Date: February 14th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 23142 41 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


046/05:01:30 000 -0 3 0 4 0 4
N/A -0 1 0 0 188 8
000/00:05:00 000 0 3 0 1 181 2

046/05:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 8
000/00:00:00 000 0 0 0 0 181 1

046/06:46:30 000 -0 0 0 4 0 4
N/A -0 3 -0 0 189 0
000/00:05:00 000 0 3 -0 0 181 2

046/07:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 9
000/00:00:00 000 0 0 0 0 181 3

049/05:46:30 000 -0 5 0 8 0 8
N/A 0 6 0 1 189 5
000/00:05:00 000 -0 1 0 1 180 7

049/06:17:00 000 -0 5 2 2 2 2
N/A -1 4 -0 1 191 1
000/00:26:00 000 1 6 -0 0 180 8

049/06:41:30 000 0 3 0 5 0 5
N/A -0 3 -0 0 191 1
000/00:05:00 000 -0 1 -0 1 181 0

049/07:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 191 2
000/00:00:00 000 0 0 0 0 180 9

Coasting Arc #1 (Orbit 384)
---------------------------------------

Vector Time (GMT): 2010/043/13:54:18
929
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5142457
34                 A    =         6726087
21  meter
 Y    =       -4159304
37  meter          E    =           
0004416
 Z    =        1222893
03                 I    =           51
83366
 XDOT =       3891
370733                 Wp   =           76
74948
 YDOT =       3074
601146  meter/sec      RA   =          149
38945  deg
 ZDOT =      -5887
791139                 TA   =           89
87983
                                          MA   =           89
82922
                                          Ha   =            188
112  n
mi
                                          Hp   =            182
047

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16871579
18                 X    =         5182644
81
 Y    =      -13646011
71  feet           Y    =        -4101573
65  meter
 Z    =        4012116
24                 Z    =         1247971
94
 XDOT =      12766
964347                 XDOT =        3885
301704
 YDOT =      10087
274102  feet/sec       YDOT =        3118
082781  meter/sec
 ZDOT =     -19316
900063                 ZDOT =       -5868
902225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18903370
51                 X    =         5761747
33
 Y    =      -10616925
64  feet           Y    =        -3236038
94  meter
 Z    =        4111492
36                 Z    =         1253182
87
 XDOT =      10225
419141                 XDOT =        3116
707754
 YDOT =      10731
564823  feet/sec       YDOT =        3270
980958  meter/sec
 ZDOT =     -19241
801506                 ZDOT =       -5864
901099


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   10043
61352491  
00016717  00000-0  10270-3 0  9006
2 25544  51
6459 150
2251 0011255 317
4630  42
5661 15
75900006  3859


Satellite: ISS
Catalog Number: 25544
Epoch time:      10043
61352491   =   yrday
fracday
Element set:     900
Inclination:       51
6459  deg
RA of node:       150
2251  deg
Eccentricity:     
0011255     
Arg of perigee:   317
4630  deg
Mean anomaly:      42
5661  deg
Mean motion:   15
75900006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             385
Checksum:              269


Coasting Arc #2 (Orbit 400)
---------------------------------------

Vector Time (GMT): 2010/044/13:54:18
929
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2999465
40                 A    =         6714678
96  meter
 Y    =       -2926965
43  meter          E    =           
0008685
 Z    =        5249352
06                 I    =           51
82160
 XDOT =       5912
621579                 Wp   =          329
07466
 YDOT =      -4891
462100  meter/sec      RA   =          144
27023  deg
 ZDOT =        658
822095                 TA   =          114
72342
                                          MA   =          114
63300
                                          Ha   =            188
275  n
mi
                                          Hp   =            181
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9840765
75                 X    =        -2992012
25
 Y    =       -9602904
94  feet           Y    =        -2960465
41  meter
 Z    =       17222283
68                 Z    =         5234799
29
 XDOT =      19398
364762                 XDOT =        5963
678999
 YDOT =     -16048
104004  feet/sec       YDOT =       -4825
058164  meter/sec
 ZDOT =       2161
489812                 ZDOT =         687
668870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8374915
73                 X    =        -2552674
31
 Y    =      -10995807
50  feet           Y    =        -3351522
13  meter
 Z    =       17164396
67                 Z    =         5231708
10
 XDOT =      20787
884827                 XDOT =        6336
147295
 YDOT =     -12320
467574  feet/sec       YDOT =       -3755
278517  meter/sec
 ZDOT =       2275
800258                 ZDOT =         693
663919


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   10044
62812066  
00016717  00000-0  10270-3 0  9018
2 25544  51
6465 145
0001 0011367 320
9537  39
0806 15
75956628  4012


Satellite: ISS
Catalog Number: 25544
Epoch time:      10044
62812066   =   yrday
fracday
Element set:     901
Inclination:       51
6465  deg
RA of node:       145
0001  deg
Eccentricity:     
0011367     
Arg of perigee:   320
9537  deg
Mean anomaly:      39
0806  deg
Mean motion:   15
75956628  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             401
Checksum:              284


Coasting Arc #3 (Orbit 416)
---------------------------------------

Vector Time (GMT): 2010/045/13:54:18
929
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5120433
98                 A    =         6726708
46  meter
 Y    =        4342532
39  meter          E    =           
0018387
 Z    =          84959
15                 I    =           51
88510
 XDOT =      -3019
163695                 Wp   =            8
06503
 YDOT =      -3681
415992  meter/sec      RA   =          139
13061  deg
 ZDOT =       6066
700877                 TA   =          352
85646
                                          MA   =          352
88262
                                          Ha   =            188
593  n
mi
                                          Hp   =            181
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16799324
07                 X    =        -5169025
09
 Y    =       14247153
51  feet           Y    =         4285000
98  meter
 Z    =         278737
36                 Z    =           59966
57
 XDOT =      -9905
392701                 XDOT =       -3007
243157
 YDOT =     -12078
136457  feet/sec       YDOT =       -3715
111147  meter/sec
 ZDOT =      19903
874267                 ZDOT =        6052
063319

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18561075
73                 X    =        -5657415
88
 Y    =       11862990
49  feet           Y    =         3615839
50  meter
 Z    =         179697
75                 Z    =           54771
87
 XDOT =      -7445
159438                 XDOT =       -2269
284597
 YDOT =     -11960
187399  feet/sec       YDOT =       -3645
465119  meter/sec
 ZDOT =      19845
615649                 ZDOT =        6048
943650


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   10045
64269586  
00016717  00000-0  10270-3 0  9025
2 25544  51
6459 139
7757 0011526 326
4931  33
5503 15
75927042  4177


Satellite: ISS
Catalog Number: 25544
Epoch time:      10045
64269586   =   yrday
fracday
Element set:     902
Inclination:       51
6459  deg
RA of node:       139
7757  deg
Eccentricity:     
0011526     
Arg of perigee:   326
4931  deg
Mean anomaly:      33
5503  deg
Mean motion:   15
75927042  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             417
Checksum:              316


Coasting Arc #4 (Orbit 425)
---------------------------------------

Vector Time (GMT): 2010/046/05:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764501
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4076277
87                 A    =         6726151
74  meter
 Y    =        5210191
11  meter          E    =           
0017659
 Z    =       -1149928
37                 I    =           51
89486
 XDOT =      -4437
010247                 Wp   =          358
56977
 YDOT =      -2167
501649  meter/sec      RA   =          135
87363  deg
 ZDOT =       5922
999857                 TA   =          348
85948
                                          MA   =          348
89852
                                          Ha   =            188
841  n
mi
                                          Hp   =            181
199

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13373615
07                 X    =        -4128650
20
 Y    =       17093802
85  feet           Y    =         5164314
86  meter
 Z    =       -3772730
87                 Z    =        -1169857
90
 XDOT =     -14557
120233                 XDOT =       -4441
215198
 YDOT =      -7111
225882  feet/sec       YDOT =       -2217
142116  meter/sec
 ZDOT =      19432
414229                 ZDOT =        5901
435337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -884617
55                 X    =         -269631
43
 Y    =      -21671813
58  feet           Y    =        -6605568
78  meter
 Z    =       -3851638
87                 Z    =        -1173979
53
 XDOT =      14205
892463                 XDOT =        4329
956023
 YDOT =      -4009
516918  feet/sec       YDOT =       -1222
100757  meter/sec
 ZDOT =      19346
715455                 ZDOT =        5896
878871


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   10046
21337920  
00016717  00000-0  10270-3 0  9038
2 25544  51
6435 136
8348 0011995 328
6936  31
3512 15
75908872  4260


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
21337920   =   yrday
fracday
Element set:     903
Inclination:       51
6435  deg
RA of node:       136
8348  deg
Eccentricity:     
0011995     
Arg of perigee:   328
6936  deg
Mean anomaly:      31
3512  deg
Mean motion:   15
75908872  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             426
Checksum:              312


Coasting Arc #5 (Orbit 426)
---------------------------------------

Vector Time (GMT): 2010/046/05:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010385
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4166452
81                 A    =         6726079
13  meter
 Y    =       -5182157
94  meter          E    =           
0005915
 Z    =        1020281
08                 I    =           51
89590
 XDOT =       4319
086139                 Wp   =           62
66645
 YDOT =       2296
907005  meter/sec      RA   =          135
71043  deg
 ZDOT =      -5942
401112                 TA   =          106
22082
                                          MA   =          106
15573
                                          Ha   =            188
807  n
mi
                                          Hp   =            181
056

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13669464
60                 X    =         4219134
75
 Y    =      -17001830
50  feet           Y    =        -5135271
57  meter
 Z    =        3347378
87                 Z    =         1040649
42
 XDOT =      14170
230115                 XDOT =        4321
947069
 YDOT =       7535
784138  feet/sec       YDOT =        2345
221256  meter/sec
 ZDOT =     -19496
066641                 ZDOT =       -5921
412723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4942516
93                 X    =         1506479
16
 Y    =       21235385
16  feet           Y    =         6472545
40  meter
 Z    =        3428030
26                 Z    =         1044863
62
 XDOT =     -13199
871094                 XDOT =       -4023
320710
 YDOT =       6220
953782  feet/sec       YDOT =        1896
146713  meter/sec
 ZDOT =     -19412
649707                 ZDOT =       -5916
975631


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   10046
27679015  
00016717  00000-0  10270-3 0  9049
2 25544  51
6434 136
5078 0012119 329
2439  30
8014 15
75975756  4277


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
27679015   =   yrday
fracday
Element set:     904
Inclination:       51
6434  deg
RA of node:       136
5078  deg
Eccentricity:     
0012119     
Arg of perigee:   329
2439  deg
Mean anomaly:      30
8014  deg
Mean motion:   15
75975756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             427
Checksum:              310


Coasting Arc #6 (Orbit 427)
---------------------------------------

Vector Time (GMT): 2010/046/06:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010305
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5512724
10                 A    =         6721636
95  meter
 Y    =        1565010
99  meter          E    =           
0011808
 Z    =        3497904
55                 I    =           51
87995
 XDOT =       1144
844989                 Wp   =           33
79726
 YDOT =      -6121
221022  meter/sec      RA   =          135
53406  deg
 ZDOT =       4545
334217                 TA   =            7
67441
                                          MA   =            7
65636
                                          Ha   =            189
039  n
mi
                                          Hp   =            181
243

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18086365
16                 X    =        -5546806
36
 Y    =        5134550
50  feet           Y    =         1503174
07  meter
 Z    =       11476064
79                 Z    =         3471041
56
 XDOT =       3756
053114                 XDOT =        1191
128645
 YDOT =     -20082
746136  feet/sec       YDOT =       -6108
159647  meter/sec
 ZDOT =      14912
513834                 ZDOT =        4551
008490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2480374
75                 X    =          756018
22
 Y    =      -18701948
66  feet           Y    =        -5700353
95  meter
 Z    =       11369482
58                 Z    =         3465418
29
 XDOT =      15620
207748                 XDOT =        4761
039322
 YDOT =      11146
275553  feet/sec       YDOT =        3397
384789  meter/sec
 ZDOT =      14934
791923                 ZDOT =        4552
124578


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   10046
34020703  
00016717  00000-0  10270-3 0  9052
2 25544  51
6428 136
1795 0011754 330
3629  29
6868 15
75862958  4283


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
34020703   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:       136
1795  deg
Eccentricity:     
0011754     
Arg of perigee:   330
3629  deg
Mean anomaly:      29
6868  deg
Mean motion:   15
75862958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             428
Checksum:              319


Coasting Arc #7 (Orbit 427)
---------------------------------------

Vector Time (GMT): 2010/046/07:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1882723
15                 A    =         6715278
86  meter
 Y    =        3852782
04  meter          E    =           
0011521
 Z    =       -5173717
71                 I    =           51
86096
 XDOT =      -6041
013640                 Wp   =           47
75328
 YDOT =       4608
524018  meter/sec      RA   =          135
28147  deg
 ZDOT =       1242
889326                 TA   =          234
03736
                                          MA   =          234
14427
                                          Ha   =            188
949  n
mi
                                          Hp   =            181
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6176913
24                 X    =         1864633
07
 Y    =       12640361
02  feet           Y    =         3873734
33  meter
 Z    =      -16974139
47                 Z    =        -5164615
84
 XDOT =     -19819
598558                 XDOT =       -6098
135570
 YDOT =      15119
829457  feet/sec       YDOT =        4540
650505  meter/sec
 ZDOT =       4077
720886                 ZDOT =        1213
403841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13394904
21                 X    =        -4082766
80
 Y    =        4442996
92  feet           Y    =         1354225
46  meter
 Z    =      -16937848
57                 Z    =        -5162656
24
 XDOT =     -11865
513707                 XDOT =       -3616
608578
 YDOT =     -20789
744566  feet/sec       YDOT =       -6336
714144  meter/sec
 ZDOT =       3960
850690                 ZDOT =        1207
267290


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   10046
34020830  
00016717  00000-0  10270-3 0  9064
2 25544  51
6442 136
1803 0011561 330
7963  29
2553 15
75858410  4285


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
34020830   =   yrday
fracday
Element set:     906
Inclination:       51
6442  deg
RA of node:       136
1803  deg
Eccentricity:     
0011561     
Arg of perigee:   330
7963  deg
Mean anomaly:      29
2553  deg
Mean motion:   15
75858410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             428
Checksum:              283


Coasting Arc #8 (Orbit 443)
---------------------------------------

Vector Time (GMT): 2010/047/07:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5131978
33                 A    =         6725515
30  meter
 Y    =       -4001066
05  meter          E    =           
0004455
 Z    =       -1710052
38                 I    =           51
91602
 XDOT =       1828
524853                 Wp   =          357
13626
 YDOT =       4797
457699  meter/sec      RA   =          130
17467  deg
 ZDOT =      -5732
257946                 TA   =          201
70222
                                          MA   =          201
72111
                                          Ha   =            189
051  n
mi
                                          Hp   =            180
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16837199
24                 X    =         5184644
49
 Y    =      -13126857
10  feet           Y    =        -3943382
86  meter
 Z    =       -5610408
07                 Z    =        -1684993
58
 XDOT =       5999
097288                 XDOT =        1802
588596
 YDOT =      15739
690614  feet/sec       YDOT =        4817
759947  meter/sec
 ZDOT =     -18806
620559                 ZDOT =       -5723
438488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10950367
61                 X    =         3337672
05
 Y    =       18357553
48  feet           Y    =         5595382
30  meter
 Z    =       -5511081
00                 Z    =        -1679777
49
 XDOT =     -15032
993575                 XDOT =       -4582
056442
 YDOT =       3326
923308  feet/sec       YDOT =        1014
046224  meter/sec
 ZDOT =     -18771
412714                 ZDOT =       -5721
526595


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   10047
35483542  
00016717  00000-0  10270-3 0  9070
2 25544  51
6437 130
9548 0011728 334
9521  25
1073 15
75908869  4442


Satellite: ISS
Catalog Number: 25544
Epoch time:      10047
35483542   =   yrday
fracday
Element set:     907
Inclination:       51
6437  deg
RA of node:       130
9548  deg
Eccentricity:     
0011728     
Arg of perigee:   334
9521  deg
Mean anomaly:      25
1073  deg
Mean motion:   15
75908869  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             444
Checksum:              316


Coasting Arc #9 (Orbit 459)
---------------------------------------

Vector Time (GMT): 2010/048/07:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1357261
62                 A    =         6717008
94  meter
 Y    =       -4554260
62  meter          E    =           
0014628
 Z    =        4750964
91                 I    =           51
90605
 XDOT =       5675
545956                 Wp   =            9
74219
 YDOT =      -4476
244262  meter/sec      RA   =          125
00782  deg
 ZDOT =      -2654
220585                 TA   =          106
31364
                                          MA   =          106
15271
                                          Ha   =            189
215  n
mi
                                          Hp   =            180
746

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4452958
06                 X    =        -1329313
12
 Y    =      -14941799
94  feet           Y    =        -4569281
73  meter
 Z    =       15587155
23                 Z    =         4744439
66
 XDOT =      18620
557600                 XDOT =        5738
071795
 YDOT =     -14685
840753  feet/sec       YDOT =       -4412
427524  meter/sec
 ZDOT =      -8708
072787                 ZDOT =       -2626
497083

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15339023
91                 X    =         4675334
49
 Y    =       -2934814
32  feet           Y    =         -894531
41  meter
 Z    =       15561068
08                 Z    =         4743013
55
 XDOT =      12409
788714                 XDOT =        3782
503600
 YDOT =      19004
598162  feet/sec       YDOT =        5792
601520  meter/sec
 ZDOT =      -8598
177707                 ZDOT =       -2620
724565


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10048
36944030  
00016717  00000-0  10270-3 0  9087
2 25544  51
6440 125
7300 0011565 339
0346  21
0343 15
75888783  4609


Satellite: ISS
Catalog Number: 25544
Epoch time:      10048
36944030   =   yrday
fracday
Element set:     908
Inclination:       51
6440  deg
RA of node:       125
7300  deg
Eccentricity:     
0011565     
Arg of perigee:   339
0346  deg
Mean anomaly:      21
0343  deg
Mean motion:   15
75888783  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             460
Checksum:              290


Coasting Arc #10 (Orbit 473)
---------------------------------------

Vector Time (GMT): 2010/049/05:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764501
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3208659
36                 A    =         6715037
72  meter
 Y    =        2682467
87  meter          E    =           
0014694
 Z    =       -5261943
44                 I    =           51
91254
 XDOT =      -4293
501201                 Wp   =           47
26879
 YDOT =       6356
819571  meter/sec      RA   =          120
32547  deg
 ZDOT =        633
363146                 TA   =          228
66905
                                          MA   =          228
79558
                                          Ha   =            189
536  n
mi
                                          Hp   =            180
729

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10527097
62                 X    =         3203986
27
 Y    =        8800747
61  feet           Y    =         2718322
53  meter
 Z    =      -17263593
98                 Z    =        -5246367
52
 XDOT =     -14086
290031                 XDOT =       -4367
341906
 YDOT =      20855
707254  feet/sec       YDOT =        6308
394269  meter/sec
 ZDOT =       2077
963078                 ZDOT =         612
325833

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13332259
68                 X    =        -4063672
75
 Y    =        3557922
34  feet           Y    =         1084454
73  meter
 Z    =      -17201647
02                 Z    =        -5243062
01
 XDOT =      -8560
248800                 XDOT =       -2609
163834
 YDOT =     -22606
096224  feet/sec       YDOT =       -6890
338129  meter/sec
 ZDOT =       1994
679378                 ZDOT =         607
978274


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10049
25719685  
00016717  00000-0  10270-3 0  9093
2 25544  51
6428 121
1595 0011944 340
0727  19
9969 15
75818372  4749


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
25719685   =   yrday
fracday
Element set:     909
Inclination:       51
6428  deg
RA of node:       121
1595  deg
Eccentricity:     
0011944     
Arg of perigee:   340
0727  deg
Mean anomaly:      19
9969  deg
Mean motion:   15
75818372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             474
Checksum:              336


Coasting Arc #11 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/06:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010385
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4212841
14                 A    =         6717019
98  meter
 Y    =        -810426
65  meter          E    =           
0010628
 Z    =        5166396
50                 I    =           51
91455
 XDOT =       2915
182875                 Wp   =             
93923
 YDOT =      -7015
408752  meter/sec      RA   =          120
19433  deg
 ZDOT =       1287
022761                 TA   =           76
86791
                                          MA   =           76
74933
                                          Ha   =            191
142  n
mi
                                          Hp   =            180
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13821657
27                 X    =        -4228562
77
 Y    =       -2658880
08  feet           Y    =         -857624
70  meter
 Z    =       16950119
75                 Z    =         5145892
67
 XDOT =       9564
248279                 XDOT =        2987
161720
 YDOT =     -23016
432914  feet/sec       YDOT =       -6982
406908  meter/sec
 ZDOT =       4222
515621                 ZDOT =        1301
359818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8323719
82                 X    =         2537069
80
 Y    =      -11470736
00  feet           Y    =        -3496280
33  meter
 Z    =       16868678
58                 Z    =         5141573
23
 XDOT =      15942
227700                 XDOT =        4859
191003
 YDOT =      17811
087247  feet/sec       YDOT =        5428
819393  meter/sec
 ZDOT =       4279
171085                 ZDOT =        1304
291347


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10049
32063536  
00016717  00000-0  10270-3 0  9100
2 25544  51
6429 120
8319 0013493 345
9081  14
1704 15
75273208  4756


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32063536   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:       120
8319  deg
Eccentricity:     
0013493     
Arg of perigee:   345
9081  deg
Mean anomaly:      14
1704  deg
Mean motion:   15
75273208  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              290


Coasting Arc #12 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/06:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010305
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -321516
70                 A    =         6722351
16  meter
 Y    =       -5489597
78  meter          E    =           
0016742
 Z    =        3871134
96                 I    =           51
93169
 XDOT =       5623
600894                 Wp   =           29
65172
 YDOT =      -3254
843545  meter/sec      RA   =          120
10810  deg
 ZDOT =      -4126
787908                 TA   =          103
36304
                                          MA   =          103
17634
                                          Ha   =            191
133  n
mi
                                          Hp   =            180
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1054844
82                 X    =         -278912
17
 Y    =      -18010491
40  feet           Y    =        -5492954
70  meter
 Z    =       12700574
03                 Z    =         3869676
90
 XDOT =      18450
134167                 XDOT =        5679
626092
 YDOT =     -10678
620555  feet/sec       YDOT =       -3191
644119  meter/sec
 ZDOT =     -13539
330408                 ZDOT =       -4099
332535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17156819
94                 X    =         5229398
72
 Y    =        5593424
67  feet           Y    =         1704875
84  meter
 Z    =       12694574
00                 Z    =         3869306
15
 XDOT =       3499
055508                 XDOT =        1066
512119
 YDOT =      19910
701850  feet/sec       YDOT =        6068
781924  meter/sec
 ZDOT =     -13430
444317                 ZDOT =       -4093
599428


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10049
32063880  
00016717  00000-0  10270-3 0  9113
2 25544  51
6429 120
8321 0013106 347
2021  12
8809 15
75166501  4757


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32063880   =   yrday
fracday
Element set:     911
Inclination:       51
6429  deg
RA of node:       120
8321  deg
Eccentricity:     
0013106     
Arg of perigee:   347
2021  deg
Mean anomaly:      12
8809  deg
Mean motion:   15
75166501  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              274


Coasting Arc #13 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         254298
69                 A    =         6722513
85  meter
 Y    =        5530583
05  meter          E    =           
0011620
 Z    =       -3806624
26                 I    =           51
93462
 XDOT =      -5625
949308                 Wp   =           15
72893
 YDOT =       3151
165171  meter/sec      RA   =          119
94522  deg
 ZDOT =       4216
351463                 TA   =          298
24796
                                          MA   =          298
36521
                                          Ha   =            191
154  n
mi
                                          Hp   =            180
937

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         834313
30                 X    =          210927
47
 Y    =       18144957
52  feet           Y    =         5533184
02  meter
 Z    =      -12488924
73                 Z    =        -3805494
60
 XDOT =     -18457
838938                 XDOT =       -5681
250061
 YDOT =      10338
468409  feet/sec       YDOT =        3087
943539  meter/sec
 ZDOT =      13833
174092                 ZDOT =        4188
886446

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18022108
34                 X    =        -5493138
62
 Y    =       -2292702
29  feet           Y    =         -698815
66  meter
 Z    =      -12484227
26                 Z    =        -3805192
47
 XDOT =      -7089
830086                 XDOT =       -2160
980210
 YDOT =     -18752
060993  feet/sec       YDOT =       -5715
628191  meter/sec
 ZDOT =      13724
245461                 ZDOT =        4183
150016


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10049
32063851  
00016717  00000-0  10270-3 0  9122
2 25544  51
6447 120
8330 0013136 347
0001  13
0823 15
75175572  4753


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32063851   =   yrday
fracday
Element set:     912
Inclination:       51
6447  deg
RA of node:       120
8330  deg
Eccentricity:     
0013136     
Arg of perigee:   347
0001  deg
Mean anomaly:      13
0823  deg
Mean motion:   15
75175572  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              269


Coasting Arc #14 (Orbit 490)
---------------------------------------

Vector Time (GMT): 2010/050/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4695542
15                 A    =         6721951
75  meter
 Y    =       -2731374
71  meter          E    =           
0015673
 Z    =       -3974461
28                 I    =           51
94693
 XDOT =        415
107647                 Wp   =           16
65822
 YDOT =       6553
491477  meter/sec      RA   =          114
87343  deg
 ZDOT =      -4002
538218                 TA   =          211
92125
                                          MA   =          212
01630
                                          Ha   =            191
218  n
mi
                                          Hp   =            180
774

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15405322
01                 X    =         4745042
90
 Y    =       -8961203
12  feet           Y    =        -2678589
81  meter
 Z    =      -13039571
13                 Z    =        -3951530
20
 XDOT =       1361
901729                 XDOT =         361
237895
 YDOT =      21500
956289  feet/sec       YDOT =        6557
832042  meter/sec
 ZDOT =     -13131
687066                 ZDOT =       -4000
652843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6391940
55                 X    =         1948263
48
 Y    =       16707299
03  feet           Y    =         5092384
74  meter
 Z    =      -12948620
70                 Z    =        -3946739
59
 XDOT =     -20238
342391                 XDOT =       -6168
646761
 YDOT =      -2456
244738  feet/sec       YDOT =        -748
663396  meter/sec
 ZDOT =     -13123
958632                 ZDOT =       -4000
182591


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10050
33569496  
00016717  00000-0  10270-3 0  9132
2 25544  51
6446 115
6111 0013139 350
8429   9
2493 15
75217294  4916


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
33569496   =   yrday
fracday
Element set:     913
Inclination:       51
6446  deg
RA of node:       115
6111  deg
Eccentricity:     
0013139     
Arg of perigee:   350
8429  deg
Mean anomaly:       9
2493  deg
Mean motion:   15
75217294  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             491
Checksum:              302


Coasting Arc #15 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2010/051/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -499324
20                 A    =         6724325
62  meter
 Y    =       -5920555
66  meter          E    =           
0016929
 Z    =        3152488
14                 I    =           51
96711
 XDOT =       5131
279004                 Wp   =           44
39670
 YDOT =      -3038
620711  meter/sec      RA   =          109
70020  deg
 ZDOT =      -4866
499296                 TA   =           99
08719
                                          MA   =           98
89559
                                          Ha   =            191
309  n
mi
                                          Hp   =            180
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1638202
75                 X    =         -448396
46
 Y    =      -19424395
22  feet           Y    =        -5925854
53  meter
 Z    =       10342808
84                 Z    =         3150186
36
 XDOT =      16834
904868                 XDOT =        5188
516395
 YDOT =      -9969
228054  feet/sec       YDOT =       -2980
919853  meter/sec
 ZDOT =     -15966
205041                 ZDOT =       -4841
432628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19468965
49                 X    =         5934140
68
 Y    =        1069359
33  feet           Y    =          325940
73  meter
 Z    =       10333459
54                 Z    =         3149638
47
 XDOT =       7549
379602                 XDOT =        2301
050903
 YDOT =      16750
133202  feet/sec       YDOT =        5105
440600  meter/sec
 ZDOT =     -15866
776262                 ZDOT =       -4836
193405


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10051
35072853  
00016717  00000-0  10270-3 0  9142
2 25544  51
6449 110
3891 0013101 354
9924   5
1106 15
75244650  5070


Satellite: ISS
Catalog Number: 25544
Epoch time:      10051
35072853   =   yrday
fracday
Element set:     914
Inclination:       51
6449  deg
RA of node:       110
3891  deg
Eccentricity:     
0013101     
Arg of perigee:   354
9924  deg
Mean anomaly:       5
1106  deg
Mean motion:   15
75244650  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              276


Coasting Arc #16 (Orbit 522)
---------------------------------------

Vector Time (GMT): 2010/052/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4293648
12                 A    =         6719689
73  meter
 Y    =        2537732
67  meter          E    =           
0012571
 Z    =        4491248
24                 I    =           51
96232
 XDOT =       -772
313839                 Wp   =           39
37051
 YDOT =      -6970
711934  meter/sec      RA   =          104
62608  deg
 ZDOT =       3205
055716                 TA   =           18
80016
                                          MA   =           18
75378
                                          Ha   =            191
460  n
mi
                                          Hp   =            180
015

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14086772
03                 X    =        -4343523
85
 Y    =        8325894
60  feet           Y    =         2489439
77  meter
 Z    =       14735066
42                 Z    =         4470268
70
 XDOT =      -2533
838055                 XDOT =        -709
878135
 YDOT =     -22869
789811  feet/sec       YDOT =       -6978
999247  meter/sec
 ZDOT =      10515
274658                 ZDOT =        3201
455641

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6495564
90                 X    =        -1979848
18
 Y    =      -15100035
56  feet           Y    =        -4602490
84  meter
 Z    =       14651839
89                 Z    =         4465880
80
 XDOT =      21913
621938                 XDOT =        6679
271967
 YDOT =        747
577750  feet/sec       YDOT =         227
861698  meter/sec
 ZDOT =      10500
743612                 ZDOT =        3200
626653


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10052
36573680  
00016717  00000-0  10270-3 0  9159
2 25544  51
6459 105
1671 0013166 358
6749   1
4378 15
75325918  5231


Satellite: ISS
Catalog Number: 25544
Epoch time:      10052
36573680   =   yrday
fracday
Element set:     915
Inclination:       51
6459  deg
RA of node:       105
1671  deg
Eccentricity:     
0013166     
Arg of perigee:   358
6749  deg
Mean anomaly:       1
4378  deg
Mean motion:   15
75325918  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             523
Checksum:              314


Coasting Arc #17 (Orbit 537)
---------------------------------------

Vector Time (GMT): 2010/053/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         878195
81                 A    =         6725934
91  meter
 Y    =        6206619
67  meter          E    =           
0017753
 Z    =       -2413679
95                 I    =           51
98994
 XDOT =      -4746
023867                 Wp   =           15
08970
 YDOT =       2764
837876  meter/sec      RA   =           99
46085  deg
 ZDOT =       5408
359657                 TA   =          317
77684
                                          MA   =          317
91342
                                          Ha   =            191
604  n
mi
                                          Hp   =            179
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2881219
84                 X    =          820452
10
 Y    =       20362925
42  feet           Y    =         6216117
30  meter
 Z    =       -7918897
49                 Z    =        -2409554
01
 XDOT =     -15570
944445                 XDOT =       -4802
860561
 YDOT =       9070
990406  feet/sec       YDOT =        2711
447249  meter/sec
 ZDOT =      17743
962129                 ZDOT =        5385
165685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20559467
62                 X    =        -6266525
73
 Y    =         721695
61  feet           Y    =          219972
82  meter
 Z    =       -7902312
54                 Z    =        -2408624
86
 XDOT =      -7281
117542                 XDOT =       -2219
284627
 YDOT =     -15060
086795  feet/sec       YDOT =       -4590
314455  meter/sec
 ZDOT =      17651
938122                 ZDOT =        5380
310739


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10053
31728834  
00016717  00000-0  10270-3 0  9169
2 25544  51
6463 100
2722 0013383   2
3814 357
7412 15
75303568  5385


Satellite: ISS
Catalog Number: 25544
Epoch time:      10053
31728834   =   yrday
fracday
Element set:     916
Inclination:       51
6463  deg
RA of node:       100
2722  deg
Eccentricity:     
0013383     
Arg of perigee:     2
3814  deg
Mean anomaly:     357
7412  deg
Mean motion:   15
75303568  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             538
Checksum:              288


Coasting Arc #18 (Orbit 553)
---------------------------------------

Vector Time (GMT): 2010/054/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4025309
92                 A    =         6717955
52  meter
 Y    =       -2224395
48  meter          E    =           
0021335
 Z    =       -4914021
18                 I    =           51
96759
 XDOT =       1223
145073                 Wp   =           38
50759
 YDOT =       7244
420435  meter/sec      RA   =           94
37869  deg
 ZDOT =      -2266
275764                 TA   =          209
45600
                                          MA   =          209
57639
                                          Ha   =            191
588  n
mi
                                          Hp   =            179
631

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13206397
39                 X    =         4073755
38
 Y    =       -7297885
44  feet           Y    =        -2179111
17  meter
 Z    =      -16122116
74                 Z    =        -4894348
88
 XDOT =       4012
943154                 XDOT =        1153
054752
 YDOT =      23767
783579  feet/sec       YDOT =        7257
706489  meter/sec
 ZDOT =      -7435
287938                 ZDOT =       -2260
504016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6066193
26                 X    =         1848975
70
 Y    =       13906128
48  feet           Y    =         4238587
96  meter
 Z    =      -16044051
93                 Z    =        -4890227
03
 XDOT =     -23022
925974                 XDOT =       -7017
387837
 YDOT =       1449
381124  feet/sec       YDOT =         441
771366  meter/sec
 ZDOT =      -7412
141218                 ZDOT =       -2259
220643


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10054
33225277  
00016717  00000-0  10270-3 0  9176
2 25544  51
6467  95
0505 0013254   6
1858 353
9467 15
75352304  5544


Satellite: ISS
Catalog Number: 25544
Epoch time:      10054
33225277   =   yrday
fracday
Element set:     917
Inclination:       51
6467  deg
RA of node:        95
0505  deg
Eccentricity:     
0013254     
Arg of perigee:     6
1858  deg
Mean anomaly:     353
9467  deg
Mean motion:   15
75352304  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             554
Checksum:              304


Coasting Arc #19 (Orbit 569)
---------------------------------------

Vector Time (GMT): 2010/055/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1269400
84                 A    =         6727224
39  meter
 Y    =       -6432032
87  meter          E    =           
0016172
 Z    =        1513290
21                 I    =           52
00013
 XDOT =       4508
628346                 Wp   =           66
68520
 YDOT =      -2269
576367  meter/sec      RA   =           89
22518  deg
 ZDOT =      -5809
562200                 TA   =           96
73132
                                          MA   =           96
54726
                                          Ha   =            191
650  n
mi
                                          Hp   =            179
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4164700
91                 X    =        -1204733
49
 Y    =      -21102470
06  feet           Y    =        -6445866
50  meter
 Z    =        4964862
91                 Z    =         1507280
62
 XDOT =      14792
087750                 XDOT =        4561
893271
 YDOT =      -7446
116689  feet/sec       YDOT =       -2218
860347  meter/sec
 ZDOT =     -19060
243437                 ZDOT =       -5787
530384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21352835
19                 X    =         6508344
16
 Y    =       -2636998
11  feet           Y    =         -803757
02  meter
 Z    =        4940800
59                 Z    =         1505956
02
 XDOT =       6142
708287                 XDOT =        1872
297486
 YDOT =      13852
146518  feet/sec       YDOT =        4222
134259  meter/sec
 ZDOT =     -18972
798866                 ZDOT =       -5782
909094


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10055
34719378  
00016717  00000-0  10270-3 0  9189
2 25544  51
6464  89
8285 0013258  10
7221 349
4223 15
75393811  5702


Satellite: ISS
Catalog Number: 25544
Epoch time:      10055
34719378   =   yrday
fracday
Element set:     918
Inclination:       51
6464  deg
RA of node:        89
8285  deg
Eccentricity:     
0013258     
Arg of perigee:    10
7221  deg
Mean anomaly:     349
4223  deg
Mean motion:   15
75393811  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             570
Checksum:              315


Coasting Arc #20 (Orbit 585)
---------------------------------------

Vector Time (GMT): 2010/056/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3898075
17                 A    =         6716347
89  meter
 Y    =        1726516
03  meter          E    =           
0012482
 Z    =        5182377
12                 I    =           51
96320
 XDOT =      -1706
273144                 Wp   =           31
39194
 YDOT =      -7422
957546  meter/sec      RA   =           84
12693  deg
 ZDOT =       1198
693312                 TA   =           47
27623
                                          MA   =           47
17121
                                          Ha   =            191
771  n
mi
                                          Hp   =            178
878

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12788960
53                 X    =        -3942266
06
 Y    =        5664422
69  feet           Y    =         1682678
39  meter
 Z    =       17002549
62                 Z    =         5163333
42
 XDOT =      -5598
009004                 XDOT =       -1628
964385
 YDOT =     -24353
535255  feet/sec       YDOT =       -7441
605841  meter/sec
 ZDOT =       3932
720839                 ZDOT =        1190
592273

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4933181
44                 X    =        -1503633
70
 Y    =      -13186050
71  feet           Y    =        -4019108
26  meter
 Z    =       16926951
20                 Z    =         5159334
73
 XDOT =      23668
779976                 XDOT =        7214
244137
 YDOT =      -3886
841522  feet/sec       YDOT =       -1184
709296  meter/sec
 ZDOT =       3900
322972                 ZDOT =        1188
818442


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10056
36210893  
00016717  00000-0  10270-3 0  9191
2 25544  51
6470  84
6057 0013314  14
2502 345
9035 15
75474021  5865


Satellite: ISS
Catalog Number: 25544
Epoch time:      10056
36210893   =   yrday
fracday
Element set:     919
Inclination:       51
6470  deg
RA of node:        84
6057  deg
Eccentricity:     
0013314     
Arg of perigee:    14
2502  deg
Mean anomaly:     345
9035  deg
Mean motion:   15
75474021  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             586
Checksum:              290


Coasting Arc #21 (Orbit 600)
---------------------------------------

Vector Time (GMT): 2010/057/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1710608
48                 A    =         6727940
79  meter
 Y    =        6468081
98  meter          E    =           
0024091
 Z    =        -568014
59                 I    =           51
99742
 XDOT =      -4478
724968                 Wp   =           28
07813
 YDOT =       1704
342748  meter/sec      RA   =           78
98980  deg
 ZDOT =       6043
051390                 TA   =          325
75894
                                          MA   =          325
91404
                                          Ha   =            191
899  n
mi
                                          Hp   =            178
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5612232
55                 X    =         1640913
33
 Y    =       21220741
40  feet           Y    =         6486821
31  meter
 Z    =       -1863564
92                 Z    =         -559874
18
 XDOT =     -14693
979553                 XDOT =       -4526
805558
 YDOT =       5591
675682  feet/sec       YDOT =        1653
990344  meter/sec
 ZDOT =      19826
284087                 ZDOT =        6021
177545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21423336
83                 X    =        -6529833
07
 Y    =        4793519
87  feet           Y    =         1461064
86  meter
 Z    =       -1831037
97                 Z    =         -558100
37
 XDOT =      -4662
355037                 XDOT =       -1421
085815
 YDOT =     -13454
338200  feet/sec       YDOT =       -4100
882283  meter/sec
 ZDOT =      19739
437152                 ZDOT =        6016
580444


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10057
31357247  
00016717  00000-0  10270-3 0  9204
2 25544  51
6468  79
7104 0013544  17
9048 342
2591 15
75443780  6013


Satellite: ISS
Catalog Number: 25544
Epoch time:      10057
31357247   =   yrday
fracday
Element set:     920
Inclination:       51
6468  deg
RA of node:        79
7104  deg
Eccentricity:     
0013544     
Arg of perigee:    17
9048  deg
Mean anomaly:     342
2591  deg
Mean motion:   15
75443780  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             601
Checksum:              301


Coasting Arc #22 (Orbit 616)
---------------------------------------

Vector Time (GMT): 2010/058/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3965740
61                 A    =         6715840
69  meter
 Y    =       -1216102
64  meter          E    =           
0023623
 Z    =       -5298846
39                 I    =           51
94925
 XDOT =       2175
029836                 Wp   =           57
69039
 YDOT =       7374
346666  meter/sec      RA   =           73
87276  deg
 ZDOT =        -52
450661                 TA   =          211
74189
                                          MA   =          211
88452
                                          Ha   =            191
868  n
mi
                                          Hp   =            178
531

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13010960
00                 X    =         4004784
62
 Y    =       -3989838
07  feet           Y    =        -1171537
41  meter
 Z    =      -17384666
65                 Z    =        -5279486
49
 XDOT =       7135
924660                 XDOT =        2092
661717
 YDOT =      24194
050742  feet/sec       YDOT =        7398
208593  meter/sec
 ZDOT =       -172
082222                 ZDOT =         -42
085213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3704773
96                 X    =         1129215
10
 Y    =       13196422
77  feet           Y    =         4022269
66  meter
 Z    =      -17307790
11                 Z    =        -5275414
43
 XDOT =     -23380
907613                 XDOT =       -7126
500641
 YDOT =       6340
015213  feet/sec       YDOT =        1932
436637  meter/sec
 ZDOT =       -130
688790                 ZDOT =         -39
833943


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


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   10058
32844198  
00016717  00000-0  10270-3 0  9213
2 25544  51
6459  74
4877 0013427  21
5646 338
6081 15
75497316  6171


Satellite: ISS
Catalog Number: 25544
Epoch time:      10058
32844198   =   yrday
fracday
Element set:     921
Inclination:       51
6459  deg
RA of node:        74
4877  deg
Eccentricity:     
0013427     
Arg of perigee:    21
5646  deg
Mean anomaly:     338
6081  deg
Mean motion:   15
75497316  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             617
Checksum:              328

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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