Date: February 14th 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 12852 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 877)
---------------------------------------

Vector Time (GMT): 2008/043/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4550094
14                 A    =         6718557
89  meter
 Y    =       -4542887
06  meter          E    =           
0018850
 Z    =        1914014
87                 I    =           51
37710
 XDOT =       2361
607208                 Wp   =           59
27180
 YDOT =       4741
245212  meter/sec      RA   =          301
28679  deg
 ZDOT =       5607
917248                 TA   =          322
14727
                                          MA   =          322
27967
                                          Ha   =            185
094  n
mi
                                          Hp   =            175
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14928130
37                 X    =         4591257
38
 Y    =      -14904485
10  feet           Y    =        -4491775
15  meter
 Z    =        6279576
33                 Z    =         1936219
02
 XDOT =       7748
055144                 XDOT =        2281
172360
 YDOT =      15555
266445  feet/sec       YDOT =        4767
204336  meter/sec
 ZDOT =      18398
678635                 ZDOT =        5619
194436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21065433
97                 X    =        -6420744
27
 Y    =        -415167
89  feet           Y    =         -126543
17  meter
 Z    =        6364036
35                 Z    =         1939758
28
 XDOT =       5892
853059                 XDOT =        1796
141612
 YDOT =     -14752
156178  feet/sec       YDOT =       -4496
457203  meter/sec
 ZDOT =      18442
310242                 ZDOT =        5621
216162


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   08044
03785776  
00020000  00000-0  20000-3 0  9008
2 25544  51
6400 301
5720 0005238  37
1976 322
9551 15
78221715  8786


Satellite: ISS
Catalog Number: 25544
Epoch time:      08044
03785776   =   yrday
fracday
Element set:     900
Inclination:       51
6400  deg
RA of node:       301
5720  deg
Eccentricity:     
0005238     
Arg of perigee:    37
1976  deg
Mean anomaly:     322
9551  deg
Mean motion:   15
78221715  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             878
Checksum:              286


Coasting Arc #2 (Orbit 892)
---------------------------------------

Vector Time (GMT): 2008/044/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1236273
59                 A    =         6712285
84  meter
 Y    =       -5103013
00  meter          E    =           
0011169
 Z    =       -4190382
29                 I    =           51
34182
 XDOT =       5302
202525                 Wp   =           84
02889
 YDOT =      -4250
074285  meter/sec      RA   =          296
05587  deg
 ZDOT =       3620
817679                 TA   =          222
95499
                                          MA   =          223
04225
                                          Ha   =            185
062  n
mi
                                          Hp   =            175
774

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4056015
72                 X    =        -1158763
12
 Y    =      -16742168
63  feet           Y    =        -5116404
23  meter
 Z    =      -13747973
39                 Z    =        -4196199
89
 XDOT =      17395
677577                 XDOT =        5331
744339
 YDOT =     -13943
813270  feet/sec       YDOT =       -4190
616945  meter/sec
 ZDOT =      11879
323094                 ZDOT =        3646
647178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9068219
19                 X    =        -2763993
21
 Y    =       14625040
82  feet           Y    =         4457712
44  meter
 Z    =      -13770759
89                 Z    =        -4197327
61
 XDOT =     -21039
044326                 XDOT =       -6412
700710
 YDOT =      -1796
161627  feet/sec       YDOT =        -547
470064  meter/sec
 ZDOT =      11977
684331                 ZDOT =        3650
798184


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   08044
98763764  
00020000  00000-0  20000-3 0  9016
2 25544  51
6393 296
6642 0005237  40
7920 319
3636 15
78295316  8931


Satellite: ISS
Catalog Number: 25544
Epoch time:      08044
98763764   =   yrday
fracday
Element set:     901
Inclination:       51
6393  deg
RA of node:       296
6642  deg
Eccentricity:     
0005237     
Arg of perigee:    40
7920  deg
Mean anomaly:     319
3636  deg
Mean motion:   15
78295316  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             893
Checksum:              319


Coasting Arc #3 (Orbit 908)
---------------------------------------

Vector Time (GMT): 2008/045/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4575913
47                 A    =         6712222
38  meter
 Y    =        2593561
77  meter          E    =           
0013113
 Z    =       -4183997
90                 I    =           51
32949
 XDOT =       -521
075894                 Wp   =           59
46343
 YDOT =      -6767
730248  meter/sec      RA   =          290
91606  deg
 ZDOT =      -3627
133290                 TA   =          173
41394
                                          MA   =          173
39668
                                          Ha   =            185
082  n
mi
                                          Hp   =            175
642

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15012839
45                 X    =        -4584250
15
 Y    =        8509060
93  feet           Y    =         2542344
88  meter
 Z    =      -13727027
22                 Z    =        -4206247
52
 XDOT =      -1709
566582                 XDOT =        -427
739644
 YDOT =     -22203
839395  feet/sec       YDOT =       -6773
035180  meter/sec
 ZDOT =     -11900
043601                 ZDOT =       -3629
438241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16640564
01                 X    =         5072043
91
 Y    =        4306340
70  feet           Y    =         1312572
65  meter
 Z    =      -13811871
77                 Z    =        -4209858
52
 XDOT =     -13982
889538                 XDOT =       -4261
984731
 YDOT =      15854
198473  feet/sec       YDOT =        4832
359694  meter/sec
 ZDOT =     -11909
568794                 ZDOT =       -3630
036568


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   08046
00070365  
00020000  00000-0  20000-3 0  9020
2 25544  51
6386 291
4279 0005188  43
6126 316
5449 15
78306230  9094


Satellite: ISS
Catalog Number: 25544
Epoch time:      08046
00070365   =   yrday
fracday
Element set:     902
Inclination:       51
6386  deg
RA of node:       291
4279  deg
Eccentricity:     
0005188     
Arg of perigee:    43
6126  deg
Mean anomaly:     316
5449  deg
Mean motion:   15
78306230  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             909
Checksum:              286


Coasting Arc #4 (Orbit 924)
---------------------------------------

Vector Time (GMT): 2008/046/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -241951
80                 A    =         6718152
32  meter
 Y    =        6438484
75  meter          E    =           
0016963
 Z    =        1884346
44                 I    =           51
34143
 XDOT =      -5075
750078                 Wp   =           96
13740
 YDOT =       1464
407572  meter/sec      RA   =          285
68242  deg
 ZDOT =      -5613
958067                 TA   =           62
79492
                                          MA   =           62
62214
                                          Ha   =            185
030  n
mi
                                          Hp   =            175
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -793805
11                 X    =         -323083
58
 Y    =       21123637
62  feet           Y    =         6435325
37  meter
 Z    =        6182238
97                 Z    =         1882974
35
 XDOT =     -16652
723352                 XDOT =       -5064
476991
 YDOT =       4804
486784  feet/sec       YDOT =        1407
710990  meter/sec
 ZDOT =     -18418
497594                 ZDOT =       -5638
588133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15063187
48                 X    =         4591259
55
 Y    =      -14832231
43  feet           Y    =        -4520864
14  meter
 Z    =        6177666
61                 Z    =         1882952
78
 XDOT =      14270
947125                 XDOT =        4349
784684
 YDOT =       6726
010724  feet/sec       YDOT =        2050
088069  meter/sec
 ZDOT =     -18512
572877                 ZDOT =       -5642
632213


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   08047
01373474  
00020000  00000-0  20000-3 0  9030
2 25544  51
6390 286
1917 0005353  46
0643 314
0963 15
78396273  9252


Satellite: ISS
Catalog Number: 25544
Epoch time:      08047
01373474   =   yrday
fracday
Element set:     903
Inclination:       51
6390  deg
RA of node:       286
1917  deg
Eccentricity:     
0005353     
Arg of perigee:    46
0643  deg
Mean anomaly:     314
0963  deg
Mean motion:   15
78396273  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             925
Checksum:              294


Coasting Arc #5 (Orbit 940)
---------------------------------------

Vector Time (GMT): 2008/047/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4212782
61                 A    =         6707537
62  meter
 Y    =         178778
14  meter          E    =           
0006895
 Z    =        5210715
23                 I    =           51
29922
 XDOT =       -981
649457                 Wp   =           70
27974
 YDOT =       7632
617924  meter/sec      RA   =          280
51273  deg
 ZDOT =        533
504293                 TA   =           14
64602
                                          MA   =           14
62605
                                          Ha   =            184
813  n
mi
                                          Hp   =            175
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13821465
24                 X    =         4185158
30
 Y    =         586542
44  feet           Y    =          225733
15  meter
 Z    =       17095522
41                 Z    =         5231113
33
 XDOT =      -3220
634701                 XDOT =       -1069
517212
 YDOT =      25041
397388  feet/sec       YDOT =        7621
149240  meter/sec
 ZDOT =       1750
342169                 ZDOT =         528
522525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9771388
88                 X    =        -2978319
33
 Y    =       -9655138
36  feet           Y    =        -2942886
17  meter
 Z    =       17173586
77                 Z    =         5234509
25
 XDOT =      18512
801802                 XDOT =        5642
701989
 YDOT =     -15664
873476  feet/sec       YDOT =       -4774
653435  meter/sec
 ZDOT =       1732
091897                 ZDOT =         527
941610


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   08048
02673167  
00020000  00000-0  20000-3 0  9045
2 25544  51
6387 280
9555 0005201  49
5709 310
5910 15
78447029  9418


Satellite: ISS
Catalog Number: 25544
Epoch time:      08048
02673167   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:       280
9555  deg
Eccentricity:     
0005201     
Arg of perigee:    49
5709  deg
Mean anomaly:     310
5910  deg
Mean motion:   15
78447029  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             941
Checksum:              295


Coasting Arc #6 (Orbit 956)
---------------------------------------

Vector Time (GMT): 2008/048/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1412796
12                 A    =         6719139
90  meter
 Y    =       -6481706
48  meter          E    =           
0019304
 Z    =        1006161
19                 I    =           51
33343
 XDOT =       4569
159662                 Wp   =           54
83030
 YDOT =       1923
759239  meter/sec      RA   =          275
32535  deg
 ZDOT =       5908
550209                 TA   =          316
24239
                                          MA   =          316
39522
                                          Ha   =            185
077  n
mi
                                          Hp   =            175
277

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4635157
88                 X    =         1480282
96
 Y    =      -21265441
19  feet           Y    =        -6465530
48  meter
 Z    =        3301053
78                 Z    =         1013188
05
 XDOT =      14990
681306                 XDOT =        4518
606489
 YDOT =       6311
546061  feet/sec       YDOT =        1974
571329  meter/sec
 ZDOT =      19385
007247                 ZDOT =        5930
623801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17486278
12                 X    =        -5329817
57
 Y    =       12952226
15  feet           Y    =         3947838
53  meter
 Z    =        3327243
48                 Z    =         1014143
81
 XDOT =      -6088
326798                 XDOT =       -1855
722008
 YDOT =     -13278
429211  feet/sec       YDOT =       -4047
265223  meter/sec
 ZDOT =      19469
677320                 ZDOT =        5934
357647


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   08049
03969783  
00020000  00000-0  20000-3 0  9050
2 25544  51
6379 275
7189 0005527  52
5084 307
6583 15
78438864  9572


Satellite: ISS
Catalog Number: 25544
Epoch time:      08049
03969783   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:       275
7189  deg
Eccentricity:     
0005527     
Arg of perigee:    52
5084  deg
Mean anomaly:     307
6583  deg
Mean motion:   15
78438864  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             957
Checksum:              344


Coasting Arc #7 (Orbit 971)
---------------------------------------

Vector Time (GMT): 2008/049/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3716280
33                 A    =         6709827
85  meter
 Y    =       -3122403
10  meter          E    =           
0014878
 Z    =       -4645722
59                 I    =           51
30136
 XDOT =       2246
446802                 Wp   =           92
25334
 YDOT =      -6813
189906  meter/sec      RA   =          270
10037  deg
 ZDOT =       2789
258100                 TA   =          205
37624
                                          MA   =          205
44938
                                          Ha   =            184
946  n
mi
                                          Hp   =            175
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12192520
76                 X    =        -3658521
59
 Y    =      -10244104
66  feet           Y    =        -3163637
68  meter
 Z    =      -15241872
01                 Z    =        -4663635
42
 XDOT =       7370
232291                 XDOT =        2308
916714
 YDOT =     -22352
985256  feet/sec       YDOT =       -6787
719592  meter/sec
 ZDOT =       9151
109251                 ZDOT =        2800
322664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2623739
01                 X    =          799715
65
 Y    =       15640028
69  feet           Y    =         4767080
74  meter
 Z    =      -15310760
97                 Z    =        -4666719
94
 XDOT =     -18885
432835                 XDOT =       -5756
279928
 YDOT =      12144
626730  feet/sec       YDOT =        3701
682227  meter/sec
 ZDOT =       9192
703714                 ZDOT =        2801
936092


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   08049
98931838  
00020000  00000-0  20000-3 0  9065
2 25544  51
6378 270
8092 0005441  55
8671 304
3010 15
78524853  9723


Satellite: ISS
Catalog Number: 25544
Epoch time:      08049
98931838   =   yrday
fracday
Element set:     906
Inclination:       51
6378  deg
RA of node:       270
8092  deg
Eccentricity:     
0005441     
Arg of perigee:    55
8671  deg
Mean anomaly:     304
3010  deg
Mean motion:   15
78524853  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             972
Checksum:              310


Coasting Arc #8 (Orbit 987)
---------------------------------------

Vector Time (GMT): 2008/050/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2510575
22                 A    =         6713196
02  meter
 Y    =        5033961
51  meter          E    =           
0011149
 Z    =       -3676196
19                 I    =           51
31486
 XDOT =      -3894
733513                 Wp   =           69
38948
 YDOT =      -5069
243196  meter/sec      RA   =          264
95384  deg
 ZDOT =      -4288
306631                 TA   =          155
10330
                                          MA   =          155
04947
                                          Ha   =            184
912  n
mi
                                          Hp   =            174
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8236795
33                 X    =        -2548821
45
 Y    =       16515621
76  feet           Y    =         5005672
91  meter
 Z    =      -12061011
11                 Z    =        -3688485
16
 XDOT =     -12777
997090                 XDOT =       -3816
927855
 YDOT =     -16631
375316  feet/sec       YDOT =       -5112
361382  meter/sec
 ZDOT =     -14069
247478                 ZDOT =       -4307
037535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16775427
40                 X    =         5113150
27
 Y    =       -7620534
48  feet           Y    =        -2322738
91  meter
 Z    =      -12107478
61                 Z    =        -3690359
48
 XDOT =      -1246
349446                 XDOT =        -379
887311
 YDOT =      19689
983378  feet/sec       YDOT =        6001
506933  meter/sec
 ZDOT =     -14141
493881                 ZDOT =       -4310
327335


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   08051
00221536  
00020000  00000-0  20000-3 0  9079
2 25544  51
6380 265
5716 0005480  60
0970 300
0739 15
78591843  9884


Satellite: ISS
Catalog Number: 25544
Epoch time:      08051
00221536   =   yrday
fracday
Element set:     907
Inclination:       51
6380  deg
RA of node:       265
5716  deg
Eccentricity:     
0005480     
Arg of perigee:    60
0970  deg
Mean anomaly:     300
0739  deg
Mean motion:   15
78591843  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             988
Checksum:              285


Coasting Arc #9 (Orbit 1003)
---------------------------------------

Vector Time (GMT): 2008/051/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3023322
10                 A    =         6716181
82  meter
 Y    =        5442406
52  meter          E    =           
0018316
 Z    =        2502258
58                 I    =           51
32843
 XDOT =      -3501
774224                 Wp   =           92
56830
 YDOT =       4389
926322  meter/sec      RA   =          259
71129  deg
 ZDOT =      -5284
706140                 TA   =           58
89928
                                          MA   =           58
71969
                                          Ha   =            184
807  n
mi
                                          Hp   =            174
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9919035
76                 X    =         2950084
42
 Y    =       17855664
45  feet           Y    =         5475805
66  meter
 Z    =        8209509
76                 Z    =         2516767
28
 XDOT =     -11488
760579                 XDOT =       -3524
931435
 YDOT =      14402
645415  feet/sec       YDOT =        4350
637759  meter/sec
 ZDOT =     -17338
274739                 ZDOT =       -5301
773693

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3307595
20                 X    =         1008155
02
 Y    =      -20133228
36  feet           Y    =        -6136608
00  meter
 Z    =        8265652
04                 Z    =         2519370
74
 XDOT =      16394
765583                 XDOT =        4997
124550
 YDOT =      -4494
724920  feet/sec       YDOT =       -1369
992156  meter/sec
 ZDOT =     -17403
095296                 ZDOT =       -5304
463446


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   08052
01507666  
00020000  00000-0  20000-3 0  9083
2 25544  51
6369 260
3338 0005491  62
2370 297
9352 15
78659185 10043


Satellite: ISS
Catalog Number: 25544
Epoch time:      08052
01507666   =   yrday
fracday
Element set:     908
Inclination:       51
6369  deg
RA of node:       260
3338  deg
Eccentricity:     
0005491     
Arg of perigee:    62
2370  deg
Mean anomaly:     297
9352  deg
Mean motion:   15
78659185  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1004
Checksum:              298


Coasting Arc #10 (Orbit 1019)
---------------------------------------

Vector Time (GMT): 2008/052/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3595876
66                 A    =         6707225
42  meter
 Y    =       -2394627
40  meter          E    =           
0008410
 Z    =        5123320
50                 I    =           51
30461
 XDOT =       2949
169170                 Wp   =           90
71342
 YDOT =       7025
641490  meter/sec      RA   =          254
54911  deg
 ZDOT =       1212
038788                 TA   =          347
66449
                                          MA   =          347
68507
                                          Ha   =            184
704  n
mi
                                          Hp   =            174
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11797495
60                 X    =         3597498
99
 Y    =       -7856389
12  feet           Y    =        -2354406
85  meter
 Z    =       16808794
29                 Z    =         5140792
91
 XDOT =       9675
751869                 XDOT =        2864
500464
 YDOT =      23050
004889  feet/sec       YDOT =        7058
147456  meter/sec
 ZDOT =       3976
505211                 ZDOT =        1226
159349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14069810
17                 X    =        -4288478
14
 Y    =        -837277
46  feet           Y    =         -255202
17  meter
 Z    =       16875388
18                 Z    =         5143618
32
 XDOT =       6220
623823                 XDOT =        1896
046141
 YDOT =     -23161
286473  feet/sec       YDOT =       -7059
560117  meter/sec
 ZDOT =       4031
354007                 ZDOT =        1228
756701


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   08053
02790391  
00020000  00000-0  20000-3 0  9095
2 25544  51
6364 255
0957 0005541  66
2033 293
9713 15
78701173 10202


Satellite: ISS
Catalog Number: 25544
Epoch time:      08053
02790391   =   yrday
fracday
Element set:     909
Inclination:       51
6364  deg
RA of node:       255
0957  deg
Eccentricity:     
0005541     
Arg of perigee:    66
2033  deg
Mean anomaly:     293
9713  deg
Mean motion:   15
78701173  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1020
Checksum:              279


Coasting Arc #11 (Orbit 1035)
---------------------------------------

Vector Time (GMT): 2008/053/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1979254
60                 A    =         6718620
38  meter
 Y    =       -6392325
53  meter          E    =           
0018496
 Z    =         503047
12                 I    =           51
35314
 XDOT =       4750
068667                 Wp   =           55
47153
 YDOT =       -987
593318  meter/sec      RA   =          249
34969  deg
 ZDOT =       5994
233717                 TA   =          310
03631
                                          MA   =          310
19844
                                          Ha   =            184
744  n
mi
                                          Hp   =            174
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6493617
46                 X    =        -1910071
19
 Y    =      -20972196
62  feet           Y    =        -6414071
82  meter
 Z    =        1650417
08                 Z    =          493600
65
 XDOT =      15584
214786                 XDOT =        4731
640771
 YDOT =      -3240
135558  feet/sec       YDOT =        -934
577913  meter/sec
 ZDOT =      19666
121119                 ZDOT =        6017
264370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7173659
94                 X    =        -2186531
55
 Y    =       20752328
28  feet           Y    =         6325309
66  meter
 Z    =        1613520
86                 Z    =          491801
16
 XDOT =     -12875
065292                 XDOT =       -3924
319901
 YDOT =      -6024
525888  feet/sec       YDOT =       -1836
275491  meter/sec
 ZDOT =      19754
149106                 ZDOT =        6021
064648


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   08054
04069598  
00020000  00000-0  20000-3 0  9108
2 25544  51
6370 249
8577 0005523  68
0609 292
1143 15
78743215 10365


Satellite: ISS
Catalog Number: 25544
Epoch time:      08054
04069598   =   yrday
fracday
Element set:     910
Inclination:       51
6370  deg
RA of node:       249
8577  deg
Eccentricity:     
0005523     
Arg of perigee:    68
0609  deg
Mean anomaly:     292
1143  deg
Mean motion:   15
78743215  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1036
Checksum:              295


Coasting Arc #12 (Orbit 1050)
---------------------------------------

Vector Time (GMT): 2008/054/23:28:48
314
Vector Time (MET): N/A
Weight (LBS)     : 540617
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4624247
51                 A    =         6708333
61  meter
 Y    =        -683798
07  meter          E    =           
0016858
 Z    =       -4826571
30                 I    =           51
33081
 XDOT =      -1391
235353                 Wp   =           96
20525
 YDOT =      -7192
738339  meter/sec      RA   =          244
13175  deg
 ZDOT =       2357
186036                 TA   =          196
86399
                                          MA   =          196
92010
                                          Ha   =            184
658  n
mi
                                          Hp   =            174
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15171415
71                 X    =        -4592811
26
 Y    =       -2243431
98  feet           Y    =         -735333
65  meter
 Z    =      -15835207
69                 Z    =        -4848959
11
 XDOT =      -4564
420450                 XDOT =       -1322
152238
 YDOT =     -23598
222898  feet/sec       YDOT =       -7207
909480  meter/sec
 ZDOT =       7733
549987                 ZDOT =        2350
595886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11010152
70                 X    =         3355894
54
 Y    =       10547883
00  feet           Y    =         3214994
74  meter
 Z    =      -15920971
89                 Z    =        -4852712
23
 XDOT =      -9110
460789                 XDOT =       -2776
868448
 YDOT =      21117
563421  feet/sec       YDOT =        6436
633331  meter/sec
 ZDOT =       7707
485870                 ZDOT =        2349
241693


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   08054
99015494  
00020000  00000-0  20000-3 0  9119
2 25544  51
6374 244
9465 0005409  70
5383 289
6367 15
78781023 10516


Satellite: ISS
Catalog Number: 25544
Epoch time:      08054
99015494   =   yrday
fracday
Element set:     911
Inclination:       51
6374  deg
RA of node:       244
9465  deg
Eccentricity:     
0005409     
Arg of perigee:    70
5383  deg
Mean anomaly:     289
6367  deg
Mean motion:   15
78781023  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1051
Checksum:              307

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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