Date: February 2nd 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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


There are no maneuvers



Coasting Arc #1 (Orbit 209)
---------------------------------------

Vector Time (GMT): 2010/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2305786
65                 A    =         6715711
86  meter
 Y    =        3514628
02  meter          E    =           
0003858
 Z    =       -5240800
94                 I    =           51
46811
 XDOT =      -6718
605560                 Wp   =          102
21214
 YDOT =      -3737
203334  meter/sec      RA   =          206
41813  deg
 ZDOT =        449
174782                 TA   =          172
06685
                                          MA   =          172
06075
                                          Ha   =            185
355  n
mi
                                          Hp   =            183
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7564916
83                 X    =        -2319458
29
 Y    =       11530931
84  feet           Y    =         3488766
80  meter
 Z    =      -17194228
82                 Z    =        -5252035
43
 XDOT =     -22042
669160                 XDOT =       -6678
498103
 YDOT =     -12261
165794  feet/sec       YDOT =       -3812
110501  meter/sec
 ZDOT =       1473
670544                 ZDOT =         416
634169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13605050
28                 X    =        -4146819
33
 Y    =        1887901
31  feet           Y    =          575432
32  meter
 Z    =      -17238628
02                 Z    =        -5254333
82
 XDOT =      -4995
973931                 XDOT =       -1522
772854
 YDOT =     -23710
640272  feet/sec       YDOT =       -7227
003155  meter/sec
 ZDOT =       1344
507486                 ZDOT =         409
805882


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   10032
51516884  
00016717  00000-0  10270-3 0  9001
2 25544  51
6399 207
3520 0011187 270
2602  89
7280 15
75557979  2108


Satellite: ISS
Catalog Number: 25544
Epoch time:      10032
51516884   =   yrday
fracday
Element set:     900
Inclination:       51
6399  deg
RA of node:       207
3520  deg
Eccentricity:     
0011187     
Arg of perigee:   270
2602  deg
Mean anomaly:      89
7280  deg
Mean motion:   15
75557979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             210
Checksum:              303


Coasting Arc #2 (Orbit 225)
---------------------------------------

Vector Time (GMT): 2010/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5900018
68                 A    =         6727244
30  meter
 Y    =        3085696
65  meter          E    =           
0008402
 Z    =        -924946
30                 I    =           51
53552
 XDOT =      -2975
401483                 Wp   =          215
76204
 YDOT =       3903
272004  meter/sec      RA   =          201
27340  deg
 ZDOT =      -5937
423448                 TA   =          334
35921
                                          MA   =          334
40085
                                          Ha   =            185
609  n
mi
                                          Hp   =            183
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19357016
68                 X    =         5869568
50
 Y    =       10123676
66  feet           Y    =         3151503
87  meter
 Z    =       -3034600
72                 Z    =         -896358
67
 XDOT =      -9761
815889                 XDOT =       -2989
985112
 YDOT =      12806
010511  feet/sec       YDOT =        3869
917605  meter/sec
 ZDOT =     -19479
735721                 ZDOT =       -5951
913161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5367271
19                 X    =         1635944
26
 Y    =       21190826
88  feet           Y    =         6458964
03  meter
 Z    =       -2921126
71                 Z    =         -890359
42
 XDOT =     -14431
153555                 XDOT =       -4398
615604
 YDOT =        952
453808  feet/sec       YDOT =         290
307921  meter/sec
 ZDOT =     -19537
025738                 ZDOT =       -5954
885445


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   10033
52999129  
00016717  00000-0  10270-3 0  9011
2 25544  51
6404 202
1281 0011264 275
5556  84
4323 15
75613318  2261


Satellite: ISS
Catalog Number: 25544
Epoch time:      10033
52999129   =   yrday
fracday
Element set:     901
Inclination:       51
6404  deg
RA of node:       202
1281  deg
Eccentricity:     
0011264     
Arg of perigee:   275
5556  deg
Mean anomaly:      84
4323  deg
Mean motion:   15
75613318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             226
Checksum:              286


Coasting Arc #3 (Orbit 241)
---------------------------------------

Vector Time (GMT): 2010/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2906417
64                 A    =         6716573
33  meter
 Y    =       -3342884
16  meter          E    =           
0008218
 Z    =        5055796
17                 I    =           51
52744
 XDOT =       6737
550440                 Wp   =          303
30295
 YDOT =       3326
386363  meter/sec      RA   =          196
09522  deg
 ZDOT =      -1671
316605                 TA   =          162
81181
                                          MA   =          162
78397
                                          Ha   =            185
865  n
mi
                                          Hp   =            183
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9535490
95                 X    =         2919022
62
 Y    =      -10967467
71  feet           Y    =        -3310312
30  meter
 Z    =       16587257
78                 Z    =         5069945
99
 XDOT =      22104
824279                 XDOT =        6707
972267
 YDOT =      10913
341085  feet/sec       YDOT =        3401
564234  meter/sec
 ZDOT =      -5483
322194                 ZDOT =       -1638
658046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14459504
47                 X    =         4407256
96
 Y    =        -523263
70  feet           Y    =         -159490
78  meter
 Z    =       16643226
31                 Z    =         5072855
38
 XDOT =       6989
594372                 XDOT =        2130
428365
 YDOT =      22604
417616  feet/sec       YDOT =        6889
826489  meter/sec
 ZDOT =      -5353
688104                 ZDOT =       -1631
804134


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   10034
54480491  
00016717  00000-0  10270-3 0  9022
2 25544  51
6402 196
9039 0011096 278
1494  81
8411 15
75548417  2427


Satellite: ISS
Catalog Number: 25544
Epoch time:      10034
54480491   =   yrday
fracday
Element set:     902
Inclination:       51
6402  deg
RA of node:       196
9039  deg
Eccentricity:     
0011096     
Arg of perigee:   278
1494  deg
Mean anomaly:      81
8411  deg
Mean motion:   15
75548417  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             242
Checksum:              303


Coasting Arc #4 (Orbit 257)
---------------------------------------

Vector Time (GMT): 2010/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5812177
31                 A    =         6725896
52  meter
 Y    =       -2729332
74  meter          E    =           
0007889
 Z    =        1983953
47                 I    =           51
58974
 XDOT =       3692
900264                 Wp   =           16
06369
 YDOT =      -3800
607382  meter/sec      RA   =          190
97360  deg
 ZDOT =       5592
360790                 TA   =            6
06798
                                          MA   =            6
05843
                                          Ha   =            186
201  n
mi
                                          Hp   =            183
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19068823
19                 X    =        -5790863
00
 Y    =       -8954503
74  feet           Y    =        -2794208
77  meter
 Z    =        6509033
70                 Z    =         1955770
09
 XDOT =      12115
814516                 XDOT =        3707
958572
 YDOT =     -12469
184325  feet/sec       YDOT =       -3759
226974  meter/sec
 ZDOT =      18347
640387                 ZDOT =        5610
337229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6752067
85                 X    =        -2058030
28
 Y    =      -19991412
85  feet           Y    =        -6093382
64  meter
 Z    =        6397160
84                 Z    =         1949854
62
 XDOT =      15852
787486                 XDOT =        4831
929626
 YDOT =        537
345348  feet/sec       YDOT =         163
782862  meter/sec
 ZDOT =      18418
769614                 ZDOT =        5614
040978


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   10035
55960188  
00016717  00000-0  10270-3 0  9031
2 25544  51
6411 191
6799 0011173 281
8187  78
1724 15
75626802  2586


Satellite: ISS
Catalog Number: 25544
Epoch time:      10035
55960188   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:       191
6799  deg
Eccentricity:     
0011173     
Arg of perigee:   281
8187  deg
Mean anomaly:      78
1724  deg
Mean motion:   15
75626802  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             258
Checksum:              321


Coasting Arc #5 (Orbit 272)
---------------------------------------

Vector Time (GMT): 2010/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3526371
99                 A    =         6718071
89  meter
 Y    =        3340660
95  meter          E    =           
0000697
 Z    =       -4640766
12                 I    =           51
59404
 XDOT =      -6528
300907                 Wp   =          212
40427
 YDOT =      -2931
728893  meter/sec      RA   =          185
78357  deg
 ZDOT =       2849
466471                 TA   =           85
76831
                                          MA   =           85
76034
                                          Ha   =            186
463  n
mi
                                          Hp   =            183
895

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11569461
91                 X    =        -3540922
07
 Y    =       10960173
73  feet           Y    =         3301145
69  meter
 Z    =      -15225610
62                 Z    =        -4657932
29
 XDOT =     -21418
310061                 XDOT =       -6508
874603
 YDOT =      -9618
533114  feet/sec       YDOT =       -3004
623648  meter/sec
 ZDOT =       9348
643279                 ZDOT =        2817
799555

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15865538
08                 X    =        -4835816
01
 Y    =        -434734
51  feet           Y    =         -132507
08  meter
 Z    =      -15293553
65                 Z    =        -4661475
15
 XDOT =      -8321
201126                 XDOT =       -2536
302103
 YDOT =     -20863
033439  feet/sec       YDOT =       -6359
052592  meter/sec
 ZDOT =       9222
937395                 ZDOT =        2811
151318


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   10036
51096487  
00016717  00000-0  10270-3 0  9041
2 25544  51
6417 186
7834 0011118 285
9045  74
0894 15
75627595  2734


Satellite: ISS
Catalog Number: 25544
Epoch time:      10036
51096487   =   yrday
fracday
Element set:     904
Inclination:       51
6417  deg
RA of node:       186
7834  deg
Eccentricity:     
0011118     
Arg of perigee:   285
9045  deg
Mean anomaly:      74
0894  deg
Mean motion:   15
75627595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             273
Checksum:              329


Coasting Arc #6 (Orbit 288)
---------------------------------------

Vector Time (GMT): 2010/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5526814
58                 A    =         6723710
61  meter
 Y    =        2415158
79  meter          E    =           
0006611
 Z    =       -2968790
76                 I    =           51
64305
 XDOT =      -4387
525641                 Wp   =          288
88905
 YDOT =       3895
445792  meter/sec      RA   =          180
67991  deg
 ZDOT =      -4987
865874                 TA   =          285
38651
                                          MA   =          285
45954
                                          Ha   =            186
838  n
mi
                                          Hp   =            183
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18132593
78                 X    =         5513818
72
 Y    =        7923749
31  feet           Y    =         2476890
33  meter
 Z    =       -9740127
18                 Z    =        -2941973
39
 XDOT =     -14394
769162                 XDOT =       -4406
529322
 YDOT =      12780
333962  feet/sec       YDOT =        3846
275782  meter/sec
 ZDOT =     -16364
389352                 ZDOT =       -5009
226196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7498171
21                 X    =         2285442
58
 Y    =       18368907
96  feet           Y    =         5598843
15  meter
 Z    =       -9633664
23                 Z    =        -2936340
86
 XDOT =     -17820
126820                 XDOT =       -5431
574655
 YDOT =      -1371
907822  feet/sec       YDOT =        -418
157504  meter/sec
 ZDOT =     -16448
954481                 ZDOT =       -5013
641326


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   10037
52573869  
00016717  00000-0  10270-3 0  9058
2 25544  51
6415 181
5594 0011157 290
3089  69
6876 15
75656621  2898


Satellite: ISS
Catalog Number: 25544
Epoch time:      10037
52573869   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       181
5594  deg
Eccentricity:     
0011157     
Arg of perigee:   290
3089  deg
Mean anomaly:      69
6876  deg
Mean motion:   15
75656621  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             289
Checksum:              340


Coasting Arc #7 (Orbit 304)
---------------------------------------

Vector Time (GMT): 2010/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4110414
68                 A    =         6720428
55  meter
 Y    =       -3501986
59  meter          E    =           
0006819
 Z    =        4005214
85                 I    =           51
66249
 XDOT =       6075
898545                 Wp   =            3
63271
 YDOT =       2633
954205  meter/sec      RA   =          175
48291  deg
 ZDOT =      -3925
425338                 TA   =          126
94685
                                          MA   =          126
88438
                                          Ha   =            187
077  n
mi
                                          Hp   =            183
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13485612
48                 X    =         4129812
76
 Y    =      -11489457
31  feet           Y    =        -3455913
20  meter
 Z    =       13140468
67                 Z    =         4025229
86
 XDOT =      19934
050345                 XDOT =        6065
062299
 YDOT =       8641
582038  feet/sec       YDOT =        2701
838079  meter/sec
 ZDOT =     -12878
692054                 ZDOT =       -3895
935353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17638008
99                 X    =         5376065
14
 Y    =         825107
00  feet           Y    =          251492
61  meter
 Z    =       13219724
93                 Z    =         4029372
16
 XDOT =       8706
299537                 XDOT =        2653
680099
 YDOT =      18721
060228  feet/sec       YDOT =        5706
179158  meter/sec
 ZDOT =     -12761
606436                 ZDOT =       -3889
737642


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   10038
54050081  
00016717  00000-0  10270-3 0  9068
2 25544  51
6416 176
3354 0011092 293
9261  66
0741 15
75646443  3056


Satellite: ISS
Catalog Number: 25544
Epoch time:      10038
54050081   =   yrday
fracday
Element set:     906
Inclination:       51
6416  deg
RA of node:       176
3354  deg
Eccentricity:     
0011092     
Arg of perigee:   293
9261  deg
Mean anomaly:      66
0741  deg
Mean motion:   15
75646443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             305
Checksum:              288


Coasting Arc #8 (Orbit 320)
---------------------------------------

Vector Time (GMT): 2010/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5036925
84                 A    =         6720933
29  meter
 Y    =       -2229070
57  meter          E    =           
0003831
 Z    =        3847099
76                 I    =           51
69578
 XDOT =       4996
378851                 Wp   =           21
97321
 YDOT =      -4158
229515  meter/sec      RA   =          170
38928  deg
 ZDOT =       4134
476475                 TA   =           24
88661
                                          MA   =           24
86814
                                          Ha   =            187
359  n
mi
                                          Hp   =            183
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16525347
24                 X    =        -5030313
73
 Y    =       -7313223
65  feet           Y    =        -2285359
66  meter
 Z    =       12621718
37                 Z    =         3822646
86
 XDOT =      16392
319065                 XDOT =        5022
421462
 YDOT =     -13642
485286  feet/sec       YDOT =       -4102
211624  meter/sec
 ZDOT =      13564
555363                 ZDOT =        4158
811429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7359899
53                 X    =        -2243297
38
 Y    =      -16578418
00  feet           Y    =        -5053101
81  meter
 Z    =       12524617
82                 Z    =         3817503
51
 XDOT =      20037
783276                 XDOT =        6107
516342
 YDOT =       1419
444423  feet/sec       YDOT =         432
646660  meter/sec
 ZDOT =      13660
935306                 ZDOT =        4163
853081


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   10039
55524740  
00016717  00000-0  10270-3 0  9079
2 25544  51
6428 171
1112 0011214 297
8900  62
1128 15
75719552  3219


Satellite: ISS
Catalog Number: 25544
Epoch time:      10039
55524740   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       171
1112  deg
Eccentricity:     
0011214     
Arg of perigee:   297
8900  deg
Mean anomaly:      62
1128  deg
Mean motion:   15
75719552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             321
Checksum:              282


Coasting Arc #9 (Orbit 335)
---------------------------------------

Vector Time (GMT): 2010/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4558707
74                 A    =         6722925
53  meter
 Y    =        3785859
46  meter          E    =           
0008447
 Z    =       -3163363
64                 I    =           51
73244
 XDOT =      -5444
763291                 Wp   =          324
10549
 YDOT =      -2511
153420  meter/sec      RA   =          165
19586  deg
 ZDOT =       4841
348006                 TA   =          359
03782
                                          MA   =          359
03945
                                          Ha   =            187
564  n
mi
                                          Hp   =            183
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14956390
21                 X    =        -4585336
42
 Y    =       12420798
75  feet           Y    =         3734732
53  meter
 Z    =      -10378489
62                 Z    =        -3185573
80
 XDOT =     -17863
396624                 XDOT =       -5439
796259
 YDOT =      -8238
692323  feet/sec       YDOT =       -2572
012416  meter/sec
 ZDOT =      15883
687685                 ZDOT =        4814
909979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19387790
36                 X    =        -5909398
50
 Y    =        -499564
78  feet           Y    =         -152267
34  meter
 Z    =      -10466466
27                 Z    =        -3190178
92
 XDOT =      -8089
274536                 XDOT =       -2465
610878
 YDOT =     -16626
542923  feet/sec       YDOT =       -5067
770283  meter/sec
 ZDOT =      15778
686565                 ZDOT =        4809
343665


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   10040
50656340  
00016717  00000-0  10270-3 0  9089
2 25544  51
6431 166
2144 0011295 302
4814  57
5258 15
75691246  3366


Satellite: ISS
Catalog Number: 25544
Epoch time:      10040
50656340   =   yrday
fracday
Element set:     908
Inclination:       51
6431  deg
RA of node:       166
2144  deg
Eccentricity:     
0011295     
Arg of perigee:   302
4814  deg
Mean anomaly:      57
5258  deg
Mean motion:   15
75691246  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             336
Checksum:              289


Coasting Arc #10 (Orbit 351)
---------------------------------------

Vector Time (GMT): 2010/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4428171
90                 A    =         6718384
07  meter
 Y    =        2211088
95  meter          E    =           
0010150
 Z    =       -4548448
84                 I    =           51
74655
 XDOT =      -5418
539387                 Wp   =            2
11130
 YDOT =       4529
862853  meter/sec      RA   =          160
10281  deg
 ZDOT =      -3063
467360                 TA   =          237
39242
                                          MA   =          237
49044
                                          Ha   =            187
832  n
mi
                                          Hp   =            183
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14528123
02                 X    =         4425212
90
 Y    =        7254228
83  feet           Y    =         2260590
98  meter
 Z    =      -14922732
41                 Z    =        -4526944
52
 XDOT =     -17777
360194                 XDOT =       -5453
909057
 YDOT =      14861
754767  feet/sec       YDOT =        4469
071862  meter/sec
 ZDOT =     -10050
745932                 ZDOT =       -3089
875647

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6451439
19                 X    =         1966398
67
 Y    =       14987039
51  feet           Y    =         4568049
64  meter
 Z    =      -14837308
24                 Z    =        -4522411
55
 XDOT =     -22032
335146                 XDOT =       -6715
455753
 YDOT =       -601
486063  feet/sec       YDOT =        -183
332952  meter/sec
 ZDOT =     -10155
363058                 ZDOT =       -3095
354660


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   10041
52128705  
00016717  00000-0  10270-3 0  9092
2 25544  51
6437 160
9907 0011289 306
1414  53
8705 15
75719331  3520


Satellite: ISS
Catalog Number: 25544
Epoch time:      10041
52128705   =   yrday
fracday
Element set:     909
Inclination:       51
6437  deg
RA of node:       160
9907  deg
Eccentricity:     
0011289     
Arg of perigee:   306
1414  deg
Mean anomaly:      53
8705  deg
Mean motion:   15
75719331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             352
Checksum:              296


Coasting Arc #11 (Orbit 367)
---------------------------------------

Vector Time (GMT): 2010/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4855577
60                 A    =         6725184
37  meter
 Y    =       -4132051
30  meter          E    =           
0005400
 Z    =        2140439
31                 I    =           51
79827
 XDOT =       4671
898049                 Wp   =           61
54953
 YDOT =       2618
610995  meter/sec      RA   =          154
92181  deg
 ZDOT =      -5530
012313                 TA   =           94
55981
                                          MA   =           94
49812
                                          Ha   =            187
975  n
mi
                                          Hp   =            182
694

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15930372
70                 X    =         4891024
51
 Y    =      -13556598
74  feet           Y    =        -4077555
18  meter
 Z    =        7022438
67                 Z    =         2164113
02
 XDOT =      15327
749505                 XDOT =        4669
132024
 YDOT =       8591
243422  feet/sec       YDOT =        2670
839532  meter/sec
 ZDOT =     -18143
085017                 ZDOT =       -5507
323619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20882015
86                 X    =         6364838
44
 Y    =        -416507
69  feet           Y    =         -126951
54  meter
 Z    =        7116229
58                 Z    =         2169026
78
 XDOT =       6463
766805                 XDOT =        1970
156122
 YDOT =      14904
025796  feet/sec       YDOT =        4542
747063  meter/sec
 ZDOT =     -18052
933420                 ZDOT =       -5502
534106


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   10042
53599822  
00016717  00000-0  10270-3 0  9108
2 25544  51
6441 155
7669 0011203 310
3857  49
6329 15
75738337  3685


Satellite: ISS
Catalog Number: 25544
Epoch time:      10042
53599822   =   yrday
fracday
Element set:     910
Inclination:       51
6441  deg
RA of node:       155
7669  deg
Eccentricity:     
0011203     
Arg of perigee:   310
3857  deg
Mean anomaly:      49
6329  deg
Mean motion:   15
75738337  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             368
Checksum:              317


Coasting Arc #12 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2010/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3721481
83                 A    =         6716074
64  meter
 Y    =       -2424058
90  meter          E    =           
0005949
 Z    =        5039628
30                 I    =           51
79581
 XDOT =       5641
957302                 Wp   =          323
42373
 YDOT =      -4923
577753  meter/sec      RA   =          149
81834  deg
 ZDOT =       1803
795583                 TA   =          109
26984
                                          MA   =          109
20548
                                          Ha   =            188
198  n
mi
                                          Hp   =            182
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12209586
06                 X    =        -3718579
82
 Y    =       -7952949
15  feet           Y    =        -2465658
46  meter
 Z    =       16534213
60                 Z    =         5021556
98
 XDOT =      18510
358602                 XDOT =        5687
832066
 YDOT =     -16153
470318  feet/sec       YDOT =       -4860
229531  meter/sec
 ZDOT =       5917
964511                 ZDOT =        1831
314800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4718700
99                 X    =        -1438260
06
 Y    =      -13871816
05  feet           Y    =        -4228129
53  meter
 Z    =       16462387
18                 Z    =         5017735
61
 XDOT =      23499
807293                 XDOT =        7162
741263
 YDOT =       -863
811619  feet/sec       YDOT =        -263
289781  meter/sec
 ZDOT =       6026
995231                 ZDOT =        1837
028146


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   10043
55069478  
00016717  00000-0  10270-3 0  9111
2 25544  51
6451 150
5425 0011319 314
5954  45
4285 15
75801784  3841


Satellite: ISS
Catalog Number: 25544
Epoch time:      10043
55069478   =   yrday
fracday
Element set:     911
Inclination:       51
6451  deg
RA of node:       150
5425  deg
Eccentricity:     
0011319     
Arg of perigee:   314
5954  deg
Mean anomaly:      45
4285  deg
Mean motion:   15
75801784  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              306


Coasting Arc #13 (Orbit 398)
---------------------------------------

Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4931905
20                 A    =         6726717
63  meter
 Y    =        4449580
05  meter          E    =           
0016445
 Z    =        -989155
27                 I    =           51
85719
 XDOT =      -3882
790102                 Wp   =          355
35142
 YDOT =      -2981
474922  meter/sec      RA   =          144
65883  deg
 ZDOT =       5956
943873                 TA   =          353
85458
                                          MA   =          353
87473
                                          Ha   =            188
457  n
mi
                                          Hp   =            182
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16180791
35                 X    =        -4976489
66
 Y    =       14598359
76  feet           Y    =         4394179
25  meter
 Z    =       -3245260
08                 Z    =        -1013222
13
 XDOT =     -12738
812672                 XDOT =       -3878
099008
 YDOT =      -9781
741869  feet/sec       YDOT =       -3024
868201  meter/sec
 ZDOT =      19543
779110                 ZDOT =        5938
093334

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21704191
17                 X    =        -6615437
47
 Y    =        1797279
71  feet           Y    =          547810
86  meter
 Z    =       -3340613
79                 Z    =        -1018219
08
 XDOT =      -4150
638308                 XDOT =       -1265
114556
 YDOT =     -13991
349278  feet/sec       YDOT =       -4264
563260  meter/sec
 ZDOT =      19468
830042                 ZDOT =        5934
099397


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   10044
50196368  
00016717  00000-0  10270-3 0  9127
2 25544  51
6453 145
6457 0011459 319
2379  40
7927 15
75762121  3999


Satellite: ISS
Catalog Number: 25544
Epoch time:      10044
50196368   =   yrday
fracday
Element set:     912
Inclination:       51
6453  deg
RA of node:       145
6457  deg
Eccentricity:     
0011459     
Arg of perigee:   319
2379  deg
Mean anomaly:      40
7927  deg
Mean motion:   15
75762121  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             399
Checksum:              320


Coasting Arc #14 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3060438
82                 A    =         6715041
04  meter
 Y    =        2832811
07  meter          E    =           
0012847
 Z    =       -5270629
31                 I    =           51
84184
 XDOT =      -5619
426774                 Wp   =           38
74203
 YDOT =       5242
879909  meter/sec      RA   =          139
53925  deg
 ZDOT =       -435
832363                 TA   =          227
07488
                                          MA   =          227
18275
                                          Ha   =            188
637  n
mi
                                          Hp   =            181
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10040809
78                 X    =         3054137
40
 Y    =        9293999
57  feet           Y    =         2866999
25  meter
 Z    =      -17292090
90                 Z    =        -5255777
55
 XDOT =     -18436
439548                 XDOT =       -5675
518807
 YDOT =      17201
049571  feet/sec       YDOT =        5179
726499  meter/sec
 ZDOT =      -1429
896203                 ZDOT =        -463
267224

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2655149
69                 X    =          809289
63
 Y    =       13497629
65  feet           Y    =         4114077
52  meter
 Z    =      -17233016
88                 Z    =        -5252623
55
 XDOT =     -24054
048680                 XDOT =       -7331
674038
 YDOT =       2728
489581  feet/sec       YDOT =         831
643624  meter/sec
 ZDOT =      -1538
594090                 ZDOT =        -468
963479


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   10045
51663699  
00016717  00000-0  10270-3 0  9136
2 25544  51
6451 140
4223 0011455 322
7341  37
3027 15
75801372  4159


Satellite: ISS
Catalog Number: 25544
Epoch time:      10045
51663699   =   yrday
fracday
Element set:     913
Inclination:       51
6451  deg
RA of node:       140
4223  deg
Eccentricity:     
0011455     
Arg of perigee:   322
7341  deg
Mean anomaly:      37
3027  deg
Mean motion:   15
75801372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              279


Coasting Arc #15 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4841901
35                 A    =         6726969
70  meter
 Y    =       -4664250
95  meter          E    =           
0002135
 Z    =        -249195
23                 I    =           51
90369
 XDOT =       3136
409846                 Wp   =           64
17784
 YDOT =       3577
048594  meter/sec      RA   =          134
40539  deg
 ZDOT =      -6050
594839                 TA   =          118
51989
                                          MA   =          118
49839
                                          Ha   =            188
728  n
mi
                                          Hp   =            181
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15885503
12                 X    =         4894908
49
 Y    =      -15302660
59  feet           Y    =        -4609809
57  meter
 Z    =        -817569
66                 Z    =         -225544
85
 XDOT =      10290
058549                 XDOT =        3125
569505
 YDOT =      11735
723732  feet/sec       YDOT =        3612
060822  meter/sec
 ZDOT =     -19851
032936                 ZDOT =       -6035
385088

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21816151
75                 X    =         6649563
05
 Y    =       -3274231
46  feet           Y    =         -997985
75  meter
 Z    =        -723866
06                 Z    =         -220634
38
 XDOT =       1449
713579                 XDOT =         441
872699
 YDOT =      14002
761921  feet/sec       YDOT =        4268
041834  meter/sec
 ZDOT =     -19790
504518                 ZDOT =       -6032
145777


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   10046
53129811  
00016717  00000-0  10270-3 0  9143
2 25544  51
6443 135
1984 0011367 327
0840  32
9615 15
75821517  4314


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
53129811   =   yrday
fracday
Element set:     914
Inclination:       51
6443  deg
RA of node:       135
1984  deg
Eccentricity:     
0011367     
Arg of perigee:   327
0840  deg
Mean anomaly:      32
9615  deg
Mean motion:   15
75821517  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              291

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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