Date: March 31st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 1578)
---------------------------------------

Vector Time (GMT): 2008/088/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4445463
93                 A    =         6716293
53  meter
 Y    =        2339990
51  meter          E    =           
0008652
 Z    =       -4466089
44                 I    =           51
93875
 XDOT =       -400
573698                 Wp   =          106
46990
 YDOT =       6964
646822  meter/sec      RA   =           71
87590  deg
 ZDOT =       3253
138112                 TA   =          195
98066
                                          MA   =          196
00797
                                          Ha   =            185
972  n
mi
                                          Hp   =            180
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14584855
43                 X    =         4440662
89
 Y    =        7677134
20  feet           Y    =         2389675
34  meter
 Z    =      -14652524
42                 Z    =        -4444505
03
 XDOT =      -1314
218170                 XDOT =        -494
226872
 YDOT =      22849
891147  feet/sec       YDOT =        6959
643761  meter/sec
 ZDOT =      10673
025303                 ZDOT =        3250
964584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13197135
49                 X    =         4022486
90
 Y    =        9995930
50  feet           Y    =         3046759
62  meter
 Z    =      -14569483
77                 Z    =        -4440778
65
 XDOT =      -4403
693967                 XDOT =       -1342
245921
 YDOT =      21346
011565  feet/sec       YDOT =        6506
264325  meter/sec
 ZDOT =      10665
433970                 ZDOT =        3250
824274


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
46845422  
00020000  00000-0  20000-3 0  9008
2 25544  51
6383  72
5135 0001120 323
7478  36
3611 15
76565376 15792


Satellite: ISS
Catalog Number: 25544
Epoch time:      08088
46845422   =   yrday
fracday
Element set:     900
Inclination:       51
6383  deg
RA of node:        72
5135  deg
Eccentricity:     
0001120     
Arg of perigee:   323
7478  deg
Mean anomaly:      36
3611  deg
Mean motion:   15
76565376  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1579
Checksum:              292


Coasting Arc #2 (Orbit 1594)
---------------------------------------

Vector Time (GMT): 2008/089/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         591244
48                 A    =         6719262
47  meter
 Y    =       -5676911
02  meter          E    =           
0004970
 Z    =       -3551151
20                 I    =           51
93824
 XDOT =       5270
456177                 Wp   =           71
61660
 YDOT =       3358
901985  meter/sec      RA   =           66
79051  deg
 ZDOT =      -4495
647016                 TA   =          150
52425
                                          MA   =          150
49622
                                          Ha   =            185
918  n
mi
                                          Hp   =            179
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1939778
46                 X    =          671931
46
 Y    =      -18625036
14  feet           Y    =        -5669848
26  meter
 Z    =      -11650758
54                 Z    =        -3548082
92
 XDOT =      17291
522891                 XDOT =        5254
343708
 YDOT =      11020
019637  feet/sec       YDOT =        3417
749118  meter/sec
 ZDOT =     -14749
498083                 ZDOT =       -4470
082339

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4745714
92                 X    =         1446493
91
 Y    =      -18121616
63  feet           Y    =        -5523468
75  meter
 Z    =      -11639591
36                 Z    =        -3547747
45
 XDOT =      14227
188728                 XDOT =        4336
447124
 YDOT =      13128
765895  feet/sec       YDOT =        4001
647845  meter/sec
 ZDOT =     -14651
079716                 ZDOT =       -4465
649097


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
48260520  
00020000  00000-0  20000-3 0  9012
2 25544  51
6375  67
2843 0001060 328
6837  31
4259 15
76613813 15958


Satellite: ISS
Catalog Number: 25544
Epoch time:      08089
48260520   =   yrday
fracday
Element set:     901
Inclination:       51
6375  deg
RA of node:        67
2843  deg
Eccentricity:     
0001060     
Arg of perigee:   328
6837  deg
Mean anomaly:      31
4259  deg
Mean motion:   15
76613813  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1595
Checksum:              292


Coasting Arc #3 (Orbit 1610)
---------------------------------------

Vector Time (GMT): 2008/090/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4760577
02                 A    =         6719996
11  meter
 Y    =       -3434457
87  meter          E    =           
0012230
 Z    =        3261235
63                 I    =           51
92832
 XDOT =       1023
958744                 Wp   =           87
33719
 YDOT =      -5965
217010  meter/sec      RA   =           61
60444  deg
 ZDOT =      -4771
538497                 TA   =           54
57273
                                          MA   =           54
45860
                                          Ha   =            185
866  n
mi
                                          Hp   =            179
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15618691
01                 X    =        -4737660
98
 Y    =      -11267906
39  feet           Y    =        -3487565
19  meter
 Z    =       10699591
95                 Z    =         3238164
55
 XDOT =       3359
444698                 XDOT =        1113
765790
 YDOT =     -19570
921950  feet/sec       YDOT =       -5953
264439  meter/sec
 ZDOT =     -15654
653860                 ZDOT =       -4766
345916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14064465
73                 X    =        -4286849
16
 Y    =      -13228519
50  feet           Y    =        -4032052
74  meter
 Z    =       10610728
84                 Z    =         3234150
15
 XDOT =       5022
714809                 XDOT =        1530
923474
 YDOT =     -17923
335100  feet/sec       YDOT =       -5463
032539  meter/sec
 ZDOT =     -15635
364047                 ZDOT =       -4765
658962


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
49673095  
00020000  00000-0  20000-3 0  9021
2 25544  51
6374  62
0556 0001264 330
1683  29
9409 15
76681516 16117


Satellite: ISS
Catalog Number: 25544
Epoch time:      08090
49673095   =   yrday
fracday
Element set:     902
Inclination:       51
6374  deg
RA of node:        62
0556  deg
Eccentricity:     
0001264     
Arg of perigee:   330
1683  deg
Mean anomaly:      29
9409  deg
Mean motion:   15
76681516  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1611
Checksum:              290


Coasting Arc #4 (Orbit 1626)
---------------------------------------

Vector Time (GMT): 2008/091/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1280674
46                 A    =         6715056
97  meter
 Y    =        4670025
68  meter          E    =           
0007076
 Z    =        4647697
21                 I    =           51
89696
 XDOT =      -5625
892717                 Wp   =          110
93227
 YDOT =      -4413
401320  meter/sec      RA   =           56
51506  deg
 ZDOT =       2878
419539                 TA   =          310
70648
                                          MA   =          310
76793
                                          Ha   =            185
801  n
mi
                                          Hp   =            179
830

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4201687
87                 X    =        -1355377
75
 Y    =       15321606
57  feet           Y    =         4655286
87  meter
 Z    =       15248350
44                 Z    =         4641294
18
 XDOT =     -18457
653272                 XDOT =       -5590
105993
 YDOT =     -14479
663122  feet/sec       YDOT =       -4476
113102  meter/sec
 ZDOT =       9443
633659                 ZDOT =        2851
176178

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6009722
96                 X    =        -1831763
56
 Y    =       14731686
26  feet           Y    =         4490217
97  meter
 Z    =       15224278
30                 Z    =         4640360
03
 XDOT =     -15662
195400                 XDOT =       -4773
837158
 YDOT =     -16060
509356  feet/sec       YDOT =       -4895
243252  meter/sec
 ZDOT =       9338
660171                 ZDOT =        2846
423620


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
51083303  
00020000  00000-0  20000-3 0  9033
2 25544  51
6373  56
8269 0001245 329
5344  30
5748 15
76714977 16272


Satellite: ISS
Catalog Number: 25544
Epoch time:      08091
51083303   =   yrday
fracday
Element set:     903
Inclination:       51
6373  deg
RA of node:        56
8269  deg
Eccentricity:     
0001245     
Arg of perigee:   329
5344  deg
Mean anomaly:      30
5748  deg
Mean motion:   15
76714977  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1627
Checksum:              297


Coasting Arc #5 (Orbit 1641)
---------------------------------------

Vector Time (GMT): 2008/092/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5004823
14                 A    =         6723209
27  meter
 Y    =        4161235
12  meter          E    =           
0008601
 Z    =       -1669336
18                 I    =           51
90725
 XDOT =      -2006
177520                 Wp   =           30
90167
 YDOT =       4713
266807  meter/sec      RA   =           51
34000  deg
 ZDOT =       5754
495308                 TA   =          310
69726
                                          MA   =          310
77195
                                          Ha   =            185
845  n
mi
                                          Hp   =            179
709

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16420023
44                 X    =         4966028
87
 Y    =       13652346
19  feet           Y    =         4216984
93  meter
 Z    =       -5476824
75                 Z    =        -1645117
36
 XDOT =      -6581
947245                 XDOT =       -2086
686975
 YDOT =      15463
473775  feet/sec       YDOT =        4690
382673  meter/sec
 ZDOT =      18879
577782                 ZDOT =        5744
553623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15047706
14                 X    =         4586540
83
 Y    =       15184993
54  feet           Y    =         4628386
03  meter
 Z    =       -5383479
06                 Z    =        -1640884
42
 XDOT =      -7051
395213                 XDOT =       -2149
265261
 YDOT =      13643
687773  feet/sec       YDOT =        4158
596033  meter/sec
 ZDOT =      18841
934039                 ZDOT =        5743
021495


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
46153154  
00020000  00000-0  20000-3 0  9041
2 25544  51
6371  51
9246 0001139 341
8745  18
2378 15
76740497 16420


Satellite: ISS
Catalog Number: 25544
Epoch time:      08092
46153154   =   yrday
fracday
Element set:     904
Inclination:       51
6371  deg
RA of node:        51
9246  deg
Eccentricity:     
0001139     
Arg of perigee:   341
8745  deg
Mean anomaly:      18
2378  deg
Mean motion:   15
76740497  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1642
Checksum:              293


Coasting Arc #6 (Orbit 1657)
---------------------------------------

Vector Time (GMT): 2008/093/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2306400
14                 A    =         6712459
48  meter
 Y    =       -3533554
90  meter          E    =           
0014490
 Z    =       -5232788
40                 I    =           51
85263
 XDOT =       5757
338456                 Wp   =           78
51038
 YDOT =       5032
344926  meter/sec      RA   =           46
22242  deg
 ZDOT =       -859
770691                 TA   =          183
31672
                                          MA   =          183
32634
                                          Ha   =            185
753  n
mi
                                          Hp   =            179
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7566929
61                 X    =         2371161
25
 Y    =      -11593027
88  feet           Y    =        -3507401
64  meter
 Z    =      -17167940
95                 Z    =        -5221426
47
 XDOT =      18888
905694                 XDOT =        5704
814675
 YDOT =      16510
317998  feet/sec       YDOT =        5096
433046  meter/sec
 ZDOT =      -2820
769984                 ZDOT =        -831
929636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8566616
45                 X    =         2611104
69
 Y    =      -10943116
34  feet           Y    =        -3335461
86  meter
 Z    =      -17124724
91                 Z    =        -5219616
15
 XDOT =      16726
109167                 XDOT =        5098
118074
 YDOT =      17344
216051  feet/sec       YDOT =        5286
517052  meter/sec
 ZDOT =      -2713
437304                 ZDOT =        -827
055690


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
47558519  
00020000  00000-0  20000-3 0  9058
2 25544  51
6378  46
6946 0001242 340
7012  19
4105 15
76765490 16583


Satellite: ISS
Catalog Number: 25544
Epoch time:      08093
47558519   =   yrday
fracday
Element set:     905
Inclination:       51
6378  deg
RA of node:        46
6946  deg
Eccentricity:     
0001242     
Arg of perigee:   340
7012  deg
Mean anomaly:      19
4105  deg
Mean motion:   15
76765490  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1658
Checksum:              303


Coasting Arc #7 (Orbit 1673)
---------------------------------------

Vector Time (GMT): 2008/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4956426
30                 A    =         6724140
88  meter
 Y    =       -4532465
89  meter          E    =           
0010617
 Z    =        -203917
51                 I    =           51
87209
 XDOT =       3342
843574                 Wp   =          133
25494
 YDOT =      -3392
187411  meter/sec      RA   =           41
07625  deg
 ZDOT =      -6056
425810                 TA   =           48
95601
                                          MA   =           48
86429
                                          Ha   =            185
679  n
mi
                                          Hp   =            179
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16261241
13                 X    =        -4904384
60
 Y    =      -14870294
92  feet           Y    =        -4587600
52  meter
 Z    =        -669020
70                 Z    =         -227868
96
 XDOT =      10967
334561                 XDOT =        3409
948005
 YDOT =     -11129
223791  feet/sec       YDOT =       -3354
431114  meter/sec
 ZDOT =     -19870
163420                 ZDOT =       -6040
023071

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15291358
61                 X    =        -4660806
10
 Y    =      -15861774
17  feet           Y    =        -4834668
77  meter
 Z    =        -761377
15                 Z    =         -232067
76
 XDOT =      10600
284895                 XDOT =        3230
966836
 YDOT =      -9296
414392  feet/sec       YDOT =       -2833
547107  meter/sec
 ZDOT =     -19807
595678                 ZDOT =       -6037
355163


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   08094
48961323  
00020000  00000-0  20000-3 0  9062
2 25544  51
6385  41
4651 0001335 343
0753  17
0367 15
76820365 16743


Satellite: ISS
Catalog Number: 25544
Epoch time:      08094
48961323   =   yrday
fracday
Element set:     906
Inclination:       51
6385  deg
RA of node:        41
4651  deg
Eccentricity:     
0001335     
Arg of perigee:   343
0753  deg
Mean anomaly:      17
0367  deg
Mean motion:   15
76820365  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1674
Checksum:              287


Coasting Arc #8 (Orbit 1689)
---------------------------------------

Vector Time (GMT): 2008/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3560065
59                 A    =         6712587
29  meter
 Y    =        2421344
48  meter          E    =           
0004970
 Z    =        5147944
07                 I    =           51
81095
 XDOT =      -5484
431606                 Wp   =           39
84047
 YDOT =      -5252
907873  meter/sec      RA   =           35
92060  deg
 ZDOT =      -1317
611180                 TA   =           62
74696
                                          MA   =           62
69635
                                          Ha   =            185
767  n
mi
                                          Hp   =            179
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11680005
21                 X    =        -3611884
67
 Y    =        7944043
58  feet           Y    =         2381244
53  meter
 Z    =       16889580
29                 Z    =         5130523
16
 XDOT =     -17993
542015                 XDOT =       -5418
884429
 YDOT =     -17233
949713  feet/sec       YDOT =       -5313
871550  meter/sec
 ZDOT =      -4322
871325                 ZDOT =       -1344
094889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12125830
80                 X    =        -3695953
23
 Y    =        7398577
84  feet           Y    =         2255086
52  meter
 Z    =       16823006
44                 Z    =         5127652
36
 XDOT =     -16624
352180                 XDOT =       -5067
102545
 YDOT =     -17151
424121  feet/sec       YDOT =       -5227
754072  meter/sec
 ZDOT =      -4425
011723                 ZDOT =       -1348
743573


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   08095
50361630  
00020000  00000-0  20000-3 0  9072
2 25544  51
6390  36
2361 0001319 345
0527  15
0598 15
76850563 16907


Satellite: ISS
Catalog Number: 25544
Epoch time:      08095
50361630   =   yrday
fracday
Element set:     907
Inclination:       51
6390  deg
RA of node:        36
2361  deg
Eccentricity:     
0001319     
Arg of perigee:   345
0527  deg
Mean anomaly:      15
0598  deg
Mean motion:   15
76850563  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1690
Checksum:              281


Coasting Arc #9 (Orbit 1705)
---------------------------------------

Vector Time (GMT): 2008/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4476088
62                 A    =         6722015
52  meter
 Y    =        4559485
33  meter          E    =           
0014286
 Z    =        2064974
29                 I    =           51
81949
 XDOT =      -4841
019526                 Wp   =           64
27517
 YDOT =       2217
158294  meter/sec      RA   =           30
80582  deg
 ZDOT =       5574
419673                 TA   =          318
75535
                                          MA   =          318
86319
                                          Ha   =            185
556  n
mi
                                          Hp   =            179
395

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14685330
13                 X    =         4414739
72
 Y    =       14958941
36  feet           Y    =         4609196
67  meter
 Z    =        6774850
03                 Z    =         2086569
88
 XDOT =     -15882
609994                 XDOT =       -4892
532081
 YDOT =       7274
141384  feet/sec       YDOT =        2162
735720  meter/sec
 ZDOT =      18288
778454                 ZDOT =        5550
776494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14215492
23                 X    =         4332882
03
 Y    =       15369218
06  feet           Y    =         4684537
67  meter
 Z    =        6858159
90                 Z    =         2090367
14
 XDOT =     -15065
768623                 XDOT =       -4592
046276
 YDOT =       5780
135659  feet/sec       YDOT =        1761
785349  meter/sec
 ZDOT =      18198
316732                 ZDOT =        5546
846940


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   08096
51759262  
00020000  00000-0  20000-3 0  9087
2 25544  51
6396  31
0065 0001268 345
4640  14
6488 15
76908727 17067


Satellite: ISS
Catalog Number: 25544
Epoch time:      08096
51759262   =   yrday
fracday
Element set:     908
Inclination:       51
6396  deg
RA of node:        31
0065  deg
Eccentricity:     
0001268     
Arg of perigee:   345
4640  deg
Mean anomaly:      14
6488  deg
Mean motion:   15
76908727  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1706
Checksum:              306


Coasting Arc #10 (Orbit 1720)
---------------------------------------

Vector Time (GMT): 2008/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4864289
00                 A    =         6715572
09  meter
 Y    =       -1501009
81  meter          E    =           
0008423
 Z    =       -4388097
50                 I    =           51
77241
 XDOT =       4622
446836                 Wp   =          102
52996
 YDOT =       5155
224034  meter/sec      RA   =           25
61633  deg
 ZDOT =       3364
256678                 TA   =          201
25412
                                          MA   =          201
28914
                                          Ha   =            185
587  n
mi
                                          Hp   =            179
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15958953
42                 X    =         4902028
88
 Y    =       -4924572
87  feet           Y    =        -1446403
85  meter
 Z    =      -14396645
33                 Z    =        -4364374
68
 XDOT =      15165
507992                 XDOT =        4548
113589
 YDOT =      16913
464677  feet/sec       YDOT =        5206
499497  meter/sec
 ZDOT =      11037
587525                 ZDOT =        3386
531906

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16094719
05                 X    =         4905670
37
 Y    =       -4744149
36  feet           Y    =        -1446016
73  meter
 Z    =      -14305805
62                 Z    =        -4360409
55
 XDOT =      14565
804572                 XDOT =        4439
657234
 YDOT =      15908
285342  feet/sec       YDOT =        4848
845372  meter/sec
 ZDOT =      11123
556505                 ZDOT =        3390
460023


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   08097
46817332  
00020000  00000-0  20000-3 0  9096
2 25544  51
6400  26
1039 0001374 347
3511  12
7619 15
76926545 17215


Satellite: ISS
Catalog Number: 25544
Epoch time:      08097
46817332   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:        26
1039  deg
Eccentricity:     
0001374     
Arg of perigee:   347
3511  deg
Mean anomaly:      12
7619  deg
Mean motion:   15
76926545  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1721
Checksum:              283


Coasting Arc #11 (Orbit 1736)
---------------------------------------

Vector Time (GMT): 2008/098/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3444101
79                 A    =         6717609
95  meter
 Y    =       -4416629
15  meter          E    =           
0006263
 Z    =       -3716355
36                 I    =           51
75400
 XDOT =       6261
424818                 Wp   =           63
72839
 YDOT =      -1271
266583  meter/sec      RA   =           20
51760  deg
 ZDOT =      -4294
750085                 TA   =          161
02092
                                          MA   =          160
99757
                                          Ha   =            185
506  n
mi
                                          Hp   =            179
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11299546
56                 X    =        -3376404
69
 Y    =      -14490253
13  feet           Y    =        -4454764
71  meter
 Z    =      -12192766
93                 Z    =        -3732922
47
 XDOT =      20542
732343                 XDOT =        6296
038428
 YDOT =      -4170
822122  feet/sec       YDOT =       -1201
054393  meter/sec
 ZDOT =     -14090
387419                 ZDOT =       -4264
247441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11316509
30                 X    =        -3449272
04
 Y    =      -14422872
96  feet           Y    =        -4396091
68  meter
 Z    =      -12256757
58                 Z    =        -3735859
71
 XDOT =      19545
389469                 XDOT =        5957
434710
 YDOT =      -3468
730556  feet/sec       YDOT =       -1057
269074  meter/sec
 ZDOT =     -13973
519351                 ZDOT =       -4259
128698


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   08098
48210073  
00020000  00000-0  20000-3 0  9100
2 25544  51
6408  20
8742 0001395 352
1752   7
9391 15
76985414 17379


Satellite: ISS
Catalog Number: 25544
Epoch time:      08098
48210073   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:        20
8742  deg
Eccentricity:     
0001395     
Arg of perigee:   352
1752  deg
Mean anomaly:       7
9391  deg
Mean motion:   15
76985414  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1737
Checksum:              291


Coasting Arc #12 (Orbit 1752)
---------------------------------------

Vector Time (GMT): 2008/099/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 590825
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5974417
58                 A    =         6719856
90  meter
 Y    =         786413
04  meter          E    =           
0013098
 Z    =        2962349
64                 I    =           51
73399
 XDOT =      -3141
311049                 Wp   =           91
36104
 YDOT =      -4951
431823  meter/sec      RA   =           15
31694  deg
 ZDOT =      -5002
286168                 TA   =           54
45172
                                          MA   =           54
32967
                                          Ha   =            185
532  n
mi
                                          Hp   =            179
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19601107
53                 X    =        -5997158
13
 Y    =        2580095
27  feet           Y    =          719476
56  meter
 Z    =        9718994
87                 Z    =         2933270
19
 XDOT =     -10306
138613                 XDOT =       -3061
409289
 YDOT =     -16244
855062  feet/sec       YDOT =       -4986
113040  meter/sec
 ZDOT =     -16411
700025                 ZDOT =       -5017
352791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19590908
49                 X    =        -5971308
91
 Y    =        3034920
23  feet           Y    =          925043
69  meter
 Z    =        9607535
23                 Z    =         2928376
74
 XDOT =     -10365
201423                 XDOT =       -3159
313394
 YDOT =     -14575
195154  feet/sec       YDOT =       -4442
519483  meter/sec
 ZDOT =     -16469
981622                 ZDOT =       -5020
050398


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   08099
49600256  
00020000  00000-0  20000-3 0  9119
2 25544  51
6411  15
6447 0001392 353
3156   6
7990 15
77020310 17531


Satellite: ISS
Catalog Number: 25544
Epoch time:      08099
49600256   =   yrday
fracday
Element set:     911
Inclination:       51
6411  deg
RA of node:        15
6447  deg
Eccentricity:     
0001392     
Arg of perigee:   353
3156  deg
Mean anomaly:       6
7990  deg
Mean motion:   15
77020310  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            1753
Checksum:              272

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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