Date: February 13th 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


046/05:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 6
000/00:00:00 000 0 0 0 0 181 0

046/05:56:31 000 -0 1 0 2 0 3
N/A 0 2 0 1 188 6
000/00:04:58 000 -0 2 0 2 181 3

046/07:41:31 000 -0 2 0 4 0 4
N/A 0 4 -0 1 188 6
000/00:04:58 000 -0 0 0 1 181 6

046/07:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 6
000/00:00:00 000 0 0 0 0 181 6

049/06:36:31 000 0 3 0 7 0 8
N/A -0 7 0 0 189 2
000/00:04:58 000 0 1 -0 3 180 8

049/07:03:31 000 0 9 1 8 2 0
N/A 1 6 -0 8 189 3
000/00:24:58 000 -0 7 0 1 182 0

049/07:27:01 000 -0 3 0 3 0 4
N/A 0 2 0 2 189 4
000/00:05:58 000 -0 0 -0 1 182 1

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 426)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4166803
03                 A    =         6725866
78  meter
 Y    =       -5181503
27  meter          E    =           
0005873
 Z    =        1019368
34                 I    =           51
89593
 XDOT =       4318
530681                 Wp   =           65
75570
 YDOT =       2297
957412  meter/sec      RA   =          135
71040  deg
 ZDOT =      -5942
872326                 TA   =          103
14093
                                          MA   =          103
07538
                                          Ha   =            188
586  n
mi
                                          Hp   =            181
028

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13670613
63                 X    =         4219482
06
 Y    =      -16999682
64  feet           Y    =        -5134613
01  meter
 Z    =        3344384
32                 Z    =         1039738
38
 XDOT =      14168
407745                 XDOT =        4321
382195
 YDOT =       7539
230355  feet/sec       YDOT =        2346
265399  meter/sec
 ZDOT =     -19497
612619                 ZDOT =       -5921
886658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4940107
19                 X    =         1505744
67
 Y    =       21234976
30  feet           Y    =         6472420
78  meter
 Z    =        3425042
46                 Z    =         1043952
94
 XDOT =     -13201
491561                 XDOT =       -4023
814628
 YDOT =       6217
575085  feet/sec       YDOT =        1895
116886  meter/sec
 ZDOT =     -19414
206446                 ZDOT =       -5917
450125


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
27678718  
00016717  00000-0  10270-3 0  9037
2 25544  51
6434 136
5078 0011807 328
9224  31
1241 15
76050887  4274


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
27678718   =   yrday
fracday
Element set:     903
Inclination:       51
6434  deg
RA of node:       136
5078  deg
Eccentricity:     
0011807     
Arg of perigee:   328
9224  deg
Mean anomaly:      31
1241  deg
Mean motion:   15
76050887  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             427
Checksum:              305


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

Vector Time (GMT): 2010/046/05:59:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010305
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5581642
45                 A    =         6724538
62  meter
 Y    =       -3058875
32  meter          E    =           
0005418
 Z    =       -2177907
16                 I    =           51
89064
 XDOT =        754
056179                 Wp   =          340
41725
 YDOT =       5311
278791  meter/sec      RA   =          135
70764  deg
 ZDOT =      -5518
241997                 TA   =          223
87912
                                          MA   =          223
92216
                                          Ha   =            188
595  n
mi
                                          Hp   =            181
308

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18312475
21                 X    =         5626012
10
 Y    =      -10035680
18  feet           Y    =        -2996210
12  meter
 Z    =       -7145364
68                 Z    =        -2150684
31
 XDOT =       2473
937596                 XDOT =         721
414395
 YDOT =      17425
455352  feet/sec       YDOT =        5319
528279  meter/sec
 ZDOT =     -18104
468493                 ZDOT =       -5514
658467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2626726
97                 X    =         -800626
38
 Y    =       20753143
40  feet           Y    =         6325558
11  meter
 Z    =       -7037414
73                 Z    =        -2145004
01
 XDOT =     -14117
077533                 XDOT =       -4302
885232
 YDOT =      -7931
235630  feet/sec       YDOT =       -2417
440620  meter/sec
 ZDOT =     -18090
026067                 ZDOT =       -5513
839945


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
27678897  
00016717  00000-0  10270-3 0  9046
2 25544  51
6433 136
5078 0011514 328
5446  31
5029 15
75980732  4278


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
27678897   =   yrday
fracday
Element set:     904
Inclination:       51
6433  deg
RA of node:       136
5078  deg
Eccentricity:     
0011514     
Arg of perigee:   328
5446  deg
Mean anomaly:      31
5029  deg
Mean motion:   15
75980732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             427
Checksum:              318


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

Vector Time (GMT): 2010/046/07:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010226
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3835964
99                 A    =         6715214
64  meter
 Y    =        1921406
34  meter          E    =           
0014174
 Z    =       -5174933
96                 I    =           51
86092
 XDOT =      -4676
724206                 Wp   =           34
40635
 YDOT =       5986
826189  meter/sec      RA   =          135
32346  deg
 ZDOT =      -1233
994371                 TA   =          223
77520
                                          MA   =          223
88765
                                          Ha   =            188
592  n
mi
                                          Hp   =            181
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12585186
96                 X    =         3839332
63
 Y    =        6303826
56  feet           Y    =         1964320
91  meter
 Z    =      -16978129
78                 Z    =        -5156291
25
 XDOT =     -15343
583353                 XDOT =       -4737
328009
 YDOT =      19641
818204  feet/sec       YDOT =        5934
189360  meter/sec
 ZDOT =      -4048
537962                 ZDOT =       -1256
860845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8322788
77                 X    =        -2536786
02
 Y    =       11461529
62  feet           Y    =         3493474
23  meter
 Z    =      -16904040
25                 Z    =        -5152351
47
 XDOT =     -15988
540023                 XDOT =       -4873
306999
 YDOT =     -17762
286484  feet/sec       YDOT =       -5413
944920  meter/sec
 ZDOT =      -4139
074655                 ZDOT =       -1261
589955


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
34020130  
00016717  00000-0  10270-3 0  9056
2 25544  51
6442 136
1802 0011147 326
9879  33
0588 15
75902100  4284


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
34020130   =   yrday
fracday
Element set:     905
Inclination:       51
6442  deg
RA of node:       136
1802  deg
Eccentricity:     
0011147     
Arg of perigee:   326
9879  deg
Mean anomaly:      33
0588  deg
Mean motion:   15
75902100  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             428
Checksum:              274


Coasting Arc #7 (Orbit 443)
---------------------------------------

Vector Time (GMT): 2010/047/07:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4513207
79                 A    =         6726598
38  meter
 Y    =       -4980006
91  meter          E    =           
0002732
 Z    =        -300793
52                 I    =           51
91969
 XDOT =       3340
455819                 Wp   =           61
88830
 YDOT =       3390
262790  meter/sec      RA   =          130
17527  deg
 ZDOT =      -6048
802826                 TA   =          121
36791
                                          MA   =          121
34117
                                          Ha   =            188
685  n
mi
                                          Hp   =            181
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14807112
17                 X    =         4570020
85
 Y    =      -16338605
33  feet           Y    =        -4929219
90  meter
 Z    =        -986855
37                 Z    =         -278730
51
 XDOT =      10959
500720                 XDOT =        3331
680380
 YDOT =      11122
909415  feet/sec       YDOT =        3427
568277  meter/sec
 ZDOT =     -19845
153628                 ZDOT =       -6032
596791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14096178
70                 X    =         4296515
27
 Y    =       16960636
60  feet           Y    =         5169602
04  meter
 Z    =        -899461
49                 Z    =         -274155
86
 XDOT =     -11331
058016                 XDOT =       -3453
706483
 YDOT =       8376
023336  feet/sec       YDOT =        2553
011913  meter/sec
 ZDOT =     -19780
676320                 ZDOT =       -6029
150142


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
35480652  
00016717  00000-0  10270-3 0  9068
2 25544  51
6434 130
9542 0011326 330
6971  29
3556 15
75948081  4441


Satellite: ISS
Catalog Number: 25544
Epoch time:      10047
35480652   =   yrday
fracday
Element set:     906
Inclination:       51
6434  deg
RA of node:       130
9542  deg
Eccentricity:     
0011326     
Arg of perigee:   330
6971  deg
Mean anomaly:      29
3556  deg
Mean motion:   15
75948081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             444
Checksum:              303


Coasting Arc #8 (Orbit 459)
---------------------------------------

Vector Time (GMT): 2010/048/07:46:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2631222
30                 A    =         6715000
39  meter
 Y    =       -3345599
33  meter          E    =           
0012316
 Z    =        5196981
88                 I    =           51
89955
 XDOT =       5054
818308                 Wp   =          352
78488
 YDOT =      -5705
259865  meter/sec      RA   =          125
03225  deg
 ZDOT =      -1101
881739                 TA   =          107
75749
                                          MA   =          107
62305
                                          Ha   =            188
907  n
mi
                                          Hp   =            181
010

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8632619
09                 X    =        -2618861
21
 Y    =      -10976375
74  feet           Y    =        -3374953
74  meter
 Z    =       17050465
49                 Z    =         5184229
89
 XDOT =      16584
049568                 XDOT =        5123
592501
 YDOT =     -18718
044176  feet/sec       YDOT =       -5648
349427  meter/sec
 ZDOT =      -3615
097568                 ZDOT =       -1077
158415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11969715
73                 X    =         3648369
36
 Y    =       -7311449
04  feet           Y    =        -2228529
67  meter
 Z    =       16999703
78                 Z    =         5181509
71
 XDOT =      15992
812594                 XDOT =        4874
609279
 YDOT =      17915
092912  feet/sec       YDOT =        5460
520319  meter/sec
 ZDOT =      -3517
162746                 ZDOT =       -1072
031205


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
36939010  
00016717  00000-0  10270-3 0  9078
2 25544  51
6440 125
7292 0011180 335
1466  24
9159 15
75924978  4606


Satellite: ISS
Catalog Number: 25544
Epoch time:      10048
36939010   =   yrday
fracday
Element set:     907
Inclination:       51
6440  deg
RA of node:       125
7292  deg
Eccentricity:     
0011180     
Arg of perigee:   335
1466  deg
Mean anomaly:      24
9159  deg
Mean motion:   15
75924978  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             460
Checksum:              308


Coasting Arc #9 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/06:39:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010305
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1924130
15                 A    =         6716802
76  meter
 Y    =       -4242656
44  meter          E    =           
0014248
 Z    =        4841800
29                 I    =           51
91906
 XDOT =       5188
798634                 Wp   =           10
15382
 YDOT =      -5144
827810  meter/sec      RA   =          120
13080  deg
 ZDOT =      -2431
353200                 TA   =          103
57252
                                          MA   =          103
41377
                                          Ha   =            189
248  n
mi
                                          Hp   =            180
793

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6312762
96                 X    =        -1900065
28
 Y    =      -13919476
49  feet           Y    =        -4264038
33  meter
 Z    =       15885171
54                 Z    =         4832511
72
 XDOT =      17023
617566                 XDOT =        5257
754283
 YDOT =     -16879
356333  feet/sec       YDOT =       -5086
418193  meter/sec
 ZDOT =      -7976
880576                 ZDOT =       -2405
978535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15314793
25                 X    =         4667948
98
 Y    =        -485187
40  feet           Y    =         -147885
12  meter
 Z    =       15848128
53                 Z    =         4830509
57
 XDOT =       8871
883129                 XDOT =        2704
149978
 YDOT =      21176
072990  feet/sec       YDOT =        6454
467047  meter/sec
 ZDOT =      -7876
328541                 ZDOT =       -2400
704939


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
32054241  
00016717  00000-0  10270-3 0  9080
2 25544  51
6427 120
8305 0011015 341
6488  18
4277 15
75832015  4750


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32054241   =   yrday
fracday
Element set:     908
Inclination:       51
6427  deg
RA of node:       120
8305  deg
Eccentricity:     
0011015     
Arg of perigee:   341
6488  deg
Mean anomaly:      18
4277  deg
Mean motion:   15
75832015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              284


Coasting Arc #10 (Orbit 474)
---------------------------------------

Vector Time (GMT): 2010/049/07:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1009908
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4151662
50                 A    =         6716353
31  meter
 Y    =         962764
40  meter          E    =           
0015032
 Z    =       -5201271
72                 I    =           51
91428
 XDOT =      -3028
217500                 Wp   =           41
46687
 YDOT =       6985
268811  meter/sec      RA   =          120
02775  deg
 ZDOT =      -1114
951224                 TA   =          217
87175
                                          MA   =          217
97759
                                          Ha   =            189
284  n
mi
                                          Hp   =            181
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13620939
95                 X    =         4165854
63
 Y    =        3158675
84  feet           Y    =         1009269
76  meter
 Z    =      -17064539
77                 Z    =        -5181068
81
 XDOT =      -9935
096785                 XDOT =       -3100
686794
 YDOT =      22917
548591  feet/sec       YDOT =        6951
000215  meter/sec
 ZDOT =      -3657
976457                 ZDOT =       -1129
838585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6301245
93                 X    =        -1920619
76
 Y    =       12591029
90  feet           Y    =         3837745
91  meter
 Z    =      -16984287
49                 Z    =        -5176810
83
 XDOT =     -19019
526539                 XDOT =       -5797
151689
 YDOT =     -14572
977172  feet/sec       YDOT =       -4441
843442  meter/sec
 ZDOT =      -3716
818408                 ZDOT =       -1132
886251


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
32054663  
00016717  00000-0  10270-3 0  9099
2 25544  51
6426 120
8308 0010085 334
7487  25
3183 15
75466408  4752


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32054663   =   yrday
fracday
Element set:     909
Inclination:       51
6426  deg
RA of node:       120
8308  deg
Eccentricity:     
0010085     
Arg of perigee:   334
7487  deg
Mean anomaly:      25
3183  deg
Mean motion:   15
75466408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              305


Coasting Arc #11 (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    =         208503
84                 A    =         6722051
74  meter
 Y    =        5556495
61  meter          E    =           
0007828
 Z    =       -3771951
97                 I    =           51
93304
 XDOT =      -5627
846234                 Wp   =            9
87405
 YDOT =       3093
743900  meter/sec      RA   =          119
94233  deg
 ZDOT =       4255
162185                 TA   =          304
64198
                                          MA   =          304
71575
                                          Ha   =            189
406  n
mi
                                          Hp   =            182
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         684067
71                 X    =          164677
84
 Y    =       18229972
47  feet           Y    =         5558581
93  meter
 Z    =      -12375170
51                 Z    =        -3771045
89
 XDOT =     -18464
062448                 XDOT =       -5682
693284
 YDOT =      10150
078413  feet/sec       YDOT =        3030
503595  meter/sec
 ZDOT =      13960
505857                 ZDOT =        4227
689058

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18079304
17                 X    =        -5510571
91
 Y    =       -2456198
04  feet           Y    =         -748649
16  meter
 Z    =      -12371359
75                 Z    =        -3770790
45
 XDOT =      -6915
068472                 XDOT =       -2107
712870
 YDOT =     -18721
671907  feet/sec       YDOT =       -5706
365597  meter/sec
 ZDOT =      13851
542823                 ZDOT =        4221
950253


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
32054673  
00016717  00000-0  10270-3 0  9102
2 25544  51
6427 120
8306 0010299 333
2638  26
7993 15
75378665  4751


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
32054673   =   yrday
fracday
Element set:     910
Inclination:       51
6427  deg
RA of node:       120
8306  deg
Eccentricity:     
0010299     
Arg of perigee:   333
2638  deg
Mean anomaly:      26
7993  deg
Mean motion:   15
75378665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             475
Checksum:              317


Coasting Arc #12 (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    =        4700124
93                 A    =         6721116
49  meter
 Y    =       -2605755
18  meter          E    =           
0012130
 Z    =       -4047315
63                 I    =           51
94411
 XDOT =        300
387697                 Wp   =           13
67040
 YDOT =       6621
806350  meter/sec      RA   =          114
86874  deg
 ZDOT =      -3905
273479                 TA   =          216
14873
                                          MA   =          216
23078
                                          Ha   =            189
481  n
mi
                                          Hp   =            181
914

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15420357
38                 X    =         4748574
55
 Y    =       -8549065
55  feet           Y    =        -2552924
91  meter
 Z    =      -13278594
57                 Z    =        -4024364
84
 XDOT =        985
523941                 XDOT =         245
290073
 YDOT =      21725
086451  feet/sec       YDOT =        6624
857189  meter/sec
 ZDOT =     -12812
577032                 ZDOT =       -3903
948395

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5982419
81                 X    =         1823441
56
 Y    =       16658148
11  feet           Y    =         5077403
55  meter
 Z    =      -13187561
27                 Z    =        -4019568
67
 XDOT =     -20403
219064                 XDOT =       -6218
901171
 YDOT =      -2835
396199  feet/sec       YDOT =        -864
228761  meter/sec
 ZDOT =     -12807
070799                 ZDOT =       -3903
595180


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
33547193  
00016717  00000-0  10270-3 0  9110
2 25544  51
6427 115
6077 0010315 337
0970  22
9732 15
75419868  4916


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
33547193   =   yrday
fracday
Element set:     911
Inclination:       51
6427  deg
RA of node:       115
6077  deg
Eccentricity:     
0010315     
Arg of perigee:   337
0970  deg
Mean anomaly:      22
9732  deg
Mean motion:   15
75419868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             491
Checksum:              300


Coasting Arc #13 (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    =        -349745
39                 A    =         6724128
38  meter
 Y    =       -6004535
01  meter          E    =           
0012837
 Z    =        3007867
51                 I    =           51
96643
 XDOT =       5148
591205                 Wp   =           50
32109
 YDOT =      -2808
943403  meter/sec      RA   =          109
69449  deg
 ZDOT =      -4986
754880                 TA   =           95
07782
                                          MA   =           94
93129
                                          Ha   =            189
572  n
mi
                                          Hp   =            181
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1147458
63                 X    =         -297187
17
 Y    =      -19699918
01  feet           Y    =        -6008152
09  meter
 Z    =        9868331
71                 Z    =         3006296
34
 XDOT =      16891
703427                 XDOT =        5203
843191
 YDOT =      -9215
693581  feet/sec       YDOT =       -2751
060056  meter/sec
 ZDOT =     -16360
744356                 ZDOT =       -4961
608940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19671820
37                 X    =         5995970
85
 Y    =        1596933
35  feet           Y    =          486745
29  meter
 Z    =        9861880
60                 Z    =         3005901
21
 XDOT =       6833
549223                 XDOT =        2082
865803
 YDOT =      16687
133596  feet/sec       YDOT =        5086
238320  meter/sec
 ZDOT =     -16260
992681                 ZDOT =       -4956
350569


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
35037396  
00016717  00000-0  10270-3 0  9123
2 25544  51
6429 110
3845 0010263 341
2887  18
7898 15
75448289  5072


Satellite: ISS
Catalog Number: 25544
Epoch time:      10051
35037396   =   yrday
fracday
Element set:     912
Inclination:       51
6429  deg
RA of node:       110
3845  deg
Eccentricity:     
0010263     
Arg of perigee:   341
2887  deg
Mean anomaly:      18
7898  deg
Mean motion:   15
75448289  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              319


Coasting Arc #14 (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    =       -4321531
69                 A    =         6718616
16  meter
 Y    =        2252118
49  meter          E    =           
0008021
 Z    =        4617988
16                 I    =           51
95868
 XDOT =       -541
232779                 Wp   =           37
19459
 YDOT =      -7097
216501  meter/sec      RA   =          104
61685  deg
 ZDOT =       2958
315061                 TA   =           23
65965
                                          MA   =           23
62278
                                          Ha   =            189
739  n
mi
                                          Hp   =            181
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14178253
59                 X    =        -4368827
24
 Y    =        7388840
19  feet           Y    =         2203528
20  meter
 Z    =       15150879
78                 Z    =         4596879
43
 XDOT =      -1775
698093                 XDOT =        -476
201042
 YDOT =     -23284
831039  feet/sec       YDOT =       -7102
905218  meter/sec
 ZDOT =       9705
758075                 ZDOT =        2955
843876

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5554119
49                 X    =        -1692895
62
 Y    =      -15076482
46  feet           Y    =        -4595311
85  meter
 Z    =       15067130
63                 Z    =         4592461
42
 XDOT =      22232
119497                 XDOT =        6776
350023
 YDOT =       1487
577769  feet/sec       YDOT =         453
413704  meter/sec
 ZDOT =       9695
705725                 ZDOT =        2955
251105


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
36525045  
00016717  00000-0  10270-3 0  9139
2 25544  51
6440 105
1614 0010348 345
0212  15
0644 15
75529714  5239


Satellite: ISS
Catalog Number: 25544
Epoch time:      10052
36525045   =   yrday
fracday
Element set:     913
Inclination:       51
6440  deg
RA of node:       105
1614  deg
Eccentricity:     
0010348     
Arg of perigee:   345
0212  deg
Mean anomaly:      15
0644  deg
Mean motion:   15
75529714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             523
Checksum:              262


Coasting Arc #15 (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    =         626815
18                 A    =         6725918
98  meter
 Y    =        6341726
27  meter          E    =           
0015307
 Z    =       -2123739
41                 I    =           51
98992
 XDOT =      -4797
373369                 Wp   =            8
42283
 YDOT =       2331
143015  meter/sec      RA   =           99
45290  deg
 ZDOT =       5564
921959                 TA   =          327
91932
                                          MA   =          328
01239
                                          Ha   =            189
892  n
mi
                                          Hp   =            180
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2056480
26                 X    =          566170
91
 Y    =       20806188
54  feet           Y    =         6348396
60  meter
 Z    =       -6967648
98                 Z    =        -2120841
70
 XDOT =     -15739
413939                 XDOT =       -4850
117135
 YDOT =       7648
107003  feet/sec       YDOT =        2277
201053  meter/sec
 ZDOT =      18257
617975                 ZDOT =        5541
488477

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20910923
39                 X    =        -6373649
45
 Y    =        -151462
17  feet           Y    =          -46165
67  meter
 Z    =       -6955937
54                 Z    =        -2120169
76
 XDOT =      -5911
728707                 XDOT =       -1801
894910
 YDOT =     -15051
987452  feet/sec       YDOT =       -4587
845776  meter/sec
 ZDOT =      18164
628856                 ZDOT =        5536
578875


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
31667819  
00016717  00000-0  10270-3 0  9142
2 25544  51
6443 100
2654 0010542 349
1547  10
9388 15
75510303  5383


Satellite: ISS
Catalog Number: 25544
Epoch time:      10053
31667819   =   yrday
fracday
Element set:     914
Inclination:       51
6443  deg
RA of node:       100
2654  deg
Eccentricity:     
0010542     
Arg of perigee:   349
1547  deg
Mean anomaly:      10
9388  deg
Mean motion:   15
75510303  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             538
Checksum:              289


Coasting Arc #16 (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    =        4090730
24                 A    =         6716800
30  meter
 Y    =       -1756685
25  meter          E    =           
0017803
 Z    =       -5043027
96                 I    =           51
96372
 XDOT =        887
662797                 Wp   =           40
47406
 YDOT =       7412
488006  meter/sec      RA   =           94
36425  deg
 ZDOT =      -1852
415950                 TA   =          211
66796
                                          MA   =          211
77519
                                          Ha   =            189
902  n
mi
                                          Hp   =            180
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13421030
97                 X    =         4134567
50
 Y    =       -5763403
04  feet           Y    =        -1710695
13  meter
 Z    =      -16545367
34                 Z    =        -5023049
05
 XDOT =       2912
279517                 XDOT =         813
707624
 YDOT =      24319
186371  feet/sec       YDOT =        7422
000885  meter/sec
 ZDOT =      -6077
480150                 ZDOT =       -1848
283335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4518377
52                 X    =         1377201
47
 Y    =       13983664
03  feet           Y    =         4262220
80  meter
 Z    =      -16466070
33                 Z    =        -5018858
24
 XDOT =     -23466
247016                 XDOT =       -7152
512091
 YDOT =        408
321621  feet/sec       YDOT =         124
456430  meter/sec
 ZDOT =      -6060
838495                 ZDOT =       -1847
343573


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
33151031  
00016717  00000-0  10270-3 0  9150
2 25544  51
6447  95
0427 0010452 352
7370   7
3641 15
75559221  5542


Satellite: ISS
Catalog Number: 25544
Epoch time:      10054
33151031   =   yrday
fracday
Element set:     915
Inclination:       51
6447  deg
RA of node:        95
0427  deg
Eccentricity:     
0010452     
Arg of perigee:   352
7370  deg
Mean anomaly:       7
3641  deg
Mean motion:   15
75559221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             554
Checksum:              276


Coasting Arc #17 (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    =        -931943
32                 A    =         6727124
74  meter
 Y    =       -6574873
26  meter          E    =           
0011371
 Z    =        1077524
34                 I    =           51
99980
 XDOT =       4616
912091                 Wp   =           75
79714
 YDOT =      -1636
423438  meter/sec      RA   =           89
21572  deg
 ZDOT =      -5937
451003                 TA   =           92
47537
                                          MA   =           92
34519
                                          Ha   =            189
954  n
mi
                                          Hp   =            180
379

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3057556
81                 X    =         -863586
96
 Y    =      -21571106
50  feet           Y    =        -6584912
61  meter
 Z    =        3535184
84                 Z    =         1073163
04
 XDOT =      15147
349380                 XDOT =        4663
710187
 YDOT =      -5368
843299  feet/sec       YDOT =       -1584
532682  meter/sec
 ZDOT =     -19479
826124                 ZDOT =       -5914
908858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21738544
84                 X    =         6625908
47
 Y    =       -1490140
69  feet           Y    =         -454194
88  meter
 Z    =        3517665
44                 Z    =         1072184
43
 XDOT =       4128
454146                 XDOT =        1258
352824
 YDOT =      14028
641013  feet/sec       YDOT =        4275
929781  meter/sec
 ZDOT =     -19390
335612                 ZDOT =       -5910
174295


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
34631887  
00016717  00000-0  10270-3 0  9165
2 25544  51
6445  89
8196 0010404 357
3701   2
7407 15
75599448  5702


Satellite: ISS
Catalog Number: 25544
Epoch time:      10055
34631887   =   yrday
fracday
Element set:     916
Inclination:       51
6445  deg
RA of node:        89
8196  deg
Eccentricity:     
0010404     
Arg of perigee:   357
3701  deg
Mean anomaly:       2
7407  deg
Mean motion:   15
75599448  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             570
Checksum:              321


Coasting Arc #18 (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    =       -4026100
54                 A    =         6715417
72  meter
 Y    =        1084880
97  meter          E    =           
0009690
 Z    =        5260945
17                 I    =           51
96006
 XDOT =      -1260
077549                 Wp   =           16
33076
 YDOT =      -7579
084546  meter/sec      RA   =           84
10695  deg
 ZDOT =        607
431696                 TA   =           67
97739
                                          MA   =           67
87448
                                          Ha   =            190
091  n
mi
                                          Hp   =            180
018

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13208991
29                 X    =        -4063488
71
 Y    =        3559320
75  feet           Y    =         1039649
70  meter
 Z    =       17260318
80                 Z    =         5241296
06
 XDOT =      -4134
112692                 XDOT =       -1178
183944
 YDOT =     -24865
762947  feet/sec       YDOT =       -7592
717586  meter/sec
 ZDOT =       1992
886142                 ZDOT =         601
509356

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2807760
12                 X    =         -855805
29
 Y    =      -13488883
71  feet           Y    =        -4111411
75  meter
 Z    =       17182296
69                 Z    =         5237164
03
 XDOT =      24075
438931                 XDOT =        7338
193786
 YDOT =      -2540
152389  feet/sec       YDOT =        -774
238448  meter/sec
 ZDOT =       1969
138375                 ZDOT =         600
193377


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
36110138  
00016717  00000-0  10270-3 0  9170
2 25544  51
6450  84
5956 0010498    
9056 359
2125 15
75680996  5864


Satellite: ISS
Catalog Number: 25544
Epoch time:      10056
36110138   =   yrday
fracday
Element set:     917
Inclination:       51
6450  deg
RA of node:        84
5956  deg
Eccentricity:     
0010498     
Arg of perigee:      
9056  deg
Mean anomaly:     359
2125  deg
Mean motion:   15
75680996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             586
Checksum:              318


Coasting Arc #19 (Orbit 601)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1264168
20                 A    =         6727470
04  meter
 Y    =        6594331
95  meter          E    =           
0021603
 Z    =          25373
15                 I    =           51
99590
 XDOT =      -4669
419241                 Wp   =           26
79954
 YDOT =        864
208727  meter/sec      RA   =           78
97858  deg
 ZDOT =       6076
921470                 TA   =          333
47524
                                          MA   =          333
58563
                                          Ha   =            190
221  n
mi
                                          Hp   =            179
766

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4147533
47                 X    =         1190212
00
 Y    =       21634947
34  feet           Y    =         6608055
12  meter
 Z    =          83245
23                 Z    =           31334
46
 XDOT =     -15319
616934                 XDOT =       -4708
255661
 YDOT =       2835
330470  feet/sec       YDOT =         811
775555  meter/sec
 ZDOT =      19937
406398                 ZDOT =        6054
143739

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21779865
38                 X    =        -6638502
97
 Y    =        3302408
13  feet           Y    =         1006574
00  meter
 Z    =         107119
11                 Z    =           32649
90
 XDOT =      -1992
474029                 XDOT =        -607
306084
 YDOT =     -13946
945939  feet/sec       YDOT =       -4251
029122  meter/sec
 ZDOT =      19846
944225                 ZDOT =        6049
348600


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
37586323  
00016717  00000-0  10270-3 0  9186
2 25544  51
6448  79
3725 0010675   5
3289 354
7987 15
75659507  6020


Satellite: ISS
Catalog Number: 25544
Epoch time:      10057
37586323   =   yrday
fracday
Element set:     918
Inclination:       51
6448  deg
RA of node:        79
3725  deg
Eccentricity:     
0010675     
Arg of perigee:     5
3289  deg
Mean anomaly:     354
7987  deg
Mean motion:   15
75659507  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             602
Checksum:              340


Coasting Arc #20 (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    =        4169873
53                 A    =         6715384
63  meter
 Y    =        -406067
81  meter          E    =           
0018701
 Z    =       -5261213
81                 I    =           51
94780
 XDOT =       1599
305578                 Wp   =           60
72860
 YDOT =       7491
920239  meter/sec      RA   =           73
84772  deg
 ZDOT =        700
108115                 TA   =          215
84539
                                          MA   =          215
97102
                                          Ha   =            190
241  n
mi
                                          Hp   =            179
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13680687
44                 X    =         4199661
61
 Y    =       -1332243
49  feet           Y    =         -359271
59  meter
 Z    =      -17261200
18                 Z    =        -5240884
79
 XDOT =       5247
065544                 XDOT =        1512
009832
 YDOT =      24579
790812  feet/sec       YDOT =        7509
316572  meter/sec
 ZDOT =       2296
942634                 ZDOT =         707
664801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1033286
40                 X    =          314945
69
 Y    =       13807590
94  feet           Y    =         4208553
72  meter
 Z    =      -17180450
08                 Z    =        -5236601
18
 XDOT =     -23680
747844                 XDOT =       -7217
891943
 YDOT =       4623
559762  feet/sec       YDOT =        1409
261016  meter/sec
 ZDOT =       2327
180962                 ZDOT =         709
324757


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
32717690  
00016717  00000-0  10270-3 0  9196
2 25544  51
6439  74
4755 0010638   8
6191 351
5154 15
75713217  6172


Satellite: ISS
Catalog Number: 25544
Epoch time:      10058
32717690   =   yrday
fracday
Element set:     919
Inclination:       51
6439  deg
RA of node:        74
4755  deg
Eccentricity:     
0010638     
Arg of perigee:     8
6191  deg
Mean anomaly:     351
5154  deg
Mean motion:   15
75713217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             617
Checksum:              312

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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