Date: January 6th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


There are no maneuvers



Coasting Arc #1 (Orbit 3767)
---------------------------------------

Vector Time (GMT): 2010/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6195935
42                 A    =         6722267
64  meter
 Y    =       -2144505
79  meter          E    =           
0009442
 Z    =       -1489763
63                 I    =           51
60985
 XDOT =       2839
921502                 Wp   =           86
51886
 YDOT =       4205
306728  meter/sec      RA   =          351
27980  deg
 ZDOT =       5789
718064                 TA   =          257
06055
                                          MA   =          257
16602
                                          Ha   =            187
540  n
mi
                                          Hp   =            177
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20327872
10                 X    =         6226692
05
 Y    =       -7035780
14  feet           Y    =        -2075047
10  meter
 Z    =       -4887675
95                 Z    =        -1459589
71
 XDOT =       9317
327762                 XDOT =        2764
561007
 YDOT =      13796
938084  feet/sec       YDOT =        4236
642643  meter/sec
 ZDOT =      18995
138004                 ZDOT =        5803
331424

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11504214
64                 X    =         3506484
62
 Y    =       18207989
94  feet           Y    =         5549795
33  meter
 Z    =       -4768239
77                 Z    =        -1453359
48
 XDOT =      -9999
070266                 XDOT =       -3047
716617
 YDOT =      11277
973865  feet/sec       YDOT =        3437
526434  meter/sec
 ZDOT =      19049
092258                 ZDOT =        5806
163320


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   10004
50282405  
00016717  00000-0  10270-3 0  9008
2 25544  51
6428 351
7849 0007599 145
6176 214
5482 15
77159841 37683


Satellite: ISS
Catalog Number: 25544
Epoch time:      10004
50282405   =   yrday
fracday
Element set:     900
Inclination:       51
6428  deg
RA of node:       351
7849  deg
Eccentricity:     
0007599     
Arg of perigee:   145
6176  deg
Mean anomaly:     214
5482  deg
Mean motion:   15
77159841  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3768
Checksum:              325


Coasting Arc #2 (Orbit 3783)
---------------------------------------

Vector Time (GMT): 2010/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1525816
41                 A    =         6711219
07  meter
 Y    =       -3916321
27  meter          E    =           
0019487
 Z    =       -5247785
82                 I    =           51
54289
 XDOT =       7350
323394                 Wp   =          105
91539
 YDOT =      -2215
657986  meter/sec      RA   =          346
13326  deg
 ZDOT =       -490
388214                 TA   =          159
45443
                                          MA   =          159
37595
                                          Ha   =            187
407  n
mi
                                          Hp   =            177
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5005959
34                 X    =        -1456417
52
 Y    =      -12848823
07  feet           Y    =        -3932995
52  meter
 Z    =      -17217145
07                 Z    =        -5255029
80
 XDOT =      24115
234231                 XDOT =        7376
935167
 YDOT =      -7269
219115  feet/sec       YDOT =       -2133
313501  meter/sec
 ZDOT =      -1608
885217                 ZDOT =        -454
616262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11252872
09                 X    =         3429875
41
 Y    =       -7907874
60  feet           Y    =        -2410320
18  meter
 Z    =      -17245879
40                 Z    =        -5256544
04
 XDOT =      12389
880130                 XDOT =        3776
435464
 YDOT =      20782
452812  feet/sec       YDOT =        6334
491617  meter/sec
 ZDOT =      -1467
291536                 ZDOT =        -447
230460


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   10005
51662480  
00016717  00000-0  10270-3 0  9016
2 25544  51
6429 346
5537 0007402 149
6581 210
5013 15
77144707 37846


Satellite: ISS
Catalog Number: 25544
Epoch time:      10005
51662480   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:       346
5537  deg
Eccentricity:     
0007402     
Arg of perigee:   149
6581  deg
Mean anomaly:     210
5013  deg
Mean motion:   15
77144707  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3784
Checksum:              296


Coasting Arc #3 (Orbit 3799)
---------------------------------------

Vector Time (GMT): 2010/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6466613
65                 A    =         6722933
41  meter
 Y    =        1684925
22  meter          E    =           
0017861
 Z    =        -649569
47                 I    =           51
55415
 XDOT =       -659
673836                 Wp   =          144
98560
 YDOT =      -4805
531447  meter/sec      RA   =          340
96995  deg
 ZDOT =      -5993
236994                 TA   =           42
11028
                                          MA   =           41
97317
                                          Ha   =            187
192  n
mi
                                          Hp   =            177
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21215924
06                 X    =        -6481818
70
 Y    =        5527969
90  feet           Y    =         1612526
75  meter
 Z    =       -2131133
43                 Z    =         -681020
87
 XDOT =      -2164
284239                 XDOT =        -576
774675
 YDOT =     -15766
179288  feet/sec       YDOT =       -4812
444439  meter/sec
 ZDOT =     -19662
851031                 ZDOT =       -5996
240591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10890312
55                 X    =        -3319367
27
 Y    =      -19013912
40  feet           Y    =        -5795440
50  meter
 Z    =       -2255624
66                 Z    =         -687514
40
 XDOT =      13292
464979                 XDOT =        4051
543325
 YDOT =      -5314
350524  feet/sec       YDOT =       -1619
814040  meter/sec
 ZDOT =     -19674
810485                 ZDOT =       -5996
882236


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   10006
53041267  
00016717  00000-0  10270-3 0  9024
2 25544  51
6433 341
3232 0007265 153
3041 206
8499 15
77181864 38006


Satellite: ISS
Catalog Number: 25544
Epoch time:      10006
53041267   =   yrday
fracday
Element set:     902
Inclination:       51
6433  deg
RA of node:       341
3232  deg
Eccentricity:     
0007265     
Arg of perigee:   153
3041  deg
Mean anomaly:     206
8499  deg
Mean motion:   15
77181864  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3800
Checksum:              284


Coasting Arc #4 (Orbit 3815)
---------------------------------------

Vector Time (GMT): 2010/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -334778
54                 A    =         6712280
64  meter
 Y    =        4488714
33  meter          E    =           
0008289
 Z    =        4971890
13                 I    =           51
48984
 XDOT =      -7294
087420                 Wp   =          113
54380
 YDOT =       1595
313794  meter/sec      RA   =          335
77987  deg
 ZDOT =      -1932
153009                 TA   =          355
12471
                                          MA   =          355
13277
                                          Ha   =            187
104  n
mi
                                          Hp   =            177
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1098354
80                 X    =         -409099
69
 Y    =       14726753
07  feet           Y    =         4484554
74  meter
 Z    =       16311975
50                 Z    =         4970083
58
 XDOT =     -23930
733006                 XDOT =       -7301
998378
 YDOT =       5233
969141  feet/sec       YDOT =        1513
702900  meter/sec
 ZDOT =      -6339
084674                 ZDOT =       -1967
606632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14476784
82                 X    =        -4412524
01
 Y    =        2955931
63  feet           Y    =          900967
96  meter
 Z    =       16304887
41                 Z    =         4969729
68
 XDOT =     -11467
148301                 XDOT =       -3495
186802
 YDOT =     -20433
638369  feet/sec       YDOT =       -6228
172975  meter/sec
 ZDOT =      -6479
418417                 ZDOT =       -1974
926734


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   10007
54418816  
00016717  00000-0  10270-3 0  9035
2 25544  51
6431 336
0932 0007211 157
7699 202
3780 15
77195782 38165


Satellite: ISS
Catalog Number: 25544
Epoch time:      10007
54418816   =   yrday
fracday
Element set:     903
Inclination:       51
6431  deg
RA of node:       336
0932  deg
Eccentricity:     
0007211     
Arg of perigee:   157
7699  deg
Mean anomaly:     202
3780  deg
Mean motion:   15
77195782  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3816
Checksum:              314


Coasting Arc #5 (Orbit 3831)
---------------------------------------

Vector Time (GMT): 2010/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6088247
74                 A    =         6719789
23  meter
 Y    =        -999782
19  meter          E    =           
0016234
 Z    =        2655118
51                 I    =           51
48922
 XDOT =      -1374
152353                 Wp   =          104
76329
 YDOT =       5518
709361  meter/sec      RA   =          330
64871  deg
 ZDOT =       5198
559621                 TA   =          285
57949
                                          MA   =          285
75862
                                          Ha   =            186
940  n
mi
                                          Hp   =            177
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19974566
09                 X    =         6086076
94
 Y    =       -3280125
31  feet           Y    =         -931712
18  meter
 Z    =        8711018
74                 Z    =         2684689
78
 XDOT =      -4508
373863                 XDOT =       -1461
014994
 YDOT =      18106
001841  feet/sec       YDOT =        5502
856648  meter/sec
 ZDOT =      17055
641800                 ZDOT =        5191
673500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9012323
71                 X    =         2746956
27
 Y    =       18068412
19  feet           Y    =         5507252
03  meter
 Z    =        8828072
40                 Z    =         2690796
47
 XDOT =     -17342
469022                 XDOT =       -5285
984558
 YDOT =        282
079586  feet/sec       YDOT =          85
977858  meter/sec
 ZDOT =      17028
458372                 ZDOT =        5190
274112


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   10008
55794954  
00016717  00000-0  10270-3 0  9048
2 25544  51
6435 330
8629 0007312 162
2636 197
8786 15
77249994 38325


Satellite: ISS
Catalog Number: 25544
Epoch time:      10008
55794954   =   yrday
fracday
Element set:     904
Inclination:       51
6435  deg
RA of node:       330
8629  deg
Eccentricity:     
0007312     
Arg of perigee:   162
2636  deg
Mean anomaly:     197
8786  deg
Mean motion:   15
77249994  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3832
Checksum:              347


Coasting Arc #6 (Orbit 3846)
---------------------------------------

Vector Time (GMT): 2010/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1975075
27                 A    =         6716497
32  meter
 Y    =       -5120808
81  meter          E    =           
0011867
 Z    =       -3885172
98                 I    =           51
45183
 XDOT =       6514
613927                 Wp   =          136
63730
 YDOT =       -565
112391  meter/sec      RA   =          325
42721  deg
 ZDOT =       4055
447688                 TA   =          175
73728
                                          MA   =          175
72716
                                          Ha   =            186
872  n
mi
                                          Hp   =            177
779

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6479905
73                 X    =         2051063
67
 Y    =      -16800553
82  feet           Y    =        -5098297
06  meter
 Z    =      -12746630
50                 Z    =        -3875394
05
 XDOT =      21373
405272                 XDOT =        6500
748363
 YDOT =      -1854
043277  feet/sec       YDOT =        -492
340080  meter/sec
 ZDOT =      13305
274568                 ZDOT =        4087
061849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18006651
69                 X    =         5488427
44
 Y    =         995941
57  feet           Y    =          303562
99  meter
 Z    =      -12707988
49                 Z    =        -3873394
89
 XDOT =       8466
416985                 XDOT =        2580
563897
 YDOT =      18345
476026  feet/sec       YDOT =        5591
701093  meter/sec
 ZDOT =      13430
422724                 ZDOT =        4093
592846


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   10009
50834173  
00016717  00000-0  10270-3 0  9053
2 25544  51
6435 325
9589 0007081 165
3371 194
8000 15
77218075 38476


Satellite: ISS
Catalog Number: 25544
Epoch time:      10009
50834173   =   yrday
fracday
Element set:     905
Inclination:       51
6435  deg
RA of node:       325
9589  deg
Eccentricity:     
0007081     
Arg of perigee:   165
3371  deg
Mean anomaly:     194
8000  deg
Mean motion:   15
77218075  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3847
Checksum:              313


Coasting Arc #7 (Orbit 3862)
---------------------------------------

Vector Time (GMT): 2010/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5182125
40                 A    =         6714813
59  meter
 Y    =        -128924
85  meter          E    =           
0010303
 Z    =       -4274144
52                 I    =           51
42341
 XDOT =       3033
695647                 Wp   =          111
40025
 YDOT =      -6149
767378  meter/sec      RA   =          320
30327  deg
 ZDOT =      -3503
117248                 TA   =          123
06344
                                          MA   =          122
96445
                                          Ha   =            186
631  n
mi
                                          Hp   =            177
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17001723
74                 X    =        -5159535
68
 Y    =        -422981
79  feet           Y    =         -186747
62  meter
 Z    =      -14022783
85                 Z    =        -4299264
29
 XDOT =       9953
069709                 XDOT =        3119
255374
 YDOT =     -20176
402160  feet/sec       YDOT =       -6115
363987  meter/sec
 ZDOT =     -11493
166823                 ZDOT =       -3488
172552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5145265
89                 X    =        -1568277
04
 Y    =      -16123422
13  feet           Y    =        -4914419
07  meter
 Z    =      -14122233
82                 Z    =        -4304456
87
 XDOT =      21170
630198                 XDOT =        6452
808084
 YDOT =       3229
167436  feet/sec       YDOT =         984
250235  meter/sec
 ZDOT =     -11434
087309                 ZDOT =       -3485
109812


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   10010
52207984  
00016717  00000-0  10270-3 0  9062
2 25544  51
6442 320
7278 0007052 169
0839 191
0480 15
77265167 38633


Satellite: ISS
Catalog Number: 25544
Epoch time:      10010
52207984   =   yrday
fracday
Element set:     906
Inclination:       51
6442  deg
RA of node:       320
7278  deg
Eccentricity:     
0007052     
Arg of perigee:   169
0839  deg
Mean anomaly:     191
0480  deg
Mean motion:   15
77265167  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3863
Checksum:              309


Coasting Arc #8 (Orbit 3878)
---------------------------------------

Vector Time (GMT): 2010/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3175468
23                 A    =         6720999
46  meter
 Y    =        5526906
52  meter          E    =           
0018465
 Z    =        2095799
71                 I    =           51
42215
 XDOT =      -5298
940809                 Wp   =          129
89703
 YDOT =       -941
260874  meter/sec      RA   =          315
08392  deg
 ZDOT =      -5526
149640                 TA   =           26
55357
                                          MA   =           26
45909
                                          Ha   =            186
592  n
mi
                                          Hp   =            177
981

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10418202
84                 X    =        -3247215
98
 Y    =       18132895
41  feet           Y    =         5490995
12  meter
 Z    =        6875983
31                 Z    =         2080199
88
 XDOT =     -17384
976407                 XDOT =       -5261
176846
 YDOT =      -3088
126227  feet/sec       YDOT =       -1000
304889  meter/sec
 ZDOT =     -18130
412206                 ZDOT =       -5551
800060

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20623884
60                 X    =        -6286160
03
 Y    =       -3583389
62  feet           Y    =        -1092217
16  meter
 Z    =        6814300
82                 Z    =         2076998
89
 XDOT =      -3304
044684                 XDOT =       -1007
072820
 YDOT =     -15782
564845  feet/sec       YDOT =       -4810
525765  meter/sec
 ZDOT =     -18231
978520                 ZDOT =       -5557
107053


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   10011
53580582  
00016717  00000-0  10270-3 0  9073
2 25544  51
6447 315
4973 0007038 172
9253 187
2012 15
77272768 38798


Satellite: ISS
Catalog Number: 25544
Epoch time:      10011
53580582   =   yrday
fracday
Element set:     907
Inclination:       51
6447  deg
RA of node:       315
4973  deg
Eccentricity:     
0007038     
Arg of perigee:   172
9253  deg
Mean anomaly:     187
2012  deg
Mean motion:   15
77272768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3879
Checksum:              325


Coasting Arc #9 (Orbit 3894)
---------------------------------------

Vector Time (GMT): 2010/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4014344
05                 A    =         6711077
65  meter
 Y    =        1596772
72  meter          E    =           
0009952
 Z    =        5134144
32                 I    =           51
36915
 XDOT =      -4107
213169                 Wp   =          159
12805
 YDOT =       6409
764326  meter/sec      RA   =          309
93617  deg
 ZDOT =       1207
997494                 TA   =          279
24258
                                          MA   =          279
35513
                                          Ha   =            186
258  n
mi
                                          Hp   =            178
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13170420
11                 X    =         3971249
89
 Y    =        5238755
65  feet           Y    =         1641421
85  meter
 Z    =       16844305
50                 Z    =         5153541
28
 XDOT =     -13475
108822                 XDOT =       -4184
451180
 YDOT =      21029
410519  feet/sec       YDOT =        6363
403019  meter/sec
 ZDOT =       3963
246370                 ZDOT =        1187
858164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -181438
46                 X    =          -55302
44
 Y    =       14081110
14  feet           Y    =         4291922
37  meter
 Z    =       16921127
97                 Z    =         5157559
81
 XDOT =     -23452
318671                 XDOT =       -7148
266731
 YDOT =      -5007
907033  feet/sec       YDOT =       -1526
410064  meter/sec
 ZDOT =       3883
604544                 ZDOT =        1183
722665


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   10012
54951709  
00016717  00000-0  10270-3 0  9089
2 25544  51
6450 310
2672 0007048 178
4518 181
6670 15
77332410 38954


Satellite: ISS
Catalog Number: 25544
Epoch time:      10012
54951709   =   yrday
fracday
Element set:     908
Inclination:       51
6450  deg
RA of node:       310
2672  deg
Eccentricity:     
0007048     
Arg of perigee:   178
4518  deg
Mean anomaly:     181
6670  deg
Mean motion:   15
77332410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3895
Checksum:              307


Coasting Arc #10 (Orbit 3910)
---------------------------------------

Vector Time (GMT): 2010/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3863765
35                 A    =         6722761
41  meter
 Y    =       -5499811
40  meter          E    =           
0008947
 Z    =          50262
07                 I    =           51
38970
 XDOT =       3902
813533                 Wp   =           78
90752
 YDOT =       2805
072903  meter/sec      RA   =          304
74691  deg
 ZDOT =       6017
667570                 TA   =          281
64078
                                          MA   =          281
74119
                                          Ha   =            186
291  n
mi
                                          Hp   =            178
249

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12676395
49                 X    =         3924733
88
 Y    =      -18044000
65  feet           Y    =        -5456263
60  meter
 Z    =         164901
82                 Z    =           69179
30
 XDOT =      12804
506343                 XDOT =        3841
924427
 YDOT =       9202
995088  feet/sec       YDOT =        2848
375250  meter/sec
 ZDOT =      19743
003839                 ZDOT =        6036
479569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21486043
15                 X    =         6548945
95
 Y    =        4959500
03  feet           Y    =         1511655
61  meter
 Z    =         239716
83                 Z    =           73065
69
 XDOT =      -3394
877120                 XDOT =       -1034
758546
 YDOT =      13651
310314  feet/sec       YDOT =        4160
919384  meter/sec
 ZDOT =      19817
535199                 ZDOT =        6040
384729


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   10013
56321901  
00016717  00000-0  10270-3 0  9098
2 25544  51
6448 305
0359 0006958 181
4870 178
6275 15
77312933 39113


Satellite: ISS
Catalog Number: 25544
Epoch time:      10013
56321901   =   yrday
fracday
Element set:     909
Inclination:       51
6448  deg
RA of node:       305
0359  deg
Eccentricity:     
0006958     
Arg of perigee:   181
4870  deg
Mean anomaly:     178
6275  deg
Mean motion:   15
77312933  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3911
Checksum:              315


Coasting Arc #11 (Orbit 3925)
---------------------------------------

Vector Time (GMT): 2010/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2816740
29                 A    =         6711246
85  meter
 Y    =       -3329188
18  meter          E    =           
0016271
 Z    =       -5114580
64                 I    =           51
33545
 XDOT =       4634
443384                 Wp   =          125
30814
 YDOT =      -5994
338394  meter/sec      RA   =          299
55403  deg
 ZDOT =       1343
258211                 TA   =          157
64565
                                          MA   =          157
57465
                                          Ha   =            186
122  n
mi
                                          Hp   =            178
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9241273
92                 X    =        -2754458
20
 Y    =      -10922533
41  feet           Y    =        -3360337
80  meter
 Z    =      -16780120
22                 Z    =        -5128113
19
 XDOT =      15204
866747                 XDOT =        4694
603526
 YDOT =     -19666
464547  feet/sec       YDOT =       -5942
177092  meter/sec
 ZDOT =       4407
015127                 ZDOT =        1365
917286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6465798
41                 X    =         1970775
36
 Y    =      -12692248
62  feet           Y    =        -3868597
38  meter
 Z    =      -16833763
40                 Z    =        -5130931
08
 XDOT =      23116
410938                 XDOT =        7045
882054
 YDOT =       5785
084966  feet/sec       YDOT =        1763
293898  meter/sec
 ZDOT =       4496
634568                 ZDOT =        1370
574216


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   10014
51355164  
00016717  00000-0  10270-3 0  9104
2 25544  51
6455 300
1318 0006917 185
1884 174
9210 15
77331533 39264


Satellite: ISS
Catalog Number: 25544
Epoch time:      10014
51355164   =   yrday
fracday
Element set:     910
Inclination:       51
6455  deg
RA of node:       300
1318  deg
Eccentricity:     
0006917     
Arg of perigee:   185
1884  deg
Mean anomaly:     174
9210  deg
Mean motion:   15
77331533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3926
Checksum:              292


Coasting Arc #12 (Orbit 3941)
---------------------------------------

Vector Time (GMT): 2010/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4140555
60                 A    =         6720411
88  meter
 Y    =        4786839
96  meter          E    =           
0011524
 Z    =       -2242066
85                 I    =           51
35330
 XDOT =      -2604
846931                 Wp   =          164
69654
 YDOT =      -4794
990945  meter/sec      RA   =          294
40433  deg
 ZDOT =      -5444
143623                 TA   =           40
61492
                                          MA   =           40
52902
                                          Ha   =            185
911  n
mi
                                          Hp   =            178
526

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13584499
99                 X    =        -4182883
85
 Y    =       15704855
50  feet           Y    =         4740301
37  meter
 Z    =       -7355862
37                 Z    =        -2262283
52
 XDOT =      -8546
085733                 XDOT =       -2524
588866
 YDOT =     -15731
597589  feet/sec       YDOT =       -4823
670588  meter/sec
 ZDOT =     -17861
363591                 ZDOT =       -5456
603211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19860866
66                 X    =        -6053592
16
 Y    =       -5961902
53  feet           Y    =        -1817187
89  meter
 Z    =       -7435827
54                 Z    =        -2266440
23
 XDOT =      10489
042893                 XDOT =        3197
060274
 YDOT =     -12673
383096  feet/sec       YDOT =       -3862
847168  meter/sec
 ZDOT =     -17910
793872                 ZDOT =       -5459
209972


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   10015
52722790  
00016717  00000-0  10270-3 0  9110
2 25544  51
6460 294
9012 0006924 189
2126 170
8913 15
77350568 39425


Satellite: ISS
Catalog Number: 25544
Epoch time:      10015
52722790   =   yrday
fracday
Element set:     911
Inclination:       51
6460  deg
RA of node:       294
9012  deg
Eccentricity:     
0006924     
Arg of perigee:   189
2126  deg
Mean anomaly:     170
8913  deg
Mean motion:   15
77350568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3942
Checksum:              309


Coasting Arc #13 (Orbit 3957)
---------------------------------------

Vector Time (GMT): 2010/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1793234
81                 A    =         6715035
36  meter
 Y    =        4957010
20  meter          E    =           
0009294
 Z    =        4149974
41                 I    =           51
32312
 XDOT =      -4783
517842                 Wp   =          115
02820
 YDOT =       4806
574766  meter/sec      RA   =          289
17653  deg
 ZDOT =      -3671
786032                 TA   =           12
56619
                                          MA   =           12
54304
                                          Ha   =            185
767  n
mi
                                          Hp   =            178
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5883316
30                 X    =         1717512
05
 Y    =       16263156
84  feet           Y    =         4976639
49  meter
 Z    =       13615401
62                 Z    =         4158502
21
 XDOT =     -15693
956174                 XDOT =       -4819
073861
 YDOT =      15769
602250  feet/sec       YDOT =        4752
884137  meter/sec
 ZDOT =     -12046
542101                 ZDOT =       -3695
109753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12277441
04                 X    =        -3742164
03
 Y    =       12142674
87  feet           Y    =         3701087
30  meter
 Z    =       13649275
84                 Z    =         4160299
28
 XDOT =     -20014
931586                 XDOT =       -6100
551148
 YDOT =      -6582
877412  feet/sec       YDOT =       -2006
461035  meter/sec
 ZDOT =     -12138
805506                 ZDOT =       -3699
907918


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   10016
54089207  
00016717  00000-0  10270-3 0  9123
2 25544  51
6452 289
6707 0006871 192
8054 167
2938 15
77367752 39586


Satellite: ISS
Catalog Number: 25544
Epoch time:      10016
54089207   =   yrday
fracday
Element set:     912
Inclination:       51
6452  deg
RA of node:       289
6707  deg
Eccentricity:     
0006871     
Arg of perigee:   192
8054  deg
Mean anomaly:     167
2938  deg
Mean motion:   15
77367752  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3958
Checksum:              343


Coasting Arc #14 (Orbit 3973)
---------------------------------------

Vector Time (GMT): 2010/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4164668
71                 A    =         6715448
09  meter
 Y    =       -3413948
20  meter          E    =           
0012337
 Z    =        4011277
33                 I    =           51
31619
 XDOT =       1570
665919                 Wp   =          136
19296
 YDOT =       6477
096556  meter/sec      RA   =          284
04340  deg
 ZDOT =       3865
971153                 TA   =          273
73745
                                          MA   =          273
87851
                                          Ha   =            185
634  n
mi
                                          Hp   =            178
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13663611
24                 X    =         4183048
97
 Y    =      -11200617
45  feet           Y    =        -3367273
89  meter
 Z    =       13160358
68                 Z    =         4031553
22
 XDOT =       5153
103410                 XDOT =        1479
341420
 YDOT =      21250
316785  feet/sec       YDOT =        6494
149808  meter/sec
 ZDOT =      12683
632391                 ZDOT =        3873
379845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16026532
48                 X    =         4884887
10
 Y    =        7292496
24  feet           Y    =         2222752
85  meter
 Z    =       13240577
75                 Z    =         4035728
10
 XDOT =     -16334
245235                 XDOT =       -4978
677948
 YDOT =      12720
849751  feet/sec       YDOT =        3877
315004  meter/sec
 ZDOT =      12713
119499                 ZDOT =        3874
958823


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   10017
55454333  
00016717  00000-0  10270-3 0  9132
2 25544  51
6454 284
4392 0006832 196
9870 163
1067 15
77386623 39743


Satellite: ISS
Catalog Number: 25544
Epoch time:      10017
55454333   =   yrday
fracday
Element set:     913
Inclination:       51
6454  deg
RA of node:       284
4392  deg
Eccentricity:     
0006832     
Arg of perigee:   196
9870  deg
Mean anomaly:     163
1067  deg
Mean motion:   15
77386623  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3974
Checksum:              329


Coasting Arc #15 (Orbit 3988)
---------------------------------------

Vector Time (GMT): 2010/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 751809
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -999375
67                 A    =         6719874
29  meter
 Y    =       -6191548
82  meter          E    =           
0003078
 Z    =       -2418769
63                 I    =           51
32559
 XDOT =       4763
002337                 Wp   =          149
38172
 YDOT =      -2852
602656  meter/sec      RA   =          278
81149  deg
 ZDOT =       5334
481603                 TA   =          183
17283
                                          MA   =          183
17478
                                          Ha   =            185
472  n
mi
                                          Hp   =            178
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3278791
56                 X    =         -918316
72
 Y    =      -20313480
37  feet           Y    =        -6202271
10  meter
 Z    =       -7935595
88                 Z    =        -2423427
87
 XDOT =      15626
648087                 XDOT =        4768
633287
 YDOT =      -9358
932600  feet/sec       YDOT =       -2799
308698  meter/sec
 ZDOT =      17501
580061                 ZDOT =        5357
633296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16628648
15                 X    =         5068411
96
 Y    =      -12107042
22  feet           Y    =        -3690226
47  meter
 Z    =       -7954195
77                 Z    =        -2424438
87
 XDOT =      14506
076268                 XDOT =        4421
452047
 YDOT =       8365
890987  feet/sec       YDOT =        2549
923573  meter/sec
 ZDOT =      17593
197604                 ZDOT =        5362
406630


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   10018
50482981  
00016717  00000-0  10270-3 0  9149
2 25544  51
6457 279
5347 0006842 201
2097 158
8786 15
77425984 39892


Satellite: ISS
Catalog Number: 25544
Epoch time:      10018
50482981   =   yrday
fracday
Element set:     914
Inclination:       51
6457  deg
RA of node:       279
5347  deg
Eccentricity:     
0006842     
Arg of perigee:   201
2097  deg
Mean anomaly:     158
8786  deg
Mean motion:   15
77425984  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3989
Checksum:              355

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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