Date: February 9th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


There are no maneuvers



Coasting Arc #1 (Orbit 269)
---------------------------------------

Vector Time (GMT): 2010/036/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4330545
80                 A    =         6721403
75  meter
 Y    =       -3522716
55  meter          E    =           
0002507
 Z    =        3740767
10                 I    =           51
60193
 XDOT =       5842
586361                 Wp   =           21
74449
 YDOT =      -2671
214797  meter/sec      RA   =          187
04855  deg
 ZDOT =       4249
618198                 TA   =           23
51496
                                          MA   =           23
50350
                                          Ha   =            186
773  n
mi
                                          Hp   =            183
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14207827
42                 X    =        -4309004
03
 Y    =      -11557468
99  feet           Y    =        -3571022
87  meter
 Z    =       12272857
94                 Z    =         3719781
88
 XDOT =      19168
590422                 XDOT =        5851
378525
 YDOT =      -8763
828074  feet/sec       YDOT =       -2605
830423  meter/sec
 ZDOT =      13942
316924                 ZDOT =        4278
022425

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18034577
00                 X    =         5496939
07
 Y    =       -3497257
78  feet           Y    =        -1065964
17  meter
 Z    =       12189491
85                 Z    =         3715357
12
 XDOT =      -5824
649255                 XDOT =       -1775
353093
 YDOT =      18935
036979  feet/sec       YDOT =        5771
399271  meter/sec
 ZDOT =      14054
852690                 ZDOT =        4283
919100


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   10036
32061981  
00016717  00000-0  10270-3 0  9007
2 25544  51
6453 187
7709 0011359 288
7645  71
2286 15
75672958  2704


Satellite: ISS
Catalog Number: 25544
Epoch time:      10036
32061981   =   yrday
fracday
Element set:     900
Inclination:       51
6453  deg
RA of node:       187
7709  deg
Eccentricity:     
0011359     
Arg of perigee:   288
7645  deg
Mean anomaly:      71
2286  deg
Mean motion:   15
75672958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             270
Checksum:              325


Coasting Arc #2 (Orbit 284)
---------------------------------------

Vector Time (GMT): 2010/037/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5346416
07                 A    =         6722511
67  meter
 Y    =        2417711
38  meter          E    =           
0007599
 Z    =       -3270452
90                 I    =           51
63605
 XDOT =      -4662
500442                 Wp   =          308
26713
 YDOT =      -3900
834532  meter/sec      RA   =          181
84707  deg
 ZDOT =       4735
582407                 TA   =           13
34960
                                          MA   =           13
32950
                                          Ha   =            186
839  n
mi
                                          Hp   =            183
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17540735
13                 X    =        -5357166
95
 Y    =        7932123
95  feet           Y    =         2357864
57  meter
 Z    =      -10729832
33                 Z    =        -3296451
46
 XDOT =     -15296
917461                 XDOT =       -4641
538366
 YDOT =     -12798
013557  feet/sec       YDOT =       -3952
856302  meter/sec
 ZDOT =      15536
687686                 ZDOT =        4712
983110

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4852510
87                 X    =         1479045
31
 Y    =      -18569538
77  feet           Y    =        -5659995
42  meter
 Z    =      -10832850
46                 Z    =        -3301852
82
 XDOT =      18279
176283                 XDOT =        5571
492931
 YDOT =      -4239
831764  feet/sec       YDOT =       -1292
300722  meter/sec
 ZDOT =      15446
897275                 ZDOT =        4708
214289


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   10037
27192728  
00016717  00000-0  10270-3 0  9017
2 25544  51
6447 182
8734 0011579 292
1418  67
8516 15
75725879  2856


Satellite: ISS
Catalog Number: 25544
Epoch time:      10037
27192728   =   yrday
fracday
Element set:     901
Inclination:       51
6447  deg
RA of node:       182
8734  deg
Eccentricity:     
0011579     
Arg of perigee:   292
1418  deg
Mean anomaly:      67
8516  deg
Mean motion:   15
75725879  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             285
Checksum:              337


Coasting Arc #3 (Orbit 300)
---------------------------------------

Vector Time (GMT): 2010/038/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3750048
01                 A    =         6718544
68  meter
 Y    =        3331318
29  meter          E    =           
0008614
 Z    =       -4473065
58                 I    =           51
65202
 XDOT =      -6384
055017                 Wp   =          350
81107
 YDOT =       2890
617217  meter/sec      RA   =          176
74776  deg
 ZDOT =      -3190
166649                 TA   =          247
25378
                                          MA   =          247
34484
                                          Ha   =            187
197  n
mi
                                          Hp   =            183
293

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12303307
13                 X    =         3734246
89
 Y    =       10929521
96  feet           Y    =         3373165
38  meter
 Z    =      -14675412
00                 Z    =        -4454886
40
 XDOT =     -20945
062391                 XDOT =       -6400
406943
 YDOT =       9483
652286  feet/sec       YDOT =        2819
135631  meter/sec
 ZDOT =     -10466
426013                 ZDOT =       -3221
219468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16243567
31                 X    =        -4951039
32
 Y    =        3014553
23  feet           Y    =          918835
82  meter
 Z    =      -14603168
29                 Z    =        -4451045
69
 XDOT =       5630
805517                 XDOT =        1716
269522
 YDOT =     -21103
735304  feet/sec       YDOT =       -6432
418521  meter/sec
 ZDOT =     -10589
487367                 ZDOT =       -3227
675750


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   10038
28663428  
00016717  00000-0  10270-3 0  9020
2 25544  51
6438 177
6493 0011631 296
0890  63
9077 15
75759377  3014


Satellite: ISS
Catalog Number: 25544
Epoch time:      10038
28663428   =   yrday
fracday
Element set:     902
Inclination:       51
6438  deg
RA of node:       177
6493  deg
Eccentricity:     
0011631     
Arg of perigee:   296
0890  deg
Mean anomaly:      63
9077  deg
Mean motion:   15
75759377  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             301
Checksum:              328


Coasting Arc #4 (Orbit 316)
---------------------------------------

Vector Time (GMT): 2010/039/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5758242
73                 A    =         6724721
18  meter
 Y    =       -2648559
80  meter          E    =           
0003759
 Z    =        2247256
86                 I    =           51
70428
 XDOT =       3878
923657                 Wp   =           63
90639
 YDOT =       3787
861681  meter/sec      RA   =          171
55798  deg
 ZDOT =      -5466
196669                 TA   =           90
89238
                                          MA   =           90
84931
                                          Ha   =            187
368  n
mi
                                          Hp   =            182
923

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18891872
46                 X    =         5776514
88
 Y    =       -8689500
65  feet           Y    =        -2584065
65  meter
 Z    =        7372889
96                 Z    =         2275274
09
 XDOT =      12726
127485                 XDOT =        3862
832077
 YDOT =      12427
367719  feet/sec       YDOT =        3831
148380  meter/sec
 ZDOT =     -17933
716107                 ZDOT =       -5447
392158

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4433208
91                 X    =        -1351242
08
 Y    =       20275777
43  feet           Y    =         6180056
96  meter
 Z    =        7483934
89                 Z    =         2281103
35
 XDOT =     -16172
117809                 XDOT =       -4929
261508
 YDOT =       3066
239824  feet/sec       YDOT =         934
589898  meter/sec
 ZDOT =     -17858
964965                 ZDOT =       -5443
412521


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   10039
30131838  
00016717  00000-0  10270-3 0  9030
2 25544  51
6442 172
4250 0011614 300
7934  59
2087 15
75824778  3170


Satellite: ISS
Catalog Number: 25544
Epoch time:      10039
30131838   =   yrday
fracday
Element set:     903
Inclination:       51
6442  deg
RA of node:       172
4250  deg
Eccentricity:     
0011614     
Arg of perigee:   300
7934  deg
Mean anomaly:      59
2087  deg
Mean motion:   15
75824778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             317
Checksum:              294


Coasting Arc #5 (Orbit 332)
---------------------------------------

Vector Time (GMT): 2010/040/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2986860
06                 A    =         6716225
60  meter
 Y    =       -3344111
27  meter          E    =           
0005763
 Z    =        5003421
94                 I    =           51
70400
 XDOT =       6749
752248                 Wp   =          305
04170
 YDOT =      -3178
249371  meter/sec      RA   =          166
44829  deg
 ZDOT =       1909
913679                 TA   =          126
56366
                                          MA   =          126
51060
                                          Ha   =            187
685  n
mi
                                          Hp   =            182
899

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9799409
65                 X    =        -2973548
75
 Y    =      -10971493
66  feet           Y    =        -3377437
89  meter
 Z    =       16415426
30                 Z    =         4988944
31
 XDOT =      22144
856458                 XDOT =        6775
512554
 YDOT =     -10427
327334  feet/sec       YDOT =       -3102
625691  meter/sec
 ZDOT =       6266
120993                 ZDOT =        1942
765606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14694971
94                 X    =         4479027
45
 Y    =       -1531937
18  feet           Y    =         -466934
45  meter
 Z    =       16357851
07                 Z    =         4985873
00
 XDOT =      -4711
649703                 XDOT =       -1436
110830
 YDOT =      22934
996880  feet/sec       YDOT =        6990
587049  meter/sec
 ZDOT =       6396
342471                 ZDOT =        1949
605185


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   10040
31598121  
00016717  00000-0  10270-3 0  9046
2 25544  51
6434 167
1994 0011555 304
7583  55
2492 15
75799262  3338


Satellite: ISS
Catalog Number: 25544
Epoch time:      10040
31598121   =   yrday
fracday
Element set:     904
Inclination:       51
6434  deg
RA of node:       167
1994  deg
Eccentricity:     
0011555     
Arg of perigee:   304
7583  deg
Mean anomaly:      55
2492  deg
Mean motion:   15
75799262  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             333
Checksum:              308


Coasting Arc #6 (Orbit 347)
---------------------------------------

Vector Time (GMT): 2010/041/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5963515
75                 A    =         6726389
05  meter
 Y    =        2902063
31  meter          E    =           
0015157
 Z    =       -1059140
46                 I    =           51
76724
 XDOT =      -2966
267704                 Wp   =          347
62633
 YDOT =      -3929
890192  meter/sec      RA   =          161
27874  deg
 ZDOT =       5932
650966                 TA   =             
79212
                                          MA   =             
78972
                                          Ha   =            187
765  n
mi
                                          Hp   =            182
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19565340
39                 X    =        -5990378
95
 Y    =        9521205
08  feet           Y    =         2835225
58  meter
 Z    =       -3474870
27                 Z    =        -1088175
56
 XDOT =      -9731
849422                 XDOT =       -2950
921455
 YDOT =     -12893
340525  feet/sec       YDOT =       -3962
975143  meter/sec
 ZDOT =      19464
077972                 ZDOT =        5918
278388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3453244
20                 X    =         1052548
83
 Y    =      -21464338
16  feet           Y    =        -6542330
27  meter
 Z    =       -3589972
97                 Z    =        -1094223
76
 XDOT =      14644
744919                 XDOT =        4463
718251
 YDOT =       -890
313317  feet/sec       YDOT =        -271
367499  meter/sec
 ZDOT =      19406
888506                 ZDOT =        5915
219617


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   10041
26720385  
00016717  00000-0  10270-3 0  9051
2 25544  51
6426 162
3006 0011716 308
0457  51
9649 15
75852919  3488


Satellite: ISS
Catalog Number: 25544
Epoch time:      10041
26720385   =   yrday
fracday
Element set:     905
Inclination:       51
6426  deg
RA of node:       162
3006  deg
Eccentricity:     
0011716     
Arg of perigee:   308
0457  deg
Mean anomaly:      51
9649  deg
Mean motion:   15
75852919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             348
Checksum:              303


Coasting Arc #7 (Orbit 363)
---------------------------------------

Vector Time (GMT): 2010/042/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2174841
42                 A    =         6714751
75  meter
 Y    =        3571327
89  meter          E    =           
0010842
 Z    =       -5259942
75                 I    =           51
75591
 XDOT =      -6864
387913                 Wp   =           35
81943
 YDOT =       3452
941744  meter/sec      RA   =          156
15214  deg
 ZDOT =       -485
683562                 TA   =          229
52632
                                          MA   =          229
62088
                                          Ha   =            187
953  n
mi
                                          Hp   =            182
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7135306
49                 X    =         2160295
63
 Y    =       11716955
00  feet           Y    =         3595567
01  meter
 Z    =      -17257030
01                 Z    =        -5249412
96
 XDOT =     -22520
957721                 XDOT =       -6900
129855
 YDOT =      11328
549029  feet/sec       YDOT =        3375
980254  meter/sec
 ZDOT =      -1593
450006                 ZDOT =        -519
116498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13758827
61                 X    =        -4193690
65
 Y    =        -582908
50  feet           Y    =         -177670
51  meter
 Z    =      -17215097
98                 Z    =        -5247161
86
 XDOT =       3209
216987                 XDOT =         978
169338
 YDOT =     -23987
006002  feet/sec       YDOT =       -7311
239429  meter/sec
 ZDOT =      -1725
997247                 ZDOT =        -526
083961


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   10042
28182081  
00016717  00000-0  10270-3 0  9060
2 25544  51
6418 157
0753 0011591 312
1251  47
8927 15
75909554  3647


Satellite: ISS
Catalog Number: 25544
Epoch time:      10042
28182081   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:       157
0753  deg
Eccentricity:     
0011591     
Arg of perigee:   312
1251  deg
Mean anomaly:      47
8927  deg
Mean motion:   15
75909554  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             364
Checksum:              301


Coasting Arc #8 (Orbit 379)
---------------------------------------

Vector Time (GMT): 2010/043/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5968311
73                 A    =         6726565
13  meter
 Y    =       -3093320
60  meter          E    =           
0000125
 Z    =        -237457
31                 I    =           51
82429
 XDOT =       2001
219184                 Wp   =          146
42575
 YDOT =       4325
140940  meter/sec      RA   =          151
01124  deg
 ZDOT =      -6045
424367                 TA   =           36
14806
                                          MA   =           36
14722
                                          Ha   =            188
087  n
mi
                                          Hp   =            181
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19581075
22                 X    =         6003611
70
 Y    =      -10148689
62  feet           Y    =        -3026382
02  meter
 Z    =        -779059
42                 Z    =         -208378
42
 XDOT =       6565
679738                 XDOT =        1982
072608
 YDOT =      14190
094948  feet/sec       YDOT =        4347
412695  meter/sec
 ZDOT =     -19834
069445                 ZDOT =       -6035
749265

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2209648
75                 X    =         -673500
94
 Y    =       21947624
19  feet           Y    =         6689635
85  meter
 Z    =        -663766
59                 Z    =         -202316
06
 XDOT =     -13934
012099                 XDOT =       -4247
086888
 YDOT =      -2001
343799  feet/sec       YDOT =        -610
009590  meter/sec
 ZDOT =     -19795
493755                 ZDOT =       -6033
666496


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   10043
29641409  
00016717  00000-0  10270-3 0  9077
2 25544  51
6426 151
8508 0011732 316
5032  43
5206 15
75965495  3805


Satellite: ISS
Catalog Number: 25544
Epoch time:      10043
29641409   =   yrday
fracday
Element set:     907
Inclination:       51
6426  deg
RA of node:       151
8508  deg
Eccentricity:     
0011732     
Arg of perigee:   316
5032  deg
Mean anomaly:      43
5206  deg
Mean motion:   15
75965495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             380
Checksum:              296


Coasting Arc #9 (Orbit 395)
---------------------------------------

Vector Time (GMT): 2010/044/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1336521
70                 A    =         6714896
74  meter
 Y    =       -4037507
09  meter          E    =           
0011643
 Z    =        5201678
19                 I    =           51
81008
 XDOT =       6736
998541                 Wp   =          338
06570
 YDOT =      -3580
796442  meter/sec      RA   =          145
86188  deg
 ZDOT =      -1038
541632                 TA   =          121
87231
                                          MA   =          121
75895
                                          Ha   =            188
255  n
mi
                                          Hp   =            181
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4384913
71                 X    =        -1316542
27
 Y    =      -13246414
35  feet           Y    =        -4052341
05  meter
 Z    =       17065873
34                 Z    =         5195234
19
 XDOT =      22103
013585                 XDOT =        6781
583826
 YDOT =     -11748
019823  feet/sec       YDOT =       -3505
210062  meter/sec
 ZDOT =      -3407
288819                 ZDOT =       -1005
705948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13601206
80                 X    =         4145647
83
 Y    =        3252710
15  feet           Y    =          991426
05  meter
 Z    =       17040130
41                 Z    =         5193831
75
 XDOT =      -1590
975526                 XDOT =        -484
929340
 YDOT =      23989
922830  feet/sec       YDOT =        7312
128479  meter/sec
 ZDOT =      -3277
093856                 ZDOT =        -998
858207


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   10044
31098621  
00016717  00000-0  10270-3 0  9084
2 25544  51
6421 146
6247 0011544 319
9936  40
0376 15
75944202  3963


Satellite: ISS
Catalog Number: 25544
Epoch time:      10044
31098621   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:       146
6247  deg
Eccentricity:     
0011544     
Arg of perigee:   319
9936  deg
Mean anomaly:      40
0376  deg
Mean motion:   15
75944202  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             396
Checksum:              301


Coasting Arc #10 (Orbit 411)
---------------------------------------

Vector Time (GMT): 2010/045/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5742694
72                 A    =         6725470
26  meter
 Y    =        3107596
68  meter          E    =           
0016857
 Z    =        1563346
76                 I    =           51
87009
 XDOT =      -1109
529311                 Wp   =           19
95626
 YDOT =      -4966
489810  meter/sec      RA   =          140
74817  deg
 ZDOT =       5793
977785                 TA   =          357
26174
                                          MA   =          357
27095
                                          Ha   =            188
412  n
mi
                                          Hp   =            181
455

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18840861
93                 X    =        -5784611
84
 Y    =       10195527
15  feet           Y    =         3043144
15  meter
 Z    =        5129090
41                 Z    =         1535347
63
 XDOT =      -3640
188027                 XDOT =       -1082
055950
 YDOT =     -16294
257906  feet/sec       YDOT =       -4978
743383  meter/sec
 ZDOT =      19009
113467                 ZDOT =        5788
654778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1043348
16                 X    =          318012
52
 Y    =      -21423464
87  feet           Y    =        -6529872
09  meter
 Z    =        5018067
20                 Z    =         1529506
88
 XDOT =      14321
187701                 XDOT =        4365
098011
 YDOT =       5147
101547  feet/sec       YDOT =        1568
836551  meter/sec
 ZDOT =      18987
780225                 ZDOT =        5787
475413


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   10045
32553366  
00016717  00000-0  10270-3 0  9099
2 25544  51
6417 141
3986 0011527 324
0787  35
9601 15
76002870  4122


Satellite: ISS
Catalog Number: 25544
Epoch time:      10045
32553366   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:       141
3986  deg
Eccentricity:     
0011527     
Arg of perigee:   324
0787  deg
Mean anomaly:      35
9601  deg
Mean motion:   15
76002870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             412
Checksum:              295


Coasting Arc #11 (Orbit 426)
---------------------------------------

Vector Time (GMT): 2010/046/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         641118
16                 A    =         6716306
48  meter
 Y    =        4652360
48  meter          E    =           
0008008
 Z    =       -4803546
41                 I    =           51
86257
 XDOT =      -6388
250588                 Wp   =           41
37204
 YDOT =       3481
644693  meter/sec      RA   =          135
57910  deg
 ZDOT =       2527
700712                 TA   =          253
24567
                                          MA   =          253
33355
                                          Ha   =            188
472  n
mi
                                          Hp   =            181
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2103406
03                 X    =          612381
14
 Y    =       15263649
86  feet           Y    =         4659368
90  meter
 Z    =      -15759666
71                 Z    =        -4800502
00
 XDOT =     -20958
827387                 XDOT =       -6438
986962
 YDOT =      11422
718809  feet/sec       YDOT =        3409
923943  meter/sec
 ZDOT =       8292
981339                 ZDOT =        2496
543977

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14297849
25                 X    =        -4357984
45
 Y    =       -5775949
16  feet           Y    =        -1760509
30  meter
 Z    =      -15747391
44                 Z    =        -4799804
91
 XDOT =        266
843841                 XDOT =          81
334003
 YDOT =     -22859
507690  feet/sec       YDOT =       -6967
577944  meter/sec
 ZDOT =       8169
430928                 ZDOT =        2490
042547


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   10046
27665131  
00016717  00000-0  10270-3 0  9100
2 25544  51
6418 136
4996 0011381 328
1232  31
9242 15
76047062  4272


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
27665131   =   yrday
fracday
Element set:     910
Inclination:       51
6418  deg
RA of node:       136
4996  deg
Eccentricity:     
0011381     
Arg of perigee:   328
1232  deg
Mean anomaly:      31
9242  deg
Mean motion:   15
76047062  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             427
Checksum:              286


Coasting Arc #12 (Orbit 442)
---------------------------------------

Vector Time (GMT): 2010/047/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5378611
86                 A    =         6722784
63  meter
 Y    =       -2882823
33  meter          E    =           
0008008
 Z    =       -2830304
67                 I    =           51
90562
 XDOT =        376
943338                 Wp   =          351
68396
 YDOT =       5735
818421  meter/sec      RA   =          130
48881  deg
 ZDOT =      -5116
376797                 TA   =          220
63442
                                          MA   =          220
69421
                                          Ha   =            188
597  n
mi
                                          Hp   =            180
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17646364
36                 X    =         5424197
16
 Y    =       -9458081
80  feet           Y    =        -2822421
81  meter
 Z    =       -9285776
49                 Z    =        -2804065
04
 XDOT =       1236
690741                 XDOT =         337
630269
 YDOT =      18818
301905  feet/sec       YDOT =        5739
813473  meter/sec
 ZDOT =     -16786
013115                 ZDOT =       -5114
641519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -378670
15                 X    =         -115418
66
 Y    =       20065587
94  feet           Y    =         6115991
20  meter
 Z    =       -9181716
67                 Z    =        -2798587
24
 XDOT =     -15614
960066                 XDOT =       -4759
439828
 YDOT =      -7986
944491  feet/sec       YDOT =       -2434
420681  meter/sec
 ZDOT =     -16778
892857                 ZDOT =       -5114
206543


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   10047
29115389  
00016717  00000-0  10270-3 0  9119
2 25544  51
6419 131
2743 0011515 332
7517  27
3042 15
76103919  4431


Satellite: ISS
Catalog Number: 25544
Epoch time:      10047
29115389   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:       131
2743  deg
Eccentricity:     
0011515     
Arg of perigee:   332
7517  deg
Mean anomaly:      27
3042  deg
Mean motion:   15
76103919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             443
Checksum:              284


Coasting Arc #13 (Orbit 458)
---------------------------------------

Vector Time (GMT): 2010/048/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -72420
17                 A    =         6719123
09  meter
 Y    =       -5373308
23  meter          E    =           
0014028
 Z    =        4037608
27                 I    =           51
91119
 XDOT =       5900
514168                 Wp   =           24
91111
 YDOT =      -3030
048357  meter/sec      RA   =          125
30665  deg
 ZDOT =      -3909
252119                 TA   =          105
34061
                                          MA   =          105
18554
                                          Ha   =            188
702  n
mi
                                          Hp   =            180
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -237598
98                 X    =          -31943
13
 Y    =      -17628964
00  feet           Y    =        -5373891
47  meter
 Z    =       13246746
30                 Z    =         4037355
15
 XDOT =      19358
642283                 XDOT =        5952
948272
 YDOT =      -9941
103535  feet/sec       YDOT =       -2963
772406  meter/sec
 ZDOT =     -12825
630313                 ZDOT =       -3880
460362

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15683387
36                 X    =         4780296
47
 Y    =        8056080
54  feet           Y    =         2455493
35  meter
 Z    =       13245529
05                 Z    =         4037237
25
 XDOT =        160
400439                 XDOT =          48
890054
 YDOT =      20681
022248  feet/sec       YDOT =        6303
575581  meter/sec
 ZDOT =     -12711
437250                 ZDOT =       -3874
446074


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   10048
30563436  
00016717  00000-0  10270-3 0  9123
2 25544  51
6411 126
0477 0011376 336
0558  24
0076 15
76095839  4595


Satellite: ISS
Catalog Number: 25544
Epoch time:      10048
30563436   =   yrday
fracday
Element set:     912
Inclination:       51
6411  deg
RA of node:       126
0477  deg
Eccentricity:     
0011376     
Arg of perigee:   336
0558  deg
Mean anomaly:      24
0076  deg
Mean motion:   15
76095839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             459
Checksum:              302


Coasting Arc #14 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4918357
95                 A    =         6719360
61  meter
 Y    =        2327713
82  meter          E    =           
0011211
 Z    =        3929538
06                 I    =           51
92943
 XDOT =        139
181291                 Wp   =           39
42495
 YDOT =      -6554
280478  meter/sec      RA   =          120
22597  deg
 ZDOT =       4058
929898                 TA   =            8
62022
                                          MA   =            8
60098
                                          Ha   =            188
859  n
mi
                                          Hp   =            180
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16136344
99                 X    =        -4963110
04
 Y    =        7636856
37  feet           Y    =         2272463
86  meter
 Z    =       12892185
24                 Z    =         3905536
16
 XDOT =        456
631532                 XDOT =         192
744796
 YDOT =     -21503
544876  feet/sec       YDOT =       -6552
424315  meter/sec
 ZDOT =      13316
699142                 ZDOT =        4059
736566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         626422
27                 X    =          190933
51
 Y    =      -17909680
49  feet           Y    =        -5458870
61  meter
 Z    =       12796975
62                 Z    =         3900518
17
 XDOT =      17641
470831                 XDOT =        5377
120309
 YDOT =      10129
088767  feet/sec       YDOT =        3087
346256  meter/sec
 ZDOT =      13319
650120                 ZDOT =        4059
829357


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   10049
32009019  
00016717  00000-0  10270-3 0  9139
2 25544  51
6415 120
8212 0011336 339
9015  20
1702 15
76169660  4759


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32009019   =   yrday
fracday
Element set:     913
Inclination:       51
6415  deg
RA of node:       120
8212  deg
Eccentricity:     
0011336     
Arg of perigee:   339
9015  deg
Mean anomaly:      20
1702  deg
Mean motion:   15
76169660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              272


Coasting Arc #15 (Orbit 489)
---------------------------------------

Vector Time (GMT): 2010/050/06:21:43
892
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -252209
25                 A    =         6722117
79  meter
 Y    =        6020417
53  meter          E    =           
0012581
 Z    =       -2964822
13                 I    =           51
95416
 XDOT =      -5392
851238                 Wp   =            5
47194
 YDOT =       2243
938288  meter/sec      RA   =          115
04569  deg
 ZDOT =       5029
312248                 TA   =          320
43070
                                          MA   =          320
52247
                                          Ha   =            188
907  n
mi
                                          Hp   =            179
980

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -827458
15                 X    =         -305109
46
 Y    =       19752026
02  feet           Y    =         6017301
24  meter
 Z    =       -9727106
72                 Z    =        -2966176
17
 XDOT =     -17693
081489                 XDOT =       -5441
973778
 YDOT =       7362
002257  feet/sec       YDOT =        2183
357838  meter/sec
 ZDOT =      16500
368269                 ZDOT =        5002
994618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17375469
38                 X    =        -5296043
07
 Y    =       -9424436
27  feet           Y    =        -2872568
17  meter
 Z    =       -9732260
21                 Z    =        -2966392
91
 XDOT =        575
163954                 XDOT =         175
309973
 YDOT =     -17944
556527  feet/sec       YDOT =       -5469
500830  meter/sec
 ZDOT =      16395
953327                 ZDOT =        4997
486574


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   10050
27112312  
00016717  00000-0  10270-3 0  9147
2 25544  51
6425 115
9221 0011322 344
2397  15
8413 15
76185467  4902


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
27112312   =   yrday
fracday
Element set:     914
Inclination:       51
6425  deg
RA of node:       115
9221  deg
Eccentricity:     
0011322     
Arg of perigee:   344
2397  deg
Mean anomaly:      15
8413  deg
Mean motion:   15
76185467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             490
Checksum:              273

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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