Date: July 24th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 1120)
---------------------------------------

Vector Time (GMT): 2009/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4900436
76                 A    =         6732337
81  meter
 Y    =        4599614
81  meter          E    =           
0008286
 Z    =         289528
92                 I    =           51
89357
 XDOT =      -3063
533187                 Wp   =           24
75357
 YDOT =      -3648
160790  meter/sec      RA   =          134
87752  deg
 ZDOT =       6050
111717                 TA   =          338
38188
                                          MA   =          338
41684
                                          Ha   =            188
214  n
mi
                                          Hp   =            186
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16077548
41                 X    =        -4952912
68
 Y    =       15090599
77  feet           Y    =         4544521
79  meter
 Z    =         949898
03                 Z    =          265596
34
 XDOT =     -10050
961900                 XDOT =       -3051
901071
 YDOT =     -11969
031463  feet/sec       YDOT =       -3682
355115  meter/sec
 ZDOT =      19849
447890                 ZDOT =        6035
256845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20828959
99                 X    =         6348667
00
 Y    =        7248282
04  feet           Y    =         2209276
37  meter
 Z    =         856097
98                 Z    =          260938
66
 XDOT =      -5359
110414                 XDOT =       -1633
456854
 YDOT =      13039
184495  feet/sec       YDOT =        3974
343434  meter/sec
 ZDOT =      19790
870319                 ZDOT =        6032
257273


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   09201
56299492  
00010596  00000-0  82463-4 0  9008
2 25544  51
6381 135
5004 0006095 260
6257  99
4217 15
73933536 11214


Satellite: ISS
Catalog Number: 25544
Epoch time:      09201
56299492   =   yrday
fracday
Element set:     900
Inclination:       51
6381  deg
RA of node:       135
5004  deg
Eccentricity:     
0006095     
Arg of perigee:   260
6257  deg
Mean anomaly:      99
4217  deg
Mean motion:   15
73933536  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1121
Checksum:              302


Coasting Arc #2 (Orbit 1135)
---------------------------------------

Vector Time (GMT): 2009/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2949707
14                 A    =         6720265
15  meter
 Y    =        2937716
21  meter          E    =           
0009011
 Z    =       -5283195
43                 I    =           51
87434
 XDOT =      -5114
955500                 Wp   =           97
95727
 YDOT =       5738
656312  meter/sec      RA   =          129
75431  deg
 ZDOT =        334
462141                 TA   =          175
21456
                                          MA   =          175
20594
                                          Ha   =            188
043  n
mi
                                          Hp   =            186
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9677516
88                 X    =         2942302
15
 Y    =        9638176
53  feet           Y    =         2970661
05  meter
 Z    =      -17333318
35                 Z    =        -5268883
53
 XDOT =     -16781
350065                 XDOT =       -5180
370703
 YDOT =      18827
612573  feet/sec       YDOT =        5681
092074  meter/sec
 ZDOT =       1097
316737                 ZDOT =         309
456279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3776267
54                 X    =         1151006
35
 Y    =      -13200039
14  feet           Y    =        -4023371
93  meter
 Z    =      -17276905
83                 Z    =        -5266000
90
 XDOT =      23605
908193                 XDOT =        7195
080817
 YDOT =       5442
005950  feet/sec       YDOT =        1658
723414  meter/sec
 ZDOT =        999
346677                 ZDOT =         304
600867


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   09202
51537098  
00010596  00000-0  82463-4 0  9012
2 25544  51
6392 130
6099 0006094 264
5447  95
5021 15
73952286 11368


Satellite: ISS
Catalog Number: 25544
Epoch time:      09202
51537098   =   yrday
fracday
Element set:     901
Inclination:       51
6392  deg
RA of node:       130
6099  deg
Eccentricity:     
0006094     
Arg of perigee:   264
5447  deg
Mean anomaly:      95
5021  deg
Mean motion:   15
73952286  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1136
Checksum:              310


Coasting Arc #3 (Orbit 1151)
---------------------------------------

Vector Time (GMT): 2009/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4011093
44                 A    =         6732271
95  meter
 Y    =       -5391276
52  meter          E    =           
0008978
 Z    =        -300257
98                 I    =           51
93375
 XDOT =       3653
088747                 Wp   =          168
30801
 YDOT =       3052
807329  meter/sec      RA   =          124
64375  deg
 ZDOT =      -6053
558129                 TA   =           14
94231
                                          MA   =           14
91580
                                          Ha   =            187
995  n
mi
                                          Hp   =            186
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13159755
38                 X    =         4072540
07
 Y    =      -17687915
10  feet           Y    =        -5346078
52  meter
 Z    =        -985098
35                 Z    =         -280624
06
 XDOT =      11985
199302                 XDOT =        3648
086603
 YDOT =      10015
772076  feet/sec       YDOT =        3093
631180  meter/sec
 ZDOT =     -19860
755015                 ZDOT =       -6035
823577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21882762
74                 X    =        -6669866
08
 Y    =       -2707722
54  feet           Y    =         -825313
83  meter
 Z    =        -908215
18                 Z    =         -276823
99
 XDOT =       2532
113264                 XDOT =         771
788123
 YDOT =     -13872
995621  feet/sec       YDOT =       -4228
489065  meter/sec
 ZDOT =     -19790
874621                 ZDOT =       -6032
258585


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   09203
53122854  
00010596  00000-0  82463-4 0  9026
2 25544  51
6400 125
3936 0006101 267
9550  92
0915 15
73954804 11520


Satellite: ISS
Catalog Number: 25544
Epoch time:      09203
53122854   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       125
3936  deg
Eccentricity:     
0006101     
Arg of perigee:   267
9550  deg
Mean anomaly:      92
0915  deg
Mean motion:   15
73954804  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1152
Checksum:              286


Coasting Arc #4 (Orbit 1167)
---------------------------------------

Vector Time (GMT): 2009/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3409471
35                 A    =         6720071
61  meter
 Y    =       -2381322
99  meter          E    =           
0003910
 Z    =        5281938
01                 I    =           51
90899
 XDOT =       4027
946552                 Wp   =          284
07551
 YDOT =      -6551
373551  meter/sec      RA   =          119
52293  deg
 ZDOT =       -352
900473                 TA   =          169
26764
                                          MA   =          169
25929
                                          Ha   =            187
924  n
mi
                                          Hp   =            186
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11185929
63                 X    =        -3408247
66
 Y    =       -7812739
46  feet           Y    =        -2419443
41  meter
 Z    =       17329192
95                 Z    =         5265377
92
 XDOT =      13215
047744                 XDOT =        4102
620050
 YDOT =     -21494
007714  feet/sec       YDOT =       -6505
913135  meter/sec
 ZDOT =      -1157
809952                 ZDOT =        -333
152497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -980984
01                 X    =         -299003
93
 Y    =       13691537
99  feet           Y    =         4173180
78  meter
 Z    =       17263959
73                 Z    =         5262054
93
 XDOT =     -24232
672391                 XDOT =       -7386
118545
 YDOT =       -370
809025  feet/sec       YDOT =        -113
022591  meter/sec
 ZDOT =      -1080
536702                 ZDOT =        -329
347587


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   09204
54707305  
00010596  00000-0  82463-4 0  9039
2 25544  51
6398 120
1773 0006248 272
6388  87
4060 15
74021240 11688


Satellite: ISS
Catalog Number: 25544
Epoch time:      09204
54707305   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       120
1773  deg
Eccentricity:     
0006248     
Arg of perigee:   272
6388  deg
Mean anomaly:      87
4060  deg
Mean motion:   15
74021240  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1168
Checksum:              297


Coasting Arc #5 (Orbit 1183)
---------------------------------------

Vector Time (GMT): 2009/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3004033
17                 A    =         6732161
10  meter
 Y    =        6009018
78  meter          E    =           
0009916
 Z    =         321799
17                 I    =           51
96320
 XDOT =      -4119
014439                 Wp   =           20
50162
 YDOT =      -2385
936862  meter/sec      RA   =          114
41384  deg
 ZDOT =       6054
902860                 TA   =          342
98110
                                          MA   =          343
01434
                                          Ha   =            188
041  n
mi
                                          Hp   =            186
072

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9855751
86                 X    =        -3072566
98
 Y    =       19714628
54  feet           Y    =         5975042
70  meter
 Z    =        1055771
56                 Z    =          307039
89
 XDOT =     -13513
826900                 XDOT =       -4121
441349
 YDOT =      -7827
876843  feet/sec       YDOT =       -2432
012140  meter/sec
 ZDOT =      19865
166862                 ZDOT =        6034
887029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21959639
70                 X    =         6693298
18
 Y    =       -1922275
62  feet           Y    =         -585909
61  meter
 Z    =         998076
77                 Z    =          304213
80
 XDOT =        328
368726                 XDOT =         100
086788
 YDOT =      14108
710324  feet/sec       YDOT =        4300
334907  meter/sec
 ZDOT =      19786
343086                 ZDOT =        6030
877373


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   09205
56290963  
00010596  00000-0  82463-4 0  9040
2 25544  51
6399 114
9599 0006161 277
3256  82
7207 15
73992391 11848


Satellite: ISS
Catalog Number: 25544
Epoch time:      09205
56290963   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       114
9599  deg
Eccentricity:     
0006161     
Arg of perigee:   277
3256  deg
Mean anomaly:      82
7207  deg
Mean motion:   15
73992391  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1184
Checksum:              338


Coasting Arc #6 (Orbit 1198)
---------------------------------------

Vector Time (GMT): 2009/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3760932
01                 A    =         6720047
08  meter
 Y    =        1781045
16  meter          E    =           
0008912
 Z    =       -5284163
55                 I    =           51
93447
 XDOT =      -2829
272093                 Wp   =           87
71456
 YDOT =       7144
856355  meter/sec      RA   =          109
29349  deg
 ZDOT =        395
418398                 TA   =          186
02245
                                          MA   =          186
03317
                                          Ha   =            188
139  n
mi
                                          Hp   =            186
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12339015
78                 X    =         3766405
63
 Y    =        5843324
01  feet           Y    =         1823133
05  meter
 Z    =      -17336494
59                 Z    =        -5265879
83
 XDOT =      -9282
388757                 XDOT =       -2910
877659
 YDOT =      23441
129772  feet/sec       YDOT =        7112
761470  meter/sec
 ZDOT =       1297
304454                 ZDOT =         381
476260

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1771006
54                 X    =         -539802
79
 Y    =      -13629011
51  feet           Y    =        -4154122
71  meter
 Z    =      -17264511
92                 Z    =        -5262223
23
 XDOT =      23762
315583                 XDOT =        7242
753790
 YDOT =      -4658
356212  feet/sec       YDOT =       -1419
866973  meter/sec
 ZDOT =       1242
879663                 ZDOT =         378
829721


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   09206
51524387  
00010596  00000-0  82463-4 0  9057
2 25544  51
6404 110
0691 0006167 280
7544  79
2925 15
74034382 11991


Satellite: ISS
Catalog Number: 25544
Epoch time:      09206
51524387   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       110
0691  deg
Eccentricity:     
0006167     
Arg of perigee:   280
7544  deg
Mean anomaly:      79
2925  deg
Mean motion:   15
74034382  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1199
Checksum:              308


Coasting Arc #7 (Orbit 1214)
---------------------------------------

Vector Time (GMT): 2009/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1930125
74                 A    =         6732088
32  meter
 Y    =       -6433577
64  meter          E    =           
0007257
 Z    =        -376690
75                 I    =           51
98344
 XDOT =       4452
478434                 Wp   =          166
85119
 YDOT =       1688
348691  meter/sec      RA   =          104
18693  deg
 ZDOT =      -6051
125579                 TA   =           17
22441
                                          MA   =           17
19979
                                          Ha   =            188
253  n
mi
                                          Hp   =            186
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6332433
52                 X    =         2003753
52
 Y    =      -21107538
20  feet           Y    =        -6411582
15  meter
 Z    =       -1235862
04                 Z    =         -367135
87
 XDOT =      14607
868878                 XDOT =        4462
663046
 YDOT =       5539
201741  feet/sec       YDOT =        1738
196236  meter/sec
 ZDOT =     -19852
774208                 ZDOT =       -6029
470844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21094829
74                 X    =        -6429704
10
 Y    =        6381744
05  feet           Y    =         1945155
59  meter
 Z    =       -1198640
58                 Z    =         -365345
65
 XDOT =      -3055
271827                 XDOT =        -931
246853
 YDOT =     -13793
232679  feet/sec       YDOT =       -4204
177321  meter/sec
 ZDOT =     -19767
541825                 ZDOT =       -6025
146748


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   09207
53105759  
00010596  00000-0  82463-4 0  9069
2 25544  51
6404 104
8519 0006217 283
4904  76
5566 15
74010144 12157


Satellite: ISS
Catalog Number: 25544
Epoch time:      09207
53105759   =   yrday
fracday
Element set:     906
Inclination:       51
6404  deg
RA of node:       104
8519  deg
Eccentricity:     
0006217     
Arg of perigee:   283
4904  deg
Mean anomaly:      76
5566  deg
Mean motion:   15
74010144  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1215
Checksum:              296


Coasting Arc #8 (Orbit 1230)
---------------------------------------

Vector Time (GMT): 2009/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3997537
71                 A    =         6719911
86  meter
 Y    =       -1164104
58  meter          E    =           
0004590
 Z    =        5277839
64                 I    =           51
94928
 XDOT =       1570
517171                 Wp   =          309
75962
 YDOT =      -7522
452566  meter/sec      RA   =           99
06606  deg
 ZDOT =       -467
042977                 TA   =          144
67388
                                          MA   =          144
64345
                                          Ha   =            188
479  n
mi
                                          Hp   =            185
959

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13115281
22                 X    =        -4009861
98
 Y    =       -3819240
75  feet           Y    =        -1208876
67  meter
 Z    =       17315746
84                 Z    =         5258389
73
 XDOT =       5152
615390                 XDOT =        1656
786589
 YDOT =     -24679
962488  feet/sec       YDOT =       -7504
407733  meter/sec
 ZDOT =      -1532
293233                 ZDOT =        -459
204442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4346163
22                 X    =         1324710
55
 Y    =       13051925
71  feet           Y    =         3978226
95  meter
 Z    =       17239210
85                 Z    =         5254511
47
 XDOT =     -22305
215064                 XDOT =       -6798
629552
 YDOT =       9422
444033  feet/sec       YDOT =        2871
960941  meter/sec
 ZDOT =      -1501
867888                 ZDOT =        -457
769332


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   09208
54685775  
00010596  00000-0  82463-4 0  9073
2 25544  51
6404  99
6344 0006369 288
5232  71
5239 15
74089102 12312


Satellite: ISS
Catalog Number: 25544
Epoch time:      09208
54685775   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:        99
6344  deg
Eccentricity:     
0006369     
Arg of perigee:   288
5232  deg
Mean anomaly:      71
5239  deg
Mean motion:   15
74089102  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1231
Checksum:              325


Coasting Arc #9 (Orbit 1246)
---------------------------------------

Vector Time (GMT): 2009/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -808104
06                 A    =         6731873
84  meter
 Y    =        6660878
18  meter          E    =           
0011647
 Z    =         442820
22                 I    =           51
99321
 XDOT =      -4670
824628                 Wp   =           20
23129
 YDOT =       -971
185429  meter/sec      RA   =           93
96103  deg
 ZDOT =       6048
491862                 TA   =          344
56292
                                          MA   =          344
59841
                                          Ha   =            188
690  n
mi
                                          Hp   =            185
939

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2651260
03                 X    =         -884678
20
 Y    =       21853274
88  feet           Y    =         6651413
30  meter
 Z    =        1452822
25                 Z    =          438709
03
 XDOT =     -15324
227783                 XDOT =       -4688
999840
 YDOT =      -3186
303900  feet/sec       YDOT =       -1023
519453  meter/sec
 ZDOT =      19844
133404                 ZDOT =        6025
756888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19331825
21                 X    =         5892340
32
 Y    =      -10531907
29  feet           Y    =        -3210125
34  meter
 Z    =        1436996
21                 Z    =          437996
44
 XDOT =       5609
133092                 XDOT =        1709
663766
 YDOT =      13007
601929  feet/sec       YDOT =        3964
717068  meter/sec
 ZDOT =      19754
689171                 ZDOT =        6021
229259


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   09209
56264936  
00010596  00000-0  82463-4 0  9089
2 25544  51
6406  94
4167 0006400 293
0424  67
0064 15
74078650 12479


Satellite: ISS
Catalog Number: 25544
Epoch time:      09209
56264936   =   yrday
fracday
Element set:     908
Inclination:       51
6406  deg
RA of node:        94
4167  deg
Eccentricity:     
0006400     
Arg of perigee:   293
0424  deg
Mean anomaly:      67
0064  deg
Mean motion:   15
74078650  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1247
Checksum:              308


Coasting Arc #10 (Orbit 1261)
---------------------------------------

Vector Time (GMT): 2009/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4139238
70                 A    =         6719886
40  meter
 Y    =         534244
31  meter          E    =           
0009248
 Z    =       -5274305
28                 I    =           51
95398
 XDOT =       -281
651057                 Wp   =           78
82383
 YDOT =       7669
441074  meter/sec      RA   =           88
83907  deg
 ZDOT =        558
386183                 TA   =          196
44818
                                          MA   =          196
47821
                                          Ha   =            188
874  n
mi
                                          Hp   =            185
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13580179
46                 X    =         4158578
55
 Y    =        1752770
06  feet           Y    =          580640
36  meter
 Z    =      -17304151
19                 Z    =        -5254149
93
 XDOT =       -924
052025                 XDOT =        -370
103651
 YDOT =      25162
208247  feet/sec       YDOT =        7665
796867  meter/sec
 ZDOT =       1831
975665                 ZDOT =         556
803837

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6730097
60                 X    =        -2051333
75
 Y    =      -12038969
10  feet           Y    =        -3669477
78  meter
 Z    =      -17224869
66                 Z    =        -5250140
27
 XDOT =      19903
411885                 XDOT =        6066
559943
 YDOT =     -13727
153143  feet/sec       YDOT =       -4184
036278  meter/sec
 ZDOT =       1826
131608                 ZDOT =         556
604914


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   09210
51494309  
00010596  00000-0  82463-4 0  9096
2 25544  51
6407  89
5254 0006474 296
7642  63
2858 15
74109826 12621


Satellite: ISS
Catalog Number: 25544
Epoch time:      09210
51494309   =   yrday
fracday
Element set:     909
Inclination:       51
6407  deg
RA of node:        89
5254  deg
Eccentricity:     
0006474     
Arg of perigee:   296
7642  deg
Mean anomaly:      63
2858  deg
Mean motion:   15
74109826  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1262
Checksum:              327


Coasting Arc #11 (Orbit 1277)
---------------------------------------

Vector Time (GMT): 2009/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -308720
26                 A    =         6731851
84  meter
 Y    =       -6699438
24  meter          E    =           
0005468
 Z    =        -542568
11                 I    =           51
99232
 XDOT =       4773
484935                 Wp   =          163
03476
 YDOT =        267
094696  meter/sec      RA   =           83
73668  deg
 ZDOT =      -6034
348237                 TA   =           22
83927
                                          MA   =           22
81495
                                          Ha   =            188
966  n
mi
                                          Hp   =            185
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1012861
76                 X    =         -231147
37
 Y    =      -21979784
26  feet           Y    =        -6702456
74  meter
 Z    =       -1780079
11                 Z    =         -543880
20
 XDOT =      15661
039812                 XDOT =        4799
457054
 YDOT =        876
294936  feet/sec       YDOT =         320
620506  meter/sec
 ZDOT =     -19797
730435                 ZDOT =       -6011
095667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16829538
62                 X    =        -5129643
37
 Y    =       14173351
66  feet           Y    =         4320037
58  meter
 Z    =       -1785558
54                 Z    =         -544238
24
 XDOT =      -7873
441203                 XDOT =       -2399
824879
 YDOT =     -11823
231109  feet/sec       YDOT =       -3603
720842  meter/sec
 ZDOT =     -19706
278454                 ZDOT =       -6006
473673


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   09211
53071379  
00010596  00000-0  82463-4 0  9109
2 25544  51
6409  84
3086 0006449 299
0821  60
9696 15
74067850 12787


Satellite: ISS
Catalog Number: 25544
Epoch time:      09211
53071379   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:        84
3086  deg
Eccentricity:     
0006449     
Arg of perigee:   299
0821  deg
Mean anomaly:      60
9696  deg
Mean motion:   15
74067850  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1278
Checksum:              326


Coasting Arc #12 (Orbit 1293)
---------------------------------------

Vector Time (GMT): 2009/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4185833
86                 A    =         6719860
80  meter
 Y    =          67411
20  meter          E    =           
0005783
 Z    =        5259358
13                 I    =           51
94812
 XDOT =       -986
472639                 Wp   =          331
32371
 YDOT =      -7605
111743  meter/sec      RA   =           78
61192  deg
 ZDOT =       -682
986098                 TA   =          125
17166
                                          MA   =          125
11748
                                          Ha   =            189
208  n
mi
                                          Hp   =            185
546

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13733050
72                 X    =        -4211825
35
 Y    =         221165
36  feet           Y    =           20456
78  meter
 Z    =       17255111
97                 Z    =         5238960
40
 XDOT =      -3236
458789                 XDOT =        -898
039869
 YDOT =     -24951
154014  feet/sec       YDOT =       -7615
648520  meter/sec
 ZDOT =      -2240
768037                 ZDOT =        -687
564486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8780479
06                 X    =         2676290
02
 Y    =       10691612
16  feet           Y    =         3258803
38  meter
 Z    =       17174897
45                 Z    =         5234908
74
 XDOT =     -16747
920058                 XDOT =       -5104
766034
 YDOT =      17407
892306  feet/sec       YDOT =        5305
925575  meter/sec
 ZDOT =      -2259
125770                 ZDOT =        -688
581535


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   09212
54647117  
00010596  00000-0  82463-4 0  9111
2 25544  51
6410  79
0908 0006592 304
3179  55
7360 15
74137927 12949


Satellite: ISS
Catalog Number: 25544
Epoch time:      09212
54647117   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:        79
0908  deg
Eccentricity:     
0006592     
Arg of perigee:   304
3179  deg
Mean anomaly:      55
7360  deg
Mean motion:   15
74137927  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1294
Checksum:              310


Coasting Arc #13 (Orbit 1309)
---------------------------------------

Vector Time (GMT): 2009/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1404958
72                 A    =         6731534
74  meter
 Y    =        6542014
99  meter          E    =           
0013374
 Z    =         652030
48                 I    =           51
97991
 XDOT =      -4785
800818                 Wp   =           22
90535
 YDOT =        424
560001  meter/sec      RA   =           73
50979  deg
 ZDOT =       6023
486098                 TA   =          344
16638
                                          MA   =          344
20815
                                          Ha   =            189
290  n
mi
                                          Hp   =            185
388

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4609444
62                 X    =         1328532
96
 Y    =       21463303
77  feet           Y    =         6557298
66  meter
 Z    =        2139207
62                 Z    =          658670
89
 XDOT =     -15701
446252                 XDOT =       -4819
453277
 YDOT =       1392
913390  feet/sec       YDOT =         370
853437  meter/sec
 ZDOT =      19762
093497                 ZDOT =        6000
155271

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13648770
62                 X    =         4160145
28
 Y    =      -17190629
69  feet           Y    =        -5239703
93  meter
 Z    =        2165619
79                 Z    =          660080
91
 XDOT =       9874
522493                 XDOT =        3009
754456
 YDOT =      10329
860332  feet/sec       YDOT =        3148
541429  meter/sec
 ZDOT =      19670
354202                 ZDOT =        5995
523961


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   09213
56221849  
00010596  00000-0  82463-4 0  9125
2 25544  51
6403  73
8728 0006669 307
9320  52
1240 15
74160985 13102


Satellite: ISS
Catalog Number: 25544
Epoch time:      09213
56221849   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:        73
8728  deg
Eccentricity:     
0006669     
Arg of perigee:   307
9320  deg
Mean anomaly:      52
1240  deg
Mean motion:   15
74160985  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1310
Checksum:              297


Coasting Arc #14 (Orbit 1324)
---------------------------------------

Vector Time (GMT): 2009/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4155512
86                 A    =         6719835
06  meter
 Y    =        -667852
55  meter          E    =           
0010013
 Z    =       -5246356
94                 I    =           51
92989
 XDOT =       2210
042009                 Wp   =           73
39789
 YDOT =       7324
523379  meter/sec      RA   =           68
38117  deg
 ZDOT =        822
202418                 TA   =          204
37912
                                          MA   =          204
42651
                                          Ha   =            189
491  n
mi
                                          Hp   =            185
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13633572
38                 X    =         4188157
50
 Y    =       -2191117
30  feet           Y    =         -621199
99  meter
 Z    =      -17212457
16                 Z    =        -5226090
57
 XDOT =       7250
793992                 XDOT =        2123
979634
 YDOT =      24030
588513  feet/sec       YDOT =        7348
756061  meter/sec
 ZDOT =       2697
514496                 ZDOT =         832
730508

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10577470
95                 X    =        -3224013
15
 Y    =       -9029345
09  feet           Y    =        -2752144
38  meter
 Z    =      -17132775
84                 Z    =        -5222070
07
 XDOT =      12934
825674                 XDOT =        3942
534865
 YDOT =     -20324
642524  feet/sec       YDOT =       -6194
951041  meter/sec
 ZDOT =       2739
248740                 ZDOT =         834
923016


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   09214
51447280  
00010596  00000-0  82463-4 0  9131
2 25544  51
6393  68
9806 0006715 311
9280  48
1310 15
74172695 13254


Satellite: ISS
Catalog Number: 25544
Epoch time:      09214
51447280   =   yrday
fracday
Element set:     913
Inclination:       51
6393  deg
RA of node:        68
9806  deg
Eccentricity:     
0006715     
Arg of perigee:   311
9280  deg
Mean anomaly:      48
1310  deg
Mean motion:   15
74172695  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1325
Checksum:              305


Coasting Arc #15 (Orbit 1340)
---------------------------------------

Vector Time (GMT): 2009/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 672678
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2434326
62                 A    =         6731450
62  meter
 Y    =       -6222920
37  meter          E    =           
0003740
 Z    =        -796783
17                 I    =           51
95667
 XDOT =       4708
595940                 Wp   =          151
10825
 YDOT =      -1076
450429  meter/sec      RA   =           63
28133  deg
 ZDOT =      -5993
345757                 TA   =           37
53859
                                          MA   =           37
51248
                                          Ha   =            189
584  n
mi
                                          Hp   =            185
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7986635
88                 X    =        -2360689
38
 Y    =      -20416405
41  feet           Y    =        -6249730
62  meter
 Z    =       -2614118
00                 Z    =         -808430
75
 XDOT =      15448
149410                 XDOT =        4749
397075
 YDOT =      -3531
661512  feet/sec       YDOT =       -1023
567331  meter/sec
 ZDOT =     -19663
207864                 ZDOT =       -5970
372849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10031488
93                 X    =        -3057597
83
 Y    =       19486972
83  feet           Y    =         5939629
32  meter
 Z    =       -2660205
92                 Z    =         -810830
76
 XDOT =     -11525
505730                 XDOT =       -3512
974146
 YDOT =      -8598
507264  feet/sec       YDOT =       -2620
825014  meter/sec
 ZDOT =     -19572
894085                 ZDOT =       -5965
818117


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   09215
53020012  
00010596  00000-0  82463-4 0  9145
2 25544  51
6392  63
7637 0006720 315
1025  44
9594 15
74153124 13419


Satellite: ISS
Catalog Number: 25544
Epoch time:      09215
53020012   =   yrday
fracday
Element set:     914
Inclination:       51
6392  deg
RA of node:        63
7637  deg
Eccentricity:     
0006720     
Arg of perigee:   315
1025  deg
Mean anomaly:      44
9594  deg
Mean motion:   15
74153124  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:            1341
Checksum:              274

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics 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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