Date: January 2nd 2007

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6243 07 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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


There are no maneuvers



Coasting Arc #1 (Orbit 2446)
---------------------------------------

Vector Time (GMT): 2007/001/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -170260
07                 A    =         6719820
41  meter
 Y    =        5813737
54  meter          E    =           
0027100
 Z    =       -3401309
05                 I    =           51
35073
 XDOT =      -5476
765859                 Wp   =           50
10498
 YDOT =      -2835
224389  meter/sec      RA   =          243
79493  deg
 ZDOT =      -4579
060138                 TA   =          170
16430
                                          MA   =          170
11115
                                          Ha   =            194
254  n
mi
                                          Hp   =            172
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -558596
01                 X    =         -218734
56
 Y    =       19073942
07  feet           Y    =         5811563
19  meter
 Z    =      -11159150
43                 Z    =        -3402252
86
 XDOT =     -17968
391925                 XDOT =       -5422
410767
 YDOT =      -9301
917287  feet/sec       YDOT =       -2896
163880  meter/sec
 ZDOT =     -15023
163183                 ZDOT =       -4605
534672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13220469
02                 X    =        -4029598
96
 Y    =       13758029
53  feet           Y    =         4193447
40  meter
 Z    =      -11161978
16                 Z    =        -3402170
94
 XDOT =      -5942
598107                 XDOT =       -1811
303903
 YDOT =     -17960
688793  feet/sec       YDOT =       -5474
417944  meter/sec
 ZDOT =     -15122
617943                 ZDOT =       -4609
373949


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   07001
62886652  
00020000  00000-0  20000-3 0  9000
2 25544  51
6324 244
4839 0023520  42
4205 317
8773 15
76579276 24474


Satellite: ISS
Catalog Number: 25544
Epoch time:      07001
62886652   =   yrday
fracday
Element set:     900
Inclination:       51
6324  deg
RA of node:       244
4839  deg
Eccentricity:     
0023520     
Arg of perigee:    42
4205  deg
Mean anomaly:     317
8773  deg
Mean motion:   15
76579276  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2447
Checksum:              296


Coasting Arc #2 (Orbit 2462)
---------------------------------------

Vector Time (GMT): 2007/002/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4981012
21                 A    =         6719661
36  meter
 Y    =        2998063
43  meter          E    =           
0033586
 Z    =        3361108
83                 I    =           51
36484
 XDOT =       -558
018210                 Wp   =           60
97765
 YDOT =       6151
326785  meter/sec      RA   =          238
56654  deg
 ZDOT =      -4609
178887                 TA   =           79
17482
                                          MA   =           78
79697
                                          Ha   =            194
130  n
mi
                                          Hp   =            172
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16341903
58                 X    =         4930789
74
 Y    =        9836166
11  feet           Y    =         3053482
45  meter
 Z    =       11027259
95                 Z    =         3385184
93
 XDOT =      -1830
768404                 XDOT =        -604
371399
 YDOT =      20181
518322  feet/sec       YDOT =        6144
828395  meter/sec
 ZDOT =     -15121
977977                 ZDOT =       -4612
001166

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5713404
55                 X    =         1741445
71
 Y    =       18142785
16  feet           Y    =         5529920
92  meter
 Z    =       11117769
26                 Z    =         3388696
07
 XDOT =     -13329
094549                 XDOT =       -4062
708019
 YDOT =      13571
392652  feet/sec       YDOT =        4136
560480  meter/sec
 ZDOT =     -15131
795221                 ZDOT =       -4612
171183


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   07002
64302810  
00020000  00000-0  20000-3 0  9013
2 25544  51
6326 239
2538 0023421  45
8268 314
4816 15
76645318 24630


Satellite: ISS
Catalog Number: 25544
Epoch time:      07002
64302810   =   yrday
fracday
Element set:     901
Inclination:       51
6326  deg
RA of node:       239
2538  deg
Eccentricity:     
0023421     
Arg of perigee:    45
8268  deg
Mean anomaly:     314
4816  deg
Mean motion:   15
76645318  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2463
Checksum:              275


Coasting Arc #3 (Orbit 2478)
---------------------------------------

Vector Time (GMT): 2007/003/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         866989
74                 A    =         6715808
45  meter
 Y    =       -4877453
74  meter          E    =           
0028391
 Z    =        4506308
86                 I    =           51
36581
 XDOT =       5931
762323                 Wp   =           66
10877
 YDOT =       3888
181062  meter/sec      RA   =          233
43959  deg
 ZDOT =       3063
422634                 TA   =          353
36783
                                          MA   =          353
40532
                                          Ha   =            194
264  n
mi
                                          Hp   =            172
068

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2844454
51                 X    =          899575
18
 Y    =      -16002144
81  feet           Y    =        -4867577
18  meter
 Z    =       14784477
90                 Z    =         4510598
92
 XDOT =      19461
162477                 XDOT =        5872
961952
 YDOT =      12756
499546  feet/sec       YDOT =        3954
184014  meter/sec
 ZDOT =      10050
599193                 ZDOT =        3092
096562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12474236
08                 X    =         3802147
16
 Y    =      -10396896
12  feet           Y    =        -3168973
94  meter
 Z    =       14799943
65                 Z    =         4511022
82
 XDOT =       5753
604112                 XDOT =        1753
698533
 YDOT =      21381
227452  feet/sec       YDOT =        6516
998127  meter/sec
 ZDOT =      10158
449811                 ZDOT =        3096
295502


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   07003
65717517  
00020000  00000-0  20000-3 0  9020
2 25544  51
6309 234
0242 0023454  50
0752 310
2469 15
76615133 24795


Satellite: ISS
Catalog Number: 25544
Epoch time:      07003
65717517   =   yrday
fracday
Element set:     902
Inclination:       51
6309  deg
RA of node:       234
0242  deg
Eccentricity:     
0023454     
Arg of perigee:    50
0752  deg
Mean anomaly:     310
2469  deg
Mean motion:   15
76615133  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2479
Checksum:              267


Coasting Arc #4 (Orbit 2493)
---------------------------------------

Vector Time (GMT): 2007/004/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5298470
61                 A    =         6723021
85  meter
 Y    =       -3671903
96  meter          E    =           
0030215
 Z    =       -1885932
14                 I    =           51
40804
 XDOT =       1518
776847                 Wp   =           50
83481
 YDOT =      -5041
760391  meter/sec      RA   =          228
22420  deg
 ZDOT =       5628
085000                 TA   =          288
11169
                                          MA   =          288
44053
                                          Ha   =            194
201  n
mi
                                          Hp   =            171
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17383433
76                 X    =        -5247855
73
 Y    =      -12046928
99  feet           Y    =        -3730871
10  meter
 Z    =       -6187441
39                 Z    =        -1911549
24
 XDOT =       4982
863670                 XDOT =        1547
701970
 YDOT =     -16541
208631  feet/sec       YDOT =       -5024
615748  meter/sec
 ZDOT =      18464
845801                 ZDOT =        5635
532532

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5755971
34                 X    =        -1754420
06
 Y    =      -20321882
41  feet           Y    =        -6194109
76  meter
 Z    =       -6283835
42                 Z    =        -1915313
04
 XDOT =      12790
282187                 XDOT =        3898
478011
 YDOT =      -9262
095757  feet/sec       YDOT =       -2823
086787  meter/sec
 ZDOT =      18492
112114                 ZDOT =        5636
395772


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   07004
60791902  
00020000  00000-0  20000-3 0  9037
2 25544  51
6302 229
1210 0023370  54
0408 306
2919 15
76654774 24943


Satellite: ISS
Catalog Number: 25544
Epoch time:      07004
60791902   =   yrday
fracday
Element set:     903
Inclination:       51
6302  deg
RA of node:       229
1210  deg
Eccentricity:     
0023370     
Arg of perigee:    54
0408  deg
Mean anomaly:     306
2919  deg
Mean motion:   15
76654774  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2494
Checksum:              272


Coasting Arc #5 (Orbit 2509)
---------------------------------------

Vector Time (GMT): 2007/005/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1889082
23                 A    =         6712936
11  meter
 Y    =        3885130
91  meter          E    =           
0037075
 Z    =       -5169909
67                 I    =           51
39365
 XDOT =      -6123
842289                 Wp   =           67
05929
 YDOT =      -4491
250552  meter/sec      RA   =          223
07812  deg
 ZDOT =      -1129
709161                 TA   =          192
04324
                                          MA   =          192
13213
                                          Ha   =            194
295  n
mi
                                          Hp   =            171
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6197776
34                 X    =        -1907271
99
 Y    =       12746492
47  feet           Y    =         3863905
13  meter
 Z    =      -16961645
89                 Z    =        -5179130
29
 XDOT =     -20091
346093                 XDOT =       -6067
677557
 YDOT =     -14735
073989  feet/sec       YDOT =       -4559
416577  meter/sec
 ZDOT =      -3706
394886                 ZDOT =       -1159
322314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12703489
96                 X    =        -3872023
74
 Y    =        6192789
91  feet           Y    =         1887562
37  meter
 Z    =      -16995694
43                 Z    =        -5180287
66
 XDOT =      -6114
665754                 XDOT =       -1863
750122
 YDOT =     -23090
935135  feet/sec       YDOT =       -7038
117029  meter/sec
 ZDOT =      -3817
874752                 ZDOT =       -1163
688224


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   07005
62202929  
00020000  00000-0  20000-3 0  9047
2 25544  51
6297 223
8909 0023440  58
1733 302
1709 15
76684860 25106


Satellite: ISS
Catalog Number: 25544
Epoch time:      07005
62202929   =   yrday
fracday
Element set:     904
Inclination:       51
6297  deg
RA of node:       223
8909  deg
Eccentricity:     
0023440     
Arg of perigee:    58
1733  deg
Mean anomaly:     302
1709  deg
Mean motion:   15
76684860  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2510
Checksum:              285


Coasting Arc #6 (Orbit 2525)
---------------------------------------

Vector Time (GMT): 2007/006/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5329334
67                 A    =         6724306
93  meter
 Y    =        4102709
84  meter          E    =           
0029622
 Z    =          44842
38                 I    =           51
45485
 XDOT =      -2876
186737                 Wp   =           85
11609
 YDOT =       3839
182024  meter/sec      RA   =          217
89471  deg
 ZDOT =      -6019
961503                 TA   =           94
39548
                                          MA   =           94
05698
                                          Ha   =            194
223  n
mi
                                          Hp   =            171
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17484693
80                 X    =         5282843
67
 Y    =       13460334
13  feet           Y    =         4162045
48  meter
 Z    =         147120
66                 Z    =           70619
23
 XDOT =      -9436
308192                 XDOT =       -2889
660022
 YDOT =      12595
741549  feet/sec       YDOT =        3806
944227  meter/sec
 ZDOT =     -19750
529865                 ZDOT =       -6033
966014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5699344
49                 X    =         1737160
20
 Y    =       21316064
28  feet           Y    =         6497136
39  meter
 Z    =         244197
77                 Z    =           74431
48
 XDOT =     -13508
141110                 XDOT =       -4117
281410
 YDOT =       3915
802403  feet/sec       YDOT =        1193
536573  meter/sec
 ZDOT =     -19802
501722                 ZDOT =       -6035
802525


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   07006
63611950  
00020000  00000-0  20000-3 0  9058
2 25544  51
6298 218
6599 0023469  61
2728 299
0791 15
76766994 25265


Satellite: ISS
Catalog Number: 25544
Epoch time:      07006
63611950   =   yrday
fracday
Element set:     905
Inclination:       51
6298  deg
RA of node:       218
6599  deg
Eccentricity:     
0023469     
Arg of perigee:    61
2728  deg
Mean anomaly:     299
0791  deg
Mean motion:   15
76766994  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2526
Checksum:              335


Coasting Arc #7 (Orbit 2541)
---------------------------------------

Vector Time (GMT): 2007/007/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3148682
94                 A    =         6712692
20  meter
 Y    =       -2872716
96  meter          E    =           
0026932
 Z    =        5166524
99                 I    =           51
43800
 XDOT =       5989
672885                 Wp   =           65
14808
 YDOT =       4775
918609  meter/sec      RA   =          212
71605  deg
 ZDOT =       -979
660006                 TA   =           34
27468
                                          MA   =           34
10117
                                          Ha   =            194
279  n
mi
                                          Hp   =            171
408

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10330324
62                 X    =         3155474
53
 Y    =       -9424924
41  feet           Y    =        -2837469
11  meter
 Z    =       16950541
32                 Z    =         5181837
23
 XDOT =      19651
157758                 XDOT =        5940
581639
 YDOT =      15669
024307  feet/sec       YDOT =        4842
624066  meter/sec
 ZDOT =      -3214
107632                 ZDOT =        -950
681600

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13833378
58                 X    =         4216413
79
 Y    =       -1499012
69  feet           Y    =         -456899
07  meter
 Z    =       17007535
27                 Z    =         5183896
75
 XDOT =       6401
071184                 XDOT =        1951
046497
 YDOT =      23280
986762  feet/sec       YDOT =        7096
044765  meter/sec
 ZDOT =      -3104
937949                 ZDOT =        -946
385087


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   07007
65019634  
00020000  00000-0  20000-3 0  9063
2 25544  51
6294 213
4294 0023467  66
0108 294
3510 15
76703091 25423


Satellite: ISS
Catalog Number: 25544
Epoch time:      07007
65019634   =   yrday
fracday
Element set:     906
Inclination:       51
6294  deg
RA of node:       213
4294  deg
Eccentricity:     
0023467     
Arg of perigee:    66
0108  deg
Mean anomaly:     294
3510  deg
Mean motion:   15
76703091  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2542
Checksum:              278


Coasting Arc #8 (Orbit 2557)
---------------------------------------

Vector Time (GMT): 2007/008/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4983743
47                 A    =         6723062
30  meter
 Y    =       -4145190
67  meter          E    =           
0037491
 Z    =        1719344
11                 I    =           51
49908
 XDOT =       4359
060712                 Wp   =           68
05019
 YDOT =      -2840
629314  meter/sec      RA   =          207
57162  deg
 ZDOT =       5701
905083                 TA   =          311
07241
                                          MA   =          311
39569
                                          Ha   =            194
257  n
mi
                                          Hp   =            171
257

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16350864
41                 X    =        -4945373
08
 Y    =      -13599706
92  feet           Y    =        -4200707
25  meter
 Z    =        5640892
74                 Z    =         1695226
41
 XDOT =      14301
380288                 XDOT =        4362
802721
 YDOT =      -9319
649980  feet/sec       YDOT =       -2791
863355  meter/sec
 ZDOT =      18707
037673                 ZDOT =        5723
089916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5451028
76                 X    =        -1661473
57
 Y    =      -20581696
29  feet           Y    =        -6273301
03  meter
 Z    =        5550002
64                 Z    =         1691640
80
 XDOT =      15469
845033                 XDOT =        4715
208766
 YDOT =       1044
958489  feet/sec       YDOT =         318
503347  meter/sec
 ZDOT =      18786
037890                 ZDOT =        5725
984349


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   07008
66425144  
00020000  00000-0  20000-3 0  9073
2 25544  51
6303 208
1995 0023384  69
9566 290
4113 15
76775742 25586


Satellite: ISS
Catalog Number: 25544
Epoch time:      07008
66425144   =   yrday
fracday
Element set:     907
Inclination:       51
6303  deg
RA of node:       208
1995  deg
Eccentricity:     
0023384     
Arg of perigee:    69
9566  deg
Mean anomaly:     290
4113  deg
Mean motion:   15
76775742  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2558
Checksum:              311


Coasting Arc #9 (Orbit 2572)
---------------------------------------

Vector Time (GMT): 2007/009/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4452196
60                 A    =         6715022
72  meter
 Y    =        2113838
35  meter          E    =           
0032545
 Z    =       -4587274
53                 I    =           51
49919
 XDOT =      -5281
155445                 Wp   =           84
98422
 YDOT =      -4726
498597  meter/sec      RA   =          202
36622  deg
 ZDOT =       2968
492202                 TA   =          214
49033
                                          MA   =          214
70194
                                          Ha   =            194
247  n
mi
                                          Hp   =            171
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14606944
21                 X    =        -4453219
10
 Y    =        6935165
20  feet           Y    =         2064045
99  meter
 Z    =      -15050113
28                 Z    =        -4608905
35
 XDOT =     -17326
625476                 XDOT =       -5242
330764
 YDOT =     -15506
885160  feet/sec       YDOT =       -4785
338527  meter/sec
 ZDOT =       9739
147644                 ZDOT =        2942
930702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15897930
63                 X    =        -4845689
26
 Y    =       -2505486
09  feet           Y    =         -763672
16  meter
 Z    =      -15130881
87                 Z    =        -4611892
79
 XDOT =      -5730
258435                 XDOT =       -1746
582771
 YDOT =     -21462
997994  feet/sec       YDOT =       -6541
921789  meter/sec
 ZDOT =       9642
764321                 ZDOT =        2939
114565


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   07009
61491325  
00020000  00000-0  20000-3 0  9084
2 25544  51
6312 203
2964 0023431  73
5436 286
8301 15
76787089 25730


Satellite: ISS
Catalog Number: 25544
Epoch time:      07009
61491325   =   yrday
fracday
Element set:     908
Inclination:       51
6312  deg
RA of node:       203
2964  deg
Eccentricity:     
0023431     
Arg of perigee:    73
5436  deg
Mean anomaly:     286
8301  deg
Mean motion:   15
76787089  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2573
Checksum:              296


Coasting Arc #10 (Orbit 2588)
---------------------------------------

Vector Time (GMT): 2007/010/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4101253
02                 A    =         6719135
08  meter
 Y    =        4109871
81  meter          E    =           
0028219
 Z    =       -3410615
21                 I    =           51
54037
 XDOT =      -5820
052283                 Wp   =           79
69385
 YDOT =       2015
952002  meter/sec      RA   =          197
24791  deg
 ZDOT =      -4596
555881                 TA   =          140
60882
                                          MA   =          140
40327
                                          Ha   =            194
236  n
mi
                                          Hp   =            171
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13455554
54                 X    =         4071559
03
 Y    =       13483831
41  feet           Y    =         4155568
50  meter
 Z    =      -11189682
43                 Z    =        -3390763
37
 XDOT =     -19094
659722                 XDOT =       -5819
833373
 YDOT =       6614
015755  feet/sec       YDOT =        1950
870463  meter/sec
 ZDOT =     -15080
563914                 ZDOT =       -4624
828750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3830944
71                 X    =         1167671
95
 Y    =       18704558
35  feet           Y    =         5701149
39  meter
 Z    =      -11114765
39                 Z    =        -3387780
49
 XDOT =     -18139
684089                 XDOT =       -5528
975710
 YDOT =      -5255
380443  feet/sec       YDOT =       -1601
839959  meter/sec
 ZDOT =     -15186
236528                 ZDOT =       -4628
764894


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   07010
62893426  
00020000  00000-0  20000-3 0  9096
2 25544  51
6313 198
0654 0023443  77
2118 283
1664 15
76831803 25892


Satellite: ISS
Catalog Number: 25544
Epoch time:      07010
62893426   =   yrday
fracday
Element set:     909
Inclination:       51
6313  deg
RA of node:       198
0654  deg
Eccentricity:     
0023443     
Arg of perigee:    77
2118  deg
Mean anomaly:     283
1664  deg
Mean motion:   15
76831803  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2589
Checksum:              300


Coasting Arc #11 (Orbit 2604)
---------------------------------------

Vector Time (GMT): 2007/011/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5635142
28                 A    =         6719233
31  meter
 Y    =       -1489032
88  meter          E    =           
0035910
 Z    =        3315800
74                 I    =           51
56831
 XDOT =       4008
203577                 Wp   =           84
76862
 YDOT =       4649
330204  meter/sec      RA   =          192
03252  deg
 ZDOT =      -4677
562886                 TA   =           56
09044
                                          MA   =           55
74944
                                          Ha   =            194
149  n
mi
                                          Hp   =            170
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18487999
62                 X    =         5635266
59
 Y    =       -4885278
49  feet           Y    =        -1426017
14  meter
 Z    =       10878611
35                 Z    =         3343176
27
 XDOT =      13150
274202                 XDOT =        3978
638810
 YDOT =      15253
708017  feet/sec       YDOT =        4693
987208  meter/sec
 ZDOT =     -15346
334928                 ZDOT =       -4658
162633

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18165290
32                 X    =         5536780
49
 Y    =        5784132
16  feet           Y    =         1763003
48  meter
 Z    =       10980997
38                 Z    =         3347008
00
 XDOT =       3384
676098                 XDOT =        1031
649275
 YDOT =      18652
127636  feet/sec       YDOT =        5685
168503  meter/sec
 ZDOT =     -15273
034879                 ZDOT =       -4655
221031


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   07011
64293790  
00020000  00000-0  20000-3 0  9109
2 25544  51
6310 192
8346 0023391  81
2231 279
1582 15
76834604 26057


Satellite: ISS
Catalog Number: 25544
Epoch time:      07011
64293790   =   yrday
fracday
Element set:     910
Inclination:       51
6310  deg
RA of node:       192
8346  deg
Eccentricity:     
0023391     
Arg of perigee:    81
2231  deg
Mean anomaly:     279
1582  deg
Mean motion:   15
76834604  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2605
Checksum:              278


Coasting Arc #12 (Orbit 2620)
---------------------------------------

Vector Time (GMT): 2007/012/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 471443
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2791765
00                 A    =         6714725
75  meter
 Y    =       -4002887
94  meter          E    =           
0030782
 Z    =        4586461
04                 I    =           51
58285
 XDOT =       6988
937640                 Wp   =           93
12150
 YDOT =      -1494
047063  meter/sec      RA   =          186
91908  deg
 ZDOT =       2931
749823                 TA   =          327
81220
                                          MA   =          327
99973
                                          Ha   =            194
123  n
mi
                                          Hp   =            170
890

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9159334
00                 X    =        -2769076
75
 Y    =      -13132834
44  feet           Y    =        -4033980
56  meter
 Z    =       15047444
36                 Z    =         4572953
47
 XDOT =      22929
585433                 XDOT =        6990
883012
 YDOT =      -4901
729210  feet/sec       YDOT =       -1415
882255  meter/sec
 ZDOT =       9618
601783                 ZDOT =        2965
706517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1011743
26                 X    =         -308379
35
 Y    =      -16027398
25  feet           Y    =        -4885150
99  meter
 Z    =       14996306
30                 Z    =         4570874
16
 XDOT =      20893
916444                 XDOT =        6368
465732
 YDOT =       7856
568588  feet/sec       YDOT =        2394
682105  meter/sec
 ZDOT =       9745
658143                 ZDOT =        2970
476602


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   07012
65692086  
00020000  00000-0  20000-3 0  9113
2 25544  51
6320 187
6049 0023234  84
9804 275
4012 15
76914176 26210


Satellite: ISS
Catalog Number: 25544
Epoch time:      07012
65692086   =   yrday
fracday
Element set:     911
Inclination:       51
6320  deg
RA of node:       187
6049  deg
Eccentricity:     
0023234     
Arg of perigee:    84
9804  deg
Mean anomaly:     275
4012  deg
Mean motion:   15
76914176  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            2621
Checksum:              285

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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