Date: January 27th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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 99)
---------------------------------------

Vector Time (GMT): 2010/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4662189
93                 A    =         6724253
13  meter
 Y    =        3820244
26  meter          E    =           
0007131
 Z    =        2970210
74                 I    =           51
35178
 XDOT =      -1509
862651                 Wp   =          157
14864
 YDOT =       5698
007368  meter/sec      RA   =          242
53892  deg
 ZDOT =      -4961
245218                 TA   =          348
38124
                                          MA   =          348
39768
                                          Ha   =            187
570  n
mi
                                          Hp   =            183
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15295898
72                 X    =         4604696
17
 Y    =       12533609
77  feet           Y    =         3872057
92  meter
 Z    =        9744785
91                 Z    =         2992720
11
 XDOT =      -4953
617620                 XDOT =       -1549
365954
 YDOT =      18694
249896  feet/sec       YDOT =        5680
902722  meter/sec
 ZDOT =     -16277
051239                 ZDOT =       -4968
675548

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1898500
19                 X    =         -578662
86
 Y    =       19639333
25  feet           Y    =         5986068
77  meter
 Z    =        9834074
97                 Z    =         2997426
05
 XDOT =     -16791
703681                 XDOT =       -5118
111282
 YDOT =       6537
821394  feet/sec       YDOT =        1992
727961  meter/sec
 ZDOT =     -16306
311067                 ZDOT =       -4970
163613


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
53781759  
00016717  00000-0  10270-3 0  9000
2 25544  51
6439 243
2603 0011547 244
2265 115
7708 15
75408922  1006


Satellite: ISS
Catalog Number: 25544
Epoch time:      10025
53781759   =   yrday
fracday
Element set:     900
Inclination:       51
6439  deg
RA of node:       243
2603  deg
Eccentricity:     
0011547     
Arg of perigee:   244
2265  deg
Mean anomaly:     115
7708  deg
Mean motion:   15
75408922  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             100
Checksum:              290


Coasting Arc #2 (Orbit 115)
---------------------------------------

Vector Time (GMT): 2010/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1319444
61                 A    =         6719150
38  meter
 Y    =       -4740414
62  meter          E    =           
0008487
 Z    =        4581866
06                 I    =           51
34750
 XDOT =       5594
656731                 Wp   =          201
09291
 YDOT =       4398
052817  meter/sec      RA   =          237
41801  deg
 ZDOT =       2933
018235                 TA   =          219
67092
                                          MA   =          219
73304
                                          Ha   =            187
478  n
mi
                                          Hp   =            183
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4328886
53                 X    =         1350097
13
 Y    =      -15552541
41  feet           Y    =        -4725488
87  meter
 Z    =       15032368
95                 Z    =         4588349
82
 XDOT =      18355
173003                 XDOT =        5530
813243
 YDOT =      14429
307143  feet/sec       YDOT =        4460
258323  meter/sec
 ZDOT =       9622
763237                 ZDOT =        2960
042069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15181185
80                 X    =         4627225
43
 Y    =       -5420692
19  feet           Y    =        -1652226
98  meter
 Z    =       15057908
65                 Z    =         4589650
56
 XDOT =      -1759
590252                 XDOT =        -536
323109
 YDOT =      22156
272328  feet/sec       YDOT =        6753
231806  meter/sec
 ZDOT =       9729
969410                 ZDOT =        2965
694676


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
55275967  
00016717  00000-0  10270-3 0  9013
2 25544  51
6425 238
0367 0011490 247
9328 112
0616 15
75358475  1169


Satellite: ISS
Catalog Number: 25544
Epoch time:      10026
55275967   =   yrday
fracday
Element set:     901
Inclination:       51
6425  deg
RA of node:       238
0367  deg
Eccentricity:     
0011490     
Arg of perigee:   247
9328  deg
Mean anomaly:     112
0616  deg
Mean motion:   15
75358475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             116
Checksum:              306


Coasting Arc #3 (Orbit 130)
---------------------------------------

Vector Time (GMT): 2010/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5108311
81                 A    =         6726142
18  meter
 Y    =       -3822278
64  meter          E    =           
0006954
 Z    =       -2121990
98                 I    =           51
38775
 XDOT =       1564
831075                 Wp   =          278
29943
 YDOT =      -5154
571629  meter/sec      RA   =          232
20977  deg
 ZDOT =       5503
360783                 TA   =           57
87846
                                          MA   =           57
81100
                                          Ha   =            187
138  n
mi
                                          Hp   =            183
885

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16759553
17                 X    =        -5054882
70
 Y    =      -12540284
24  feet           Y    =        -3879103
84  meter
 Z    =       -6961912
65                 Z    =        -2146677
29
 XDOT =       5133
960221                 XDOT =        1595
620299
 YDOT =     -16911
324243  feet/sec       YDOT =       -5136
901185  meter/sec
 ZDOT =      18055
645614                 ZDOT =        5511
036832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         359639
79                 X    =          109618
21
 Y    =      -20895900
75  feet           Y    =        -6369070
55  meter
 Z    =       -7059856
23                 Z    =        -2151844
18
 XDOT =      15124
241108                 XDOT =        4609
868690
 YDOT =      -5865
870465  feet/sec       YDOT =       -1787
917318  meter/sec
 ZDOT =      18085
895224                 ZDOT =        5512
580864


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   10027
50425067  
00016717  00000-0  10270-3 0  9028
2 25544  51
6412 233
1395 0011672 251
4440 108
5457 15
75412069  1319


Satellite: ISS
Catalog Number: 25544
Epoch time:      10027
50425067   =   yrday
fracday
Element set:     902
Inclination:       51
6412  deg
RA of node:       233
1395  deg
Eccentricity:     
0011672     
Arg of perigee:   251
4440  deg
Mean anomaly:     108
5457  deg
Mean motion:   15
75412069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             131
Checksum:              271


Coasting Arc #4 (Orbit 146)
---------------------------------------

Vector Time (GMT): 2010/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 750718
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1464822
63                 A    =         6717235
53  meter
 Y    =        4266269
66  meter          E    =           
0001521
 Z    =       -4978765
95                 I    =           51
37592
 XDOT =      -6089
737448                 Wp   =           78
78778
 YDOT =      -4313
746216  meter/sec      RA   =          227
08009  deg
 ZDOT =      -1904
932266                 TA   =          172
75739
                                          MA   =          172
75520
                                          Ha   =            186
695  n
mi
                                          Hp   =            183
961

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4805848
53                 X    =        -1488234
63
 Y    =       13996947
72  feet           Y    =         4249758
72  meter
 Z    =      -16334533
95                 Z    =        -4985938
34
 XDOT =     -19979
453571                 XDOT =       -6031
794201
 YDOT =     -14152
710681  feet/sec       YDOT =       -4381
521106  meter/sec
 ZDOT =      -6249
777777                 ZDOT =       -1934
375107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14022893
73                 X    =        -4274178
01
 Y    =        4630817
52  feet           Y    =         1411473
18  meter
 Z    =      -16362814
72                 Z    =        -4987385
93
 XDOT =       -306
853039                 XDOT =         -93
528806
 YDOT =     -23423
055575  feet/sec       YDOT =       -7139
347339  meter/sec
 ZDOT =      -6366
607072                 ZDOT =       -1940
541835


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   10028
51916154  
00016717  00000-0  10270-3 0  9033
2 25544  51
6398 227
9163 0011582 255
2250 104
7630 15
75440622  1471


Satellite: ISS
Catalog Number: 25544
Epoch time:      10028
51916154   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       227
9163  deg
Eccentricity:     
0011582     
Arg of perigee:   255
2250  deg
Mean anomaly:     104
7630  deg
Mean motion:   15
75440622  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             147
Checksum:              288


Coasting Arc #5 (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    =        5505002
45                 A    =         6727248
52  meter
 Y    =        3669781
16  meter          E    =           
0009313
 Z    =        1183577
88                 I    =           51
43243
 XDOT =      -1834
068758                 Wp   =          178
11222
 YDOT =       4641
748574  meter/sec      RA   =          221
88934  deg
 ZDOT =      -5869
446912                 TA   =          348
87157
                                          MA   =          348
89216
                                          Ha   =            186
150  n
mi
                                          Hp   =            183
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18061031
65                 X    =         5457807
74
 Y    =       12039964
44  feet           Y    =         3731077
40  meter
 Z    =        3883129
53                 Z    =         1210205
97
 XDOT =      -6017
285950                 XDOT =       -1857
325481
 YDOT =      15228
833904  feet/sec       YDOT =        4621
109299  meter/sec
 ZDOT =     -19256
715592                 ZDOT =       -5878
412710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1564233
29                 X    =          476778
31
 Y    =       21630601
80  feet           Y    =         6593007
43  meter
 Z    =        3988802
17                 Z    =         1215786
90
 XDOT =     -14069
319574                 XDOT =       -4288
328606
 YDOT =       4570
373294  feet/sec       YDOT =        1393
049780  meter/sec
 ZDOT =     -19292
087667                 ZDOT =       -5880
228321


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
53405572  
00016717  00000-0  10270-3 0  9044
2 25544  51
6403 222
6931 0011650 260
2906  99
6942 15
75506917  1639


Satellite: ISS
Catalog Number: 25544
Epoch time:      10029
53405572   =   yrday
fracday
Element set:     904
Inclination:       51
6403  deg
RA of node:       222
6931  deg
Eccentricity:     
0011650     
Arg of perigee:   260
2906  deg
Mean anomaly:      99
6942  deg
Mean motion:   15
75506917  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             163
Checksum:              297


Coasting Arc #6 (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    =        1790071
52                 A    =         6716227
67  meter
 Y    =       -3851398
92  meter          E    =           
0009087
 Z    =        5210603
63                 I    =           51
41675
 XDOT =       6486
990093                 Wp   =          250
87207
 YDOT =       4069
166194  meter/sec      RA   =          216
74443  deg
 ZDOT =        777
312650                 TA   =          191
69449
                                          MA   =          191
71561
                                          Ha   =            186
056  n
mi
                                          Hp   =            183
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5872938
05                 X    =         1807694
17
 Y    =      -12635823
22  feet           Y    =        -3831282
92  meter
 Z    =       17095156
26                 Z    =         5219342
18
 XDOT =      21282
775897                 XDOT =        6437
229914
 YDOT =      13350
282790  feet/sec       YDOT =        4141
429309  meter/sec
 ZDOT =       2550
238354                 ZDOT =         808
704675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13461648
01                 X    =         4103110
31
 Y    =       -3429116
24  feet           Y    =        -1045194
63  meter
 Z    =       17129652
41                 Z    =         5221118
06
 XDOT =       2691
076242                 XDOT =         820
240039
 YDOT =      23955
990385  feet/sec       YDOT =        7301
785869  meter/sec
 ZDOT =       2674
828875                 ZDOT =         815
287841


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
54893875  
00016717  00000-0  10270-3 0  9055
2 25544  51
6393 217
4684 0011467 263
1214  96
8646 15
75437414  1796


Satellite: ISS
Catalog Number: 25544
Epoch time:      10030
54893875   =   yrday
fracday
Element set:     905
Inclination:       51
6393  deg
RA of node:       217
4684  deg
Eccentricity:     
0011467     
Arg of perigee:   263
1214  deg
Mean anomaly:      96
8646  deg
Mean motion:   15
75437414  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             179
Checksum:              325


Coasting Arc #7 (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    =       -5791127
08                 A    =         6727880
61  meter
 Y    =       -3410191
31  meter          E    =           
0008563
 Z    =        -159415
14                 I    =           51
48158
 XDOT =       2309
816182                 Wp   =          337
38240
 YDOT =      -4208
736600  meter/sec      RA   =          211
57417  deg
 ZDOT =       6024
306154                 TA   =           20
88078
                                          MA   =           20
84583
                                          Ha   =            185
749  n
mi
                                          Hp   =            183
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18999760
77                 X    =        -5751788
93
 Y    =      -11188291
69  feet           Y    =        -3474731
17  meter
 Z    =        -523015
54                 Z    =         -187452
00
 XDOT =       7578
137080                 XDOT =        2327
443279
 YDOT =     -13808
190945  feet/sec       YDOT =       -4182
808315  meter/sec
 ZDOT =      19764
783970                 ZDOT =        6035
569699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3575344
39                 X    =        -1089764
97
 Y    =      -21754468
62  feet           Y    =        -6630762
04  meter
 Z    =        -634297
29                 Z    =         -193333
81
 XDOT =      13796
720150                 XDOT =        4205
240302
 YDOT =      -2852
884268  feet/sec       YDOT =        -869
559125  meter/sec
 ZDOT =      19809
272602                 ZDOT =        6037
866289


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
50037333  
00016717  00000-0  10270-3 0  9062
2 25544  51
6391 212
5703 0011553 266
4441  93
5401 15
75504192  1944


Satellite: ISS
Catalog Number: 25544
Epoch time:      10031
50037333   =   yrday
fracday
Element set:     906
Inclination:       51
6391  deg
RA of node:       212
5703  deg
Eccentricity:     
0011553     
Arg of perigee:   266
4441  deg
Mean anomaly:      93
5401  deg
Mean motion:   15
75504192  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             194
Checksum:              270


Coasting Arc #8 (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    =       -2273292
88                 A    =         6715759
46  meter
 Y    =        3532640
68  meter          E    =           
0003680
 Z    =       -5242792
81                 I    =           51
46776
 XDOT =      -6733
393455                 Wp   =          102
14830
 YDOT =      -3714
565183  meter/sec      RA   =          206
41368  deg
 ZDOT =        416
198029                 TA   =          171
81616
                                          MA   =          171
81016
                                          Ha   =            185
454  n
mi
                                          Hp   =            183
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7458309
97                 X    =        -2287158
68
 Y    =       11590028
48  feet           Y    =         3507141
74  meter
 Z    =      -17200763
80                 Z    =        -5253869
92
 XDOT =     -22091
185877                 XDOT =       -6693
377852
 YDOT =     -12186
893644  feet/sec       YDOT =       -3789
638231  meter/sec
 ZDOT =       1365
479097                 ZDOT =         383
585355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13580070
58                 X    =        -4139205
51
 Y    =        2007237
91  feet           Y    =          611806
12  meter
 Z    =      -17244538
32                 Z    =        -5256135
28
 XDOT =      -5074
776280                 XDOT =       -1546
791810
 YDOT =     -23700
154137  feet/sec       YDOT =       -7223
806981  meter/sec
 ZDOT =       1236
031247                 ZDOT =         376
742324


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
51522408  
00016717  00000-0  10270-3 0  9077
2 25544  51
6395 207
3467 0011377 270
1276  89
8584 15
75538228  2105


Satellite: ISS
Catalog Number: 25544
Epoch time:      10032
51522408   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:       207
3467  deg
Eccentricity:     
0011377     
Arg of perigee:   270
1276  deg
Mean anomaly:      89
8584  deg
Mean motion:   15
75538228  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             210
Checksum:              306


Coasting Arc #9 (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    =        5917345
71                 A    =         6727311
62  meter
 Y    =        3062589
36  meter          E    =           
0008516
 Z    =        -890644
05                 I    =           51
53527
 XDOT =      -2930
379228                 Wp   =          216
12771
 YDOT =       3926
820509  meter/sec      RA   =          201
26843  deg
 ZDOT =      -5944
287662                 TA   =          333
61444
                                          MA   =          333
65778
                                          Ha   =            185
673  n
mi
                                          Hp   =            183
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19413863
87                 X    =         5886986
00
 Y    =       10047865
35  feet           Y    =         3128590
85  meter
 Z    =       -2922060
52                 Z    =         -861972
02
 XDOT =      -9614
105080                 XDOT =       -2945
196183
 YDOT =      12883
269386  feet/sec       YDOT =        3893
968271  meter/sec
 ZDOT =     -19502
256108                 ZDOT =       -5958
559229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5461233
90                 X    =         1664584
09
 Y    =       21182180
87  feet           Y    =         6456328
73  meter
 Z    =       -2808252
84                 Z    =         -855955
47
 XDOT =     -14390
834412                 XDOT =       -4386
326329
 YDOT =       1107
307834  feet/sec       YDOT =         337
507428  meter/sec
 ZDOT =     -19558
680232                 ZDOT =       -5961
485735


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
53005760  
00016717  00000-0  10270-3 0  9088
2 25544  51
6400 202
1228 0011457 275
4237  84
5620 15
75598849  2269


Satellite: ISS
Catalog Number: 25544
Epoch time:      10033
53005760   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       202
1228  deg
Eccentricity:     
0011457     
Arg of perigee:   275
4237  deg
Mean anomaly:      84
5620  deg
Mean motion:   15
75598849  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             226
Checksum:              291


Coasting Arc #10 (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    =        2862891
83                 A    =         6716556
86  meter
 Y    =       -3364491
68  meter          E    =           
0008425
 Z    =        5066473
51                 I    =           51
52693
 XDOT =       6761
908097                 Wp   =          302
01503
 YDOT =       3297
593825  meter/sec      RA   =          196
09094  deg
 ZDOT =      -1628
672150                 TA   =          163
67831
                                          MA   =          163
65117
                                          Ha   =            185
909  n
mi
                                          Hp   =            183
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9392689
75                 X    =         2875689
80
 Y    =      -11038358
54  feet           Y    =        -3332405
48  meter
 Z    =       16622288
42                 Z    =         5080412
35
 XDOT =      22184
737851                 XDOT =        6732
442921
 YDOT =      10818
877379  feet/sec       YDOT =        3373
044711  meter/sec
 ZDOT =      -5343
412566                 ZDOT =       -1595
894989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14414390
71                 X    =         4393506
29
 Y    =        -676366
32  feet           Y    =         -206156
45  meter
 Z    =       16677419
51                 Z    =         5083277
47
 XDOT =       7101
477196                 XDOT =        2164
530249
 YDOT =      22601
586591  feet/sec       YDOT =        6888
963593  meter/sec
 ZDOT =      -5213
309378                 ZDOT =       -1589
016699


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
54487897  
00016717  00000-0  10270-3 0  9096
2 25544  51
6398 196
8986 0011284 278
0565  81
9319 15
75538253  2423


Satellite: ISS
Catalog Number: 25544
Epoch time:      10034
54487897   =   yrday
fracday
Element set:     909
Inclination:       51
6398  deg
RA of node:       196
8986  deg
Eccentricity:     
0011284     
Arg of perigee:   278
0565  deg
Mean anomaly:      81
9319  deg
Mean motion:   15
75538253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             242
Checksum:              353


Coasting Arc #11 (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    =       -5837232
00                 A    =         6725972
61  meter
 Y    =       -2703086
35  meter          E    =           
0007968
 Z    =        1946101
64                 I    =           51
58959
 XDOT =       3640
693904                 Wp   =           14
16629
 YDOT =      -3825
123555  meter/sec      RA   =          190
96872  deg
 ZDOT =       5609
846579                 TA   =            7
52140
                                          MA   =            7
50946
                                          Ha   =            186
222  n
mi
                                          Hp   =            183
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19151023
61                 X    =        -5816025
45
 Y    =       -8868393
53  feet           Y    =        -2768243
16  meter
 Z    =        6384847
90                 Z    =         1917796
29
 XDOT =      11944
533805                 XDOT =        3655
945294
 YDOT =     -12549
617961  feet/sec       YDOT =       -3784
325869  meter/sec
 ZDOT =      18405
008462                 ZDOT =        5627
569873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6870605
72                 X    =        -2094160
62
 Y    =      -19990673
02  feet           Y    =        -6093157
14  meter
 Z    =        6272492
42                 Z    =         1911855
69
 XDOT =      15792
198785                 XDOT =        4813
462190
 YDOT =        366
424782  feet/sec       YDOT =         111
686274  meter/sec
 ZDOT =      18475
132840                 ZDOT =        5631
220490


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
55968024  
00016717  00000-0  10270-3 0  9106
2 25544  51
6407 191
6746 0011363 281
7400  78
2489 15
75622531  2585


Satellite: ISS
Catalog Number: 25544
Epoch time:      10035
55968024   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:       191
6746  deg
Eccentricity:     
0011363     
Arg of perigee:   281
7400  deg
Mean anomaly:      78
2489  deg
Mean motion:   15
75622531  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             258
Checksum:              305


Coasting Arc #12 (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    =       -3481011
23                 A    =         6717990
73  meter
 Y    =        3360991
31  meter          E    =           
0000705
 Z    =       -4660103
89                 I    =           51
59338
 XDOT =      -6560
308712                 Wp   =          217
94336
 YDOT =      -2900
978070  meter/sec      RA   =          185
77920  deg
 ZDOT =       2807
396070                 TA   =           79
77704
                                          MA   =           79
76910
                                          Ha   =            186
474  n
mi
                                          Hp   =            183
808

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11420640
53                 X    =        -3495698
08
 Y    =       11026874
37  feet           Y    =         3321982
53  meter
 Z    =      -15289054
75                 Z    =        -4677050
03
 XDOT =     -21523
322546                 XDOT =       -6541
019523
 YDOT =      -9517
644586  feet/sec       YDOT =       -2974
231521  meter/sec
 ZDOT =       9210
617028                 ZDOT =        2775
573329

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15807852
45                 X    =        -4818233
43
 Y    =        -281831
89  feet           Y    =          -85902
36  meter
 Z    =      -15356124
35                 Z    =        -4680546
70
 XDOT =      -8455
057308                 XDOT =       -2577
101468
 YDOT =     -20870
196366  feet/sec       YDOT =       -6361
235852  meter/sec
 ZDOT =       9084
294408                 ZDOT =        2768
892936


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
51104416  
00016717  00000-0  10270-3 0  9111
2 25544  51
6412 186
7781 0011309 285
8400  74
1517 15
75628698  2734


Satellite: ISS
Catalog Number: 25544
Epoch time:      10036
51104416   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:       186
7781  deg
Eccentricity:     
0011309     
Arg of perigee:   285
8400  deg
Mean anomaly:      74
1517  deg
Mean motion:   15
75628698  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             273
Checksum:              299


Coasting Arc #13 (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    =        5556314
72                 A    =         6723778
42  meter
 Y    =        2388407
02  meter          E    =           
0006790
 Z    =       -2935130
01                 I    =           51
64292
 XDOT =      -4338
441965                 Wp   =          287
71098
 YDOT =       3917
031903  meter/sec      RA   =          180
67507  deg
 ZDOT =      -5013
923959                 TA   =          286
12318
                                          MA   =          286
19792
                                          Ha   =            186
848  n
mi
                                          Hp   =            183
731

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18229378
99                 X    =         5543452
29
 Y    =        7835981
04  feet           Y    =         2450469
20  meter
 Z    =       -9629691
64                 Z    =        -2908169
00
 XDOT =     -14233
733480                 XDOT =       -4357
564091
 YDOT =      12851
154539  feet/sec       YDOT =        3868
410115  meter/sec
 ZDOT =     -16449
881755                 ZDOT =       -5035
046123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7628274
39                 X    =         2325098
03
 Y    =       18373137
82  feet           Y    =         5600132
41  meter
 Z    =       -9522660
07                 Z    =        -2902506
79
 XDOT =     -17753
545169                 XDOT =       -5411
280568
 YDOT =      -1217
942735  feet/sec       YDOT =        -371
228946  meter/sec
 ZDOT =     -16533
501414                 ZDOT =       -5039
411231


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
52581563  
00016717  00000-0  10270-3 0  9126
2 25544  51
6410 181
5540 0011349 290
2631  69
7312 15
75663032  2899


Satellite: ISS
Catalog Number: 25544
Epoch time:      10037
52581563   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:       181
5540  deg
Eccentricity:     
0011349     
Arg of perigee:   290
2631  deg
Mean anomaly:      69
7312  deg
Mean motion:   15
75663032  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             289
Checksum:              289


Coasting Arc #14 (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    =        4072288
28                 A    =         6720312
56  meter
 Y    =       -3518710
41  meter          E    =           
0006955
 Z    =        4029538
03                 I    =           51
66179
 XDOT =       6109
323647                 Wp   =            1
27441
 YDOT =       2604
835714  meter/sec      RA   =          175
47817  deg
 ZDOT =      -3892
564342                 TA   =          128
89719
                                          MA   =          128
83514
                                          Ha   =            187
086  n
mi
                                          Hp   =            183
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13360525
84                 X    =         4091758
04
 Y    =      -11544325
51  feet           Y    =        -3473062
98  meter
 Z    =       13220269
13                 Z    =         4049368
00
 XDOT =      20043
712753                 XDOT =        6098
650895
 YDOT =       8546
048929  feet/sec       YDOT =        2673
094280  meter/sec
 ZDOT =     -12770
880388                 ZDOT =       -3862
911585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17584198
77                 X    =         5359663
79
 Y    =         699097
63  feet           Y    =          213084
96  meter
 Z    =       13298790
70                 Z    =         4053471
41
 XDOT =       8841
977112                 XDOT =        2695
034624
 YDOT =      18730
158632  feet/sec       YDOT =        5708
952351  meter/sec
 ZDOT =     -12653
150239                 ZDOT =       -3856
680193


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
54057196  
00016717  00000-0  10270-3 0  9130
2 25544  51
6411 176
3299 0011283 293
8994  66
0987 15
75657505  3056


Satellite: ISS
Catalog Number: 25544
Epoch time:      10038
54057196   =   yrday
fracday
Element set:     913
Inclination:       51
6411  deg
RA of node:       176
3299  deg
Eccentricity:     
0011283     
Arg of perigee:   293
8994  deg
Mean anomaly:      66
0987  deg
Mean motion:   15
75657505  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             305
Checksum:              330


Coasting Arc #15 (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    =       -5063978
35                 A    =         6720959
88  meter
 Y    =       -2206162
85  meter          E    =           
0003954
 Z    =        3824702
58                 I    =           51
69560
 XDOT =       4960
105115                 Wp   =           19
83949
 YDOT =      -4174
459003  meter/sec      RA   =          170
38434  deg
 ZDOT =       4161
764203                 TA   =           26
66581
                                          MA   =           26
64548
                                          Ha   =            187
366  n
mi
                                          Hp   =            183
346

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16614102
21                 X    =        -5057511
60
 Y    =       -7238067
08  feet           Y    =        -2262755
27  meter
 Z    =       12548236
82                 Z    =         3800117
91
 XDOT =      16273
310746                 XDOT =        4986
199347
 YDOT =     -13695
731637  feet/sec       YDOT =       -4118
846459  meter/sec
 ZDOT =      13654
082030                 ZDOT =        4185
923067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7475806
20                 X    =        -2278625
73
 Y    =      -16582242
83  feet           Y    =        -5054267
61  meter
 Z    =       12450614
39                 Z    =         3794947
27
 XDOT =      19984
897607                 XDOT =        6091
396790
 YDOT =       1308
082471  feet/sec       YDOT =         398
703537  meter/sec
 ZDOT =      13749
762735                 ZDOT =        4190
927682


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
55530923  
00016717  00000-0  10270-3 0  9147
2 25544  51
6423 171
1056 0011405 297
8791  62
1217 15
75736490  3210


Satellite: ISS
Catalog Number: 25544
Epoch time:      10039
55530923   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:       171
1056  deg
Eccentricity:     
0011405     
Arg of perigee:   297
8791  deg
Mean anomaly:      62
1217  deg
Mean motion:   15
75736490  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             321
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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