Date: July 1st 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 2532)
---------------------------------------

Vector Time (GMT): 2010/179/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -877721
67                 A    =         6726269
00  meter
 Y    =        4288004
96  meter          E    =           
0017964
 Z    =       -5120428
09                 I    =           51
68468
 XDOT =      -7535
116766                 Wp   =           69
54419
 YDOT =        237
073727  meter/sec      RA   =          169
14881  deg
 ZDOT =       1500
553564                 TA   =          214
80367
                                          MA   =          214
92129
                                          Ha   =            195
700  n
mi
                                          Hp   =            184
828

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2879664
27                 X    =         -900731
93
 Y    =       14068257
74  feet           Y    =         4278061
95  meter
 Z    =      -16799304
76                 Z    =        -5124747
18
 XDOT =     -24721
511701                 XDOT =       -7544
497054
 YDOT =        777
800941  feet/sec       YDOT =         152
758861  meter/sec
 ZDOT =       4923
075999                 ZDOT =        1463
925739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14172480
13                 X    =        -4319771
94
 Y    =       -2184322
11  feet           Y    =         -665781
38  meter
 Z    =      -16816495
67                 Z    =        -5125667
88
 XDOT =      -1980
775263                 XDOT =        -603
740300
 YDOT =     -23661
843017  feet/sec       YDOT =       -7212
129752  meter/sec
 ZDOT =       4776
850218                 ZDOT =        1455
983947


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   10180
00297908  
00016717  00000-0  10270-3 0  9002
2 25544  51
6415 170
1307 0009592  18
9367 341
2150 15
72082592 25332


Satellite: ISS
Catalog Number: 25544
Epoch time:      10180
00297908   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:       170
1307  deg
Eccentricity:     
0009592     
Arg of perigee:    18
9367  deg
Mean anomaly:     341
2150  deg
Mean motion:   15
72082592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2533
Checksum:              288


Coasting Arc #2 (Orbit 2548)
---------------------------------------

Vector Time (GMT): 2010/180/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6575657
34                 A    =         6737237
57  meter
 Y    =       -1279589
00  meter          E    =           
0010552
 Z    =        -731167
25                 I    =           51
75205
 XDOT =        281
646666                 Wp   =           85
31038
 YDOT =       4823
929999  meter/sec      RA   =          164
05248  deg
 ZDOT =      -5982
224728                 TA   =          102
63093
                                          MA   =          102
51292
                                          Ha   =            195
761  n
mi
                                          Hp   =            184
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21573678
95                 X    =         6593029
05
 Y    =       -4198126
66  feet           Y    =        -1205958
85  meter
 Z    =       -2398842
68                 Z    =         -699181
15
 XDOT =        924
037619                 XDOT =         256
743821
 YDOT =      15826
541990  feet/sec       YDOT =        4826
941179  meter/sec
 ZDOT =     -19626
721547                 ZDOT =       -5980
916287

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5472453
58                 X    =         1668003
85
 Y    =       21300152
12  feet           Y    =         6492286
37  meter
 Z    =       -2271146
90                 Z    =         -692245
58
 XDOT =     -14183
002404                 XDOT =       -4322
979133
 YDOT =       1578
727574  feet/sec       YDOT =         481
196164  meter/sec
 ZDOT =     -19621
436749                 ZDOT =       -5980
613921


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   10181
02004490  
00016717  00000-0  10270-3 0  9018
2 25544  51
6419 164
9222 0009823  21
9897 338
1685 15
72147345 25495


Satellite: ISS
Catalog Number: 25544
Epoch time:      10181
02004490   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:       164
9222  deg
Eccentricity:     
0009823     
Arg of perigee:    21
9897  deg
Mean anomaly:     338
1685  deg
Mean motion:   15
72147345  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2549
Checksum:              307


Coasting Arc #3 (Orbit 2564)
---------------------------------------

Vector Time (GMT): 2010/181/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1351284
49                 A    =         6725581
07  meter
 Y    =       -3938244
68  meter          E    =           
0011102
 Z    =        5276130
20                 I    =           51
74079
 XDOT =       7224
796734                 Wp   =           38
07324
 YDOT =      -2670
131581  meter/sec      RA   =          158
93084  deg
 ZDOT =       -133
971298                 TA   =           53
24676
                                          MA   =           53
14488
                                          Ha   =            195
952  n
mi
                                          Hp   =            184
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4433348
06                 X    =        -1332776
05
 Y    =      -12920750
27  feet           Y    =        -3953252
75  meter
 Z    =       17310138
46                 Z    =         5269610
19
 XDOT =      23703
401359                 XDOT =        7254
768467
 YDOT =      -8760
274217  feet/sec       YDOT =       -2589
171996  meter/sec
 ZDOT =       -439
538379                 ZDOT =         -98
801221

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12535170
61                 X    =         3820720
00
 Y    =       -5511103
49  feet           Y    =        -1679784
35  meter
 Z    =       17284053
12                 Z    =         5268179
39
 XDOT =      10146
965480                 XDOT =        3092
795078
 YDOT =      22051
532091  feet/sec       YDOT =        6721
306981  meter/sec
 ZDOT =       -299
134189                 ZDOT =         -91
176101


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   10182
03710272  
00016717  00000-0  10270-3 0  9023
2 25544  51
6418 159
7136 0009659  27
3150 332
8518 15
72076187 25658


Satellite: ISS
Catalog Number: 25544
Epoch time:      10182
03710272   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:       159
7136  deg
Eccentricity:     
0009659     
Arg of perigee:    27
3150  deg
Mean anomaly:     332
8518  deg
Mean motion:   15
72076187  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2565
Checksum:              305


Coasting Arc #4 (Orbit 2579)
---------------------------------------

Vector Time (GMT): 2010/182/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5833963
81                 A    =         6737352
10  meter
 Y    =        3311179
92  meter          E    =           
0020520
 Z    =        -504788
24                 I    =           51
81016
 XDOT =      -2742
832502                 Wp   =           36
72753
 YDOT =      -3935
200932  meter/sec      RA   =          153
81565  deg
 ZDOT =       6027
787125                 TA   =          317
79397
                                          MA   =          317
95176
                                          Ha   =            195
834  n
mi
                                          Hp   =            184
313

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19140301
23                 X    =        -5868104
29
 Y    =       10863451
20  feet           Y    =         3245750
23  meter
 Z    =       -1656129
39                 Z    =         -533211
89
 XDOT =      -8998
794297                 XDOT =       -2727
906122
 YDOT =     -12910
764214  feet/sec       YDOT =       -3965
790168  meter/sec
 ZDOT =      19776
204479                 ZDOT =        6014
498372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12607593
70                 X    =        -3842794
56
 Y    =      -18028465
79  feet           Y    =        -5495076
37  meter
 Z    =       -1769595
98                 Z    =         -539372
85
 XDOT =      10684
827999                 XDOT =        3256
735574
 YDOT =      -9365
416319  feet/sec       YDOT =       -2854
578894  meter/sec
 ZDOT =      19723
086423                 ZDOT =        6011
596742


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   10182
99057931  
00016717  00000-0  10270-3 0  9035
2 25544  51
6431 154
8313 0009542  30
9716 329
2007 15
72139579 25800


Satellite: ISS
Catalog Number: 25544
Epoch time:      10182
99057931   =   yrday
fracday
Element set:     903
Inclination:       51
6431  deg
RA of node:       154
8313  deg
Eccentricity:     
0009542     
Arg of perigee:    30
9716  deg
Mean anomaly:     329
2007  deg
Mean motion:   15
72139579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2580
Checksum:              309


Coasting Arc #5 (Orbit 2595)
---------------------------------------

Vector Time (GMT): 2010/183/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3300368
70                 A    =         6725860
81  meter
 Y    =        2768395
54  meter          E    =           
0022047
 Z    =       -5183921
07                 I    =           51
79868
 XDOT =      -5921
720851                 Wp   =           62
54703
 YDOT =       4734
916851  meter/sec      RA   =          148
72269  deg
 ZDOT =      -1235
543363                 TA   =          195
60886
                                          MA   =          195
67694
                                          Ha   =            195
922  n
mi
                                          Hp   =            184
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10827981
29                 X    =         3294349
09
 Y    =        9082662
54  feet           Y    =         2805269
15  meter
 Z    =      -17007615
07                 Z    =        -5167902
30
 XDOT =     -19428
218015                 XDOT =       -5968
225428
 YDOT =      15534
504105  feet/sec       YDOT =        4668
436751  meter/sec
 ZDOT =      -4053
619957                 ZDOT =       -1264
423333

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7815521
74                 X    =        -2382171
03
 Y    =       11867213
12  feet           Y    =         3617126
56  meter
 Z    =      -16943605
90                 Z    =        -5164411
08
 XDOT =     -16723
019758                 XDOT =       -5097
176422
 YDOT =     -16993
598910  feet/sec       YDOT =       -5179
648948  meter/sec
 ZDOT =      -4168
901306                 ZDOT =       -1270
681118


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   10184
00761044  
00016717  00000-0  10270-3 0  9047
2 25544  51
6435 149
6240 0009624  35
0463 325
1331 15
72172742 25962


Satellite: ISS
Catalog Number: 25544
Epoch time:      10184
00761044   =   yrday
fracday
Element set:     904
Inclination:       51
6435  deg
RA of node:       149
6240  deg
Eccentricity:     
0009624     
Arg of perigee:    35
0463  deg
Mean anomaly:     325
1331  deg
Mean motion:   15
72172742  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2596
Checksum:              283


Coasting Arc #6 (Orbit 2611)
---------------------------------------

Vector Time (GMT): 2010/184/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4390894
05                 A    =         6736179
82  meter
 Y    =       -4835049
61  meter          E    =           
0018580
 Z    =        1635927
13                 I    =           51
85809
 XDOT =       4605
794041                 Wp   =           86
40076
 YDOT =       2216
799755  meter/sec      RA   =          143
58749  deg
 ZDOT =      -5753
315300                 TA   =           75
60437
                                          MA   =           75
39821
                                          Ha   =            195
924  n
mi
                                          Hp   =            183
991

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14405820
37                 X    =         4436687
10
 Y    =      -15863023
65  feet           Y    =        -4785692
15  meter
 Z    =        5367215
00                 Z    =         1657368
73
 XDOT =      15110
872838                 XDOT =        4608
611550
 YDOT =       7272
965077  feet/sec       YDOT =        2268
320886  meter/sec
 ZDOT =     -18875
706365                 ZDOT =       -5730
933326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17570524
56                 X    =         5355495
89
 Y    =       12227585
20  feet           Y    =         3726967
97  meter
 Z    =        5452797
78                 Z    =         1662012
76
 XDOT =      -4374
654182                 XDOT =       -1333
394595
 YDOT =      14745
848263  feet/sec       YDOT =        4494
534551  meter/sec
 ZDOT =     -18786
286024                 ZDOT =       -5726
059980


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   10185
02462863  
00016717  00000-0  10270-3 0  9058
2 25544  51
6428 144
4143 0009517  38
2999 321
8838 15
72175065 26124


Satellite: ISS
Catalog Number: 25544
Epoch time:      10185
02462863   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:       144
4143  deg
Eccentricity:     
0009517     
Arg of perigee:    38
2999  deg
Mean anomaly:     321
8838  deg
Mean motion:   15
72175065  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2612
Checksum:              316


Coasting Arc #7 (Orbit 2627)
---------------------------------------

Vector Time (GMT): 2010/185/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4590697
45                 A    =         6727275
76  meter
 Y    =        -980280
08  meter          E    =           
0013051
 Z    =        4806703
63                 I    =           51
85320
 XDOT =       3944
396285                 Wp   =           75
10529
 YDOT =      -6125
149752  meter/sec      RA   =          138
51628  deg
 ZDOT =       2515
625586                 TA   =          350
36113
                                          MA   =          350
38615
                                          Ha   =            196
017  n
mi
                                          Hp   =            183
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15061343
34                 X    =        -4602744
69
 Y    =       -3216142
01  feet           Y    =        -1031683
93  meter
 Z    =       15770025
02                 Z    =         4784372
63
 XDOT =      12940
932693                 XDOT =        4000
375209
 YDOT =     -20095
635668  feet/sec       YDOT =       -6080
728463  meter/sec
 ZDOT =       8253
364782                 ZDOT =        2534
922714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         985766
25                 X    =          300461
55
 Y    =      -15460322
01  feet           Y    =        -4712306
15  meter
 Z    =       15680817
25                 Z    =         4779513
10
 XDOT =      20623
979893                 XDOT =        6286
189071
 YDOT =       9772
062278  feet/sec       YDOT =        2978
524582  meter/sec
 ZDOT =       8330
379769                 ZDOT =        2539
099754


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   10186
04163345  
00016717  00000-0  10270-3 0  9065
2 25544  51
6438 139
2061 0009442  41
9111 318
2772 15
72227619 26287


Satellite: ISS
Catalog Number: 25544
Epoch time:      10186
04163345   =   yrday
fracday
Element set:     906
Inclination:       51
6438  deg
RA of node:       139
2061  deg
Eccentricity:     
0009442     
Arg of perigee:    41
9111  deg
Mean anomaly:     318
2772  deg
Mean motion:   15
72227619  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2628
Checksum:              296


Coasting Arc #8 (Orbit 2642)
---------------------------------------

Vector Time (GMT): 2010/186/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2409551
99                 A    =         6734015
89  meter
 Y    =        5664413
79  meter          E    =           
0014301
 Z    =       -2726745
50                 I    =           51
89839
 XDOT =      -5675
457953                 Wp   =           50
09690
 YDOT =         74
270331  meter/sec      RA   =          133
36959  deg
 ZDOT =       5196
372617                 TA   =          278
92694
                                          MA   =          279
08881
                                          Ha   =            196
007  n
mi
                                          Hp   =            183
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7905354
31                 X    =        -2459467
35
 Y    =       18584034
73  feet           Y    =         5637190
01  meter
 Z    =       -8946015
42                 Z    =        -2738571
62
 XDOT =     -18620
268876                 XDOT =       -5701
109737
 YDOT =        243
669064  feet/sec       YDOT =          10
659856  meter/sec
 ZDOT =      17048
466592                 ZDOT =        5168
738877

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19609871
82                 X    =        -5977088
93
 Y    =       -4739974
06  feet           Y    =        -1444744
09  meter
 Z    =       -8993205
14                 Z    =        -2741128
93
 XDOT =      -3617
583884                 XDOT =       -1102
639568
 YDOT =     -17004
229011  feet/sec       YDOT =       -5182
889003  meter/sec
 ZDOT =      16938
080055                 ZDOT =        5162
726801


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   10186
99506573  
00016717  00000-0  10270-3 0  9074
2 25544  51
6445 134
3239 0009579  45
6736 314
5210 15
72207091 26438


Satellite: ISS
Catalog Number: 25544
Epoch time:      10186
99506573   =   yrday
fracday
Element set:     907
Inclination:       51
6445  deg
RA of node:       134
3239  deg
Eccentricity:     
0009579     
Arg of perigee:    45
6736  deg
Mean anomaly:     314
5210  deg
Mean motion:   15
72207091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2643
Checksum:              316


Coasting Arc #9 (Orbit 2658)
---------------------------------------

Vector Time (GMT): 2010/187/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5120359
48                 A    =         6729571
79  meter
 Y    =       -1119119
64  meter          E    =           
0017376
 Z    =       -4239490
61                 I    =           51
90347
 XDOT =      -1569
370453                 Wp   =           59
04025
 YDOT =       6583
780387  meter/sec      RA   =          128
31356  deg
 ZDOT =      -3635
623438                 TA   =          174
00676
                                          MA   =          173
98595
                                          Ha   =            196
015  n
mi
                                          Hp   =            183
726

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16799079
65                 X    =         5153087
85
 Y    =       -3671652
37  feet           Y    =        -1061677
09  meter
 Z    =      -13909089
94                 Z    =        -4214536
51
 XDOT =      -5148
853191                 XDOT =       -1625
213593
 YDOT =      21600
329353  feet/sec       YDOT =        6565
919067  meter/sec
 ZDOT =     -11927
898418                 ZDOT =       -3643
382105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6632121
31                 X    =         2021470
58
 Y    =       15952057
88  feet           Y    =         4862187
24  meter
 Z    =      -13809406
49                 Z    =        -4209107
10
 XDOT =     -20996
669275                 XDOT =       -6399
784795
 YDOT =      -1616
767960  feet/sec       YDOT =        -492
790874  meter/sec
 ZDOT =     -11958
844900                 ZDOT =       -3645
055926


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   10188
01204653  
00016717  00000-0  10270-3 0  9084
2 25544  51
6446 129
1152 0009493  49
4084 310
7903 15
72225230 26597


Satellite: ISS
Catalog Number: 25544
Epoch time:      10188
01204653   =   yrday
fracday
Element set:     908
Inclination:       51
6446  deg
RA of node:       129
1152  deg
Eccentricity:     
0009493     
Arg of perigee:    49
4084  deg
Mean anomaly:     310
7903  deg
Mean motion:   15
72225230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2659
Checksum:              295


Coasting Arc #10 (Orbit 2674)
---------------------------------------

Vector Time (GMT): 2010/188/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         328379
69                 A    =         6731553
94  meter
 Y    =       -5667340
82  meter          E    =           
0020743
 Z    =        3606661
90                 I    =           51
92863
 XDOT =       5781
099717                 Wp   =           71
89265
 YDOT =      -2502
195124  meter/sec      RA   =          123
16072  deg
 ZDOT =      -4431
176978                 TA   =           65
17152
                                          MA   =           64
95594
                                          Ha   =            196
083  n
mi
                                          Hp   =            183
465

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1077361
19                 X    =          374207
99
 Y    =      -18593637
85  feet           Y    =        -5663413
06  meter
 Z    =       11832880
26                 Z    =         3608367
51
 XDOT =      18966
862588                 XDOT =        5830
175935
 YDOT =      -8209
301588  feet/sec       YDOT =       -2437
272253  meter/sec
 ZDOT =     -14537
982210                 ZDOT =       -4402
973576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18430729
05                 X    =         5617686
22
 Y    =       -2651747
84  feet           Y    =         -808252
74  meter
 Z    =       11839661
78                 Z    =         3608728
91
 XDOT =      11587
119847                 XDOT =        3531
754129
 YDOT =      15732
833245  feet/sec       YDOT =        4795
367573  meter/sec
 ZDOT =     -14425
312415                 ZDOT =       -4396
835224


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   10189
02901505  
00016717  00000-0  10270-3 0  9097
2 25544  51
6450 123
9068 0009560  53
8169 306
3876 15
72234586 26750


Satellite: ISS
Catalog Number: 25544
Epoch time:      10189
02901505   =   yrday
fracday
Element set:     909
Inclination:       51
6450  deg
RA of node:       123
9068  deg
Eccentricity:     
0009560     
Arg of perigee:    53
8169  deg
Mean anomaly:     306
3876  deg
Mean motion:   15
72234586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2675
Checksum:              321


Coasting Arc #11 (Orbit 2690)
---------------------------------------

Vector Time (GMT): 2010/189/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4783099
37                 A    =         6731915
45  meter
 Y    =        3222199
04  meter          E    =           
0021060
 Z    =        3450087
04                 I    =           51
94700
 XDOT =       -803
091873                 Wp   =           76
40984
 YDOT =      -6134
483916  meter/sec      RA   =          118
11079  deg
 ZDOT =       4597
471081                 TA   =          324
27929
                                          MA   =          324
42000
                                          Ha   =            196
100  n
mi
                                          Hp   =            183
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15692583
23                 X    =        -4835534
95
 Y    =       10571519
15  feet           Y    =         3168417
73  meter
 Z    =       11319183
21                 Z    =         3426724
04
 XDOT =      -2634
815857                 XDOT =        -756
768905
 YDOT =     -20126
259566  feet/sec       YDOT =       -6143
206438  meter/sec
 ZDOT =      15083
566539                 ZDOT =        4593
681018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13680495
71                 X    =        -4169815
09
 Y    =      -13151525
35  feet           Y    =        -4008584
93  meter
 Z    =       11225841
27                 Z    =         3421636
42
 XDOT =      18127
599071                 XDOT =        5525
292197
 YDOT =      -5942
634329  feet/sec       YDOT =       -1811
314944  meter/sec
 ZDOT =      15068
395600                 ZDOT =        4592
846979


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   10190
04596813  
00016717  00000-0  10270-3 0  9105
2 25544  51
6461 118
6983 0009532  57
2683 302
9396 15
72305371 26915


Satellite: ISS
Catalog Number: 25544
Epoch time:      10190
04596813   =   yrday
fracday
Element set:     910
Inclination:       51
6461  deg
RA of node:       118
6983  deg
Eccentricity:     
0009532     
Arg of perigee:    57
2683  deg
Mean anomaly:     302
9396  deg
Mean motion:   15
72305371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2691
Checksum:              314


Coasting Arc #12 (Orbit 2705)
---------------------------------------

Vector Time (GMT): 2010/190/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1649821
92                 A    =         6728800
19  meter
 Y    =        4860965
24  meter          E    =           
0016770
 Z    =       -4363757
16                 I    =           51
95023
 XDOT =      -4949
654036                 Wp   =           84
79624
 YDOT =       4764
036332  meter/sec      RA   =          112
96186  deg
 ZDOT =       3448
292799                 TA   =          219
86948
                                          MA   =          219
99278
                                          Ha   =            196
057  n
mi
                                          Hp   =            183
248

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5412801
57                 X    =         1616541
29
 Y    =       15948048
68  feet           Y    =         4879229
32  meter
 Z    =      -14316788
58                 Z    =        -4355822
25
 XDOT =     -16239
022427                 XDOT =       -5019
309543
 YDOT =      15630
040459  feet/sec       YDOT =        4708
296198  meter/sec
 ZDOT =      11313
296584                 ZDOT =        3424
079306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14261494
23                 X    =        -4346903
44
 Y    =        9008654
97  feet           Y    =         2745838
03  meter
 Z    =      -14285063
21                 Z    =        -4354087
27
 XDOT =     -18296
761983                 XDOT =       -5576
853052
 YDOT =     -11245
868913  feet/sec       YDOT =       -3427
740845  meter/sec
 ZDOT =      11216
544555                 ZDOT =        3418
802780


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   10190
99935285  
00016717  00000-0  10270-3 0  9110
2 25544  51
6465 113
8164 0009554  60
2349 299
9763 15
72302838 27069


Satellite: ISS
Catalog Number: 25544
Epoch time:      10190
99935285   =   yrday
fracday
Element set:     911
Inclination:       51
6465  deg
RA of node:       113
8164  deg
Eccentricity:     
0009554     
Arg of perigee:    60
2349  deg
Mean anomaly:     299
9763  deg
Mean motion:   15
72302838  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2706
Checksum:              333


Coasting Arc #13 (Orbit 2721)
---------------------------------------

Vector Time (GMT): 2010/191/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3728152
73                 A    =         6734144
06  meter
 Y    =       -4987801
58  meter          E    =           
0012671
 Z    =       -2575663
88                 I    =           51
97934
 XDOT =       2797
762842                 Wp   =           85
94998
 YDOT =       4816
643260  meter/sec      RA   =          107
90807  deg
 ZDOT =      -5299
225296                 TA   =          123
07388
                                          MA   =          122
95215
                                          Ha   =            196
079  n
mi
                                          Hp   =            183
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12231472
22                 X    =         3796162
09
 Y    =      -16364178
40  feet           Y    =        -4945730
39  meter
 Z    =       -8450340
82                 Z    =        -2557388
53
 XDOT =       9179
011948                 XDOT =        2769
436653
 YDOT =      15802
635368  feet/sec       YDOT =        4847
772163  meter/sec
 ZDOT =     -17385
909765                 ZDOT =       -5285
701811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18883374
73                 X    =         5755652
62
 Y    =        7876699
49  feet           Y    =         2400818
01  meter
 Z    =       -8377306
94                 Z    =        -2553403
15
 XDOT =     -12457
780113                 XDOT =       -3797
131378
 YDOT =      11507
772736  feet/sec       YDOT =        3507
569130  meter/sec
 ZDOT =     -17331
848029                 ZDOT =       -5282
747279


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   10192
01628296  
00016717  00000-0  10270-3 0  9127
2 25544  51
6468 108
6077 0009573  64
2053 296
0096 15
72314729 27221


Satellite: ISS
Catalog Number: 25544
Epoch time:      10192
01628296   =   yrday
fracday
Element set:     912
Inclination:       51
6468  deg
RA of node:       108
6077  deg
Eccentricity:     
0009573     
Arg of perigee:    64
2053  deg
Mean anomaly:     296
0096  deg
Mean motion:   15
72314729  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2722
Checksum:              312


Coasting Arc #14 (Orbit 2737)
---------------------------------------

Vector Time (GMT): 2010/192/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3128896
01                 A    =         6726629
29  meter
 Y    =       -3417830
38  meter          E    =           
0016427
 Z    =        4866161
21                 I    =           51
96309
 XDOT =       3382
147356                 Wp   =           63
56340
 YDOT =      -6502
612094  meter/sec      RA   =          102
76867  deg
 ZDOT =      -2379
235237                 TA   =           49
58744
                                          MA   =           49
44423
                                          Ha   =            196
146  n
mi
                                          Hp   =            182
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10265406
86                 X    =        -3114083
15
 Y    =      -11213354
25  feet           Y    =        -3452737
59  meter
 Z    =       15965095
84                 Z    =         4850996
70
 XDOT =      11096
283976                 XDOT =        3466
167055
 YDOT =     -21334
029180  feet/sec       YDOT =       -6464
320706  meter/sec
 ZDOT =      -7805
889884                 ZDOT =       -2362
602135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8097365
09                 X    =         2468076
88
 Y    =      -12941506
65  feet           Y    =        -3944571
23  meter
 Z    =       15904472
99                 Z    =         4847683
37
 XDOT =      22568
398798                 XDOT =        6878
847954
 YDOT =       4555
645535  feet/sec       YDOT =        1388
560759  meter/sec
 ZDOT =      -7739
412092                 ZDOT =       -2358
972806


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   10193
03319967  
00016717  00000-0  10270-3 0  9133
2 25544  51
6473 103
3992 0009642  67
1020 293
1159 15
72355948 27381


Satellite: ISS
Catalog Number: 25544
Epoch time:      10193
03319967   =   yrday
fracday
Element set:     913
Inclination:       51
6473  deg
RA of node:       103
3992  deg
Eccentricity:     
0009642     
Arg of perigee:    67
1020  deg
Mean anomaly:     293
1159  deg
Mean motion:   15
72355948  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2738
Checksum:              318


Coasting Arc #15 (Orbit 2753)
---------------------------------------

Vector Time (GMT): 2010/193/23:44:56
394
Vector Time (MET): N/A
Weight (LBS)     : 813514
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2064682
61                 A    =         6735851
88  meter
 Y    =        6209189
05  meter          E    =           
0023659
 Z    =        1553452
15                 I    =           51
99953
 XDOT =      -4187
236202                 Wp   =           65
86170
 YDOT =      -2858
610696  meter/sec      RA   =           97
70365  deg
 ZDOT =       5801
415349                 TA   =          311
18351
                                          MA   =          311
38731
                                          Ha   =            196
115  n
mi
                                          Hp   =            182
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6773893
09                 X    =        -2141507
67
 Y    =       20371355
16  feet           Y    =         6185670
76  meter
 Z    =        5096627
78                 Z    =         1543236
45
 XDOT =     -13737
651580                 XDOT =       -4183
141103
 YDOT =      -9378
644015  feet/sec       YDOT =       -2905
412834  meter/sec
 ZDOT =      19033
514926                 ZDOT =        5781
083717

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21461123
87                 X    =        -6541350
55
 Y    =        -844058
50  feet           Y    =         -257269
03  meter
 Z    =        5055796
78                 Z    =         1541006
86
 XDOT =       5075
453779                 XDOT =        1546
998312
 YDOT =     -14352
970998  feet/sec       YDOT =       -4374
785560  meter/sec
 ZDOT =      18952
231497                 ZDOT =        5776
640160


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   10194
05010446  
00016717  00000-0  10270-3 0  9147
2 25544  51
6472  98
1911 0009656  71
0523 289
1685 15
72351325 27541


Satellite: ISS
Catalog Number: 25544
Epoch time:      10194
05010446   =   yrday
fracday
Element set:     914
Inclination:       51
6472  deg
RA of node:        98
1911  deg
Eccentricity:     
0009656     
Arg of perigee:    71
0523  deg
Mean anomaly:     289
1685  deg
Mean motion:   15
72351325  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2754
Checksum:              302

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

The following information is a reminder of your current mailing list subscription:

You are subscribed to the following list: [list_name]

using the following email: example@example.com

You may automatically unsubscribe from this list at any time by visiting the following URL:

https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/

If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism

You may also change your subscription by visiting this list's main screen:

<[program_url]/list/[list]>

If you're still having trouble, please contact the list owner at:

<mailto:[list_owner_email]>

The following physical address is associated with this mailing list:

[physical_address]

Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list