Date: May 24th 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


143/15:22:00 000 0 0 0 0 0 0
N/A 0 0 0 0 191 6
000/00:00:00 000 0 0 0 0 183 0

146/06:34:55 368 1 4 -2 4 2 4
N/A -1 5 0 0 190 5
000/00:09:46 736 -1 3 0 1 182 4

Coasting Arc #1 (Orbit 1926)
---------------------------------------

Vector Time (GMT): 2010/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6250731
73                 A    =         6729610
55  meter
 Y    =       -1021521
52  meter          E    =           
0014226
 Z    =       -2248654
45                 I    =           51
70298
 XDOT =       2729
775135                 Wp   =             
47364
 YDOT =       4688
893631  meter/sec      RA   =            7
00010  deg
 ZDOT =       5472
252683                 TA   =          334
29271
                                          MA   =          334
36335
                                          Ha   =            191
596  n
mi
                                          Hp   =            183
648

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20507650
05                 X    =         6272613
60
 Y    =       -3351448
56  feet           Y    =         -951499
63  meter
 Z    =       -7377475
22                 Z    =        -2218235
19
 XDOT =       8955
955166                 XDOT =        2650
556882
 YDOT =      15383
509287  feet/sec       YDOT =        4718
976330  meter/sec
 ZDOT =      17953
584918                 ZDOT =        5485
321850

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7964921
58                 X    =         2427708
10
 Y    =      -19238738
69  feet           Y    =        -5863967
55  meter
 Z    =       -7256308
73                 Z    =        -2211722
90
 XDOT =      16335
869193                 XDOT =        4979
172930
 YDOT =        -10
236758  feet/sec       YDOT =          -3
120164  meter/sec
 ZDOT =      18005
633150                 ZDOT =        5488
116984


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   10141
50437152  
00016717  00000-0  10270-3 0  9001
2 25544  51
6476   7
5061 0010505 338
1206  21
9508 15
74152520 19270


Satellite: ISS
Catalog Number: 25544
Epoch time:      10141
50437152   =   yrday
fracday
Element set:     900
Inclination:       51
6476  deg
RA of node:         7
5061  deg
Eccentricity:     
0010505     
Arg of perigee:   338
1206  deg
Mean anomaly:      21
9508  deg
Mean motion:   15
74152520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1927
Checksum:              265


Coasting Arc #2 (Orbit 1942)
---------------------------------------

Vector Time (GMT): 2010/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2650206
07                 A    =         6721541
43  meter
 Y    =       -3894089
81  meter          E    =           
0015769
 Z    =       -4807055
40                 I    =           51
64534
 XDOT =       7069
422994                 Wp   =           30
25425
 YDOT =      -1732
005155  meter/sec      RA   =            1
90506  deg
 ZDOT =      -2484
586139                 TA   =          215
36512
                                          MA   =          215
46981
                                          Ha   =            191
575  n
mi
                                          Hp   =            183
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8694901
81                 X    =        -2583112
68
 Y    =      -12775885
20  feet           Y    =        -3923350
58  meter
 Z    =      -15771179
14                 Z    =        -4819767
46
 XDOT =      23193
644993                 XDOT =        7100
334941
 YDOT =      -5682
431611  feet/sec       YDOT =       -1652
777678  meter/sec
 ZDOT =      -8151
529329                 ZDOT =       -2450
167602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15378346
99                 X    =        -4687320
16
 Y    =         855350
49  feet           Y    =          260710
83  meter
 Z    =      -15821803
66                 Z    =        -4822485
75
 XDOT =       7068
587926                 XDOT =        2154
505600
 YDOT =     -21755
751751  feet/sec       YDOT =       -6631
153134  meter/sec
 ZDOT =      -8014
436965                 ZDOT =       -2442
800387


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   10142
52009207  
00016717  00000-0  10270-3 0  9011
2 25544  51
6468   2
2889 0010494 341
6611  18
4173 15
74191751 19433


Satellite: ISS
Catalog Number: 25544
Epoch time:      10142
52009207   =   yrday
fracday
Element set:     901
Inclination:       51
6468  deg
RA of node:         2
2889  deg
Eccentricity:     
0010494     
Arg of perigee:   341
6611  deg
Mean anomaly:      18
4173  deg
Mean motion:   15
74191751  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1943
Checksum:              288


Coasting Arc #3 (Orbit 1958)
---------------------------------------

Vector Time (GMT): 2010/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 794797
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6080847
07                 A    =         6729667
41  meter
 Y    =        1996861
09  meter          E    =           
0011762
 Z    =        2081004
25                 I    =           51
64325
 XDOT =      -3287
987183                 Wp   =           63
31386
 YDOT =      -4205
728600  meter/sec      RA   =          356
73071  deg
 ZDOT =      -5542
841984                 TA   =           93
46289
                                          MA   =           93
32834
                                          Ha   =            191
709  n
mi
                                          Hp   =            183
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19950285
67                 X    =        -6112833
67
 Y    =        6551381
52  feet           Y    =         1928682
45  meter
 Z    =        6827441
77                 Z    =         2051385
53
 XDOT =     -10787
359523                 XDOT =       -3213
787110
 YDOT =     -13798
322177  feet/sec       YDOT =       -4242
081597  meter/sec
 ZDOT =     -18185
177114                 ZDOT =       -5558
635279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4242704
82                 X    =        -1293176
43
 Y    =       20604148
09  feet           Y    =         6280144
34  meter
 Z    =        6709470
66                 Z    =         2045046
66
 XDOT =     -15778
563893                 XDOT =       -4809
306275
 YDOT =       2724
970011  feet/sec       YDOT =         830
570859  meter/sec
 ZDOT =     -18248
068668                 ZDOT =       -5562
011330


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   10143
53579521  
00016717  00000-0  10270-3 0  9025
2 25544  51
6473 357
0720 0010578 345
8232  14
2633 15
74243056 19590


Satellite: ISS
Catalog Number: 25544
Epoch time:      10143
53579521   =   yrday
fracday
Element set:     902
Inclination:       51
6473  deg
RA of node:       357
0720  deg
Eccentricity:     
0010578     
Arg of perigee:   345
8232  deg
Mean anomaly:      14
2633  deg
Mean motion:   15
74243056  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1959
Checksum:              299


Coasting Arc #4 (Orbit 1960)
---------------------------------------

Vector Time (GMT): 2010/143/15:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816784
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4351321
15                 A    =         6723891
49  meter
 Y    =       -3006403
89  meter          E    =           
0013687
 Z    =       -4164875
98                 I    =           51
61708
 XDOT =       5856
453736                 Wp   =           22
79990
 YDOT =      -3341
035565  meter/sec      RA   =          356
04983  deg
 ZDOT =      -3698
567161                 TA   =          209
31561
                                          MA   =          209
39247
                                          Ha   =            191
589  n
mi
                                          Hp   =            182
972

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14275988
03                 X    =        -4297147
10
 Y    =       -9863529
83  feet           Y    =        -3054759
77  meter
 Z    =      -13664291
28                 Z    =        -4185883
61
 XDOT =      19214
087062                 XDOT =        5911
345753
 YDOT =     -10961
402772  feet/sec       YDOT =       -3275
238045  meter/sec
 ZDOT =     -12134
406697                 ZDOT =       -3669
982997

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4163634
03                 X    =        -1269075
65
 Y    =       16776884
52  feet           Y    =         5113594
40  meter
 Z    =      -13747952
88                 Z    =        -4190376
04
 XDOT =     -15886
303044                 XDOT =       -4842
145168
 YDOT =     -13815
236931  feet/sec       YDOT =       -4210
884216  meter/sec
 ZDOT =     -12020
553031                 ZDOT =       -3663
864564


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   10143
66275862  
00016717  00000-0  10270-3 0  9031
2 25544  51
6447 356
4159 0010033 347
3896  12
7015 15
74234595 19617


Satellite: ISS
Catalog Number: 25544
Epoch time:      10143
66275862   =   yrday
fracday
Element set:     903
Inclination:       51
6447  deg
RA of node:       356
4159  deg
Eccentricity:     
0010033     
Arg of perigee:   347
3896  deg
Mean anomaly:      12
7015  deg
Mean motion:   15
74234595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1961
Checksum:              312


Coasting Arc #5 (Orbit 1976)
---------------------------------------

Vector Time (GMT): 2010/144/15:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816784
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4934911
85                 A    =         6727305
93  meter
 Y    =        3318980
65  meter          E    =           
0014327
 Z    =        3144965
72                 I    =           51
59731
 XDOT =      -5150
967319                 Wp   =           51
90375
 YDOT =      -3053
951701  meter/sec      RA   =          350
85965  deg
 ZDOT =      -4836
108195                 TA   =           91
47474
                                          MA   =           91
31061
                                          Ha   =            191
712  n
mi
                                          Hp   =            182
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16190655
69                 X    =        -4986936
46
 Y    =       10889044
13  feet           Y    =         3263504
36  meter
 Z    =       10318129
00                 Z    =         3120865
41
 XDOT =     -16899
499078                 XDOT =       -5092
941292
 YDOT =     -10019
526579  feet/sec       YDOT =       -3111
228019  meter/sec
 ZDOT =     -15866
496702                 ZDOT =       -4860
991360

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16153964
74                 X    =         4923728
45
 Y    =       11033122
50  feet           Y    =         3362895
74  meter
 Z    =       10222134
36                 Z    =         3115706
55
 XDOT =      -2243
507585                 XDOT =        -683
821112
 YDOT =      18149
193012  feet/sec       YDOT =        5531
874030  meter/sec
 ZDOT =     -15965
587759                 ZDOT =       -4866
311149


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
67844276  
00016717  00000-0  10270-3 0  9045
2 25544  51
6439 351
1976 0009959 350
3686   9
7285 15
74230142 19779


Satellite: ISS
Catalog Number: 25544
Epoch time:      10144
67844276   =   yrday
fracday
Element set:     904
Inclination:       51
6439  deg
RA of node:       351
1976  deg
Eccentricity:     
0009959     
Arg of perigee:   350
3686  deg
Mean anomaly:       9
7285  deg
Mean motion:   15
74230142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1977
Checksum:              338


Coasting Arc #6 (Orbit 1992)
---------------------------------------

Vector Time (GMT): 2010/145/15:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 816784
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4622317
40                 A    =         6723255
11  meter
 Y    =        2331557
32  meter          E    =           
0010579
 Z    =        4278423
63                 I    =           51
55554
 XDOT =      -5390
951058                 Wp   =           49
77371
 YDOT =       4244
088691  meter/sec      RA   =          345
76717  deg
 ZDOT =       3512
459014                 TA   =            4
65193
                                          MA   =            4
64210
                                          Ha   =            191
604  n
mi
                                          Hp   =            182
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15165083
33                 X    =         4575117
76
 Y    =        7649466
29  feet           Y    =         2382982
44  meter
 Z    =       14036822
93                 Z    =         4300764
89
 XDOT =     -17686
847304                 XDOT =       -5455
071769
 YDOT =      13924
175495  feet/sec       YDOT =        4183
444949  meter/sec
 ZDOT =      11523
815664                 ZDOT =        3486
113999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1199381
78                 X    =          365571
57
 Y    =      -16868611
34  feet           Y    =        -5141552
74  meter
 Z    =       14125789
17                 Z    =         4305540
54
 XDOT =      18491
939137                 XDOT =        5636
343049
 YDOT =      10874
147673  feet/sec       YDOT =        3314
440211  meter/sec
 ZDOT =      11418
875896                 ZDOT =        3480
473373


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
69410890  
00016717  00000-0  10270-3 0  9050
2 25544  51
6445 345
9799 0009935 353
9750   6
1292 15
74293803 19935


Satellite: ISS
Catalog Number: 25544
Epoch time:      10145
69410890   =   yrday
fracday
Element set:     905
Inclination:       51
6445  deg
RA of node:       345
9799  deg
Eccentricity:     
0009935     
Arg of perigee:   353
9750  deg
Mean anomaly:       6
1292  deg
Mean motion:   15
74293803  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1993
Checksum:              339


Coasting Arc #7 (Orbit 2002)
---------------------------------------

Vector Time (GMT): 2010/146/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3455476
85                 A    =         6719365
23  meter
 Y    =        3003612
64  meter          E    =           
0006499
 Z    =        4913656
14                 I    =           51
53049
 XDOT =      -6351
561545                 Wp   =           27
47060
 YDOT =       3796
184205  meter/sec      RA   =          342
48675  deg
 ZDOT =       2150
691242                 TA   =           41
67002
                                          MA   =           41
62052
                                          Ha   =            190
499  n
mi
                                          Hp   =            182
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11336866
29                 X    =         3397762
99
 Y    =        9854372
17  feet           Y    =         3041930
50  meter
 Z    =       16120919
10                 Z    =         4930303
37
 XDOT =     -20838
456513                 XDOT =       -6403
986960
 YDOT =      12454
672587  feet/sec       YDOT =        3724
863857  meter/sec
 ZDOT =       7056
073627                 ZDOT =        2119
707917

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7848965
35                 X    =         2392364
64
 Y    =       12723419
48  feet           Y    =         3878098
26  meter
 Z    =       16187203
60                 Z    =         4933859
66
 XDOT =     -22690
178826                 XDOT =       -6915
966506
 YDOT =       5196
292032  feet/sec       YDOT =        1583
829811  meter/sec
 ZDOT =       6932
661296                 ZDOT =        2113
075163


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
32887326  
00016717  00000-0  10270-3 0  9064
2 25544  51
6466 342
7241 0009407 347
1437  12
9485 15
74770676 20036


Satellite: ISS
Catalog Number: 25544
Epoch time:      10146
32887326   =   yrday
fracday
Element set:     906
Inclination:       51
6466  deg
RA of node:       342
7241  deg
Eccentricity:     
0009407     
Arg of perigee:   347
1437  deg
Mean anomaly:      12
9485  deg
Mean motion:   15
74770676  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2003
Checksum:              314


Coasting Arc #8 (Orbit 2017)
---------------------------------------

Vector Time (GMT): 2010/147/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5395325
34                 A    =         6728861
62  meter
 Y    =       -3658942
81  meter          E    =           
0016159
 Z    =       -1628803
29                 I    =           51
53409
 XDOT =       3955
346921                 Wp   =           11
57838
 YDOT =       3288
593047  meter/sec      RA   =          337
30540  deg
 ZDOT =       5739
737434                 TA   =          330
38705
                                          MA   =          330
47845
                                          Ha   =            190
766  n
mi
                                          Hp   =            182
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17701198
62                 X    =         5443751
87
 Y    =      -12004405
53  feet           Y    =        -3598338
05  meter
 Z    =       -5343842
82                 Z    =        -1602475
28
 XDOT =      12976
859977                 XDOT =        3890
396239
 YDOT =      10789
347267  feet/sec       YDOT =        3332
460063  meter/sec
 ZDOT =      18831
159560                 ZDOT =        5758
795563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20366561
48                 X    =         6207727
94
 Y    =       -6614471
66  feet           Y    =        -2016090
96  meter
 Z    =       -5238967
37                 Z    =        -1596837
25
 XDOT =       8885
180884                 XDOT =        2708
203133
 YDOT =      12450
228407  feet/sec       YDOT =        3794
829618  meter/sec
 ZDOT =      18907
042862                 ZDOT =        5762
866664


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
28075520  
00016717  00000-0  10270-3 0  9076
2 25544  51
6469 337
8306 0009543 350
8050   9
2937 15
74774592 20187


Satellite: ISS
Catalog Number: 25544
Epoch time:      10147
28075520   =   yrday
fracday
Element set:     907
Inclination:       51
6469  deg
RA of node:       337
8306  deg
Eccentricity:     
0009543     
Arg of perigee:   350
8050  deg
Mean anomaly:       9
2937  deg
Mean motion:   15
74774592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2018
Checksum:              317


Coasting Arc #9 (Orbit 2033)
---------------------------------------

Vector Time (GMT): 2010/148/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3422678
62                 A    =         6718512
63  meter
 Y    =       -2773154
39  meter          E    =           
0017713
 Z    =       -5086498
75                 I    =           51
47293
 XDOT =       6000
102636                 Wp   =           45
54195
 YDOT =      -4556
269405  meter/sec      RA   =          332
18223  deg
 ZDOT =      -1544
467108                 TA   =          209
53331
                                          MA   =          209
63348
                                          Ha   =            190
783  n
mi
                                          Hp   =            181
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11229260
56                 X    =        -3366704
72
 Y    =       -9098275
55  feet           Y    =        -2811115
00  meter
 Z    =      -16687988
04                 Z    =        -5102990
85
 XDOT =      19685
376104                 XDOT =        6058
108556
 YDOT =     -14948
390437  feet/sec       YDOT =       -4488
848100  meter/sec
 ZDOT =      -5067
149304                 ZDOT =       -1515
178091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8372061
34                 X    =        -2551804
30
 Y    =      -11687064
32  feet           Y    =        -3562217
20  meter
 Z    =      -16753655
48                 Z    =        -5106514
19
 XDOT =      22079
308291                 XDOT =        6729
773167
 YDOT =      -8678
288955  feet/sec       YDOT =       -2645
142473  meter/sec
 ZDOT =      -4950
471070                 ZDOT =       -1508
903582


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
29607790  
00016717  00000-0  10270-3 0  9089
2 25544  51
6475 332
6107 0009596 354
9281   5
1783 15
74824632 20348


Satellite: ISS
Catalog Number: 25544
Epoch time:      10148
29607790   =   yrday
fracday
Element set:     908
Inclination:       51
6475  deg
RA of node:       332
6107  deg
Eccentricity:     
0009596     
Arg of perigee:   354
9281  deg
Mean anomaly:       5
1783  deg
Mean motion:   15
74824632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2034
Checksum:              321


Coasting Arc #10 (Orbit 2049)
---------------------------------------

Vector Time (GMT): 2010/149/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5074464
70                 A    =         6729414
35  meter
 Y    =        4292521
43  meter          E    =           
0011274
 Z    =        1051542
88                 I    =           51
48312
 XDOT =      -3853
247212                 Wp   =           80
29089
 YDOT =      -3096
420022  meter/sec      RA   =          327
00592  deg
 ZDOT =      -5899
290767                 TA   =           88
18848
                                          MA   =           88
05936
                                          Ha   =            190
924  n
mi
                                          Hp   =            181
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16648506
22                 X    =        -5127195
54
 Y    =       14083075
54  feet           Y    =         4235480
72  meter
 Z    =        3449943
84                 Z    =         1026763
59
 XDOT =     -12641
887177                 XDOT =       -3789
678177
 YDOT =     -10158
858339  feet/sec       YDOT =       -3139
152860  meter/sec
 ZDOT =     -19354
628502                 ZDOT =       -5917
856134

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19602922
81                 X    =        -5974970
87
 Y    =        9586584
32  feet           Y    =         2921990
90  meter
 Z    =        3351224
70                 Z    =         1021453
29
 XDOT =      -8968
363899                 XDOT =       -2733
557317
 YDOT =     -11481
514641  feet/sec       YDOT =       -3499
565663  meter/sec
 ZDOT =     -19428
554153                 ZDOT =       -5921
823306


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
31138391  
00016717  00000-0  10270-3 0  9090
2 25544  51
6474 327
3906 0009527 358
4586   1
6546 15
74810391 20509


Satellite: ISS
Catalog Number: 25544
Epoch time:      10149
31138391   =   yrday
fracday
Element set:     909
Inclination:       51
6474  deg
RA of node:       327
3906  deg
Eccentricity:     
0009527     
Arg of perigee:   358
4586  deg
Mean anomaly:       1
6546  deg
Mean motion:   15
74810391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2050
Checksum:              313


Coasting Arc #11 (Orbit 2065)
---------------------------------------

Vector Time (GMT): 2010/150/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3317177
45                 A    =         6717814
40  meter
 Y    =        2664464
57  meter          E    =           
0008574
 Z    =        5195045
81                 I    =           51
42042
 XDOT =      -5569
909254                 Wp   =           20
68858
 YDOT =       5254
009758  meter/sec      RA   =          321
86782  deg
 ZDOT =        869
301912                 TA   =           61
05755
                                          MA   =           60
97160
                                          Ha   =            190
880  n
mi
                                          Hp   =            181
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10883128
12                 X    =         3261899
70
 Y    =        8741681
67  feet           Y    =         2701249
25  meter
 Z    =       17044113
55                 Z    =         5211026
92
 XDOT =     -18273
980491                 XDOT =       -5632
469496
 YDOT =      17237
564824  feet/sec       YDOT =        5191
373773  meter/sec
 ZDOT =       2852
040395                 ZDOT =         842
092139

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8511110
34                 X    =         2594186
43
 Y    =       10965722
94  feet           Y    =         3342352
35  meter
 Z    =       17107752
75                 Z    =         5214443
04
 XDOT =     -20932
440327                 XDOT =       -6380
207812
 YDOT =      12004
556999  feet/sec       YDOT =        3658
988973  meter/sec
 ZDOT =       2743
633127                 ZDOT =         836
259377


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
32667019  
00016717  00000-0  10270-3 0  9109
2 25544  51
6478 322
1704 0009654   1
7074 358
4121 15
74877948 20663


Satellite: ISS
Catalog Number: 25544
Epoch time:      10150
32667019   =   yrday
fracday
Element set:     910
Inclination:       51
6478  deg
RA of node:       322
1704  deg
Eccentricity:     
0009654     
Arg of perigee:     1
7074  deg
Mean anomaly:     358
4121  deg
Mean motion:   15
74877948  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2066
Checksum:              306


Coasting Arc #12 (Orbit 2080)
---------------------------------------

Vector Time (GMT): 2010/151/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4616201
96                 A    =         6729548
59  meter
 Y    =       -4858444
57  meter          E    =           
0020013
 Z    =        -463919
74                 I    =           51
43734
 XDOT =       3773
517505                 Wp   =           24
37915
 YDOT =       3022
406650  meter/sec      RA   =          316
69897  deg
 ZDOT =       6005
327654                 TA   =          330
55400
                                          MA   =          330
66660
                                          Ha   =            191
048  n
mi
                                          Hp   =            181
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15145019
56                 X    =         4672440
52
 Y    =      -15939778
77  feet           Y    =        -4806508
93  meter
 Z    =       -1522046
41                 Z    =         -441358
42
 XDOT =      12380
306776                 XDOT =        3710
267151
 YDOT =       9916
032315  feet/sec       YDOT =        3064
249728  meter/sec
 ZDOT =      19702
518551                 ZDOT =        6023
506274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18171908
46                 X    =         5538797
70
 Y    =      -12389328
42  feet           Y    =        -3776267
30  meter
 Z    =       -1432157
09                 Z    =         -436521
48
 XDOT =       8995
798864                 XDOT =        2741
919494
 YDOT =      10952
778600  feet/sec       YDOT =        3338
406917  meter/sec
 ZDOT =      19774
913679                 ZDOT =        6027
393689


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
27848661  
00016717  00000-0  10270-3 0  9119
2 25544  51
6482 317
2767 0009762   4
8982 355
2276 15
74896215 20815


Satellite: ISS
Catalog Number: 25544
Epoch time:      10151
27848661   =   yrday
fracday
Element set:     911
Inclination:       51
6482  deg
RA of node:       317
2767  deg
Eccentricity:     
0009762     
Arg of perigee:     4
8982  deg
Mean anomaly:     355
2276  deg
Mean motion:   15
74896215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2081
Checksum:              328


Coasting Arc #13 (Orbit 2096)
---------------------------------------

Vector Time (GMT): 2010/152/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3264098
63                 A    =         6717444
26  meter
 Y    =       -2647110
45  meter          E    =           
0019277
 Z    =       -5254827
31                 I    =           51
37554
 XDOT =       5003
983205                 Wp   =           58
42343
 YDOT =      -5837
432109  meter/sec      RA   =          311
54579  deg
 ZDOT =       -158
176472                 TA   =          210
01261
                                          MA   =          210
12324
                                          Ha   =            191
091  n
mi
                                          Hp   =            180
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10708985
01                 X    =        -3208728
62
 Y    =       -8684745
57  feet           Y    =        -2683301
17  meter
 Z    =      -17240247
07                 Z    =        -5270550
17
 XDOT =      16417
267732                 XDOT =        5069
654908
 YDOT =     -19151
680149  feet/sec       YDOT =       -5781
107376  meter/sec
 ZDOT =       -518
951679                 ZDOT =        -133
708517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8722316
56                 X    =        -2658562
09
 Y    =      -10576638
05  feet           Y    =        -3223759
28  meter
 Z    =      -17302866
98                 Z    =        -5273913
85
 XDOT =      19049
727784                 XDOT =        5806
357029
 YDOT =     -14969
522620  feet/sec       YDOT =       -4562
710495  meter/sec
 ZDOT =       -421
466801                 ZDOT =        -128
463081


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
29373939  
00016717  00000-0  10270-3 0  9124
2 25544  51
6480 312
0565 0009842   8
3363 351
7962 15
74934788 20971


Satellite: ISS
Catalog Number: 25544
Epoch time:      10152
29373939   =   yrday
fracday
Element set:     912
Inclination:       51
6480  deg
RA of node:       312
0565  deg
Eccentricity:     
0009842     
Arg of perigee:     8
3363  deg
Mean anomaly:     351
7962  deg
Mean motion:   15
74934788  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2097
Checksum:              329


Coasting Arc #14 (Orbit 2112)
---------------------------------------

Vector Time (GMT): 2010/153/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4122815
40                 A    =         6729571
48  meter
 Y    =        5315883
53  meter          E    =           
0010143
 Z    =        -207261
21                 I    =           51
39697
 XDOT =      -3686
957766                 Wp   =           84
66464
 YDOT =      -3083
974473  meter/sec      RA   =          306
38646  deg
 ZDOT =      -6009
234091                 TA   =           97
59368
                                          MA   =           97
47846
                                          Ha   =            191
220  n
mi
                                          Hp   =            180
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13526297
25                 X    =        -4180945
32
 Y    =       17440562
76  feet           Y    =         5269454
76  meter
 Z    =        -679990
83                 Z    =         -227430
30
 XDOT =     -12096
318131                 XDOT =       -3623
006480
 YDOT =     -10118
026487  feet/sec       YDOT =       -3124
845871  meter/sec
 ZDOT =     -19715
334945                 ZDOT =       -6026
990361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16394581
35                 X    =        -4997068
40
 Y    =       14772809
88  feet           Y    =         4502752
45  meter
 Z    =        -760345
00                 Z    =         -231753
16
 XDOT =      -8923
132743                 XDOT =       -2719
770860
 YDOT =     -10883
148952  feet/sec       YDOT =       -3317
183801  meter/sec
 ZDOT =     -19786
058193                 ZDOT =       -6030
790537


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
30897580  
00016717  00000-0  10270-3 0  9131
2 25544  51
6480 306
8366 0009688  12
1439 347
9956 15
74904960 21134


Satellite: ISS
Catalog Number: 25544
Epoch time:      10153
30897580   =   yrday
fracday
Element set:     913
Inclination:       51
6480  deg
RA of node:       306
8366  deg
Eccentricity:     
0009688     
Arg of perigee:    12
1439  deg
Mean anomaly:     347
9956  deg
Mean motion:   15
74904960  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2113
Checksum:              329


Coasting Arc #15 (Orbit 2128)
---------------------------------------

Vector Time (GMT): 2010/154/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3206350
44                 A    =         6717420
65  meter
 Y    =        2758933
31  meter          E    =           
0012031
 Z    =        5214875
00                 I    =           51
33953
 XDOT =      -4395
943945                 Wp   =           25
50408
 YDOT =       6299
159657  meter/sec      RA   =          301
21637  deg
 ZDOT =       -618
496031                 TA   =           70
46028
                                          MA   =           70
33040
                                          Ha   =            191
167  n
mi
                                          Hp   =            180
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10519522
43                 X    =         3149928
35
 Y    =        9051618
48  feet           Y    =         2794472
56  meter
 Z    =       17109169
93                 Z    =         5230314
70
 XDOT =     -14422
388272                 XDOT =       -4463
051031
 YDOT =      20666
534308  feet/sec       YDOT =        6249
626449  meter/sec
 ZDOT =      -2029
186452                 ZDOT =        -640
013780

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8836008
33                 X    =         2693215
34
 Y    =       10602305
40  feet           Y    =         3231582
69  meter
 Z    =       17170670
41                 Z    =         5233620
34
 XDOT =     -16757
673537                 XDOT =       -5107
738894
 YDOT =      17450
599203  feet/sec       YDOT =        5318
942637  meter/sec
 ZDOT =      -2114
907999                 ZDOT =        -644
623958


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
32419166  
00016717  00000-0  10270-3 0  9145
2 25544  51
6478 301
6158 0009882  15
2973 344
8488 15
74985711 21292


Satellite: ISS
Catalog Number: 25544
Epoch time:      10154
32419166   =   yrday
fracday
Element set:     914
Inclination:       51
6478  deg
RA of node:       301
6158  deg
Eccentricity:     
0009882     
Arg of perigee:    15
2973  deg
Mean anomaly:     344
8488  deg
Mean motion:   15
74985711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2129
Checksum:              331


Coasting Arc #16 (Orbit 2144)
---------------------------------------

Vector Time (GMT): 2010/155/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3533266
95                 A    =         6728953
29  meter
 Y    =       -5645019
20  meter          E    =           
0022403
 Z    =         867422
69                 I    =           51
36313
 XDOT =       3700
844662                 Wp   =           39
21185
 YDOT =       3239
241412  meter/sec      RA   =          296
06659  deg
 ZDOT =       5939
601664                 TA   =          330
30590
                                          MA   =          330
43288
                                          Ha   =            191
236  n
mi
                                          Hp   =            180
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11592083
17                 X    =         3591914
19
 Y    =      -18520404
21  feet           Y    =        -5605180
28  meter
 Z    =        2845874
98                 Z    =          884729
20
 XDOT =      12141
878811                 XDOT =        3635
494275
 YDOT =      10627
432455  feet/sec       YDOT =        3280
260449  meter/sec
 ZDOT =      19486
882100                 ZDOT =        5957
421995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14104154
65                 X    =         4298946
34
 Y    =      -16675054
71  feet           Y    =        -5082556
68  meter
 Z    =        2914814
02                 Z    =          888435
31
 XDOT =       9167
562228                 XDOT =        2794
272967
 YDOT =      11209
900998  feet/sec       YDOT =        3416
777824  meter/sec
 ZDOT =      19557
869291                 ZDOT =        5961
238560


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
33939063  
00016717  00000-0  10270-3 0  9151
2 25544  51
6469 296
3949 0009899  18
6544 341
4981 15
75016796 21457


Satellite: ISS
Catalog Number: 25544
Epoch time:      10155
33939063   =   yrday
fracday
Element set:     915
Inclination:       51
6469  deg
RA of node:       296
3949  deg
Eccentricity:     
0009899     
Arg of perigee:    18
6544  deg
Mean anomaly:     341
4981  deg
Mean motion:   15
75016796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2145
Checksum:              352


Coasting Arc #17 (Orbit 2159)
---------------------------------------

Vector Time (GMT): 2010/156/06:39:48
736
Vector Time (MET): N/A
Weight (LBS)     : 816529
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3266401
14                 A    =         6717811
26  meter
 Y    =       -2915521
38  meter          E    =           
0018705
 Z    =       -5108710
12                 I    =           51
31239
 XDOT =       3711
832448                 Wp   =           69
16190
 YDOT =      -6589
375616  meter/sec      RA   =          290
88057  deg
 ZDOT =       1397
942433                 TA   =          214
24324
                                          MA   =          214
36399
                                          Ha   =            191
315  n
mi
                                          Hp   =            179
993

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10716539
16                 X    =        -3208739
18
 Y    =       -9565358
85  feet           Y    =        -2951725
31  meter
 Z    =      -16760859
98                 Z    =        -5124438
60
 XDOT =      12177
927979                 XDOT =        3778
449182
 YDOT =     -21618
686403  feet/sec       YDOT =       -6547
495358  meter/sec
 ZDOT =       4586
425305                 ZDOT =        1416
135760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9328255
99                 X    =        -2843252
43
 Y    =      -10826801
43  feet           Y    =        -3300009
08  meter
 Z    =      -16823517
46                 Z    =        -5127808
12
 XDOT =      13986
877446                 XDOT =        4263
200245
 YDOT =     -19236
051557  feet/sec       YDOT =       -5863
148515  meter/sec
 ZDOT =       4658
890052                 ZDOT =        1420
029688


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
29112427  
00016717  00000-0  10270-3 0  9165
2 25544  51
6458 291
4997 0009957  22
0376 338
1214 15
75035546 21604


Satellite: ISS
Catalog Number: 25544
Epoch time:      10156
29112427   =   yrday
fracday
Element set:     916
Inclination:       51
6458  deg
RA of node:       291
4997  deg
Eccentricity:     
0009957     
Arg of perigee:    22
0376  deg
Mean anomaly:     338
1214  deg
Mean motion:   15
75035546  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2160
Checksum:              313

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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