Date: March 17th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 29062 56 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 871)
---------------------------------------

Vector Time (GMT): 2010/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6538189
47                 A    =         6731013
51  meter
 Y    =        -248415
83  meter          E    =           
0010652
 Z    =       -1586131
66                 I    =           51
61275
 XDOT =       1572
175199                 Wp   =           96
13892
 YDOT =      -4859
805074  meter/sec      RA   =          351
10333  deg
 ZDOT =      -5753
640391                 TA   =          101
35291
                                          MA   =          101
23323
                                          Ha   =            192
604  n
mi
                                          Hp   =            181
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21450752
85                 X    =        -6527220
65
 Y    =        -815012
57  feet           Y    =         -321468
61  meter
 Z    =       -5203844
04                 Z    =        -1617867
16
 XDOT =       5158
055114                 XDOT =        1654
351398
 YDOT =     -15944
242368  feet/sec       YDOT =       -4841
765280  meter/sec
 ZDOT =     -18876
772936                 ZDOT =       -5745
802676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21111703
12                 X    =        -6434847
11
 Y    =       -3710425
48  feet           Y    =        -1130937
69  meter
 Z    =       -5329894
04                 Z    =        -1624551
70
 XDOT =       7110
633445                 XDOT =        2167
321074
 YDOT =     -13544
031516  feet/sec       YDOT =       -4128
220806  meter/sec
 ZDOT =     -18845
747513                 ZDOT =       -5744
183842


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   10074
52864055  
00016717  00000-0  10270-3 0  9004
2 25544  51
6478 351
4487 0007679  48
5410 311
6411 15
74002968  8722


Satellite: ISS
Catalog Number: 25544
Epoch time:      10074
52864055   =   yrday
fracday
Element set:     900
Inclination:       51
6478  deg
RA of node:       351
4487  deg
Eccentricity:     
0007679     
Arg of perigee:    48
5410  deg
Mean anomaly:     311
6411  deg
Mean motion:   15
74002968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             872
Checksum:              310


Coasting Arc #2 (Orbit 887)
---------------------------------------

Vector Time (GMT): 2010/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1028214
08                 A    =         6721021
09  meter
 Y    =        4356193
85  meter          E    =           
0013285
 Z    =        5007004
20                 I    =           51
54961
 XDOT =      -7474
727582                 Wp   =           52
51457
 YDOT =        365
374795  meter/sec      RA   =          345
93386  deg
 ZDOT =      -1841
573458                 TA   =           55
31314
                                          MA   =           55
18803
                                          Ha   =            192
551  n
mi
                                          Hp   =            181
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3373405
77                 X    =        -1101172
37
 Y    =       14291974
58  feet           Y    =         4344288
41  meter
 Z    =       16427179
12                 Z    =         5001831
43
 XDOT =     -24523
384455                 XDOT =       -7469
311752
 YDOT =       1198
736203  feet/sec       YDOT =         281
818011  meter/sec
 ZDOT =      -6041
907671                 ZDOT =       -1877
872338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5138564
62                 X    =        -1566234
50
 Y    =       13780675
03  feet           Y    =         4200349
75  meter
 Z    =       16406729
32                 Z    =         5000771
10
 XDOT =     -23452
093006                 XDOT =       -7148
197948
 YDOT =      -1335
852370  feet/sec       YDOT =        -407
167802  meter/sec
 ZDOT =      -6186
060103                 ZDOT =       -1885
511119


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   10075
54444932  
00016717  00000-0  10270-3 0  9016
2 25544  51
6473 346
2329 0007653  51
3781 308
8066 15
74087993  8881


Satellite: ISS
Catalog Number: 25544
Epoch time:      10075
54444932   =   yrday
fracday
Element set:     901
Inclination:       51
6473  deg
RA of node:       346
2329  deg
Eccentricity:     
0007653     
Arg of perigee:    51
3781  deg
Mean anomaly:     308
8066  deg
Mean motion:   15
74087993  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             888
Checksum:              331


Coasting Arc #3 (Orbit 903)
---------------------------------------

Vector Time (GMT): 2010/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6459316
57                 A    =         6730699
38  meter
 Y    =        -872271
98  meter          E    =           
0021759
 Z    =        1634952
34                 I    =           51
55376
 XDOT =       -775
996719                 Wp   =           60
51689
 YDOT =       5090
745285  meter/sec      RA   =          340
82246  deg
 ZDOT =       5735
349922                 TA   =          317
58171
                                          MA   =          317
74969
                                          Ha   =            192
526  n
mi
                                          Hp   =            181
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21191983
51                 X    =         6460648
11
 Y    =       -2861784
71  feet           Y    =         -800032
43  meter
 Z    =        5364016
87                 Z    =         1666334
97
 XDOT =      -2545
920994                 XDOT =        -860
725912
 YDOT =      16701
920228  feet/sec       YDOT =        5081
594518  meter/sec
 ZDOT =      18816
764837                 ZDOT =        5731
373768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21341148
72                 X    =         6504782
13
 Y    =        -702142
23  feet           Y    =         -214012
95  meter
 Z    =        5488626
53                 Z    =         1672933
37
 XDOT =      -4387
009501                 XDOT =       -1337
160496
 YDOT =      14790
843212  feet/sec       YDOT =        4508
249011  meter/sec
 ZDOT =      18801
083583                 ZDOT =        5730
570276


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   10076
56022854  
00016717  00000-0  10270-3 0  9025
2 25544  51
6476 341
0163 0007705  55
4003 304
7886 15
74094633  9046


Satellite: ISS
Catalog Number: 25544
Epoch time:      10076
56022854   =   yrday
fracday
Element set:     902
Inclination:       51
6476  deg
RA of node:       341
0163  deg
Eccentricity:     
0007705     
Arg of perigee:    55
4003  deg
Mean anomaly:     304
7886  deg
Mean motion:   15
74094633  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             904
Checksum:              295


Coasting Arc #4 (Orbit 918)
---------------------------------------

Vector Time (GMT): 2010/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         348724
44                 A    =         6720952
39  meter
 Y    =       -4511735
65  meter          E    =           
0019028
 Z    =       -4985402
46                 I    =           51
49366
 XDOT =       7265
035566                 Wp   =           87
70601
 YDOT =      -1585
400143  meter/sec      RA   =          335
64640  deg
 ZDOT =       1950
099712                 TA   =          201
16961
                                          MA   =          201
24845
                                          Ha   =            192
449  n
mi
                                          Hp   =            181
051

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1144109
07                 X    =          423367
78
 Y    =      -14802282
31  feet           Y    =        -4507419
13  meter
 Z    =      -16356307
28                 Z    =        -4983526
61
 XDOT =      23835
418525                 XDOT =        7272
750590
 YDOT =      -5201
444039  feet/sec       YDOT =       -1504
114873  meter/sec
 ZDOT =       6397
964934                 ZDOT =        1985
412196

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2482736
65                 X    =          756738
13
 Y    =      -14645581
69  feet           Y    =        -4463973
30  meter
 Z    =      -16348953
81                 Z    =        -4983161
12
 XDOT =      23082
948166                 XDOT =        7035
682601
 YDOT =      -3359
352286  feet/sec       YDOT =       -1023
930577  meter/sec
 ZDOT =       6538
159561                 ZDOT =        1992
831034


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   10077
51249022  
00016717  00000-0  10270-3 0  9030
2 25544  51
6480 336
1258 0007575  58
6158 301
5746 15
74161219  9193


Satellite: ISS
Catalog Number: 25544
Epoch time:      10077
51249022   =   yrday
fracday
Element set:     903
Inclination:       51
6480  deg
RA of node:       336
1258  deg
Eccentricity:     
0007575     
Arg of perigee:    58
6158  deg
Mean anomaly:     301
5746  deg
Mean motion:   15
74161219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             919
Checksum:              307


Coasting Arc #5 (Orbit 934)
---------------------------------------

Vector Time (GMT): 2010/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6212128
02                 A    =         6730191
90  meter
 Y    =        1863347
25  meter          E    =           
0011326
 Z    =       -1802256
82                 I    =           51
49814
 XDOT =         69
721999                 Wp   =          101
39891
 YDOT =      -5211
414613  meter/sec      RA   =          330
53214  deg
 ZDOT =      -5660
575571                 TA   =           98
60740
                                          MA   =           98
47905
                                          Ha   =            192
376  n
mi
                                          Hp   =            180
993

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20380997
44                 X    =        -6223747
53
 Y    =        6113343
99  feet           Y    =         1793814
44  meter
 Z    =       -5912916
07                 Z    =        -1832463
80
 XDOT =        228
746716                 XDOT =         155
489935
 YDOT =     -17097
816973  feet/sec       YDOT =       -5210
155816  meter/sec
 ZDOT =     -18571
442162                 ZDOT =       -5660
028134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20710111
46                 X    =        -6312441
97
 Y    =        4734647
22  feet           Y    =         1443120
47  meter
 Z    =       -6032827
43                 Z    =        -1838805
80
 XDOT =       1829
404698                 XDOT =         557
602552
 YDOT =     -15526
862439  feet/sec       YDOT =       -4732
587671  meter/sec
 ZDOT =     -18569
377044                 ZDOT =       -5659
946123


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   10078
52820620  
00016717  00000-0  10270-3 0  9042
2 25544  51
6479 330
9086 0007391  62
8496 297
3420 15
74178379  9354


Satellite: ISS
Catalog Number: 25544
Epoch time:      10078
52820620   =   yrday
fracday
Element set:     904
Inclination:       51
6479  deg
RA of node:       330
9086  deg
Eccentricity:     
0007391     
Arg of perigee:    62
8496  deg
Mean anomaly:     297
3420  deg
Mean motion:   15
74178379  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             935
Checksum:              330


Coasting Arc #6 (Orbit 950)
---------------------------------------

Vector Time (GMT): 2010/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         237656
17                 A    =         6720835
50  meter
 Y    =        4584365
28  meter          E    =           
0013792
 Z    =        4900704
77                 I    =           51
44174
 XDOT =      -6898
517042                 Wp   =           60
85175
 YDOT =       2676
814137  meter/sec      RA   =          325
34838  deg
 ZDOT =      -2158
307766                 TA   =           50
19119
                                          MA   =           50
06986
                                          Ha   =            192
224  n
mi
                                          Hp   =            180
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         779711
85                 X    =          162568
50
 Y    =       15040568
52  feet           Y    =         4586603
33  meter
 Z    =       16078427
72                 Z    =         4901676
67
 XDOT =     -22632
929927                 XDOT =       -6917
452235
 YDOT =       8782
198612  feet/sec       YDOT =        2599
564829  meter/sec
 ZDOT =      -7081
062224                 ZDOT =       -2191
867011

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         -66370
11                 X    =          -20229
61
 Y    =       15056396
98  feet           Y    =         4589189
80  meter
 Z    =       16082381
50                 Z    =         4901909
88
 XDOT =     -21903
091771                 XDOT =       -6676
062372
 YDOT =       7648
485805  feet/sec       YDOT =        2331
258473  meter/sec
 ZDOT =      -7214
267374                 ZDOT =       -2198
908696


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   10079
54388788  
00016717  00000-0  10270-3 0  9050
2 25544  51
6477 325
6912 0007399  64
8418 295
3512 15
74301686  9512


Satellite: ISS
Catalog Number: 25544
Epoch time:      10079
54388788   =   yrday
fracday
Element set:     905
Inclination:       51
6477  deg
RA of node:       325
6912  deg
Eccentricity:     
0007399     
Arg of perigee:    64
8418  deg
Mean anomaly:     295
3512  deg
Mean motion:   15
74301686  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             951
Checksum:              346


Coasting Arc #7 (Orbit 966)
---------------------------------------

Vector Time (GMT): 2010/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5792654
23                 A    =         6729588
99  meter
 Y    =       -2776996
74  meter          E    =           
0021534
 Z    =        1971131
44                 I    =           51
44699
 XDOT =        615
861542                 Wp   =           68
09258
 YDOT =       5277
112675  meter/sec      RA   =          320
23242  deg
 ZDOT =       5584
031522                 TA   =          313
93823
                                          MA   =          314
11573
                                          Ha   =            192
219  n
mi
                                          Hp   =            180
725

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19004771
10                 X    =         5813701
17
 Y    =       -9110881
69  feet           Y    =        -2712102
09  meter
 Z    =        6466966
66                 Z    =         1999323
41
 XDOT =       2020
543116                 XDOT =         529
679903
 YDOT =      17313
361795  feet/sec       YDOT =        5283
517941  meter/sec
 ZDOT =      18320
313393                 ZDOT =        5586
813853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19254346
93                 X    =         5868724
94
 Y    =       -8485275
48  feet           Y    =        -2586311
97  meter
 Z    =        6578857
96                 Z    =         2005235
91
 XDOT =        726
467890                 XDOT =         221
427413
 YDOT =      15963
062008  feet/sec       YDOT =        4865
541300  meter/sec
 ZDOT =      18331
470114                 ZDOT =        5587
432091


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   10080
55954052  
00016717  00000-0  10270-3 0  9067
2 25544  51
6475 320
4734 0007424  68
4763 291
7192 15
74297484  9678


Satellite: ISS
Catalog Number: 25544
Epoch time:      10080
55954052   =   yrday
fracday
Element set:     906
Inclination:       51
6475  deg
RA of node:       320
4734  deg
Eccentricity:     
0007424     
Arg of perigee:    68
4763  deg
Mean anomaly:     291
7192  deg
Mean motion:   15
74297484  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             967
Checksum:              329


Coasting Arc #8 (Orbit 981)
---------------------------------------

Vector Time (GMT): 2010/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -818369
63                 A    =         6721028
93  meter
 Y    =       -4625185
16  meter          E    =           
0018336
 Z    =       -4823510
16                 I    =           51
39603
 XDOT =       6341
534142                 Wp   =           93
86773
 YDOT =      -3621
151744  meter/sec      RA   =          315
04112  deg
 ZDOT =       2402
977111                 TA   =          199
67340
                                          MA   =          199
74423
                                          Ha   =            192
120  n
mi
                                          Hp   =            180
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2684939
72                 X    =         -743157
47
 Y    =      -15174491
98  feet           Y    =        -4633916
24  meter
 Z    =      -15825164
56                 Z    =        -4827302
98
 XDOT =      20805
558208                 XDOT =        6369
881989
 YDOT =     -11880
419106  feet/sec       YDOT =       -3550
078380  meter/sec
 ZDOT =       7883
783173                 ZDOT =        2433
853151

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2355937
93                 X    =         -718089
88
 Y    =      -15213273
57  feet           Y    =        -4637005
78  meter
 Z    =      -15840322
14                 Z    =        -4828130
19
 XDOT =      19831
363753                 XDOT =        6044
599672
 YDOT =     -11384
768519  feet/sec       YDOT =       -3470
077444  meter/sec
 ZDOT =       8006
317418                 ZDOT =        2440
325549


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   10081
51168314  
00016717  00000-0  10270-3 0  9073
2 25544  51
6473 315
5815 0007261  71
8269 288
3685 15
74364897  9828


Satellite: ISS
Catalog Number: 25544
Epoch time:      10081
51168314   =   yrday
fracday
Element set:     907
Inclination:       51
6473  deg
RA of node:       315
5815  deg
Eccentricity:     
0007261     
Arg of perigee:    71
8269  deg
Mean anomaly:     288
3685  deg
Mean motion:   15
74364897  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             982
Checksum:              335


Coasting Arc #9 (Orbit 997)
---------------------------------------

Vector Time (GMT): 2010/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5282970
55                 A    =         6728818
06  meter
 Y    =        3507614
99  meter          E    =           
0011272
 Z    =       -2255301
41                 I    =           51
40183
 XDOT =      -1215
086819                 Wp   =          102
57334
 YDOT =      -5308
906774  meter/sec      RA   =          309
92532  deg
 ZDOT =      -5435
755895                 TA   =          102
81506
                                          MA   =          102
68909
                                          Ha   =            192
043  n
mi
                                          Hp   =            180
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17332580
56                 X    =        -5310844
92
 Y    =       11507923
19  feet           Y    =         3448381
77  meter
 Z    =       -7399282
85                 Z    =        -2281033
69
 XDOT =      -3986
505313                 XDOT =       -1129
225634
 YDOT =     -17417
673144  feet/sec       YDOT =       -5322
014645  meter/sec
 ZDOT =     -17833
844801                 ZDOT =       -5441
450069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17269406
28                 X    =        -5263715
03
 Y    =       11536755
04  feet           Y    =         3516402
94  meter
 Z    =       -7501394
63                 Z    =        -2286425
08
 XDOT =      -3069
488888                 XDOT =        -935
580213
 YDOT =     -16152
253909  feet/sec       YDOT =       -4923
206991  meter/sec
 ZDOT =     -17856
571263                 ZDOT =       -5442
682921


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   10082
52727163  
00016717  00000-0  10270-3 0  9089
2 25544  51
6470 310
3638 0007104  76
1147 284
0806 15
74379215  9985


Satellite: ISS
Catalog Number: 25544
Epoch time:      10082
52727163   =   yrday
fracday
Element set:     908
Inclination:       51
6470  deg
RA of node:       310
3638  deg
Eccentricity:     
0007104     
Arg of perigee:    76
1147  deg
Mean anomaly:     284
0806  deg
Mean motion:   15
74379215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             998
Checksum:              308


Coasting Arc #10 (Orbit 1013)
---------------------------------------

Vector Time (GMT): 2010/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1320907
34                 A    =         6721240
65  meter
 Y    =        4643501
13  meter          E    =           
0014821
 Z    =        4666636
81                 I    =           51
35879
 XDOT =      -5711
094574                 Wp   =           69
73705
 YDOT =       4392
088314  meter/sec      RA   =          304
72616  deg
 ZDOT =      -2741
678419                 TA   =           47
41286
                                          MA   =           47
28791
                                          Ha   =            191
848  n
mi
                                          Hp   =            180
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4333685
50                 X    =         1246215
28
 Y    =       15234583
77  feet           Y    =         4657854
83  meter
 Z    =       15310488
21                 Z    =         4672872
13
 XDOT =     -18737
186922                 XDOT =       -5746
464800
 YDOT =      14409
738564  feet/sec       YDOT =        4328
025607  meter/sec
 ZDOT =      -8995
007936                 ZDOT =       -2769
508657

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4530415
73                 X    =         1380870
71
 Y    =       15152116
11  feet           Y    =         4618364
99  meter
 Z    =       15335355
63                 Z    =         4674216
40
 XDOT =     -17303
650603                 XDOT =       -5274
152704
 YDOT =      14429
343390  feet/sec       YDOT =        4398
063865  meter/sec
 ZDOT =      -9105
431125                 ZDOT =       -2775
335407


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   10083
54282547  
00016717  00000-0  10270-3 0  9095
2 25544  51
6470 305
1452 0007058  78
3758 281
8197 15
74493209 10149


Satellite: ISS
Catalog Number: 25544
Epoch time:      10083
54282547   =   yrday
fracday
Element set:     909
Inclination:       51
6470  deg
RA of node:       305
1452  deg
Eccentricity:     
0007058     
Arg of perigee:    78
3758  deg
Mean anomaly:     281
8197  deg
Mean motion:   15
74493209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1014
Checksum:              318


Coasting Arc #11 (Orbit 1029)
---------------------------------------

Vector Time (GMT): 2010/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4667862
44                 A    =         6727855
68  meter
 Y    =       -4115155
82  meter          E    =           
0020756
 Z    =        2533384
83                 I    =           51
36398
 XDOT =       1817
443549                 Wp   =           78
20981
 YDOT =       5324
526598  meter/sec      RA   =          299
61024  deg
 ZDOT =       5268
146628                 TA   =          310
65308
                                          MA   =          310
83335
                                          Ha   =            191
776  n
mi
                                          Hp   =            180
430

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15314509
31                 X    =         4701225
37
 Y    =      -13501167
38  feet           Y    =        -4062770
33  meter
 Z    =        8311630
01                 Z    =         2556142
23
 XDOT =       5962
741301                 XDOT =        1732
177318
 YDOT =      17468
919285  feet/sec       YDOT =        5344
373857  meter/sec
 ZDOT =      17283
945629                 ZDOT =        5276
768258

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14768351
17                 X    =         4501393
44
 Y    =      -14042884
96  feet           Y    =        -4280271
34  meter
 Z    =        8401910
18                 Z    =         2560902
22
 XDOT =       5463
323713                 XDOT =        1665
221068
 YDOT =      16169
596860  feet/sec       YDOT =        4928
493123  meter/sec
 ZDOT =      17318
314216                 ZDOT =        5278
622173


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   10084
55834852  
00016717  00000-0  10270-3 0  9101
2 25544  51
6458 299
9264 0006980  82
3488 277
8468 15
74517572 10308


Satellite: ISS
Catalog Number: 25544
Epoch time:      10084
55834852   =   yrday
fracday
Element set:     910
Inclination:       51
6458  deg
RA of node:       299
9264  deg
Eccentricity:     
0006980     
Arg of perigee:    82
3488  deg
Mean anomaly:     277
8468  deg
Mean motion:   15
74517572  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1030
Checksum:              343


Coasting Arc #12 (Orbit 1044)
---------------------------------------

Vector Time (GMT): 2010/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1843198
03                 A    =         6721748
26  meter
 Y    =       -4655125
14  meter          E    =           
0016551
 Z    =       -4500457
14                 I    =           51
32872
 XDOT =       4981
354422                 Wp   =          100
18967
 YDOT =      -4966
701106  meter/sec      RA   =          294
40363  deg
 ZDOT =       3104
044787                 TA   =          200
91343
                                          MA   =          200
98120
                                          Ha   =            191
762  n
mi
                                          Hp   =            180
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6047237
64                 X    =        -1769144
51
 Y    =      -15272720
26  feet           Y    =        -4675323
17  meter
 Z    =      -14765279
34                 Z    =        -4509231
03
 XDOT =      16343
026318                 XDOT =        5021
444063
 YDOT =     -16294
951136  feet/sec       YDOT =       -4910
772245  meter/sec
 ZDOT =      10183
873972                 ZDOT =        3128
341617

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6765245
83                 X    =        -2062046
93
 Y    =      -14933945
82  feet           Y    =        -4551866
69  meter
 Z    =      -14800245
01                 Z    =        -4511114
68
 XDOT =      14302
850883                 XDOT =        4359
508949
 YDOT =     -16645
480249  feet/sec       YDOT =       -5073
542380  meter/sec
 ZDOT =      10280
240313                 ZDOT =        3133
417247


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   10085
51037087  
00016717  00000-0  10270-3 0  9114
2 25544  51
6446 295
0331 0006983  85
9771 274
2190 15
74561343 10458


Satellite: ISS
Catalog Number: 25544
Epoch time:      10085
51037087   =   yrday
fracday
Element set:     911
Inclination:       51
6446  deg
RA of node:       295
0331  deg
Eccentricity:     
0006983     
Arg of perigee:    85
9771  deg
Mean anomaly:     274
2190  deg
Mean motion:   15
74561343  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1045
Checksum:              306


Coasting Arc #13 (Orbit 1060)
---------------------------------------

Vector Time (GMT): 2010/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4050819
78                 A    =         6726703
88  meter
 Y    =        4515700
82  meter          E    =           
0011242
 Z    =       -2913946
23                 I    =           51
33362
 XDOT =      -2371
009727                 Wp   =           98
48108
 YDOT =      -5343
402893  meter/sec      RA   =          289
28934  deg
 ZDOT =      -5002
623319                 TA   =          115
19803
                                          MA   =          115
08142
                                          Ha   =            191
658  n
mi
                                          Hp   =            180
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13290091
14                 X    =        -4086858
83
 Y    =       14815291
39  feet           Y    =         4470200
34  meter
 Z    =       -9560191
03                 Z    =        -2933712
87
 XDOT =      -7778
903304                 XDOT =       -2286
781068
 YDOT =     -17530
849388  feet/sec       YDOT =       -5369
446494  meter/sec
 ZDOT =     -16412
806165                 ZDOT =       -5013
936416

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12157332
00                 X    =        -3705554
79
 Y    =       15710311
35  feet           Y    =         4788502
90  meter
 Z    =       -9638569
92                 Z    =        -2937836
11
 XDOT =      -7752
219588                 XDOT =       -2362
876530
 YDOT =     -16060
121322  feet/sec       YDOT =       -4895
124979  meter/sec
 ZDOT =     -16457
882708                 ZDOT =       -5016
362649


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   10086
52582866  
00016717  00000-0  10270-3 0  9127
2 25544  51
6436 289
8144 0006914  89
4472 270
7483 15
74602780 10616


Satellite: ISS
Catalog Number: 25544
Epoch time:      10086
52582866   =   yrday
fracday
Element set:     912
Inclination:       51
6436  deg
RA of node:       289
8144  deg
Eccentricity:     
0006914     
Arg of perigee:    89
4472  deg
Mean anomaly:     270
7483  deg
Mean motion:   15
74602780  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1061
Checksum:              327


Coasting Arc #14 (Orbit 1076)
---------------------------------------

Vector Time (GMT): 2010/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2321178
07                 A    =         6722409
19  meter
 Y    =        4669929
68  meter          E    =           
0016473
 Z    =        4229656
53                 I    =           51
31088
 XDOT =      -4270
318074                 Wp   =           80
83713
 YDOT =       5348
806178  meter/sec      RA   =          284
07637  deg
 ZDOT =      -3547
754024                 TA   =           45
35722
                                          MA   =           45
22303
                                          Ha   =            191
458  n
mi
                                          Hp   =            180
277

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7615413
62                 X    =         2248238
80
 Y    =       15321291
59  feet           Y    =         4695479
14  meter
 Z    =       13876825
87                 Z    =         4240755
02
 XDOT =     -14010
229900                 XDOT =       -4312
577768
 YDOT =      17548
576698  feet/sec       YDOT =        5300
816242  meter/sec
 ZDOT =     -11639
612938                 ZDOT =       -3568
602352

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8846514
00                 X    =         2696417
47
 Y    =       14602969
04  feet           Y    =         4450984
96  meter
 Z    =       13921037
40                 Z    =         4243132
20
 XDOT =     -11286
230145                 XDOT =       -3440
042948
 YDOT =      18056
742072  feet/sec       YDOT =        5503
694983  meter/sec
 ZDOT =     -11722
256379                 ZDOT =       -3572
943744


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   10087
54125163  
00016717  00000-0  10270-3 0  9134
2 25544  51
6436 284
5942 0006758  93
2055 266
9882 15
74672601 10776


Satellite: ISS
Catalog Number: 25544
Epoch time:      10087
54125163   =   yrday
fracday
Element set:     913
Inclination:       51
6436  deg
RA of node:       284
5942  deg
Eccentricity:     
0006758     
Arg of perigee:    93
2055  deg
Mean anomaly:     266
9882  deg
Mean motion:   15
74672601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1077
Checksum:              324


Coasting Arc #15 (Orbit 1092)
---------------------------------------

Vector Time (GMT): 2010/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3407674
48                 A    =         6725372
56  meter
 Y    =       -4773526
40  meter          E    =           
0019424
 Z    =        3275026
36                 I    =           51
31402
 XDOT =       2960
503134                 Wp   =           91
59471
 YDOT =       5349
829499  meter/sec      RA   =          278
96179  deg
 ZDOT =       4692
773805                 TA   =          307
05674
                                          MA   =          307
23421
                                          Ha   =            191
362  n
mi
                                          Hp   =            180
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11180034
38                 X    =         3444890
16
 Y    =      -15661175
87  feet           Y    =        -4735211
29  meter
 Z    =       10744837
12                 Z    =         3291671
78
 XDOT =       9712
936791                 XDOT =        2877
663715
 YDOT =      17551
934052  feet/sec       YDOT =        5382
472976  meter/sec
 ZDOT =      15396
239519                 ZDOT =        4706
954075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9415824
11                 X    =         2869943
19
 Y    =      -16738756
80  feet           Y    =        -5101973
07  meter
 Z    =       10810800
16                 Z    =         3295131
89
 XDOT =      10186
405638                 XDOT =        3104
816438
 YDOT =      15761
772390  feet/sec       YDOT =        4804
188224  meter/sec
 ZDOT =      15452
713536                 ZDOT =        4709
987086


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   10088
55664121  
00016717  00000-0  10270-3 0  9149
2 25544  51
6423 279
3737 0006743  97
8248 262
3681 15
74730469 10936


Satellite: ISS
Catalog Number: 25544
Epoch time:      10088
55664121   =   yrday
fracday
Element set:     914
Inclination:       51
6423  deg
RA of node:       279
3737  deg
Eccentricity:     
0006743     
Arg of perigee:    97
8248  deg
Mean anomaly:     262
3681  deg
Mean motion:   15
74730469  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1093
Checksum:              329

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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