Date: January 13th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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


022/09:06:27 407 1 5 3 3 3 3
N/A 2 7 0 0 185 5
000/00:00:54 813 1 2 -0 0 179 7

024/09:15:15 470 -0 4 8 2 8 2
N/A -7 6 0 0 185 6
000/00:02:16 939 3 1 0 0 184 8

Coasting Arc #1 (Orbit 3878)
---------------------------------------

Vector Time (GMT): 2010/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3213848
15                 A    =         6720961
83  meter
 Y    =        5519504
49  meter          E    =           
0018659
 Z    =        2055881
36                 I    =           51
42196
 XDOT =      -5268
652837                 Wp   =          130
52472
 YDOT =       -994
254209  meter/sec      RA   =          315
08866  deg
 ZDOT =      -5546
034457                 TA   =           26
39998
                                          MA   =           26
30502
                                          Ha   =            186
587  n
mi
                                          Hp   =            177
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10544121
23                 X    =        -3285316
37
 Y    =       18108610
53  feet           Y    =         5483165
47  meter
 Z    =        6745017
57                 Z    =         2040095
75
 XDOT =     -17285
606419                 XDOT =       -5230
201948
 YDOT =      -3261
988874  feet/sec       YDOT =       -1052
955683  meter/sec
 ZDOT =     -18195
651106                 ZDOT =       -5571
536077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20644122
95                 X    =        -6292328
68
 Y    =       -3709256
16  feet           Y    =        -1130581
28  meter
 Z    =        6682599
49                 Z    =         2036856
32
 XDOT =      -3115
657204                 XDOT =        -949
652316
 YDOT =     -15747
224836  feet/sec       YDOT =       -4799
754130  meter/sec
 ZDOT =     -18296
629068                 ZDOT =       -5576
812540


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   10011
53572171  
00016717  00000-0  10270-3 0  9001
2 25544  51
6444 315
5024 0007191 172
6509 187
4762 15
77311535 38794


Satellite: ISS
Catalog Number: 25544
Epoch time:      10011
53572171   =   yrday
fracday
Element set:     900
Inclination:       51
6444  deg
RA of node:       315
5024  deg
Eccentricity:     
0007191     
Arg of perigee:   172
6509  deg
Mean anomaly:     187
4762  deg
Mean motion:   15
77311535  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3879
Checksum:              299


Coasting Arc #2 (Orbit 3894)
---------------------------------------

Vector Time (GMT): 2010/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3974901
06                 A    =         6710898
94  meter
 Y    =        1657885
63  meter          E    =           
0009972
 Z    =        5145176
69                 I    =           51
36853
 XDOT =      -4157
771404                 Wp   =          159
50494
 YDOT =       6389
135692  meter/sec      RA   =          309
93972  deg
 ZDOT =       1143
480816                 TA   =          279
49168
                                          MA   =          279
60437
                                          Ha   =            186
243  n
mi
                                          Hp   =            177
985

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13041013
99                 X    =         3931072
87
 Y    =        5439257
31  feet           Y    =         1702089
58  meter
 Z    =       16880500
95                 Z    =         5164380
27
 XDOT =     -13640
982298                 XDOT =       -4234
461579
 YDOT =      20961
731272  feet/sec       YDOT =        6342
212084  meter/sec
 ZDOT =       3751
577481                 ZDOT =        1123
097206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -415162
29                 X    =         -126541
47
 Y    =       14032378
16  feet           Y    =         4277068
86  meter
 Z    =       16956558
66                 Z    =         5168359
08
 XDOT =     -23452
001915                 XDOT =       -7148
170184
 YDOT =      -5168
821473  feet/sec       YDOT =       -1575
456785  meter/sec
 ZDOT =       3670
968158                 ZDOT =        1118
911094


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   10012
54940546  
00016717  00000-0  10270-3 0  9019
2 25544  51
6447 310
2720 0007199 178
1537 181
9655 15
77377835 38955


Satellite: ISS
Catalog Number: 25544
Epoch time:      10012
54940546   =   yrday
fracday
Element set:     901
Inclination:       51
6447  deg
RA of node:       310
2720  deg
Eccentricity:     
0007199     
Arg of perigee:   178
1537  deg
Mean anomaly:     181
9655  deg
Mean motion:   15
77377835  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3895
Checksum:              328


Coasting Arc #3 (Orbit 3910)
---------------------------------------

Vector Time (GMT): 2010/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3911413
16                 A    =         6722605
86  meter
 Y    =       -5464704
90  meter          E    =           
0009147
 Z    =         123698
63                 I    =           51
38922
 XDOT =       3840
227562                 Wp   =           80
25869
 YDOT =       2893
362009  meter/sec      RA   =          304
75129  deg
 ZDOT =       6016
199205                 TA   =          281
09087
                                          MA   =          281
19372
                                          Ha   =            186
266  n
mi
                                          Hp   =            178
133

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12832720
34                 X    =         3971628
86
 Y    =      -17928821
86  feet           Y    =        -5420628
50  meter
 Z    =         405835
41                 Z    =          142845
50
 XDOT =      12599
171792                 XDOT =        3778
362976
 YDOT =       9492
657510  feet/sec       YDOT =        2935
959028  meter/sec
 ZDOT =      19738
186368                 ZDOT =        6034
704808

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21437565
42                 X    =         6534169
94
 Y    =        5146353
63  feet           Y    =         1568608
59  meter
 Z    =         481560
27                 Z    =          146779
57
 XDOT =      -3726
856132                 XDOT =       -1135
945749
 YDOT =      13573
537806  feet/sec       YDOT =        4137
214323  meter/sec
 ZDOT =      19811
505965                 ZDOT =        6038
547018


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   10013
56307562  
00016717  00000-0  10270-3 0  9028
2 25544  51
6445 305
0404 0007117 181
2214 178
8935 15
77365318 39119


Satellite: ISS
Catalog Number: 25544
Epoch time:      10013
56307562   =   yrday
fracday
Element set:     902
Inclination:       51
6445  deg
RA of node:       305
0404  deg
Eccentricity:     
0007117     
Arg of perigee:   181
2214  deg
Mean anomaly:     178
8935  deg
Mean motion:   15
77365318  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3911
Checksum:              291


Coasting Arc #4 (Orbit 3925)
---------------------------------------

Vector Time (GMT): 2010/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2745271
84                 A    =         6711177
88  meter
 Y    =       -3420378
78  meter          E    =           
0016319
 Z    =       -5093151
49                 I    =           51
33529
 XDOT =       4690
466256                 Wp   =          126
54747
 YDOT =      -5926
625798  meter/sec      RA   =          299
55638  deg
 ZDOT =       1445
515054                 TA   =          157
40925
                                          MA   =          157
33733
                                          Ha   =            186
088  n
mi
                                          Hp   =            178
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9006797
39                 X    =        -2682079
45
 Y    =      -11221715
17  feet           Y    =        -3450724
11  meter
 Z    =      -16709814
61                 Z    =        -5106334
65
 XDOT =      15388
668819                 XDOT =        4749
368325
 YDOT =     -19444
310362  feet/sec       YDOT =       -5873
845061  meter/sec
 ZDOT =       4742
503457                 ZDOT =        1468
443234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6832777
48                 X    =         2082630
58
 Y    =      -12594171
59  feet           Y    =        -3838703
50  meter
 Z    =      -16762075
90                 Z    =        -5109080
73
 XDOT =      22990
438810                 XDOT =        7007
485749
 YDOT =       6012
680018  feet/sec       YDOT =        1832
664869  meter/sec
 ZDOT =       4833
189666                 ZDOT =        1473
156210


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   10014
51337470  
00016717  00000-0  10270-3 0  9036
2 25544  51
6452 300
1361 0007077 184
9351 175
1746 15
77390015 39260


Satellite: ISS
Catalog Number: 25544
Epoch time:      10014
51337470   =   yrday
fracday
Element set:     903
Inclination:       51
6452  deg
RA of node:       300
1361  deg
Eccentricity:     
0007077     
Arg of perigee:   184
9351  deg
Mean anomaly:     175
1746  deg
Mean motion:   15
77390015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3926
Checksum:              290


Coasting Arc #5 (Orbit 3941)
---------------------------------------

Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4188323
58                 A    =         6720018
76  meter
 Y    =        4695859
58  meter          E    =           
0011321
 Z    =       -2342942
36                 I    =           51
35213
 XDOT =      -2502
367898                 Wp   =          164
63645
 YDOT =      -4911
756463  meter/sec      RA   =          294
40767  deg
 ZDOT =      -5387
793680                 TA   =           41
90170
                                          MA   =           41
81512
                                          Ha   =            185
862  n
mi
                                          Hp   =            178
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13741219
09                 X    =        -4229140
91
 Y    =       15406363
45  feet           Y    =         4648795
28  meter
 Z    =       -7686818
75                 Z    =        -2363387
42
 XDOT =      -8209
868431                 XDOT =       -2421
085488
 YDOT =     -16114
686560  feet/sec       YDOT =       -4939
284403  meter/sec
 ZDOT =     -17676
488450                 ZDOT =       -5399
752960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19651401
65                 X    =        -5989747
22
 Y    =       -6224927
59  feet           Y    =        -1897357
93  meter
 Z    =       -7767690
07                 Z    =        -2367591
93
 XDOT =      10956
293703                 XDOT =        3339
478321
 YDOT =     -12538
829029  feet/sec       YDOT =       -3821
835088  meter/sec
 ZDOT =     -17723
939778                 ZDOT =       -5402
256844


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   10015
52701111  
00016717  00000-0  10270-3 0  9046
2 25544  51
6457 294
9051 0007084 188
9599 171
1441 15
77416793 39425


Satellite: ISS
Catalog Number: 25544
Epoch time:      10015
52701111   =   yrday
fracday
Element set:     904
Inclination:       51
6457  deg
RA of node:       294
9051  deg
Eccentricity:     
0007084     
Arg of perigee:   188
9599  deg
Mean anomaly:     171
1441  deg
Mean motion:   15
77416793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3942
Checksum:              315


Coasting Arc #6 (Orbit 3957)
---------------------------------------

Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1685430
94                 A    =         6715140
32  meter
 Y    =        5062680
67  meter          E    =           
0009815
 Z    =        4066374
42                 I    =           51
32365
 XDOT =      -4835
222024                 Wp   =          116
30643
 YDOT =       4658
725117  meter/sec      RA   =          289
17828  deg
 ZDOT =      -3793
305228                 TA   =           12
76063
                                          MA   =           12
73581
                                          Ha   =            185
720  n
mi
                                          Hp   =            178
557

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5529629
05                 X    =         1608940
66
 Y    =       16609844
73  feet           Y    =         5081100
15  meter
 Z    =       13341123
44                 Z    =         4074376
67
 XDOT =     -15863
589319                 XDOT =       -4868
530617
 YDOT =      15284
531225  feet/sec       YDOT =        4604
468878  meter/sec
 ZDOT =     -12445
227127                 ZDOT =       -3816
874675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12740570
51                 X    =        -3883325
89
 Y    =       11970473
03  feet           Y    =         3648600
18  meter
 Z    =       13372918
63                 Z    =         4076065
60
 XDOT =     -19658
841422                 XDOT =       -5992
014865
 YDOT =      -6906
021610  feet/sec       YDOT =       -2104
955387  meter/sec
 ZDOT =     -12538
466713                 ZDOT =       -3821
724654


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   10016
54063134  
00016717  00000-0  10270-3 0  9056
2 25544  51
6449 289
6743 0007046 192
5465 167
5526 15
77437586 39589


Satellite: ISS
Catalog Number: 25544
Epoch time:      10016
54063134   =   yrday
fracday
Element set:     905
Inclination:       51
6449  deg
RA of node:       289
6743  deg
Eccentricity:     
0007046     
Arg of perigee:   192
5465  deg
Mean anomaly:     167
5526  deg
Mean motion:   15
77437586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3958
Checksum:              339


Coasting Arc #7 (Orbit 3973)
---------------------------------------

Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4204390
98                 A    =         6714866
67  meter
 Y    =       -3240887
81  meter          E    =           
0012373
 Z    =        4111496
98                 I    =           51
31447
 XDOT =       1424
829210                 Wp   =          139
29025
 YDOT =       6592
925256  meter/sec      RA   =          284
04453  deg
 ZDOT =       3724
297887                 TA   =          272
37930
                                          MA   =          272
52095
                                          Ha   =            185
566  n
mi
                                          Hp   =            178
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13793933
65                 X    =         4220346
26
 Y    =      -10632834
03  feet           Y    =        -3193782
87  meter
 Z    =       13489163
31                 Z    =         4131959
96
 XDOT =       4674
636515                 XDOT =        1332
908538
 YDOT =      21630
332205  feet/sec       YDOT =        6608
344351  meter/sec
 ZDOT =      12218
825088                 ZDOT =        3730
996681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15572687
39                 X    =         4746555
12
 Y    =        7657045
56  feet           Y    =         2333867
49  meter
 Z    =       13570127
21                 Z    =         4136174
77
 XDOT =     -16857
896960                 XDOT =       -5138
286993
 YDOT =      12493
244178  feet/sec       YDOT =        3807
940825  meter/sec
 ZDOT =      12245
503489                 ZDOT =        3732
429463


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   10017
55423438  
00016717  00000-0  10270-3 0  9066
2 25544  51
6451 284
4424 0007008 196
7644 163
3290 15
77464883 39744


Satellite: ISS
Catalog Number: 25544
Epoch time:      10017
55423438   =   yrday
fracday
Element set:     906
Inclination:       51
6451  deg
RA of node:       284
4424  deg
Eccentricity:     
0007008     
Arg of perigee:   196
7644  deg
Mean anomaly:     163
3290  deg
Mean motion:   15
77464883  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3974
Checksum:              324


Coasting Arc #8 (Orbit 3988)
---------------------------------------

Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -851273
80                 A    =         6719976
73  meter
 Y    =       -6275725
56  meter          E    =           
0002736
 Z    =       -2252333
23                 I    =           51
32622
 XDOT =       4800
744980                 Wp   =          144
31622
 YDOT =      -2599
429678  meter/sec      RA   =          278
81337  deg
 ZDOT =       5429
517760                 TA   =          190
26730
                                          MA   =          190
27289
                                          Ha   =            185
397  n
mi
                                          Hp   =            178
811

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2792893
04                 X    =         -770093
08
 Y    =      -20589650
80  feet           Y    =        -6284791
01  meter
 Z    =       -7389544
72                 Z    =        -2256271
72
 XDOT =      15750
475655                 XDOT =        4803
080442
 YDOT =      -8528
312592  feet/sec       YDOT =       -2545
732089  meter/sec
 ZDOT =      17813
378478                 ZDOT =        5452
844810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17093931
16                 X    =         5210230
22
 Y    =      -11802476
35  feet           Y    =        -3597394
79  meter
 Z    =       -7405296
23                 Z    =        -2257134
29
 XDOT =      13843
720138                 XDOT =        4219
565898
 YDOT =       8817
961619  feet/sec       YDOT =        2687
714702  meter/sec
 ZDOT =      17905
696693                 ZDOT =        5457
656352


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   10018
50447197  
00016717  00000-0  10270-3 0  9071
2 25544  51
6453 279
5375 0007020 201
0111 159
0766 15
77510077 39892


Satellite: ISS
Catalog Number: 25544
Epoch time:      10018
50447197   =   yrday
fracday
Element set:     907
Inclination:       51
6453  deg
RA of node:       279
5375  deg
Eccentricity:     
0007020     
Arg of perigee:   201
0111  deg
Mean anomaly:     159
0766  deg
Mean motion:   15
77510077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3989
Checksum:              307


Coasting Arc #9 (Orbit 4004)
---------------------------------------

Vector Time (GMT): 2010/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4186343
93                 A    =         6710569
56  meter
 Y    =        1178317
74  meter          E    =           
0011656
 Z    =       -5119315
43                 I    =           51
29132
 XDOT =       -555
345559                 Wp   =          109
05723
 YDOT =      -7569
502455  meter/sec      RA   =          273
65872  deg
 ZDOT =      -1294
295575                 TA   =          148
53725
                                          MA   =          148
46748
                                          Ha   =            185
097  n
mi
                                          Hp   =            178
866

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13734724
18                 X    =        -4174340
73
 Y    =        3865871
85  feet           Y    =         1131570
83  meter
 Z    =      -16795654
31                 Z    =        -5139623
10
 XDOT =      -1821
999866                 XDOT =        -464
373442
 YDOT =     -24834
325640  feet/sec       YDOT =       -7575
203967  meter/sec
 ZDOT =      -4246
376557                 ZDOT =       -1296
772653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9815150
16                 X    =        -2991657
77
 Y    =      -10224646
74  feet           Y    =        -3116472
33  meter
 Z    =      -16876049
41                 Z    =        -5143819
86
 XDOT =      20337
635338                 XDOT =        6198
911251
 YDOT =     -12530
995832  feet/sec       YDOT =       -3819
447529  meter/sec
 ZDOT =      -4256
384620                 ZDOT =       -1297
346032


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   10019
51804292  
00016717  00000-0  10270-3 0  9087
2 25544  51
6453 274
3056 0006935 205
5858 154
4965 15
77542852 40058


Satellite: ISS
Catalog Number: 25544
Epoch time:      10019
51804292   =   yrday
fracday
Element set:     908
Inclination:       51
6453  deg
RA of node:       274
3056  deg
Eccentricity:     
0006935     
Arg of perigee:   205
5858  deg
Mean anomaly:     154
4965  deg
Mean motion:   15
77542852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4005
Checksum:              319


Coasting Arc #10 (Orbit 4020)
---------------------------------------

Vector Time (GMT): 2010/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         138102
77                 A    =         6722221
09  meter
 Y    =        6710633
48  meter          E    =           
0015725
 Z    =         -52537
34                 I    =           51
32940
 XDOT =      -4818
675119                 Wp   =          160
99491
 YDOT =         56
089484  meter/sec      RA   =          268
46212  deg
 ZDOT =      -6020
729966                 TA   =           19
57949
                                          MA   =           19
51917
                                          Ha   =            185
097  n
mi
                                          Hp   =            179
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         453093
07                 X    =           63308
23
 Y    =       22016514
03  feet           Y    =         6711759
63  meter
 Z    =        -172366
61                 Z    =          -52047
97
 XDOT =     -15809
301572                 XDOT =       -4789
697041
 YDOT =        184
020616  feet/sec       YDOT =           2
366368  meter/sec
 ZDOT =     -19753
051070                 ZDOT =       -6044
068325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19038195
47                 X    =        -5802841
98
 Y    =       11067069
35  feet           Y    =         3373242
74  meter
 Z    =        -170243
79                 Z    =          -51890
31
 XDOT =      -6958
877853                 XDOT =       -2121
065970
 YDOT =     -12249
843940  feet/sec       YDOT =       -3733
752433  meter/sec
 ZDOT =     -19845
479692                 ZDOT =       -6048
902210


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   10020
53159900  
00016717  00000-0  10270-3 0  9091
2 25544  51
6451 269
0736 0007119 209
2357 150
8411 15
77506462 40213


Satellite: ISS
Catalog Number: 25544
Epoch time:      10020
53159900   =   yrday
fracday
Element set:     909
Inclination:       51
6451  deg
RA of node:       269
0736  deg
Eccentricity:     
0007119     
Arg of perigee:   209
2357  deg
Mean anomaly:     150
8411  deg
Mean motion:   15
77506462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4021
Checksum:              288


Coasting Arc #11 (Orbit 4036)
---------------------------------------

Vector Time (GMT): 2010/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4235610
79                 A    =         6710482
82  meter
 Y    =        1083661
61  meter          E    =           
0003111
 Z    =        5090419
02                 I    =           51
29283
 XDOT =       -244
618638                 Wp   =          186
41480
 YDOT =       7573
068817  meter/sec      RA   =          263
26309  deg
 ZDOT =      -1411
769801                 TA   =          277
14308
                                          MA   =          277
17846
                                          Ha   =            184
614  n
mi
                                          Hp   =            179
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13896360
86                 X    =         4198450
26
 Y    =        3555320
24  feet           Y    =         1130818
83  meter
 Z    =       16700849
79                 Z    =         5110905
12
 XDOT =       -802
554587                 XDOT =        -322
425813
 YDOT =      24846
026302  feet/sec       YDOT =        7569
898336  meter/sec
 ZDOT =      -4631
790687                 ZDOT =       -1413
146961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3813442
81                 X    =         1162337
37
 Y    =       13729133
26  feet           Y    =         4184639
82  meter
 Z    =       16782016
71                 Z    =         5115158
69
 XDOT =     -20909
089837                 XDOT =       -6373
090582
 YDOT =      11463
393475  feet/sec       YDOT =        3494
042331  meter/sec
 ZDOT =      -4637
028320                 ZDOT =       -1413
366232


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   10021
54513552  
00016717  00000-0  10270-3 0  9102
2 25544  51
6451 263
8412 0006973 215
1688 144
9018 15
77608620 40379


Satellite: ISS
Catalog Number: 25544
Epoch time:      10021
54513552   =   yrday
fracday
Element set:     910
Inclination:       51
6451  deg
RA of node:       263
8412  deg
Eccentricity:     
0006973     
Arg of perigee:   215
1688  deg
Mean anomaly:     144
9018  deg
Mean motion:   15
77608620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4037
Checksum:              295


Coasting Arc #12 (Orbit 4050)
---------------------------------------

Vector Time (GMT): 2010/022/09:06:54
813
Vector Time (MET): N/A
Weight (LBS)     : 751525
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3102502
99                 A    =         6714008
82  meter
 Y    =       -3664798
98  meter          E    =           
0009340
 Z    =        4691922
18                 I    =           51
30118
 XDOT =       3447
929360                 Wp   =          148
51233
 YDOT =       6352
384817  meter/sec      RA   =          258
73228  deg
 ZDOT =       2671
586781                 TA   =          275
05990
                                          MA   =          275
16650
                                          Ha   =            185
541  n
mi
                                          Hp   =            179
714

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10178815
59                 X    =         3120460
55
 Y    =      -12023618
72  feet           Y    =        -3630004
69  meter
 Z    =       15393445
46                 Z    =         4707037
50
 XDOT =      11312
104200                 XDOT =        3363
661652
 YDOT =      20841
157537  feet/sec       YDOT =        6390
470361  meter/sec
 ZDOT =       8765
048495                 ZDOT =        2688
132162

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9569800
83                 X    =         2916875
29
 Y    =       12439905
14  feet           Y    =         3791683
09  meter
 Z    =       15453204
49                 Z    =         4710136
73
 XDOT =     -21869
564874                 XDOT =       -6665
843374
 YDOT =       5812
403409  feet/sec       YDOT =        1771
620559  meter/sec
 ZDOT =       8830
765154                 ZDOT =        2691
617219


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   10022
43199557  
00016717  00000-0  10270-3 0  9117
2 25544  51
6435 259
2624 0004704 203
8713 156
2234 15
76984436 40511


Satellite: ISS
Catalog Number: 25544
Epoch time:      10022
43199557   =   yrday
fracday
Element set:     911
Inclination:       51
6435  deg
RA of node:       259
2624  deg
Eccentricity:     
0004704     
Arg of perigee:   203
8713  deg
Mean anomaly:     156
2234  deg
Mean motion:   15
76984436  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4051
Checksum:              302


Coasting Arc #13 (Orbit 4065)
---------------------------------------

Vector Time (GMT): 2010/023/09:06:54
813
Vector Time (MET): N/A
Weight (LBS)     : 751525
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2906498
22                 A    =         6722802
98  meter
 Y    =       -5898679
26  meter          E    =           
0004143
 Z    =       -1391583
71                 I    =           51
33841
 XDOT =       3870
261575                 Wp   =           46
91202
 YDOT =      -3271
893596  meter/sec      RA   =          253
51631  deg
 ZDOT =       5799
094329                 TA   =          297
71270
                                          MA   =          297
75472
                                          Ha   =            185
429  n
mi
                                          Hp   =            179
831

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9535755
32                 X    =        -2833562
12
 Y    =      -19352622
23  feet           Y    =        -5930773
57  meter
 Z    =       -4565563
36                 Z    =        -1405526
46
 XDOT =      12697
708579                 XDOT =        3878
390081
 YDOT =     -10734
559042  feet/sec       YDOT =       -3228
568834  meter/sec
 ZDOT =      19025
900030                 ZDOT =        5817
915525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20854724
43                 X    =         6356520
01
 Y    =       -5479611
25  feet           Y    =        -1670185
51  meter
 Z    =       -4620964
73                 Z    =        -1408470
05
 XDOT =       7623
692294                 XDOT =        2323
701411
 YDOT =      12944
766390  feet/sec       YDOT =        3945
564796  meter/sec
 ZDOT =      19100
349793                 ZDOT =        5821
786617


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   10023
38253523  
00016717  00000-0  10270-3 0  9127
2 25544  51
6437 254
3593 0004606 208
5314 151
5599 15
76992058 40661


Satellite: ISS
Catalog Number: 25544
Epoch time:      10023
38253523   =   yrday
fracday
Element set:     912
Inclination:       51
6437  deg
RA of node:       254
3593  deg
Eccentricity:     
0004606     
Arg of perigee:   208
5314  deg
Mean anomaly:     151
5599  deg
Mean motion:   15
76992058  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4066
Checksum:              312


Coasting Arc #14 (Orbit 4081)
---------------------------------------

Vector Time (GMT): 2010/024/09:06:54
813
Vector Time (MET): N/A
Weight (LBS)     : 751525
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3713618
48                 A    =         6711529
94  meter
 Y    =        1999597
36  meter          E    =           
0012859
 Z    =       -5231238
81                 I    =           51
31115
 XDOT =      -3158
719373                 Wp   =          103
27308
 YDOT =      -7005
319955  meter/sec      RA   =          248
35256  deg
 ZDOT =       -439
189043                 TA   =          162
55691
                                          MA   =          162
51270
                                          Ha   =            185
213  n
mi
                                          Hp   =            179
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12183787
68                 X    =        -3710290
10
 Y    =        6560358
78  feet           Y    =         1958088
40  meter
 Z    =      -17162856
98                 Z    =        -5249271
23
 XDOT =     -10363
252536                 XDOT =       -3078
016399
 YDOT =     -22983
333187  feet/sec       YDOT =       -7040
191365  meter/sec
 ZDOT =      -1440
908934                 ZDOT =        -454
338383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4257423
56                 X    =        -1297662
70
 Y    =      -13072968
00  feet           Y    =        -3984640
65  meter
 Z    =      -17234224
72                 Z    =        -5252991
69
 XDOT =      23527
942085                 XDOT =        7171
316747
 YDOT =      -5699
737084  feet/sec       YDOT =       -1737
279863  meter/sec
 ZDOT =      -1501
129622                 ZDOT =        -457
544309


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   10024
39642844  
00016717  00000-0  10270-3 0  9138
2 25544  51
6444 249
1295 0004546 212
3123 147
7764 15
77034783 40826


Satellite: ISS
Catalog Number: 25544
Epoch time:      10024
39642844   =   yrday
fracday
Element set:     913
Inclination:       51
6444  deg
RA of node:       249
1295  deg
Eccentricity:     
0004546     
Arg of perigee:   212
3123  deg
Mean anomaly:     147
7764  deg
Mean motion:   15
77034783  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4082
Checksum:              308


Coasting Arc #15 (Orbit 4081)
---------------------------------------

Vector Time (GMT): 2010/024/09:16:23
939
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4626724
19                 A    =         6719441
60  meter
 Y    =       -2120834
66  meter          E    =           
0004109
 Z    =       -4389917
09                 I    =           51
32318
 XDOT =         64
466536                 Wp   =          170
86526
 YDOT =      -6960
674728  meter/sec      RA   =          248
29072  deg
 ZDOT =       3291
280782                 TA   =          132
34986
                                          MA   =          132
31505
                                          Ha   =            185
606  n
mi
                                          Hp   =            184
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15179541
30                 X    =        -4581339
50
 Y    =       -6958118
96  feet           Y    =        -2172319
41  meter
 Z    =      -14402615
13                 Z    =        -4412283
44
 XDOT =        211
504384                 XDOT =         126
308909
 YDOT =     -22836
859343  feet/sec       YDOT =       -6959
608242  meter/sec
 ZDOT =      10798
165296                 ZDOT =        3291
743757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9011430
76                 X    =         2746684
10
 Y    =      -13966612
99  feet           Y    =        -4257023
64  meter
 Z    =      -14491275
07                 Z    =        -4416940
64
 XDOT =      21570
514377                 XDOT =        6574
692782
 YDOT =       2699
958340  feet/sec       YDOT =         822
947302  meter/sec
 ZDOT =      10799
787963                 ZDOT =        3291
775371


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   10024
39642748  
00016717  00000-0  10270-3 0  9142
2 25544  51
6444 249
1296 0008188 264
9536  95
0694 15
75489735 40820


Satellite: ISS
Catalog Number: 25544
Epoch time:      10024
39642748   =   yrday
fracday
Element set:     914
Inclination:       51
6444  deg
RA of node:       249
1296  deg
Eccentricity:     
0008188     
Arg of perigee:   264
9536  deg
Mean anomaly:      95
0694  deg
Mean motion:   15
75489735  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4082
Checksum:              346


Coasting Arc #16 (Orbit 4097)
---------------------------------------

Vector Time (GMT): 2010/025/09:20:23
939
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1297055
21                 A    =         6719842
78  meter
 Y    =        5018156
21  meter          E    =           
0002960
 Z    =       -4278623
46                 I    =           51
33736
 XDOT =      -5320
042708                 Wp   =          357
67025
 YDOT =      -4345
227390  meter/sec      RA   =          243
15676  deg
 ZDOT =      -3480
511721                 TA   =          236
94614
                                          MA   =          236
97457
                                          Ha   =            184
764  n
mi
                                          Hp   =            184
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4255430
47                 X    =        -1332288
13
 Y    =       16463767
09  feet           Y    =         5003455
11  meter
 Z    =      -14037478
56                 Z    =        -4285009
68
 XDOT =     -17454
208358                 XDOT =       -5254
150667
 YDOT =     -14255
995374  feet/sec       YDOT =       -4404
350557  meter/sec
 ZDOT =     -11419
001708                 ZDOT =       -3506
196552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15927462
06                 X    =        -4854690
44
 Y    =       -5896923
25  feet           Y    =        -1797382
21  meter
 Z    =      -14062623
08                 Z    =        -4286287
52
 XDOT =      15591
281460                 XDOT =        4752
222589
 YDOT =     -14613
968870  feet/sec       YDOT =       -4454
337712  meter/sec
 ZDOT =     -11520
885149                 ZDOT =       -3511
565793


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   10025
41129365  
00016717  00000-0  10270-3 0  9152
2 25544  51
6447 243
9069 0008248 269
4050  90
6169 15
75522581 40983


Satellite: ISS
Catalog Number: 25544
Epoch time:      10025
41129365   =   yrday
fracday
Element set:     915
Inclination:       51
6447  deg
RA of node:       243
9069  deg
Eccentricity:     
0008248     
Arg of perigee:   269
4050  deg
Mean anomaly:      90
6169  deg
Mean motion:   15
75522581  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4098
Checksum:              319


Coasting Arc #17 (Orbit 4113)
---------------------------------------

Vector Time (GMT): 2010/026/09:20:23
939
Vector Time (MET): N/A
Weight (LBS)     : 750815
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4859390
65                 A    =         6724878
29  meter
 Y    =        3850771
76  meter          E    =           
0005866
 Z    =        2595746
02                 I    =           51
36847
 XDOT =      -1519
761358                 Wp   =          116
34025
 YDOT =       5447
330063  meter/sec      RA   =          237
94211  deg
 ZDOT =      -5229
448828                 TA   =           34
03248
                                          MA   =           33
99487
                                          Ha   =            185
353  n
mi
                                          Hp   =            184
809

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15942882
70                 X    =         4803359
98
 Y    =       12633765
63  feet           Y    =         3904798
81  meter
 Z    =        8516227
09                 Z    =         2619216
91
 XDOT =      -4986
093695                 XDOT =       -1555
158029
 YDOT =      17871
817791  feet/sec       YDOT =        5430
137785  meter/sec
 ZDOT =     -17156
984344                 ZDOT =       -5236
917183

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13998674
45                 X    =        -4266795
97
 Y    =       14704763
96  feet           Y    =         4482012
06  meter
 Z    =        8609337
79                 Z    =         2624126
16
 XDOT =     -16293
215998                 XDOT =       -4966
172236
 YDOT =      -5436
129715  feet/sec       YDOT =       -1656
932337  meter/sec
 ZDOT =     -17186
402727                 ZDOT =       -5238
415551


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   10026
42614741  
00016717  00000-0  10270-3 0  9162
2 25544  51
6441 238
6839 0008157 272
9099  87
1132 15
75511736 41144


Satellite: ISS
Catalog Number: 25544
Epoch time:      10026
42614741   =   yrday
fracday
Element set:     916
Inclination:       51
6441  deg
RA of node:       238
6839  deg
Eccentricity:     
0008157     
Arg of perigee:   272
9099  deg
Mean anomaly:      87
1132  deg
Mean motion:   15
75511736  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4114
Checksum:              310

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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