Date: February 16th 2010

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 26909 78 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


050/05:53:00 000 0 0 0 0 0 0
N/A 0 0 0 0 188 9
000/00:00:00 000 0 0 0 0 179 9

050/06:00:30 000 -0 0 0 6 0 6
N/A 0 6 -0 1 189 0
000/00:05:00 000 -0 1 0 0 180 3

050/06:37:30 000 -1 0 1 8 1 9
N/A -0 8 0 0 190 7
000/00:39:00 000 1 5 -0 6 180 5

050/07:11:31 000 0 3 0 4 0 5
N/A -0 0 -0 0 190 6
000/00:04:58 000 -0 3 -0 0 180 7

050/07:19:00 000 0 0 0 0 0 0
N/A 0 0 0 0 190 6
000/00:00:00 000 0 0 0 0 180 7

Coasting Arc #1 (Orbit 398)
---------------------------------------

Vector Time (GMT): 2010/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5146179
89                 A    =         6726496
63  meter
 Y    =        4265889
00  meter          E    =           
0017065
 Z    =        -641523
72                 I    =           51
85969
 XDOT =      -3496
770675                 Wp   =          359
76082
 YDOT =      -3315
468993  meter/sec      RA   =          144
66523  deg
 ZDOT =       6019
944883                 TA   =          353
26235
                                          MA   =          353
28527
                                          Ha   =            188
271  n
mi
                                          Hp   =            181
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16883792
28                 X    =        -5190383
03
 Y    =       13995698
82  feet           Y    =         4208094
20  meter
 Z    =       -2104736
63                 Z    =         -666630
57
 XDOT =     -11472
344733                 XDOT =       -3488
679527
 YDOT =     -10877
522942  feet/sec       YDOT =       -3354
526562  meter/sec
 ZDOT =      19750
475338                 ZDOT =        6002
977835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21902635
21                 X    =        -6675923
21
 Y    =         887638
51  feet           Y    =          270552
22  meter
 Z    =       -2204226
05                 Z    =         -671848
10
 XDOT =      -2546
380869                 XDOT =        -776
136889
 YDOT =     -14080
159639  feet/sec       YDOT =       -4291
632658  meter/sec
 ZDOT =      19682
989301                 ZDOT =        5999
375139


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
50129195  
00016717  00000-0  10270-3 0  9008
2 25544  51
6469 145
6527 0011323 321
2984  38
7368 15
75930139  3991


Satellite: ISS
Catalog Number: 25544
Epoch time:      10044
50129195   =   yrday
fracday
Element set:     900
Inclination:       51
6469  deg
RA of node:       145
6527  deg
Eccentricity:     
0011323     
Arg of perigee:   321
2984  deg
Mean anomaly:      38
7368  deg
Mean motion:   15
75930139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             399
Checksum:              313


Coasting Arc #2 (Orbit 414)
---------------------------------------

Vector Time (GMT): 2010/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2670246
96                 A    =         6714410
84  meter
 Y    =        3179303
38  meter          E    =           
0012630
 Z    =       -5284161
84                 I    =           51
84326
 XDOT =      -5874
355125                 Wp   =           43
01058
 YDOT =       4975
354715  meter/sec      RA   =          139
53724  deg
 ZDOT =         34
103849                 TA   =          227
25903
                                          MA   =          227
36539
                                          Ha   =            188
410  n
mi
                                          Hp   =            181
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8760652
75                 X    =         2660165
73
 Y    =       10430785
36  feet           Y    =         3209107
06  meter
 Z    =      -17336488
97                 Z    =        -5271214
78
 XDOT =     -19272
818652                 XDOT =       -5929
719497
 YDOT =      16323
342240  feet/sec       YDOT =        4909
354634  meter/sec
 ZDOT =        111
889270                 ZDOT =           5
432361

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         950475
21                 X    =          289704
85
 Y    =       13653968
32  feet           Y    =         4161729
54  meter
 Z    =      -17284962
12                 Z    =        -5268456
45
 XDOT =     -24202
899230                 XDOT =       -7377
043685
 YDOT =       1644
753780  feet/sec       YDOT =         501
320952  meter/sec
 ZDOT =         -1
728691                 ZDOT =           -
526905


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
51585118  
00016717  00000-0  10270-3 0  9012
2 25544  51
6466 140
4288 0011336 324
9595  35
0822 15
75996186  4155


Satellite: ISS
Catalog Number: 25544
Epoch time:      10045
51585118   =   yrday
fracday
Element set:     901
Inclination:       51
6466  deg
RA of node:       140
4288  deg
Eccentricity:     
0011336     
Arg of perigee:   324
9595  deg
Mean anomaly:      35
0822  deg
Mean motion:   15
75996186  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             415
Checksum:              311


Coasting Arc #3 (Orbit 430)
---------------------------------------

Vector Time (GMT): 2010/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5069352
77                 A    =         6726170
86  meter
 Y    =       -4362546
36  meter          E    =           
0001807
 Z    =        -724989
16                 I    =           51
90469
 XDOT =       2623
204240                 Wp   =           36
29706
 YDOT =       4044
355211  meter/sec      RA   =          134
41059  deg
 ZDOT =      -6000
358960                 TA   =          151
57371
                                          MA   =          151
56385
                                          Ha   =            188
464  n
mi
                                          Hp   =            181
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16631734
80                 X    =         5121280
55
 Y    =      -14312816
16  feet           Y    =        -4305567
55  meter
 Z    =       -2378573
38                 Z    =         -700236
49
 XDOT =       8606
313123                 XDOT =        2606
932505
 YDOT =      13268
881925  feet/sec       YDOT =        4073
598104  meter/sec
 ZDOT =     -19686
217061                 ZDOT =       -5987
655518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21858821
58                 X    =         6662568
82
 Y    =       -2029838
33  feet           Y    =         -618694
72  meter
 Z    =       -2280481
41                 Z    =         -695090
73
 XDOT =       -720
841225                 XDOT =        -219
712405
 YDOT =      14274
025763  feet/sec       YDOT =        4350
723053  meter/sec
 ZDOT =     -19635
619815                 ZDOT =       -5984
936920


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
53038223  
00016717  00000-0  10270-3 0  9026
2 25544  51
6458 135
2041 0011258 329
2145  30
8358 15
76036132  4319


Satellite: ISS
Catalog Number: 25544
Epoch time:      10046
53038223   =   yrday
fracday
Element set:     902
Inclination:       51
6458  deg
RA of node:       135
2041  deg
Eccentricity:     
0011258     
Arg of perigee:   329
2145  deg
Mean anomaly:      30
8358  deg
Mean motion:   15
76036132  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             431
Checksum:              269


Coasting Arc #4 (Orbit 446)
---------------------------------------

Vector Time (GMT): 2010/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1947138
49                 A    =         6714900
05  meter
 Y    =       -3927694
41  meter          E    =           
0013116
 Z    =        5090507
87                 I    =           51
88834
 XDOT =       5681
542971                 Wp   =          355
00678
 YDOT =      -4938
305022  meter/sec      RA   =          129
25693  deg
 ZDOT =      -1624
565219                 TA   =          110
61562
                                          MA   =          110
47489
                                          Ha   =            188
576  n
mi
                                          Hp   =            180
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6388249
63                 X    =        -1927801
84
 Y    =      -12886136
50  feet           Y    =        -3949360
00  meter
 Z    =       16701141
32                 Z    =         5081096
11
 XDOT =      18640
232845                 XDOT =        5744
233389
 YDOT =     -16201
788130  feet/sec       YDOT =       -4874
420227  meter/sec
 ZDOT =      -5329
938384                 ZDOT =       -1596
812261

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1928175
76                 X    =          587707
97
 Y    =      -14296725
90  feet           Y    =        -4357642
05  meter
 Z    =       16663617
12                 Z    =         5079070
50
 XDOT =      23516
903022                 XDOT =        7167
952041
 YDOT =      -2960
292254  feet/sec       YDOT =        -902
297079  meter/sec
 ZDOT =      -5219
951354                 ZDOT =       -1591
041173


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
54488248  
00016717  00000-0  10270-3 0  9035
2 25544  51
6464 129
9782 0011443 333
0559  27
0010 15
76122332  4474


Satellite: ISS
Catalog Number: 25544
Epoch time:      10047
54488248   =   yrday
fracday
Element set:     903
Inclination:       51
6464  deg
RA of node:       129
9782  deg
Eccentricity:     
0011443     
Arg of perigee:   333
0559  deg
Mean anomaly:      27
0010  deg
Mean motion:   15
76122332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             447
Checksum:              293


Coasting Arc #5 (Orbit 462)
---------------------------------------

Vector Time (GMT): 2010/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4815405
36                 A    =         6724280
27  meter
 Y    =        4183785
31  meter          E    =           
0017878
 Z    =        2088850
62                 I    =           51
93741
 XDOT =      -1901
694764                 Wp   =           29
88136
 YDOT =      -4976
115781  meter/sec      RA   =          124
15749  deg
 ZDOT =       5577
684727                 TA   =          353
40024
                                          MA   =          353
42375
                                          Ha   =            188
811  n
mi
                                          Hp   =            180
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15798574
00                 X    =        -4871978
38
 Y    =       13726329
77  feet           Y    =         4129620
42  meter
 Z    =        6853184
46                 Z    =         2065320
07
 XDOT =      -6239
156051                 XDOT =       -1873
004548
 YDOT =     -16325
839178  feet/sec       YDOT =       -4997
220856  meter/sec
 ZDOT =      18299
490574                 ZDOT =        5568
516485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20779658
90                 X    =        -6333640
03
 Y    =        2735399
47  feet           Y    =          833749
76  meter
 Z    =        6759924
00                 Z    =         2060424
84
 XDOT =       3892
246612                 XDOT =        1186
356767
 YDOT =     -15606
684395  feet/sec       YDOT =       -4756
917403  meter/sec
 ZDOT =      18262
893743                 ZDOT =        5566
530013


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
55935663  
00016717  00000-0  10270-3 0  9046
2 25544  51
6457 124
7531 0011413 337
7995  22
2674 15
76128355  4635


Satellite: ISS
Catalog Number: 25544
Epoch time:      10048
55935663   =   yrday
fracday
Element set:     904
Inclination:       51
6457  deg
RA of node:       124
7531  deg
Eccentricity:     
0011413     
Arg of perigee:   337
7995  deg
Mean anomaly:      22
2674  deg
Mean motion:   15
76128355  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              315


Coasting Arc #6 (Orbit 477)
---------------------------------------

Vector Time (GMT): 2010/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1420284
26                 A    =         6717023
29  meter
 Y    =        4755104
75  meter          E    =           
0009456
 Z    =       -4527845
77                 I    =           51
92862
 XDOT =      -5343
916741                 Wp   =           38
71765
 YDOT =       4574
064691  meter/sec      RA   =          118
98522  deg
 ZDOT =       3138
088182                 TA   =          262
39489
                                          MA   =          262
50230
                                          Ha   =            188
877  n
mi
                                          Hp   =            180
088

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4659725
25                 X    =         1389001
45
 Y    =       15600737
36  feet           Y    =         4770812
01  meter
 Z    =      -14855137
02                 Z    =        -4521022
40
 XDOT =     -17532
535240                 XDOT =       -5409
911643
 YDOT =      15006
773919  feet/sec       YDOT =        4513
937044  meter/sec
 ZDOT =      10295
564902                 ZDOT =        3111
967182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4359101
01                 X    =        -1328653
99
 Y    =       15713174
24  feet           Y    =         4789375
51  meter
 Z    =      -14827863
48                 Z    =        -4519532
79
 XDOT =     -21751
003963                 XDOT =       -6629
706008
 YDOT =       3550
463515  feet/sec       YDOT =        1082
181279  meter/sec
 ZDOT =      10192
025394                 ZDOT =        3106
529340


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
51039877  
00016717  00000-0  10270-3 0  9056
2 25544  51
6446 119
8545 0011466 342
0208  18
0550 15
76194776  4789


Satellite: ISS
Catalog Number: 25544
Epoch time:      10049
51039877   =   yrday
fracday
Element set:     905
Inclination:       51
6446  deg
RA of node:       119
8545  deg
Eccentricity:     
0011466     
Arg of perigee:   342
0208  deg
Mean anomaly:      18
0550  deg
Mean motion:   15
76194776  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             478
Checksum:              319


Coasting Arc #7 (Orbit 489)
---------------------------------------

Vector Time (GMT): 2010/050/05:53:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010367
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4422955
43                 A    =         6722441
45  meter
 Y    =       -4211648
27  meter          E    =           
0008862
 Z    =       -2822054
28                 I    =           51
95531
 XDOT =       1884
124371                 Wp   =            8
35019
 YDOT =       5418
541579  meter/sec      RA   =          115
20402  deg
 ZDOT =      -5127
130841                 TA   =          203
83260
                                          MA   =          203
87366
                                          Ha   =            188
918  n
mi
                                          Hp   =            179
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14511008
63                 X    =         4483430
99
 Y    =      -13817743
65  feet           Y    =        -4161850
17  meter
 Z    =       -9258708
28                 Z    =        -2800420
68
 XDOT =       6181
510402                 XDOT =        1848
299656
 YDOT =      17777
367386  feet/sec       YDOT =        5439
410391  meter/sec
 ZDOT =     -16821
295411                 ZDOT =       -5118
065174

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3502668
75                 X    =         1067613
44
 Y    =       19768943
16  feet           Y    =         6025573
88  meter
 Z    =       -9172965
07                 Z    =        -2795919
75
 XDOT =     -16853
107506                 XDOT =       -5136
827168
 YDOT =      -4812
495611  feet/sec       YDOT =       -1466
848662  meter/sec
 ZDOT =     -16785
098028                 ZDOT =       -5116
097879


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
27121468  
00016717  00000-0  10270-3 0  9060
2 25544  51
6425 115
9305 0011450 345
7763  14
3077 15
76226913  4902


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
27121468   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:       115
9305  deg
Eccentricity:     
0011450     
Arg of perigee:   345
7763  deg
Mean anomaly:      14
3077  deg
Mean motion:   15
76226913  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             490
Checksum:              286


Coasting Arc #8 (Orbit 489)
---------------------------------------

Vector Time (GMT): 2010/050/06:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1010288
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4465383
79                 A    =         6715337
93  meter
 Y    =        -256172
22  meter          E    =           
0016947
 Z    =       -5021167
38                 I    =           51
93058
 XDOT =      -1747
517658                 Wp   =           34
26867
 YDOT =       7244
527524  meter/sec      RA   =          115
16115  deg
 ZDOT =      -1913
106481                 TA   =          217
26085
                                          MA   =          217
37854
                                          Ha   =            188
985  n
mi
                                          Hp   =            180
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14650209
27                 X    =         4492308
14
 Y    =        -840460
04  feet           Y    =         -206087
38  meter
 Z    =      -16473646
27                 Z    =        -4999409
37
 XDOT =      -5733
325648                 XDOT =       -1819
103944
 YDOT =      23768
134922  feet/sec       YDOT =        7224
585381  meter/sec
 ZDOT =      -6276
596065                 ZDOT =       -1921
770104

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6860186
86                 X    =        -2090984
95
 Y    =       13080959
11  feet           Y    =         3987076
34  meter
 Z    =      -16387262
47                 Z    =        -4994837
60
 XDOT =     -16504
024110                 XDOT =       -5030
426549
 YDOT =     -16604
929722  feet/sec       YDOT =       -5061
182579  meter/sec
 ZDOT =      -6310
727789                 ZDOT =       -1923
509830


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
27121574  
00016717  00000-0  10270-3 0  9079
2 25544  51
6428 115
9310 0011243 343
4699  16
6098 15
76106772  4902


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
27121574   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       115
9310  deg
Eccentricity:     
0011243     
Arg of perigee:   343
4699  deg
Mean anomaly:      16
6098  deg
Mean motion:   15
76106772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             490
Checksum:              295


Coasting Arc #9 (Orbit 490)
---------------------------------------

Vector Time (GMT): 2010/050/06:57:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1009667
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2916068
08                 A    =         6716731
15  meter
 Y    =       -3233388
70  meter          E    =           
0015351
 Z    =        5116456
19                 I    =           51
92959
 XDOT =       4227
555472                 Wp   =            5
49356
 YDOT =      -6253
838415  meter/sec      RA   =          114
93948  deg
 ZDOT =      -1527
389421                 TA   =           99
18403
                                          MA   =           99
01034
                                          Ha   =            190
715  n
mi
                                          Hp   =            180
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9567152
51                 X    =        -2904549
59
 Y    =      -10608230
63  feet           Y    =        -3265933
22  meter
 Z    =       16786273
60                 Z    =         5102318
24
 XDOT =      13869
932651                 XDOT =        4304
592506
 YDOT =     -20517
842569  feet/sec       YDOT =       -6206
132726  meter/sec
 ZDOT =      -5011
120147                 ZDOT =       -1506
664718

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13012926
88                 X    =         3966340
11
 Y    =       -6050967
39  feet           Y    =        -1844334
86  meter
 Z    =       16730017
14                 Z    =         5099309
22
 XDOT =      14981
144550                 XDOT =        4566
252859
 YDOT =      18450
116522  feet/sec       YDOT =        5623
595516  meter/sec
 ZDOT =      -4929
060942                 ZDOT =       -1502
377775


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
33464714  
00016717  00000-0  10270-3 0  9083
2 25544  51
6429 115
6034 0012763 349
2304  10
8585 15
75447248  4911


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
33464714   =   yrday
fracday
Element set:     908
Inclination:       51
6429  deg
RA of node:       115
6034  deg
Eccentricity:     
0012763     
Arg of perigee:   349
2304  deg
Mean anomaly:      10
8585  deg
Mean motion:   15
75447248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             491
Checksum:              298


Coasting Arc #10 (Orbit 490)
---------------------------------------

Vector Time (GMT): 2010/050/07:14:00
000
Vector Time (MET): N/A
Weight (LBS)     : 1009588
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2252895
29                 A    =         6727893
67  meter
 Y    =       -6294206
54  meter          E    =           
0009335
 Z    =         773156
02                 I    =           51
96694
 XDOT =       4729
397495                 Wp   =           63
79607
 YDOT =        949
039550  meter/sec      RA   =          114
88419  deg
 ZDOT =      -5995
361493                 TA   =          107
81700
                                          MA   =          107
71514
                                          Ha   =            190
611  n
mi
                                          Hp   =            180
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7391388
74                 X    =         2319354
97
 Y    =      -20650283
91  feet           Y    =        -6268641
69  meter
 Z    =        2536601
11                 Z    =          784262
23
 XDOT =      15516
395981                 XDOT =        4747
557746
 YDOT =       3113
646819  feet/sec       YDOT =        1002
027699  meter/sec
 ZDOT =     -19669
821172                 ZDOT =       -5972
342264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18432849
82                 X    =         5618332
63
 Y    =       11877391
72  feet           Y    =         3620229
00  meter
 Z    =        2580467
30                 Z    =          786526
43
 XDOT =      -5718
924886                 XDOT =       -1743
128305
 YDOT =      13170
652452  feet/sec       YDOT =        4014
414867  meter/sec
 ZDOT =     -19578
384668                 ZDOT =       -5967
491647


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
33464749  
00016717  00000-0  10270-3 0  9092
2 25544  51
6428 115
6035 0012470 348
6862  11
4019 15
75409154  4911


Satellite: ISS
Catalog Number: 25544
Epoch time:      10050
33464749   =   yrday
fracday
Element set:     909
Inclination:       51
6428  deg
RA of node:       115
6035  deg
Eccentricity:     
0012470     
Arg of perigee:   348
6862  deg
Mean anomaly:      11
4019  deg
Mean motion:   15
75409154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             491
Checksum:              297


Coasting Arc #11 (Orbit 506)
---------------------------------------

Vector Time (GMT): 2010/051/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3859278
10                 A    =         6715962
58  meter
 Y    =       -1501108
40  meter          E    =           
0012619
 Z    =        5286909
78                 I    =           51
93983
 XDOT =       2670
934507                 Wp   =            3
55806
 YDOT =      -7226
090579  meter/sec      RA   =          109
76337  deg
 ZDOT =        -89
664321                 TA   =           87
36108
                                          MA   =           87
21663
                                          Ha   =            190
811  n
mi
                                          Hp   =            180
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12661673
57                 X    =        -3867888
23
 Y    =       -4924896
34  feet           Y    =        -1544313
09  meter
 Z    =       17345504
53                 Z    =         5268140
72
 XDOT =       8762
908488                 XDOT =        2751
974994
 YDOT =     -23707
646255  feet/sec       YDOT =       -7195
769486  meter/sec
 ZDOT =       -294
174281                 ZDOT =         -76
491924

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7451091
61                 X    =         2271092
72
 Y    =      -11473255
30  feet           Y    =        -3497048
22  meter
 Z    =       17270922
25                 Z    =         5264177
10
 XDOT =      20553
563770                 XDOT =        6264
726237
 YDOT =      12922
467315  feet/sec       YDOT =        3938
768038  meter/sec
 ZDOT =       -242
124166                 ZDOT =         -73
799446


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
34956323  
00016717  00000-0  10270-3 0  9100
2 25544  51
6439 110
3808 0012543 352
7510   7
3470 15
75450446  5073


Satellite: ISS
Catalog Number: 25544
Epoch time:      10051
34956323   =   yrday
fracday
Element set:     910
Inclination:       51
6439  deg
RA of node:       110
3808  deg
Eccentricity:     
0012543     
Arg of perigee:   352
7510  deg
Mean anomaly:       7
3470  deg
Mean motion:   15
75450446  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             507
Checksum:              277


Coasting Arc #12 (Orbit 522)
---------------------------------------

Vector Time (GMT): 2010/052/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2117257
02                 A    =         6727845
76  meter
 Y    =        6345189
17  meter          E    =           
0022958
 Z    =         568165
63                 I    =           51
98999
 XDOT =      -4358
001915                 Wp   =           24
69667
 YDOT =      -2001
151010  meter/sec      RA   =          104
64637  deg
 ZDOT =       6042
199399                 TA   =          341
46976
                                          MA   =          341
55323
                                          Ha   =            190
853  n
mi
                                          Hp   =            180
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6946381
31                 X    =        -2190812
72
 Y    =       20817549
76  feet           Y    =         6321101
48  meter
 Z    =        1864060
46                 Z    =          557701
30
 XDOT =     -14297
906546                 XDOT =       -4364
652429
 YDOT =      -6565
456069  feet/sec       YDOT =       -2049
921839  meter/sec
 ZDOT =      19823
488843                 ZDOT =        6021
012312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19123198
25                 X    =        -5828750
83
 Y    =      -10773963
79  feet           Y    =        -3283904
16  meter
 Z    =        1822719
29                 Z    =          555564
84
 XDOT =       8390
433390                 XDOT =        2557
404097
 YDOT =     -11515
439601  feet/sec       YDOT =       -3509
905991  meter/sec
 ZDOT =      19739
285238                 ZDOT =        6016
534141


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
36445148  
00016717  00000-0  10270-3 0  9112
2 25544  51
6447 105
1582 0012541 357
0644   3
0444 15
75480749  5238


Satellite: ISS
Catalog Number: 25544
Epoch time:      10052
36445148   =   yrday
fracday
Element set:     911
Inclination:       51
6447  deg
RA of node:       105
1582  deg
Eccentricity:     
0012541     
Arg of perigee:   357
0644  deg
Mean anomaly:       3
0444  deg
Mean motion:   15
75480749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             523
Checksum:              284


Coasting Arc #13 (Orbit 537)
---------------------------------------

Vector Time (GMT): 2010/053/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3776384
50                 A    =         6716164
67  meter
 Y    =        2015822
54  meter          E    =           
0017555
 Z    =       -5185520
20                 I    =           51
95796
 XDOT =      -2199
117240                 Wp   =           54
43517
 YDOT =       7269
224580  meter/sec      RA   =           99
50849  deg
 ZDOT =       1237
205706                 TA   =          227
27109
                                          MA   =          227
41899
                                          Ha   =            190
909  n
mi
                                          Hp   =            179
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12389712
91                 X    =         3778752
56
 Y    =        6613591
02  feet           Y    =         2058065
54  meter
 Z    =      -17012861
56                 Z    =        -5167169
00
 XDOT =      -7214
951576                 XDOT =       -2286
249608
 YDOT =      23849
162007  feet/sec       YDOT =        7244
145568  meter/sec
 ZDOT =       4059
073837                 ZDOT =        1226
310853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8668180
79                 X    =        -2642061
50
 Y    =       11161715
33  feet           Y    =         3402090
83  meter
 Z    =      -16939916
87                 Z    =        -5163286
66
 XDOT =     -21429
458023                 XDOT =       -6531
698805
 YDOT =     -10611
458604  feet/sec       YDOT =       -3234
372583  meter/sec
 ZDOT =       4016
039326                 ZDOT =        1224
088787


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
31588360  
00016717  00000-0  10270-3 0  9123
2 25544  51
6449 100
2629 0012551    
7753 359
3429 15
75552496  5387


Satellite: ISS
Catalog Number: 25544
Epoch time:      10053
31588360   =   yrday
fracday
Element set:     912
Inclination:       51
6449  deg
RA of node:       100
2629  deg
Eccentricity:     
0012551     
Arg of perigee:      
7753  deg
Mean anomaly:     359
3429  deg
Mean motion:   15
75552496  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             538
Checksum:              304


Coasting Arc #14 (Orbit 553)
---------------------------------------

Vector Time (GMT): 2010/054/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1748807
77                 A    =         6726557
64  meter
 Y    =       -6297560
47  meter          E    =           
0008475
 Z    =       -1611814
08                 I    =           51
99746
 XDOT =       4319
695436                 Wp   =           43
66269
 YDOT =       2674
651562  meter/sec      RA   =           94
40991  deg
 ZDOT =      -5775
292211                 TA   =          154
02693
                                          MA   =          153
98437
                                          Ha   =            190
931  n
mi
                                          Hp   =            179
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5737558
30                 X    =         1826928
01
 Y    =      -20661287
63  feet           Y    =        -6277567
46  meter
 Z    =       -5288103
92                 Z    =        -1603128
80
 XDOT =      14172
229120                 XDOT =        4317
520836
 YDOT =       8775
103551  feet/sec       YDOT =        2722
944840  meter/sec
 ZDOT =     -18947
809090                 ZDOT =       -5754
312729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19513043
50                 X    =         5947575
66
 Y    =        8911291
84  feet           Y    =         2716161
75  meter
 Z    =       -5253802
03                 Z    =        -1601358
86
 XDOT =     -10239
205078                 XDOT =       -3120
909708
 YDOT =      11322
180828  feet/sec       YDOT =        3451
000716  meter/sec
 ZDOT =     -18864
401780                 ZDOT =       -5749
869663


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
33071808  
00016717  00000-0  10270-3 0  9131
2 25544  51
6453  95
0392 0012556   4
5677 355
5600 15
75580438  5546


Satellite: ISS
Catalog Number: 25544
Epoch time:      10054
33071808   =   yrday
fracday
Element set:     913
Inclination:       51
6453  deg
RA of node:        95
0392  deg
Eccentricity:     
0012556     
Arg of perigee:     4
5677  deg
Mean anomaly:     355
5600  deg
Mean motion:   15
75580438  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             554
Checksum:              301


Coasting Arc #15 (Orbit 569)
---------------------------------------

Vector Time (GMT): 2010/055/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3822830
64                 A    =         6717449
51  meter
 Y    =       -2655240
57  meter          E    =           
0017956
 Z    =        4842804
98                 I    =           51
96870
 XDOT =       1811
276091                 Wp   =           26
13087
 YDOT =      -7081
259806  meter/sec      RA   =           89
25274  deg
 ZDOT =      -2433
593670                 TA   =           87
61588
                                          MA   =           87
41031
                                          Ha   =            191
109  n
mi
                                          Hp   =            179
172

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12542095
27                 X    =        -3816380
12
 Y    =       -8711419
20  feet           Y    =        -2697953
70  meter
 Z    =       15888467
77                 Z    =         4824249
70
 XDOT =       5942
506861                 XDOT =        1902
147089
 YDOT =     -23232
479678  feet/sec       YDOT =       -7060
496937  meter/sec
 ZDOT =      -7984
231202                 ZDOT =       -2424
574008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10376944
87                 X    =         3162892
80
 Y    =      -11307126
92  feet           Y    =        -3446412
29  meter
 Z    =       15814685
64                 Z    =         4820316
18
 XDOT =      21354
815621                 XDOT =        6508
947801
 YDOT =       8392
380117  feet/sec       YDOT =        2557
997460  meter/sec
 ZDOT =      -7948
615479                 ZDOT =       -2422
737998


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
34552495  
00016717  00000-0  10270-3 0  9140
2 25544  51
6458  89
8161 0012666   8
7498 351
3884 15
75617136  5707


Satellite: ISS
Catalog Number: 25544
Epoch time:      10055
34552495   =   yrday
fracday
Element set:     914
Inclination:       51
6458  deg
RA of node:        89
8161  deg
Eccentricity:     
0012666     
Arg of perigee:     8
7498  deg
Mean anomaly:     351
3884  deg
Mean motion:   15
75617136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             570
Checksum:              331


Coasting Arc #16 (Orbit 585)
---------------------------------------

Vector Time (GMT): 2010/056/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1436818
79                 A    =         6724489
67  meter
 Y    =        6012285
49  meter          E    =           
0022298
 Z    =        2610332
59                 I    =           51
99138
 XDOT =      -4496
110087                 Wp   =           46
36520
 YDOT =      -3374
442008  meter/sec      RA   =           84
17049  deg
 ZDOT =       5284
674367                 TA   =          343
22041
                                          MA   =          343
29406
                                          Ha   =            191
114  n
mi
                                          Hp   =            178
855

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4713972
40                 X    =        -1516622
64
 Y    =       19725346
09  feet           Y    =         5995771
93  meter
 Z    =        8564083
29                 Z    =         2603158
83
 XDOT =     -14751
017346                 XDOT =       -4483
713646
 YDOT =     -11071
003963  feet/sec       YDOT =       -3424
650837  meter/sec
 ZDOT =      17338
170495                 ZDOT =        5262
862960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19001039
20                 X    =        -5791516
75
 Y    =       -7124296
85  feet           Y    =        -2171485
68  meter
 Z    =        8535762
42                 Z    =         2601700
39
 XDOT =      12272
758121                 XDOT =        3740
736675
 YDOT =     -12012
849353  feet/sec       YDOT =       -3661
516483  meter/sec
 ZDOT =      17251
428294                 ZDOT =        5258
235344


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
36030270  
00016717  00000-0  10270-3 0  9156
2 25544  51
6459  84
5927 0012627  12
7024 347
4456 15
75666336  5861


Satellite: ISS
Catalog Number: 25544
Epoch time:      10056
36030270   =   yrday
fracday
Element set:     915
Inclination:       51
6459  deg
RA of node:        84
5927  deg
Eccentricity:     
0012627     
Arg of perigee:    12
7024  deg
Mean anomaly:     347
4456  deg
Mean motion:   15
75666336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             586
Checksum:              311


Coasting Arc #17 (Orbit 600)
---------------------------------------

Vector Time (GMT): 2010/057/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4049901
84                 A    =         6719307
92  meter
 Y    =        3208026
81  meter          E    =           
0014726
 Z    =       -4300303
77                 I    =           51
96988
 XDOT =      -1529
954071                 Wp   =           51
77015
 YDOT =       6660
725219  meter/sec      RA   =           79
00050  deg
 ZDOT =       3545
071179                 TA   =          253
92177
                                          MA   =          254
08397
                                          Ha   =            191
149  n
mi
                                          Hp   =            178
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13287079
54                 X    =         4034617
61
 Y    =       10525022
35  feet           Y    =         3253229
63  meter
 Z    =      -14108608
16                 Z    =        -4280667
14
 XDOT =      -5019
534354                 XDOT =       -1621
542588
 YDOT =      21852
773027  feet/sec       YDOT =        6643
104376  meter/sec
 ZDOT =      11630
810956                 ZDOT =        3537
416212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11862258
51                 X    =        -3615616
39
 Y    =       12198652
61  feet           Y    =         3718149
31  meter
 Z    =      -14030506
05                 Z    =        -4276498
24
 XDOT =     -20313
355939                 XDOT =       -6191
510890
 YDOT =      -6475
194700  feet/sec       YDOT =       -1973
639345  meter/sec
 ZDOT =      11600
594455                 ZDOT =        3535
861190


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
31163175  
00016717  00000-0  10270-3 0  9164
2 25544  51
6456  79
6966 0012628  16
1923 343
9643 15
75721935  6017


Satellite: ISS
Catalog Number: 25544
Epoch time:      10057
31163175   =   yrday
fracday
Element set:     916
Inclination:       51
6456  deg
RA of node:        79
6966  deg
Eccentricity:     
0012628     
Arg of perigee:    16
1923  deg
Mean anomaly:     343
9643  deg
Mean motion:   15
75721935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             601
Checksum:              315


Coasting Arc #18 (Orbit 616)
---------------------------------------

Vector Time (GMT): 2010/058/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1301941
36                 A    =         6721734
25  meter
 Y    =       -5558910
13  meter          E    =           
0015787
 Z    =       -3567548
01                 I    =           51
97052
 XDOT =       4799
507933                 Wp   =           37
27460
 YDOT =       4000
700320  meter/sec      RA   =           73
92547  deg
 ZDOT =      -4480
308639                 TA   =          185
00445
                                          MA   =          185
02025
                                          Ha   =            191
151  n
mi
                                          Hp   =            178
429

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4271461
15                 X    =         1381335
31
 Y    =      -18237894
11  feet           Y    =        -5543907
35  meter
 Z    =      -11704553
84                 Z    =        -3561030
18
 XDOT =      15746
417104                 XDOT =        4776
178570
 YDOT =      13125
657217  feet/sec       YDOT =        4054
240543  meter/sec
 ZDOT =     -14699
175325                 ZDOT =       -4457
050240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17790121
02                 X    =         5422428
89
 Y    =        5914343
75  feet           Y    =         1802691
97  meter
 Z    =      -11678821
64                 Z    =        -3559704
83
 XDOT =     -14024
902045                 XDOT =       -4274
790143
 YDOT =      13330
183007  feet/sec       YDOT =        4063
039781  meter/sec
 ZDOT =     -14606
659537                 ZDOT =       -4452
109827


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
32635473  
00016717  00000-0  10270-3 0  9172
2 25544  51
6448  74
4724 0012622  19
9911 340
1745 15
75736254  6174


Satellite: ISS
Catalog Number: 25544
Epoch time:      10058
32635473   =   yrday
fracday
Element set:     917
Inclination:       51
6448  deg
RA of node:        74
4724  deg
Eccentricity:     
0012622     
Arg of perigee:    19
9911  deg
Mean anomaly:     340
1745  deg
Mean motion:   15
75736254  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             617
Checksum:              310


Coasting Arc #19 (Orbit 632)
---------------------------------------

Vector Time (GMT): 2010/059/07:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 764580
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4369184
28                 A    =         6721884
17  meter
 Y    =       -3746709
62  meter          E    =           
0021255
 Z    =        3468965
46                 I    =           51
96208
 XDOT =       1500
428210                 Wp   =           55
62704
 YDOT =      -6013
334898  meter/sec      RA   =           68
74760  deg
 ZDOT =      -4573
496889                 TA   =           83
42266
                                          MA   =           83
18075
                                          Ha   =            191
243  n
mi
                                          Hp   =            178
091

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14334594
08                 X    =        -4343814
34
 Y    =      -12292354
41  feet           Y    =        -3795426
27  meter
 Z    =       11381120
27                 Z    =         3447802
49
 XDOT =       4922
664730                 XDOT =        1589
775510
 YDOT =     -19728
789035  feet/sec       YDOT =       -5996
057070  meter/sec
 ZDOT =     -15004
911052                 ZDOT =       -4565
990433

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13270966
29                 X    =         4044990
52
 Y    =      -13504559
58  feet           Y    =        -4116189
76  meter
 Z    =       11296937
08                 Z    =         3443306
42
 XDOT =      18344
770323                 XDOT =        5591
485994
 YDOT =       5413
138571  feet/sec       YDOT =        1649
924637  meter/sec
 ZDOT =     -14975
263297                 ZDOT =       -4564
460253


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   10059
34104795  
00016717  00000-0  10270-3 0  9184
2 25544  51
6449  69
2477 0012788  23
8747 336
3008 15
75805174  6331


Satellite: ISS
Catalog Number: 25544
Epoch time:      10059
34104795   =   yrday
fracday
Element set:     918
Inclination:       51
6449  deg
RA of node:        69
2477  deg
Eccentricity:     
0012788     
Arg of perigee:    23
8747  deg
Mean anomaly:     336
3008  deg
Mean motion:   15
75805174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             633
Checksum:              329

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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