Date: June 4th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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


156/03:22:07 080 -1 3 14 0 14 0
N/A -12 0 0 0 190 9
000/00:04:10 159 -7 0 0 1 187 6

158/23:59:56 477 -0 7 2 6 2 6
N/A -2 2 0 0 191 2
000/00:09:52 954 -1 2 0 2 188 8

159/01:30:56 389 -0 7 2 7 2 7
N/A -2 2 0 0 191 1
000/00:09:52 778 -1 3 0 2 190 2

Coasting Arc #1 (Orbit 2116)
---------------------------------------

Vector Time (GMT): 2010/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816195
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4235814
36                 A    =         6728720
35  meter
 Y    =       -5178430
67  meter          E    =           
0021374
 Z    =         590592
99                 I    =           51
39065
 XDOT =       3399
210729                 Wp   =           35
83351
 YDOT =       3473
684475  meter/sec      RA   =          305
23981  deg
 ZDOT =       5986
552364                 TA   =          330
62787
                                          MA   =          330
74784
                                          Ha   =            190
683  n
mi
                                          Hp   =            180
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13897028
73                 X    =         4290536
70
 Y    =      -16989601
92  feet           Y    =        -5130757
37  meter
 Z    =        1937641
03                 Z    =          611302
79
 XDOT =      11152
266171                 XDOT =        3331
033201
 YDOT =      11396
602608  feet/sec       YDOT =        3511
314510  meter/sec
 ZDOT =      19640
919829                 ZDOT =        6002
900536

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11240442
42                 X    =        -3426086
85
 Y    =      -18844094
35  feet           Y    =        -5743679
96  meter
 Z    =        2020147
52                 Z    =          615740
96
 XDOT =      13101
891815                 XDOT =        3993
456625
 YDOT =      -5671
731210  feet/sec       YDOT =       -1728
743673  meter/sec
 ZDOT =      19706
034344                 ZDOT =        6006
399268


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
56226467  
00016717  00000-0  10270-3 0  9005
2 25544  51
6463 305
5315 0009247  13
9047 346
2370 15
75161414 21176


Satellite: ISS
Catalog Number: 25544
Epoch time:      10153
56226467   =   yrday
fracday
Element set:     900
Inclination:       51
6463  deg
RA of node:       305
5315  deg
Eccentricity:     
0009247     
Arg of perigee:    13
9047  deg
Mean anomaly:     346
2370  deg
Mean motion:   15
75161414  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2117
Checksum:              285


Coasting Arc #2 (Orbit 2131)
---------------------------------------

Vector Time (GMT): 2010/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816195
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2932560
90                 A    =         6717128
93  meter
 Y    =       -3171426
07  meter          E    =           
0018250
 Z    =       -5157595
38                 I    =           51
33563
 XDOT =       4574
957377                 Wp   =           68
37271
 YDOT =      -6076
022506  meter/sec      RA   =          300
06116  deg
 ZDOT =       1144
761323                 TA   =          212
55955
                                          MA   =          212
67223
                                          Ha   =            190
746  n
mi
                                          Hp   =            180
108

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9621262
80                 X    =        -2871824
84
 Y    =      -10404941
16  feet           Y    =        -3203879
54  meter
 Z    =      -16921244
70                 Z    =        -5171694
59
 XDOT =      15009
702679                 XDOT =        4636
999497
 YDOT =     -19934
457042  feet/sec       YDOT =       -6024
515840  meter/sec
 ZDOT =       3755
778620                 ZDOT =        1167
136471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12932461
04                 X    =        -3941814
12
 Y    =        5628424
45  feet           Y    =         1715543
77  meter
 Z    =      -16977405
87                 Z    =        -5174713
31
 XDOT =     -13580
205441                 XDOT =       -4139
246619
 YDOT =     -19702
975089  feet/sec       YDOT =       -6005
466807  meter/sec
 ZDOT =       3844
913758                 ZDOT =        1171
929713


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
51390013  
00016717  00000-0  10270-3 0  9011
2 25544  51
6465 300
6377 0009333  17
5691 342
5794 15
75200834 21329


Satellite: ISS
Catalog Number: 25544
Epoch time:      10154
51390013   =   yrday
fracday
Element set:     901
Inclination:       51
6465  deg
RA of node:       300
6377  deg
Eccentricity:     
0009333     
Arg of perigee:    17
5691  deg
Mean anomaly:     342
5794  deg
Mean motion:   15
75200834  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2132
Checksum:              284


Coasting Arc #3 (Orbit 2147)
---------------------------------------

Vector Time (GMT): 2010/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816195
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3765824
91                 A    =         6727682
65  meter
 Y    =        5392029
88  meter          E    =           
0008725
 Z    =       -1430242
23                 I    =           51
35719
 XDOT =      -3314
283612                 Wp   =           75
90748
 YDOT =      -3841
638609  meter/sec      RA   =          294
91799  deg
 ZDOT =      -5783
922501                 TA   =          119
87977
                                          MA   =          119
79305
                                          Ha   =            190
819  n
mi
                                          Hp   =            179
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12355068
60                 X    =        -3818891
81
 Y    =       17690386
74  feet           Y    =         5349621
61  meter
 Z    =       -4692395
77                 Z    =        -1448664
99
 XDOT =     -10873
633896                 XDOT =       -3242
982084
 YDOT =     -12603
801212  feet/sec       YDOT =       -3878
301642  meter/sec
 ZDOT =     -18976
123692                 ZDOT =       -5799
850527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13028880
49                 X    =         3971202
77
 Y    =       17179979
46  feet           Y    =         5236457
74  meter
 Z    =       -4765780
12                 Z    =        -1452609
78
 XDOT =     -14055
095290                 XDOT =       -4283
993044
 YDOT =       5401
961683  feet/sec       YDOT =        1646
517921  meter/sec
 ZDOT =     -19039
574019                 ZDOT =       -5803
262161


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
52894974  
00016717  00000-0  10270-3 0  9029
2 25544  51
6460 295
4150 0009470  20
7116 339
4429 15
75254287 21482


Satellite: ISS
Catalog Number: 25544
Epoch time:      10155
52894974   =   yrday
fracday
Element set:     902
Inclination:       51
6460  deg
RA of node:       295
4150  deg
Eccentricity:     
0009470     
Arg of perigee:    20
7116  deg
Mean anomaly:     339
4429  deg
Mean motion:   15
75254287  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2148
Checksum:              315


Coasting Arc #4 (Orbit 2157)
---------------------------------------

Vector Time (GMT): 2010/156/03:24:12
159
Vector Time (MET): N/A
Weight (LBS)     : 814961
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4630779
60                 A    =         6727404
24  meter
 Y    =        2026610
01  meter          E    =           
0006893
 Z    =       -4445809
34                 I    =           51
32602
 XDOT =         15
328751                 Wp   =           37
44274
 YDOT =      -6994
514573  meter/sec      RA   =          291
61746  deg
 ZDOT =      -3201
605823                 TA   =          200
32817
                                          MA   =          200
35563
                                          Ha   =            190
872  n
mi
                                          Hp   =            187
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15192846
45                 X    =        -4631500
32
 Y    =        6648982
97  feet           Y    =         1974822
28  meter
 Z    =      -14585988
65                 Z    =        -4468307
31
 XDOT =         50
291177                 XDOT =         109
094424
 YDOT =     -22947
882458  feet/sec       YDOT =       -6993
818568  meter/sec
 ZDOT =     -10503
956111                 ZDOT =       -3201
304293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13917538
02                 X    =        -4242065
59
 Y    =       -8871940
61  feet           Y    =        -2704167
50  meter
 Z    =      -14675606
57                 Z    =        -4473124
88
 XDOT =      18500
775642                 XDOT =        5639
036416
 YDOT =     -11634
126387  feet/sec       YDOT =       -3546
081723  meter/sec
 ZDOT =     -10502
762397                 ZDOT =       -3201
241979


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
16336347  
00016717  00000-0  10270-3 0  9036
2 25544  51
6488 292
1574 0005294 292
8655  67
1949 15
72629024 21581


Satellite: ISS
Catalog Number: 25544
Epoch time:      10156
16336347   =   yrday
fracday
Element set:     903
Inclination:       51
6488  deg
RA of node:       292
1574  deg
Eccentricity:     
0005294     
Arg of perigee:   292
8655  deg
Mean anomaly:      67
1949  deg
Mean motion:   15
72629024  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2158
Checksum:              331


Coasting Arc #5 (Orbit 2173)
---------------------------------------

Vector Time (GMT): 2010/157/03:24:12
159
Vector Time (MET): N/A
Weight (LBS)     : 814961
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         896146
57                 A    =         6731748
77  meter
 Y    =        5878178
47  meter          E    =           
0008372
 Z    =        3150604
50                 I    =           51
32995
 XDOT =      -4996
328398                 Wp   =           79
79980
 YDOT =       3344
710077  meter/sec      RA   =          286
42200  deg
 ZDOT =      -4806
892036                 TA   =           63
35383
                                          MA   =           63
26811
                                          Ha   =            191
012  n
mi
                                          Hp   =            187
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2940113
43                 X    =          815043
93
 Y    =       19285362
44  feet           Y    =         5887745
93  meter
 Z    =       10336628
94                 Z    =         3154761
60
 XDOT =     -16392
153537                 XDOT =       -5010
007017
 YDOT =      10973
458259  feet/sec       YDOT =        3288
762155  meter/sec
 ZDOT =     -15770
643164                 ZDOT =       -4831
197283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14213188
82                 X    =        -4332179
95
 Y    =       13349602
42  feet           Y    =         4068958
82  meter
 Z    =       10353199
90                 Z    =         3155655
33
 XDOT =     -17328
296032                 XDOT =       -5281
664630
 YDOT =      -6112
118706  feet/sec       YDOT =       -1862
973781  meter/sec
 ZDOT =     -15867
456237                 ZDOT =       -4836
400661


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
18008411  
00016717  00000-0  10270-3 0  9048
2 25544  51
6481 286
9474 0005279 296
7740  63
2883 15
72632846 21743


Satellite: ISS
Catalog Number: 25544
Epoch time:      10157
18008411   =   yrday
fracday
Element set:     904
Inclination:       51
6481  deg
RA of node:       286
9474  deg
Eccentricity:     
0005279     
Arg of perigee:   296
7740  deg
Mean anomaly:      63
2883  deg
Mean motion:   15
72632846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2174
Checksum:              325


Coasting Arc #6 (Orbit 2189)
---------------------------------------

Vector Time (GMT): 2010/158/03:24:12
159
Vector Time (MET): N/A
Weight (LBS)     : 814961
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3962715
75                 A    =         6729156
05  meter
 Y    =       -3750225
95  meter          E    =           
0006263
 Z    =        3932887
60                 I    =           51
31482
 XDOT =       1991
939406                 Wp   =           83
22741
 YDOT =       6283
793502  meter/sec      RA   =          281
32427  deg
 ZDOT =       3980
203527                 TA   =          325
28666
                                          MA   =          325
32752
                                          Ha   =            191
024  n
mi
                                          Hp   =            187
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13001035
92                 X    =         3985251
46
 Y    =      -12303890
92  feet           Y    =        -3705786
92  meter
 Z    =       12903174
56                 Z    =         3952193
03
 XDOT =       6535
234271                 XDOT =        1902
189518
 YDOT =      20616
120415  feet/sec       YDOT =        6305
566310  meter/sec
 ZDOT =      13058
410521                 ZDOT =        3989
663149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17533545
56                 X    =         5344224
69
 Y    =        3316199
22  feet           Y    =         1010777
52  meter
 Z    =       12980068
70                 Z    =         3956324
94
 XDOT =     -12731
879131                 XDOT =       -3880
676759
 YDOT =      15996
584387  feet/sec       YDOT =        4875
758921  meter/sec
 ZDOT =      13096
108741                 ZDOT =        3991
693944


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
19678008  
00016717  00000-0  10270-3 0  9056
2 25544  51
6487 281
7367 0005398 301
7779  58
2857 15
72672791 21900


Satellite: ISS
Catalog Number: 25544
Epoch time:      10158
19678008   =   yrday
fracday
Element set:     905
Inclination:       51
6487  deg
RA of node:       281
7367  deg
Eccentricity:     
0005398     
Arg of perigee:   301
7779  deg
Mean anomaly:      58
2857  deg
Mean motion:   15
72672791  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2190
Checksum:              350


Coasting Arc #7 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2010/159/00:04:52
954
Vector Time (MET): N/A
Weight (LBS)     : 814706
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4201123
65                 A    =         6726612
28  meter
 Y    =        1827774
36  meter          E    =           
0008121
 Z    =       -4932146
79                 I    =           51
29581
 XDOT =       -777
871100                 Wp   =           49
58714
 YDOT =      -7368
653058  meter/sec      RA   =          276
87840  deg
 ZDOT =      -2065
169733                 TA   =          200
27361
                                          MA   =          200
30588
                                          Ha   =            191
202  n
mi
                                          Hp   =            188
758

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13783214
06                 X    =        -4197290
11
 Y    =        5996635
05  feet           Y    =         1780816
92  meter
 Z    =      -16181583
97                 Z    =        -4952546
60
 XDOT =      -2552
070537                 XDOT =        -685
383317
 YDOT =     -24175
370924  feet/sec       YDOT =       -7376
834301  meter/sec
 ZDOT =      -6775
491251                 ZDOT =       -2068
724912

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2691510
30                 X    =         -820372
34
 Y    =      -14698842
94  feet           Y    =        -4480207
33  meter
 Z    =      -16262843
24                 Z    =        -4956914
62
 XDOT =      23034
265624                 XDOT =        7020
844162
 YDOT =       3304
981760  feet/sec       YDOT =        1007
358440  meter/sec
 ZDOT =      -6789
674339                 ZDOT =       -2069
492739


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
02283231  
00016717  00000-0  10270-3 0  9060
2 25544  51
6469 277
5025 0006437 287
0302  73
0154 15
72214414 22031


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
02283231   =   yrday
fracday
Element set:     906
Inclination:       51
6469  deg
RA of node:       277
5025  deg
Eccentricity:     
0006437     
Arg of perigee:   287
0302  deg
Mean anomaly:      73
0154  deg
Mean motion:   15
72214414  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              275


Coasting Arc #8 (Orbit 2203)
---------------------------------------

Vector Time (GMT): 2010/159/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4161732
78                 A    =         6728357
93  meter
 Y    =        2085134
66  meter          E    =           
0005741
 Z    =       -4863221
03                 I    =           51
29779
 XDOT =       -993
695046                 Wp   =           44
96856
 YDOT =      -7282
834745  meter/sec      RA   =          276
55526  deg
 ZDOT =      -2269
826702                 TA   =          202
80369
                                          MA   =          202
82920
                                          Ha   =            191
120  n
mi
                                          Hp   =            190
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13653978
92                 X    =        -4161114
84
 Y    =        6840992
98  feet           Y    =         2038599
73  meter
 Z    =      -15955449
57                 Z    =        -4883437
26
 XDOT =      -3260
154350                 XDOT =        -901
156657
 YDOT =     -23893
814779  feet/sec       YDOT =       -7293
429150  meter/sec
 ZDOT =      -7446
938000                 ZDOT =       -2274
430244

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8991287
48                 X    =        -2740544
42
 Y    =      -12239725
93  feet           Y    =        -3730668
46  meter
 Z    =      -16035976
90                 Z    =        -4887765
76
 XDOT =      22139
143595                 XDOT =        6748
010968
 YDOT =      -6472
528397  feet/sec       YDOT =       -1972
826655  meter/sec
 ZDOT =      -7465
297242                 ZDOT =       -2275
422599


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
08639845  
00016717  00000-0  10270-3 0  9073
2 25544  51
6481 277
1777 0007775 274
0264  86
0009 15
71706171 22043


Satellite: ISS
Catalog Number: 25544
Epoch time:      10159
08639845   =   yrday
fracday
Element set:     907
Inclination:       51
6481  deg
RA of node:       277
1777  deg
Eccentricity:     
0007775     
Arg of perigee:   274
0264  deg
Mean anomaly:      86
0009  deg
Mean motion:   15
71706171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2204
Checksum:              320


Coasting Arc #9 (Orbit 2219)
---------------------------------------

Vector Time (GMT): 2010/160/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1977173
46                 A    =         6735652
70  meter
 Y    =        5867355
83  meter          E    =           
0005926
 Z    =        2644600
01                 I    =           51
31986
 XDOT =      -4247
320559                 Wp   =          107
88982
 YDOT =       3774
395392  meter/sec      RA   =          271
37325  deg
 ZDOT =      -5190
778800                 TA   =           41
90004
                                          MA   =           41
85470
                                          Ha   =            191
609  n
mi
                                          Hp   =            190
541

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6486789
55                 X    =         1898569
49
 Y    =       19249855
09  feet           Y    =         5889025
89  meter
 Z    =        8676509
23                 Z    =         2654015
17
 XDOT =     -13934
778737                 XDOT =       -4263
994609
 YDOT =      12383
186982  feet/sec       YDOT =        3726
806832  meter/sec
 ZDOT =     -17030
114174                 ZDOT =       -5211
452568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17752151
97                 X    =        -5410855
92
 Y    =        9840928
56  feet           Y    =         2999515
03  meter
 Z    =        8714034
52                 Z    =         2656037
72
 XDOT =     -13982
034865                 XDOT =       -4261
724227
 YDOT =     -10047
018435  feet/sec       YDOT =       -3062
331219  meter/sec
 ZDOT =     -17112
461726                 ZDOT =       -5215
878334


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   10160
10371707  
00016717  00000-0  10270-3 0  9089
2 25544  51
6479 271
9719 0007811 277
7873  82
2402 15
71706658 22208


Satellite: ISS
Catalog Number: 25544
Epoch time:      10160
10371707   =   yrday
fracday
Element set:     908
Inclination:       51
6479  deg
RA of node:       271
9719  deg
Eccentricity:     
0007811     
Arg of perigee:   277
7873  deg
Mean anomaly:      82
2402  deg
Mean motion:   15
71706658  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2220
Checksum:              311


Coasting Arc #10 (Orbit 2235)
---------------------------------------

Vector Time (GMT): 2010/161/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3032617
16                 A    =         6731128
04  meter
 Y    =       -4362345
96  meter          E    =           
0002541
 Z    =        4131595
40                 I    =           51
30601
 XDOT =       3357
106058                 Wp   =          112
83331
 YDOT =       5848
813480  meter/sec      RA   =          266
27916  deg
 ZDOT =       3708
549309                 TA   =          299
02868
                                          MA   =          299
05413
                                          Ha   =            191
822  n
mi
                                          Hp   =            190
476

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9949531
37                 X    =         3061101
47
 Y    =      -14312158
65  feet           Y    =        -4328274
85  meter
 Z    =       13555103
01                 Z    =         4146396
53
 XDOT =      11014
127486                 XDOT =        3273
438330
 YDOT =      19189
020603  feet/sec       YDOT =        5885
886209  meter/sec
 ZDOT =      12167
156525                 ZDOT =        3724
656121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15992313
86                 X    =         4874457
26
 Y    =        6817274
37  feet           Y    =         2077905
23  meter
 Z    =       13614056
89                 Z    =         4149564
54
 XDOT =     -16124
966425                 XDOT =       -4914
889766
 YDOT =      13382
690230  feet/sec       YDOT =        4079
043982  meter/sec
 ZDOT =      12231
343977                 ZDOT =        3728
113644


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   10161
12101320  
00016717  00000-0  10270-3 0  9095
2 25544  51
6484 266
7654 0007846 282
6482  77
3803 15
71747063 22365


Satellite: ISS
Catalog Number: 25544
Epoch time:      10161
12101320   =   yrday
fracday
Element set:     909
Inclination:       51
6484  deg
RA of node:       266
7654  deg
Eccentricity:     
0007846     
Arg of perigee:   282
6482  deg
Mean anomaly:      77
3803  deg
Mean motion:   15
71747063  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2236
Checksum:              304


Coasting Arc #11 (Orbit 2250)
---------------------------------------

Vector Time (GMT): 2010/162/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3711812
62                 A    =         6732216
21  meter
 Y    =       -4156775
74  meter          E    =           
0001789
 Z    =       -3775058
38                 I    =           51
31377
 XDOT =       2448
376771                 Wp   =          295
05040
 YDOT =      -5981
406202  meter/sec      RA   =          261
08625  deg
 ZDOT =       4178
062121                 TA   =           19
01957
                                          MA   =           19
01289
                                          Ha   =            192
023  n
mi
                                          Hp   =            190
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12177862
94                 X    =        -3646716
16
 Y    =      -13637715
68  feet           Y    =        -4197918
75  meter
 Z    =      -12385362
12                 Z    =        -3792933
25
 XDOT =       8032
732187                 XDOT =        2494
783451
 YDOT =     -19624
036096  feet/sec       YDOT =       -5953
768315  meter/sec
 ZDOT =      13707
552890                 ZDOT =        4190
068070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10698056
14                 X    =         3260767
51
 Y    =      -14767182
05  feet           Y    =        -4501037
09  meter
 Z    =      -12456595
00                 Z    =        -3796770
16
 XDOT =      19801
908223                 XDOT =        6035
621626
 YDOT =       2740
154693  feet/sec       YDOT =         835
199151  meter/sec
 ZDOT =      13755
368612                 ZDOT =        4192
636353


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   10162
07470838  
00016717  00000-0  10270-3 0  9105
2 25544  51
6489 261
8848 0007971 286
7862  73
2425 15
71790673 22514


Satellite: ISS
Catalog Number: 25544
Epoch time:      10162
07470838   =   yrday
fracday
Element set:     910
Inclination:       51
6489  deg
RA of node:       261
8848  deg
Eccentricity:     
0007971     
Arg of perigee:   286
7862  deg
Mean anomaly:      73
2425  deg
Mean motion:   15
71790673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2251
Checksum:              333


Coasting Arc #12 (Orbit 2266)
---------------------------------------

Vector Time (GMT): 2010/163/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1111374
72                 A    =         6734195
85  meter
 Y    =        5863122
76  meter          E    =           
0003648
 Z    =       -3119915
03                 I    =           51
32642
 XDOT =      -4859
088445                 Wp   =          299
19610
 YDOT =      -3496
222324  meter/sec      RA   =          255
99596  deg
 ZDOT =      -4833
389486                 TA   =          277
20595
                                          MA   =          277
24741
                                          Ha   =            192
351  n
mi
                                          Hp   =            190
111

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3646242
51                 X    =        -1161698
52
 Y    =       19235967
07  feet           Y    =         5850413
98  meter
 Z    =      -10235941
69                 Z    =        -3125435
16
 XDOT =     -15941
891225                 XDOT =       -4796
152009
 YDOT =     -11470
545684  feet/sec       YDOT =       -3550
206653  meter/sec
 ZDOT =     -15857
577054                 ZDOT =       -4856
842968

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19541689
10                 X    =        -5956306
84
 Y    =         994765
52  feet           Y    =          303204
53  meter
 Z    =      -10257916
17                 Z    =        -3126612
85
 XDOT =       7535
375737                 XDOT =        2296
782525
 YDOT =     -16659
528881  feet/sec       YDOT =       -5077
824403  meter/sec
 ZDOT =     -15951
045873                 ZDOT =       -4861
878782


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   10163
09196306  
00016717  00000-0  10270-3 0  9114
2 25544  51
6490 256
6789 0008103 290
2807  69
7483 15
71803765 22677


Satellite: ISS
Catalog Number: 25544
Epoch time:      10163
09196306   =   yrday
fracday
Element set:     911
Inclination:       51
6490  deg
RA of node:       256
6789  deg
Eccentricity:     
0008103     
Arg of perigee:   290
2807  deg
Mean anomaly:      69
7483  deg
Mean motion:   15
71803765  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2267
Checksum:              325


Coasting Arc #13 (Orbit 2282)
---------------------------------------

Vector Time (GMT): 2010/164/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4547791
38                 A    =         6728906
69  meter
 Y    =        1864343
78  meter          E    =           
0007086
 Z    =        4598987
74                 I    =           51
31768
 XDOT =         20
347604                 Wp   =             
32795
 YDOT =       7125
750197  meter/sec      RA   =          250
80790  deg
 ZDOT =      -2901
758310                 TA   =          118
59819
                                          MA   =          118
52687
                                          Ha   =            192
460  n
mi
                                          Hp   =            189
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14920575
41                 X    =         4504264
87
 Y    =        6116613
46  feet           Y    =         1914955
55  meter
 Z    =       15088542
47                 Z    =         4620975
62
 XDOT =         66
757231                 XDOT =         -45
239098
 YDOT =      23378
445529  feet/sec       YDOT =        7125
611633  meter/sec
 ZDOT =      -9520
204430                 ZDOT =       -2901
817270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2220155
22                 X    =         -676703
31
 Y    =       15888838
87  feet           Y    =         4842918
09  meter
 Z    =       15176177
20                 Z    =         4625698
81
 XDOT =     -21448
319188                 XDOT =       -6537
447688
 YDOT =       6118
241445  feet/sec       YDOT =        1864
839992  meter/sec
 ZDOT =      -9520
407303                 ZDOT =       -2901
820146


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   10164
10919544  
00016717  00000-0  10270-3 0  9125
2 25544  51
6487 251
4726 0008167 295
4960  64
5357 15
71892183 22837


Satellite: ISS
Catalog Number: 25544
Epoch time:      10164
10919544   =   yrday
fracday
Element set:     912
Inclination:       51
6487  deg
RA of node:       251
4726  deg
Eccentricity:     
0008167     
Arg of perigee:   295
4960  deg
Mean anomaly:      64
5357  deg
Mean motion:   15
71892183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2283
Checksum:              326


Coasting Arc #14 (Orbit 2298)
---------------------------------------

Vector Time (GMT): 2010/165/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1177285
73                 A    =         6736634
47  meter
 Y    =       -6340970
38  meter          E    =           
0011163
 Z    =        1920618
76                 I    =           51
35394
 XDOT =       5238
096761                 Wp   =           31
97016
 YDOT =        724
688448  meter/sec      RA   =          245
70621  deg
 ZDOT =       5597
883125                 TA   =          349
46437
                                          MA   =          349
48774
                                          Ha   =            192
688  n
mi
                                          Hp   =            189
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3862486
01                 X    =        -1115622
34
 Y    =      -20803708
59  feet           Y    =        -6353791
10  meter
 Z    =        6301242
66                 Z    =         1915048
02
 XDOT =      17185
356827                 XDOT =        5202
410465
 YDOT =       2377
586773  feet/sec       YDOT =         783
063297  meter/sec
 ZDOT =      18365
758285                 ZDOT =        5623
243169

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19013736
14                 X    =         5795386
77
 Y    =       -9298962
54  feet           Y    =        -2834323
78  meter
 Z    =        6279003
28                 Z    =         1913840
20
 XDOT =       1577
255385                 XDOT =         480
747441
 YDOT =      15706
761781  feet/sec       YDOT =        4787
420991  meter/sec
 ZDOT =      18466
839980                 ZDOT =        5628
692826


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   10165
12640880  
00016717  00000-0  10270-3 0  9133
2 25544  51
6481 246
2655 0008182 299
7515  60
2833 15
71878883 22994


Satellite: ISS
Catalog Number: 25544
Epoch time:      10165
12640880   =   yrday
fracday
Element set:     913
Inclination:       51
6481  deg
RA of node:       246
2655  deg
Eccentricity:     
0008182     
Arg of perigee:   299
7515  deg
Mean anomaly:      60
2833  deg
Mean motion:   15
71878883  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2299
Checksum:              331


Coasting Arc #15 (Orbit 2313)
---------------------------------------

Vector Time (GMT): 2010/166/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4356675
01                 A    =         6726684
83  meter
 Y    =         581075
77  meter          E    =           
0007029
 Z    =       -5097612
92                 I    =           51
33384
 XDOT =      -2650
932176                 Wp   =           75
06169
 YDOT =      -7072
216382  meter/sec      RA   =          240
53584  deg
 ZDOT =       1462
924221                 TA   =          209
01468
                                          MA   =          209
05377
                                          Ha   =            192
716  n
mi
                                          Hp   =            189
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14293553
17                 X    =        -4338085
83
 Y    =        1906416
57  feet           Y    =          532461
71  meter
 Z    =      -16724451
85                 Z    =        -5118732
23
 XDOT =      -8697
284042                 XDOT =       -2578
758911
 YDOT =     -23202
809653  feet/sec       YDOT =       -7101
457412  meter/sec
 ZDOT =       4799
620149                 ZDOT =        1450
220099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5842963
66                 X    =        -1780935
32
 Y    =      -13075817
89  feet           Y    =        -3985509
29  meter
 Z    =      -16808632
85                 Z    =        -5123271
29
 XDOT =      18833
655080                 XDOT =        5740
498068
 YDOT =     -14505
953881  feet/sec       YDOT =       -4421
414743  meter/sec
 ZDOT =       4748
928412                 ZDOT =        1447
473380


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   10166
08002550  
00016717  00000-0  10270-3 0  9146
2 25544  51
6474 241
3840 0008246 303
1181  56
9189 15
71932743 23148


Satellite: ISS
Catalog Number: 25544
Epoch time:      10166
08002550   =   yrday
fracday
Element set:     914
Inclination:       51
6474  deg
RA of node:       241
3840  deg
Eccentricity:     
0008246     
Arg of perigee:   303
1181  deg
Mean anomaly:      56
9189  deg
Mean motion:   15
71932743  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2314
Checksum:              288


Coasting Arc #16 (Orbit 2329)
---------------------------------------

Vector Time (GMT): 2010/167/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3377577
29                 A    =         6737961
79  meter
 Y    =        5792899
83  meter          E    =           
0003474
 Z    =        -635415
91                 I    =           51
38706
 XDOT =      -4451
028346                 Wp   =          173
33243
 YDOT =       1941
300289  meter/sec      RA   =          235
41521  deg
 ZDOT =      -5968
008019                 TA   =           13
60179
                                          MA   =           13
59243
                                          Ha   =            192
975  n
mi
                                          Hp   =            189
139

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11081290
31                 X    =         3315635
71
 Y    =       19005576
87  feet           Y    =         5830323
68  meter
 Z    =       -2084697
88                 Z    =         -619157
33
 XDOT =     -14603
111373                 XDOT =       -4443
414288
 YDOT =       6369
095435  feet/sec       YDOT =        1891
569760  meter/sec
 ZDOT =     -19580
078802                 ZDOT =       -5989
612105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14813908
33                 X    =        -4515279
26
 Y    =       16273331
47  feet           Y    =         4960111
43  meter
 Z    =       -2019830
50                 Z    =         -615644
34
 XDOT =      -9225
962510                 XDOT =       -2812
073373
 YDOT =     -10836
709405  feet/sec       YDOT =       -3303
029027  meter/sec
 ZDOT =     -19666
188017                 ZDOT =       -5994
254108


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   10167
09719815  
00016717  00000-0  10270-3 0  9158
2 25544  51
6470 236
1776 0008190 306
1256  53
9148 15
71910427 23303


Satellite: ISS
Catalog Number: 25544
Epoch time:      10167
09719815   =   yrday
fracday
Element set:     915
Inclination:       51
6470  deg
RA of node:       236
1776  deg
Eccentricity:     
0008190     
Arg of perigee:   306
1256  deg
Mean anomaly:      53
9148  deg
Mean motion:   15
71910427  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2330
Checksum:              305


Coasting Arc #17 (Orbit 2345)
---------------------------------------

Vector Time (GMT): 2010/168/01:35:52
778
Vector Time (MET): N/A
Weight (LBS)     : 814451
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3222516
58                 A    =         6725878
70  meter
 Y    =       -2695141
76  meter          E    =           
0006597
 Z    =        5255826
77                 I    =           51
36467
 XDOT =       4927
760829                 Wp   =          324
35317
 YDOT =       5910
607655  meter/sec      RA   =          230
26979  deg
 ZDOT =         14
829709                 TA   =          125
53624
                                          MA   =          125
47471
                                          Ha   =            193
042  n
mi
                                          Hp   =            188
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10572560
96                 X    =         3226883
01
 Y    =       -8842328
60  feet           Y    =        -2659081
95  meter
 Z    =       17243526
16                 Z    =         5271491
87
 XDOT =      16167
194320                 XDOT =        4861
229061
 YDOT =      19391
757398  feet/sec       YDOT =        5965
340813  meter/sec
 ZDOT =         48
653902                 ZDOT =          38
607760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11694956
20                 X    =         3564622
65
 Y    =        7144017
07  feet           Y    =         2177496
40  meter
 Z    =       17305953
73                 Z    =         5274854
70
 XDOT =     -12775
855342                 XDOT =       -3894
080708
 YDOT =      20608
671320  feet/sec       YDOT =        6281
523018  meter/sec
 ZDOT =        143
516529                 ZDOT =          43
743838


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   10168
11434846  
00016717  00000-0  10270-3 0  9161
2 25544  51
6466 230
9695 0008276 311
1744  48
8704 15
71973461 23468


Satellite: ISS
Catalog Number: 25544
Epoch time:      10168
11434846   =   yrday
fracday
Element set:     916
Inclination:       51
6466  deg
RA of node:       230
9695  deg
Eccentricity:     
0008276     
Arg of perigee:   311
1744  deg
Mean anomaly:      48
8704  deg
Mean motion:   15
71973461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2346
Checksum:              323

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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