Date: June 21st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11302 11 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 2889)
---------------------------------------

Vector Time (GMT): 2008/171/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -383823
34                 A    =         6718501
49  meter
 Y    =        4155376
16  meter          E    =           
0006405
 Z    =        5270827
92                 I    =           51
63847
 XDOT =      -7674
093384                 Wp   =          270
38447
 YDOT =       -594
099612  meter/sec      RA   =            3
89352  deg
 ZDOT =        -90
510149                 TA   =          180
47445
                                          MA   =          180
47506
                                          Ha   =            187
029  n
mi
                                          Hp   =            186
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1259262
93                 X    =         -455865
54
 Y    =       13633123
88  feet           Y    =         4150680
07  meter
 Z    =       17292742
52                 Z    =         5268789
23
 XDOT =     -25177
471732                 XDOT =       -7666
440032
 YDOT =      -1949
145708  feet/sec       YDOT =        -679
872905  meter/sec
 ZDOT =       -296
949307                 ZDOT =        -127
772340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13682642
06                 X    =         4170469
30
 Y    =         702662
92  feet           Y    =          214171
66  meter
 Z    =       17285205
38                 Z    =         5268530
60
 XDOT =       -688
706368                 XDOT =        -209
917701
 YDOT =      24242
113161  feet/sec       YDOT =        7388
996092  meter/sec
 ZDOT =       -440
473066                 ZDOT =        -134
256190


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   08171
56237797  
00020000  00000-0  20000-3 0  9002
2 25544  51
6371   4
1419 0008792 268
9936  91
0220 15
74564316 28908


Satellite: ISS
Catalog Number: 25544
Epoch time:      08171
56237797   =   yrday
fracday
Element set:     900
Inclination:       51
6371  deg
RA of node:         4
1419  deg
Eccentricity:     
0008792     
Arg of perigee:   268
9936  deg
Mean anomaly:      91
0220  deg
Mean motion:   15
74564316  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2890
Checksum:              302


Coasting Arc #2 (Orbit 2905)
---------------------------------------

Vector Time (GMT): 2008/172/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6716799
38                 A    =         6730364
77  meter
 Y    =          94634
90  meter          E    =           
0008966
 Z    =         303805
32                 I    =           51
64922
 XDOT =       -340
288026                 Wp   =            4
76959
 YDOT =       4779
848924  meter/sec      RA   =          358
75657  deg
 ZDOT =       6030
566461                 TA   =          358
53310
                                          MA   =          358
53573
                                          Ha   =            187
150  n
mi
                                          Hp   =            186
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22036743
38                 X    =         6713766
13
 Y    =         310481
95  feet           Y    =          169728
97  meter
 Z    =         996736
61                 Z    =          336427
98
 XDOT =      -1116
430532                 XDOT =        -423
006966
 YDOT =      15681
919043  feet/sec       YDOT =        4775
579858  meter/sec
 ZDOT =      19785
323034                 ZDOT =        6028
713432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1124735
54                 X    =         -342819
39
 Y    =      -22004163
51  feet           Y    =        -6706869
04  meter
 Z    =        1122363
44                 Z    =          342096
38
 XDOT =      14124
220261                 XDOT =        4305
062336
 YDOT =        287
467964  feet/sec       YDOT =          87
620235  meter/sec
 ZDOT =      19778
548727                 ZDOT =        6028
501652


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   08172
57781165  
00020000  00000-0  20000-3 0  9018
2 25544  51
6366 358
9208 0008861 272
8755  87
1394 15
74622096 29064


Satellite: ISS
Catalog Number: 25544
Epoch time:      08172
57781165   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       358
9208  deg
Eccentricity:     
0008861     
Arg of perigee:   272
8755  deg
Mean anomaly:      87
1394  deg
Mean motion:   15
74622096  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2906
Checksum:              324


Coasting Arc #3 (Orbit 2920)
---------------------------------------

Vector Time (GMT): 2008/173/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         216268
59                 A    =         6718367
12  meter
 Y    =       -4206112
66  meter          E    =           
0006123
 Z    =       -5239611
86                 I    =           51
57990
 XDOT =       7664
517556                 Wp   =           93
11381
 YDOT =       -369
502558  meter/sec      RA   =          353
60552  deg
 ZDOT =        613
264657                 TA   =          182
72065
                                          MA   =          182
72399
                                          Ha   =            187
331  n
mi
                                          Hp   =            186
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         709542
60                 X    =          288738
78
 Y    =      -13799582
21  feet           Y    =        -4203288
00  meter
 Z    =      -17190327
61                 Z    =        -5238386
02
 XDOT =      25146
054975                 XDOT =        7665
100649
 YDOT =      -1212
278733  feet/sec       YDOT =        -283
790392  meter/sec
 ZDOT =       2012
023153                 ZDOT =         650
499894

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13819332
22                 X    =        -4212132
46
 Y    =         330510
71  feet           Y    =          100739
67  meter
 Z    =      -17185927
47                 Z    =        -5238270
69
 XDOT =      -3251
889994                 XDOT =        -991
176070
 YDOT =     -23941
509869  feet/sec       YDOT =       -7297
372208  meter/sec
 ZDOT =       2155
381055                 ZDOT =         656
960145


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   08173
52976586  
00020000  00000-0  20000-3 0  9028
2 25544  51
6366 354
0269 0008716 276
2201  83
7969 15
74657540 29210


Satellite: ISS
Catalog Number: 25544
Epoch time:      08173
52976586   =   yrday
fracday
Element set:     902
Inclination:       51
6366  deg
RA of node:       354
0269  deg
Eccentricity:     
0008716     
Arg of perigee:   276
2201  deg
Mean anomaly:      83
7969  deg
Mean motion:   15
74657540  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2921
Checksum:              320


Coasting Arc #4 (Orbit 2936)
---------------------------------------

Vector Time (GMT): 2008/174/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6640925
69                 A    =         6729829
50  meter
 Y    =         725463
27  meter          E    =           
0006571
 Z    =        -777042
53                 I    =           51
59067
 XDOT =        167
913607                 Wp   =          198
36648
 YDOT =      -4863
707210  meter/sec      RA   =          348
47421  deg
 ZDOT =      -5968
402366                 TA   =          350
11244
                                          MA   =          350
12536
                                          Ha   =            187
567  n
mi
                                          Hp   =            186
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21787813
93                 X    =        -6644769
67
 Y    =        2380128
84  feet           Y    =          651179
28  meter
 Z    =       -2549352
14                 Z    =         -809313
04
 XDOT =        550
897660                 XDOT =         251
280987
 YDOT =     -15957
044653  feet/sec       YDOT =       -4861
362340  meter/sec
 ZDOT =     -19581
372593                 ZDOT =       -5967
384995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4532612
99                 X    =         1381540
44
 Y    =       21428497
53  feet           Y    =         6531406
05  meter
 Z    =       -2673566
64                 Z    =         -814903
11
 XDOT =     -14381
384733                 XDOT =       -4383
446066
 YDOT =        596
390707  feet/sec       YDOT =         181
779888  meter/sec
 ZDOT =     -19577
829098                 ZDOT =       -5967
322309


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   08174
54516565  
00020000  00000-0  20000-3 0  9039
2 25544  51
6370 348
8067 0008835 281
9229  78
0943 15
74724051 29375


Satellite: ISS
Catalog Number: 25544
Epoch time:      08174
54516565   =   yrday
fracday
Element set:     903
Inclination:       51
6370  deg
RA of node:       348
8067  deg
Eccentricity:     
0008835     
Arg of perigee:   281
9229  deg
Mean anomaly:      78
0943  deg
Mean motion:   15
74724051  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2937
Checksum:              316


Coasting Arc #5 (Orbit 2952)
---------------------------------------

Vector Time (GMT): 2008/175/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -78417
30                 A    =         6718705
83  meter
 Y    =        4306291
25  meter          E    =           
0006716
 Z    =        5161726
02                 I    =           51
52370
 XDOT =      -7500
290777                 Wp   =          310
90037
 YDOT =       1274
734170  meter/sec      RA   =          343
30909  deg
 ZDOT =      -1174
089298                 TA   =          150
35309
                                          MA   =          150
31500
                                          Ha   =            187
770  n
mi
                                          Hp   =            186
185

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -257274
59                 X    =         -151639
59
 Y    =       14128252
14  feet           Y    =         4305004
16  meter
 Z    =       16934796
65                 Z    =         5161167
87
 XDOT =     -24607
253207                 XDOT =       -7508
284161
 YDOT =       4182
198720  feet/sec       YDOT =        1190
817106  meter/sec
 ZDOT =      -3851
999008                 ZDOT =       -1210
544594

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14073351
26                 X    =         4289557
46
 Y    =       -1294573
60  feet           Y    =         -394586
03  meter
 Z    =       16932982
60                 Z    =         5161173
10
 XDOT =       6923
536558                 XDOT =        2110
293943
 YDOT =      22903
982464  feet/sec       YDOT =        6981
133855  meter/sec
 ZDOT =      -3992
286145                 ZDOT =       -1216
848817


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   08175
56055174  
00020000  00000-0  20000-3 0  9047
2 25544  51
6367 343
5859 0008650 284
3491  75
6712 15
74663163 29536


Satellite: ISS
Catalog Number: 25544
Epoch time:      08175
56055174   =   yrday
fracday
Element set:     904
Inclination:       51
6367  deg
RA of node:       343
5859  deg
Eccentricity:     
0008650     
Arg of perigee:   284
3491  deg
Mean anomaly:      75
6712  deg
Mean motion:   15
74663163  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2953
Checksum:              315


Coasting Arc #6 (Orbit 2968)
---------------------------------------

Vector Time (GMT): 2008/176/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6431422
96                 A    =         6729300
53  meter
 Y    =       -1480390
04  meter          E    =           
0010418
 Z    =        1278681
68                 I    =           51
53361
 XDOT =        -10
696340                 Wp   =           20
53990
 YDOT =       5011
747062  meter/sec      RA   =          338
18258  deg
 ZDOT =       5851
378322                 TA   =          353
52011
                                          MA   =          353
53357
                                          Ha   =            187
757  n
mi
                                          Hp   =            185
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21100469
03                 X    =         6441287
36
 Y    =       -4856922
70  feet           Y    =        -1408415
20  meter
 Z    =        4195149
86                 Z    =         1309949
09
 XDOT =        -35
092980                 XDOT =         -95
162436
 YDOT =      16442
739705  feet/sec       YDOT =        5011
154392  meter/sec
 ZDOT =      19197
435438                 ZDOT =        5851
121863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7628550
02                 X    =        -2325182
05
 Y    =      -20238600
97  feet           Y    =        -6168725
58  meter
 Z    =        4315440
76                 Z    =         1315346
34
 XDOT =      14838
982724                 XDOT =        4522
921934
 YDOT =      -1496
724548  feet/sec       YDOT =        -456
201642  meter/sec
 ZDOT =      19196
842275                 ZDOT =        5851
197526


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   08176
57591611  
00020000  00000-0  20000-3 0  9051
2 25544  51
6376 338
3654 0008730 287
8330  72
1881 15
74749612 29690


Satellite: ISS
Catalog Number: 25544
Epoch time:      08176
57591611   =   yrday
fracday
Element set:     905
Inclination:       51
6376  deg
RA of node:       338
3654  deg
Eccentricity:     
0008730     
Arg of perigee:   287
8330  deg
Mean anomaly:      72
1881  deg
Mean motion:   15
74749612  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2969
Checksum:              323


Coasting Arc #7 (Orbit 2983)
---------------------------------------

Vector Time (GMT): 2008/177/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -69516
65                 A    =         6718988
24  meter
 Y    =       -4459071
34  meter          E    =           
0004950
 Z    =       -5029807
73                 I    =           51
47270
 XDOT =       7196
480117                 Wp   =           88
14078
 YDOT =      -2094
300076  meter/sec      RA   =          333
00533  deg
 ZDOT =       1758
840766                 TA   =          198
82982
                                          MA   =          198
84814
                                          Ha   =            187
978  n
mi
                                          Hp   =            185
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -228072
99                 X    =            4784
39
 Y    =      -14629499
14  feet           Y    =        -4459432
65  meter
 Z    =      -16501993
86                 Z    =        -5029965
52
 XDOT =      23610
499073                 XDOT =        7210
819947
 YDOT =      -6871
063242  feet/sec       YDOT =       -2013
744951  meter/sec
 ZDOT =       5770
474955                 ZDOT =        1793
835751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14442555
38                 X    =        -4402090
88
 Y    =        2335620
50  feet           Y    =          711897
13  meter
 Z    =      -16502955
33                 Z    =        -5030100
78
 XDOT =     -10173
045475                 XDOT =       -3100
744261
 YDOT =     -21220
372466  feet/sec       YDOT =       -6467
969528  meter/sec
 ZDOT =       5905
068482                 ZDOT =        1799
864873


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   08177
52780658  
00020000  00000-0  20000-3 0  9069
2 25544  51
6381 333
4722 0008681 292
0191  68
0050 15
74764790 29849


Satellite: ISS
Catalog Number: 25544
Epoch time:      08177
52780658   =   yrday
fracday
Element set:     906
Inclination:       51
6381  deg
RA of node:       333
4722  deg
Eccentricity:     
0008681     
Arg of perigee:   292
0191  deg
Mean anomaly:      68
0050  deg
Mean motion:   15
74764790  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2984
Checksum:              310


Coasting Arc #8 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2008/178/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6115388
31                 A    =         6728411
22  meter
 Y    =        2144625
21  meter          E    =           
0003765
 Z    =       -1802453
20                 I    =           51
47916
 XDOT =       -159
931484                 Wp   =          242
15072
 YDOT =      -5218
023942  meter/sec      RA   =          327
88316  deg
 ZDOT =      -5658
725547                 TA   =          317
87823
                                          MA   =          317
90716
                                          Ha   =            188
208  n
mi
                                          Hp   =            185
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20063609
93                 X    =        -6130159
32
 Y    =        7036171
96  feet           Y    =         2076157
07  meter
 Z    =       -5913560
38                 Z    =        -1832197
44
 XDOT =       -524
709592                 XDOT =         -74
081708
 YDOT =     -17119
501122  feet/sec       YDOT =       -5219
331669  meter/sec
 ZDOT =     -18565
372528                 ZDOT =       -5659
294619

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10293219
16                 X    =         3137373
20
 Y    =       18567177
67  feet           Y    =         5659275
75  meter
 Z    =       -6027927
36                 Z    =        -1837312
26
 XDOT =     -15453
364828                 XDOT =       -4710
185600
 YDOT =       2531
225007  feet/sec       YDOT =         771
517382  meter/sec
 ZDOT =     -18567
979674                 ZDOT =       -5659
520205


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   08178
54313804  
00020000  00000-0  20000-3 0  9078
2 25544  51
6377 328
2510 0008793 296
8946  63
1318 15
74807460 30000


Satellite: ISS
Catalog Number: 25544
Epoch time:      08178
54313804   =   yrday
fracday
Element set:     907
Inclination:       51
6377  deg
RA of node:       328
2510  deg
Eccentricity:     
0008793     
Arg of perigee:   296
8946  deg
Mean anomaly:      63
1318  deg
Mean motion:   15
74807460  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3000
Checksum:              300


Coasting Arc #9 (Orbit 3015)
---------------------------------------

Vector Time (GMT): 2008/179/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         224199
02                 A    =         6719817
11  meter
 Y    =        4671629
39  meter          E    =           
0008112
 Z    =        4829369
29                 I    =           51
42592
 XDOT =      -6774
093130                 Wp   =          348
94493
 YDOT =       2784
048854  meter/sec      RA   =          322
69221  deg
 ZDOT =      -2371
448504                 TA   =          124
29872
                                          MA   =          124
22190
                                          Ha   =            188
408  n
mi
                                          Hp   =            185
075

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         735561
09                 X    =          148483
11
 Y    =       15326868
08  feet           Y    =         4673712
50  meter
 Z    =       15844387
44                 Z    =         4830275
18
 XDOT =     -22224
714995                 XDOT =       -6793
201200
 YDOT =       9134
018550  feet/sec       YDOT =        2708
190550  meter/sec
 ZDOT =      -7780
342861                 ZDOT =       -2404
403288

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14944735
07                 X    =         4555155
25
 Y    =       -3462148
84  feet           Y    =        -1055262
97  meter
 Z    =       15848248
09                 Z    =         4830546
02
 XDOT =      12817
212734                 XDOT =        3906
686441
 YDOT =      19024
003152  feet/sec       YDOT =        5798
516161  meter/sec
 ZDOT =      -7907
020538                 ZDOT =       -2410
059860


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   08179
55845414  
00020000  00000-0  20000-3 0  9088
2 25544  51
6381 323
0304 0008671 300
5209  59
5098 15
74777683 30163


Satellite: ISS
Catalog Number: 25544
Epoch time:      08179
55845414   =   yrday
fracday
Element set:     908
Inclination:       51
6381  deg
RA of node:       323
0304  deg
Eccentricity:     
0008671     
Arg of perigee:   300
5209  deg
Mean anomaly:      59
5098  deg
Mean motion:   15
74777683  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3016
Checksum:              303


Coasting Arc #10 (Orbit 3031)
---------------------------------------

Vector Time (GMT): 2008/180/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5700119
49                 A    =         6727247
88  meter
 Y    =       -2683415
60  meter          E    =           
0010694
 Z    =        2338362
35                 I    =           51
43063
 XDOT =        369
942732                 Wp   =           34
25995
 YDOT =       5489
713592  meter/sec      RA   =          317
57503  deg
 ZDOT =       5394
769389                 TA   =          352
16661
                                          MA   =          352
18330
                                          Ha   =            188
351  n
mi
                                          Hp   =            184
750

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18701179
44                 X    =         5718342
78
 Y    =       -8803856
95  feet           Y    =        -2619572
08  meter
 Z    =        7671792
48                 Z    =         2366097
61
 XDOT =       1213
722873                 XDOT =         282
321351
 YDOT =      18010
871365  feet/sec       YDOT =        5493
359718  meter/sec
 ZDOT =      17699
374636                 ZDOT =        5396
354637

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12380848
37                 X    =        -3773682
58
 Y    =      -16501811
91  feet           Y    =        -5029752
27  meter
 Z    =        7778380
73                 Z    =         2370850
45
 XDOT =      16214
496339                 XDOT =        4942
178484
 YDOT =      -3814
412416  feet/sec       YDOT =       -1162
632904  meter/sec
 ZDOT =      17705
914940                 ZDOT =        5396
762874


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   08180
57374820  
00020000  00000-0  20000-3 0  9091
2 25544  51
6392 317
8095 0008804 303
9788  56
0538 15
74874851 30324


Satellite: ISS
Catalog Number: 25544
Epoch time:      08180
57374820   =   yrday
fracday
Element set:     909
Inclination:       51
6392  deg
RA of node:       317
8095  deg
Eccentricity:     
0008804     
Arg of perigee:   303
9788  deg
Mean anomaly:      56
0538  deg
Mean motion:   15
74874851  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3032
Checksum:              317


Coasting Arc #11 (Orbit 3046)
---------------------------------------

Vector Time (GMT): 2008/181/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -446179
71                 A    =         6720631
80  meter
 Y    =       -4916448
47  meter          E    =           
0003347
 Z    =       -4561617
75                 I    =           51
38741
 XDOT =       6267
098570                 Wp   =           53
12441
 YDOT =      -3333
917356  meter/sec      RA   =          312
37380  deg
 ZDOT =       2983
739724                 TA   =          246
58683
                                          MA   =          246
62203
                                          Ha   =            188
659  n
mi
                                          Hp   =            184
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1463844
18                 X    =         -369010
34
 Y    =      -16130080
27  feet           Y    =        -4921005
56  meter
 Z    =      -14965937
51                 Z    =        -4563598
81
 XDOT =      20561
347014                 XDOT =        6289
418584
 YDOT =     -10938
049068  feet/sec       YDOT =       -3263
710841  meter/sec
 ZDOT =       9789
172324                 ZDOT =        3014
239139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15440651
66                 X    =        -4706310
63
 Y    =        4865035
26  feet           Y    =         1482862
75  meter
 Z    =      -14973954
82                 Z    =        -4564061
43
 XDOT =     -14794
121853                 XDOT =       -4509
248341
 YDOT =     -16498
269964  feet/sec       YDOT =       -5028
672685  meter/sec
 ZDOT =       9906
357991                 ZDOT =        3019
457916


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   08181
52557395  
00020000  00000-0  20000-3 0  9109
2 25544  51
6392 312
9159 0008926 308
4304  51
6058 15
74869047 30475


Satellite: ISS
Catalog Number: 25544
Epoch time:      08181
52557395   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:       312
9159  deg
Eccentricity:     
0008926     
Arg of perigee:   308
4304  deg
Mean anomaly:      51
6058  deg
Mean motion:   15
74869047  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3047
Checksum:              306


Coasting Arc #12 (Orbit 3062)
---------------------------------------

Vector Time (GMT): 2008/182/12:21:36
010
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5237481
68                 A    =         6725952
90  meter
 Y    =        3090533
37  meter          E    =           
0004804
 Z    =       -2876660
89                 I    =           51
38737
 XDOT =       -647
021972                 Wp   =          329
62759
 YDOT =      -5787
620718  meter/sec      RA   =          307
25934  deg
 ZDOT =      -5032
151285                 TA   =          243
55031
                                          MA   =          243
59960
                                          Ha   =            188
849  n
mi
                                          Hp   =            184
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17183338
83                 X    =        -5257676
88
 Y    =       10139545
18  feet           Y    =         3031852
57  meter
 Z    =       -9437863
81                 Z    =        -2902153
10
 XDOT =      -2122
775500                 XDOT =        -557
810385
 YDOT =     -18988
256950  feet/sec       YDOT =       -5794
356178  meter/sec
 ZDOT =     -16509
682693                 ZDOT =       -5035
079108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13880418
22                 X    =         4230751
47
 Y    =       14267214
79  feet           Y    =         4348647
07  meter
 Z    =       -9535793
38                 Z    =        -2906509
82
 XDOT =     -16939
716583                 XDOT =       -5163
225615
 YDOT =       5421
224865  feet/sec       YDOT =        1652
389339  meter/sec
 ZDOT =     -16521
413903                 ZDOT =       -5035
726958


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   08182
54083658  
00020000  00000-0  20000-3 0  9119
2 25544  51
6395 307
6944 0008932 312
6523  47
3887 15
74896635 30631


Satellite: ISS
Catalog Number: 25544
Epoch time:      08182
54083658   =   yrday
fracday
Element set:     911
Inclination:       51
6395  deg
RA of node:       307
6944  deg
Eccentricity:     
0008932     
Arg of perigee:   312
6523  deg
Mean anomaly:      47
3887  deg
Mean motion:   15
74896635  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3063
Checksum:              322

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 normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! 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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