Date: March 23rd 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 8234 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 1481)
---------------------------------------

Vector Time (GMT): 2008/082/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1959480
33                 A    =         6725476
47  meter
 Y    =       -6407681
26  meter          E    =           
0010084
 Z    =        -515000
92                 I    =           51
97530
 XDOT =       4417
554778                 Wp   =          144
58566
 YDOT =       1831
060289  meter/sec      RA   =          103
55804  deg
 ZDOT =      -6040
698371                 TA   =           40
99698
                                          MA   =           40
92122
                                          Ha   =            186
015  n
mi
                                          Hp   =            180
758

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6428741
22                 X    =         2033488
15
 Y    =      -21022576
31  feet           Y    =        -6385355
49  meter
 Z    =       -1689635
57                 Z    =         -505301
36
 XDOT =      14493
289955                 XDOT =        4426
095801
 YDOT =       6007
415647  feet/sec       YDOT =        1880
507033  meter/sec
 ZDOT =     -19818
564210                 ZDOT =       -6019
217397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21941777
54                 X    =         6687853
79
 Y    =        1399169
15  feet           Y    =          426466
76  meter
 Z    =       -1653185
07                 Z    =         -503890
81
 XDOT =      -2362
891998                 XDOT =        -720
209481
 YDOT =      13999
195547  feet/sec       YDOT =        4266
954803  meter/sec
 ZDOT =     -19735
973053                 ZDOT =       -6015
524587


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   08082
31957819  
00020000  00000-0  20000-3 0  9000
2 25544  51
6391 104
2004 0001499 277
7934  82
3061 15
76319087 14822


Satellite: ISS
Catalog Number: 25544
Epoch time:      08082
31957819   =   yrday
fracday
Element set:     900
Inclination:       51
6391  deg
RA of node:       104
2004  deg
Eccentricity:     
0001499     
Arg of perigee:   277
7934  deg
Mean anomaly:      82
3061  deg
Mean motion:   15
76319087  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1482
Checksum:              294


Coasting Arc #2 (Orbit 1497)
---------------------------------------

Vector Time (GMT): 2008/083/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3729247
69                 A    =         6714010
88  meter
 Y    =       -2211057
11  meter          E    =           
0003896
 Z    =        5125328
63                 I    =           51
94339
 XDOT =       2240
587906                 Wp   =           35
66051
 YDOT =      -7222
810150  meter/sec      RA   =           98
40935  deg
 ZDOT =      -1481
970958                 TA   =           68
49673
                                          MA   =           68
45519
                                          Ha   =            186
015  n
mi
                                          Hp   =            180
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12235064
60                 X    =        -3729144
11
 Y    =       -7254124
37  feet           Y    =        -2252758
63  meter
 Z    =       16815382
64                 Z    =         5107212
37
 XDOT =       7351
010189                 XDOT =        2328
387125
 YDOT =     -23696
883693  feet/sec       YDOT =       -7197
263842  meter/sec
 ZDOT =      -4862
109443                 ZDOT =       -1470
872230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3968406
97                 X    =         1209570
44
 Y    =      -13744492
31  feet           Y    =        -4189321
26  meter
 Z    =       16745653
07                 Z    =         5104075
06
 XDOT =      23784
294676                 XDOT =        7249
453017
 YDOT =        979
560247  feet/sec       YDOT =         298
569963  meter/sec
 ZDOT =      -4820
377914                 ZDOT =       -1469
251188


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   08083
33390013  
00020000  00000-0  20000-3 0  9011
2 25544  51
6396  98
9725 0001568 287
4981  72
6012 15
76389386 14987


Satellite: ISS
Catalog Number: 25544
Epoch time:      08083
33390013   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:        98
9725  deg
Eccentricity:     
0001568     
Arg of perigee:   287
4981  deg
Mean anomaly:      72
6012  deg
Mean motion:   15
76389386  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1498
Checksum:              320


Coasting Arc #3 (Orbit 1513)
---------------------------------------

Vector Time (GMT): 2008/084/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1956521
64                 A    =         6723580
24  meter
 Y    =        6090511
97  meter          E    =           
0013074
 Z    =        2048446
35                 I    =           51
97850
 XDOT =      -4195
617401                 Wp   =           64
61759
 YDOT =      -3237
357905  meter/sec      RA   =           93
30947  deg
 ZDOT =       5596
068262                 TA   =          318
15767
                                          MA   =          318
25754
                                          Ha   =            185
978  n
mi
                                          Hp   =            180
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6419034
24                 X    =        -2034432
30
 Y    =       19981994
66  feet           Y    =         6068197
56  meter
 Z    =        6720624
50                 Z    =         2038751
82
 XDOT =     -13765
148953                 XDOT =       -4186
289752
 YDOT =     -10621
252970  feet/sec       YDOT =       -3284
223123  meter/sec
 ZDOT =      18359
804010                 ZDOT =        5575
708759

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20978436
83                 X    =        -6394227
55
 Y    =        -937230
77  feet           Y    =         -285667
94  meter
 Z    =        6684137
29                 Z    =         2037325
05
 XDOT =       6502
717996                 XDOT =        1982
028445
 YDOT =     -14656
205481  feet/sec       YDOT =       -4467
211431  meter/sec
 ZDOT =      18281
357417                 ZDOT =        5572
157741


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   08084
34820442  
00020000  00000-0  20000-3 0  9028
2 25544  51
6395  93
7453 0001469 291
7631  68
3377 15
76391282 15140


Satellite: ISS
Catalog Number: 25544
Epoch time:      08084
34820442   =   yrday
fracday
Element set:     902
Inclination:       51
6395  deg
RA of node:        93
7453  deg
Eccentricity:     
0001469     
Arg of perigee:   291
7631  deg
Mean anomaly:      68
3377  deg
Mean motion:   15
76391282  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1514
Checksum:              300


Coasting Arc #4 (Orbit 1528)
---------------------------------------

Vector Time (GMT): 2008/085/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3639023
02                 A    =         6716471
48  meter
 Y    =        3411487
92  meter          E    =           
0008425
 Z    =       -4506052
67                 I    =           51
95496
 XDOT =      -2276
177728                 Wp   =          109
24444
 YDOT =       6628
747883  meter/sec      RA   =           88
13747  deg
 ZDOT =       3182
432376                 TA   =          192
41290
                                          MA   =          192
43366
                                          Ha   =            185
928  n
mi
                                          Hp   =            180
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11939051
90                 X    =         3622494
49
 Y    =       11192545
66  feet           Y    =         3452088
89  meter
 Z    =      -14783637
36                 Z    =        -4488414
52
 XDOT =      -7467
774698                 XDOT =       -2365
592023
 YDOT =      21747
860507  feet/sec       YDOT =        6602
794595  meter/sec
 ZDOT =      10441
051104                 ZDOT =        3171
157090

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7359198
90                 X    =        -2243083
83
 Y    =       14685466
90  feet           Y    =         4476130
31  meter
 Z    =      -14715611
62                 Z    =        -4485318
42
 XDOT =     -21916
051621                 XDOT =       -6680
012534
 YDOT =       -569
576521  feet/sec       YDOT =        -173
606923  meter/sec
 ZDOT =      10398
550258                 ZDOT =        3169
478118


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   08085
29909626  
00020000  00000-0  20000-3 0  9036
2 25544  51
6391  88
8452 0001424 298
0272  62
0748 15
76442085 15299


Satellite: ISS
Catalog Number: 25544
Epoch time:      08085
29909626   =   yrday
fracday
Element set:     903
Inclination:       51
6391  deg
RA of node:        88
8452  deg
Eccentricity:     
0001424     
Arg of perigee:   298
0272  deg
Mean anomaly:      62
0748  deg
Mean motion:   15
76442085  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1529
Checksum:              307


Coasting Arc #5 (Orbit 1544)
---------------------------------------

Vector Time (GMT): 2008/086/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2064533
17                 A    =         6720101
06  meter
 Y    =       -5385935
04  meter          E    =           
0003885
 Z    =       -3452264
99                 I    =           51
96451
 XDOT =       4177
882705                 Wp   =           75
04051
 YDOT =       4546
957390  meter/sec      RA   =           83
05481  deg
 ZDOT =      -4598
600173                 TA   =          145
65428
                                          MA   =          145
62916
                                          Ha   =            185
940  n
mi
                                          Hp   =            180
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6773402
77                 X    =         2141376
67
 Y    =      -17670390
56  feet           Y    =        -5362418
72  meter
 Z    =      -11326328
69                 Z    =        -3442048
59
 XDOT =      13706
964256                 XDOT =        4149
066714
 YDOT =      14917
839206  feet/sec       YDOT =        4593
515584  meter/sec
 ZDOT =     -15087
270908                 ZDOT =       -4578
374050

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18904766
65                 X    =         5762172
88
 Y    =        1266549
54  feet           Y    =          386044
30  meter
 Z    =      -11287739
33                 Z    =        -3440502
95
 XDOT =     -10042
632996                 XDOT =       -3060
994537
 YDOT =      16229
806265  feet/sec       YDOT =        4946
844949  meter/sec
 ZDOT =     -15009
197923                 ZDOT =       -4574
803527


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   08086
31336191  
00020000  00000-0  20000-3 0  9042
2 25544  51
6387  83
6173 0001468 301
4360  58
6660 15
76433550 15451


Satellite: ISS
Catalog Number: 25544
Epoch time:      08086
31336191   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:        83
6173  deg
Eccentricity:     
0001468     
Arg of perigee:   301
4360  deg
Mean anomaly:      58
6660  deg
Mean motion:   15
76433550  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1545
Checksum:              285


Coasting Arc #6 (Orbit 1560)
---------------------------------------

Vector Time (GMT): 2008/087/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3689273
96                 A    =         6720027
24  meter
 Y    =       -4453355
20  meter          E    =           
0011360
 Z    =        3414302
68                 I    =           51
96099
 XDOT =       2496
759852                 Wp   =           84
30446
 YDOT =      -5630
512615  meter/sec      RA   =           77
87192  deg
 ZDOT =      -4631
992281                 TA   =           55
49083
                                          MA   =           55
38361
                                          Ha   =            185
907  n
mi
                                          Hp   =            180
383

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12103917
19                 X    =        -3655787
79
 Y    =      -14610745
42  feet           Y    =        -4494423
48  meter
 Z    =       11201780
43                 Z    =         3396461
52
 XDOT =       8191
469331                 XDOT =        2582
037038
 YDOT =     -18472
810417  feet/sec       YDOT =       -5602
115697  meter/sec
 ZDOT =     -15196
825070                 ZDOT =       -4619
655725

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10049485
69                 X    =         3063083
24
 Y    =      -16140807
00  feet           Y    =        -4919717
97  meter
 Z    =       11132868
66                 Z    =         3393298
37
 XDOT =      18960
868581                 XDOT =        5779
272743
 YDOT =       1323
447511  feet/sec       YDOT =         403
386801  meter/sec
 ZDOT =     -15150
120408                 ZDOT =       -4617
756700


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   08087
32760564  
00020000  00000-0  20000-3 0  9050
2 25544  51
6396  78
3895 0001619 310
6281  49
4742 15
76508521 15613


Satellite: ISS
Catalog Number: 25544
Epoch time:      08087
32760564   =   yrday
fracday
Element set:     905
Inclination:       51
6396  deg
RA of node:        78
3895  deg
Eccentricity:     
0001619     
Arg of perigee:   310
6281  deg
Mean anomaly:      49
4742  deg
Mean motion:   15
76508521  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1561
Checksum:              305


Coasting Arc #7 (Orbit 1576)
---------------------------------------

Vector Time (GMT): 2008/088/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2355211
14                 A    =         6716121
32  meter
 Y    =        4365493
36  meter          E    =           
0007362
 Z    =        4523225
84                 I    =           51
94040
 XDOT =      -4298
382792                 Wp   =          109
45574
 YDOT =      -5575
839868  meter/sec      RA   =           72
78812  deg
 ZDOT =       3136
758970                 TA   =          309
38849
                                          MA   =          309
45366
                                          Ha   =            185
941  n
mi
                                          Hp   =            180
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7727070
68                 X    =        -2425824
78
 Y    =       14322484
79  feet           Y    =         4338761
27  meter
 Z    =       14839979
78                 Z    =         4511612
64
 XDOT =     -14102
305748                 XDOT =       -4250
951257
 YDOT =     -18293
437886  feet/sec       YDOT =       -5623
641608  meter/sec
 ZDOT =      10291
203970                 ZDOT =        3115
992645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16098907
52                 X    =        -4906947
01
 Y    =       -2640565
39  feet           Y    =         -804844
33  meter
 Z    =       14795904
26                 Z    =         4509791
62
 XDOT =      12395
161630                 XDOT =        3778
045265
 YDOT =     -18235
315601  feet/sec       YDOT =       -5558
124195  meter/sec
 ZDOT =      10210
954404                 ZDOT =        3112
298902


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   08088
34182989  
00020000  00000-0  20000-3 0  9063
2 25544  51
6394  73
1616 0001520 312
7049  47
3987 15
76525236 15778


Satellite: ISS
Catalog Number: 25544
Epoch time:      08088
34182989   =   yrday
fracday
Element set:     906
Inclination:       51
6394  deg
RA of node:        73
1616  deg
Eccentricity:     
0001520     
Arg of perigee:   312
7049  deg
Mean anomaly:      47
3987  deg
Mean motion:   15
76525236  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1577
Checksum:              313


Coasting Arc #8 (Orbit 1591)
---------------------------------------

Vector Time (GMT): 2008/089/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3802781
87                 A    =         6723326
76  meter
 Y    =        5177128
74  meter          E    =           
0007400
 Z    =       -1973686
36                 I    =           51
95444
 XDOT =      -2981
380706                 Wp   =           27
14332
 YDOT =       4330
769923  meter/sec      RA   =           67
61420  deg
 ZDOT =       5630
240310                 TA   =          310
95943
                                          MA   =          311
02344
                                          Ha   =            185
961  n
mi
                                          Hp   =            180
265

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12476318
48                 X    =         3754195
58
 Y    =       16985330
52  feet           Y    =         5219381
95  meter
 Z    =       -6475348
95                 Z    =        -1955330
51
 XDOT =      -9781
432762                 XDOT =       -3056
937128
 YDOT =      14208
562739  feet/sec       YDOT =        4297
007998  meter/sec
 ZDOT =      18471
917027                 ZDOT =        5615
573225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11595970
95                 X    =        -3534451
94
 Y    =       17624056
65  feet           Y    =         5371812
47  meter
 Z    =       -6404389
51                 Z    =        -1952057
92
 XDOT =     -15469
041204                 XDOT =       -4714
963759
 YDOT =      -3503
495935  feet/sec       YDOT =       -1067
865561  meter/sec
 ZDOT =      18416
116929                 ZDOT =        5613
232440


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   08089
29264683  
00020000  00000-0  20000-3 0  9071
2 25544  51
6391  68
2605 0001570 321
3772  38
7280 15
76527353 15921


Satellite: ISS
Catalog Number: 25544
Epoch time:      08089
29264683   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:        68
2605  deg
Eccentricity:     
0001570     
Arg of perigee:   321
3772  deg
Mean anomaly:      38
7280  deg
Mean motion:   15
76527353  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1592
Checksum:              304


Coasting Arc #9 (Orbit 1607)
---------------------------------------

Vector Time (GMT): 2008/090/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2926397
47                 A    =         6713366
31  meter
 Y    =       -3150725
71  meter          E    =           
0013678
 Z    =       -5167357
84                 I    =           51
90924
 XDOT =       4373
525826                 Wp   =           74
34770
 YDOT =       6196
234268  meter/sec      RA   =           62
50831  deg
 ZDOT =      -1300
460627                 TA   =          183
24803
                                          MA   =          183
25692
                                          Ha   =            185
931  n
mi
                                          Hp   =            180
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9601041
56                 X    =         2986513
86
 Y    =      -10337026
61  feet           Y    =        -3117664
99  meter
 Z    =      -16953273
75                 Z    =        -5152995
40
 XDOT =      14348
838011                 XDOT =        4310
230897
 YDOT =      20328
852585  feet/sec       YDOT =        6244
787618  meter/sec
 ZDOT =      -4266
603108                 ZDOT =       -1279
367936

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13150028
44                 X    =         4008128
67
 Y    =        5288161
07  feet           Y    =         1611831
49  meter
 Z    =      -16898512
17                 Z    =        -5150666
51
 XDOT =     -13346
847672                 XDOT =       -4068
119170
 YDOT =      19807
888208  feet/sec       YDOT =        6037
444326  meter/sec
 ZDOT =      -4185
037885                 ZDOT =       -1275
599547


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   08090
30683041  
00020000  00000-0  20000-3 0  9089
2 25544  51
6395  63
0319 0001485 325
9525  34
1544 15
76556115 16080


Satellite: ISS
Catalog Number: 25544
Epoch time:      08090
30683041   =   yrday
fracday
Element set:     908
Inclination:       51
6395  deg
RA of node:        63
0319  deg
Eccentricity:     
0001485     
Arg of perigee:   325
9525  deg
Mean anomaly:      34
1544  deg
Mean motion:   15
76556115  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1608
Checksum:              281


Coasting Arc #10 (Orbit 1623)
---------------------------------------

Vector Time (GMT): 2008/091/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3788947
48                 A    =         6724692
29  meter
 Y    =       -5543580
23  meter          E    =           
0011320
 Z    =         256080
87                 I    =           51
93373
 XDOT =       3790
819706                 Wp   =          129
19426
 YDOT =      -2878
691397  meter/sec      RA   =           57
35954  deg
 ZDOT =      -6058
621864                 TA   =           48
03122
                                          MA   =           47
93483
                                          Ha   =            185
913  n
mi
                                          Hp   =            179
978

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12430930
04                 X    =        -3727920
68
 Y    =      -18187599
17  feet           Y    =        -5585609
18  meter
 Z    =         840160
33                 Z    =          237822
64
 XDOT =      12437
072527                 XDOT =        3852
159433
 YDOT =      -9444
525581  feet/sec       YDOT =       -2835
957450  meter/sec
 ZDOT =     -19877
368319                 ZDOT =       -6040
057130

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12124927
28                 X    =         3695677
83
 Y    =      -18396103
04  feet           Y    =        -5607132
21  meter
 Z    =         769536
50                 Z    =          234554
73
 XDOT =      12151
618367                 XDOT =        3703
813278
 YDOT =       7155
157174  feet/sec       YDOT =        2180
891906  meter/sec
 ZDOT =     -19806
454230                 ZDOT =       -6037
007249


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   08091
32099137  
00020000  00000-0  20000-3 0  9090
2 25544  51
6398  57
8034 0001539 335
8981  24
2112 15
76626290 16245


Satellite: ISS
Catalog Number: 25544
Epoch time:      08091
32099137   =   yrday
fracday
Element set:     909
Inclination:       51
6398  deg
RA of node:        57
8034  deg
Eccentricity:     
0001539     
Arg of perigee:   335
8981  deg
Mean anomaly:      24
2112  deg
Mean motion:   15
76626290  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1624
Checksum:              297


Coasting Arc #11 (Orbit 1639)
---------------------------------------

Vector Time (GMT): 2008/092/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3739901
81                 A    =         6712717
80  meter
 Y    =        1890575
82  meter          E    =           
0003627
 Z    =        5242402
33                 I    =           51
87601
 XDOT =      -4243
152977                 Wp   =           37
43551
 YDOT =      -6393
889543  meter/sec      RA   =           52
21905  deg
 ZDOT =       -718
124539                 TA   =           59
38453
                                          MA   =           59
34876
                                          Ha   =            186
029  n
mi
                                          Hp   =            179
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12270019
07                 X    =        -3786231
01
 Y    =        6202676
57  feet           Y    =         1848495
26  meter
 Z    =       17199482
71                 Z    =         5224121
43
 XDOT =     -13921
105568                 XDOT =       -4167
851658
 YDOT =     -20977
327897  feet/sec       YDOT =       -6440
917901  meter/sec
 ZDOT =      -2356
051636                 ZDOT =        -738
554457

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10578557
56                 X    =        -3224344
34
 Y    =       -8917474
26  feet           Y    =        -2718046
15  meter
 Z    =       17129551
75                 Z    =         5221087
37
 XDOT =      13139
180682                 XDOT =        4004
822272
 YDOT =     -20283
711165  feet/sec       YDOT =       -6182
475163  meter/sec
 ZDOT =      -2435
096524                 ZDOT =        -742
217421


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   08092
33513074  
00020000  00000-0  20000-3 0  9105
2 25544  51
6391  52
5750 0001484 339
9379  20
1727 15
76656470 16408


Satellite: ISS
Catalog Number: 25544
Epoch time:      08092
33513074   =   yrday
fracday
Element set:     910
Inclination:       51
6391  deg
RA of node:        52
5750  deg
Eccentricity:     
0001484     
Arg of perigee:   339
9379  deg
Mean anomaly:      20
1727  deg
Mean motion:   15
76656470  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1640
Checksum:              285


Coasting Arc #12 (Orbit 1655)
---------------------------------------

Vector Time (GMT): 2008/093/06:55:53
577
Vector Time (MET): N/A
Weight (LBS)     : 567227
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3522702
46                 A    =         6723654
77  meter
 Y    =        5518014
57  meter          E    =           
0014654
 Z    =        1498987
62                 I    =           51
89417
 XDOT =      -4833
662914                 Wp   =           55
70648
 YDOT =       1497
531762  meter/sec      RA   =           47
10084  deg
 ZDOT =       5814
746287                 TA   =          320
77166
                                          MA   =          320
87777
                                          Ha   =            186
018  n
mi
                                          Hp   =            179
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11557422
76                 X    =         3453455
59
 Y    =       18103722
35  feet           Y    =         5557020
35  meter
 Z    =        4917938
39                 Z    =         1515932
26
 XDOT =     -15858
474128                 XDOT =       -4878
296078
 YDOT =       4913
161948  feet/sec       YDOT =        1443
229766  meter/sec
 ZDOT =      19077
251599                 ZDOT =        5791
156029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11780227
96                 X    =        -3590613
48
 Y    =       17941450
57  feet           Y    =         5468554
13  meter
 Z    =        4983521
07                 Z    =         1518977
22
 XDOT =      -9722
573534                 XDOT =       -2963
440413
 YDOT =     -11686
436683  feet/sec       YDOT =       -3562
025901  meter/sec
 ZDOT =      18986
911097                 ZDOT =        5787
210502


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   08093
34924992  
00020000  00000-0  20000-3 0  9113
2 25544  51
6393  47
3459 0001624 349
4493  10
6637 15
76648743 16562


Satellite: ISS
Catalog Number: 25544
Epoch time:      08093
34924992   =   yrday
fracday
Element set:     911
Inclination:       51
6393  deg
RA of node:        47
3459  deg
Eccentricity:     
0001624     
Arg of perigee:   349
4493  deg
Mean anomaly:      10
6637  deg
Mean motion:   15
76648743  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1656
Checksum:              317

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 may contain past, current and future orbital data 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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