Date: February 18th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 30138 95 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


049/06:58:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 7
000/00:00:00 000 0 0 0 0 180 1

049/07:11:30 000 0 0 0 7 0 7
N/A 0 7 -0 2 188 8
000/00:05:00 000 -0 2 -0 1 180 6

049/07:47:30 000 -0 5 1 7 1 7
N/A -1 3 0 2 190 3
000/00:33:00 000 1 0 0 1 180 7

049/08:11:30 000 0 2 0 4 0 5
N/A -0 5 0 0 190 4
000/00:05:00 000 -0 0 -0 3 180 8

Coasting Arc #1 (Orbit 462)
---------------------------------------

Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4823079
59                 A    =         6724106
20  meter
 Y    =        4163548
18  meter          E    =           
0017784
 Z    =        2111130
88                 I    =           51
93738
 XDOT =      -1875
956397                 Wp   =           30
47605
 YDOT =      -4998
315291  meter/sec      RA   =          124
15996  deg
 ZDOT =       5566
565941                 TA   =          353
06917
                                          MA   =          353
09373
                                          Ha   =            188
711  n
mi
                                          Hp   =            180
394

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15823751
93                 X    =        -4879533
98
 Y    =       13659934
96  feet           Y    =         4109298
13  meter
 Z    =        6926282
40                 Z    =         2087563
33
 XDOT =      -6154
712587                 XDOT =       -1846
965842
 YDOT =     -16398
672215  feet/sec       YDOT =       -5019
130865  meter/sec
 ZDOT =      18263
011616                 ZDOT =        5557
523465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20764470
96                 X    =        -6329010
75
 Y    =        2665879
03  feet           Y    =          812559
93  meter
 Z    =        6832874
28                 Z    =         2082660
08
 XDOT =       3997
949528                 XDOT =        1218
575016
 YDOT =     -15621
967169  feet/sec       YDOT =       -4761
575593  meter/sec
 ZDOT =      18226
913248                 ZDOT =        5555
563158


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
55930847  
00016717  00000-0  10270-3 0  9001
2 25544  51
6457 124
7558 0011285 338
0399  22
0280 15
76175425  4634


Satellite: ISS
Catalog Number: 25544
Epoch time:      10048
55930847   =   yrday
fracday
Element set:     900
Inclination:       51
6457  deg
RA of node:       124
7558  deg
Eccentricity:     
0011285     
Arg of perigee:   338
0399  deg
Mean anomaly:      22
0280  deg
Mean motion:   15
76175425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              309


Coasting Arc #2 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/06:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010367
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3988899
09                 A    =         6725380
00  meter
 Y    =       -5324669
13  meter          E    =           
0003916
 Z    =        -998767
65                 I    =           51
95220
 XDOT =       3303
890017                 Wp   =           42
32282
 YDOT =       3589
539942  meter/sec      RA   =          120
09096  deg
 ZDOT =      -5952
147430                 TA   =          148
54351
                                          MA   =          148
52009
                                          Ha   =            188
678  n
mi
                                          Hp   =            180
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13086939
27                 X    =         4052995
79
 Y    =      -17469386
92  feet           Y    =        -5279704
58  meter
 Z    =       -3276796
76                 Z    =         -979233
81
 XDOT =      10839
534176                 XDOT =        3292
419656
 YDOT =      11776
705846  feet/sec       YDOT =        3626
421477  meter/sec
 ZDOT =     -19528
042750                 ZDOT =       -5936
125449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12522132
97                 X    =         3816746
13
 Y    =       17892585
34  feet           Y    =         5453660
01  meter
 Z    =       -3199442
40                 Z    =         -975190
04
 XDOT =     -13296
150491                 XDOT =       -4052
666670
 YDOT =       5831
198215  feet/sec       YDOT =        1777
349216  meter/sec
 ZDOT =     -19464
289865                 ZDOT =       -5932
715551


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
32012087  
00016717  00000-0  10270-3 0  9015
2 25544  51
6427 120
8321 0011254 341
8518  18
2243 15
76242531  4759


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32012087   =   yrday
fracday
Element set:     901
Inclination:       51
6427  deg
RA of node:       120
8321  deg
Eccentricity:     
0011254     
Arg of perigee:   341
8518  deg
Mean anomaly:      18
2243  deg
Mean motion:   15
76242531  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              268


Coasting Arc #3 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/07:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010288
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4385792
67                 A    =         6715065
61  meter
 Y    =         371799
81  meter          E    =           
0016259
 Z    =       -5082613
07                 I    =           51
91712
 XDOT =      -2559
527386                 Wp   =           35
02435
 YDOT =       7058
979036  meter/sec      RA   =          120
03925  deg
 ZDOT =      -1681
863129                 TA   =          218
79498
                                          MA   =          218
91182
                                          Ha   =            188
768  n
mi
                                          Hp   =            180
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14389083
56                 X    =         4405999
26
 Y    =        1219815
66  feet           Y    =          420957
00  meter
 Z    =      -16675239
74                 Z    =        -5061258
13
 XDOT =      -8397
399559                 XDOT =       -2630
101836
 YDOT =      23159
380038  feet/sec       YDOT =        7029
962169  meter/sec
 ZDOT =      -5517
923653                 ZDOT =       -1694
469027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4717840
27                 X    =        -1437997
71
 Y    =       13751244
05  feet           Y    =         4191379
19  meter
 Z    =      -16590435
99                 Z    =        -5056764
89
 XDOT =     -19415
008012                 XDOT =       -5917
694442
 YDOT =     -13419
553649  feet/sec       YDOT =       -4090
279952  meter/sec
 ZDOT =      -5567
704239                 ZDOT =       -1697
036252


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
32012214  
00016717  00000-0  10270-3 0  9028
2 25544  51
6436 120
8330 0011061 339
2342  20
8371 15
76106210  4755


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32012214   =   yrday
fracday
Element set:     902
Inclination:       51
6436  deg
RA of node:       120
8330  deg
Eccentricity:     
0011061     
Arg of perigee:   339
2342  deg
Mean anomaly:      20
8371  deg
Mean motion:   15
76106210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              247


Coasting Arc #4 (Orbit 475)
---------------------------------------

Vector Time (GMT): 2010/049/08:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1009763
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3523678
22                 A    =         6715666
85  meter
 Y    =       -2181563
49  meter          E    =           
0012240
 Z    =        5285293
08                 I    =           51
91465
 XDOT =       3912
953601                 Wp   =          356
08896
 YDOT =      -6634
459005  meter/sec      RA   =          119
84525  deg
 ZDOT =       -117
764109                 TA   =           95
09381
                                          MA   =           94
95409
                                          Ha   =            190
303  n
mi
                                          Hp   =            180
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11560624
09                 X    =        -3524696
36
 Y    =       -7157360
54  feet           Y    =        -2220972
70  meter
 Z    =       17340200
40                 Z    =         5268172
95
 XDOT =      12837
774281                 XDOT =        3987
422549
 YDOT =     -21766
597784  feet/sec       YDOT =       -6590
285665  meter/sec
 ZDOT =       -386
365188                 ZDOT =         -98
573925

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7477908
50                 X    =         2279266
51
 Y    =      -11459162
37  feet           Y    =        -3492752
69  meter
 Z    =       17272141
48                 Z    =         5264548
72
 XDOT =      20566
214078                 XDOT =        6268
582051
 YDOT =      12893
743955  feet/sec       YDOT =        3930
013157  meter/sec
 ZDOT =       -310
425081                 ZDOT =         -94
617565


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
38354930  
00016717  00000-0  10270-3 0  9039
2 25544  51
6438 120
5055 0012440 345
0056  15
0738 15
75555283  4768


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
38354930   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:       120
5055  deg
Eccentricity:     
0012440     
Arg of perigee:   345
0056  deg
Mean anomaly:      15
0738  deg
Mean motion:   15
75555283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             476
Checksum:              291


Coasting Arc #5 (Orbit 475)
---------------------------------------

Vector Time (GMT): 2010/049/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1009683
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -556936
07                 A    =         6721062
56  meter
 Y    =       -5361710
80  meter          E    =           
0016059
 Z    =        4017867
97                 I    =           51
93186
 XDOT =       5583
937523                 Wp   =           29
11840
 YDOT =      -3546
476989  meter/sec      RA   =          119
78539  deg
 ZDOT =      -3938
359176                 TA   =          101
49781
                                          MA   =          101
31743
                                          Ha   =            190
364  n
mi
                                          Hp   =            180
844

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1827218
09                 X    =         -516456
89
 Y    =      -17590914
69  feet           Y    =        -5367712
20  meter
 Z    =       13181981
53                 Z    =         4015261
08
 XDOT =      18320
004997                 XDOT =        5642
311429
 YDOT =     -11635
423191  feet/sec       YDOT =       -3483
707955  meter/sec
 ZDOT =     -12921
125907                 ZDOT =       -3911
090757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17557901
42                 X    =         5351648
35
 Y    =       -2185701
91  feet           Y    =         -666201
94  meter
 Z    =       13171425
42                 Z    =         4014650
47
 XDOT =      11769
028683                 XDOT =        3587
199943
 YDOT =      16926
835874  feet/sec       YDOT =        5159
299574  meter/sec
 ZDOT =     -12812
992764                 ZDOT =       -3905
400194


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
38355316  
00016717  00000-0  10270-3 0  9049
2 25544  51
6437 120
5059 0012105 346
6235  13
4606 15
75443026  4762


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
38355316   =   yrday
fracday
Element set:     904
Inclination:       51
6437  deg
RA of node:       120
5059  deg
Eccentricity:     
0012105     
Arg of perigee:   346
6235  deg
Mean anomaly:      13
4606  deg
Mean motion:   15
75443026  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             476
Checksum:              285


Coasting Arc #6 (Orbit 491)
---------------------------------------

Vector Time (GMT): 2010/050/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4653267
69                 A    =         6721541
90  meter
 Y    =        2985747
48  meter          E    =           
0014038
 Z    =        3805931
20                 I    =           51
94910
 XDOT =       -675
404535                 Wp   =           41
93051
 YDOT =      -6422
779621  meter/sec      RA   =          114
71130  deg
 ZDOT =       4214
260234                 TA   =            4
12912
                                          MA   =            4
11755
                                          Ha   =            190
482  n
mi
                                          Hp   =            180
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15266626
28                 X    =        -4704797
34
 Y    =        9795759
45  feet           Y    =         2933423
96  meter
 Z    =       12486650
93                 Z    =         3783200
54
 XDOT =      -2215
894145                 XDOT =        -624
005579
 YDOT =     -21072
111619  feet/sec       YDOT =       -6430
044786  meter/sec
 ZDOT =      13826
313104                 ZDOT =        4211
104339

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10299756
48                 X    =        -3139365
77
 Y    =      -15006162
13  feet           Y    =        -4573878
22  meter
 Z    =       12396505
44                 Z    =         3778454
86
 XDOT =      19889
677633                 XDOT =        6062
373743
 YDOT =      -2244
103894  feet/sec       YDOT =        -684
002867  meter/sec
 ZDOT =      13813
544992                 ZDOT =        4210
368513


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
39842192  
00016717  00000-0  10270-3 0  9056
2 25544  51
6445 115
2827 0012177 350
2367   9
8559 15
75546767  4921


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
39842192   =   yrday
fracday
Element set:     905
Inclination:       51
6445  deg
RA of node:       115
2827  deg
Eccentricity:     
0012177     
Arg of perigee:   350
2367  deg
Mean anomaly:       9
8559  deg
Mean motion:   15
75546767  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              321


Coasting Arc #7 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2010/051/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         661077
70                 A    =         6723102
89  meter
 Y    =        5822223
61  meter          E    =           
0013141
 Z    =       -3285388
05                 I    =           51
96591
 XDOT =      -5108
304857                 Wp   =           14
94267
 YDOT =       3257
643524  meter/sec      RA   =          109
53610  deg
 ZDOT =       4761
769600                 TA   =          306
67475
                                          MA   =          306
79546
                                          Ha   =            190
621  n
mi
                                          Hp   =            180
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2168890
09                 X    =          611883
11
 Y    =       19101783
51  feet           Y    =         5829340
99  meter
 Z    =      -10778832
19                 Z    =        -3282296
27
 XDOT =     -16759
530372                 XDOT =       -5167
484355
 YDOT =      10687
806838  feet/sec       YDOT =        3200
188712  meter/sec
 ZDOT =      15622
603674                 ZDOT =        4736
809815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18964831
02                 X    =        -5780480
49
 Y    =        3191604
70  feet           Y    =          972801
11  meter
 Z    =      -10766349
65                 Z    =        -3281583
37
 XDOT =     -11290
746018                 XDOT =       -3441
419386
 YDOT =     -14908
282021  feet/sec       YDOT =       -4544
044360  meter/sec
 ZDOT =      15523
606712                 ZDOT =        4731
595326


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   10051
34983636  
00016717  00000-0  10270-3 0  9062
2 25544  51
6445 110
3867 0012395 353
8504   6
2506 15
75536865  5073


Satellite: ISS
Catalog Number: 25544
Epoch time:      10051
34983636   =   yrday
fracday
Element set:     906
Inclination:       51
6445  deg
RA of node:       110
3867  deg
Eccentricity:     
0012395     
Arg of perigee:   353
8504  deg
Mean anomaly:       6
2506  deg
Mean motion:   15
75536865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              309


Coasting Arc #8 (Orbit 522)
---------------------------------------

Vector Time (GMT): 2010/052/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4290436
05                 A    =         6719044
44  meter
 Y    =       -2618728
36  meter          E    =           
0017796
 Z    =       -4474438
60                 I    =           51
96201
 XDOT =        834
121883                 Wp   =           28
62061
 YDOT =       6923
313561  meter/sec      RA   =          104
46036  deg
 ZDOT =      -3242
163092                 TA   =          208
96640
                                          MA   =          209
06528
                                          Ha   =            190
603  n
mi
                                          Hp   =            179
997

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14076233
75                 X    =         4341136
06
 Y    =       -8591628
48  feet           Y    =        -2570466
77  meter
 Z    =      -14679916
65                 Z    =        -4453472
66
 XDOT =       2736
620350                 XDOT =         772
391860
 YDOT =      22714
283336  feet/sec       YDOT =        6932
295995  meter/sec
 ZDOT =     -10637
018017                 ZDOT =       -3238
261038

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9528976
07                 X    =         2904431
91
 Y    =       13549538
53  feet           Y    =         4129899
34  meter
 Z    =      -14596746
56                 Z    =        -4449088
35
 XDOT =     -21485
035897                 XDOT =       -6548
638941
 YDOT =       3632
100155  feet/sec       YDOT =        1107
064127  meter/sec
 ZDOT =     -10621
289707                 ZDOT =       -3237
369103


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   10052
36464737  
00016717  00000-0  10270-3 0  9072
2 25544  51
6449 105
1634 0012267 357
8805   2
2305 15
75595725  5238


Satellite: ISS
Catalog Number: 25544
Epoch time:      10052
36464737   =   yrday
fracday
Element set:     907
Inclination:       51
6449  deg
RA of node:       105
1634  deg
Eccentricity:     
0012267     
Arg of perigee:   357
8805  deg
Mean anomaly:       2
2305  deg
Mean motion:   15
75595725  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             523
Checksum:              304


Coasting Arc #9 (Orbit 538)
---------------------------------------

Vector Time (GMT): 2010/053/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -822431
37                 A    =         6725146
56  meter
 Y    =       -6255345
18  meter          E    =           
0016125
 Z    =        2330814
80                 I    =           51
98939
 XDOT =       4746
547945                 Wp   =           59
55376
 YDOT =      -2665
354326  meter/sec      RA   =           99
29259  deg
 ZDOT =      -5442
623206                 TA   =           94
35322
                                          MA   =           94
16896
                                          Ha   =            190
678  n
mi
                                          Hp   =            179
569

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2698265
63                 X    =         -763744
40
 Y    =      -20522786
01  feet           Y    =        -6264213
95  meter
 Z    =        7647030
20                 Z    =         2326962
05
 XDOT =      15572
663861                 XDOT =        4802
438598
 YDOT =      -8744
600806  feet/sec       YDOT =       -2611
963126  meter/sec
 ZDOT =     -17856
375347                 ZDOT =       -5419
428989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20216512
88                 X    =         6161993
13
 Y    =       -4471557
62  feet           Y    =        -1362930
76  meter
 Z    =        7631528
89                 Z    =         2326090
01
 XDOT =       9715
391106                 XDOT =        2961
251209
 YDOT =      13406
079649  feet/sec       YDOT =        4086
173077  meter/sec
 ZDOT =     -17764
346823                 ZDOT =       -5414
572912


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   10053
37942757  
00016717  00000-0  10270-3 0  9088
2 25544  51
6448  99
9402 0012283   2
5263 357
5961 15
75644840  5394


Satellite: ISS
Catalog Number: 25544
Epoch time:      10053
37942757   =   yrday
fracday
Element set:     908
Inclination:       51
6448  deg
RA of node:        99
9402  deg
Eccentricity:     
0012283     
Arg of perigee:     2
5263  deg
Mean anomaly:     357
5961  deg
Mean motion:   15
75644840  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             539
Checksum:              326


Coasting Arc #10 (Orbit 554)
---------------------------------------

Vector Time (GMT): 2010/054/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4044290
27                 A    =         6716548
56  meter
 Y    =        1995750
09  meter          E    =           
0010907
 Z    =        4969082
77                 I    =           51
96572
 XDOT =      -1086
021132                 Wp   =           35
40928
 YDOT =      -7346
757295  meter/sec      RA   =           94
20502  deg
 ZDOT =       2073
255402                 TA   =           34
66526
                                          MA   =           34
59421
                                          Ha   =            190
796  n
mi
                                          Hp   =            179
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13268668
86                 X    =        -4090445
04
 Y    =        6547736
51  feet           Y    =         1950266
34  meter
 Z    =       16302764
98                 Z    =         4949323
83
 XDOT =      -3563
061457                 XDOT =       -1013
859009
 YDOT =     -24103
534434  feet/sec       YDOT =       -7358
498363  meter/sec
 ZDOT =       6802
019037                 ZDOT =        2068
154823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7874923
51                 X    =        -2400276
69
 Y    =      -12628010
95  feet           Y    =        -3849017
74  meter
 Z    =       16224348
74                 Z    =         4945181
50
 XDOT =      22690
359457                 XDOT =        6916
021563
 YDOT =      -5464
365110  feet/sec       YDOT =       -1665
538486  meter/sec
 ZDOT =       6781
535108                 ZDOT =        2067
011901


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   10054
39417450  
00016717  00000-0  10270-3 0  9099
2 25544  51
6456  94
7160 0012343   6
1084 354
0229 15
75735803  5552


Satellite: ISS
Catalog Number: 25544
Epoch time:      10054
39417450   =   yrday
fracday
Element set:     909
Inclination:       51
6456  deg
RA of node:        94
7160  deg
Eccentricity:     
0012343     
Arg of perigee:     6
1084  deg
Mean anomaly:     354
0229  deg
Mean motion:   15
75735803  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             555
Checksum:              295


Coasting Arc #11 (Orbit 569)
---------------------------------------

Vector Time (GMT): 2010/055/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1089562
48                 A    =         6726617
17  meter
 Y    =        6505717
43  meter          E    =           
0021087
 Z    =       -1256793
50                 I    =           52
00048
 XDOT =      -4582
193819                 Wp   =           21
24540
 YDOT =       1898
437781  meter/sec      RA   =           89
05306  deg
 ZDOT =       5904
399883                 TA   =          325
01491
                                          MA   =          325
15328
                                          Ha   =            190
921  n
mi
                                          Hp   =            178
938

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3574680
06                 X    =         1022838
56
 Y    =       21344217
30  feet           Y    =         6517528
50  meter
 Z    =       -4123338
26                 Z    =        -1251662
54
 XDOT =     -15033
444289                 XDOT =       -4631
763829
 YDOT =       6228
470410  feet/sec       YDOT =        1846
919769  meter/sec
 ZDOT =      19371
390692                 ZDOT =        5882
019669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20764661
29                 X    =        -6329068
76
 Y    =        6111631
39  feet           Y    =         1862825
25  meter
 Z    =       -4102763
86                 Z    =        -1250522
43
 XDOT =      -7540
396042                 XDOT =       -2298
312714
 YDOT =     -12784
596387  feet/sec       YDOT =       -3896
744979  meter/sec
 ZDOT =      19282
550916                 ZDOT =        5877
321519


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   10055
34547363  
00016717  00000-0  10270-3 0  9104
2 25544  51
6457  89
8197 0012591   9
6324 350
5079 15
75715904  5709


Satellite: ISS
Catalog Number: 25544
Epoch time:      10055
34547363   =   yrday
fracday
Element set:     910
Inclination:       51
6457  deg
RA of node:        89
8197  deg
Eccentricity:     
0012591     
Arg of perigee:     9
6324  deg
Mean anomaly:     350
5079  deg
Mean motion:   15
75715904  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             570
Checksum:              317


Coasting Arc #12 (Orbit 585)
---------------------------------------

Vector Time (GMT): 2010/056/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4003046
11                 A    =         6715211
45  meter
 Y    =       -1263023
20  meter          E    =           
0022217
 Z    =       -5258036
52                 I    =           51
96021
 XDOT =       1383
433562                 Wp   =           52
26315
 YDOT =       7527
572689  meter/sec      RA   =           83
94698  deg
 ZDOT =       -743
794102                 TA   =          210
61737
                                          MA   =          210
74722
                                          Ha   =            190
869  n
mi
                                          Hp   =            178
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13133353
38                 X    =         4042413
87
 Y    =       -4143776
91  feet           Y    =        -1218038
68  meter
 Z    =      -17250775
99                 Z    =        -5238494
60
 XDOT =       4538
824021                 XDOT =        1302
769210
 YDOT =      24696
760790  feet/sec       YDOT =        7542
592041  meter/sec
 ZDOT =      -2440
269362                 ZDOT =        -737
269533

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5905385
16                 X    =         1799961
40
 Y    =       12548039
03  feet           Y    =         3824642
30  meter
 Z    =      -17173184
71                 Z    =        -5234386
70
 XDOT =     -22933
122787                 XDOT =       -6990
015825
 YDOT =       7438
553594  feet/sec       YDOT =        2267
271135  meter/sec
 ZDOT =      -2414
130844                 ZDOT =        -735
827081


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   10056
36016088  
00016717  00000-0  10270-3 0  9113
2 25544  51
6450  84
5960 0012442  13
4084 346
7409 15
75782630  5864


Satellite: ISS
Catalog Number: 25544
Epoch time:      10056
36016088   =   yrday
fracday
Element set:     911
Inclination:       51
6450  deg
RA of node:        84
5960  deg
Eccentricity:     
0012442     
Arg of perigee:    13
4084  deg
Mean anomaly:     346
7409  deg
Mean motion:   15
75782630  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             586
Checksum:              301


Coasting Arc #13 (Orbit 601)
---------------------------------------

Vector Time (GMT): 2010/057/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1310864
23                 A    =         6726906
53  meter
 Y    =       -6600170
92  meter          E    =           
0013003
 Z    =           7281
20                 I    =           51
99522
 XDOT =       4644
206798                 Wp   =           75
38333
 YDOT =       -938
956516  meter/sec      RA   =           78
81508  deg
 ZDOT =      -6063
488510                 TA   =          104
53799
                                          MA   =          104
39372
                                          Ha   =            190
888  n
mi
                                          Hp   =            178
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4300735
68                 X    =        -1236997
89
 Y    =      -21654104
08  feet           Y    =        -6614416
78  meter
 Z    =          23888
46                 Z    =            1092
84
 XDOT =      15236
898942                 XDOT =        4683
815679
 YDOT =      -3080
565996  feet/sec       YDOT =        -886
800970  meter/sec
 ZDOT =     -19893
335008                 ZDOT =       -6040
831380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20741079
38                 X    =         6321881
00
 Y    =       -7563381
97  feet           Y    =        -2305318
82  meter
 Z    =           -887
60                 Z    =            -270
54
 XDOT =       4842
417000                 XDOT =        1475
968702
 YDOT =      13188
905763  feet/sec       YDOT =        4019
978477  meter/sec
 ZDOT =     -19803
353986                 ZDOT =       -6036
062295


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   10057
37481627  
00016717  00000-0  10270-3 0  9121
2 25544  51
6442  79
3715 0012507  18
0929 342
0678 15
75850600  6025


Satellite: ISS
Catalog Number: 25544
Epoch time:      10057
37481627   =   yrday
fracday
Element set:     912
Inclination:       51
6442  deg
RA of node:        79
3715  deg
Eccentricity:     
0012507     
Arg of perigee:    18
0929  deg
Mean anomaly:     342
0678  deg
Mean motion:   15
75850600  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             602
Checksum:              300


Coasting Arc #14 (Orbit 617)
---------------------------------------

Vector Time (GMT): 2010/058/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4167297
48                 A    =         6714755
56  meter
 Y    =         381599
57  meter          E    =           
0014941
 Z    =        5246512
86                 I    =           51
94837
 XDOT =      -1610
222025                 Wp   =           28
62411
 YDOT =      -7504
490768  meter/sec      RA   =           73
68197  deg
 ZDOT =       -719
488091                 TA   =           68
26222
                                          MA   =           68
10325
                                          Ha   =            190
939  n
mi
                                          Hp   =            178
077

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13672235
83                 X    =        -4196740
73
 Y    =        1251967
10  feet           Y    =          334834
09  meter
 Z    =       17212968
70                 Z    =         5226197
19
 XDOT =      -5282
880661                 XDOT =       -1522
690760
 YDOT =     -24621
032705  feet/sec       YDOT =       -7522
007860  meter/sec
 ZDOT =      -2360
525233                 ZDOT =        -727
097228

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3575340
53                 X    =        -1089763
79
 Y    =      -13359864
51  feet           Y    =        -4072086
70  meter
 Z    =       17132270
90                 Z    =         5221916
17
 XDOT =      22392
936744                 XDOT =        6825
367120
 YDOT =      -9116
677757  feet/sec       YDOT =       -2778
763380  meter/sec
 ZDOT =      -2390
972280                 ZDOT =        -728
768351


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   10058
38943687  
00016717  00000-0  10270-3 0  9133
2 25544  51
6446  74
1461 0012465  21
1547 339
0130 15
75935905  6182


Satellite: ISS
Catalog Number: 25544
Epoch time:      10058
38943687   =   yrday
fracday
Element set:     913
Inclination:       51
6446  deg
RA of node:        74
1461  deg
Eccentricity:     
0012465     
Arg of perigee:    21
1547  deg
Mean anomaly:     339
0130  deg
Mean motion:   15
75935905  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             618
Checksum:              309


Coasting Arc #15 (Orbit 633)
---------------------------------------

Vector Time (GMT): 2010/059/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1467575
45                 A    =         6726021
45  meter
 Y    =        6427092
57  meter          E    =           
0025544
 Z    =        1255526
27                 I    =           51
97589
 XDOT =      -4969
056439                 Wp   =           42
90890
 YDOT =        -28
341184  meter/sec      RA   =           68
57299  deg
 ZDOT =       5902
142138                 TA   =          330
82965
                                          MA   =          330
97208
                                          Ha   =            191
042  n
mi
                                          Hp   =            177
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4814880
10                 X    =         1389498
53
 Y    =       21086261
71  feet           Y    =         6443067
43  meter
 Z    =        4119180
67                 Z    =         1262465
32
 XDOT =     -16302
678605                 XDOT =       -4997
041001
 YDOT =        -92
982888  feet/sec       YDOT =         -84
064048  meter/sec
 ZDOT =      19363
983394                 ZDOT =        5877
935131

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19819356
74                 X    =        -6040939
93
 Y    =        8647380
91  feet           Y    =         2635721
70  meter
 Z    =        4146933
14                 Z    =         1263985
22
 XDOT =      -2346
845508                 XDOT =        -715
318511
 YDOT =     -14698
978267  feet/sec       YDOT =       -4480
248576  meter/sec
 ZDOT =      19267
814284                 ZDOT =        5872
829794


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   10059
40402865  
00016717  00000-0  10270-3 0  9146
2 25544  51
6440  68
9212 0012699  25
8374 334
3421 15
75924916  6348


Satellite: ISS
Catalog Number: 25544
Epoch time:      10059
40402865   =   yrday
fracday
Element set:     914
Inclination:       51
6440  deg
RA of node:        68
9212  deg
Eccentricity:     
0012699     
Arg of perigee:    25
8374  deg
Mean anomaly:     334
3421  deg
Mean motion:   15
75924916  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             634
Checksum:              308


Coasting Arc #16 (Orbit 648)
---------------------------------------

Vector Time (GMT): 2010/060/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4541480
03                 A    =         6715995
10  meter
 Y    =         424782
33  meter          E    =           
0019795
 Z    =       -4942473
80                 I    =           51
93008
 XDOT =       1685
074059                 Wp   =           67
28122
 YDOT =       7182
596509  meter/sec      RA   =           63
41479  deg
 ZDOT =       2180
017208                 TA   =          223
73772
                                          MA   =          223
89471
                                          Ha   =            191
041  n
mi
                                          Hp   =            177
625

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14899868
88                 X    =         4560401
66
 Y    =        1393642
83  feet           Y    =          475673
12  meter
 Z    =      -16215465
24                 Z    =        -4920365
84
 XDOT =       5528
458200                 XDOT =        1594
041836
 YDOT =      23564
949178  feet/sec       YDOT =        7200
931257  meter/sec
 ZDOT =       7152
287427                 ZDOT =        2187
981236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1691614
05                 X    =          515603
96
 Y    =       14964216
36  feet           Y    =         4561093
15  meter
 Z    =      -16127625
88                 Z    =        -4915700
37
 XDOT =     -20861
437563                 XDOT =       -6358
566169
 YDOT =      10049
921569  feet/sec       YDOT =        3063
216094  meter/sec
 ZDOT =       7184
128906                 ZDOT =        2189
722491


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   10060
35517473  
00016717  00000-0  10270-3 0  9155
2 25544  51
6435  64
0223 0012680  29
3002 330
8871 15
75994519  6490


Satellite: ISS
Catalog Number: 25544
Epoch time:      10060
35517473   =   yrday
fracday
Element set:     915
Inclination:       51
6435  deg
RA of node:        64
0223  deg
Eccentricity:     
0012680     
Arg of perigee:    29
3002  deg
Mean anomaly:     330
8871  deg
Mean motion:   15
75994519  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             649
Checksum:              299


Coasting Arc #17 (Orbit 664)
---------------------------------------

Vector Time (GMT): 2010/061/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1397176
37                 A    =         6723444
46  meter
 Y    =       -6069931
95  meter          E    =           
0013306
 Z    =       -2552526
89                 I    =           51
94208
 XDOT =       5479
881878                 Wp   =           56
15618
 YDOT =        965
870836  meter/sec      RA   =           58
32363  deg
 ZDOT =      -5308
791747                 TA   =          152
63309
                                          MA   =          152
56294
                                          Ha   =            190
994  n
mi
                                          Hp   =            177
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4583911
99                 X    =        -1316797
94
 Y    =      -19914474
91  feet           Y    =        -6085106
87  meter
 Z    =       -8374432
04                 Z    =        -2559118
38
 XDOT =      17978
615086                 XDOT =        5494
462844
 YDOT =       3168
867573  feet/sec       YDOT =        1027
231081  meter/sec
 ZDOT =     -17417
295759                 ZDOT =       -5282
135558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18423817
51                 X    =         5615579
58
 Y    =       -8815864
94  feet           Y    =        -2687075
63  meter
 Z    =       -8400782
46                 Z    =        -2560558
49
 XDOT =        255
122008                 XDOT =          77
761188
 YDOT =      16990
754332  feet/sec       YDOT =        5178
781920  meter/sec
 ZDOT =     -17311
376851                 ZDOT =       -5276
507664


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   10061
36969913  
00016717  00000-0  10270-3 0  9168
2 25544  51
6442  58
7961 0012731  33
7692 326
4281 15
76065778  6659


Satellite: ISS
Catalog Number: 25544
Epoch time:      10061
36969913   =   yrday
fracday
Element set:     916
Inclination:       51
6442  deg
RA of node:        58
7961  deg
Eccentricity:     
0012731     
Arg of perigee:    33
7692  deg
Mean anomaly:     326
4281  deg
Mean motion:   15
76065778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             665
Checksum:              331


Coasting Arc #18 (Orbit 680)
---------------------------------------

Vector Time (GMT): 2010/062/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5062355
47                 A    =         6718352
56  meter
 Y    =       -1210626
80  meter          E    =           
0021641
 Z    =        4241306
45                 I    =           51
90852
 XDOT =      -1452
940138                 Wp   =           52
71037
 YDOT =      -6653
761987  meter/sec      RA   =           53
14558  deg
 ZDOT =      -3608
083053                 TA   =           73
90864
                                          MA   =           73
67048
                                          Ha   =            191
013  n
mi
                                          Hp   =            177
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16608777
79                 X    =        -5069045
08
 Y    =       -3971872
70  feet           Y    =        -1267274
07  meter
 Z    =       13915047
42                 Z    =         4216697
64
 XDOT =      -4766
863970                 XDOT =       -1360
901353
 YDOT =     -21829
927778  feet/sec       YDOT =       -6669
495354  meter/sec
 ZDOT =     -11837
542825                 ZDOT =       -3614
917174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -103098
45                 X    =          -31424
41
 Y    =      -17156005
36  feet           Y    =        -5229150
43  meter
 Z    =       13817259
78                 Z    =         4211500
78
 XDOT =      18840
625651                 XDOT =        5742
622698
 YDOT =      -9736
522946  feet/sec       YDOT =       -2967
692194  meter/sec
 ZDOT =     -11864
862810                 ZDOT =       -3616
410185


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   10062
38418755  
00016717  00000-0  10270-3 0  9175
2 25544  51
6442  53
5704 0012683  36
9292 323
2743 15
76141072  6812


Satellite: ISS
Catalog Number: 25544
Epoch time:      10062
38418755   =   yrday
fracday
Element set:     917
Inclination:       51
6442  deg
RA of node:        53
5704  deg
Eccentricity:     
0012683     
Arg of perigee:    36
9292  deg
Mean anomaly:     323
2743  deg
Mean motion:   15
76141072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             681
Checksum:              301


Coasting Arc #19 (Orbit 696)
---------------------------------------

Vector Time (GMT): 2010/063/08:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1064910
91                 A    =         6720104
71  meter
 Y    =        5504273
55  meter          E    =           
0021938
 Z    =        3680563
10                 I    =           51
89565
 XDOT =      -6136
792118                 Wp   =           67
27481
 YDOT =      -1728
339763  meter/sec      RA   =           48
06336  deg
 ZDOT =       4348
253262                 TA   =          336
94668
                                          MA   =          337
04497
                                          Ha   =            191
048  n
mi
                                          Hp   =            176
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3493802
20                 X    =          985402
61
 Y    =       18058640
27  feet           Y    =         5515737
74  meter
 Z    =       12075338
27                 Z    =         3685542
87
 XDOT =     -20133
832407                 XDOT =       -6138
132293
 YDOT =      -5670
406046  feet/sec       YDOT =       -1796
972187  meter/sec
 ZDOT =      14265
922776                 ZDOT =        4318
437817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16597208
69                 X    =        -5058829
21
 Y    =        7897623
31  feet           Y    =         2407195
59  meter
 Z    =       12095253
05                 Z    =         3686633
13
 XDOT =        924
624004                 XDOT =         281
825397
 YDOT =     -19784
223396  feet/sec       YDOT =       -6030
231291  meter/sec
 ZDOT =      14147
443880                 ZDOT =        4312
140895


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   10063
39864412  
00016717  00000-0  10270-3 0  9183
2 25544  51
6442  48
3445 0012820  41
9118 318
3025 15
76155710  6971


Satellite: ISS
Catalog Number: 25544
Epoch time:      10063
39864412   =   yrday
fracday
Element set:     918
Inclination:       51
6442  deg
RA of node:        48
3445  deg
Eccentricity:     
0012820     
Arg of perigee:    41
9118  deg
Mean anomaly:     318
3025  deg
Mean motion:   15
76155710  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             697
Checksum:              298

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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