Date: March 11th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 18836 84 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 763)
---------------------------------------

Vector Time (GMT): 2010/067/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6234802
97                 A    =         6730671
74  meter
 Y    =        1045767
73  meter          E    =           
0013586
 Z    =       -2295663
59                 I    =           51
81059
 XDOT =       1106
466435                 Wp   =           32
18011
 YDOT =       5321
865514  meter/sec      RA   =           26
11907  deg
 ZDOT =       5455
335592                 TA   =          302
08120
                                          MA   =          302
21303
                                          Ha   =            192
727  n
mi
                                          Hp   =            182
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20455390
31                 X    =         6233797
35
 Y    =        3430996
50  feet           Y    =         1115483
32  meter
 Z    =       -7531704
71                 Z    =        -2265377
91
 XDOT =       3630
139224                 XDOT =        1020
373567
 YDOT =      17460
188693  feet/sec       YDOT =        5333
757445  meter/sec
 ZDOT =      17898
082651                 ZDOT =        5460
501464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16820256
55                 X    =         5126814
20
 Y    =      -12209495
86  feet           Y    =        -3721454
34  meter
 Z    =       -7411375
44                 Z    =        -2258987
23
 XDOT =      14030
020551                 XDOT =        4276
350264
 YDOT =       8503
839446  feet/sec       YDOT =        2591
970263  meter/sec
 ZDOT =      17918
706991                 ZDOT =        5461
621891


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   10067
67113940  
00016717  00000-0  10270-3 0  9002
2 25544  51
6488  26
6488 0007819  24
1633 335
9895 15
73746945  7642


Satellite: ISS
Catalog Number: 25544
Epoch time:      10067
67113940   =   yrday
fracday
Element set:     900
Inclination:       51
6488  deg
RA of node:        26
6488  deg
Eccentricity:     
0007819     
Arg of perigee:    24
1633  deg
Mean anomaly:     335
9895  deg
Mean motion:   15
73746945  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             764
Checksum:              338


Coasting Arc #2 (Orbit 779)
---------------------------------------

Vector Time (GMT): 2010/068/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1443844
14                 A    =         6723017
77  meter
 Y    =       -4559344
27  meter          E    =           
0017924
 Z    =       -4741953
17                 I    =           51
75796
 XDOT =       7188
652573                 Wp   =           53
22008
 YDOT =        507
495855  meter/sec      RA   =           21
03651  deg
 ZDOT =      -2673
210459                 TA   =          190
47779
                                          MA   =          190
51519
                                          Ha   =            192
674  n
mi
                                          Hp   =            182
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4737021
46                 X    =        -1369718
34
 Y    =      -14958478
58  feet           Y    =        -4575075
90  meter
 Z    =      -15557589
14                 Z    =        -4748787
02
 XDOT =      23584
818152                 XDOT =        7195
429101
 YDOT =       1665
012649  feet/sec       YDOT =         587
921434  meter/sec
 ZDOT =      -8770
375521                 ZDOT =       -2638
272246

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14043872
28                 X    =        -4280572
27
 Y    =       -6936637
72  feet           Y    =        -2114287
18  meter
 Z    =      -15584824
09                 Z    =        -4750254
38
 XDOT =      16982
356658                 XDOT =        5176
222309
 YDOT =     -14963
235532  feet/sec       YDOT =       -4560
794190  meter/sec
 ZDOT =      -8631
573660                 ZDOT =       -2630
903652


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   10068
68713421  
00016717  00000-0  10270-3 0  9015
2 25544  51
6491  21
4339 0007864  27
3490 332
8086 15
73783857  7809


Satellite: ISS
Catalog Number: 25544
Epoch time:      10068
68713421   =   yrday
fracday
Element set:     901
Inclination:       51
6491  deg
RA of node:        21
4339  deg
Eccentricity:     
0007864     
Arg of perigee:    27
3490  deg
Mean anomaly:     332
8086  deg
Mean motion:   15
73783857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             780
Checksum:              318


Coasting Arc #3 (Orbit 795)
---------------------------------------

Vector Time (GMT): 2010/069/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6292390
47                 A    =         6730441
09  meter
 Y    =         155696
46  meter          E    =           
0017698
 Z    =        2372968
72                 I    =           51
75390
 XDOT =      -2174
373279                 Wp   =           81
17621
 YDOT =      -5041
776060  meter/sec      RA   =           15
86985  deg
 ZDOT =      -5398
225279                 TA   =           72
13291
                                          MA   =           71
93996
                                          Ha   =            192
794  n
mi
                                          Hp   =            182
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20644325
69                 X    =        -6305191
03
 Y    =         510815
15  feet           Y    =           85259
76  meter
 Z    =        7785330
45                 Z    =         2342369
86
 XDOT =      -7133
770601                 XDOT =       -2091
610609
 YDOT =     -16541
260041  feet/sec       YDOT =       -5065
628714  meter/sec
 ZDOT =     -17710
712859                 ZDOT =       -5408
586872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13615335
18                 X    =        -4149954
16
 Y    =       15586841
02  feet           Y    =         4750869
14  meter
 Z    =        7663779
78                 Z    =         2335920
08
 XDOT =     -15802
752564                 XDOT =       -4816
678981
 YDOT =      -5015
382351  feet/sec       YDOT =       -1528
688541  meter/sec
 ZDOT =     -17751
971505                 ZDOT =       -5410
800915


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   10069
70311080  
00016717  00000-0  10270-3 0  9025
2 25544  51
6489  16
2186 0007818  32
0999 328
0639 15
73777997  7960


Satellite: ISS
Catalog Number: 25544
Epoch time:      10069
70311080   =   yrday
fracday
Element set:     902
Inclination:       51
6489  deg
RA of node:        16
2186  deg
Eccentricity:     
0007818     
Arg of perigee:    32
0999  deg
Mean anomaly:     328
0639  deg
Mean motion:   15
73777997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             796
Checksum:              339


Coasting Arc #4 (Orbit 811)
---------------------------------------

Vector Time (GMT): 2010/070/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2338546
40                 A    =         6723080
11  meter
 Y    =        4208781
83  meter          E    =           
0011717
 Z    =        4681242
07                 I    =           51
70083
 XDOT =      -7137
687762                 Wp   =           75
69427
 YDOT =        873
419526  meter/sec      RA   =           10
78367  deg
 ZDOT =       2777
492044                 TA   =          346
96060
                                          MA   =          346
99087
                                          Ha   =            192
728  n
mi
                                          Hp   =            182
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7672396
34                 X    =         2268569
13
 Y    =       13808339
35  feet           Y    =         4234541
90  meter
 Z    =       15358405
76                 Z    =         4692432
22
 XDOT =     -23417
610768                 XDOT =       -7160
416261
 YDOT =       2865
549627  feet/sec       YDOT =         793
474767  meter/sec
 ZDOT =       9112
506706                 ZDOT =        2742
762672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15361986
40                 X    =         4682333
46
 Y    =        3489315
47  feet           Y    =         1063543
35  meter
 Z    =       15402940
63                 Z    =         4694816
30
 XDOT =     -13174
175798                 XDOT =       -4015
488783
 YDOT =      18341
620608  feet/sec       YDOT =        5590
525961  meter/sec
 ZDOT =       8974
563903                 ZDOT =        2735
447078


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   10070
71906562  
00016717  00000-0  10270-3 0  9034
2 25544  51
6493  11
0031 0007861  35
0501 325
1178 15
73818058  8126


Satellite: ISS
Catalog Number: 25544
Epoch time:      10070
71906562   =   yrday
fracday
Element set:     903
Inclination:       51
6493  deg
RA of node:        11
0031  deg
Eccentricity:     
0007861     
Arg of perigee:    35
0501  deg
Mean anomaly:     325
1178  deg
Mean motion:   15
73818058  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             812
Checksum:              274


Coasting Arc #5 (Orbit 826)
---------------------------------------

Vector Time (GMT): 2010/071/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6109723
10                 A    =         6730023
22  meter
 Y    =       -1356839
95  meter          E    =           
0013233
 Z    =       -2465751
95                 I    =           51
69434
 XDOT =       3158
186131                 Wp   =           40
91449
 YDOT =       4553
317582  meter/sec      RA   =            5
61118  deg
 ZDOT =       5345
781298                 TA   =          291
23791
                                          MA   =          291
37920
                                          Ha   =            192
788  n
mi
                                          Hp   =            182
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20045023
30                 X    =         6136419
37
 Y    =       -4451574
65  feet           Y    =        -1288368
34  meter
 Z    =       -8089737
37                 Z    =        -2436006
59
 XDOT =      10361
503055                 XDOT =        3081
067110
 YDOT =      14938
705977  feet/sec       YDOT =        4588
203554  meter/sec
 ZDOT =      17538
652553                 ZDOT =        5360
935733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9689492
84                 X    =         2953357
42
 Y    =      -18155730
17  feet           Y    =        -5533866
56  meter
 Z    =       -7971606
93                 Z    =        -2429745
79
 XDOT =      16695
289911                 XDOT =        5088
724365
 YDOT =       1220
789683  feet/sec       YDOT =         372
096695  meter/sec
 ZDOT =      17598
942421                 ZDOT =        5364
157650


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   10071
67150478  
00016717  00000-0  10270-3 0  9048
2 25544  51
6491   6
1136 0007803  37
0306 323
1395 15
73852144  8275


Satellite: ISS
Catalog Number: 25544
Epoch time:      10071
67150478   =   yrday
fracday
Element set:     904
Inclination:       51
6491  deg
RA of node:         6
1136  deg
Eccentricity:     
0007803     
Arg of perigee:    37
0306  deg
Mean anomaly:     323
1395  deg
Mean motion:   15
73852144  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             827
Checksum:              287


Coasting Arc #6 (Orbit 842)
---------------------------------------

Vector Time (GMT): 2010/072/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3120438
55                 A    =         6722985
26  meter
 Y    =       -3721617
91  meter          E    =           
0018085
 Z    =       -4666277
13                 I    =           51
64053
 XDOT =       6811
628399                 Wp   =           57
85520
 YDOT =      -2171
393973  meter/sec      RA   =             
52129  deg
 ZDOT =      -2821
792968                 TA   =          184
21967
                                          MA   =          184
23494
                                          Ha   =            192
692  n
mi
                                          Hp   =            181
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10237659
29                 X    =        -3055923
33
 Y    =      -12210032
50  feet           Y    =        -3756152
25  meter
 Z    =      -15309308
18                 Z    =        -4681278
86
 XDOT =      22347
862201                 XDOT =        6849
110565
 YDOT =      -7123
995975  feet/sec       YDOT =       -2095
013004  meter/sec
 ZDOT =      -9257
850946                 ZDOT =       -2788
611442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15876484
58                 X    =        -4839152
50
 Y    =          36752
11  feet           Y    =           11202
04  meter
 Z    =      -15368974
10                 Z    =        -4684463
31
 XDOT =       8791
255935                 XDOT =        2679
574809
 YDOT =     -20645
052828  feet/sec       YDOT =       -6292
612102  meter/sec
 ZDOT =      -9126
094171                 ZDOT =       -2781
633503


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   10072
68742080  
00016717  00000-0  10270-3 0  9057
2 25544  51
6486    
8978 0007714  40
4919 319
6817 15
73889526  8434


Satellite: ISS
Catalog Number: 25544
Epoch time:      10072
68742080   =   yrday
fracday
Element set:     905
Inclination:       51
6486  deg
RA of node:          
8978  deg
Eccentricity:     
0007714     
Arg of perigee:    40
4919  deg
Mean anomaly:     319
6817  deg
Mean motion:   15
73889526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             843
Checksum:              335


Coasting Arc #7 (Orbit 858)
---------------------------------------

Vector Time (GMT): 2010/073/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5766808
96                 A    =         6729781
61  meter
 Y    =        2427568
83  meter          E    =           
0018960
 Z    =        2465135
99                 I    =           51
63396
 XDOT =      -3943
299644                 Wp   =           83
87323
 YDOT =      -3914
510462  meter/sec      RA   =          355
34416  deg
 ZDOT =      -5332
916136                 TA   =           68
25361
                                          MA   =           68
05191
                                          Ha   =            192
745  n
mi
                                          Hp   =            181
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18919976
90                 X    =        -5805500
87
 Y    =        7964464
67  feet           Y    =         2362864
88  meter
 Z    =        8087716
51                 Z    =         2437027
00
 XDOT =     -12937
334791                 XDOT =       -3873
327855
 YDOT =     -12842
882094  feet/sec       YDOT =       -3958
216145  meter/sec
 ZDOT =     -17496
444016                 ZDOT =       -5351
902002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5612193
97                 X    =        -1710596
72
 Y    =       19791264
60  feet           Y    =         6032377
45  meter
 Z    =        7976121
00                 Z    =         2431121
68
 XDOT =     -16601
441082                 XDOT =       -5060
119242
 YDOT =       2423
619977  feet/sec       YDOT =         738
719369  meter/sec
 ZDOT =     -17571
937071                 ZDOT =       -5355
926419


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   10073
70331694  
00016717  00000-0  10270-3 0  9067
2 25544  51
6491 355
6825 0007811  44
5357 315
6432 15
73940294  8597


Satellite: ISS
Catalog Number: 25544
Epoch time:      10073
70331694   =   yrday
fracday
Element set:     906
Inclination:       51
6491  deg
RA of node:       355
6825  deg
Eccentricity:     
0007811     
Arg of perigee:    44
5357  deg
Mean anomaly:     315
6432  deg
Mean motion:   15
73940294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             859
Checksum:              318


Coasting Arc #8 (Orbit 874)
---------------------------------------

Vector Time (GMT): 2010/074/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3740454
70                 A    =         6722920
02  meter
 Y    =        3092012
70  meter          E    =           
0012991
 Z    =        4640728
30                 I    =           51
58007
 XDOT =      -6322
177728                 Wp   =           82
67773
 YDOT =       3374
032627  meter/sec      RA   =          350
24947  deg
 ZDOT =       2842
536419                 TA   =          339
22194
                                          MA   =          339
27470
                                          Ha   =            192
700  n
mi
                                          Hp   =            181
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12271833
02                 X    =         3683057
68
 Y    =       10144398
62  feet           Y    =         3133520
31  meter
 Z    =       15225486
55                 Z    =         4658759
46
 XDOT =     -20742
052914                 XDOT =       -6373
245272
 YDOT =      11069
660850  feet/sec       YDOT =        3303
049078  meter/sec
 ZDOT =       9325
906888                 ZDOT =        2811
699161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15471886
63                 X    =         4715831
04
 Y    =       -3455366
83  feet           Y    =        -1053195
81  meter
 Z    =       15297166
86                 Z    =         4662576
46
 XDOT =      -4180
241053                 XDOT =       -1274
137473
 YDOT =      22101
212564  feet/sec       YDOT =        6736
449589  meter/sec
 ZDOT =       9203
503241                 ZDOT =        2805
227788


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10074
71919381  
00016717  00000-0  10270-3 0  9075
2 25544  51
6482 350
4662 0007785  48
3978 311
7851 15
73919911  8752


Satellite: ISS
Catalog Number: 25544
Epoch time:      10074
71919381   =   yrday
fracday
Element set:     907
Inclination:       51
6482  deg
RA of node:       350
4662  deg
Eccentricity:     
0007785     
Arg of perigee:    48
3978  deg
Mean anomaly:     311
7851  deg
Mean motion:   15
73919911  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             875
Checksum:              341


Coasting Arc #9 (Orbit 889)
---------------------------------------

Vector Time (GMT): 2010/075/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5224968
39                 A    =         6729620
35  meter
 Y    =       -3433574
60  meter          E    =           
0012995
 Z    =       -2484530
20                 I    =           51
57247
 XDOT =       4586
245047                 Wp   =           49
59766
 YDOT =       3146
977679  meter/sec      RA   =          345
06663  deg
 ZDOT =       5322
273779                 TA   =          282
27684
                                          MA   =          282
42232
                                          Ha   =            192
703  n
mi
                                          Hp   =            181
525

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17142284
74                 X    =         5275044
23
 Y    =      -11265008
53  feet           Y    =        -3374866
20  meter
 Z    =       -8151345
80                 Z    =        -2459025
41
 XDOT =      15046
735718                 XDOT =        4524
859615
 YDOT =      10324
729919  feet/sec       YDOT =        3197
921199  meter/sec
 ZDOT =      17461
528145                 ZDOT =        5344
404157

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1219070
30                 X    =          371572
63
 Y    =      -20516141
79  feet           Y    =        -6253320
02  meter
 Z    =       -8050128
91                 Z    =        -2453679
29
 XDOT =      15706
940197                 XDOT =        4787
475372
 YDOT =      -5918
269578  feet/sec       YDOT =       -1803
888567  meter/sec
 ZDOT =      17549
485273                 ZDOT =        5349
083111


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10075
67155720  
00016717  00000-0  10270-3 0  9081
2 25544  51
6472 345
5759 0007578  51
3717 308
8123 15
73975688  8907


Satellite: ISS
Catalog Number: 25544
Epoch time:      10075
67155720   =   yrday
fracday
Element set:     908
Inclination:       51
6472  deg
RA of node:       345
5759  deg
Eccentricity:     
0007578     
Arg of perigee:    51
3717  deg
Mean anomaly:     308
8123  deg
Mean motion:   15
73975688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             890
Checksum:              342


Coasting Arc #10 (Orbit 905)
---------------------------------------

Vector Time (GMT): 2010/076/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4213715
23                 A    =         6722614
97  meter
 Y    =       -2412583
27  meter          E    =           
0018469
 Z    =       -4667396
76                 I    =           51
51933
 XDOT =       5630
228963                 Wp   =           64
20757
 YDOT =      -4420
681376  meter/sec      RA   =          339
96740  deg
 ZDOT =      -2798
590827                 TA   =          178
07694
                                          MA   =          178
06983
                                          Ha   =            192
657  n
mi
                                          Hp   =            181
235

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13824525
03                 X    =        -4163750
77
 Y    =       -7915299
44  feet           Y    =        -2459424
68  meter
 Z    =      -15312981
50                 Z    =        -4687745
34
 XDOT =      18471
879800                 XDOT =        5692
838392
 YDOT =     -14503
547823  feet/sec       YDOT =       -4357
371045  meter/sec
 ZDOT =      -9181
728434                 ZDOT =       -2771
086653

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14437315
92                 X    =        -4400493
89
 Y    =        6546021
96  feet           Y    =         1995227
49  meter
 Z    =      -15393841
80                 Z    =        -4692042
98
 XDOT =       -509
688022                 XDOT =        -155
352909
 YDOT =     -22454
258244  feet/sec       YDOT =       -6844
057913  meter/sec
 ZDOT =      -9072
597954                 ZDOT =       -2765
327857


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10076
68739319  
00016717  00000-0  10270-3 0  9096
2 25544  51
6460 340
3596 0007576  55
6688 304
5191 15
74008429  9065


Satellite: ISS
Catalog Number: 25544
Epoch time:      10076
68739319   =   yrday
fracday
Element set:     909
Inclination:       51
6460  deg
RA of node:       340
3596  deg
Eccentricity:     
0007576     
Arg of perigee:    55
6688  deg
Mean anomaly:     304
5191  deg
Mean motion:   15
74008429  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             906
Checksum:              335


Coasting Arc #11 (Orbit 921)
---------------------------------------

Vector Time (GMT): 2010/077/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4593711
53                 A    =         6729459
98  meter
 Y    =        4278889
34  meter          E    =           
0019749
 Z    =        2407230
75                 I    =           51
51563
 XDOT =      -5013
036343                 Wp   =           89
18570
 YDOT =      -2346
613406  meter/sec      RA   =          334
78063  deg
 ZDOT =      -5357
197410                 TA   =           63
59581
                                          MA   =           63
39324
                                          Ha   =            192
565  n
mi
                                          Hp   =            181
233

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15071232
05                 X    =        -4652911
33
 Y    =       14038350
85  feet           Y    =         4227188
95  meter
 Z    =        7897738
68                 Z    =         2384770
27
 XDOT =     -16446
969630                 XDOT =       -4960
399160
 YDOT =      -7698
862880  feet/sec       YDOT =       -2402
378345  meter/sec
 ZDOT =     -17576
106989                 ZDOT =       -5381
422712

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2947205
85                 X    =          898308
34
 Y    =       20418882
50  feet           Y    =         6223675
38  meter
 Z    =        7808637
64                 Z    =         2380072
75
 XDOT =     -14139
732025                 XDOT =       -4309
790321
 YDOT =       8847
447189  feet/sec       YDOT =        2696
701903  meter/sec
 ZDOT =     -17672
356237                 ZDOT =       -5386
534181


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10077
70320686  
00016717  00000-0  10270-3 0  9105
2 25544  51
6466 335
1430 0007529  57
7814 302
4078 15
74090682  9223


Satellite: ISS
Catalog Number: 25544
Epoch time:      10077
70320686   =   yrday
fracday
Element set:     910
Inclination:       51
6466  deg
RA of node:       335
1430  deg
Eccentricity:     
0007529     
Arg of perigee:    57
7814  deg
Mean anomaly:     302
4078  deg
Mean motion:   15
74090682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             922
Checksum:              302


Coasting Arc #12 (Orbit 937)
---------------------------------------

Vector Time (GMT): 2010/078/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4513326
48                 A    =         6722380
74  meter
 Y    =        1677830
16  meter          E    =           
0013540
 Z    =        4679378
09                 I    =           51
46338
 XDOT =      -4831
274276                 Wp   =           90
42168
 YDOT =       5349
457863  meter/sec      RA   =          329
67553  deg
 ZDOT =       2734
848744                 TA   =          332
57396
                                          MA   =          332
64536
                                          Ha   =            192
552  n
mi
                                          Hp   =            181
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14807501
59                 X    =         4471497
59
 Y    =        5504692
12  feet           Y    =         1728067
32  meter
 Z    =       15352290
32                 Z    =         4701202
18
 XDOT =     -15850
637389                 XDOT =       -4904
019245
 YDOT =      17550
714773  feet/sec       YDOT =        5295
025141  meter/sec
 ZDOT =       8972
600867                 ZDOT =        2711
201248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12742678
54                 X    =         3883968
42
 Y    =       -9193387
47  feet           Y    =        -2802144
50  meter
 Z    =       15438987
24                 Z    =         4705803
31
 XDOT =       5114
626118                 XDOT =        1558
938041
 YDOT =      22037
681922  feet/sec       YDOT =        6717
085450  meter/sec
 ZDOT =       8878
809651                 ZDOT =        2706
261182


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10078
71900396  
00016717  00000-0  10270-3 0  9110
2 25544  51
6452 329
9257 0007570  63
0621 297
1315 15
74046819  9382


Satellite: ISS
Catalog Number: 25544
Epoch time:      10078
71900396   =   yrday
fracday
Element set:     911
Inclination:       51
6452  deg
RA of node:       329
9257  deg
Eccentricity:     
0007570     
Arg of perigee:    63
0621  deg
Mean anomaly:     297
1315  deg
Mean motion:   15
74046819  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             938
Checksum:              316


Coasting Arc #13 (Orbit 952)
---------------------------------------

Vector Time (GMT): 2010/079/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3810942
92                 A    =         6729507
54  meter
 Y    =       -5021749
77  meter          E    =           
0012996
 Z    =       -2352242
01                 I    =           51
46182
 XDOT =       5286
680172                 Wp   =           57
68895
 YDOT =       1500
867087  meter/sec      RA   =          324
48439  deg
 ZDOT =       5389
419528                 TA   =          275
76399
                                          MA   =          275
91215
                                          Ha   =            192
608  n
mi
                                          Hp   =            181
046

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12503093
57                 X    =         3878240
59
 Y    =      -16475556
98  feet           Y    =        -4978757
38  meter
 Z    =       -7717329
43                 Z    =        -2333564
67
 XDOT =      17344
751219                 XDOT =        5243
323378
 YDOT =       4924
104616  feet/sec       YDOT =        1559
743743  meter/sec
 ZDOT =      17681
822600                 ZDOT =        5414
996908

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7086662
86                 X    =        -2160014
84
 Y    =      -19459912
12  feet           Y    =        -5931381
22  meter
 Z    =       -7643266
96                 Z    =        -2329667
77
 XDOT =      12038
236664                 XDOT =        3669
254535
 YDOT =     -11331
683826  feet/sec       YDOT =       -3453
897230  meter/sec
 ZDOT =      17783
418579                 ZDOT =        5420
385983


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10079
67129162  
00016717  00000-0  10270-3 0  9121
2 25544  51
6446 325
0343 0007496  68
0002 292
1957 15
74105805  9538


Satellite: ISS
Catalog Number: 25544
Epoch time:      10079
67129162   =   yrday
fracday
Element set:     912
Inclination:       51
6446  deg
RA of node:       325
0343  deg
Eccentricity:     
0007496     
Arg of perigee:    68
0002  deg
Mean anomaly:     292
1957  deg
Mean motion:   15
74105805  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             953
Checksum:              303


Coasting Arc #14 (Orbit 968)
---------------------------------------

Vector Time (GMT): 2010/080/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4678125
65                 A    =         6721888
81  meter
 Y    =        -975719
28  meter          E    =           
0019203
 Z    =       -4745445
55                 I    =           51
41266
 XDOT =       3906
199790                 Wp   =           71
46812
 YDOT =      -6086
449033  meter/sec      RA   =          319
37477  deg
 ZDOT =      -2601
940972                 TA   =          172
88130
                                          MA   =          172
85400
                                          Ha   =            192
593  n
mi
                                          Hp   =            180
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15348181
28                 X    =        -4643814
76
 Y    =       -3201178
74  feet           Y    =        -1027841
18  meter
 Z    =      -15569047
09                 Z    =        -4768088
53
 XDOT =      12815
616108                 XDOT =        3986
608999
 YDOT =     -19968
664806  feet/sec       YDOT =       -6042
318082  meter/sec
 ZDOT =      -8536
551747                 ZDOT =       -2582
769121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10742808
90                 X    =        -3274408
15
 Y    =       11295920
05  feet           Y    =         3442996
43  meter
 Z    =      -15658981
07                 Z    =        -4772857
43
 XDOT =      -9401
484389                 XDOT =       -2865
572442
 YDOT =     -20657
816657  feet/sec       YDOT =       -6296
502517  meter/sec
 ZDOT =      -8460
546498                 ZDOT =       -2578
774573


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10080
68704624  
00016717  00000-0  10270-3 0  9137
2 25544  51
6444 319
8174 0007630  72
0513 288
1481 15
74146795  9698


Satellite: ISS
Catalog Number: 25544
Epoch time:      10080
68704624   =   yrday
fracday
Element set:     913
Inclination:       51
6444  deg
RA of node:       319
8174  deg
Eccentricity:     
0007630     
Arg of perigee:    72
0513  deg
Mean anomaly:     288
1481  deg
Mean motion:   15
74146795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             969
Checksum:              319


Coasting Arc #15 (Orbit 984)
---------------------------------------

Vector Time (GMT): 2010/081/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 798335
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2999609
32                 A    =         6729569
44  meter
 Y    =        5600697
04  meter          E    =           
0020565
 Z    =        2196221
83                 I    =           51
41665
 XDOT =      -5380
595470                 Wp   =           97
04970
 YDOT =       -721
777313  meter/sec      RA   =          314
18140  deg
 ZDOT =      -5467
007144                 TA   =           58
24537
                                          MA   =           58
04515
                                          Ha   =            192
461  n
mi
                                          Hp   =            180
877

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9841237
94                 X    =        -3072683
19
 Y    =       18374990
30  feet           Y    =         5566745
10  meter
 Z    =        7205452
20                 Z    =         2181472
15
 XDOT =     -17652
872278                 XDOT =       -5345
566881
 YDOT =      -2368
035805  feet/sec       YDOT =        -781
750603  meter/sec
 ZDOT =     -17936
375145                 ZDOT =       -5493
060889

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10746149
18                 X    =         3275426
27
 Y    =       17884336
16  feet           Y    =         5451145
66  meter
 Z    =        7146997
43                 Z    =         2178404
82
 XDOT =      -9697
000545                 XDOT =       -2955
645766
 YDOT =      13090
224175  feet/sec       YDOT =        3989
900329  meter/sec
 ZDOT =     -18039
850803                 ZDOT =       -5498
546525


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10081
70277822  
00016717  00000-0  10270-3 0  9147
2 25544  51
6444 314
5995 0007381  74
7162 285
4817 15
74192747  9852


Satellite: ISS
Catalog Number: 25544
Epoch time:      10081
70277822   =   yrday
fracday
Element set:     914
Inclination:       51
6444  deg
RA of node:       314
5995  deg
Eccentricity:     
0007381     
Arg of perigee:    74
7162  deg
Mean anomaly:     285
4817  deg
Mean motion:   15
74192747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             985
Checksum:              333

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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