560
97
 Y    =      -21823022
60  feet           Y    =        -6655571
39  meter
 Z    =       -3058290
81                 Z    =         -933868
39
 XDOT =      15745
357698                 XDOT =        4782
424779
 YDOT =      -3617
350025  feet/sec       YDOT =       -1048
995625  meter/sec
 ZDOT =      19405
313569                 ZDOT =        5938
013086

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21015091
73                 X    =         6405399
96
 Y    =       -6016571
13  feet           Y    =        -1833850
88  meter
 Z    =       -3065489
91                 Z    =         -934361
33
 XDOT =       6520
199829                 XDOT =        1987
356908
 YDOT =      12929
701431  feet/sec       YDOT =        3940
972996  meter/sec
 ZDOT =      19493
261825                 ZDOT =        5941
546204


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07204
95212677  
00020000  00000-0  20000-3 0  9001
2 25544  51
6343 273
8003 0009121 157
8157 202
3404 15
75894785 16588


Satellite: ISS
Catalog Number: 25544
Epoch time:      07204
95212677   =   yrday
fracday
Element set:     900
Inclination:       51
6343  deg
RA of node:       273
8003  deg
Eccentricity:     
0009121     
Arg of perigee:   157
8157  deg
Mean anomaly:     202
3404  deg
Mean motion:   15
75894785  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1658
Checksum:              291


Coasting Arc #2 (Orbit 1673)
---------------------------------------

Vector Time (GMT): 2007/205/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4185973
73                 A    =         6714627
83  meter
 Y    =         488197
87  meter          E    =           
0019597
 Z    =       -5242442
99                 I    =           51
29348
 XDOT =       -523
575582                 Wp   =          114
01340
 YDOT =      -7667
395910  meter/sec      RA   =          267
91429  deg
 ZDOT =       -304
712755                 TA   =          153
12735
                                          MA   =          153
02571
                                          Ha   =            189
558  n
mi
                                          Hp   =            178
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13733509
63                 X    =        -4165655
00
 Y    =        1601699
06  feet           Y    =          441502
38  meter
 Z    =      -17199616
10                 Z    =        -5262728
93
 XDOT =      -1717
767659                 XDOT =        -436
318485
 YDOT =     -25155
498394  feet/sec       YDOT =       -7672
762901  meter/sec
 ZDOT =       -999
713764                 ZDOT =        -307
045511

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4775947
59                 X    =        -1455708
82
 Y    =      -12873233
34  feet           Y    =        -3923761
52  meter
 Z    =      -17276333
77                 Z    =        -5265826
53
 XDOT =      23101
467204                 XDOT =        7041
327204
 YDOT =      -7254
310370  feet/sec       YDOT =       -2211
113801  meter/sec
 ZDOT =      -1009
421338                 ZDOT =        -307
671624


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07205
96672694  
00020000  00000-0  20000-3 0  9013
2 25544  51
6349 268
5740 0009068 161
4354 198
7143 15
75934828 16742


Satellite: ISS
Catalog Number: 25544
Epoch time:      07205
96672694   =   yrday
fracday
Element set:     901
Inclination:       51
6349  deg
RA of node:       268
5740  deg
Eccentricity:     
0009068     
Arg of perigee:   161
4354  deg
Mean anomaly:     198
7143  deg
Mean motion:   15
75934828  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1674
Checksum:              327


Coasting Arc #3 (Orbit 1689)
---------------------------------------

Vector Time (GMT): 2007/206/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         527231
97                 A    =         6726690
49  meter
 Y    =        6682749
68  meter          E    =           
0019984
 Z    =        -401550
23                 I    =           51
33625
 XDOT =      -4838
483910                 Wp   =          150
44114
 YDOT =         29
628855  meter/sec      RA   =          262
74190  deg
 ZDOT =      -6003
474448                 TA   =           33
95077
                                          MA   =           33
82304
                                          Ha   =            189
520  n
mi
                                          Hp   =            179
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1729763
68                 X    =          454415
94
 Y    =       21925031
75  feet           Y    =         6688238
41  meter
 Z    =       -1317422
02                 Z    =         -399164
71
 XDOT =     -15874
291043                 XDOT =       -4809
292045
 YDOT =         97
207530  feet/sec       YDOT =         -24
313569  meter/sec
 ZDOT =     -19696
438479                 ZDOT =       -6026
908722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20773993
59                 X    =        -6331913
25
 Y    =        7222604
15  feet           Y    =         2201449
74  meter
 Z    =       -1307623
70                 Z    =         -398563
70
 XDOT =      -3551
933974                 XDOT =       -1082
629475
 YDOT =     -13712
274733  feet/sec       YDOT =       -4179
501339  meter/sec
 ZDOT =     -19785
131222                 ZDOT =       -6030
507996


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07206
98131308  
00020000  00000-0  20000-3 0  9029
2 25544  51
6349 263
3481 0009159 165
9169 194
2252 15
75908551 16905


Satellite: ISS
Catalog Number: 25544
Epoch time:      07206
98131308   =   yrday
fracday
Element set:     902
Inclination:       51
6349  deg
RA of node:       263
3481  deg
Eccentricity:     
0009159     
Arg of perigee:   165
9169  deg
Mean anomaly:     194
2252  deg
Mean motion:   15
75908551  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1690
Checksum:              306


Coasting Arc #4 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2007/207/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4303153
00                 A    =         6714847
92  meter
 Y    =         420015
04  meter          E    =           
0008083
 Z    =        5132383
13                 I    =           51
30206
 XDOT =        687
366113                 Wp   =          143
36743
 YDOT =       7583
827297  meter/sec      RA   =          257
55426  deg
 ZDOT =      -1202
376557                 TA   =          318
12926
                                          MA   =          318
19105
                                          Ha   =            189
085  n
mi
                                          Hp   =            179
413

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14117956
03                 X    =         4273204
61
 Y    =        1378002
09  feet           Y    =          467966
98  meter
 Z    =       16838527
33                 Z    =         5153214
94
 XDOT =       2255
138167                 XDOT =         608
352410
 YDOT =      24881
323153  feet/sec       YDOT =        7591
072231  meter/sec
 ZDOT =      -3944
804978                 ZDOT =       -1199
227986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2450463
58                 X    =          746901
30
 Y    =       13876143
86  feet           Y    =         4229448
65  meter
 Z    =       16917429
90                 Z    =         5156432
63
 XDOT =     -22336
356139                 XDOT =       -6808
121351
 YDOT =       8716
661395  feet/sec       YDOT =        2656
838393  meter/sec
 ZDOT =      -3932
008003                 ZDOT =       -1198
476039


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07207
99588136  
00020000  00000-0  20000-3 0  9037
2 25544  51
6346 258
1222 0008890 170
2329 189
9010 15
76008090 17066


Satellite: ISS
Catalog Number: 25544
Epoch time:      07207
99588136   =   yrday
fracday
Element set:     903
Inclination:       51
6346  deg
RA of node:       258
1222  deg
Eccentricity:     
0008890     
Arg of perigee:   170
2329  deg
Mean anomaly:     189
9010  deg
Mean motion:   15
76008090  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1706
Checksum:              295


Coasting Arc #5 (Orbit 1721)
---------------------------------------

Vector Time (GMT): 2007/208/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -632917
75                 A    =         6725293
05  meter
 Y    =       -6476478
71  meter          E    =           
0013978
 Z    =        1693090
39                 I    =           51
34419
 XDOT =       5091
423039                 Wp   =          100
86529
 YDOT =       1000
801128  meter/sec      RA   =          252
40650  deg
 ZDOT =       5689
273426                 TA   =          277
94537
                                          MA   =          278
10399
                                          Ha   =            189
124  n
mi
                                          Hp   =            179
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2076501
79                 X    =         -568674
36
 Y    =      -21248289
72  feet           Y    =        -6483197
43  meter
 Z    =        5554758
50                 Z    =         1690170
69
 XDOT =      16704
143830                 XDOT =        5052
216530
 YDOT =       3283
468268  feet/sec       YDOT =        1057
516116  meter/sec
 ZDOT =      18665
595229                 ZDOT =        5713
912091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19758856
68                 X    =         6022499
52
 Y    =       -8094462
83  feet           Y    =        -2467192
27  meter
 Z    =        5542947
96                 Z    =         1689490
54
 XDOT =       1009
045088                 XDOT =         307
556943
 YDOT =      15404
240996  feet/sec       YDOT =        4695
212656  meter/sec
 ZDOT =      18758
985989                 ZDOT =        5717
738929


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07209
01043814  
00020000  00000-0  20000-3 0  9042
2 25544  51
6343 252
8956 0008801 173
6803 186
4474 15
75986863 17220


Satellite: ISS
Catalog Number: 25544
Epoch time:      07209
01043814   =   yrday
fracday
Element set:     904
Inclination:       51
6343  deg
RA of node:       252
8956  deg
Eccentricity:     
0008801     
Arg of perigee:   173
6803  deg
Mean anomaly:     186
4474  deg
Mean motion:   15
75986863  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1722
Checksum:              304


Coasting Arc #6 (Orbit 1736)
---------------------------------------

Vector Time (GMT): 2007/209/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4631140
29                 A    =         6716719
97  meter
 Y    =       -1306647
50  meter          E    =           
0016614
 Z    =       -4700909
84                 I    =           51
32523
 XDOT =       -696
072677                 Wp   =          138
52418
 YDOT =      -7178
215587  meter/sec      RA   =          247
19637  deg
 ZDOT =       2674
097958                 TA   =          157
95515
                                          MA   =          157
88361
                                          Ha   =            188
919  n
mi
                                          Hp   =            179
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15194029
82                 X    =        -4593349
28
 Y    =       -4286901
25  feet           Y    =        -1358223
50  meter
 Z    =      -15422932
55                 Z    =        -4723315
86
 XDOT =      -2283
703008                 XDOT =        -628
743087
 YDOT =     -23550
576074  feet/sec       YDOT =       -7185
623411  meter/sec
 ZDOT =       8773
287263                 ZDOT =        2670
878957

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -481280
43                 X    =         -146694
28
 Y    =      -15696361
48  feet           Y    =        -4784250
98  meter
 Z    =      -15507917
93                 Z    =        -4726813
39
 XDOT =      20598
553766                 XDOT =        6278
439188
 YDOT =      -9308
829125  feet/sec       YDOT =       -2837
331117  meter/sec
 ZDOT =       8760
249993                 ZDOT =        2670
124198


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07209
96156984  
00020000  00000-0  20000-3 0  9050
2 25544  51
6339 247
9956 0008782 177
9473 182
1728 15
76021679 17375


Satellite: ISS
Catalog Number: 25544
Epoch time:      07209
96156984   =   yrday
fracday
Element set:     905
Inclination:       51
6339  deg
RA of node:       247
9956  deg
Eccentricity:     
0008782     
Arg of perigee:   177
9473  deg
Mean anomaly:     182
1728  deg
Mean motion:   15
76021679  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1737
Checksum:              347


Coasting Arc #7 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2007/210/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         527760
27                 A    =         6722696
82  meter
 Y    =        6016786
29  meter          E    =           
0011249
 Z    =       -2941801
79                 I    =           51
35699
 XDOT =      -5543
124873                 Wp   =          160
36906
 YDOT =      -1944
054275  meter/sec      RA   =          242
06900  deg
 ZDOT =      -4986
507973                 TA   =           53
73060
                                          MA   =           53
62672
                                          Ha   =            188
811  n
mi
                                          Hp   =            180
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1731496
95                 X    =          474730
85
 Y    =       19740112
50  feet           Y    =         6022391
88  meter
 Z    =       -9651580
67                 Z    =        -2939366
03
 XDOT =     -18186
105227                 XDOT =       -5496
751227
 YDOT =      -6378
130825  feet/sec       YDOT =       -2005
780692  meter/sec
 ZDOT =     -16359
934295                 ZDOT =       -5013
323440

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18141836
09                 X    =        -5529631
64
 Y    =        7983469
61  feet           Y    =         2433361
54  meter
 Z    =       -9641635
17                 Z    =        -2938770
40
 XDOT =        861
290235                 XDOT =         262
521263
 YDOT =     -17860
320577  feet/sec       YDOT =       -5443
825712  meter/sec
 ZDOT =     -16461
702780                 ZDOT =       -5017
527007


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07210
97609676  
00020000  00000-0  20000-3 0  9065
2 25544  51
6333 242
7692 0008846 182
6269 177
4850 15
76008756 17538


Satellite: ISS
Catalog Number: 25544
Epoch time:      07210
97609676   =   yrday
fracday
Element set:     906
Inclination:       51
6333  deg
RA of node:       242
7692  deg
Eccentricity:     
0008846     
Arg of perigee:   182
6269  deg
Mean anomaly:     177
4850  deg
Mean motion:   15
76008756  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1753
Checksum:              325


Coasting Arc #8 (Orbit 1768)
---------------------------------------

Vector Time (GMT): 2007/211/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5060543
05                 A    =         6719391
84  meter
 Y    =        2016853
58  meter          E    =           
0011812
 Z    =        3920197
89                 I    =           51
36154
 XDOT =        478
086374                 Wp   =          123
28917
 YDOT =       6576
147675  meter/sec      RA   =          236
84675  deg
 ZDOT =      -3998
185237                 TA   =            8
31170
                                          MA   =            8
29216
                                          Ha   =            188
376  n
mi
                                          Hp   =            180
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16602831
54                 X    =         5018571
05
 Y    =        6616973
70  feet           Y    =         2073208
36  meter
 Z    =       12861541
62                 Z    =         3944679
65
 XDOT =       1568
524849                 XDOT =         423
937369
 YDOT =      21575
287649  feet/sec       YDOT =        6581
191537  meter/sec
 ZDOT =     -13117
405632                 ZDOT =       -3995
993628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -697897
20                 X    =         -212719
07
 Y    =       17791898
12  feet           Y    =         5422970
55  meter
 Z    =       12954493
80                 Z    =         3948529
71
 XDOT =     -18481
681425                 XDOT =       -5633
216498
 YDOT =       8824
698954  feet/sec       YDOT =        2689
768241  meter/sec
 ZDOT =     -13108
304721                 ZDOT =       -3995
411279


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07211
99060743  
00020000  00000-0  20000-3 0  9075
2 25544  51
6332 237
5420 0008594 186
3759 173
7298 15
76101634 17694


Satellite: ISS
Catalog Number: 25544
Epoch time:      07211
99060743   =   yrday
fracday
Element set:     907
Inclination:       51
6332  deg
RA of node:       237
5420  deg
Eccentricity:     
0008594     
Arg of perigee:   186
3759  deg
Mean anomaly:     173
7298  deg
Mean motion:   15
76101634  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1769
Checksum:              311


Coasting Arc #9 (Orbit 1784)
---------------------------------------

Vector Time (GMT): 2007/212/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -229428
97                 A    =         6719468
25  meter
 Y    =       -5414591
55  meter          E    =           
0014128
 Z    =        3972423
56                 I    =           51
37700
 XDOT =       6077
836529                 Wp   =          138
95613
 YDOT =       2637
385943  meter/sec      RA   =          231
72667  deg
 ZDOT =       3927
497678                 TA   =          270
21785
                                          MA   =          270
37974
                                          Ha   =            188
462  n
mi
                                          Hp   =            180
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -752719
73                 X    =         -188162
04
 Y    =      -17764407
99  feet           Y    =        -5416926
70  meter
 Z    =       13032885
69                 Z    =         3971408
87
 XDOT =      19940
408560                 XDOT =        6028
814532
 YDOT =       8652
841020  feet/sec       YDOT =        2705
077363  meter/sec
 ZDOT =      12885
491071                 ZDOT =        3956
904257

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16343571
65                 X    =         4981520
64
 Y    =       -7010423
30  feet           Y    =        -2136777
02  meter
 Z    =       13028373
58                 Z    =         3971048
27
 XDOT =      -1637
438775                 XDOT =        -499
091339
 YDOT =      20449
195835  feet/sec       YDOT =        6232
914891  meter/sec
 ZDOT =      12997
179644                 ZDOT =        3961
540356


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07213
00510651  
00020000  00000-0  20000-3 0  9088
2 25544  51
6322 232
3141 0008575 189
8925 170
2072 15
76056107 17852


Satellite: ISS
Catalog Number: 25544
Epoch time:      07213
00510651   =   yrday
fracday
Element set:     908
Inclination:       51
6322  deg
RA of node:       232
3141  deg
Eccentricity:     
0008575     
Arg of perigee:   189
8925  deg
Mean anomaly:     170
2072  deg
Mean motion:   15
76056107  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1785
Checksum:              272


Coasting Arc #10 (Orbit 1799)
---------------------------------------

Vector Time (GMT): 2007/213/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5540933
08                 A    =         6722569
64  meter
 Y    =       -2528961
98  meter          E    =           
0006769
 Z    =       -2855555
64                 I    =           51
40643
 XDOT =         46
177607                 Wp   =          163
04976
 YDOT =      -5806
572461  meter/sec      RA   =          226
50616  deg
 ZDOT =       5049
490614                 TA   =          164
05415
                                          MA   =          164
03283
                                          Ha   =            188
263  n
mi
                                          Hp   =            180
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18178914
29                 X    =        -5498370
52
 Y    =       -8297119
37  feet           Y    =        -2590685
70  meter
 Z    =       -9368620
85                 Z    =        -2882369
74
 XDOT =        151
501334                 XDOT =          86
575059
 YDOT =     -19050
434583  feet/sec       YDOT =       -5805
830445  meter/sec
 ZDOT =      16566
570255                 ZDOT =        5049
812786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1062442
07                 X    =          323832
34
 Y    =      -19906462
88  feet           Y    =        -6067489
89  meter
 Z    =       -9470486
98                 Z    =        -2886604
43
 XDOT =      16289
899209                 XDOT =        4965
161279
 YDOT =      -7017
558928  feet/sec       YDOT =       -2138
951961  meter/sec
 ZDOT =      16567
064209                 ZDOT =        5049
641171


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07213
95618290  
00020000  00000-0  20000-3 0  9091
2 25544  51
6316 227
4128 0008703 194
3239 165
7680 15
76102160 18000


Satellite: ISS
Catalog Number: 25544
Epoch time:      07213
95618290   =   yrday
fracday
Element set:     909
Inclination:       51
6316  deg
RA of node:       227
4128  deg
Eccentricity:     
0008703     
Arg of perigee:   194
3239  deg
Mean anomaly:     165
7680  deg
Mean motion:   15
76102160  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1800
Checksum:              283


Coasting Arc #11 (Orbit 1815)
---------------------------------------

Vector Time (GMT): 2007/214/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -388444
48                 A    =         6716249
94  meter
 Y    =        4724412
58  meter          E    =           
0009534
 Z    =       -4763112
04                 I    =           51
40505
 XDOT =      -6577
513901                 Wp   =          119
34879
 YDOT =      -3093
128994  meter/sec      RA   =          221
38102  deg
 ZDOT =      -2539
995917                 TA   =          125
72940
                                          MA   =          125
64067
                                          Ha   =            188
072  n
mi
                                          Hp   =            180
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1274424
16                 X    =         -418106
65
 Y    =       15500041
27  feet           Y    =         4719903
11  meter
 Z    =      -15627008
01                 Z    =        -4765070
95
 XDOT =     -21579
770015                 XDOT =       -6530
098535
 YDOT =     -10148
061005  feet/sec       YDOT =       -3166
417250  meter/sec
 ZDOT =      -8333
319938                 ZDOT =       -2571
834029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14772187
17                 X    =        -4502562
65
 Y    =        4841962
56  feet           Y    =         1475830
19  meter
 Z    =      -15633831
92                 Z    =        -4765191
97
 XDOT =       1477
589835                 XDOT =         450
369382
 YDOT =     -22700
395366  feet/sec       YDOT =       -6919
080508  meter/sec
 ZDOT =      -8454
291448                 ZDOT =       -2576
868033


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07214
97065135  
00020000  00000-0  20000-3 0  9100
2 25544  51
6307 222
1851 0008694 198
0526 162
0331 15
76121361 18168


Satellite: ISS
Catalog Number: 25544
Epoch time:      07214
97065135   =   yrday
fracday
Element set:     910
Inclination:       51
6307  deg
RA of node:       222
1851  deg
Eccentricity:     
0008694     
Arg of perigee:   198
0526  deg
Mean anomaly:     162
0331  deg
Mean motion:   15
76121361  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1816
Checksum:              270


Coasting Arc #12 (Orbit 1831)
---------------------------------------

Vector Time (GMT): 2007/215/22:48:27
915
Vector Time (MET): N/A
Weight (LBS)     : 509098
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5904947
70                 A    =         6724903
32  meter
 Y    =        2799789
50  meter          E    =           
0017120
 Z    =        1538812
94                 I    =           51
45844
 XDOT =       -884
778738                 Wp   =          147
51031
 YDOT =       5043
607158  meter/sec      RA   =          216
17924  deg
 ZDOT =      -5766
062990                 TA   =           15
44978
                                          MA   =           15
39758
                                          Ha   =            187
744  n
mi
                                          Hp   =            180
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19373188
00                 X    =         5865725
95
 Y    =        9185661
09  feet           Y    =         2865602
58  meter
 Z    =        5048598
88                 Z    =         1567403
83
 XDOT =      -2902
817382                 XDOT =        -913
101046
 YDOT =      16547
267579  feet/sec       YDOT =        5033
554956  meter/sec
 ZDOT =     -18917
529494                 ZDOT =       -5770
429790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -705773
45                 X    =         -215119
75
 Y    =       21403034
36  feet           Y    =         6523644
87  meter
 Z    =        5157241
27                 Z    =         1571927
14
 XDOT =     -14728
529586                 XDOT =       -4489
255818
 YDOT =       4088
346270  feet/sec       YDOT =        1246
127943  meter/sec
 ZDOT =     -18933
431441                 ZDOT =       -5770
909903


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   07215
98510400  
00020000  00000-0  20000-3 0  9113
2 25544  51
6317 216
9580 0008567 202
4523 157
6268 15
76182676 18328


Satellite: ISS
Catalog Number: 25544
Epoch time:      07215
98510400   =   yrday
fracday
Element set:     911
Inclination:       51
6317  deg
RA of node:       216
9580  deg
Eccentricity:     
0008567     
Arg of perigee:   202
4523  deg
Mean anomaly:     157
6268  deg
Mean motion:   15
76182676  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1832
Checksum:              293

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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