Date: June 19th 2009

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 600)
---------------------------------------

Vector Time (GMT): 2009/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4426313
14                 A    =         6721677
83  meter
 Y    =         644554
01  meter          E    =           
0014162
 Z    =        5009375
92                 I    =           51
35110
 XDOT =      -3023
802445                 Wp   =          124
45424
 YDOT =       6863
159771  meter/sec      RA   =          304
70177  deg
 ZDOT =       1777
296789                 TA   =          308
30905
                                          MA   =          308
43631
                                          Ha   =            193
301  n
mi
                                          Hp   =            181
234

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14522024
74                 X    =         4394441
76
 Y    =        2114678
51  feet           Y    =          693872
78  meter
 Z    =       16434960
36                 Z    =         5030801
83
 XDOT =      -9920
611695                 XDOT =       -3108
956597
 YDOT =      22516
928382  feet/sec       YDOT =        6828
869492  meter/sec
 ZDOT =       5831
026212                 ZDOT =        1762
401054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3336918
91                 X    =         1017092
88
 Y    =      -14193614
87  feet           Y    =        -4326213
81  meter
 Z    =       16518936
37                 Z    =         5034971
81
 XDOT =      20551
597130                 XDOT =        6264
126805
 YDOT =      11594
005171  feet/sec       YDOT =        3533
852776  meter/sec
 ZDOT =       5772
963215                 ZDOT =        1759
599188


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   09168
55063554  
00010596  00000-0  82463-4 0  9007
2 25544  51
6412 305
0379 0008829 124
5735 235
6262 15
73804412  6010


Satellite: ISS
Catalog Number: 25544
Epoch time:      09168
55063554   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:       305
0379  deg
Eccentricity:     
0008829     
Arg of perigee:   124
5735  deg
Mean anomaly:     235
6262  deg
Mean motion:   15
73804412  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             601
Checksum:              297


Coasting Arc #2 (Orbit 615)
---------------------------------------

Vector Time (GMT): 2009/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2042219
81                 A    =         6731642
23  meter
 Y    =       -6211983
36  meter          E    =           
0012002
 Z    =       -1606096
93                 I    =           51
36937
 XDOT =       5134
311183                 Wp   =           85
00113
 YDOT =        217
558045  meter/sec      RA   =          299
51847  deg
 ZDOT =       5724
791224                 TA   =          257
22036
                                          MA   =          257
35451
                                          Ha   =            193
427  n
mi
                                          Hp   =            181
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6700196
22                 X    =         2119333
70
 Y    =      -20380522
85  feet           Y    =        -6188714
66  meter
 Z    =       -5269346
88                 Z    =        -1595989
30
 XDOT =      16844
852962                 XDOT =        5103
686458
 YDOT =        713
773115  feet/sec       YDOT =         274
800835  meter/sec
 ZDOT =      18782
123439                 ZDOT =        5749
659679

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19875060
90                 X    =        -6057918
56
 Y    =       -8102669
34  feet           Y    =        -2469693
62  meter
 Z    =       -5230015
40                 Z    =        -1594108
69
 XDOT =       1261
029813                 XDOT =         384
361887
 YDOT =     -15198
782842  feet/sec       YDOT =       -4632
589010  meter/sec
 ZDOT =      18879
569659                 ZDOT =        5754
492832


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   09169
50310762  
00010596  00000-0  82463-4 0  9010
2 25544  51
6420 300
1485 0008893 127
3522 232
8452 15
73796153  6167


Satellite: ISS
Catalog Number: 25544
Epoch time:      09169
50310762   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:       300
1485  deg
Eccentricity:     
0008893     
Arg of perigee:   127
3522  deg
Mean anomaly:     232
8452  deg
Mean motion:   15
73796153  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             616
Checksum:              297


Coasting Arc #3 (Orbit 631)
---------------------------------------

Vector Time (GMT): 2009/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4503000
51                 A    =         6721744
29  meter
 Y    =         236710
28  meter          E    =           
0019670
 Z    =       -5000956
08                 I    =           51
32288
 XDOT =       1667
515032                 Wp   =           97
35698
 YDOT =      -7271
208574  meter/sec      RA   =          294
39389  deg
 ZDOT =      -1854
363784                 TA   =          154
69199
                                          MA   =          154
59551
                                          Ha   =            193
266  n
mi
                                          Hp   =            181
257

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14773623
71                 X    =        -4481018
69
 Y    =         776608
54  feet           Y    =          186478
88  meter
 Z    =      -16407336
21                 Z    =        -5022778
52
 XDOT =       5470
849844                 XDOT =        1757
707272
 YDOT =     -23855
671174  feet/sec       YDOT =       -7252
056833  meter/sec
 ZDOT =      -6083
870683                 ZDOT =       -1846
045068

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          27993
47                 X    =            8532
41
 Y    =       14698622
60  feet           Y    =         4480140
17  meter
 Z    =      -16492830
86                 Z    =        -5027014
85
 XDOT =     -22472
662431                 XDOT =       -6849
667509
 YDOT =      -6715
560366  feet/sec       YDOT =       -2046
902800  meter/sec
 ZDOT =      -6051
592521                 ZDOT =       -1844
525401


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   09170
51906250  
00010596  00000-0  82463-4 0  9027
2 25544  51
6422 294
9328 0008758 131
1132 229
0789 15
73817693  6327


Satellite: ISS
Catalog Number: 25544
Epoch time:      09170
51906250   =   yrday
fracday
Element set:     902
Inclination:       51
6422  deg
RA of node:       294
9328  deg
Eccentricity:     
0008758     
Arg of perigee:   131
1132  deg
Mean anomaly:     229
0789  deg
Mean motion:   15
73817693  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             632
Checksum:              314


Coasting Arc #4 (Orbit 647)
---------------------------------------

Vector Time (GMT): 2009/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -857289
84                 A    =         6731499
18  meter
 Y    =        6458618
02  meter          E    =           
0022645
 Z    =        1644248
28                 I    =           51
34487
 XDOT =      -5114
137804                 Wp   =          123
32353
 YDOT =        787
144329  meter/sec      RA   =          289
20681  deg
 ZDOT =      -5714
103774                 TA   =           38
41561
                                          MA   =           38
25458
                                          Ha   =            193
220  n
mi
                                          Hp   =            181
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2812630
70                 X    =         -937435
04
 Y    =       21189691
66  feet           Y    =         6448582
85  meter
 Z    =        5394515
35                 Z    =         1639890
15
 XDOT =     -16778
667335                 XDOT =       -5094
801280
 YDOT =       2582
494519  feet/sec       YDOT =         730
064329  meter/sec
 ZDOT =     -18747
059626                 ZDOT =       -5738
901429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21081815
47                 X    =         6425737
35
 Y    =        3556953
69  feet           Y    =         1084159
48  meter
 Z    =        5377718
56                 Z    =         1639128
62
 XDOT =       2277
849259                 XDOT =         694
288454
 YDOT =      15209
848920  feet/sec       YDOT =        4635
961951  meter/sec
 ZDOT =     -18844
193534                 ZDOT =       -5743
710189


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   09171
53500344  
00010596  00000-0  82463-4 0  9035
2 25544  51
6424 289
7165 0008823 134
9555 225
2325 15
73830111  6484


Satellite: ISS
Catalog Number: 25544
Epoch time:      09171
53500344   =   yrday
fracday
Element set:     903
Inclination:       51
6424  deg
RA of node:       289
7165  deg
Eccentricity:     
0008823     
Arg of perigee:   134
9555  deg
Mean anomaly:     225
2325  deg
Mean motion:   15
73830111  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             648
Checksum:              299


Coasting Arc #5 (Orbit 663)
---------------------------------------

Vector Time (GMT): 2009/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4382550
58                 A    =         6721615
54  meter
 Y    =       -1133209
58  meter          E    =           
0014318
 Z    =        4962609
70                 I    =           51
30461
 XDOT =       -274
668457                 Wp   =          132
76879
 YDOT =       7454
881811  meter/sec      RA   =          284
08152  deg
 ZDOT =       1931
757236                 TA   =          298
42423
                                          MA   =          298
56845
                                          Ha   =            192
918  n
mi
                                          Hp   =            181
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14378446
79                 X    =         4370788
98
 Y    =       -3717879
19  feet           Y    =        -1084268
22  meter
 Z    =       16281527
89                 Z    =         4983871
46
 XDOT =       -901
143230                 XDOT =        -367
393986
 YDOT =      24458
273659  feet/sec       YDOT =        7451
291415  meter/sec
 ZDOT =       6337
786206                 ZDOT =        1930
199343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3480957
07                 X    =        -1060995
71
 Y    =      -14343180
00  feet           Y    =        -4371801
26  meter
 Z    =       16364798
61                 Z    =         4987990
62
 XDOT =      23393
620325                 XDOT =        7130
375475
 YDOT =       1595
944233  feet/sec       YDOT =         486
443802  meter/sec
 ZDOT =       6332
005792                 ZDOT =        1929
995365


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   09172
55092786  
00010596  00000-0  82463-4 0  9045
2 25544  51
6433 284
5009 0008665 138
6271 221
5550 15
73900421  6643


Satellite: ISS
Catalog Number: 25544
Epoch time:      09172
55092786   =   yrday
fracday
Element set:     904
Inclination:       51
6433  deg
RA of node:       284
5009  deg
Eccentricity:     
0008665     
Arg of perigee:   138
6271  deg
Mean anomaly:     221
5550  deg
Mean motion:   15
73900421  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             664
Checksum:              308


Coasting Arc #6 (Orbit 678)
---------------------------------------

Vector Time (GMT): 2009/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -367997
40                 A    =         6731277
91  meter
 Y    =       -6502569
62  meter          E    =           
0010075
 Z    =       -1710391
41                 I    =           51
33090
 XDOT =       4877
473584                 Wp   =           93
04323
 YDOT =      -1762
884559  meter/sec      RA   =          278
89268  deg
 ZDOT =       5681
025312                 TA   =          247
97172
                                          MA   =          248
07878
                                          Ha   =            192
989  n
mi
                                          Hp   =            181
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1207340
57                 X    =         -286948
45
 Y    =      -21333889
84  feet           Y    =        -6506231
21  meter
 Z    =       -5611520
36                 Z    =        -1711983
81
 XDOT =      16002
209920                 XDOT =        4869
226569
 YDOT =      -5783
741990  feet/sec       YDOT =       -1708
389256  meter/sec
 ZDOT =      18638
534487                 ZDOT =        5704
699632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21333199
13                 X    =        -6502359
10
 Y    =        1189047
40  feet           Y    =          362421
65  meter
 Z    =       -5618048
47                 Z    =        -1712381
17
 XDOT =      -5707
354698                 XDOT =       -1739
601712
 YDOT =     -14334
192971  feet/sec       YDOT =       -4369
062018  meter/sec
 ZDOT =      18731
240648                 ZDOT =        5709
282150


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   09173
50334673  
00010596  00000-0  82463-4 0  9056
2 25544  51
6434 279
6116 0008515 140
9938 219
1841 15
73864554  6796


Satellite: ISS
Catalog Number: 25544
Epoch time:      09173
50334673   =   yrday
fracday
Element set:     905
Inclination:       51
6434  deg
RA of node:       279
6116  deg
Eccentricity:     
0008515     
Arg of perigee:   140
9938  deg
Mean anomaly:     219
1841  deg
Mean motion:   15
73864554  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             679
Checksum:              332


Coasting Arc #7 (Orbit 694)
---------------------------------------

Vector Time (GMT): 2009/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4117977
99                 A    =         6721663
88  meter
 Y    =        1909248
24  meter          E    =           
0017866
 Z    =       -4971550
32                 I    =           51
29522
 XDOT =      -1076
775622                 Wp   =          102
06953
 YDOT =      -7360
657603  meter/sec      RA   =          273
76702  deg
 ZDOT =      -1944
420190                 TA   =          149
07479
                                          MA   =          148
96945
                                          Ha   =            192
832  n
mi
                                          Hp   =            181
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13510426
49                 X    =        -4114870
77
 Y    =        6263937
80  feet           Y    =         1863217
12  meter
 Z    =      -16310860
62                 Z    =        -4991547
33
 XDOT =      -3532
728419                 XDOT =        -984
941903
 YDOT =     -24149
139116  feet/sec       YDOT =       -7372
184822  meter/sec
 ZDOT =      -6379
331331                 ZDOT =       -1949
429750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6502401
66                 X    =         1981932
03
 Y    =       13301394
39  feet           Y    =         4054265
01  meter
 Z    =      -16389154
80                 Z    =        -4995414
38
 XDOT =     -23112
971332                 XDOT =       -7044
833662
 YDOT =       3452
498323  feet/sec       YDOT =        1052
321489  meter/sec
 ZDOT =      -6399
300592                 ZDOT =       -1950
506820


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   09174
51924521  
00010596  00000-0  82463-4 0  9066
2 25544  51
6433 274
3959 0008516 145
6421 214
5295 15
73891373  6951


Satellite: ISS
Catalog Number: 25544
Epoch time:      09174
51924521   =   yrday
fracday
Element set:     906
Inclination:       51
6433  deg
RA of node:       274
3959  deg
Eccentricity:     
0008516     
Arg of perigee:   145
6421  deg
Mean anomaly:     214
5295  deg
Mean motion:   15
73891373  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             695
Checksum:              327


Coasting Arc #8 (Orbit 710)
---------------------------------------

Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1516345
25                 A    =         6731168
21  meter
 Y    =        6321492
69  meter          E    =           
0021849
 Z    =        1697817
51                 I    =           51
32589
 XDOT =      -4492
730104                 Wp   =          127
82026
 YDOT =       2616
358900  meter/sec      RA   =          268
57751  deg
 ZDOT =      -5692
456026                 TA   =           33
29467
                                          MA   =           33
15742
                                          Ha   =            192
774  n
mi
                                          Hp   =            181
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4974885
98                 X    =         1437296
96
 Y    =       20739805
41  feet           Y    =         6338007
02  meter
 Z    =        5570267
44                 Z    =         1704993
12
 XDOT =     -14739
928162                 XDOT =       -4494
000204
 YDOT =       8583
854659  feet/sec       YDOT =        2566
112639  meter/sec
 ZDOT =     -18676
036830                 ZDOT =       -5714
283978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20553827
96                 X    =         6264806
76
 Y    =       -5666717
88  feet           Y    =        -1727215
61  meter
 Z    =        5598692
96                 Z    =         1706481
62
 XDOT =       8678
100980                 XDOT =        2645
085179
 YDOT =      12822
402035  feet/sec       YDOT =        3908
268140  meter/sec
 ZDOT =     -18761
480016                 ZDOT =       -5718
499109


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   09175
53513038  
00010596  00000-0  82463-4 0  9077
2 25544  51
6425 269
1805 0008601 148
4119 211
7562 15
73911740  7110


Satellite: ISS
Catalog Number: 25544
Epoch time:      09175
53513038   =   yrday
fracday
Element set:     907
Inclination:       51
6425  deg
RA of node:       269
1805  deg
Eccentricity:     
0008601     
Arg of perigee:   148
4119  deg
Mean anomaly:     211
7562  deg
Mean motion:   15
73911740  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             711
Checksum:              297


Coasting Arc #9 (Orbit 726)
---------------------------------------

Vector Time (GMT): 2009/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3693010
78                 A    =         6721456
91  meter
 Y    =       -2636765
01  meter          E    =           
0013881
 Z    =        4954204
80                 I    =           51
29590
 XDOT =       2390
967564                 Wp   =          140
92988
 YDOT =       7056
973031  meter/sec      RA   =          263
45087  deg
 ZDOT =       1959
994227                 TA   =          289
96996
                                          MA   =          290
11941
                                          Ha   =            192
497  n
mi
                                          Hp   =            181
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12116177
10                 X    =         3698154
79
 Y    =       -8650803
84  feet           Y    =        -2595439
72  meter
 Z    =       16253952
75                 Z    =         4972157
21
 XDOT =       7844
381771                 XDOT =        2302
356438
 YDOT =      23152
798657  feet/sec       YDOT =        7083
214432  meter/sec
 ZDOT =       6430
427254                 ZDOT =        1971
395385

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9266865
26                 X    =        -2824540
53
 Y    =      -11553125
62  feet           Y    =        -3521392
69  meter
 Z    =       16324203
85                 Z    =         4975617
33
 XDOT =      21870
878176                 XDOT =        6666
243668
 YDOT =      -8330
305948  feet/sec       YDOT =       -2539
077253  meter/sec
 ZDOT =       6475
468631                 ZDOT =        1973
722839


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   09176
55099923  
00010596  00000-0  82463-4 0  9083
2 25544  51
6426 263
9640 0008430 152
5755 207
5854 15
73976865  7275


Satellite: ISS
Catalog Number: 25544
Epoch time:      09176
55099923   =   yrday
fracday
Element set:     908
Inclination:       51
6426  deg
RA of node:       263
9640  deg
Eccentricity:     
0008430     
Arg of perigee:   152
5755  deg
Mean anomaly:     207
5854  deg
Mean motion:   15
73976865  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             727
Checksum:              348


Coasting Arc #10 (Orbit 741)
---------------------------------------

Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2633084
36                 A    =         6731057
05  meter
 Y    =       -5957912
03  meter          E    =           
0008196
 Z    =       -1706775
22                 I    =           51
33191
 XDOT =       3944
904682                 Wp   =           99
91368
 YDOT =      -3364
958004  meter/sec      RA   =          258
26075  deg
 ZDOT =       5682
090506                 TA   =          241
14293
                                          MA   =          241
22521
                                          Ha   =            192
490  n
mi
                                          Hp   =            182
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8638728
22                 X    =        -2557975
19
 Y    =      -19546955
48  feet           Y    =        -5986936
51  meter
 Z    =       -5599656
22                 Z    =        -1719385
01
 XDOT =      12942
600663                 XDOT =        3954
636835
 YDOT =     -11039
888466  feet/sec       YDOT =       -3320
790201  meter/sec
 ZDOT =      18642
029219                 ZDOT =        5701
277733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18902429
30                 X    =        -5761460
45
 Y    =        9942320
22  feet           Y    =         3030419
20  meter
 Z    =       -5649396
34                 Z    =        -1721936
00
 XDOT =     -11178
908960                 XDOT =       -3407
331451
 YDOT =     -10658
343621  feet/sec       YDOT =       -3248
663136  meter/sec
 ZDOT =      18717
084249                 ZDOT =        5704
967279


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   09177
50336640  
00010596  00000-0  82463-4 0  9090
2 25544  51
6419 259
0742 0008178 155
5107 204
6446 15
73937285  7424


Satellite: ISS
Catalog Number: 25544
Epoch time:      09177
50336640   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       259
0742  deg
Eccentricity:     
0008178     
Arg of perigee:   155
5107  deg
Mean anomaly:     204
6446  deg
Mean motion:   15
73937285  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             742
Checksum:              324


Coasting Arc #11 (Orbit 757)
---------------------------------------

Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3196811
63                 A    =         6721421
17  meter
 Y    =        3205226
09  meter          E    =           
0016206
 Z    =       -4980448
32                 I    =           51
30592
 XDOT =      -3581
748328                 Wp   =          106
12684
 YDOT =      -6531
014927  meter/sec      RA   =          253
13408  deg
 ZDOT =      -1913
679196                 TA   =          145
33475
                                          MA   =          145
22901
                                          Ha   =            192
339  n
mi
                                          Hp   =            182
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10488227
15                 X    =        -3208221
56
 Y    =       10515833
63  feet           Y    =         3169414
32  meter
 Z    =      -16340053
55                 Z    =        -4996005
58
 XDOT =     -11751
142807                 XDOT =       -3499
154996
 YDOT =     -21427
214328  feet/sec       YDOT =       -6570
606081  meter/sec
 ZDOT =      -6278
475053                 ZDOT =       -1930
879378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11375834
48                 X    =         3467354
35
 Y    =        9443751
46  feet           Y    =         2878455
44  meter
 Z    =      -16400883
03                 Z    =        -4998989
15
 XDOT =     -19644
067351                 XDOT =       -5987
511729
 YDOT =      12695
985360  feet/sec       YDOT =        3869
736338  meter/sec
 ZDOT =      -6346
254699                 ZDOT =       -1934
338432


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   09178
51921109  
00010596  00000-0  82463-4 0  9104
2 25544  51
6409 253
8574 0008252 159
6086 200
5408 15
73968868  7583


Satellite: ISS
Catalog Number: 25544
Epoch time:      09178
51921109   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:       253
8574  deg
Eccentricity:     
0008252     
Arg of perigee:   159
6086  deg
Mean anomaly:     200
5408  deg
Mean motion:   15
73968868  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             758
Checksum:              337


Coasting Arc #12 (Orbit 773)
---------------------------------------

Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3616347
97                 A    =         6730914
78  meter
 Y    =        5417633
92  meter          E    =           
0020605
 Z    =        1647233
99                 I    =           51
34841
 XDOT =      -3324
192923                 Wp   =          132
61712
 YDOT =       3965
963083  meter/sec      RA   =          247
94486  deg
 ZDOT =      -5714
371202                 TA   =           29
08649
                                          MA   =           28
97186
                                          Ha   =            192
146  n
mi
                                          Hp   =            182
287

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11864658
68                 X    =         3547496
37
 Y    =       17774389
50  feet           Y    =         5457688
87  meter
 Z    =        5404311
00                 Z    =         1664635
53
 XDOT =     -10906
144759                 XDOT =       -3340
534724
 YDOT =      13011
689906  feet/sec       YDOT =        3928
699336  meter/sec
 ZDOT =     -18747
937013                 ZDOT =       -5730
559247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16451606
24                 X    =         5014449
58
 Y    =      -13612435
44  feet           Y    =        -4149070
32  meter
 Z    =        5472830
96                 Z    =         1668118
88
 XDOT =      13068
207433                 XDOT =        3983
189625
 YDOT =       8189
939220  feet/sec       YDOT =        2496
293474  meter/sec
 ZDOT =     -18811
198059                 ZDOT =       -5733
653169


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   09179
53504240  
00010596  00000-0  82463-4 0  9111
2 25544  51
6410 248
6406 0008123 162
0457 198
0995 15
74020370  7746


Satellite: ISS
Catalog Number: 25544
Epoch time:      09179
53504240   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:       248
6406  deg
Eccentricity:     
0008123     
Arg of perigee:   162
0457  deg
Mean anomaly:     198
0995  deg
Mean motion:   15
74020370  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             774
Checksum:              297


Coasting Arc #13 (Orbit 789)
---------------------------------------

Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2589733
07                 A    =         6721167
59  meter
 Y    =       -3688529
37  meter          E    =           
0012899
 Z    =        4983702
48                 I    =           51
32809
 XDOT =       4676
182753                 Wp   =          149
57004
 YDOT =       5828
504007  meter/sec      RA   =          242
81862  deg
 ZDOT =       1870
760007                 TA   =          282
23449
                                          MA   =          282
37892
                                          Ha   =            192
002  n
mi
                                          Hp   =            182
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8496499
58                 X    =         2606576
48
 Y    =      -12101474
31  feet           Y    =        -3659475
90  meter
 Z    =       16350729
93                 Z    =         4996323
84
 XDOT =      15341
806931                 XDOT =        4601
572090
 YDOT =      19122
388476  feet/sec       YDOT =        5880
378416  meter/sec
 ZDOT =       6137
664064                 ZDOT =        1893
296357

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13027389
41                 X    =        -3970748
29
 Y    =       -6878154
09  feet           Y    =        -2096461
37  meter
 Z    =       16400020
62                 Z    =         4998726
29
 XDOT =      16632
115407                 XDOT =        5069
468776
 YDOT =     -16553
666405  feet/sec       YDOT =       -5045
557520  meter/sec
 ZDOT =       6226
347446                 ZDOT =        1897
790702


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   09180
55085990  
00010596  00000-0  82463-4 0  9122
2 25544  51
6410 243
4236 0008098 166
6442 193
4937 15
74044717  7909


Satellite: ISS
Catalog Number: 25544
Epoch time:      09180
55085990   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:       243
4236  deg
Eccentricity:     
0008098     
Arg of perigee:   166
6442  deg
Mean anomaly:     193
4937  deg
Mean motion:   15
74044717  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             790
Checksum:              321


Coasting Arc #14 (Orbit 804)
---------------------------------------

Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4515043
84                 A    =         6730942
63  meter
 Y    =       -4730806
76  meter          E    =           
0006446
 Z    =       -1602995
58                 I    =           51
37513
 XDOT =       2610
777543                 Wp   =          103
37228
 YDOT =      -4425
592377  meter/sec      RA   =          237
63136  deg
 ZDOT =       5725
182231                 TA   =          238
88550
                                          MA   =          238
94876
                                          Ha   =            191
943  n
mi
                                          Hp   =            182
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14813135
94                 X    =        -4454020
51
 Y    =      -15521019
57  feet           Y    =        -4780955
21  meter
 Z    =       -5259171
84                 Z    =        -1624782
11
 XDOT =       8565
543120                 XDOT =        2632
259295
 YDOT =     -14519
660030  feet/sec       YDOT =       -4396
277800  meter/sec
 ZDOT =      18783
406269                 ZDOT =        5737
916987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13335226
54                 X    =        -4064577
05
 Y    =       16780766
20  feet           Y    =         5114777
54  meter
 Z    =       -5344862
21                 Z    =        -1629114
00
 XDOT =     -14322
726923                 XDOT =       -4365
567166
 YDOT =      -5401
675672  feet/sec       YDOT =       -1646
430745  meter/sec
 ZDOT =      18833
102948                 ZDOT =        5740
329778


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   09181
50317879  
00010596  00000-0  82463-4 0  9133
2 25544  51
6405 238
5327 0007903 169
4489 190
6841 15
74025064  8059


Satellite: ISS
Catalog Number: 25544
Epoch time:      09181
50317879   =   yrday
fracday
Element set:     913
Inclination:       51
6405  deg
RA of node:       238
5327  deg
Eccentricity:     
0007903     
Arg of perigee:   169
4489  deg
Mean anomaly:     190
6841  deg
Mean motion:   15
74025064  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             805
Checksum:              322


Coasting Arc #15 (Orbit 820)
---------------------------------------

Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 686867
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1983245
62                 A    =         6721027
18  meter
 Y    =        4013369
81  meter          E    =           
0014787
 Z    =       -5023905
06                 I    =           51
35907
 XDOT =      -5596
951133                 Wp   =          109
10291
 YDOT =      -4970
475521  meter/sec      RA   =          232
50548  deg
 ZDOT =      -1770
231247                 TA   =          143
81071
                                          MA   =          143
71057
                                          Ha   =            191
803  n
mi
                                          Hp   =            182
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6506711
34                 X    =        -2003571
11
 Y    =       13167223
80  feet           Y    =         3991079
12  meter
 Z    =      -16482628
13                 Z    =        -5033588
45
 XDOT =     -18362
700567                 XDOT =       -5532
354963
 YDOT =     -16307
334385  feet/sec       YDOT =       -5032
702456  meter/sec
 ZDOT =      -5807
845298                 ZDOT =       -1797
265173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14000893
75                 X    =         4267472
41
 Y    =        4294413
67  feet           Y    =         1308937
29  meter
 Z    =      -16520384
10                 Z    =        -5035413
07
 XDOT =     -12959
089231                 XDOT =       -3949
930398
 YDOT =      19612
011932  feet/sec       YDOT =        5977
741237  meter/sec
 ZDOT =      -5914
133937                 ZDOT =       -1802
628024


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   09182
51897297  
00010596  00000-0  82463-4 0  9143
2 25544  51
6407 233
3153 0007964 172
8525 187
2754 15
74049783  8214


Satellite: ISS
Catalog Number: 25544
Epoch time:      09182
51897297   =   yrday
fracday
Element set:     914
Inclination:       51
6407  deg
RA of node:       233
3153  deg
Eccentricity:     
0007964     
Arg of perigee:   172
8525  deg
Mean anomaly:     187
2754  deg
Mean motion:   15
74049783  rev/day
Decay rate:    1
05960E-04  rev/day^2
Epoch rev:             821
Checksum:              337

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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