Date: May 5th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19375 04 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 1643)
---------------------------------------

Vector Time (GMT): 2010/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -524992
63                 A    =         6731686
01  meter
 Y    =       -6414385
56  meter          E    =           
0005850
 Z    =        1960450
77                 I    =           51
98980
 XDOT =       4799
778498                 Wp   =          148
71505
 YDOT =      -2116
188337  meter/sec      RA   =           99
09416  deg
 ZDOT =      -5636
029939                 TA   =            9
57935
                                          MA   =            9
56820
                                          Ha   =            188
109  n
mi
                                          Hp   =            187
150

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1722416
77                 X    =         -462750
36
 Y    =      -21044572
04  feet           Y    =        -6419908
47  meter
 Z    =        6431925
09                 Z    =         1958051
04
 XDOT =      15747
304783                 XDOT =        4850
464311
 YDOT =      -6942
875122  feet/sec       YDOT =       -2062
230529  meter/sec
 ZDOT =     -18490
911874                 ZDOT =       -5612
589544

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15007404
53                 X    =        -4574256
90
 Y    =      -14857417
18  feet           Y    =        -4528540
76  meter
 Z    =        6422254
76                 Z    =         1957503
25
 XDOT =       6462
477894                 XDOT =        1969
763262
 YDOT =     -14483
905206  feet/sec       YDOT =       -4414
694307  meter/sec
 ZDOT =     -18397
611532                 ZDOT =       -5607
591995


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   10123
53559400  
00016717  00000-0  10270-3 0  9005
2 25544  51
6419  99
7457 0010024 272
0194  87
9821 15
73587184 16440


Satellite: ISS
Catalog Number: 25544
Epoch time:      10123
53559400   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:        99
7457  deg
Eccentricity:     
0010024     
Arg of perigee:   272
0194  deg
Mean anomaly:      87
9821  deg
Mean motion:   15
73587184  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1644
Checksum:              309


Coasting Arc #2 (Orbit 1659)
---------------------------------------

Vector Time (GMT): 2010/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3990322
76                 A    =         6723005
71  meter
 Y    =        2351855
91  meter          E    =           
0005011
 Z    =        4877466
38                 I    =           51
96485
 XDOT =      -1349
323501                 Wp   =          238
22081
 YDOT =      -7198
010430  meter/sec      RA   =           94
02247  deg
 ZDOT =       2366
080252                 TA   =          188
79967
                                          MA   =          188
80846
                                          Ha   =            188
596  n
mi
                                          Hp   =            187
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13091610
12                 X    =        -4040018
98
 Y    =        7716062
70  feet           Y    =         2306955
57  meter
 Z    =       16002186
28                 Z    =         4857960
78
 XDOT =      -4426
914373                 XDOT =       -1280
227788
 YDOT =     -23615
519784  feet/sec       YDOT =       -7212
713183  meter/sec
 ZDOT =       7762
730485                 ZDOT =        2359
692601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4764421
69                 X    =        -1452195
73
 Y    =       14515744
06  feet           Y    =         4424398
79  meter
 Z    =       15924550
40                 Z    =         4853802
96
 XDOT =     -17937
154367                 XDOT =       -5467
244651
 YDOT =     -14378
449191  feet/sec       YDOT =       -4382
551313  meter/sec
 ZDOT =       7737
172033                 ZDOT =        2358
290036


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   10124
55168929  
00016717  00000-0  10270-3 0  9011
2 25544  51
6423  94
5314 0010124 275
4495  84
5513 15
73626415 16602


Satellite: ISS
Catalog Number: 25544
Epoch time:      10124
55168929   =   yrday
fracday
Element set:     901
Inclination:       51
6423  deg
RA of node:        94
5314  deg
Eccentricity:     
0010124     
Arg of perigee:   275
4495  deg
Mean anomaly:      84
5513  deg
Mean motion:   15
73626415  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1660
Checksum:              297


Coasting Arc #3 (Orbit 1674)
---------------------------------------

Vector Time (GMT): 2010/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1812868
34                 A    =         6731185
88  meter
 Y    =        6103876
63  meter          E    =           
0008466
 Z    =       -2166112
13                 I    =           51
99335
 XDOT =      -4264
838763                 Wp   =          318
07552
 YDOT =       3234
013137  meter/sec      RA   =           88
87575  deg
 ZDOT =       5537
586141                 TA   =           17
79879
                                          MA   =           17
76916
                                          Ha   =            189
019  n
mi
                                          Hp   =            187
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5947730
76                 X    =         1755001
55
 Y    =       20025841
96  feet           Y    =         6123825
75  meter
 Z    =       -7106667
11                 Z    =        -2157445
48
 XDOT =     -13992
253161                 XDOT =       -4327
585749
 YDOT =      10610
279321  feet/sec       YDOT =        3185
970075  meter/sec
 ZDOT =      18167
933533                 ZDOT =        5516
715253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17940850
44                 X    =         5468371
21
 Y    =       10725040
02  feet           Y    =         3268992
20  meter
 Z    =       -7072055
34                 Z    =        -2155562
47
 XDOT =      -2451
103761                 XDOT =        -747
096426
 YDOT =      16038
750543  feet/sec       YDOT =        4888
611165  meter/sec
 ZDOT =      18084
868226                 ZDOT =        5512
267835


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   10125
50425757  
00016717  00000-0  10270-3 0  9023
2 25544  51
6422  89
6423 0009968 279
4068  80
5968 15
73637784 16758


Satellite: ISS
Catalog Number: 25544
Epoch time:      10125
50425757   =   yrday
fracday
Element set:     902
Inclination:       51
6422  deg
RA of node:        89
6423  deg
Eccentricity:     
0009968     
Arg of perigee:   279
4068  deg
Mean anomaly:      80
5968  deg
Mean motion:   15
73637784  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1675
Checksum:              345


Coasting Arc #4 (Orbit 1690)
---------------------------------------

Vector Time (GMT): 2010/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3418734
22                 A    =         6723176
89  meter
 Y    =       -3251210
16  meter          E    =           
0006074
 Z    =       -4793333
91                 I    =           51
96579
 XDOT =       2756
792527                 Wp   =           11
83094
 YDOT =       6707
926390  meter/sec      RA   =           83
80587  deg
 ZDOT =      -2578
377601                 TA   =          232
97169
                                          MA   =          233
02728
                                          Ha   =            189
243  n
mi
                                          Hp   =            187
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11216319
60                 X    =         3478120
96
 Y    =      -10666700
00  feet           Y    =        -3212647
64  meter
 Z    =      -15726161
11                 Z    =        -4776581
50
 XDOT =       9044
594905                 XDOT =        2694
103724
 YDOT =      22007
632512  feet/sec       YDOT =        6738
404056  meter/sec
 ZDOT =      -8459
244097                 ZDOT =       -2565
137120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         870326
06                 X    =          265275
38
 Y    =      -15521574
82  feet           Y    =        -4730976
01  meter
 Z    =      -15659492
50                 Z    =        -4773013
31
 XDOT =      20607
558299                 XDOT =        6281
183770
 YDOT =       9654
030081  feet/sec       YDOT =        2942
548369  meter/sec
 ZDOT =      -8406
411896                 ZDOT =       -2562
274346


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   10126
52030645  
00016717  00000-0  10270-3 0  9035
2 25544  51
6429  84
4272 0010054 283
3795  76
6247 15
73683357 16910


Satellite: ISS
Catalog Number: 25544
Epoch time:      10126
52030645   =   yrday
fracday
Element set:     903
Inclination:       51
6429  deg
RA of node:        84
4272  deg
Eccentricity:     
0010054     
Arg of perigee:   283
3795  deg
Mean anomaly:      76
6247  deg
Mean motion:   15
73683357  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1691
Checksum:              309


Coasting Arc #5 (Orbit 1706)
---------------------------------------

Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2972263
32                 A    =         6730652
48  meter
 Y    =       -5570509
41  meter          E    =           
0003884
 Z    =        2326543
01                 I    =           51
98716
 XDOT =       3511
000345                 Wp   =          106
86718
 YDOT =      -4151
714322  meter/sec      RA   =           78
65650  deg
 ZDOT =      -5448
776757                 TA   =           47
10251
                                          MA   =           47
06991
                                          Ha   =            189
500  n
mi
                                          Hp   =            187
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9751520
09                 X    =        -2921053
96
 Y    =      -18275949
50  feet           Y    =        -5603460
75  meter
 Z    =        7633015
12                 Z    =         2312227
95
 XDOT =      11519
030003                 XDOT =        3583
633929
 YDOT =     -13621
109979  feet/sec       YDOT =       -4112
045995  meter/sec
 ZDOT =     -17876
564163                 ZDOT =       -5431
543885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19791347
77                 X    =        -6032402
80
 Y    =       -6186542
52  feet           Y    =        -1885658
16  meter
 Z    =        7575924
97                 Z    =         2309141
93
 XDOT =      -1691
710681                 XDOT =        -515
633416
 YDOT =     -16421
021077  feet/sec       YDOT =       -5005
127224  meter/sec
 ZDOT =     -17807
990309                 ZDOT =       -5427
875446


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   10127
53633105  
00016717  00000-0  10270-3 0  9048
2 25544  51
6432  79
2123 0010095 287
4842  72
5217 15
73721190 17072


Satellite: ISS
Catalog Number: 25544
Epoch time:      10127
53633105   =   yrday
fracday
Element set:     904
Inclination:       51
6432  deg
RA of node:        79
2123  deg
Eccentricity:     
0010095     
Arg of perigee:   287
4842  deg
Mean anomaly:      72
5217  deg
Mean motion:   15
73721190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1707
Checksum:              284


Coasting Arc #6 (Orbit 1722)
---------------------------------------

Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2693995
43                 A    =         6723111
95  meter
 Y    =        3950242
23  meter          E    =           
0002770
 Z    =        4728742
59                 I    =           51
95601
 XDOT =      -3991
511338                 Wp   =          267
66449
 YDOT =      -5989
210482  meter/sec      RA   =           73
58781  deg
 ZDOT =       2730
461408                 TA   =          155
57326
                                          MA   =          155
56014
                                          Ha   =            189
691  n
mi
                                          Hp   =            187
006

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8838567
69                 X    =        -2760939
11
 Y    =       12960112
31  feet           Y    =         3919742
00  meter
 Z    =       15514247
34                 Z    =         4715492
50
 XDOT =     -13095
509638                 XDOT =       -3937
506452
 YDOT =     -19649
640689  feet/sec       YDOT =       -6033
544023  meter/sec
 ZDOT =       8958
206719                 ZDOT =        2711
201564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2967398
51                 X    =          904463
07
 Y    =       15456790
02  feet           Y    =         4711229
60  meter
 Z    =       15461528
03                 Z    =         4712673
74
 XDOT =     -22098
369744                 XDOT =       -6735
583098
 YDOT =      -4637
565998  feet/sec       YDOT =       -1413
530116  meter/sec
 ZDOT =       8881
424008                 ZDOT =        2707
058037


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   10128
55232947  
00016717  00000-0  10270-3 0  9051
2 25544  51
6439  73
9973 0010208 290
4565  69
5502 15
73792605 17235


Satellite: ISS
Catalog Number: 25544
Epoch time:      10128
55232947   =   yrday
fracday
Element set:     905
Inclination:       51
6439  deg
RA of node:        73
9973  deg
Eccentricity:     
0010208     
Arg of perigee:   290
4565  deg
Mean anomaly:      69
5502  deg
Mean motion:   15
73792605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1723
Checksum:              320


Coasting Arc #7 (Orbit 1737)
---------------------------------------

Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3967601
41                 A    =         6730262
52  meter
 Y    =        4849911
99  meter          E    =           
0009620
 Z    =       -2438491
28                 I    =           51
96996
 XDOT =      -2613
838630                 Wp   =          326
93939
 YDOT =       4847
380500  meter/sec      RA   =           68
43463  deg
 ZDOT =       5386
035722                 TA   =            5
64661
                                          MA   =            5
63577
                                          Ha   =            190
008  n
mi
                                          Hp   =            186
761

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13017064
99                 X    =         3924919
84
 Y    =       15911784
74  feet           Y    =         4894041
46  meter
 Z    =       -8000299
46                 Z    =        -2419320
02
 XDOT =      -8575
586055                 XDOT =       -2694
013366
 YDOT =      15903
479332  feet/sec       YDOT =        4817
702636  meter/sec
 ZDOT =      17670
720874                 ZDOT =        5373
142860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20532413
40                 X    =         6258279
60
 Y    =        1505193
84  feet           Y    =          458783
08  meter
 Z    =       -7923891
59                 Z    =        -2415202
16
 XDOT =       5647
378854                 XDOT =        1721
321075
 YDOT =      15754
019147  feet/sec       YDOT =        4801
825036  meter/sec
 ZDOT =      17619
429570                 ZDOT =        5370
402133


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   10129
50480830  
00016717  00000-0  10270-3 0  9064
2 25544  51
6436  69
1075 0010226 295
0178  64
9923 15
73780398 17381


Satellite: ISS
Catalog Number: 25544
Epoch time:      10129
50480830   =   yrday
fracday
Element set:     906
Inclination:       51
6436  deg
RA of node:        69
1075  deg
Eccentricity:     
0010226     
Arg of perigee:   295
0178  deg
Mean anomaly:      64
9923  deg
Mean motion:   15
73780398  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1738
Checksum:              319


Coasting Arc #8 (Orbit 1753)
---------------------------------------

Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1861892
42                 A    =         6723145
66  meter
 Y    =       -4460078
65  meter          E    =           
0008657
 Z    =       -4678567
46                 I    =           51
93555
 XDOT =       5033
837218                 Wp   =            9
22343
 YDOT =       5083
892633  meter/sec      RA   =           63
36509  deg
 ZDOT =      -2835
561448                 TA   =          232
83335
                                          MA   =          232
91244
                                          Ha   =            190
054  n
mi
                                          Hp   =            186
535

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6108570
93                 X    =         1934355
46
 Y    =      -14632803
96  feet           Y    =        -4438852
59  meter
 Z    =      -15349630
79                 Z    =        -4669346
32
 XDOT =      16515
213970                 XDOT =        4990
388963
 YDOT =      16679
437772  feet/sec       YDOT =        5139
941131  meter/sec
 ZDOT =      -9303
023125                 ZDOT =       -2811
212076

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6576988
06                 X    =        -2004665
96
 Y    =      -14467256
27  feet           Y    =        -4409619
71  meter
 Z    =      -15312951
38                 Z    =        -4667387
58
 XDOT =      22438
105556                 XDOT =        6839
134573
 YDOT =       -429
902708  feet/sec       YDOT =        -131
034345  meter/sec
 ZDOT =      -9205
999497                 ZDOT =       -2805
988647


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   10130
52076062  
00016717  00000-0  10270-3 0  9077
2 25544  51
6447  63
8918 0010164 298
9949  61
0195 15
73847775 17549


Satellite: ISS
Catalog Number: 25544
Epoch time:      10130
52076062   =   yrday
fracday
Element set:     907
Inclination:       51
6447  deg
RA of node:        63
8918  deg
Eccentricity:     
0010164     
Arg of perigee:   298
9949  deg
Mean anomaly:      61
0195  deg
Mean motion:   15
73847775  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1754
Checksum:              330


Coasting Arc #9 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2010/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4790117
86                 A    =         6729871
62  meter
 Y    =       -4009817
21  meter          E    =           
0005174
 Z    =        2502481
61                 I    =           51
94429
 XDOT =       1636
858693                 Wp   =           67
78406
 YDOT =      -5294
904148  meter/sec      RA   =           58
20951  deg
 ZDOT =      -5340
379227                 TA   =           84
03452
                                          MA   =           83
97556
                                          Ha   =            190
211  n
mi
                                          Hp   =            186
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15715609
78                 X    =        -4757080
20
 Y    =      -13155568
27  feet           Y    =        -4063198
53  meter
 Z    =        8210241
50                 Z    =         2479290
84
 XDOT =       5370
271303                 XDOT =        1721
888732
 YDOT =     -17371
732770  feet/sec       YDOT =       -5276
124187  meter/sec
 ZDOT =     -17520
929223                 ZDOT =       -5332
220866

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20303955
12                 X    =        -6188645
52
 Y    =        3050791
62  feet           Y    =          929881
28  meter
 Z    =        8117851
31                 Z    =         2474321
08
 XDOT =      -9132
093187                 XDOT =       -2783
462003
 YDOT =     -14147
755058  feet/sec       YDOT =       -4312
235742  meter/sec
 ZDOT =     -17488
481162                 ZDOT =       -5330
489058


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   10131
53668836  
00016717  00000-0  10270-3 0  9086
2 25544  51
6452  58
6764 0010206 302
6272  57
3906 15
73875088 17709


Satellite: ISS
Catalog Number: 25544
Epoch time:      10131
53668836   =   yrday
fracday
Element set:     908
Inclination:       51
6452  deg
RA of node:        58
6764  deg
Eccentricity:     
0010206     
Arg of perigee:   302
6272  deg
Mean anomaly:      57
3906  deg
Mean motion:   15
73875088  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1770
Checksum:              319


Coasting Arc #10 (Orbit 1785)
---------------------------------------

Vector Time (GMT): 2010/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1003339
27                 A    =         6722995
53  meter
 Y    =        4745445
69  meter          E    =           
0002572
 Z    =        4655218
86                 I    =           51
90507
 XDOT =      -5870
860897                 Wp   =          335
70987
 YDOT =      -4064
874072  meter/sec      RA   =           53
13811  deg
 ZDOT =       2881
165302                 TA   =           85
91627
                                          MA   =           85
88687
                                          Ha   =            190
364  n
mi
                                          Hp   =            185
967

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3291795
49                 X    =        -1078943
84
 Y    =       15569047
53  feet           Y    =         4733802
74  meter
 Z    =       15273027
77                 Z    =         4650161
17
 XDOT =     -19261
354650                 XDOT =       -5838
966897
 YDOT =     -13336
201023  feet/sec       YDOT =       -4130
347379  meter/sec
 ZDOT =       9452
642067                 ZDOT =        2852
721243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9615565
01                 X    =         2930824
22
 Y    =       12703781
00  feet           Y    =         3872112
45  meter
 Z    =       15252914
26                 Z    =         4649088
27
 XDOT =     -21772
469256                 XDOT =       -6636
248629
 YDOT =       5277
595557  feet/sec       YDOT =        1608
611126  meter/sec
 ZDOT =       9339
338738                 ZDOT =        2846
630447


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   10132
55259090  
00016717  00000-0  10270-3 0  9098
2 25544  51
6455  53
4606 0010199 306
0275  53
9943 15
73921703 17868


Satellite: ISS
Catalog Number: 25544
Epoch time:      10132
55259090   =   yrday
fracday
Element set:     909
Inclination:       51
6455  deg
RA of node:        53
4606  deg
Eccentricity:     
0010199     
Arg of perigee:   306
0275  deg
Mean anomaly:      53
9943  deg
Mean motion:   15
73921703  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1786
Checksum:              310


Coasting Arc #11 (Orbit 1800)
---------------------------------------

Vector Time (GMT): 2010/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5424983
36                 A    =         6729611
69  meter
 Y    =        3062478
09  meter          E    =           
0010751
 Z    =       -2526243
71                 I    =           51
90892
 XDOT =       -640
755529                 Wp   =          338
70901
 YDOT =       5527
934771  meter/sec      RA   =           47
97907  deg
 ZDOT =       5328
104734                 TA   =          352
76993
                                          MA   =          352
78542
                                          Ha   =            190
586  n
mi
                                          Hp   =            185
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17798501
84                 X    =         5402607
29
 Y    =       10047500
30  feet           Y    =         3123018
59  meter
 Z    =       -8288201
15                 Z    =        -2499942
63
 XDOT =      -2102
216301                 XDOT =        -728
405824
 YDOT =      18136
268935  feet/sec       YDOT =        5520
278923  meter/sec
 ZDOT =      17480
658575                 ZDOT =        5324
779442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19122496
72                 X    =         5828537
00
 Y    =       -7334478
46  feet           Y    =        -2235549
04  meter
 Z    =       -8183443
84                 Z    =        -2494313
68
 XDOT =      12025
434440                 XDOT =        3665
352417
 YDOT =      11873
766571  feet/sec       YDOT =        3619
124051  meter/sec
 ZDOT =      17467
437424                 ZDOT =        5324
074927


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   10133
50497813  
00016717  00000-0  10270-3 0  9103
2 25544  51
6461  48
5708 0010264 309
8484  50
1776 15
73949117 18019


Satellite: ISS
Catalog Number: 25544
Epoch time:      10133
50497813   =   yrday
fracday
Element set:     910
Inclination:       51
6461  deg
RA of node:        48
5708  deg
Eccentricity:     
0010264     
Arg of perigee:   309
8484  deg
Mean anomaly:      50
1776  deg
Mean motion:   15
73949117  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1801
Checksum:              306


Coasting Arc #12 (Orbit 1816)
---------------------------------------

Vector Time (GMT): 2010/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         135402
77                 A    =         6722770
85  meter
 Y    =       -4859189
26  meter          E    =           
0011114
 Z    =       -4651219
05                 I    =           51
86628
 XDOT =       6496
160601                 Wp   =           14
33021
 YDOT =       2948
599132  meter/sec      RA   =           42
90521  deg
 ZDOT =      -2882
248578                 TA   =          227
18292
                                          MA   =          227
27639
                                          Ha   =            190
612  n
mi
                                          Hp   =            185
377

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         444234
80                 X    =          212324
28
 Y    =      -15942221
99  feet           Y    =        -4857244
50  meter
 Z    =      -15259905
02                 Z    =        -4650374
94
 XDOT =      21312
862863                 XDOT =        6476
707753
 YDOT =       9673
881666  feet/sec       YDOT =        3021
134619  meter/sec
 ZDOT =      -9456
196122                 ZDOT =       -2850
736492

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12116858
03                 X    =        -3693218
33
 Y    =      -10374768
81  feet           Y    =        -3162229
53  meter
 Z    =      -15256553
06                 Z    =        -4650197
37
 XDOT =      20144
449044                 XDOT =        6140
028068
 YDOT =      -9762
017712  feet/sec       YDOT =       -2975
462999  meter/sec
 ZDOT =      -9330
689097                 ZDOT =       -2843
994037


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   10134
52083332  
00016717  00000-0  10270-3 0  9114
2 25544  51
6469  43
3552 0010270 314
0917  45
9400 15
74005356 18175


Satellite: ISS
Catalog Number: 25544
Epoch time:      10134
52083332   =   yrday
fracday
Element set:     911
Inclination:       51
6469  deg
RA of node:        43
3552  deg
Eccentricity:     
0010270     
Arg of perigee:   314
0917  deg
Mean anomaly:      45
9400  deg
Mean motion:   15
74005356  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1817
Checksum:              273


Coasting Arc #13 (Orbit 1832)
---------------------------------------

Vector Time (GMT): 2010/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5892442
14                 A    =         6729524
18  meter
 Y    =       -2083286
28  meter          E    =           
0007569
 Z    =        2495933
34                 I    =           51
86548
 XDOT =       -309
258537                 Wp   =           58
35867
 YDOT =      -5536
961299  meter/sec      RA   =           37
74294  deg
 ZDOT =      -5335
974381                 TA   =           93
50868
                                          MA   =           93
42211
                                          Ha   =            190
771  n
mi
                                          Hp   =            185
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19332159
24                 X    =        -5880833
51
 Y    =       -6834928
75  feet           Y    =        -2149114
49  meter
 Z    =        8188757
69                 Z    =         2467335
29
 XDOT =      -1014
627745                 XDOT =        -221
398616
 YDOT =     -18165
883528  feet/sec       YDOT =       -5539
927666  meter/sec
 ZDOT =     -17506
477628                 ZDOT =       -5337
264091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17252665
24                 X    =        -5258612
36
 Y    =       11164524
40  feet           Y    =         3402947
04  meter
 Z    =        8074857
37                 Z    =         2461216
53
 XDOT =     -14123
006579                 XDOT =       -4304
692405
 YDOT =      -9121
261022  feet/sec       YDOT =       -2780
160359  meter/sec
 ZDOT =     -17511
616053                 ZDOT =       -5337
540573


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   10135
53666482  
00016717  00000-0  10270-3 0  9120
2 25544  51
6465  38
1391 0010236 317
4602  42
5768 15
74007185 18334


Satellite: ISS
Catalog Number: 25544
Epoch time:      10135
53666482   =   yrday
fracday
Element set:     912
Inclination:       51
6465  deg
RA of node:        38
1391  deg
Eccentricity:     
0010236     
Arg of perigee:   317
4602  deg
Mean anomaly:      42
5768  deg
Mean motion:   15
74007185  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1833
Checksum:              298


Coasting Arc #14 (Orbit 1848)
---------------------------------------

Vector Time (GMT): 2010/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         654192
71                 A    =         6722487
72  meter
 Y    =        4785215
27  meter          E    =           
0004453
 Z    =        4673615
74                 I    =           51
81827
 XDOT =      -6934
020264                 Wp   =            6
87892
 YDOT =      -1806
820130  meter/sec      RA   =           32
66396  deg
 ZDOT =       2824
614518                 TA   =           55
33186
                                          MA   =           55
28989
                                          Ha   =            190
911  n
mi
                                          Hp   =            184
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2146301
55                 X    =          577931
10
 Y    =       15699525
18  feet           Y    =         4792103
79  meter
 Z    =       15333384
98                 Z    =         4676609
28
 XDOT =     -22749
410316                 XDOT =       -6927
022349
 YDOT =      -5927
887564  feet/sec       YDOT =       -1884
321738  meter/sec
 ZDOT =       9267
108000                 ZDOT =        2790
945385

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13819101
63                 X    =         4212062
18
 Y    =        7729714
09  feet           Y    =         2356016
86  meter
 Z    =       15345303
72                 Z    =         4677248
57
 XDOT =     -17812
034657                 XDOT =       -5429
108164
 YDOT =      13739
391524  feet/sec       YDOT =        4187
766537  meter/sec
 ZDOT =       9133
007168                 ZDOT =        2783
740585


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   10136
55247062  
00016717  00000-0  10270-3 0  9133
2 25544  51
6469  32
9224 0010328 321
4402  38
6023 15
74057228 18490


Satellite: ISS
Catalog Number: 25544
Epoch time:      10136
55247062   =   yrday
fracday
Element set:     913
Inclination:       51
6469  deg
RA of node:        32
9224  deg
Eccentricity:     
0010328     
Arg of perigee:   321
4402  deg
Mean anomaly:      38
6023  deg
Mean motion:   15
74057228  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1849
Checksum:              287


Coasting Arc #15 (Orbit 1863)
---------------------------------------

Vector Time (GMT): 2010/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 808518
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6175634
65                 A    =         6729370
00  meter
 Y    =        1057154
07  meter          E    =           
0012498
 Z    =       -2433244
68                 I    =           51
81588
 XDOT =       1193
005072                 Wp   =          350
41459
 YDOT =       5388
598419  meter/sec      RA   =           27
49808  deg
 ZDOT =       5377
160555                 TA   =          342
16188
                                          MA   =          342
20572
                                          Ha   =            191
095  n
mi
                                          Hp   =            184
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20261268
53                 X    =         6175174
71
 Y    =        3468353
25  feet           Y    =         1126211
46  meter
 Z    =       -7983086
23                 Z    =        -2403244
22
 XDOT =       3914
058635                 XDOT =        1106
538680
 YDOT =      17679
128670  feet/sec       YDOT =        5401
455107  meter/sec
 ZDOT =      17641
602871                 ZDOT =        5382
746932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14665716
30                 X    =         4470110
33
 Y    =      -14469237
00  feet           Y    =        -4410223
44  meter
 Z    =       -7863592
62                 Z    =        -2396823
03
 XDOT =      15526
137572                 XDOT =        4732
366732
 YDOT =       6151
936581  feet/sec       YDOT =        1875
110270  meter/sec
 ZDOT =      17663
844990                 ZDOT =        5383
939953


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   10137
50476626  
00016717  00000-0  10270-3 0  9140
2 25544  51
6472  28
0318 0010447 324
6378  35
4091 15
74106583 18649


Satellite: ISS
Catalog Number: 25544
Epoch time:      10137
50476626   =   yrday
fracday
Element set:     914
Inclination:       51
6472  deg
RA of node:        28
0318  deg
Eccentricity:     
0010447     
Arg of perigee:   324
6378  deg
Mean anomaly:      35
4091  deg
Mean motion:   15
74106583  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1864
Checksum:              303

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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