Date: December 18th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3922)
---------------------------------------

Vector Time (GMT): 2007/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2446243
61                 A    =         6713314
71  meter
 Y    =       -4354437
24  meter          E    =           
0007893
 Z    =        4480895
40                 I    =           51
32003
 XDOT =       4272
062879                 Wp   =          109
65661
 YDOT =       5611
410900  meter/sec      RA   =          253
41648  deg
 ZDOT =       3113
749277                 TA   =          309
15158
                                          MA   =          309
22169
                                          Ha   =            184
382  n
mi
                                          Hp   =            178
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8025733
62                 X    =         2472986
43
 Y    =      -14286211
43  feet           Y    =        -4326932
99  meter
 Z    =       14701100
38                 Z    =         4492843
65
 XDOT =      14015
954329                 XDOT =        4193
871714
 YDOT =      18410
140748  feet/sec       YDOT =        5658
745954  meter/sec
 ZDOT =      10215
712851                 ZDOT =        3134
313699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13048311
04                 X    =         3977125
20
 Y    =        9844910
96  feet           Y    =         3000728
86  meter
 Z    =       14746182
45                 Z    =         4494636
41
 XDOT =     -19448
187818                 XDOT =       -5927
807647
 YDOT =      10321
897506  feet/sec       YDOT =        3146
114360  meter/sec
 ZDOT =      10294
678993                 ZDOT =        3137
818157


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   07348
55303019  
00020000  00000-0  20000-3 0  9007
2 25544  51
6396 253
9353 0001092 320
3366  39
7719 15
77531681 39234


Satellite: ISS
Catalog Number: 25544
Epoch time:      07348
55303019   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:       253
9353  deg
Eccentricity:     
0001092     
Arg of perigee:   320
3366  deg
Mean anomaly:      39
7719  deg
Mean motion:   15
77531681  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3923
Checksum:              293


Coasting Arc #2 (Orbit 3937)
---------------------------------------

Vector Time (GMT): 2007/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3584137
08                 A    =         6720785
42  meter
 Y    =       -5440882
68  meter          E    =           
0008215
 Z    =       -1633982
22                 I    =           51
35575
 XDOT =       3356
352638                 Wp   =           29
71081
 YDOT =      -3923
001331  meter/sec      RA   =          248
19288  deg
 ZDOT =       5720
057813                 TA   =          312
14229
                                          MA   =          312
21206
                                          Ha   =            184
327  n
mi
                                          Hp   =            178
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11758979
94                 X    =        -3515092
34
 Y    =      -17850664
95  feet           Y    =        -5480576
32  meter
 Z    =       -5360834
07                 Z    =        -1651226
80
 XDOT =      11011
655636                 XDOT =        3372
183801
 YDOT =     -12870
739275  feet/sec       YDOT =       -3885
380762  meter/sec
 ZDOT =      18766
593876                 ZDOT =        5736
401016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19143054
04                 X    =         5834802
87
 Y    =       -9473542
45  feet           Y    =        -2887535
74  meter
 Z    =       -5427141
59                 Z    =        -1654192
76
 XDOT =      10760
037682                 XDOT =        3279
659485
 YDOT =      10992
127523  feet/sec       YDOT =        3350
400469  meter/sec
 ZDOT =      18828
470443                 ZDOT =        5738
917791


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   07349
50322444  
00020000  00000-0  20000-3 0  9017
2 25544  51
6399 249
0296 0001162 321
0213  39
0868 15
77587907 39382


Satellite: ISS
Catalog Number: 25544
Epoch time:      07349
50322444   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:       249
0296  deg
Eccentricity:     
0001162     
Arg of perigee:   321
0213  deg
Mean anomaly:      39
0868  deg
Mean motion:   15
77587907  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3938
Checksum:              301


Coasting Arc #3 (Orbit 3953)
---------------------------------------

Vector Time (GMT): 2007/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3473045
77                 A    =         6709810
19  meter
 Y    =        2399569
26  meter          E    =           
0014364
 Z    =       -5227886
31                 I    =           51
33150
 XDOT =      -3837
438080                 Wp   =           81
94081
 YDOT =      -6652
535377  meter/sec      RA   =          243
02841  deg
 ZDOT =       -503
339979                 TA   =          183
24970
                                          MA   =          183
25904
                                          Ha   =            184
286  n
mi
                                          Hp   =            178
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11394507
13                 X    =        -3474223
82
 Y    =        7872602
55  feet           Y    =         2360725
55  meter
 Z    =      -17151857
99                 Z    =        -5244761
06
 XDOT =     -12590
019946                 XDOT =       -3760
318070
 YDOT =     -21825
903469  feet/sec       YDOT =       -6695
016544  meter/sec
 ZDOT =      -1651
377883                 ZDOT =        -521
795535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6650509
85                 X    =        -2027075
40
 Y    =      -12057429
16  feet           Y    =        -3675104
41  meter
 Z    =      -17215923
35                 Z    =        -5247413
44
 XDOT =      22140
469491                 XDOT =        6748
415101
 YDOT =      -9748
893094  feet/sec       YDOT =       -2971
462615  meter/sec
 ZDOT =      -1722
442057                 ZDOT =        -525
000339


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   07350
51673297  
00020000  00000-0  20000-3 0  9026
2 25544  51
6402 243
7965 0001210 325
3618  34
7468 15
77649935 39547


Satellite: ISS
Catalog Number: 25544
Epoch time:      07350
51673297   =   yrday
fracday
Element set:     902
Inclination:       51
6402  deg
RA of node:       243
7965  deg
Eccentricity:     
0001210     
Arg of perigee:   325
3618  deg
Mean anomaly:      34
7468  deg
Mean motion:   15
77649935  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3954
Checksum:              305


Coasting Arc #4 (Orbit 3969)
---------------------------------------

Vector Time (GMT): 2007/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2995496
53                 A    =         6721551
13  meter
 Y    =        5959585
67  meter          E    =           
0009321
 Z    =        -795551
45                 I    =           51
38559
 XDOT =      -4643
523036                 Wp   =          140
99710
 YDOT =       1545
452183  meter/sec      RA   =          237
84785  deg
 ZDOT =      -5951
943477                 TA   =           47
72093
                                          MA   =           47
64193
                                          Ha   =            184
269  n
mi
                                          Hp   =            178
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9827744
52                 X    =         2932497
57
 Y    =       19552446
41  feet           Y    =         5992730
82  meter
 Z    =       -2610076
95                 Z    =         -781151
81
 XDOT =     -15234
655629                 XDOT =       -4631
545756
 YDOT =       5070
381177  feet/sec       YDOT =        1493
593100  meter/sec
 ZDOT =     -19527
373611                 ZDOT =       -5974
472641

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20336588
67                 X    =        -6198592
23
 Y    =        8098932
82  feet           Y    =         2468554
72  meter
 Z    =       -2554539
76                 Z    =         -778623
72
 XDOT =      -3140
951027                 XDOT =        -957
361873
 YDOT =     -14025
877542  feet/sec       YDOT =       -4275
087475  meter/sec
 ZDOT =     -19613
087320                 ZDOT =       -5978
069015


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   07351
53021008  
00020000  00000-0  20000-3 0  9037
2 25544  51
6402 238
5632 0001146 320
0846  40
0235 15
77648091 39705


Satellite: ISS
Catalog Number: 25544
Epoch time:      07351
53021008   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:       238
5632  deg
Eccentricity:     
0001146     
Arg of perigee:   320
0846  deg
Mean anomaly:      40
0235  deg
Mean motion:   15
77648091  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3970
Checksum:              254


Coasting Arc #5 (Orbit 3985)
---------------------------------------

Vector Time (GMT): 2007/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4625208
91                 A    =         6711058
76  meter
 Y    =        -328231
25  meter          E    =           
0006709
 Z    =        4849124
95                 I    =           51
36819
 XDOT =       2879
901792                 Wp   =           45
67092
 YDOT =       6776
916558  meter/sec      RA   =          232
63874  deg
 ZDOT =      -2281
629631                 TA   =           66
62903
                                          MA   =           66
55847
                                          Ha   =            183
952  n
mi
                                          Hp   =            178
248

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15174569
90                 X    =         4604979
05
 Y    =       -1076874
18  feet           Y    =         -276623
04  meter
 Z    =       15909202
61                 Z    =         4871545
30
 XDOT =       9448
496694                 XDOT =        2814
991102
 YDOT =      22233
978209  feet/sec       YDOT =        6808
758505  meter/sec
 ZDOT =      -7485
661519                 ZDOT =       -2267
796036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          16849
65                 X    =            5135
77
 Y    =       15122871
28  feet           Y    =         4609451
16  meter
 Z    =       15994637
78                 Z    =         4875165
60
 XDOT =     -21741
771862                 XDOT =       -6626
892064
 YDOT =       7907
510937  feet/sec       YDOT =        2410
209334  meter/sec
 ZDOT =      -7432
188192                 ZDOT =       -2265
330961


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   07352
54365239  
00020000  00000-0  20000-3 0  9047
2 25544  51
6403 233
3297 0001424 326
3000  33
8074 15
77775739 39864


Satellite: ISS
Catalog Number: 25544
Epoch time:      07352
54365239   =   yrday
fracday
Element set:     904
Inclination:       51
6403  deg
RA of node:       233
3297  deg
Eccentricity:     
0001424     
Arg of perigee:   326
3000  deg
Mean anomaly:      33
8074  deg
Mean motion:   15
77775739  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3986
Checksum:              293


Coasting Arc #6 (Orbit 4001)
---------------------------------------

Vector Time (GMT): 2007/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1858090
45                 A    =         6717378
59  meter
 Y    =       -5665808
70  meter          E    =           
0012721
 Z    =        3079815
25                 I    =           51
40779
 XDOT =       5930
673377                 Wp   =           78
92747
 YDOT =        713
043083  meter/sec      RA   =          227
49935  deg
 ZDOT =       4875
248940                 TA   =          317
02688
                                          MA   =          317
12618
                                          Ha   =            184
169  n
mi
                                          Hp   =            178
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6096097
28                 X    =        -1809557
82
 Y    =      -18588611
21  feet           Y    =        -5686315
86  meter
 Z    =       10104380
75                 Z    =         3070905
84
 XDOT =      19457
589820                 XDOT =        5898
575817
 YDOT =       2339
380195  feet/sec       YDOT =         779
183289  meter/sec
 ZDOT =      15994
911221                 ZDOT =        4903
982678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18888220
28                 X    =         5757129
54
 Y    =       -5160588
20  feet           Y    =        -1572947
28  meter
 Z    =       10069798
57                 Z    =         3069274
60
 XDOT =      -3737
464604                 XDOT =       -1139
179211
 YDOT =      17838
640899  feet/sec       YDOT =        5437
217746  meter/sec
 ZDOT =      16104
534475                 ZDOT =        4908
662108


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   07353
55706685  
00020000  00000-0  20000-3 0  9054
2 25544  51
6402 228
0957 0001436 333
9079  26
2014 15
77763434 40029


Satellite: ISS
Catalog Number: 25544
Epoch time:      07353
55706685   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       228
0957  deg
Eccentricity:     
0001436     
Arg of perigee:   333
9079  deg
Mean anomaly:      26
2014  deg
Mean motion:   15
77763434  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4002
Checksum:              285


Coasting Arc #7 (Orbit 4016)
---------------------------------------

Vector Time (GMT): 2007/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5617462
29                 A    =         6716224
80  meter
 Y    =       -1461655
77  meter          E    =           
0004348
 Z    =       -3381061
54                 I    =           51
42505
 XDOT =      -1195
296529                 Wp   =           74
37457
 YDOT =      -6054
217703  meter/sec      RA   =          222
26778  deg
 ZDOT =       4609
261285                 TA   =          245
54890
                                          MA   =          245
59425
                                          Ha   =            183
974  n
mi
                                          Hp   =            178
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18429994
38                 X    =        -5584275
48
 Y    =       -4795458
57  feet           Y    =        -1524287
43  meter
 Z    =      -11092721
59                 Z    =        -3408271
19
 XDOT =      -3921
576538                 XDOT =       -1149
899824
 YDOT =     -19862
918974  feet/sec       YDOT =       -6067
330950  meter/sec
 ZDOT =      15122
248309                 ZDOT =        4603
563936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5448882
95                 X    =         1660819
52
 Y    =      -18183917
97  feet           Y    =        -5542458
20  meter
 Z    =      -11196624
05                 Z    =        -3412731
01
 XDOT =      18667
444173                 XDOT =        5689
836984
 YDOT =      -3691
745828  feet/sec       YDOT =       -1125
244128  meter/sec
 ZDOT =      15099
870518                 ZDOT =        4602
440534


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   07354
50711151  
00020000  00000-0  20000-3 0  9065
2 25544  51
6398 223
1891 0001537 329
7324  30
3753 15
77824438 40178


Satellite: ISS
Catalog Number: 25544
Epoch time:      07354
50711151   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       223
1891  deg
Eccentricity:     
0001537     
Arg of perigee:   329
7324  deg
Mean anomaly:      30
3753  deg
Mean motion:   15
77824438  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4017
Checksum:              285


Coasting Arc #8 (Orbit 4032)
---------------------------------------

Vector Time (GMT): 2007/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          61035
71                 A    =         6711422
28  meter
 Y    =        4774433
48  meter          E    =           
0011208
 Z    =       -4727078
10                 I    =           51
43058
 XDOT =      -6786
173940                 Wp   =           63
52735
 YDOT =      -2512
705221  meter/sec      RA   =          217
13416  deg
 ZDOT =      -2625
369158                 TA   =          180
61000
                                          MA   =          180
61137
                                          Ha   =            183
951  n
mi
                                          Hp   =            178
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         200248
40                 X    =           30606
36
 Y    =       15664151
84  feet           Y    =         4774946
64  meter
 Z    =      -15508786
40                 Z    =        -4726854
73
 XDOT =     -22264
350197                 XDOT =       -6744
818369
 YDOT =      -8243
783532  feet/sec       YDOT =       -2588
360413  meter/sec
 ZDOT =      -8613
415872                 ZDOT =       -2658
236827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15666783
30                 X    =        -4775235
55
 Y    =          -2732
21  feet           Y    =            -832
78  meter
 Z    =      -15507420
85                 Z    =        -4726661
88
 XDOT =       8654
196627                 XDOT =        2637
799132
 YDOT =     -20916
190894  feet/sec       YDOT =       -6375
254985  meter/sec
 ZDOT =      -8739
017697                 ZDOT =       -2663
652594


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   07355
52046303  
00020000  00000-0  20000-3 0  9079
2 25544  51
6389 217
9549 0001592 331
5570  28
5508 15
77877606 40334


Satellite: ISS
Catalog Number: 25544
Epoch time:      07355
52046303   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:       217
9549  deg
Eccentricity:     
0001592     
Arg of perigee:   331
5570  deg
Mean anomaly:      28
5508  deg
Mean motion:   15
77877606  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4033
Checksum:              305


Coasting Arc #9 (Orbit 4048)
---------------------------------------

Vector Time (GMT): 2007/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6025368
15                 A    =         6720571
16  meter
 Y    =        2773360
67  meter          E    =           
0012633
 Z    =        1045963
71                 I    =           51
48578
 XDOT =      -1178
456540                 Wp   =          119
87000
 YDOT =       4806
587031  meter/sec      RA   =          211
92516  deg
 ZDOT =      -5909
119131                 TA   =           48
64718
                                          MA   =           48
53858
                                          Ha   =            183
961  n
mi
                                          Hp   =            177
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19768268
22                 X    =         5988827
04
 Y    =        9098952
32  feet           Y    =         2840535
24  meter
 Z    =        3431639
46                 Z    =         1075146
99
 XDOT =      -3866
327231                 XDOT =       -1203
411238
 YDOT =      15769
642489  feet/sec       YDOT =        4793
270442  meter/sec
 ZDOT =     -19386
873791                 ZDOT =       -5914
903843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9125522
81                 X    =        -2781459
35
 Y    =       19736307
48  feet           Y    =         6015626
52  meter
 Z    =        3543234
64                 Z    =         1079977
92
 XDOT =     -14325
357859                 XDOT =       -4366
369076
 YDOT =      -3112
533768  feet/sec       YDOT =        -948
700292  meter/sec
 ZDOT =     -19408
420052                 ZDOT =       -5915
686432


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   07356
53378466  
00020000  00000-0  20000-3 0  9080
2 25544  51
6387 212
7211 0001488 337
8987  22
2113 15
77909064 40490


Satellite: ISS
Catalog Number: 25544
Epoch time:      07356
53378466   =   yrday
fracday
Element set:     908
Inclination:       51
6387  deg
RA of node:       212
7211  deg
Eccentricity:     
0001488     
Arg of perigee:   337
8987  deg
Mean anomaly:      22
2113  deg
Mean motion:   15
77909064  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4049
Checksum:              312


Coasting Arc #10 (Orbit 4064)
---------------------------------------

Vector Time (GMT): 2007/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2182631
09                 A    =         6708842
35  meter
 Y    =       -3572831
61  meter          E    =           
0002724
 Z    =        5240608
06                 I    =           51
47105
 XDOT =       6765
907300                 Wp   =           42
38132
 YDOT =       3682
978210  meter/sec      RA   =          206
75524  deg
 ZDOT =       -304
916454                 TA   =           50
52872
                                          MA   =           50
50463
                                          Ha   =            183
812  n
mi
                                          Hp   =            177
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7160863
15                 X    =         2196962
83
 Y    =      -11721888
50  feet           Y    =        -3548345
12  meter
 Z    =       17193595
99                 Z    =         5251245
40
 XDOT =      22197
858596                 XDOT =        6725
702051
 YDOT =      12083
261844  feet/sec       YDOT =        3758
413683  meter/sec
 ZDOT =      -1000
382068                 ZDOT =        -272
144512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11832393
84                 X    =         3606513
64
 Y    =        6876872
76  feet           Y    =         2096070
82  meter
 Z    =       17233788
06                 Z    =         5252858
60
 XDOT =     -11228
222384                 XDOT =       -3422
362183
 YDOT =      21529
123030  feet/sec       YDOT =        6562
076700  meter/sec
 ZDOT =       -874
983258                 ZDOT =        -266
694897


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   07357
54707359  
00020000  00000-0  20000-3 0  9090
2 25544  51
6377 207
4859 0001594 338
4583  21
6515 15
77964798 40657


Satellite: ISS
Catalog Number: 25544
Epoch time:      07357
54707359   =   yrday
fracday
Element set:     909
Inclination:       51
6377  deg
RA of node:       207
4859  deg
Eccentricity:     
0001594     
Arg of perigee:   338
4583  deg
Mean anomaly:      21
6515  deg
Mean motion:   15
77964798  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4065
Checksum:              339


Coasting Arc #11 (Orbit 4080)
---------------------------------------

Vector Time (GMT): 2007/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5493852
47                 A    =         6719670
66  meter
 Y    =       -3520130
16  meter          E    =           
0014348
 Z    =        1574583
69                 I    =           51
53349
 XDOT =       3837
880065                 Wp   =           56
28266
 YDOT =      -3400
893156  meter/sec      RA   =          201
59583  deg
 ZDOT =       5758
115392                 TA   =          321
15157
                                          MA   =          321
25462
                                          Ha   =            183
776  n
mi
                                          Hp   =            177
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18024450
37                 X    =        -5461730
53
 Y    =      -11548983
48  feet           Y    =        -3581386
24  meter
 Z    =        5165956
98                 Z    =         1547972
02
 XDOT =      12591
470028                 XDOT =        3847
652402
 YDOT =     -11157
785944  feet/sec       YDOT =       -3357
922297  meter/sec
 ZDOT =      18891
454697                 ZDOT =        5776
782785

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10945955
72                 X    =         3336327
30
 Y    =      -18425209
45  feet           Y    =        -5616003
84  meter
 Z    =        5064054
91                 Z    =         1543523
94
 XDOT =      10220
726541                 XDOT =        3115
277450
 YDOT =      11310
730217  feet/sec       YDOT =        3447
510570  meter/sec
 ZDOT =      18962
305144                 ZDOT =        5779
710608


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   07358
56033089  
00020000  00000-0  20000-3 0  9107
2 25544  51
6363 202
2501 0001625 337
6515  22
4579 15
78041662 40814


Satellite: ISS
Catalog Number: 25544
Epoch time:      07358
56033089   =   yrday
fracday
Element set:     910
Inclination:       51
6363  deg
RA of node:       202
2501  deg
Eccentricity:     
0001625     
Arg of perigee:   337
6515  deg
Mean anomaly:      22
4579  deg
Mean motion:   15
78041662  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4081
Checksum:              273


Coasting Arc #12 (Orbit 4095)
---------------------------------------

Vector Time (GMT): 2007/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4437937
44                 A    =         6711891
77  meter
 Y    =        2377785
77  meter          E    =           
0008870
 Z    =       -4446967
67                 I    =           51
53426
 XDOT =      -5522
931399                 Wp   =          102
40440
 YDOT =      -4290
805540  meter/sec      RA   =          196
38213  deg
 ZDOT =       3220
940000                 TA   =          199
87162
                                          MA   =          199
90620
                                          Ha   =            183
750  n
mi
                                          Hp   =            177
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14560162
22                 X    =        -4442594
06
 Y    =        7801134
43  feet           Y    =         2328132
99  meter
 Z    =      -14589788
95                 Z    =        -4468537
82
 XDOT =     -18119
853671                 XDOT =       -5490
187045
 YDOT =     -14077
445998  feet/sec       YDOT =       -4352
383579  meter/sec
 ZDOT =      10567
388450                 ZDOT =        3194
188675

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8518612
56                 X    =        -2596473
11
 Y    =      -14067283
98  feet           Y    =        -4287708
16  meter
 Z    =      -14671834
43                 Z    =        -4471975
13
 XDOT =      12120
533609                 XDOT =        3694
338644
 YDOT =     -18242
376183  feet/sec       YDOT =       -5560
276261  meter/sec
 ZDOT =      10464
851164                 ZDOT =        3189
686635


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   07359
51023347  
00020000  00000-0  20000-3 0  9110
2 25544  51
6353 197
3411 0001660 343
2191  16
8919 15
78068929 40965


Satellite: ISS
Catalog Number: 25544
Epoch time:      07359
51023347   =   yrday
fracday
Element set:     911
Inclination:       51
6353  deg
RA of node:       197
3411  deg
Eccentricity:     
0001660     
Arg of perigee:   343
2191  deg
Mean anomaly:      16
8919  deg
Mean motion:   15
78068929  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            4096
Checksum:              297

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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