Date: March 22nd 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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


083/09:34:24 264 2 0 3 9 3 9
N/A -3 4 -0 4 192 0
000/00:08:48 528 0 1 0 3 182 7

Coasting Arc #1 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2010/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6458701
24                 A    =         6730661
02  meter
 Y    =        -867847
26  meter          E    =           
0021641
 Z    =        1639718
98                 I    =           51
55359
 XDOT =       -783
116464                 Wp   =           60
43713
 YDOT =       5091
660470  meter/sec      RA   =          340
82412  deg
 ZDOT =       5733
544586                 TA   =          317
71612
                                          MA   =          317
88277
                                          Ha   =            192
465  n
mi
                                          Hp   =            181
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21189964
70                 X    =         6459960
19
 Y    =       -2847267
91  feet           Y    =         -795615
00  meter
 Z    =        5379655
45                 Z    =         1671098
44
 XDOT =      -2569
279736                 XDOT =        -867
846591
 YDOT =      16704
922802  feet/sec       YDOT =        5082
430080  meter/sec
 ZDOT =      18810
841816                 ZDOT =        5729
533841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21337577
39                 X    =         6503693
59
 Y    =        -687913
78  feet           Y    =         -209676
12  meter
 Z    =        5504252
64                 Z    =         1677696
21
 XDOT =      -4409
479655                 XDOT =       -1344
009399
 YDOT =      14791
726546  feet/sec       YDOT =        4508
518251  meter/sec
 ZDOT =      18795
023215                 ZDOT =        5728
723076


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   10076
56021846  
00016717  00000-0  10270-3 0  9003
2 25544  51
6475 341
0180 0007593  54
9708 305
2167 15
74105643  9047


Satellite: ISS
Catalog Number: 25544
Epoch time:      10076
56021846   =   yrday
fracday
Element set:     900
Inclination:       51
6475  deg
RA of node:       341
0180  deg
Eccentricity:     
0007593     
Arg of perigee:    54
9708  deg
Mean anomaly:     305
2167  deg
Mean motion:   15
74105643  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             904
Checksum:              294


Coasting Arc #2 (Orbit 918)
---------------------------------------

Vector Time (GMT): 2010/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 784184
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         358115
50                 A    =         6720946
90  meter
 Y    =       -4513695
42  meter          E    =           
0018888
 Z    =       -4982829
43                 I    =           51
49354
 XDOT =       7264
586460                 Wp   =           87
73164
 YDOT =      -1577
729051  meter/sec      RA   =          335
64787  deg
 ZDOT =       1958
407007                 TA   =          201
22758
                                          MA   =          201
30605
                                          Ha   =            192
398  n
mi
                                          Hp   =            181
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1174919
62                 X    =          432767
56
 Y    =      -14808711
99  feet           Y    =        -4509273
83  meter
 Z    =      -16347865
60                 Z    =        -4980907
94
 XDOT =      23833
945078                 XDOT =        7272
175382
 YDOT =      -5176
276415  feet/sec       YDOT =       -1496
449507  meter/sec
 ZDOT =       6425
219839                 ZDOT =        1993
717002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2513929
28                 X    =          766245
64
 Y    =      -14649397
32  feet           Y    =        -4465136
30  meter
 Z    =      -16340330
91                 Z    =        -4980532
86
 XDOT =      23078
922042                 XDOT =        7034
455438
 YDOT =      -3336
685691  feet/sec       YDOT =       -1017
021798  meter/sec
 ZDOT =       6565
404748                 ZDOT =        2001
135367


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   10077
51247524  
00016717  00000-0  10270-3 0  9013
2 25544  51
6478 336
1274 0007470  58
1714 302
0176 15
74166981  9199


Satellite: ISS
Catalog Number: 25544
Epoch time:      10077
51247524   =   yrday
fracday
Element set:     901
Inclination:       51
6478  deg
RA of node:       336
1274  deg
Eccentricity:     
0007470     
Arg of perigee:    58
1714  deg
Mean anomaly:     302
0176  deg
Mean motion:   15
74166981  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             919
Checksum:              306


Coasting Arc #3 (Orbit 934)
---------------------------------------

Vector Time (GMT): 2010/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 784184
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6212047
95                 A    =         6730175
65  meter
 Y    =        1855666
06  meter          E    =           
0011196
 Z    =       -1810384
95                 I    =           51
49795
 XDOT =         81
625034                 Wp   =          101
38142
 YDOT =      -5214
967191  meter/sec      RA   =          330
53370  deg
 ZDOT =      -5657
153744                 TA   =           98
71910
                                          MA   =           98
59227
                                          Ha   =            192
334  n
mi
                                          Hp   =            181
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20380734
75                 X    =        -6223542
09
 Y    =        6088143
24  feet           Y    =         1786134
84  meter
 Z    =       -5939583
17                 Z    =        -1840591
24
 XDOT =        267
798669                 XDOT =         167
415189
 YDOT =     -17109
472413  feet/sec       YDOT =       -5213
575163  meter/sec
 ZDOT =     -18560
215697                 ZDOT =       -5656
548428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20708002
39                 X    =        -6311799
13
 Y    =        4709530
75  feet           Y    =         1435464
97  meter
 Z    =       -6059491
94                 Z    =        -1846933
14
 XDOT =       1867
252438                 XDOT =         569
138543
 YDOT =     -15536
030053  feet/sec       YDOT =       -4735
381960  meter/sec
 ZDOT =     -18557
920817                 ZDOT =       -5656
454265


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   10078
52818906  
00016717  00000-0  10270-3 0  9024
2 25544  51
6478 330
9102 0007290  62
3949 297
7954 15
74179527  9350


Satellite: ISS
Catalog Number: 25544
Epoch time:      10078
52818906   =   yrday
fracday
Element set:     902
Inclination:       51
6478  deg
RA of node:       330
9102  deg
Eccentricity:     
0007290     
Arg of perigee:    62
3949  deg
Mean anomaly:     297
7954  deg
Mean motion:   15
74179527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             935
Checksum:              338


Coasting Arc #4 (Orbit 950)
---------------------------------------

Vector Time (GMT): 2010/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 784184
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         227975
31                 A    =         6720858
97  meter
 Y    =        4588144
47  meter          E    =           
0013727
 Z    =        4897756
22                 I    =           51
44164
 XDOT =      -6898
938446                 Wp   =           60
59997
 YDOT =       2668
224826  meter/sec      RA   =          325
34981  deg
 ZDOT =      -2167
239968                 TA   =           50
53425
                                          MA   =           50
41290
                                          Ha   =            192
192  n
mi
                                          Hp   =            180
850

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         747950
49                 X    =          152860
42
 Y    =       15052967
43  feet           Y    =         4590274
11  meter
 Z    =       16068754
01                 Z    =         4898681
03
 XDOT =     -22634
312487                 XDOT =       -6917
734169
 YDOT =       8754
018457  feet/sec       YDOT =        2590
971585  meter/sec
 ZDOT =      -7110
367349                 ZDOT =       -2200
800921

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -98653
30                 X    =          -30069
53
 Y    =       15067197
97  feet           Y    =         4592481
94  meter
 Z    =       16072520
86                 Z    =         4898904
36
 XDOT =     -21902
106397                 XDOT =       -6675
762030
 YDOT =       7622
633808  feet/sec       YDOT =        2323
378785  meter/sec
 ZDOT =      -7243
579460                 ZDOT =       -2207
843020


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   10079
54387165  
00016717  00000-0  10270-3 0  9036
2 25544  51
6476 325
6928 0007306  64
3639 295
8279 15
74298090  9515


Satellite: ISS
Catalog Number: 25544
Epoch time:      10079
54387165   =   yrday
fracday
Element set:     903
Inclination:       51
6476  deg
RA of node:       325
6928  deg
Eccentricity:     
0007306     
Arg of perigee:    64
3639  deg
Mean anomaly:     295
8279  deg
Mean motion:   15
74298090  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             951
Checksum:              345


Coasting Arc #5 (Orbit 966)
---------------------------------------

Vector Time (GMT): 2010/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 784184
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5793428
93                 A    =         6729601
98  meter
 Y    =       -2771114
44  meter          E    =           
0021445
 Z    =        1977201
16                 I    =           51
44680
 XDOT =        607
520693                 Wp   =           67
98562
 YDOT =       5281
050136  meter/sec      RA   =          320
23398  deg
 ZDOT =       5581
196369                 TA   =          314
11658
                                          MA   =          314
29281
                                          Ha   =            192
196  n
mi
                                          Hp   =            180
774

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19007312
76                 X    =         5814380
54
 Y    =       -9091582
81  feet           Y    =        -2706211
66  meter
 Z    =        6486880
45                 Z    =         2005396
66
 XDOT =       1993
178127                 XDOT =         521
309417
 YDOT =      17326
279973  feet/sec       YDOT =        5287
361964  meter/sec
 ZDOT =      18311
011709                 ZDOT =        5583
938108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19256138
64                 X    =         5869271
06
 Y    =       -8465907
12  feet           Y    =        -2580408
49  meter
 Z    =        6598785
90                 Z    =         2011309
94
 XDOT =        700
162403                 XDOT =         213
409501
 YDOT =      15974
948827  feet/sec       YDOT =        4869
164403  meter/sec
 ZDOT =      18322
007322                 ZDOT =        5584
547832


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   10080
55952826  
00016717  00000-0  10270-3 0  9042
2 25544  51
6474 320
4751 0007336  68
0008 292
1935 15
74289173  9672


Satellite: ISS
Catalog Number: 25544
Epoch time:      10080
55952826   =   yrday
fracday
Element set:     904
Inclination:       51
6474  deg
RA of node:       320
4751  deg
Eccentricity:     
0007336     
Arg of perigee:    68
0008  deg
Mean anomaly:     292
1935  deg
Mean motion:   15
74289173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             967
Checksum:              318


Coasting Arc #6 (Orbit 981)
---------------------------------------

Vector Time (GMT): 2010/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 784184
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -815156
63                 A    =         6721070
78  meter
 Y    =       -4626957
95  meter          E    =           
0018228
 Z    =       -4822306
44                 I    =           51
39589
 XDOT =       6342
204713                 Wp   =           93
79686
 YDOT =      -3618
066558  meter/sec      RA   =          315
04268  deg
 ZDOT =       2406
053686                 TA   =          199
77616
                                          MA   =          199
84692
                                          Ha   =            192
107  n
mi
                                          Hp   =            180
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2674398
41                 X    =         -739930
75
 Y    =      -15180308
25  feet           Y    =        -4635653
03  meter
 Z    =      -15821215
37                 Z    =        -4826083
63
 XDOT =      20807
758244                 XDOT =        6370
503066
 YDOT =     -11870
297106  feet/sec       YDOT =       -3546
985972  meter/sec
 ZDOT =       7893
876921                 ZDOT =        2436
932862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2345331
02                 X    =         -714856
89
 Y    =      -15218925
77  feet           Y    =        -4638728
57  meter
 Z    =      -15836310
87                 Z    =        -4826907
55
 XDOT =      19832
934830                 XDOT =        6045
078536
 YDOT =     -11375
387737  feet/sec       YDOT =       -3467
218182  meter/sec
 ZDOT =       8016
423691                 ZDOT =        2443
405941


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   10081
51167742  
00016717  00000-0  10270-3 0  9055
2 25544  51
6472 315
5832 0007178  71
3458 288
8484 15
74351942  9827


Satellite: ISS
Catalog Number: 25544
Epoch time:      10081
51167742   =   yrday
fracday
Element set:     905
Inclination:       51
6472  deg
RA of node:       315
5832  deg
Eccentricity:     
0007178     
Arg of perigee:    71
3458  deg
Mean anomaly:     288
8484  deg
Mean motion:   15
74351942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             982
Checksum:              326


Coasting Arc #7 (Orbit 997)
---------------------------------------

Vector Time (GMT): 2010/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 784184
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5282657
12                 A    =         6728872
74  meter
 Y    =        3509477
28  meter          E    =           
0011178
 Z    =       -2253270
77                 I    =           51
40169
 XDOT =      -1217
477062                 Wp   =          102
51922
 YDOT =      -5307
248573  meter/sec      RA   =          309
92698  deg
 ZDOT =      -5436
812229                 TA   =          102
84457
                                          MA   =          102
71966
                                          Ha   =            192
040  n
mi
                                          Hp   =            180
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17331552
24                 X    =        -5310562
20
 Y    =       11514033
06  feet           Y    =         3450247
39  meter
 Z    =       -7392620
63                 Z    =        -2279001
60
 XDOT =      -3994
347317                 XDOT =       -1131
629110
 YDOT =     -17412
232852  feet/sec       YDOT =       -5320
383248  meter/sec
 ZDOT =     -17837
310463                 ZDOT =       -5442
518047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17268406
92                 X    =        -5263410
43
 Y    =       11542863
40  feet           Y    =         3518264
76  meter
 Z    =       -7494726
63                 Z    =        -2284392
68
 XDOT =      -3076
855795                 XDOT =        -937
825646
 YDOT =     -16146
873451  feet/sec       YDOT =       -4921
567028  meter/sec
 ZDOT =     -17860
083128                 ZDOT =       -5443
753337


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   10082
52727590  
00016717  00000-0  10270-3 0  9061
2 25544  51
6469 310
3655 0007026  75
6346 284
5597 15
74361436  9988


Satellite: ISS
Catalog Number: 25544
Epoch time:      10082
52727590   =   yrday
fracday
Element set:     906
Inclination:       51
6469  deg
RA of node:       310
3655  deg
Eccentricity:     
0007026     
Arg of perigee:    75
6346  deg
Mean anomaly:     284
5597  deg
Mean motion:   15
74361436  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             998
Checksum:              333


Coasting Arc #8 (Orbit 1011)
---------------------------------------

Vector Time (GMT): 2010/083/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2646901
30                 A    =         6721440
34  meter
 Y    =       -3412482
18  meter          E    =           
0018155
 Z    =       -5166165
80                 I    =           51
35363
 XDOT =       5091
741041                 Wp   =           92
89241
 YDOT =      -5647
981015  meter/sec      RA   =          305
24450  deg
 ZDOT =       1124
473973                 TA   =          187
88843
                                          MA   =          187
91702
                                          Ha   =            192
043  n
mi
                                          Hp   =            182
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8684059
39                 X    =        -2583449
56
 Y    =      -11195807
68  feet           Y    =        -3441726
79  meter
 Z    =      -16949362
86                 Z    =        -5178870
08
 XDOT =      16705
187142                 XDOT =        5149
056912
 YDOT =     -18530
121441  feet/sec       YDOT =       -5590
721636  meter/sec
 ZDOT =       3689
219073                 ZDOT =        1149
348773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -778924
53                 X    =         -237416
20
 Y    =      -14086761
32  feet           Y    =        -4293644
85  meter
 Z    =      -16999892
07                 Z    =        -5181567
10
 XDOT =      23198
191267                 XDOT =        7070
808698
 YDOT =      -5844
073721  feet/sec       YDOT =       -1781
273670  meter/sec
 ZDOT =       3787
877309                 ZDOT =        1154
545004


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   10083
41590237  
00016717  00000-0  10270-3 0  9077
2 25544  51
6473 305
7986 0004124  72
8923 287
2691 15
73685381 10124


Satellite: ISS
Catalog Number: 25544
Epoch time:      10083
41590237   =   yrday
fracday
Element set:     907
Inclination:       51
6473  deg
RA of node:       305
7986  deg
Eccentricity:     
0004124     
Arg of perigee:    72
8923  deg
Mean anomaly:     287
2691  deg
Mean motion:   15
73685381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1012
Checksum:              315


Coasting Arc #9 (Orbit 1027)
---------------------------------------

Vector Time (GMT): 2010/084/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3961694
98                 A    =         6732675
69  meter
 Y    =        5360514
10  meter          E    =           
0012299
 Z    =        -923520
28                 I    =           51
37513
 XDOT =      -3418
988819                 Wp   =          124
36482
 YDOT =      -3536
222424  meter/sec      RA   =          300
11053  deg
 ZDOT =      -5921
953294                 TA   =           65
75263
                                          MA   =           65
62417
                                          Ha   =            191
995  n
mi
                                          Hp   =            182
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12997686
95                 X    =        -4016856
53
 Y    =       17586988
53  feet           Y    =         5315903
60  meter
 Z    =       -3029922
18                 Z    =         -942900
18
 XDOT =     -11217
154919                 XDOT =       -3350
424659
 YDOT =     -11601
779605  feet/sec       YDOT =       -3574
072521  meter/sec
 ZDOT =     -19428
980622                 ZDOT =       -5938
395794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20507660
80                 X    =        -6250735
01
 Y    =        7563488
21  feet           Y    =         2305351
21  meter
 Z    =       -3106759
46                 Z    =         -946940
28
 XDOT =      -2350
795648                 XDOT =        -716
522513
 YDOT =     -14298
775662  feet/sec       YDOT =       -4358
266822  meter/sec
 ZDOT =     -19494
365371                 ZDOT =       -5941
882565


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   10084
43193120  
00016717  00000-0  10270-3 0  9081
2 25544  51
6472 300
5837 0003993  78
0578 282
1032 15
73686461 10288


Satellite: ISS
Catalog Number: 25544
Epoch time:      10084
43193120   =   yrday
fracday
Element set:     908
Inclination:       51
6472  deg
RA of node:       300
5837  deg
Eccentricity:     
0003993     
Arg of perigee:    78
0578  deg
Mean anomaly:     282
1032  deg
Mean motion:   15
73686461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1028
Checksum:              303


Coasting Arc #10 (Orbit 1043)
---------------------------------------

Vector Time (GMT): 2010/085/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3296184
81                 A    =         6720986
18  meter
 Y    =        2734655
64  meter          E    =           
0007385
 Z    =        5174115
24                 I    =           51
32250
 XDOT =      -3913
240373                 Wp   =           68
04430
 YDOT =       6566
581021  meter/sec      RA   =          294
93884  deg
 ZDOT =       -973
834359                 TA   =           31
29358
                                          MA   =           31
24964
                                          Ha   =            191
712  n
mi
                                          Hp   =            182
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10814254
63                 X    =         3240225
87
 Y    =        8971967
32  feet           Y    =         2771203
04  meter
 Z    =       16975443
69                 Z    =         5189991
74
 XDOT =     -12838
715133                 XDOT =       -3981
647571
 YDOT =      21543
900989  feet/sec       YDOT =        6522
438283  meter/sec
 ZDOT =      -3194
994617                 ZDOT =        -993
011254

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4252269
06                 X    =         1296091
61
 Y    =       13312228
39  feet           Y    =         4057567
21  meter
 Z    =       17038567
21                 Z    =         5193355
29
 XDOT =     -21385
451261                 XDOT =       -6518
285544
 YDOT =      11033
705968  feet/sec       YDOT =        3363
073579  meter/sec
 ZDOT =      -3270
986961                 ZDOT =        -996
996826


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   10085
44792926  
00016717  00000-0  10270-3 0  9093
2 25544  51
6470 295
3687 0003921  78
4329 281
7274 15
73800422 10445


Satellite: ISS
Catalog Number: 25544
Epoch time:      10085
44792926   =   yrday
fracday
Element set:     909
Inclination:       51
6470  deg
RA of node:       295
3687  deg
Eccentricity:     
0003921     
Arg of perigee:    78
4329  deg
Mean anomaly:     281
7274  deg
Mean motion:   15
73800422  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1044
Checksum:              322


Coasting Arc #11 (Orbit 1059)
---------------------------------------

Vector Time (GMT): 2010/086/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2845513
10                 A    =         6732421
76  meter
 Y    =       -6042249
32  meter          E    =           
0017088
 Z    =         788543
38                 I    =           51
34914
 XDOT =       4079
246710                 Wp   =           59
44774
 YDOT =       2708
428606  meter/sec      RA   =          289
79928  deg
 ZDOT =       5946
300139                 TA   =          309
18721
                                          MA   =          309
33885
                                          Ha   =            191
780  n
mi
                                          Hp   =            182
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9335672
89                 X    =         2909036
57
 Y    =      -19823652
61  feet           Y    =        -6010073
84  meter
 Z    =        2587084
58                 Z    =          802521
61
 XDOT =      13383
355349                 XDOT =        4019
771698
 YDOT =       8885
920625  feet/sec       YDOT =        2753
713217  meter/sec
 ZDOT =      19508
858724                 ZDOT =        5965
972142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18274307
56                 X    =         5570008
94
 Y    =      -12078585
35  feet           Y    =        -3681552
81  meter
 Z    =        2642433
91                 Z    =          805413
86
 XDOT =       5825
709187                 XDOT =        1775
676160
 YDOT =      13160
152141  feet/sec       YDOT =        4011
214373  meter/sec
 ZDOT =      19587
059787                 ZDOT =        5970
135823


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   10086
46390133  
00016717  00000-0  10270-3 0  9102
2 25544  51
6465 290
1531 0003906  81
2248 278
9358 15
73817004 10608


Satellite: ISS
Catalog Number: 25544
Epoch time:      10086
46390133   =   yrday
fracday
Element set:     910
Inclination:       51
6465  deg
RA of node:       290
1531  deg
Eccentricity:     
0003906     
Arg of perigee:    81
2248  deg
Mean anomaly:     278
9358  deg
Mean motion:   15
73817004  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1060
Checksum:              294


Coasting Arc #12 (Orbit 1074)
---------------------------------------

Vector Time (GMT): 2010/087/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3781443
07                 A    =         6720749
42  meter
 Y    =       -2002825
80  meter          E    =           
0018379
 Z    =       -5198417
70                 I    =           51
30050
 XDOT =       2599
922455                 Wp   =           94
02795
 YDOT =      -7180
787750  meter/sec      RA   =          284
62654  deg
 ZDOT =        876
740894                 TA   =          184
36733
                                          MA   =          184
38339
                                          Ha   =            191
688  n
mi
                                          Hp   =            182
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12406309
30                 X    =        -3733513
28
 Y    =       -6570950
80  feet           Y    =        -2044844
76  meter
 Z    =      -17055176
19                 Z    =        -5216671
16
 XDOT =       8529
929315                 XDOT =        2675
767058
 YDOT =     -23559
014928  feet/sec       YDOT =       -7151
289700  meter/sec
 ZDOT =       2876
446501                 ZDOT =         889
556273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7294736
10                 X    =        -2223435
56
 Y    =      -11891205
21  feet           Y    =        -3624439
35  meter
 Z    =      -17127726
16                 Z    =        -5220530
93
 XDOT =      18388
620722                 XDOT =        5604
851596
 YDOT =     -15490
204544  feet/sec       YDOT =       -4721
414345  meter/sec
 ZDOT =       2927
135823                 ZDOT =         892
190999


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   10087
41634833  
00016717  00000-0  10270-3 0  9117
2 25544  51
6458 285
2629 0003821  83
6112 276
5486 15
73865833 10750


Satellite: ISS
Catalog Number: 25544
Epoch time:      10087
41634833   =   yrday
fracday
Element set:     911
Inclination:       51
6458  deg
RA of node:       285
2629  deg
Eccentricity:     
0003821     
Arg of perigee:    83
6112  deg
Mean anomaly:     276
5486  deg
Mean motion:   15
73865833  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1075
Checksum:              321


Coasting Arc #13 (Orbit 1090)
---------------------------------------

Vector Time (GMT): 2010/088/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1699082
84                 A    =         6732323
53  meter
 Y    =        6465036
86  meter          E    =           
0013132
 Z    =        -763017
54                 I    =           51
33278
 XDOT =      -4512
525757                 Wp   =          127
67721
 YDOT =      -1878
884082  meter/sec      RA   =          279
48422  deg
 ZDOT =      -5948
971522                 TA   =           60
67455
                                          MA   =           60
54342
                                          Ha   =            191
664  n
mi
                                          Hp   =            182
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5574418
76                 X    =        -1767543
16
 Y    =       21210750
84  feet           Y    =         6445653
83  meter
 Z    =       -2503338
37                 Z    =         -771438
72
 XDOT =     -14804
874532                 XDOT =       -4462
281359
 YDOT =      -6164
317854  feet/sec       YDOT =       -1929
065598  meter/sec
 ZDOT =     -19517
623104                 ZDOT =       -5970
771078

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15251758
95                 X    =        -4648736
13
 Y    =       15753931
51  feet           Y    =         4801798
32  meter
 Z    =       -2536590
21                 Z    =         -773152
70
 XDOT =      -8626
219119                 XDOT =       -2629
271587
 YDOT =     -11467
295969  feet/sec       YDOT =       -3495
231811  meter/sec
 ZDOT =     -19604
252802                 ZDOT =       -5975
376254


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   10088
43226476  
00016717  00000-0  10270-3 0  9121
2 25544  51
6456 280
0472 0003736  89
4600 270
6991 15
73856218 10919


Satellite: ISS
Catalog Number: 25544
Epoch time:      10088
43226476   =   yrday
fracday
Element set:     912
Inclination:       51
6456  deg
RA of node:       280
0472  deg
Eccentricity:     
0003736     
Arg of perigee:    89
4600  deg
Mean anomaly:     270
6991  deg
Mean motion:   15
73856218  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1091
Checksum:              314


Coasting Arc #14 (Orbit 1106)
---------------------------------------

Vector Time (GMT): 2010/089/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4073618
67                 A    =         6720480
57  meter
 Y    =        1267303
85  meter          E    =           
0006766
 Z    =        5187303
02                 I    =           51
28972
 XDOT =      -1257
179639                 Wp   =           75
36362
 YDOT =       7554
634688  meter/sec      RA   =          274
31011  deg
 ZDOT =       -855
775380                 TA   =           22
83320
                                          MA   =           22
80313
                                          Ha   =            191
388  n
mi
                                          Hp   =            182
508

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13364890
63                 X    =         4033945
59
 Y    =        4157821
05  feet           Y    =         1312636
21  meter
 Z    =       17018710
71                 Z    =         5206996
25
 XDOT =      -4124
605114                 XDOT =       -1337
406256
 YDOT =      24785
546877  feet/sec       YDOT =        7540
127495  meter/sec
 ZDOT =      -2807
662008                 ZDOT =        -862
078462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9690547
54                 X    =         2953678
89
 Y    =        9966525
74  feet           Y    =         3037797
05  meter
 Z    =       17096957
18                 Z    =         5211152
55
 XDOT =     -14675
049674                 XDOT =       -4472
955141
 YDOT =      19142
276996  feet/sec       YDOT =        5834
566028  meter/sec
 ZDOT =      -2832
465726                 ZDOT =        -863
335553


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   10089
44814982  
00016717  00000-0  10270-3 0  9139
2 25544  51
6453 274
8303 0003690  90
1037 270
0549 15
73948838 11073


Satellite: ISS
Catalog Number: 25544
Epoch time:      10089
44814982   =   yrday
fracday
Element set:     913
Inclination:       51
6453  deg
RA of node:       274
8303  deg
Eccentricity:     
0003690     
Arg of perigee:    90
1037  deg
Mean anomaly:     270
0549  deg
Mean motion:   15
73948838  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1107
Checksum:              316


Coasting Arc #15 (Orbit 1122)
---------------------------------------

Vector Time (GMT): 2010/090/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         498659
53                 A    =         6731930
69  meter
 Y    =       -6665337
46  meter          E    =           
0016369
 Z    =         744338
93                 I    =           51
32689
 XDOT =       4779
119269                 Wp   =           61
11626
 YDOT =       1032
325745  meter/sec      RA   =          269
16488  deg
 ZDOT =       5951
624531                 TA   =          307
03362
                                          MA   =          307
18324
                                          Ha   =            191
395  n
mi
                                          Hp   =            182
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1636022
09                 X    =          569539
57
 Y    =      -21867905
04  feet           Y    =        -6659364
77  meter
 Z    =        2442056
87                 Z    =          746934
18
 XDOT =      15679
525160                 XDOT =        4738
308259
 YDOT =       3386
895489  feet/sec       YDOT =        1085
541021  meter/sec
 ZDOT =      19526
327203                 ZDOT =        5974
742465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11507628
26                 X    =         3507525
09
 Y    =      -18665660
37  feet           Y    =        -5689293
28  meter
 Z    =        2452161
46                 Z    =          747418
81
 XDOT =      10895
924421                 XDOT =        3321
077763
 YDOT =       9333
772158  feet/sec       YDOT =        2844
933754  meter/sec
 ZDOT =      19618
168004                 ZDOT =        5979
617608


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   10090
46400604  
00016717  00000-0  10270-3 0  9146
2 25544  51
6444 269
6130 0003603  93
5906 266
5669 15
74003027 11233


Satellite: ISS
Catalog Number: 25544
Epoch time:      10090
46400604   =   yrday
fracday
Element set:     914
Inclination:       51
6444  deg
RA of node:       269
6130  deg
Eccentricity:     
0003603     
Arg of perigee:    93
5906  deg
Mean anomaly:     266
5669  deg
Mean motion:   15
74003027  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1123
Checksum:              283


Coasting Arc #16 (Orbit 1137)
---------------------------------------

Vector Time (GMT): 2010/091/09:38:48
528
Vector Time (MET): N/A
Weight (LBS)     : 783814
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4245634
13                 A    =         6720256
10  meter
 Y    =        -561032
39  meter          E    =           
0018230
 Z    =       -5194843
68                 I    =           51
28864
 XDOT =        -83
753764                 Wp   =           96
73188
 YDOT =      -7634
922756  meter/sec      RA   =          263
98931  deg
 ZDOT =        893
587663                 TA   =          181
83178
                                          MA   =          181
83847
                                          Ha   =            191
340  n
mi
                                          Hp   =            182
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13929245
83                 X    =        -4213809
17
 Y    =       -1840657
43  feet           Y    =         -608331
96  meter
 Z    =      -17043450
38                 Z    =        -5215391
82
 XDOT =       -274
782690                 XDOT =          -2
713396
 YDOT =     -25048
959173  feet/sec       YDOT =       -7635
406166  meter/sec
 ZDOT =       2931
718056                 ZDOT =         893
378089

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11564164
55                 X    =        -3524757
35
 Y    =       -7803399
91  feet           Y    =        -2378476
29  meter
 Z    =      -17125073
97                 Z    =        -5219722
55
 XDOT =      10317
930601                 XDOT =        3144
905247
 YDOT =     -21717
891854  feet/sec       YDOT =       -6619
613437  meter/sec
 ZDOT =       2930
654246                 ZDOT =         893
263414


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   10091
41634533  
00016717  00000-0  10270-3 0  9153
2 25544  51
6435 264
7213 0003592  95
9006 264
2567 15
74039466 11389


Satellite: ISS
Catalog Number: 25544
Epoch time:      10091
41634533   =   yrday
fracday
Element set:     915
Inclination:       51
6435  deg
RA of node:       264
7213  deg
Eccentricity:     
0003592     
Arg of perigee:    95
9006  deg
Mean anomaly:     264
2567  deg
Mean motion:   15
74039466  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1138
Checksum:              306

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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