Date: December 24th 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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


363/07:06:12 689 -11 9 12 1 12 1
N/A -1 0 -0 0 186 4
000/00:02:25 377 2 1 0 0 183 6

Coasting Arc #1 (Orbit 33)
---------------------------------------

Vector Time (GMT): 2007/355/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5243242
50                 A    =         6721102
48  meter
 Y    =       -4187416
28  meter          E    =           
0013117
 Z    =         235099
36                 I    =           51
46339
 XDOT =       3168
850619                 Wp   =           41
73060
 YDOT =      -3619
428028  meter/sec      RA   =          217
01286  deg
 ZDOT =       6023
686885                 TA   =          320
83505
                                          MA   =          320
92991
                                          Ha   =            183
932  n
mi
                                          Hp   =            178
019

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17202239
18                 X    =        -5197170
57
 Y    =      -13738242
39  feet           Y    =        -4245791
63  meter
 Z    =         771323
35                 Z    =          209738
55
 XDOT =      10396
491531                 XDOT =        3179
825694
 YDOT =     -11874
763872  feet/sec       YDOT =       -3583
931750  meter/sec
 ZDOT =      19762
752246                 ZDOT =        6039
107462

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11715846
70                 X    =         3570990
08
 Y    =      -18642309
73  feet           Y    =        -5682176
01  meter
 Z    =         674166
33                 Z    =          205485
90
 XDOT =      11596
721771                 XDOT =        3534
680796
 YDOT =       8029
544393  feet/sec       YDOT =        2447
405131  meter/sec
 ZDOT =      19821
164842                 ZDOT =        6041
491044


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   07355
58377551  
00020000  00000-0  20000-3 0  9000
2 25544  51
6384 217
6331 0001379 332
9350  27
1743 15
77897012   345


Satellite: ISS
Catalog Number: 25544
Epoch time:      07355
58377551   =   yrday
fracday
Element set:     900
Inclination:       51
6384  deg
RA of node:       217
6331  deg
Eccentricity:     
0001379     
Arg of perigee:   332
9350  deg
Mean anomaly:      27
1743  deg
Mean motion:   15
77897012  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              34
Checksum:              287


Coasting Arc #2 (Orbit 48)
---------------------------------------

Vector Time (GMT): 2007/356/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3774448
06                 A    =         6709896
95  meter
 Y    =        2371946
89  meter          E    =           
0012722
 Z    =       -5026274
26                 I    =           51
44864
 XDOT =      -5520
001158                 Wp   =           98
24067
 YDOT =      -5070
200354  meter/sec      RA   =          211
81678  deg
 ZDOT =       1754
513857                 TA   =          188
69282
                                          MA   =          188
71488
                                          Ha   =            183
906  n
mi
                                          Hp   =            177
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12383359
76                 X    =        -3776274
04
 Y    =        7781978
00  feet           Y    =         2329729
61  meter
 Z    =      -16490401
12                 Z    =        -5044614
70
 XDOT =     -18110
240019                 XDOT =       -5471
418336
 YDOT =     -16634
515597  feet/sec       YDOT =       -5131
656826  meter/sec
 ZDOT =       5756
279059                 ZDOT =        1727
814486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9308521
97                 X    =        -2837237
50
 Y    =      -11178320
33  feet           Y    =        -3407152
04  meter
 Z    =      -16560093
08                 Z    =        -5047516
37
 XDOT =      13328
891406                 XDOT =        4062
646100
 YDOT =     -19465
750497  feet/sec       YDOT =       -5933
160752  meter/sec
 ZDOT =       5653
910454                 ZDOT =        1723
311907


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   07356
53376220  
00020000  00000-0  20000-3 0  9019
2 25544  51
6370 212
7252 0001418 335
7297  24
3801 15
77932736   496


Satellite: ISS
Catalog Number: 25544
Epoch time:      07356
53376220   =   yrday
fracday
Element set:     901
Inclination:       51
6370  deg
RA of node:       212
7252  deg
Eccentricity:     
0001418     
Arg of perigee:   335
7297  deg
Mean anomaly:      24
3801  deg
Mean motion:   15
77932736  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              49
Checksum:              277


Coasting Arc #3 (Orbit 64)
---------------------------------------

Vector Time (GMT): 2007/357/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4138602
91                 A    =         6717704
50  meter
 Y    =        4523948
48  meter          E    =           
0003694
 Z    =       -2745905
79                 I    =           51
49955
 XDOT =      -5428
611596                 Wp   =          110
06741
 YDOT =       1849
511853  meter/sec      RA   =          206
67786  deg
 ZDOT =      -5141
659249                 TA   =          101
41693
                                          MA   =          101
37543
                                          Ha   =            183
901  n
mi
                                          Hp   =            177
931

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13578093
53                 X    =         4101046
98
 Y    =       14842350
67  feet           Y    =         4570019
25  meter
 Z    =       -9008877
26                 Z    =        -2725890
72
 XDOT =     -17810
405498                 XDOT =       -5423
912351
 YDOT =       6067
952275  feet/sec       YDOT =        1788
833349  meter/sec
 ZDOT =     -16868
960790                 ZDOT =       -5168
019721

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12684248
87                 X    =        -3866159
05
 Y    =       15657209
97  feet           Y    =         4772317
60  meter
 Z    =       -8932047
55                 Z    =        -2722488
09
 XDOT =      -7457
364229                 XDOT =       -2273
004617
 YDOT =     -15709
059337  feet/sec       YDOT =       -4788
121286  meter/sec
 ZDOT =     -16969
311568                 ZDOT =       -5172
246166


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   07357
54705487  
00020000  00000-0  20000-3 0  9023
2 25544  51
6360 207
4912 0001469 336
9502  23
1597 15
77955805   656


Satellite: ISS
Catalog Number: 25544
Epoch time:      07357
54705487   =   yrday
fracday
Element set:     902
Inclination:       51
6360  deg
RA of node:       207
4912  deg
Eccentricity:     
0001469     
Arg of perigee:   336
9502  deg
Mean anomaly:      23
1597  deg
Mean motion:   15
77955805  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              65
Checksum:              301


Coasting Arc #4 (Orbit 80)
---------------------------------------

Vector Time (GMT): 2007/358/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5560422
58                 A    =         6714815
24  meter
 Y    =        -925321
18  meter          E    =           
0011482
 Z    =        3641526
20                 I    =           51
51752
 XDOT =       3715
555624                 Wp   =           77
18892
 YDOT =       5171
445961  meter/sec      RA   =          201
45197  deg
 ZDOT =      -4345
420352                 TA   =           58
92729
                                          MA   =           58
81464
                                          Ha   =            183
681  n
mi
                                          Hp   =            177
761

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18242856
25                 X    =         5552666
63
 Y    =       -3035830
64  feet           Y    =         -863185
46  meter
 Z    =       11947264
44                 Z    =         3668519
57
 XDOT =      12190
143122                 XDOT =        3678
560725
 YDOT =      16966
686225  feet/sec       YDOT =        5212
789415  meter/sec
 ZDOT =     -14256
628451                 ZDOT =       -4327
459123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5967971
92                 X    =         1819037
84
 Y    =       17433660
37  feet           Y    =         5313779
68  meter
 Z    =       12050145
08                 Z    =         3672884
22
 XDOT =     -13459
664278                 XDOT =       -4102
505672
 YDOT =      14445
403932  feet/sec       YDOT =        4402
959119  meter/sec
 ZDOT =     -14187
549930                 ZDOT =       -4324
365219


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   07358
56031904  
00020000  00000-0  20000-3 0  9033
2 25544  51
6361 202
2554 0001611 337
1539  22
9555 15
78038112   817


Satellite: ISS
Catalog Number: 25544
Epoch time:      07358
56031904   =   yrday
fracday
Element set:     903
Inclination:       51
6361  deg
RA of node:       202
2554  deg
Eccentricity:     
0001611     
Arg of perigee:   337
1539  deg
Mean anomaly:      22
9555  deg
Mean motion:   15
78038112  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              81
Checksum:              262


Coasting Arc #5 (Orbit 96)
---------------------------------------

Vector Time (GMT): 2007/359/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2124213
83                 A    =         6711625
34  meter
 Y    =       -4415256
50  meter          E    =           
0007560
 Z    =        4581627
46                 I    =           51
53258
 XDOT =       7115
470145                 Wp   =          106
14024
 YDOT =       -357
121268  meter/sec      RA   =          196
32536  deg
 ZDOT =       2948
769959                 TA   =          314
59060
                                          MA   =          314
65227
                                          Ha   =            183
915  n
mi
                                          Hp   =            177
733

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6969205
47                 X    =        -2096940
34
 Y    =      -14485749
66  feet           Y    =        -4438858
98  meter
 Z    =       15031586
15                 Z    =         4571373
61
 XDOT =      23344
718323                 XDOT =        7104
610270
 YDOT =      -1171
657702  feet/sec       YDOT =        -277
613288  meter/sec
 ZDOT =       9674
442123                 ZDOT =        2983
310079

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12974322
37                 X    =         3954573
46
 Y    =       -9553154
19  feet           Y    =        -2911801
40  meter
 Z    =       14991983
00                 Z    =         4569556
42
 XDOT =       4660
112047                 XDOT =        1420
402152
 YDOT =      21749
433813  feet/sec       YDOT =        6629
227426  meter/sec
 ZDOT =       9806
195121                 ZDOT =        2988
928273


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   07359
57355986  
00020000  00000-0  20000-3 0  9045
2 25544  51
6347 197
0194 0001573 345
6102  14
5018 15
78020278   971


Satellite: ISS
Catalog Number: 25544
Epoch time:      07359
57355986   =   yrday
fracday
Element set:     904
Inclination:       51
6347  deg
RA of node:       197
0194  deg
Eccentricity:     
0001573     
Arg of perigee:   345
6102  deg
Mean anomaly:      14
5018  deg
Mean motion:   15
78020278  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:              97
Checksum:              298


Coasting Arc #6 (Orbit 111)
---------------------------------------

Vector Time (GMT): 2007/360/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6581841
62                 A    =         6719788
67  meter
 Y    =        -234186
76  meter          E    =           
0009826
 Z    =       -1310687
69                 I    =           51
58886
 XDOT =       -984
319708                 Wp   =           31
11827
 YDOT =      -4920
428610  meter/sec      RA   =          191
11683  deg
 ZDOT =       5849
760075                 TA   =          314
45781
                                          MA   =          314
53814
                                          Ha   =            183
749  n
mi
                                          Hp   =            177
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21593968
56                 X    =        -6572366
74
 Y    =        -768329
26  feet           Y    =         -307735
47  meter
 Z    =       -4300156
47                 Z    =        -1342638
83
 XDOT =      -3229
395368                 XDOT =        -957
642224
 YDOT =     -16143
138483  feet/sec       YDOT =       -4931
287542  meter/sec
 ZDOT =      19192
126230                 ZDOT =        5845
042384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3504913
05                 X    =        -1068297
50
 Y    =      -21296517
65  feet           Y    =        -6491178
58  meter
 Z    =       -4422111
97                 Z    =        -1347859
73
 XDOT =      13613
523011                 XDOT =        4149
401814
 YDOT =      -6203
432696  feet/sec       YDOT =       -1890
806286  meter/sec
 ZDOT =      19173
584493                 ZDOT =        5844
108554


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   07360
52344556  
00020000  00000-0  20000-3 0  9054
2 25544  51
6343 192
1104 0001449 347
3561  12
7568 15
78081330  1128


Satellite: ISS
Catalog Number: 25544
Epoch time:      07360
52344556   =   yrday
fracday
Element set:     905
Inclination:       51
6343  deg
RA of node:       192
1104  deg
Eccentricity:     
0001449     
Arg of perigee:   347
3561  deg
Mean anomaly:      12
7568  deg
Mean motion:   15
78081330  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             112
Checksum:              264


Coasting Arc #7 (Orbit 127)
---------------------------------------

Vector Time (GMT): 2007/361/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -514045
59                 A    =         6708361
55  meter
 Y    =        4143751
83  meter          E    =           
0015063
 Z    =       -5263292
80                 I    =           51
57934
 XDOT =      -7648
572554                 Wp   =           85
25261
 YDOT =       -857
007515  meter/sec      RA   =          185
95805  deg
 ZDOT =         73
695884                 TA   =          185
43943
                                          MA   =          185
45581
                                          Ha   =            183
803  n
mi
                                          Hp   =            177
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1686501
29                 X    =         -534775
71
 Y    =       13594986
32  feet           Y    =         4137888
21  meter
 Z    =      -17268021
00                 Z    =        -5265839
85
 XDOT =     -25093
741975                 XDOT =       -7638
778905
 YDOT =      -2811
704446  feet/sec       YDOT =        -942
483443  meter/sec
 ZDOT =        241
784397                 ZDOT =          36
563356

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13619705
13                 X    =        -4151286
13
 Y    =        1360722
63  feet           Y    =          414748
26  meter
 Z    =      -17277284
36                 Z    =        -5266116
27
 XDOT =      -2530
886470                 XDOT =        -771
414196
 YDOT =     -24121
224620  feet/sec       YDOT =       -7352
149264  meter/sec
 ZDOT =         99
970831                 ZDOT =          30
471109


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   07361
53663210  
00020000  00000-0  20000-3 0  9068
2 25544  51
6341 186
8745 0001415 356
6128   3
5028 15
78128864  1282


Satellite: ISS
Catalog Number: 25544
Epoch time:      07361
53663210   =   yrday
fracday
Element set:     906
Inclination:       51
6341  deg
RA of node:       186
8745  deg
Eccentricity:     
0001415     
Arg of perigee:   356
6128  deg
Mean anomaly:       3
5028  deg
Mean motion:   15
78128864  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             128
Checksum:              282


Coasting Arc #8 (Orbit 143)
---------------------------------------

Vector Time (GMT): 2007/362/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 539213
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6440520
91                 A    =         6719365
63  meter
 Y    =        1238098
64  meter          E    =           
0007358
 Z    =       -1450482
03                 I    =           51
64692
 XDOT =      -2181
145999                 Wp   =          135
51525
 YDOT =       4566
769761  meter/sec      RA   =          180
80310  deg
 ZDOT =      -5809
602198                 TA   =           60
46871
                                          MA   =           60
39538
                                          Ha   =            183
763  n
mi
                                          Hp   =            177
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21130317
95                 X    =         6433243
72
 Y    =        4062003
41  feet           Y    =         1310079
65  meter
 Z    =       -4758799
31                 Z    =        -1419211
94
 XDOT =      -7155
990809                 XDOT =       -2203
828579
 YDOT =      14982
840423  feet/sec       YDOT =        4542
252688  meter/sec
 ZDOT =     -19060
374664                 ZDOT =       -5820
252720

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         935531
80                 X    =          285150
09
 Y    =       21522964
50  feet           Y    =         6560199
58  meter
 Z    =       -4639305
86                 Z    =        -1414060
43
 XDOT =     -14636
316214                 XDOT =       -4461
149182
 YDOT =      -3464
389123  feet/sec       YDOT =       -1055
945805  meter/sec
 ZDOT =     -19100
518831                 ZDOT =       -5821
838140


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   07362
54979012  
00020000  00000-0  20000-3 0  9071
2 25544  51
6347 181
6387 0001663 359
8239    
2926 15
78203660  1443


Satellite: ISS
Catalog Number: 25544
Epoch time:      07362
54979012   =   yrday
fracday
Element set:     907
Inclination:       51
6347  deg
RA of node:       181
6387  deg
Eccentricity:     
0001663     
Arg of perigee:   359
8239  deg
Mean anomaly:        
2926  deg
Mean motion:   15
78203660  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             144
Checksum:              296


Coasting Arc #9 (Orbit 155)
---------------------------------------

Vector Time (GMT): 2007/363/07:07:25
377
Vector Time (MET): N/A
Weight (LBS)     : 538460
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1803723
46                 A    =         6715605
95  meter
 Y    =        4082183
20  meter          E    =           
0003772
 Z    =       -5021105
22                 I    =           51
63961
 XDOT =      -7410
644398                 Wp   =           78
64807
 YDOT =      -1029
781638  meter/sec      RA   =          176
76892  deg
 ZDOT =       1826
778024                 TA   =          208
94901
                                          MA   =          208
96994
                                          Ha   =            186
415  n
mi
                                          Hp   =            183
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5917727
87                 X    =        -1824845
63
 Y    =       13392989
49  feet           Y    =         4061895
26  meter
 Z    =      -16473442
31                 Z    =        -5029918
57
 XDOT =     -24313
137790                 XDOT =       -7407
452513
 YDOT =      -3378
548681  feet/sec       YDOT =       -1112
633979  meter/sec
 ZDOT =       5993
366220                 ZDOT =        1790
785155

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =           6696
44                 X    =            2041
07
 Y    =      -14604695
78  feet           Y    =        -4451511
27  meter
 Z    =      -16506628
62                 Z    =        -5031220
40
 XDOT =      22612
091053                 XDOT =        6892
165353
 YDOT =      -6601
122535  feet/sec       YDOT =       -2012
022149  meter/sec
 ZDOT =       5855
860424                 ZDOT =        1784
866257


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   07363
30964303  
00020000  00000-0  20000-3 0  9084
2 25544  51
6390 177
7161 0010122 292
5504  67
4589 15
75946071  1565


Satellite: ISS
Catalog Number: 25544
Epoch time:      07363
30964303   =   yrday
fracday
Element set:     908
Inclination:       51
6390  deg
RA of node:       177
7161  deg
Eccentricity:     
0010122     
Arg of perigee:   292
5504  deg
Mean anomaly:      67
4589  deg
Mean motion:   15
75946071  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             156
Checksum:              291


Coasting Arc #10 (Orbit 171)
---------------------------------------

Vector Time (GMT): 2007/364/07:07:25
377
Vector Time (MET): N/A
Weight (LBS)     : 538460
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6290044
27                 A    =         6724582
52  meter
 Y    =         847434
28  meter          E    =           
0005055
 Z    =       -2217439
03                 I    =           51
69879
 XDOT =      -2577
002032                 Wp   =          268
69372
 YDOT =       4754
292708  meter/sec      RA   =          171
65550  deg
 ZDOT =      -5482
459569                 TA   =          296
15890
                                          MA   =          296
21089
                                          Ha   =            186
652  n
mi
                                          Hp   =            183
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20636628
19                 X    =         6290872
49
 Y    =        2780296
21  feet           Y    =          917777
93  meter
 Z    =       -7275062
42                 Z    =        -2186880
12
 XDOT =      -8454
731077                 XDOT =       -2603
341115
 YDOT =      15598
073189  feet/sec       YDOT =        4725
328368  meter/sec
 ZDOT =     -17987
072076                 ZDOT =       -5495
042166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19972487
51                 X    =        -6087614
19
 Y    =        6032025
72  feet           Y    =         1838561
44  meter
 Z    =       -7158310
66                 Z    =        -2181853
09
 XDOT =       1583
612057                 XDOT =         482
684955
 YDOT =     -16200
397902  feet/sec       YDOT =       -4937
881280  meter/sec
 ZDOT =     -18034
573966                 ZDOT =       -5496
938145


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   07364
32421726  
00020000  00000-0  20000-3 0  9095
2 25544  51
6392 172
4907 0010217 295
8361  64
1749 15
75942084  1729


Satellite: ISS
Catalog Number: 25544
Epoch time:      07364
32421726   =   yrday
fracday
Element set:     909
Inclination:       51
6392  deg
RA of node:       172
4907  deg
Eccentricity:     
0010217     
Arg of perigee:   295
8361  deg
Mean anomaly:      64
1749  deg
Mean motion:   15
75942084  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             172
Checksum:              296


Coasting Arc #11 (Orbit 187)
---------------------------------------

Vector Time (GMT): 2007/365/07:07:25
377
Vector Time (MET): N/A
Weight (LBS)     : 538460
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2671364
28                 A    =         6717641
48  meter
 Y    =       -4262827
40  meter          E    =           
0008784
 Z    =        4457013
47                 I    =           51
70521
 XDOT =       6924
032160                 Wp   =          356
70449
 YDOT =        955
119091  meter/sec      RA   =          166
46574  deg
 ZDOT =      -3228
202594                 TA   =          125
62954
                                          MA   =          125
54770
                                          Ha   =            186
789  n
mi
                                          Hp   =            182
903

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8764318
50                 X    =         2697182
03
 Y    =      -13985654
19  feet           Y    =        -4232810
69  meter
 Z    =       14622747
61                 Z    =         4470053
29
 XDOT =      22716
640945                 XDOT =        6928
519238
 YDOT =       3133
592817  feet/sec       YDOT =        1032
572900  meter/sec
 ZDOT =     -10591
215859                 ZDOT =       -3194
554772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1829436
36                 X    =         -557612
20
 Y    =       16359111
45  feet           Y    =         4986257
17  meter
 Z    =       14672054
56                 Z    =         4472042
23
 XDOT =     -20719
744062                 XDOT =       -6315
377990
 YDOT =       7090
910289  feet/sec       YDOT =        2161
309456  meter/sec
 ZDOT =     -10462
651274                 ZDOT =       -3189
016108


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   07365
33876588  
00020000  00000-0  20000-3 0  9109
2 25544  51
6392 167
2646 0010360 301
1950  58
8199 15
76050657  1888


Satellite: ISS
Catalog Number: 25544
Epoch time:      07365
33876588   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:       167
2646  deg
Eccentricity:     
0010360     
Arg of perigee:   301
1950  deg
Mean anomaly:      58
8199  deg
Mean motion:   15
76050657  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:             188
Checksum:              309

INTERNATIONAL SPACE STATION ORBITAL DATA:

The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:

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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