Date: January 31st 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 162)
---------------------------------------

Vector Time (GMT): 2010/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5500562
76                 A    =         6727197
30  meter
 Y    =        3680562
04  meter          E    =           
0009351
 Z    =        1170198
28                 I    =           51
43280
 XDOT =      -1850
721342                 Wp   =          177
96925
 YDOT =       4630
688458  meter/sec      RA   =          221
89205  deg
 ZDOT =      -5873
040705                 TA   =          349
16412
                                          MA   =          349
18425
                                          Ha   =            186
113  n
mi
                                          Hp   =            183
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18046465
75                 X    =         5453312
82
 Y    =       12075334
77  feet           Y    =         3741808
32  meter
 Z    =        3839233
19                 Z    =         1196804
66
 XDOT =      -6071
920415                 XDOT =       -1873
835695
 YDOT =      15192
547436  feet/sec       YDOT =        4609
863761  meter/sec
 ZDOT =     -19268
506249                 ZDOT =       -5882
087053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1527527
32                 X    =          465590
33
 Y    =       21641012
02  feet           Y    =         6596180
46  meter
 Z    =        3944820
19                 Z    =         1202381
20
 XDOT =     -14073
398130                 XDOT =       -4289
571750
 YDOT =       4507
700191  feet/sec       YDOT =        1373
947018  meter/sec
 ZDOT =     -19304
197985                 ZDOT =       -5883
919546


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   10029
53402907  
00016717  00000-0  10270-3 0  9009
2 25544  51
6407 222
6960 0011599 260
2015  99
7839 15
75529921  1634


Satellite: ISS
Catalog Number: 25544
Epoch time:      10029
53402907   =   yrday
fracday
Element set:     900
Inclination:       51
6407  deg
RA of node:       222
6960  deg
Eccentricity:     
0011599     
Arg of perigee:   260
2015  deg
Mean anomaly:      99
7839  deg
Mean motion:   15
75529921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             163
Checksum:              307


Coasting Arc #2 (Orbit 178)
---------------------------------------

Vector Time (GMT): 2010/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1812818
16                 A    =         6716153
43  meter
 Y    =       -3837013
50  meter          E    =           
0009052
 Z    =        5213223
78                 I    =           51
41704
 XDOT =       6478
633647                 Wp   =          250
99418
 YDOT =       4087
061785  meter/sec      RA   =          216
74668  deg
 ZDOT =        753
456863                 TA   =          191
80145
                                          MA   =          191
82268
                                          Ha   =            186
019  n
mi
                                          Hp   =            183
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5947566
13                 X    =         1830265
53
 Y    =      -12588626
97  feet           Y    =        -3816644
12  meter
 Z    =       17103752
55                 Z    =         5222072
40
 XDOT =      21255
359733                 XDOT =        6428
789860
 YDOT =      13408
995359  feet/sec       YDOT =        4159
230987  meter/sec
 ZDOT =       2471
971334                 ZDOT =         784
808090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13471663
71                 X    =         4106163
10
 Y    =       -3341430
33  feet           Y    =        -1018467
96  meter
 Z    =       17138685
57                 Z    =         5223871
36
 XDOT =       2634
836366                 XDOT =         803
098124
 YDOT =      23971
088893  feet/sec       YDOT =        7306
387895  meter/sec
 ZDOT =       2596
400799                 ZDOT =         791
382964


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   10030
54889778  
00016717  00000-0  10270-3 0  9018
2 25544  51
6396 217
4713 0011417 263
0162  96
9703 15
75458967  1799


Satellite: ISS
Catalog Number: 25544
Epoch time:      10030
54889778   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:       217
4713  deg
Eccentricity:     
0011417     
Arg of perigee:   263
0162  deg
Mean anomaly:      96
9703  deg
Mean motion:   15
75458967  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             179
Checksum:              331


Coasting Arc #3 (Orbit 193)
---------------------------------------

Vector Time (GMT): 2010/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5780192
98                 A    =         6727828
92  meter
 Y    =       -3429807
54  meter          E    =           
0008506
 Z    =        -131612
92                 I    =           51
48193
 XDOT =       2345
108726                 Wp   =          338
15287
 YDOT =      -4187
853586  meter/sec      RA   =          211
57679  deg
 ZDOT =       6025
234136                 TA   =           20
41329
                                          MA   =           20
37931
                                          Ha   =            185
709  n
mi
                                          Hp   =            183
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18963887
73                 X    =        -5740771
34
 Y    =      -11252649
41  feet           Y    =        -3494224
66  meter
 Z    =        -431800
93                 Z    =         -159596
47
 XDOT =       7693
926266                 XDOT =        2362
495174
 YDOT =     -13739
677119  feet/sec       YDOT =       -4161
531984  meter/sec
 ZDOT =      19767
828531                 ZDOT =        6036
668542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3503289
02                 X    =        -1067802
49
 Y    =      -21768552
19  feet           Y    =        -6635054
71  meter
 Z    =        -542872
06                 Z    =         -165467
41
 XDOT =      13817
229574                 XDOT =        4211
491574
 YDOT =      -2725
349799  feet/sec       YDOT =        -830
686619  meter/sec
 ZDOT =      19812
995336                 ZDOT =        6039
000978


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   10031
50031992  
00016717  00000-0  10270-3 0  9023
2 25544  51
6395 212
5731 0011503 266
3429  93
6420 15
75523902  1941


Satellite: ISS
Catalog Number: 25544
Epoch time:      10031
50031992   =   yrday
fracday
Element set:     902
Inclination:       51
6395  deg
RA of node:       212
5731  deg
Eccentricity:     
0011503     
Arg of perigee:   266
3429  deg
Mean anomaly:      93
6420  deg
Mean motion:   15
75523902  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             194
Checksum:              278


Coasting Arc #4 (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    =       -2311542
23                 A    =         6715718
31  meter
 Y    =        3511373
96  meter          E    =           
0003730
 Z    =       -5240334
92                 I    =           51
46814
 XDOT =      -6716
196946                 Wp   =          103
58013
 YDOT =      -3741
011229  meter/sec      RA   =          206
41557  deg
 ZDOT =        455
234783                 TA   =          170
75698
                                          MA   =          170
75012
                                          Ha   =            185
407  n
mi
                                          Hp   =            183
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7583799
97                 X    =        -2325179
32
 Y    =       11520255
77  feet           Y    =         3485448
57  meter
 Z    =      -17192699
88                 Z    =        -5251597
29
 XDOT =     -22034
766884                 XDOT =       -6676
076525
 YDOT =     -12273
658889  feet/sec       YDOT =       -3815
891389  meter/sec
 ZDOT =       1493
552437                 ZDOT =         422
705902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13609318
65                 X    =        -4148120
32
 Y    =        1866625
53  feet           Y    =          568947
46  meter
 Z    =      -17237209
73                 Z    =        -5253901
52
 XDOT =      -4982
982013                 XDOT =       -1518
812918
 YDOT =     -23712
602401  feet/sec       YDOT =       -7227
601212  meter/sec
 ZDOT =       1364
435736                 ZDOT =         415
880012


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
51515845  
00016717  00000-0  10270-3 0  9030
2 25544  51
6399 207
3494 0011328 270
0121  89
9745 15
75556268  2107


Satellite: ISS
Catalog Number: 25544
Epoch time:      10032
51515845   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       207
3494  deg
Eccentricity:     
0011328     
Arg of perigee:   270
0121  deg
Mean anomaly:      89
9745  deg
Mean motion:   15
75556268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             210
Checksum:              301


Coasting Arc #5 (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    =        5897585
89                 A    =         6727235
82  meter
 Y    =        3088730
67  meter          E    =           
0008517
 Z    =        -929973
38                 I    =           51
53553
 XDOT =      -2981
915527                 Wp   =          216
50837
 YDOT =       3899
935298  meter/sec      RA   =          201
27095  deg
 ZDOT =      -5936
412796                 TA   =          333
66853
                                          MA   =          333
71180
                                          Ha   =            185
626  n
mi
                                          Hp   =            183
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19349035
08                 X    =         5867126
39
 Y    =       10133630
82  feet           Y    =         3154510
64  meter
 Z    =       -3051093
78                 Z    =         -901397
59
 XDOT =      -9783
187425                 XDOT =       -2996
466270
 YDOT =      12795
063313  feet/sec       YDOT =        3866
508239  meter/sec
 ZDOT =     -19476
419936                 ZDOT =       -5950
934074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5354595
56                 X    =         1632080
73
 Y    =       21191583
87  feet           Y    =         6459194
76  meter
 Z    =       -2937666
59                 Z    =         -895400
78
 XDOT =     -14437
195578                 XDOT =       -4400
457212
 YDOT =        930
135438  feet/sec       YDOT =         283
505281  meter/sec
 ZDOT =     -19533
835242                 ZDOT =       -5953
912982


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
52998087  
00016717  00000-0  10270-3 0  9046
2 25544  51
6403 202
1255 0011404 275
3033  84
6830 15
75614944  2266


Satellite: ISS
Catalog Number: 25544
Epoch time:      10033
52998087   =   yrday
fracday
Element set:     904
Inclination:       51
6403  deg
RA of node:       202
1255  deg
Eccentricity:     
0011404     
Arg of perigee:   275
3033  deg
Mean anomaly:      84
6830  deg
Mean motion:   15
75614944  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             226
Checksum:              286


Coasting Arc #6 (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    =        2913365
31                 A    =         6716566
22  meter
 Y    =       -3339557
22  meter          E    =           
0008321
 Z    =        5054098
71                 I    =           51
52748
 XDOT =       6733
597945                 Wp   =          302
71886
 YDOT =       3330
662595  meter/sec      RA   =          196
09264  deg
 ZDOT =      -1678
287270                 TA   =          163
46474
                                          MA   =          163
43759
                                          Ha   =            185
865  n
mi
                                          Hp   =            183
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9558285
14                 X    =         2925940
82
 Y    =      -10956552
57  feet           Y    =        -3306907
84  meter
 Z    =       16581688
67                 Z    =         5068282
20
 XDOT =      22091
856774                 XDOT =        6704
006109
 YDOT =      10927
370718  feet/sec       YDOT =        3405
796191  meter/sec
 ZDOT =      -5506
191830                 ZDOT =       -1645
647945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14466999
50                 X    =         4409541
45
 Y    =        -499097
38  feet           Y    =         -152124
88  meter
 Z    =       16637790
88                 Z    =         5071198
66
 XDOT =       6972
343759                 XDOT =        2125
170378
 YDOT =      22603
982684  feet/sec       YDOT =        6889
693922  meter/sec
 ZDOT =      -5376
633826                 ZDOT =       -1638
797990


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
54479220  
00016717  00000-0  10270-3 0  9053
2 25544  51
6402 196
9013 0011237 277
9219  82
0669 15
75553607  2423


Satellite: ISS
Catalog Number: 25544
Epoch time:      10034
54479220   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       196
9013  deg
Eccentricity:     
0011237     
Arg of perigee:   277
9219  deg
Mean anomaly:      82
0669  deg
Mean motion:   15
75553607  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             242
Checksum:              300


Coasting Arc #7 (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    =       -5806909
89                 A    =         6725857
90  meter
 Y    =       -2734636
11  meter          E    =           
0007817
 Z    =        1992126
64                 I    =           51
58970
 XDOT =       3703
783778                 Wp   =           15
16576
 YDOT =      -3795
545921  meter/sec      RA   =          190
97108  deg
 ZDOT =       5588
537147                 TA   =            7
06189
                                          MA   =            7
05088
                                          Ha   =            186
185  n
mi
                                          Hp   =            183
788

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19051541
63                 X    =        -5785576
38
 Y    =       -8971903
23  feet           Y    =        -2799453
13  meter
 Z    =        6535848
56                 Z    =         1963968
90
 XDOT =      12151
521583                 XDOT =        3718
803254
 YDOT =     -12452
578481  feet/sec       YDOT =       -3754
044024  meter/sec
 ZDOT =      18335
095625                 ZDOT =        5606
566363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6727658
08                 X    =        -2050590
18
 Y    =      -19991084
32  feet           Y    =        -6093282
50  meter
 Z    =        6424077
14                 Z    =         1958058
71
 XDOT =      15865
573218                 XDOT =        4835
826717
 YDOT =        572
889588  feet/sec       YDOT =         174
616746  meter/sec
 ZDOT =      18406
434348                 ZDOT =        5610
281189


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
55958460  
00016717  00000-0  10270-3 0  9064
2 25544  51
6411 191
6773 0011315 281
6117  78
3777 15
75635446  2581


Satellite: ISS
Catalog Number: 25544
Epoch time:      10035
55958460   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:       191
6773  deg
Eccentricity:     
0011315     
Arg of perigee:   281
6117  deg
Mean anomaly:      78
3777  deg
Mean motion:   15
75635446  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             258
Checksum:              319


Coasting Arc #8 (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    =       -3539346
97                 A    =         6718060
37  meter
 Y    =        3334821
83  meter          E    =           
0000807
 Z    =       -4634909
41                 I    =           51
59412
 XDOT =      -6519
190672                 Wp   =          223
71412
 YDOT =      -2940
311358  meter/sec      RA   =          185
78084  deg
 ZDOT =       2861
811433                 TA   =           74
59138
                                          MA   =           74
58246
                                          Ha   =            186
439  n
mi
                                          Hp   =            183
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11612030
73                 X    =        -3553859
24
 Y    =       10941016
51  feet           Y    =         3295161
69  meter
 Z    =      -15206395
69                 Z    =        -4652138
52
 XDOT =     -21388
420840                 XDOT =       -6499
729044
 YDOT =      -9646
690807  feet/sec       YDOT =       -3013
104040  meter/sec
 ZDOT =       9389
145120                 ZDOT =        2830
188859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15881987
37                 X    =        -4840829
75
 Y    =        -478530
22  feet           Y    =         -145856
01  meter
 Z    =      -15274588
57                 Z    =        -4655694
60
 XDOT =      -8283
523460                 XDOT =       -2524
817951
 YDOT =     -20860
604798  feet/sec       YDOT =       -6358
312342  meter/sec
 ZDOT =       9263
614740                 ZDOT =        2823
549773


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
51094122  
00016717  00000-0  10270-3 0  9078
2 25544  51
6416 186
7807 0011259 285
7054  74
2868 15
75639767  2734


Satellite: ISS
Catalog Number: 25544
Epoch time:      10036
51094122   =   yrday
fracday
Element set:     907
Inclination:       51
6416  deg
RA of node:       186
7807  deg
Eccentricity:     
0011259     
Arg of perigee:   285
7054  deg
Mean anomaly:      74
2868  deg
Mean motion:   15
75639767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             273
Checksum:              326


Coasting Arc #9 (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    =        5514741
78                 A    =         6723630
81  meter
 Y    =        2425588
69  meter          E    =           
0006758
 Z    =       -2982467
28                 I    =           51
64293
 XDOT =      -4407
419787                 Wp   =          289
07674
 YDOT =       3886
906210  meter/sec      RA   =          180
67722  deg
 ZDOT =      -4977
093293                 TA   =          285
37958
                                          MA   =          285
45424
                                          Ha   =            186
816  n
mi
                                          Hp   =            183
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18092984
84                 X    =         5501696
62
 Y    =        7957968
15  feet           Y    =         2487184
96  meter
 Z    =       -9784997
63                 Z    =        -2955708
67
 XDOT =     -14460
038671                 XDOT =       -4426
378830
 YDOT =      12752
316962  feet/sec       YDOT =        3837
513982  meter/sec
 ZDOT =     -16329
046236                 ZDOT =       -4998
550151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7446112
00                 X    =         2269574
94
 Y    =       18365958
04  feet           Y    =         5597944
01  meter
 Z    =       -9678767
35                 Z    =        -2950088
29
 XDOT =     -17847
685783                 XDOT =       -5439
974627
 YDOT =      -1433
871150  feet/sec       YDOT =        -437
043926  meter/sec
 ZDOT =     -16413
994602                 ZDOT =       -5002
985555


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
52570600  
00016717  00000-0  10270-3 0  9081
2 25544  51
6415 181
5566 0011299 290
1157  69
8791 15
75672281  2896


Satellite: ISS
Catalog Number: 25544
Epoch time:      10037
52570600   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:       181
5566  deg
Eccentricity:     
0011299     
Arg of perigee:   290
1157  deg
Mean anomaly:      69
8791  deg
Mean motion:   15
75672281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             289
Checksum:              321


Coasting Arc #10 (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    =        4132859
91                 A    =         6720423
89  meter
 Y    =       -3492354
78  meter          E    =           
0006795
 Z    =        3990576
73                 I    =           51
66265
 XDOT =       6055
825081                 Wp   =            2
93527
 YDOT =       2650
741636  meter/sec      RA   =          175
47998  deg
 ZDOT =      -3944
988126                 TA   =          127
88877
                                          MA   =          127
82729
                                          Ha   =            187
055  n
mi
                                          Hp   =            183
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13559251
66                 X    =         4152219
71
 Y    =      -11457856
89  feet           Y    =        -3446030
61  meter
 Z    =       13092443
35                 Z    =         4010700
69
 XDOT =      19868
192523                 XDOT =        6044
897637
 YDOT =       8696
658912  feet/sec       YDOT =        2718
400528  meter/sec
 ZDOT =     -12942
874429                 ZDOT =       -3915
595877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17670172
21                 X    =         5385868
49
 Y    =         898783
33  feet           Y    =          273949
16  meter
 Z    =       13172132
15                 Z    =         4014865
88
 XDOT =       8626
243629                 XDOT =        2629
279058
 YDOT =      18713
933568  feet/sec       YDOT =        5704
006952  meter/sec
 ZDOT =     -12826
175839                 ZDOT =       -3909
418396


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
54045675  
00016717  00000-0  10270-3 0  9094
2 25544  51
6416 176
3325 0011235 293
7482  66
2503 15
75665958  3056


Satellite: ISS
Catalog Number: 25544
Epoch time:      10038
54045675   =   yrday
fracday
Element set:     909
Inclination:       51
6416  deg
RA of node:       176
3325  deg
Eccentricity:     
0011235     
Arg of perigee:   293
7482  deg
Mean anomaly:      66
2503  deg
Mean motion:   15
75665958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             305
Checksum:              314


Coasting Arc #11 (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    =       -5012380
94                 A    =         6720800
34  meter
 Y    =       -2249232
83  meter          E    =           
0003727
 Z    =        3867356
13                 I    =           51
69554
 XDOT =       5028
530083                 Wp   =           19
11176
 YDOT =      -4144
037770  meter/sec      RA   =          170
38620  deg
 ZDOT =       4109
545468                 TA   =           28
07123
                                          MA   =           28
05114
                                          Ha   =            187
338  n
mi
                                          Hp   =            183
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16444819
35                 X    =        -5005643
60
 Y    =       -7379372
82  feet           Y    =        -2305246
75  meter
 Z    =       12688176
30                 Z    =         3843022
77
 XDOT =      16497
802109                 XDOT =        5054
532717
 YDOT =     -13595
924441  feet/sec       YDOT =       -4087
660566  meter/sec
 ZDOT =      13482
760721                 ZDOT =        4134
036513

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7256108
92                 X    =        -2211662
00
 Y    =      -16573437
07  feet           Y    =        -5051583
62  meter
 Z    =       12591549
20                 Z    =         3837904
19
 XDOT =      20085
211768                 XDOT =        6121
972547
 YDOT =       1517
613575  feet/sec       YDOT =         462
568618  meter/sec
 ZDOT =      13579
760491                 ZDOT =        4139
110998


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
55518966  
00016717  00000-0  10270-3 0  9106
2 25544  51
6427 171
1083 0011356 297
7311  62
2701 15
75742336  3211


Satellite: ISS
Catalog Number: 25544
Epoch time:      10039
55518966   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:       171
1083  deg
Eccentricity:     
0011356     
Arg of perigee:   297
7311  deg
Mean anomaly:      62
2701  deg
Mean motion:   15
75742336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             321
Checksum:              291


Coasting Arc #12 (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    =       -4592396
95                 A    =         6722933
71  meter
 Y    =        3770176
76  meter          E    =           
0008692
 Z    =       -3132883
79                 I    =           51
73271
 XDOT =      -5407
342409                 Wp   =          323
79859
 YDOT =      -2542
009252  meter/sec      RA   =          165
19272  deg
 ZDOT =       4867
409894                 TA   =          359
75662
                                          MA   =          359
75704
                                          Ha   =            187
541  n
mi
                                          Hp   =            183
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15066919
12                 X    =        -4618995
82
 Y    =       12369346
31  feet           Y    =         3718673
26  meter
 Z    =      -10278490
11                 Z    =        -3155257
54
 XDOT =     -17740
624701                 XDOT =       -5402
159723
 YDOT =      -8339
925369  feet/sec       YDOT =       -2602
448581  meter/sec
 ZDOT =      15969
192566                 ZDOT =        4841
154176

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19437310
47                 X    =        -5924492
23
 Y    =        -611552
59  feet           Y    =         -186401
23  meter
 Z    =      -10367116
47                 Z    =        -3159897
10
 XDOT =      -7938
772957                 XDOT =       -2419
737997
 YDOT =     -16618
287581  feet/sec       YDOT =       -5065
254055  meter/sec
 ZDOT =      15864
913594                 ZDOT =        4835
625663


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
50649066  
00016717  00000-0  10270-3 0  9110
2 25544  51
6431 166
2114 0011436 302
3273  57
6783 15
75717852  3364


Satellite: ISS
Catalog Number: 25544
Epoch time:      10040
50649066   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:       166
2114  deg
Eccentricity:     
0011436     
Arg of perigee:   302
3273  deg
Mean anomaly:      57
6783  deg
Mean motion:   15
75717852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             336
Checksum:              288


Coasting Arc #13 (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    =        4385858
15                 A    =         6718203
55  meter
 Y    =        2245975
37  meter          E    =           
0010243
 Z    =       -4572008
07                 I    =           51
74621
 XDOT =      -5463
363101                 Wp   =            2
16914
 YDOT =       4507
467811  meter/sec      RA   =          160
09914  deg
 ZDOT =      -3016
830237                 TA   =          237
84561
                                          MA   =          237
94503
                                          Ha   =            187
810  n
mi
                                          Hp   =            182
962

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14389298
38                 X    =         4382626
64
 Y    =        7368685
60  feet           Y    =         2295002
70  meter
 Z    =      -15000026
47                 Z    =        -4550709
96
 XDOT =     -17924
419622                 XDOT =       -5498
705562
 YDOT =      14788
280220  feet/sec       YDOT =        4446
175725  meter/sec
 ZDOT =      -9897
736999                 ZDOT =       -3043
456206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6271882
46                 X    =         1911669
77
 Y    =       14984791
91  feet           Y    =         4567364
57  meter
 Z    =      -14915419
25                 Z    =        -4546219
79
 XDOT =     -22097
783158                 XDOT =       -6735
404307
 YDOT =       -740
138563  feet/sec       YDOT =        -225
594234  meter/sec
 ZDOT =     -10003
218855                 ZDOT =       -3048
981107


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
52119605  
00016717  00000-0  10270-3 0  9125
2 25544  51
6436 160
9875 0011433 306
0041  54
0063 15
75749588  3526


Satellite: ISS
Catalog Number: 25544
Epoch time:      10041
52119605   =   yrday
fracday
Element set:     912
Inclination:       51
6436  deg
RA of node:       160
9875  deg
Eccentricity:     
0011433     
Arg of perigee:   306
0041  deg
Mean anomaly:      54
0063  deg
Mean motion:   15
75749588  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             352
Checksum:              285


Coasting Arc #14 (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    =        4899607
59                 A    =         6725185
70  meter
 Y    =       -4107088
20  meter          E    =           
0005200
 Z    =        2087562
16                 I    =           51
79857
 XDOT =       4610
972992                 Wp   =           61
67896
 YDOT =       2669
909112  meter/sec      RA   =          154
91848  deg
 ZDOT =      -5556
522941                 TA   =           95
05602
                                          MA   =           94
99666
                                          Ha   =            187
949  n
mi
                                          Hp   =            182
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16074828
06                 X    =         4935028
95
 Y    =      -13474698
82  feet           Y    =        -4052099
86  meter
 Z    =        6848957
21                 Z    =         2111449
70
 XDOT =      15127
864146                 XDOT =        4607
766649
 YDOT =       8759
544332  feet/sec       YDOT =        2721
453888  meter/sec
 ZDOT =     -18230
062141                 ZDOT =       -5534
131280

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20942639
94                 X    =         6383316
65
 Y    =        -260964
31  feet           Y    =          -79541
92  meter
 Z    =        6943597
78                 Z    =         2116408
60
 XDOT =       6214
228796                 XDOT =        1894
096937
 YDOT =      14903
434820  feet/sec       YDOT =        4542
566933  meter/sec
 ZDOT =     -18141
087356                 ZDOT =       -5529
403426


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
53588661  
00016717  00000-0  10270-3 0  9130
2 25544  51
6440 155
7636 0011347 310
2442  49
7729 15
75772341  3684


Satellite: ISS
Catalog Number: 25544
Epoch time:      10042
53588661   =   yrday
fracday
Element set:     913
Inclination:       51
6440  deg
RA of node:       155
7636  deg
Eccentricity:     
0011347     
Arg of perigee:   310
2442  deg
Mean anomaly:      49
7729  deg
Mean motion:   15
75772341  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             368
Checksum:              308


Coasting Arc #15 (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    =       -3656276
33                 A    =         6715877
32  meter
 Y    =       -2480348
25  meter          E    =           
0006258
 Z    =        5059933
65                 I    =           51
79548
 XDOT =       5697
361605                 Wp   =          322
23169
 YDOT =      -4886
875229  meter/sec      RA   =          149
81380  deg
 ZDOT =       1727
328389                 TA   =          111
21957
                                          MA   =          111
15271
                                          Ha   =            188
167  n
mi
                                          Hp   =            182
329

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11995657
24                 X    =        -3652848
36
 Y    =       -8137625
49  feet           Y    =        -2521215
70  meter
 Z    =       16600832
17                 Z    =         5042180
36
 XDOT =      18692
131250                 XDOT =        5743
193289
 YDOT =     -16033
055213  feet/sec       YDOT =       -4822
907684  meter/sec
 ZDOT =       5667
087890                 ZDOT =        1755
116646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4436657
93                 X    =        -1352293
34
 Y    =      -13884190
58  feet           Y    =        -4231901
29  meter
 Z    =       16530265
83                 Z    =         5038425
03
 XDOT =      23567
927946                 XDOT =        7183
504438
 YDOT =       -676
262380  feet/sec       YDOT =        -206
124773  meter/sec
 ZDOT =       5777
187973                 ZDOT =        1760
886894


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
55056019  
00016717  00000-0  10270-3 0  9141
2 25544  51
6450 150
5390 0011463 314
4654  45
5572 15
75839335  3840


Satellite: ISS
Catalog Number: 25544
Epoch time:      10043
55056019   =   yrday
fracday
Element set:     914
Inclination:       51
6450  deg
RA of node:       150
5390  deg
Eccentricity:     
0011463     
Arg of perigee:   314
4654  deg
Mean anomaly:      45
5572  deg
Mean motion:   15
75839335  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              295

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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