Date: April 10th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 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 3992)
---------------------------------------

Vector Time (GMT): 2007/099/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3760166
98                 A    =         6707741
44  meter
 Y    =        2161423
15  meter          E    =           
0026549
 Z    =       -5136818
25                 I    =           51
92856
 XDOT =      -2172
573073                 Wp   =           72
41381
 YDOT =       7230
902156  meter/sec      RA   =           97
97386  deg
 ZDOT =       1466
225333                 TA   =          211
52024
                                          MA   =          211
67956
                                          Ha   =            188
468  n
mi
                                          Hp   =            171
887

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12336505
85                 X    =         3760671
98
 Y    =        7091283
30  feet           Y    =         2203474
38  meter
 Z    =      -16853078
23                 Z    =        -5118550
03
 XDOT =      -7127
864412                 XDOT =       -2260
391272
 YDOT =      23723
432271  feet/sec       YDOT =        7206
116181  meter/sec
 ZDOT =       4810
450568                 ZDOT =        1455
457787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14243373
44                 X    =         4341380
23
 Y    =        1387448
37  feet           Y    =          422894
26  meter
 Z    =      -16784016
84                 Z    =        -5115768
33
 XDOT =       3274
851217                 XDOT =         998
174651
 YDOT =      23536
034387  feet/sec       YDOT =        7173
783281  meter/sec
 ZDOT =       4770
861703                 ZDOT =        1454
158647


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   07099
53423300  
00020000  00000-0  20000-3 0  9004
2 25544  51
6303  98
6849 0015778  47
2274 313
0215 15
78593111 39938


Satellite: ISS
Catalog Number: 25544
Epoch time:      07099
53423300   =   yrday
fracday
Element set:     900
Inclination:       51
6303  deg
RA of node:        98
6849  deg
Eccentricity:     
0015778     
Arg of perigee:    47
2274  deg
Mean anomaly:     313
0215  deg
Mean motion:   15
78593111  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3993
Checksum:              294


Coasting Arc #2 (Orbit 4008)
---------------------------------------

Vector Time (GMT): 2007/100/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2428843
59                 A    =         6715708
21  meter
 Y    =       -5641224
64  meter          E    =           
0017990
 Z    =       -2740710
65                 I    =           51
95865
 XDOT =       3855
871056                 Wp   =           65
83363
 YDOT =       4171
125467  meter/sec      RA   =           92
85881  deg
 ZDOT =      -5187
697805                 TA   =          145
32568
                                          MA   =          145
20827
                                          Ha   =            188
445  n
mi
                                          Hp   =            171
596

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7968646
94                 X    =         2505057
92
 Y    =      -18507954
85  feet           Y    =        -5613637
77  meter
 Z    =       -8991832
85                 Z    =        -2728726
31
 XDOT =      12650
495592                 XDOT =        3834
143232
 YDOT =      13684
794838  feet/sec       YDOT =        4214
122577  meter/sec
 ZDOT =     -17020
005921                 ZDOT =       -5169
018703

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -599001
43                 X    =         -182575
64
 Y    =      -20161378
35  feet           Y    =        -6145188
12  meter
 Z    =       -8947446
85                 Z    =        -2727181
80
 XDOT =      15879
807651                 XDOT =        4840
165372
 YDOT =       7021
771990  feet/sec       YDOT =        2140
236103  meter/sec
 ZDOT =     -16949
130653                 ZDOT =       -5166
095023


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   07100
54707838  
00020000  00000-0  20000-3 0  9010
2 25544  51
6302  93
4458 0015870  51
2275 309
0305 15
78656098 40093


Satellite: ISS
Catalog Number: 25544
Epoch time:      07100
54707838   =   yrday
fracday
Element set:     901
Inclination:       51
6302  deg
RA of node:        93
4458  deg
Eccentricity:     
0015870     
Arg of perigee:    51
2275  deg
Mean anomaly:     309
0305  deg
Mean motion:   15
78656098  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4009
Checksum:              285


Coasting Arc #3 (Orbit 4024)
---------------------------------------

Vector Time (GMT): 2007/101/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2950341
97                 A    =         6713485
36  meter
 Y    =       -4894046
29  meter          E    =           
0026904
 Z    =        3511260
39                 I    =           51
95134
 XDOT =       3330
263005                 Wp   =           68
90117
 YDOT =      -5282
179982  meter/sec      RA   =           87
66047  deg
 ZDOT =      -4527
046294                 TA   =           69
43259
                                          MA   =           69
14415
                                          Ha   =            188
417  n
mi
                                          Hp   =            171
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9679599
64                 X    =        -2912453
77
 Y    =      -16056582
31  feet           Y    =        -4926826
84  meter
 Z    =       11519883
15                 Z    =         3497019
68
 XDOT =      10926
059727                 XDOT =        3411
073087
 YDOT =     -17329
986818  feet/sec       YDOT =       -5244
487262  meter/sec
 ZDOT =     -14852
514089                 ZDOT =       -4510
671674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15816201
99                 X    =        -4820778
37
 Y    =      -10129335
77  feet           Y    =        -3087421
54  meter
 Z    =       11465622
72                 Z    =         3494721
80
 XDOT =       1518
973353                 XDOT =         462
983078
 YDOT =     -19252
981219  feet/sec       YDOT =       -5868
308676  meter/sec
 ZDOT =     -14791
544869                 ZDOT =       -4508
462876


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   07101
55989983  
00020000  00000-0  20000-3 0  9026
2 25544  51
6299  88
2072 0015767  54
4134 305
8498 15
78704530 40256


Satellite: ISS
Catalog Number: 25544
Epoch time:      07101
55989983   =   yrday
fracday
Element set:     902
Inclination:       51
6299  deg
RA of node:        88
2072  deg
Eccentricity:     
0015767     
Arg of perigee:    54
4134  deg
Mean anomaly:     305
8498  deg
Mean motion:   15
78704530  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4025
Checksum:              314


Coasting Arc #4 (Orbit 4040)
---------------------------------------

Vector Time (GMT): 2007/102/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3352746
85                 A    =         6708701
67  meter
 Y    =        3268873
15  meter          E    =           
0020112
 Z    =        4785704
70                 I    =           51
93344
 XDOT =      -2886
414576                 Wp   =           76
67094
 YDOT =      -6695
640771  meter/sec      RA   =           82
55665  deg
 ZDOT =       2546
994763                 TA   =          348
54262
                                          MA   =          348
58833
                                          Ha   =            188
425  n
mi
                                          Hp   =            171
263

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10999825
63                 X    =        -3412298
66
 Y    =       10724649
43  feet           Y    =         3231047
95  meter
 Z    =       15701130
92                 Z    =         4769272
44
 XDOT =      -9469
864095                 XDOT =       -2823
701214
 YDOT =     -21967
325363  feet/sec       YDOT =       -6727
567593  meter/sec
 ZDOT =       8356
282032                 ZDOT =        2533
125046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4984966
18                 X    =        -1519417
69
 Y    =       14597614
31  feet           Y    =         4449352
84  meter
 Z    =       15639678
71                 Z    =         4766974
07
 XDOT =     -17413
627942                 XDOT =       -5307
673797
 YDOT =     -14857
727306  feet/sec       YDOT =       -4528
635283  meter/sec
 ZDOT =       8303
181757                 ZDOT =        2530
809799


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   07102
57269816  
00020000  00000-0  20000-3 0  9036
2 25544  51
6302  82
9691 0015641  58
3454 301
9235 15
78750328 40418


Satellite: ISS
Catalog Number: 25544
Epoch time:      07102
57269816   =   yrday
fracday
Element set:     903
Inclination:       51
6302  deg
RA of node:        82
9691  deg
Eccentricity:     
0015641     
Arg of perigee:    58
3454  deg
Mean anomaly:     301
9235  deg
Mean motion:   15
78750328  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4041
Checksum:              286


Coasting Arc #5 (Orbit 4055)
---------------------------------------

Vector Time (GMT): 2007/103/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1994480
55                 A    =         6718412
16  meter
 Y    =        6367223
74  meter          E    =           
0025977
 Z    =        -709490
80                 I    =           51
96118
 XDOT =      -4374
448934                 Wp   =           53
25292
 YDOT =       2022
738038  meter/sec      RA   =           77
37940  deg
 ZDOT =       6021
021763                 TA   =          299
03158
                                          MA   =          299
29160
                                          Ha   =            188
381  n
mi
                                          Hp   =            171
065

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6543571
37                 X    =         1926579
67
 Y    =       20889841
67  feet           Y    =         6389147
46  meter
 Z    =       -2327725
73                 Z    =         -699966
81
 XDOT =     -14351
866580                 XDOT =       -4425
991301
 YDOT =       6636
279652  feet/sec       YDOT =        1973
532527  meter/sec
 ZDOT =      19754
008408                 ZDOT =        5999
645496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15618576
14                 X    =         4760542
01
 Y    =       15343838
16  feet           Y    =         4676801
87  meter
 Z    =       -2291032
08                 Z    =         -698306
58
 XDOT =      -8516
156501                 XDOT =       -2595
724501
 YDOT =      11523
840310  feet/sec       YDOT =        3512
466527  meter/sec
 ZDOT =      19673
774125                 ZDOT =        5996
566353


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   07103
52217605  
00020000  00000-0  20000-3 0  9042
2 25544  51
6300  78
0576 0015778  62
4772 297
7994 15
78773303 40562


Satellite: ISS
Catalog Number: 25544
Epoch time:      07103
52217605   =   yrday
fracday
Element set:     904
Inclination:       51
6300  deg
RA of node:        78
0576  deg
Eccentricity:     
0015778     
Arg of perigee:    62
4772  deg
Mean anomaly:     297
7994  deg
Mean motion:   15
78773303  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4056
Checksum:              306


Coasting Arc #6 (Orbit 4071)
---------------------------------------

Vector Time (GMT): 2007/104/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4243882
33                 A    =         6706870
45  meter
 Y    =        -149192
80  meter          E    =           
0029003
 Z    =       -5215040
53                 I    =           51
91543
 XDOT =       1533
116535                 Wp   =           81
12147
 YDOT =       7461
034482  meter/sec      RA   =           72
22550  deg
 ZDOT =       1043
439579                 TA   =          198
75426
                                          MA   =          198
86133
                                          Ha   =            188
348  n
mi
                                          Hp   =            171
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13923498
46                 X    =         4270568
95
 Y    =        -489477
69  feet           Y    =         -101586
41  meter
 Z    =      -17109713
02                 Z    =        -5194358
91
 XDOT =       5029
909892                 XDOT =        1444
503383
 YDOT =      24478
459585  feet/sec       YDOT =        7477
683246  meter/sec
 ZDOT =       3423
358200                 ZDOT =        1050
671807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12015026
05                 X    =         3662179
94
 Y    =       -7238846
48  feet           Y    =        -2206400
41  meter
 Z    =      -17031850
40                 Z    =        -5191308
00
 XDOT =      15744
905460                 XDOT =        4799
047184
 YDOT =      18084
283415  feet/sec       YDOT =        5512
089585  meter/sec
 ZDOT =       3451
562227                 ZDOT =        1052
036167


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   07104
53492830  
00020000  00000-0  20000-3 0  9050
2 25544  51
6308  72
8178 0015688  65
7663 294
5140 15
78785611 40726


Satellite: ISS
Catalog Number: 25544
Epoch time:      07104
53492830   =   yrday
fracday
Element set:     905
Inclination:       51
6308  deg
RA of node:        72
8178  deg
Eccentricity:     
0015688     
Arg of perigee:    65
7663  deg
Mean anomaly:     294
5140  deg
Mean motion:   15
78785611  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4072
Checksum:              308


Coasting Arc #7 (Orbit 4087)
---------------------------------------

Vector Time (GMT): 2007/105/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -535877
26                 A    =         6715749
74  meter
 Y    =       -6231293
81  meter          E    =           
0018805
 Z    =       -2465681
22                 I    =           51
93688
 XDOT =       5261
642341                 Wp   =           83
84751
 YDOT =       1657
887457  meter/sec      RA   =           67
10312  deg
 ZDOT =      -5366
144309                 TA   =          123
91662
                                          MA   =          123
73766
                                          Ha   =            188
274  n
mi
                                          Hp   =            170
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1758127
49                 X    =         -454180
29
 Y    =      -20443877
33  feet           Y    =        -6236829
66  meter
 Z    =       -8089505
30                 Z    =        -2468085
68
 XDOT =      17262
606105                 XDOT =        5268
780473
 YDOT =       5439
263309  feet/sec       YDOT =        1716
765656  meter/sec
 ZDOT =     -17605
460333                 ZDOT =       -5340
565860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11721509
11                 X    =        -3572715
98
 Y    =      -16837153
47  feet           Y    =        -5131964
38  meter
 Z    =       -8099365
13                 Z    =        -2468686
49
 XDOT =      16522
726152                 XDOT =        5036
126931
 YDOT =      -3131
769257  feet/sec       YDOT =        -954
563270  meter/sec
 ZDOT =     -17508
924935                 ZDOT =       -5336
720320


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   07105
54765600  
00020000  00000-0  20000-3 0  9061
2 25544  51
6316  67
5780 0015685  69
4494 290
8353 15
78846831 40889


Satellite: ISS
Catalog Number: 25544
Epoch time:      07105
54765600   =   yrday
fracday
Element set:     906
Inclination:       51
6316  deg
RA of node:        67
5780  deg
Eccentricity:     
0015685     
Arg of perigee:    69
4494  deg
Mean anomaly:     290
8353  deg
Mean motion:   15
78846831  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4088
Checksum:              322


Coasting Arc #8 (Orbit 4103)
---------------------------------------

Vector Time (GMT): 2007/106/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4807734
89                 A    =         6712406
11  meter
 Y    =       -2854314
15  meter          E    =           
0027347
 Z    =        3696343
53                 I    =           51
91390
 XDOT =        436
801935                 Wp   =           77
80585
 YDOT =      -6377
218378  meter/sec      RA   =           61
90287  deg
 ZDOT =      -4324
042332                 TA   =           57
71384
                                          MA   =           57
44921
                                          Ha   =            188
294  n
mi
                                          Hp   =            170
773

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15773408
44                 X    =        -4793416
62
 Y    =       -9364547
73  feet           Y    =        -2907996
67  meter
 Z    =       12127111
31                 Z    =         3673022
19
 XDOT =       1433
077215                 XDOT =         529
086138
 YDOT =     -20922
632474  feet/sec       YDOT =       -6371
818069  meter/sec
 ZDOT =     -14186
490591                 ZDOT =       -4321
695803

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18401233
25                 X    =        -5608695
89
 Y    =         144477
04  feet           Y    =           44036
60  meter
 Z    =       12038925
94                 Z    =         3669464
63
 XDOT =      -9482
388406                 XDOT =       -2890
231986
 YDOT =     -17364
366697  feet/sec       YDOT =       -5292
658969  meter/sec
 ZDOT =     -14178
470872                 ZDOT =       -4321
597922


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   07106
56035933  
00020000  00000-0  20000-3 0  9074
2 25544  51
6321  62
3390 0015616  73
2235 287
0642 15
78888725 41041


Satellite: ISS
Catalog Number: 25544
Epoch time:      07106
56035933   =   yrday
fracday
Element set:     907
Inclination:       51
6321  deg
RA of node:        62
3390  deg
Eccentricity:     
0015616     
Arg of perigee:    73
2235  deg
Mean anomaly:     287
0642  deg
Mean motion:   15
78888725  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4104
Checksum:              287


Coasting Arc #9 (Orbit 4119)
---------------------------------------

Vector Time (GMT): 2007/107/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1418872
40                 A    =         6708457
31  meter
 Y    =        4557619
14  meter          E    =           
0021903
 Z    =        4695050
51                 I    =           51
88752
 XDOT =      -5576
678155                 Wp   =           90
51942
 YDOT =      -4580
932437  meter/sec      RA   =           56
79633  deg
 ZDOT =       2750
422361                 TA   =          332
51093
                                          MA   =          332
62662
                                          Ha   =            188
130  n
mi
                                          Hp   =            170
654

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4655093
18                 X    =        -1492539
02
 Y    =       14952818
70  feet           Y    =         4541340
77  meter
 Z    =       15403709
03                 Z    =         4687978
43
 XDOT =     -18296
188171                 XDOT =       -5538
400329
 YDOT =     -15029
305897  feet/sec       YDOT =       -4643
079871  meter/sec
 ZDOT =       9023
695410                 ZDOT =        2723
423490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3910112
83                 X    =         1191802
39
 Y    =       15191106
01  feet           Y    =         4630249
11  meter
 Z    =       15377654
15                 Z    =         4687108
98
 XDOT =     -22416
433716                 XDOT =       -6832
528997
 YDOT =      -3298
102331  feet/sec       YDOT =       -1005
261591  meter/sec
 ZDOT =       8921
449184                 ZDOT =        2719
257711


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   07107
57303678  
00020000  00000-0  20000-3 0  9081
2 25544  51
6330  57
1004 0015428  77
5935 282
6956 15
78954581 41201


Satellite: ISS
Catalog Number: 25544
Epoch time:      07107
57303678   =   yrday
fracday
Element set:     908
Inclination:       51
6330  deg
RA of node:        57
1004  deg
Eccentricity:     
0015428     
Arg of perigee:    77
5935  deg
Mean anomaly:     282
6956  deg
Mean motion:   15
78954581  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4120
Checksum:              304


Coasting Arc #10 (Orbit 4134)
---------------------------------------

Vector Time (GMT): 2007/108/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4632324
33                 A    =         6717847
25  meter
 Y    =        4785402
14  meter          E    =           
0024276
 Z    =        -840819
87                 I    =           51
90221
 XDOT =      -2930
891982                 Wp   =           63
98807
 YDOT =       3864
692452  meter/sec      RA   =           51
61171  deg
 ZDOT =       5991
062234                 TA   =          286
85389
                                          MA   =          287
11998
                                          Ha   =            188
149  n
mi
                                          Hp   =            170
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15197914
46                 X    =         4582553
62
 Y    =       15700138
25  feet           Y    =         4836925
11  meter
 Z    =       -2758595
36                 Z    =         -818436
46
 XDOT =      -9615
787343                 XDOT =       -3002
993773
 YDOT =      12679
437180  feet/sec       YDOT =        3831
514406  meter/sec
 ZDOT =      19655
715991                 ZDOT =        5976
648560

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21310647
78                 X    =         6495485
44
 Y    =        4877330
28  feet           Y    =         1486610
27  meter
 Z    =       -2673711
66                 Z    =         -814947
31
 XDOT =       -891
725482                 XDOT =        -271
797927
 YDOT =      14376
710409  feet/sec       YDOT =        4382
021333  meter/sec
 ZDOT =      19601
919674                 ZDOT =        5974
665117


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   07108
52240216  
00020000  00000-0  20000-3 0  9096
2 25544  51
6331  52
1885 0015512  80
7610 279
5310 15
78943948 41354


Satellite: ISS
Catalog Number: 25544
Epoch time:      07108
52240216   =   yrday
fracday
Element set:     909
Inclination:       51
6331  deg
RA of node:        52
1885  deg
Eccentricity:     
0015512     
Arg of perigee:    80
7610  deg
Mean anomaly:     279
5310  deg
Mean motion:   15
78943948  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4135
Checksum:              282


Coasting Arc #11 (Orbit 4150)
---------------------------------------

Vector Time (GMT): 2007/109/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3712731
94                 A    =         6706275
73  meter
 Y    =       -2047968
92  meter          E    =           
0029822
 Z    =       -5221228
87                 I    =           51
84550
 XDOT =       4676
652460                 Wp   =           90
65059
 YDOT =       6023
345032  meter/sec      RA   =           46
45416  deg
 ZDOT =        967
296859                 TA   =          188
53254
                                          MA   =          188
58335
                                          Ha   =            188
049  n
mi
                                          Hp   =            170
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12180879
08                 X    =         3760720
92
 Y    =       -6719058
12  feet           Y    =        -2006182
54  meter
 Z    =      -17130015
98                 Z    =        -5203075
61
 XDOT =      15343
347966                 XDOT =        4604
251928
 YDOT =      19761
630683  feet/sec       YDOT =        6075
237129  meter/sec
 ZDOT =       3173
546125                 ZDOT =         989
840814

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6420844
77                 X    =         1957073
49
 Y    =      -12434675
14  feet           Y    =        -3790088
98  meter
 Z    =      -17061905
26                 Z    =        -5200468
72
 XDOT =      22848
764990                 XDOT =        6964
303569
 YDOT =       7346
193261  feet/sec       YDOT =        2239
119706  meter/sec
 ZDOT =       3259
180051                 ZDOT =         993
398080


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   07109
53503299  
00020000  00000-0  20000-3 0  9103
2 25544  51
6341  46
9487 0015445  84
6479 275
6448 15
78982482 41518


Satellite: ISS
Catalog Number: 25544
Epoch time:      07109
53503299   =   yrday
fracday
Element set:     910
Inclination:       51
6341  deg
RA of node:        46
9487  deg
Eccentricity:     
0015445     
Arg of perigee:    84
6479  deg
Mean anomaly:     275
6448  deg
Mean motion:   15
78982482  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4151
Checksum:              323


Coasting Arc #12 (Orbit 4166)
---------------------------------------

Vector Time (GMT): 2007/110/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 465135
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3190583
80                 A    =         6715195
88  meter
 Y    =       -5377819
11  meter          E    =           
0019721
 Z    =       -2459778
80                 I    =           51
85624
 XDOT =       5463
821617                 Wp   =           98
80492
 YDOT =       -805
793756  meter/sec      RA   =           41
32528  deg
 ZDOT =      -5364
685072                 TA   =          108
93508
                                          MA   =          108
72122
                                          Ha   =            187
961  n
mi
                                          Hp   =            170
437

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10467794
61                 X    =        -3118261
80
 Y    =      -17643763
48  feet           Y    =        -5413093
48  meter
 Z    =       -8070140
44                 Z    =        -2475103
53
 XDOT =      17925
923939                 XDOT =        5498
487048
 YDOT =      -2643
680302  feet/sec       YDOT =        -744
500082  meter/sec
 ZDOT =     -17600
672810                 ZDOT =       -5338
057322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18655198
18                 X    =        -5686104
41
 Y    =       -8480288
14  feet           Y    =        -2584791
82  meter
 Z    =       -8128503
82                 Z    =        -2477567
96
 XDOT =      12633
283934                 XDOT =        3850
624943
 YDOT =     -11139
137866  feet/sec       YDOT =       -3395
209222  meter/sec
 ZDOT =     -17500
489786                 ZDOT =       -5334
149287


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   07110
54763887  
00020000  00000-0  20000-3 0  9118
2 25544  51
6348  41
7090 0015452  88
5863 271
7073 15
79035008 41678


Satellite: ISS
Catalog Number: 25544
Epoch time:      07110
54763887   =   yrday
fracday
Element set:     911
Inclination:       51
6348  deg
RA of node:        41
7090  deg
Eccentricity:     
0015452     
Arg of perigee:    88
5863  deg
Mean anomaly:     271
7073  deg
Mean motion:   15
79035008  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4167
Checksum:              298

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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