Date: May 27th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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


146/06:29:55 633 0 8 -2 4 2 4
N/A -1 6 0 0 190 5
000/00:09:51 266 -1 7 0 0 182 3

Coasting Arc #1 (Orbit 1974)
---------------------------------------

Vector Time (GMT): 2010/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816784
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3069812
54                 A    =         6721090
84  meter
 Y    =        3455377
43  meter          E    =           
0007914
 Z    =        4874199
58                 I    =           51
58384
 XDOT =      -6795
213082                 Wp   =           24
31235
 YDOT =       2828
060663  meter/sec      RA   =          351
62883  deg
 ZDOT =       2280
622283                 TA   =           43
52441
                                          MA   =           43
46198
                                          Ha   =            191
875  n
mi
                                          Hp   =            182
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10071563
44                 X    =         3007267
34
 Y    =       11336540
12  feet           Y    =         3489355
78  meter
 Z    =       15991468
43                 Z    =         4888961
35
 XDOT =     -22294
006176                 XDOT =       -6837
410968
 YDOT =       9278
414250  feet/sec       YDOT =        2751
836410  meter/sec
 ZDOT =       7482
356570                 ZDOT =        2247
508303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14740962
76                 X    =         4493045
45
 Y    =       -3282396
51  feet           Y    =        -1000474
46  meter
 Z    =       16050248
75                 Z    =         4892115
82
 XDOT =      -2867
971926                 XDOT =        -874
157843
 YDOT =      22969
996371  feet/sec       YDOT =        7001
254894  meter/sec
 ZDOT =       7350
464901                 ZDOT =        2240
421702


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   10144
55147307  
00016717  00000-0  10270-3 0  9009
2 25544  51
6468 351
8551 0010914 348
6984  11
3932 15
74228635 19751


Satellite: ISS
Catalog Number: 25544
Epoch time:      10144
55147307   =   yrday
fracday
Element set:     900
Inclination:       51
6468  deg
RA of node:       351
8551  deg
Eccentricity:     
0010914     
Arg of perigee:   348
6984  deg
Mean anomaly:      11
3932  deg
Mean motion:   15
74228635  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1975
Checksum:              314


Coasting Arc #2 (Orbit 1989)
---------------------------------------

Vector Time (GMT): 2010/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816784
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5741729
62                 A    =         6729864
97  meter
 Y    =       -2931494
86  meter          E    =           
0016629
 Z    =       -1897420
27                 I    =           51
58282
 XDOT =       3741
024635                 Wp   =            9
37783
 YDOT =       3695
144217  meter/sec      RA   =          346
45143  deg
 ZDOT =       5634
653618                 TA   =          329
49983
                                          MA   =          329
59644
                                          Ha   =            191
987  n
mi
                                          Hp   =            182
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18837695
62                 X    =         5783300
89
 Y    =       -9617765
29  feet           Y    =        -2867054
77  meter
 Z    =       -6225132
12                 Z    =        -1869425
76
 XDOT =      12273
702870                 XDOT =        3672
054172
 YDOT =      12123
176564  feet/sec       YDOT =        3736
592328  meter/sec
 ZDOT =      18486
396384                 ZDOT =        5652
660739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         298544
72                 X    =           90996
43
 Y    =      -21181285
78  feet           Y    =        -6456055
90  meter
 Z    =       -6113628
96                 Z    =        -1863434
11
 XDOT =      14854
117766                 XDOT =        4527
535095
 YDOT =      -5124
941361  feet/sec       YDOT =       -1562
082127  meter/sec
 ZDOT =      18558
096140                 ZDOT =        5656
507704


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   10145
50364799  
00016717  00000-0  10270-3 0  9012
2 25544  51
6457 346
9631 0010897 351
2789   8
8183 15
74280537 19901


Satellite: ISS
Catalog Number: 25544
Epoch time:      10145
50364799   =   yrday
fracday
Element set:     901
Inclination:       51
6457  deg
RA of node:       346
9631  deg
Eccentricity:     
0010897     
Arg of perigee:   351
2789  deg
Mean anomaly:       8
8183  deg
Mean motion:   15
74280537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1990
Checksum:              337


Coasting Arc #3 (Orbit 2002)
---------------------------------------

Vector Time (GMT): 2010/146/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5095346
50                 A    =         6722823
65  meter
 Y    =        1737582
57  meter          E    =           
0010957
 Z    =        4014432
17                 I    =           51
54304
 XDOT =      -4682
338851                 Wp   =           51
45176
 YDOT =       4721
700344  meter/sec      RA   =          342
51399  deg
 ZDOT =       3898
963789                 TA   =          358
31193
                                          MA   =          358
31562
                                          Ha   =            190
492  n
mi
                                          Hp   =            182
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16717016
08                 X    =         5056036
08
 Y    =        5700730
22  feet           Y    =         1794341
45  meter
 Z    =       13170709
22                 Z    =         4039090
57
 XDOT =     -15362
004105                 XDOT =       -4753
730568
 YDOT =      15491
142862  feet/sec       YDOT =        4668
939966  meter/sec
 ZDOT =      12791
875948                 ZDOT =        3876
043752

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14001185
25                 X    =         4267561
26
 Y    =       10645539
06  feet           Y    =         3244760
31  meter
 Z    =       13268905
10                 Z    =         4044362
27
 XDOT =     -18750
167464                 XDOT =       -5715
051043
 YDOT =       8828
479207  feet/sec       YDOT =        2690
920462  meter/sec
 ZDOT =      12700
571883                 ZDOT =        3871
134310


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   10146
32883819  
00016717  00000-0  10270-3 0  9023
2 25544  51
6473 342
7254 0009345 348
9458  11
1499 15
74779267 20032


Satellite: ISS
Catalog Number: 25544
Epoch time:      10146
32883819   =   yrday
fracday
Element set:     902
Inclination:       51
6473  deg
RA of node:       342
7254  deg
Eccentricity:     
0009345     
Arg of perigee:   348
9458  deg
Mean anomaly:      11
1499  deg
Mean motion:   15
74779267  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2003
Checksum:              329


Coasting Arc #4 (Orbit 2017)
---------------------------------------

Vector Time (GMT): 2010/147/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3958374
28                 A    =         6725485
17  meter
 Y    =       -4399364
61  meter          E    =           
0010671
 Z    =       -3186335
88                 I    =           51
52399
 XDOT =       5770
965795                 Wp   =           17
10569
 YDOT =       1724
424541  meter/sec      RA   =          337
31422  deg
 ZDOT =       4802
428404                 TA   =          305
62595
                                          MA   =          305
72530
                                          Ha   =            190
713  n
mi
                                          Hp   =            182
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12986792
26                 X    =         4022753
47
 Y    =      -14433610
93  feet           Y    =        -4354739
27  meter
 Z    =      -10453857
89                 Z    =        -3166950
06
 XDOT =      18933
614812                 XDOT =        5727
924338
 YDOT =       5657
560831  feet/sec       YDOT =        1788
717531  meter/sec
 ZDOT =      15755
998702                 ZDOT =        4830
359940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16758504
42                 X    =         5107992
15
 Y    =       -9886718
01  feet           Y    =        -3013471
65  meter
 Z    =      -10376626
58                 Z    =        -3162795
78
 XDOT =      15575
298862                 XDOT =        4747
351093
 YDOT =       9796
321846  feet/sec       YDOT =        2985
918899  meter/sec
 ZDOT =      15867
230341                 ZDOT =        4836
331808


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   10147
28070004  
00016717  00000-0  10270-3 0  9034
2 25544  51
6477 337
8319 0009404 352
2259   7
8757 15
74818387 20188


Satellite: ISS
Catalog Number: 25544
Epoch time:      10147
28070004   =   yrday
fracday
Element set:     903
Inclination:       51
6477  deg
RA of node:       337
8319  deg
Eccentricity:     
0009404     
Arg of perigee:   352
2259  deg
Mean anomaly:       7
8757  deg
Mean motion:   15
74818387  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2018
Checksum:              316


Coasting Arc #5 (Orbit 2033)
---------------------------------------

Vector Time (GMT): 2010/148/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4948912
01                 A    =         6721358
67  meter
 Y    =       -1320322
20  meter          E    =           
0015067
 Z    =       -4366435
95                 I    =           51
48374
 XDOT =       4396
405826                 Wp   =           31
66267
 YDOT =      -5340
241571  meter/sec      RA   =          332
21210  deg
 ZDOT =      -3360
724591                 TA   =          204
34788
                                          MA   =          204
41914
                                          Ha   =            190
765  n
mi
                                          Hp   =            181
610

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16236587
97                 X    =        -4912568
49
 Y    =       -4331765
74  feet           Y    =        -1375459
94  meter
 Z    =      -14325577
26                 Z    =        -4390390
02
 XDOT =      14423
903627                 XDOT =        4472
120618
 YDOT =     -17520
477596  feet/sec       YDOT =       -5290
654439  meter/sec
 ZDOT =     -11025
999314                 ZDOT =       -3339
183550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14277210
16                 X    =        -4351693
66
 Y    =       -8706891
88  feet           Y    =        -2653860
65  meter
 Z    =      -14420972
60                 Z    =        -4395512
45
 XDOT =      18202
779022                 XDOT =        5548
207046
 YDOT =     -11688
484595  feet/sec       YDOT =       -3562
650105  meter/sec
 ZDOT =     -10940
174692                 ZDOT =       -3334
565246


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   10148
29600223  
00016717  00000-0  10270-3 0  9049
2 25544  51
6483 332
6120 0009517 356
0739   4
0348 15
74855069 20349


Satellite: ISS
Catalog Number: 25544
Epoch time:      10148
29600223   =   yrday
fracday
Element set:     904
Inclination:       51
6483  deg
RA of node:       332
6120  deg
Eccentricity:     
0009517     
Arg of perigee:   356
0739  deg
Mean anomaly:       4
0348  deg
Mean motion:   15
74855069  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2034
Checksum:              292


Coasting Arc #6 (Orbit 2049)
---------------------------------------

Vector Time (GMT): 2010/149/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3705033
38                 A    =         6726719
43  meter
 Y    =        4938425
66  meter          E    =           
0014905
 Z    =        2669082
65                 I    =           51
47484
 XDOT =      -5531
768315                 Wp   =           63
44472
 YDOT =      -1331
695977  meter/sec      RA   =          327
01178  deg
 ZDOT =      -5186
019559                 TA   =           86
07529
                                          MA   =           85
90490
                                          Ha   =            190
907  n
mi
                                          Hp   =            181
591

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12155621
31                 X    =        -3772946
40
 Y    =       16202183
91  feet           Y    =         4896613
58  meter
 Z    =        8756832
84                 Z    =         2650919
35
 XDOT =     -18148
846178                 XDOT =       -5491
272962
 YDOT =      -4369
081288  feet/sec       YDOT =       -1393
328173  meter/sec
 ZDOT =     -17014
499864                 ZDOT =       -5212
794988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16066410
20                 X    =        -4897041
83
 Y    =       12385581
10  feet           Y    =         3775125
12  meter
 Z    =        8684460
73                 Z    =         2647023
63
 XDOT =     -15340
250432                 XDOT =       -4675
708332
 YDOT =      -7827
344629  feet/sec       YDOT =       -2385
774643  meter/sec
 ZDOT =     -17121
135919                 ZDOT =       -5218
522228


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   10149
31128784  
00016717  00000-0  10270-3 0  9051
2 25544  51
6478 327
3919 0009472 359
9277    
1884 15
74848031 20500


Satellite: ISS
Catalog Number: 25544
Epoch time:      10149
31128784   =   yrday
fracday
Element set:     905
Inclination:       51
6478  deg
RA of node:       327
3919  deg
Eccentricity:     
0009472     
Arg of perigee:   359
9277  deg
Mean anomaly:        
1884  deg
Mean motion:   15
74848031  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2050
Checksum:              325


Coasting Arc #7 (Orbit 2065)
---------------------------------------

Vector Time (GMT): 2010/150/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4711043
20                 A    =         6720014
88  meter
 Y    =        1037980
44  meter          E    =           
0009478
 Z    =        4669425
17                 I    =           51
42879
 XDOT =      -4040
672675                 Wp   =           50
96294
 YDOT =       5959
304041  meter/sec      RA   =          321
89987  deg
 ZDOT =       2754
131625                 TA   =           11
85674
                                          MA   =           11
83444
                                          Ha   =            190
848  n
mi
                                          Hp   =            181
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15456178
48                 X    =         4676402
87
 Y    =        3405447
63  feet           Y    =         1090467
63  meter
 Z    =       15319636
38                 Z    =         4692227
55
 XDOT =     -13256
800114                 XDOT =       -4120
389498
 YDOT =      19551
522444  feet/sec       YDOT =        5913
672634  meter/sec
 ZDOT =       9035
864910                 ZDOT =        2734
309361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14036872
16                 X    =         4278438
64
 Y    =        7117999
02  feet           Y    =         2169566
10  meter
 Z    =       15410454
10                 Z    =         4697106
41
 XDOT =     -17232
583118                 XDOT =       -5252
491334
 YDOT =      14606
686525  feet/sec       YDOT =        4452
118053  meter/sec
 ZDOT =       8956
878693                 ZDOT =        2730
056626


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   10150
32655431  
00016717  00000-0  10270-3 0  9069
2 25544  51
6485 322
1715 0009585   3
4008 356
7219 15
74888984 20663


Satellite: ISS
Catalog Number: 25544
Epoch time:      10150
32655431   =   yrday
fracday
Element set:     906
Inclination:       51
6485  deg
RA of node:       322
1715  deg
Eccentricity:     
0009585     
Arg of perigee:     3
4008  deg
Mean anomaly:     356
7219  deg
Mean motion:   15
74888984  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2066
Checksum:              316


Coasting Arc #8 (Orbit 2080)
---------------------------------------

Vector Time (GMT): 2010/151/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3311643
67                 A    =         6727605
91  meter
 Y    =       -5447917
03  meter          E    =           
0015386
 Z    =       -2124349
64                 I    =           51
43188
 XDOT =       5276
885629                 Wp   =           19
67372
 YDOT =       1067
946804  meter/sec      RA   =          316
70235  deg
 ZDOT =       5513
162701                 TA   =          316
47820
                                          MA   =          316
59951
                                          Ha   =            191
031  n
mi
                                          Hp   =            181
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10864972
67                 X    =         3382636
84
 Y    =      -17873743
55  feet           Y    =        -5410486
97  meter
 Z    =       -6969651
06                 Z    =        -2108090
13
 XDOT =      17312
616893                 XDOT =        5237
769512
 YDOT =       3503
762479  feet/sec       YDOT =        1126
736462  meter/sec
 ZDOT =      18087
804137                 ZDOT =        5538
702986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14752680
96                 X    =         4496617
16
 Y    =      -14858522
22  feet           Y    =        -4528877
57  meter
 Z    =       -6904860
42                 Z    =        -2104601
46
 XDOT =      14840
850781                 XDOT =        4523
491318
 YDOT =       6322
034257  feet/sec       YDOT =        1926
956042  meter/sec
 ZDOT =      18189
531492                 ZDOT =        5544
169199


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   10151
27835057  
00016717  00000-0  10270-3 0  9079
2 25544  51
6490 317
2778 0009671   6
1558 353
9723 15
74927014 20813


Satellite: ISS
Catalog Number: 25544
Epoch time:      10151
27835057   =   yrday
fracday
Element set:     907
Inclination:       51
6490  deg
RA of node:       317
2778  deg
Eccentricity:     
0009671     
Arg of perigee:     6
1558  deg
Mean anomaly:     353
9723  deg
Mean motion:   15
74927014  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2081
Checksum:              316


Coasting Arc #9 (Orbit 2096)
---------------------------------------

Vector Time (GMT): 2010/152/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4489846
29                 A    =         6718746
47  meter
 Y    =        -880856
22  meter          E    =           
0019105
 Z    =       -4936169
93                 I    =           51
38110
 XDOT =       3555
836900                 Wp   =           46
81655
 YDOT =      -6496
230514  meter/sec      RA   =          311
57932  deg
 ZDOT =      -2067
229608                 TA   =          203
01291
                                          MA   =          203
09861
                                          Ha   =            191
064  n
mi
                                          Hp   =            180
693

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14730466
83                 X    =        -4455683
73
 Y    =       -2889948
22  feet           Y    =         -930872
60  meter
 Z    =      -16194783
24                 Z    =        -4957898
72
 XDOT =      11666
131562                 XDOT =        3638
256852
 YDOT =     -21313
092238  feet/sec       YDOT =       -6456
005886  meter/sec
 ZDOT =      -6782
249371                 ZDOT =       -2049
756153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13670500
21                 X    =        -4166768
46
 Y    =       -5970349
79  feet           Y    =        -1819762
62  meter
 Z    =      -16281333
03                 Z    =        -4962550
31
 XDOT =      15580
579905                 XDOT =        4748
960755
 YDOT =     -17300
006376  feet/sec       YDOT =       -5273
041943  meter/sec
 ZDOT =      -6712
623497                 ZDOT =       -2046
007642


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   10152
29358264  
00016717  00000-0  10270-3 0  9083
2 25544  51
6488 312
0576 0009761   9
4181 350
7164 15
74965616 20978


Satellite: ISS
Catalog Number: 25544
Epoch time:      10152
29358264   =   yrday
fracday
Element set:     908
Inclination:       51
6488  deg
RA of node:       312
0576  deg
Eccentricity:     
0009761     
Arg of perigee:     9
4181  deg
Mean anomaly:     350
7164  deg
Mean motion:   15
74965616  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2097
Checksum:              325


Coasting Arc #10 (Orbit 2112)
---------------------------------------

Vector Time (GMT): 2010/153/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2887463
41                 A    =         6728559
74  meter
 Y    =        5895995
33  meter          E    =           
0014847
 Z    =        1469557
31                 I    =           51
39468
 XDOT =      -4993
891902                 Wp   =           79
53812
 YDOT =       -993
711090  meter/sec      RA   =          306
38813  deg
 ZDOT =      -5773
356103                 TA   =           84
22997
                                          MA   =           84
06073
                                          Ha   =            191
199  n
mi
                                          Hp   =            180
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9473305
14                 X    =        -2960317
72
 Y    =       19343816
71  feet           Y    =         5863298
45  meter
 Z    =        4821382
23                 Z    =         1455353
85
 XDOT =     -16384
159785                 XDOT =       -4954
363035
 YDOT =      -3260
206989  feet/sec       YDOT =       -1049
333988  meter/sec
 ZDOT =     -18941
457032                 ZDOT =       -5797
520493

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13147828
96                 X    =        -4007458
27
 Y    =       17076412
07  feet           Y    =         5204890
40  meter
 Z    =        4764790
28                 Z    =         1452308
08
 XDOT =     -14057
477008                 XDOT =       -4284
718992
 YDOT =      -5463
167952  feet/sec       YDOT =       -1665
173592  meter/sec
 ZDOT =     -19037
711314                 ZDOT =       -5802
694409


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   10153
30879859  
00016717  00000-0  10270-3 0  9095
2 25544  51
6488 306
8375 0009673  13
8761 346
2667 15
74948859 21138


Satellite: ISS
Catalog Number: 25544
Epoch time:      10153
30879859   =   yrday
fracday
Element set:     909
Inclination:       51
6488  deg
RA of node:       306
8375  deg
Eccentricity:     
0009673     
Arg of perigee:    13
8761  deg
Mean anomaly:     346
2667  deg
Mean motion:   15
74948859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2113
Checksum:              357


Coasting Arc #11 (Orbit 2128)
---------------------------------------

Vector Time (GMT): 2010/154/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4253714
52                 A    =         6717794
25  meter
 Y    =         881429
34  meter          E    =           
0009370
 Z    =        5117530
95                 I    =           51
34171
 XDOT =      -3010
425397                 Wp   =           41
74320
 YDOT =       6975
390602  meter/sec      RA   =          301
25043  deg
 ZDOT =       1306
388805                 TA   =           35
75410
                                          MA   =           35
69139
                                          Ha   =            191
126  n
mi
                                          Hp   =            180
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13955756
30                 X    =         4218682
06
 Y    =        2891828
55  feet           Y    =          928800
44  meter
 Z    =       16789799
72                 Z    =         5138110
49
 XDOT =      -9876
723745                 XDOT =       -3094
547926
 YDOT =      22885
139771  feet/sec       YDOT =        6941
255727  meter/sec
 ZDOT =       4286
052509                 ZDOT =        1291
560645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13102118
43                 X    =         3993525
70
 Y    =        5357315
96  feet           Y    =         1632909
90  meter
 Z    =       16871776
41                 Z    =         5142517
45
 XDOT =     -13497
332681                 XDOT =       -4113
987001
 YDOT =      19754
619768  feet/sec       YDOT =        6021
208105  meter/sec
 ZDOT =       4226
977875                 ZDOT =        1288
382856


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   10154
32399434  
00016717  00000-0  10270-3 0  9106
2 25544  51
6485 301
6168 0009810  16
9560 343
1929 15
74995455 21290


Satellite: ISS
Catalog Number: 25544
Epoch time:      10154
32399434   =   yrday
fracday
Element set:     910
Inclination:       51
6485  deg
RA of node:       301
6168  deg
Eccentricity:     
0009810     
Arg of perigee:    16
9560  deg
Mean anomaly:     343
1929  deg
Mean motion:   15
74995455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2129
Checksum:              320


Coasting Arc #12 (Orbit 2143)
---------------------------------------

Vector Time (GMT): 2010/155/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2340421
48                 A    =         6728982
27  meter
 Y    =       -6246085
53  meter          E    =           
0020000
 Z    =        -803676
14                 I    =           51
36419
 XDOT =       4787
840594                 Wp   =           29
49749
 YDOT =       1038
499030  meter/sec      RA   =          296
06768  deg
 ZDOT =       5951
546163                 TA   =          321
69353
                                          MA   =          321
83542
                                          Ha   =            191
261  n
mi
                                          Hp   =            180
236

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7678548
16                 X    =         2413996
51
 Y    =      -20492406
59  feet           Y    =        -6219502
08  meter
 Z    =       -2636732
76                 Z    =         -792128
30
 XDOT =      15708
138433                 XDOT =        4746
960495
 YDOT =       3407
149047  feet/sec       YDOT =        1091
810322  meter/sec
 ZDOT =      19526
070089                 ZDOT =        5974
706336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10958473
14                 X    =         3340142
61
 Y    =      -18948645
26  feet           Y    =        -5775547
08  meter
 Z    =       -2590733
23                 Z    =         -789655
49
 XDOT =      13438
410565                 XDOT =        4096
027540
 YDOT =       5125
887384  feet/sec       YDOT =        1562
370475  meter/sec
 ZDOT =      19618
328028                 ZDOT =        5979
666383


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   10155
27572422  
00016717  00000-0  10270-3 0  9112
2 25544  51
6478 296
7222 0009874  19
5147 340
6393 15
75028194 21449


Satellite: ISS
Catalog Number: 25544
Epoch time:      10155
27572422   =   yrday
fracday
Element set:     911
Inclination:       51
6478  deg
RA of node:       296
7222  deg
Eccentricity:     
0009874     
Arg of perigee:    19
5147  deg
Mean anomaly:     340
6393  deg
Mean motion:   15
75028194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2144
Checksum:              315


Coasting Arc #13 (Orbit 2159)
---------------------------------------

Vector Time (GMT): 2010/156/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4114922
83                 A    =         6717134
35  meter
 Y    =        -977134
00  meter          E    =           
0021310
 Z    =       -5235346
56                 I    =           51
31120
 XDOT =       2368
137542                 Wp   =           61
67235
 YDOT =      -7297
992799  meter/sec      RA   =          290
91406  deg
 ZDOT =       -490
774846                 TA   =          203
58776
                                          MA   =          203
68562
                                          Ha   =            191
278  n
mi
                                          Hp   =            179
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13500403
00                 X    =        -4078258
03
 Y    =       -3205820
22  feet           Y    =        -1022944
00  meter
 Z    =      -17176333
85                 Z    =        -5255247
98
 XDOT =       7769
480124                 XDOT =        2451
953117
 YDOT =     -23943
545927  feet/sec       YDOT =       -7271
042187  meter/sec
 ZDOT =      -1610
153695                 ZDOT =        -479
067514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12779720
63                 X    =        -3895258
85
 Y    =       -5146572
60  feet           Y    =        -1568675
33  meter
 Z    =      -17255611
84                 Z    =        -5259510
49
 XDOT =      10848
322284                 XDOT =        3306
568632
 YDOT =     -21603
318921  feet/sec       YDOT =       -6584
691607  meter/sec
 ZDOT =      -1563
526541                 ZDOT =        -476
562890


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   10156
29088564  
00016717  00000-0  10270-3 0  9125
2 25544  51
6466 291
5006 0009878  23
1387 337
0220 15
75069641 21609


Satellite: ISS
Catalog Number: 25544
Epoch time:      10156
29088564   =   yrday
fracday
Element set:     912
Inclination:       51
6466  deg
RA of node:       291
5006  deg
Eccentricity:     
0009878     
Arg of perigee:    23
1387  deg
Mean anomaly:     337
0220  deg
Mean motion:   15
75069641  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2160
Checksum:              308


Coasting Arc #14 (Orbit 2175)
---------------------------------------

Vector Time (GMT): 2010/157/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1799005
51                 A    =         6729125
68  meter
 Y    =        6484140
02  meter          E    =           
0013255
 Z    =          34868
41                 I    =           51
34208
 XDOT =      -4643
808110                 Wp   =           89
26887
 YDOT =      -1245
506364  meter/sec      RA   =          285
74402  deg
 ZDOT =      -6009
836714                 TA   =           90
35094
                                          MA   =           90
19905
                                          Ha   =            191
371  n
mi
                                          Hp   =            179
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5902249
05                 X    =        -1871548
02
 Y    =       21273425
28  feet           Y    =         6463616
86  meter
 Z    =         114397
67                 Z    =           25953
21
 XDOT =     -15235
590912                 XDOT =       -4600
340552
 YDOT =      -4086
306970  feet/sec       YDOT =       -1297
192550  meter/sec
 ZDOT =     -19717
312055                 ZDOT =       -6032
291065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8626159
57                 X    =        -2629253
44
 Y    =       20322189
84  feet           Y    =         6194203
46  meter
 Z    =          78897
11                 Z    =           24047
84
 XDOT =     -12975
102011                 XDOT =       -3954
811093
 YDOT =      -5394
286411  feet/sec       YDOT =       -1644
178498  meter/sec
 ZDOT =     -19806
761034                 ZDOT =       -6037
100763


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   10157
30602996  
00016717  00000-0  10270-3 0  9130
2 25544  51
6467 286
2801 0009838  27
0816 333
0859 15
75070412 21769


Satellite: ISS
Catalog Number: 25544
Epoch time:      10157
30602996   =   yrday
fracday
Element set:     913
Inclination:       51
6467  deg
RA of node:       286
2801  deg
Eccentricity:     
0009838     
Arg of perigee:    27
0816  deg
Mean anomaly:     333
0859  deg
Mean motion:   15
75070412  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2176
Checksum:              313


Coasting Arc #15 (Orbit 2191)
---------------------------------------

Vector Time (GMT): 2010/158/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4035674
42                 A    =         6717016
01  meter
 Y    =        1205050
92  meter          E    =           
0011938
 Z    =        5226650
98                 I    =           51
29378
 XDOT =      -1720
311893                 Wp   =           38
63284
 YDOT =       7503
986600  meter/sec      RA   =          280
57304  deg
 ZDOT =       -392
105964                 TA   =           55
16058
                                          MA   =           55
04836
                                          Ha   =            191
294  n
mi
                                          Hp   =            179
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13240401
63                 X    =         3996508
95
 Y    =        3953579
14  feet           Y    =         1249960
68  meter
 Z    =       17147805
04                 Z    =         5246161
51
 XDOT =      -5644
067889                 XDOT =       -1802
190167
 YDOT =      24619
378609  feet/sec       YDOT =        7484
291284  meter/sec
 ZDOT =      -1286
436891                 ZDOT =        -400
661405

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12606297
72                 X    =         3842399
55
 Y    =        5417439
86  feet           Y    =         1651235
67  meter
 Z    =       17225528
84                 Z    =         5250341
19
 XDOT =      -7994
667864                 XDOT =       -2436
774765
 YDOT =      22902
850266  feet/sec       YDOT =        6980
788761  meter/sec
 ZDOT =      -1320
498426                 ZDOT =        -402
487920


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   10158
32115546  
00016717  00000-0  10270-3 0  9144
2 25544  51
6460 281
0580 0009851  30
6197 329
5540 15
75097144 21922


Satellite: ISS
Catalog Number: 25544
Epoch time:      10158
32115546   =   yrday
fracday
Element set:     914
Inclination:       51
6460  deg
RA of node:       281
0580  deg
Eccentricity:     
0009851     
Arg of perigee:    30
6197  deg
Mean anomaly:     329
5540  deg
Mean motion:   15
75097144  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2192
Checksum:              300


Coasting Arc #16 (Orbit 2207)
---------------------------------------

Vector Time (GMT): 2010/159/06:34:51
266
Vector Time (MET): N/A
Weight (LBS)     : 816529
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1198224
80                 A    =         6728734
53  meter
 Y    =       -6569708
46  meter          E    =           
0023002
 Z    =         715787
99                 I    =           51
32820
 XDOT =       4650
558044                 Wp   =           44
68999
 YDOT =       1508
700445  meter/sec      RA   =          275
41521  deg
 ZDOT =       5962
669321                 TA   =          323
15563
                                          MA   =          323
31347
                                          Ha   =            191
384  n
mi
                                          Hp   =            179
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3931183
73                 X    =         1268122
20
 Y    =      -21554161
61  feet           Y    =        -6555918
47  meter
 Z    =        2348385
78                 Z    =          721778
01
 XDOT =      15257
736366                 XDOT =        4604
375859
 YDOT =       4949
804611  feet/sec       YDOT =        1560
446792  meter/sec
 ZDOT =      19562
563388                 ZDOT =        5985
150069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5972663
82                 X    =         1820467
93
 Y    =      -21077258
41  feet           Y    =        -6424348
36  meter
 Z    =        2372228
71                 Z    =          723055
31
 XDOT =      13058
546339                 XDOT =        3980
244924
 YDOT =       5948
644342  feet/sec       YDOT =        1813
146796  meter/sec
 ZDOT =      19652
122395                 ZDOT =        5989
966906


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   10159
33626303  
00016717  00000-0  10270-3 0  9155
2 25544  51
6450 275
8359 0009862  34
1791 326
0005 15
75134475 22082


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
33626303   =   yrday
fracday
Element set:     915
Inclination:       51
6450  deg
RA of node:       275
8359  deg
Eccentricity:     
0009862     
Arg of perigee:    34
1791  deg
Mean anomaly:     326
0005  deg
Mean motion:   15
75134475  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2208
Checksum:              301

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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