[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: July 25th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 ET - UTC (sec) : 68 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


209/14:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 3

209/15:41:12 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 3

209/22:00:48 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 4

212/23:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 1

216/02:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 3

219/05:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 212 2

Coasting Arc #1 (Orbit 2755)
---------------------------------------

Vector Time (GMT): 2017/205/13:31:09
955
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2991796
49                 A    =         6784058
89  meter
 Y    =        5013533
49  meter          E    =           
0010950
 Z    =       -3466960
93                 I    =           51
44142
 XDOT =      -6145
545174                 Wp   =           75
60555
 YDOT =        535
537262  meter/sec      RA   =          210
92216  deg
 ZDOT =      -4538
224737                 TA   =          145
15869
                                          MA   =          145
08695
                                          Ha   =            223
073  n
mi
                                          Hp   =            212
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9815605
29                 X    =         2952351
89
 Y    =       16448600
70  feet           Y    =         5046769
49  meter
 Z    =      -11374543
73                 Z    =        -3452523
50
 XDOT =     -20162
549784                 XDOT =       -6129
032986
 YDOT =       1757
012015  feet/sec       YDOT =         466
906242  meter/sec
 ZDOT =     -14889
188769                 ZDOT =       -4568
037065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1536084
89                 X    =          468198
68
 Y    =      -19130438
67  feet           Y    =        -5830957
71  meter
 Z    =      -11311479
87                 Z    =        -3447739
06
 XDOT =      15939
988611                 XDOT =        4858
508529
 YDOT =      10143
239264  feet/sec       YDOT =        3091
659328  meter/sec
 ZDOT =     -15021
016755                 ZDOT =       -4578
405907


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   17205
58829981  
00016717  00000-0  10270-3 0  9002
2 25544  51
6359 211
8912 0006250  64
7846 295
3954 15
54209618 27561


Satellite: ISS
Catalog Number: 25544
Epoch time:      17205
58829981   =   yrday
fracday
Element set:     900
Inclination:       51
6359  deg
RA of node:       211
8912  deg
Eccentricity:     
0006250     
Arg of perigee:    64
7846  deg
Mean anomaly:     295
3954  deg
Mean motion:   15
54209618  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2756
Checksum:              337


Coasting Arc #2 (Orbit 2771)
---------------------------------------

Vector Time (GMT): 2017/206/13:31:09
955
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1500396
01                 A    =         6780173
20  meter
 Y    =       -4772777
63  meter          E    =           
0013558
 Z    =        4564994
78                 I    =           51
45731
 XDOT =       7011
290856                 Wp   =           95
41450
 YDOT =        713
670327  meter/sec      RA   =          205
92162  deg
 ZDOT =       3041
541440                 TA   =          324
10115
                                          MA   =          324
19217
                                          Ha   =            222
970  n
mi
                                          Hp   =            212
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4922559
10                 X    =        -1469088
05
 Y    =      -15658719
26  feet           Y    =        -4789381
23  meter
 Z    =       14977016
98                 Z    =         4557782
31
 XDOT =      23002
922755                 XDOT =        6988
015329
 YDOT =       2341
438081  feet/sec       YDOT =         791
945069  meter/sec
 ZDOT =       9978
810499                 ZDOT =        3075
542863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4764829
68                 X    =        -1452320
09
 Y    =       15737108
37  feet           Y    =         4796670
63  meter
 Z    =       14945833
30                 Z    =         4555489
99
 XDOT =     -16396
618582                 XDOT =       -4997
689344
 YDOT =     -14612
442635  feet/sec       YDOT =       -4453
872515  meter/sec
 ZDOT =      10128
986543                 ZDOT =        3087
315098


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   17206
61707285  
00016717  00000-0  10270-3 0  9010
2 25544  51
6360 206
7625 0005993  68
1081 292
0708 15
54242695 27720


Satellite: ISS
Catalog Number: 25544
Epoch time:      17206
61707285   =   yrday
fracday
Element set:     901
Inclination:       51
6360  deg
RA of node:       206
7625  deg
Eccentricity:     
0005993     
Arg of perigee:    68
1081  deg
Mean anomaly:     292
0708  deg
Mean motion:   15
54242695  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2772
Checksum:              314


Coasting Arc #3 (Orbit 2786)
---------------------------------------

Vector Time (GMT): 2017/207/13:31:09
955
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -218532
59                 A    =         6777614
31  meter
 Y    =        4353981
60  meter          E    =           
0020187
 Z    =       -5207378
27                 I    =           51
47945
 XDOT =      -7344
776274                 Wp   =           78
15400
 YDOT =      -1792
248354  meter/sec      RA   =          200
91195  deg
 ZDOT =      -1190
166068                 TA   =          180
38066
                                          MA   =          180
38220
                                          Ha   =            223
067  n
mi
                                          Hp   =            212
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -716970
43                 X    =         -241909
32
 Y    =       14284716
55  feet           Y    =         4351407
24  meter
 Z    =      -17084574
38                 Z    =        -5208496
49
 XDOT =     -24097
035021                 XDOT =       -7318
407876
 YDOT =      -5880
079902  feet/sec       YDOT =       -1874
235170  meter/sec
 ZDOT =      -3904
744316                 ZDOT =       -1225
780012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8415843
79                 X    =         2565149
19
 Y    =      -11556402
68  feet           Y    =        -3522391
54  meter
 Z    =      -17090142
94                 Z    =        -5209075
57
 XDOT =      15940
307911                 XDOT =        4858
605851
 YDOT =      17615
974635  feet/sec       YDOT =        5369
349069  meter/sec
 ZDOT =      -4061
910825                 ZDOT =       -1238
070419


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   17207
58154537  
00016717  00000-0  10270-3 0  9024
2 25544  51
6371 201
9529 0006169  71
3755 288
8067 15
54216768 27871


Satellite: ISS
Catalog Number: 25544
Epoch time:      17207
58154537   =   yrday
fracday
Element set:     902
Inclination:       51
6371  deg
RA of node:       201
9529  deg
Eccentricity:     
0006169     
Arg of perigee:    71
3755  deg
Mean anomaly:     288
8067  deg
Mean motion:   15
54216768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2787
Checksum:              339


Coasting Arc #4 (Orbit 2802)
---------------------------------------

Vector Time (GMT): 2017/208/13:31:09
955
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1997955
40                 A    =         6777243
15  meter
 Y    =       -3775321
62  meter          E    =           
0009242
 Z    =        5254571
24                 I    =           51
50943
 XDOT =       7147
547798                 Wp   =           70
52632
 YDOT =       2684
882520  meter/sec      RA   =          195
90142  deg
 ZDOT =       -784
535326                 TA   =           27
00141
                                          MA   =           26
95336
                                          Ha   =            222
998  n
mi
                                          Hp   =            212
320

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6554971
77                 X    =         2014499
84
 Y    =      -12386225
80  feet           Y    =        -3752886
69  meter
 Z    =       17239406
94                 Z    =         5264316
66
 XDOT =      23449
959966                 XDOT =        7120
804341
 YDOT =       8808
669684  feet/sec       YDOT =        2764
661735  meter/sec
 ZDOT =      -2573
934797                 ZDOT =        -749
880241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12105911
11                 X    =        -3689881
71
 Y    =        6951783
85  feet           Y    =         2118903
72  meter
 Z    =       17283026
75                 Z    =         5267866
55
 XDOT =     -14498
304790                 XDOT =       -4419
083300
 YDOT =     -19194
560734  feet/sec       YDOT =       -5850
502112  meter/sec
 ZDOT =      -2421
115681                 ZDOT =        -737
956059


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   17208
61031099  
00016717  00000-0  10270-3 0  9037
2 25544  51
6373 196
8239 0006166  74
1686 286
0146 15
54224724 28032


Satellite: ISS
Catalog Number: 25544
Epoch time:      17208
61031099   =   yrday
fracday
Element set:     903
Inclination:       51
6373  deg
RA of node:       196
8239  deg
Eccentricity:     
0006166     
Arg of perigee:    74
1686  deg
Mean anomaly:     286
0146  deg
Mean motion:   15
54224724  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2803
Checksum:              313


Coasting Arc #5 (Orbit 2817)
---------------------------------------

Vector Time (GMT): 2017/209/13:31:09
955
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3677528
34                 A    =         6779377
09  meter
 Y    =        3144424
14  meter          E    =           
0016809
 Z    =       -4763939
31                 I    =           51
54810
 XDOT =      -6332
873433                 Wp   =           98
07567
 YDOT =      -3375
342808  meter/sec      RA   =          190
89591  deg
 ZDOT =       2666
552809                 TA   =          198
30262
                                          MA   =          198
36318
                                          Ha   =            223
054  n
mi
                                          Hp   =            212
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12065381
68                 X    =        -3689276
22
 Y    =       10316352
18  feet           Y    =         3103233
89  meter
 Z    =      -15629722
14                 Z    =        -4781831
87
 XDOT =     -20777
143809                 XDOT =       -6307
611426
 YDOT =     -11073
959344  feet/sec       YDOT =       -3446
020083  meter/sec
 ZDOT =       8748
532837                 ZDOT =        2635
851391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15596856
60                 X    =         4753921
89
 Y    =       -2499108
44  feet           Y    =         -761728
25  meter
 Z    =      -15709274
10                 Z    =        -4788186
75
 XDOT =      11736
772129                 XDOT =        3577
368145
 YDOT =      19224
580326  feet/sec       YDOT =        5859
652083  meter/sec
 ZDOT =       8613
273384                 ZDOT =        2625
325727


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   17209
57477547  
00016717  00000-0  10270-3 0  9046
2 25544  51
6372 192
0156 0006099  77
2158 282
9676 15
54217997 28183


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
57477547   =   yrday
fracday
Element set:     904
Inclination:       51
6372  deg
RA of node:       192
0156  deg
Eccentricity:     
0006099     
Arg of perigee:    77
2158  deg
Mean anomaly:     282
9676  deg
Mean motion:   15
54217997  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2818
Checksum:              353


Coasting Arc #6 (Orbit 2818)
---------------------------------------

Vector Time (GMT): 2017/209/14:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3158791
04                 A    =         6780976
12  meter
 Y    =        4126369
98  meter          E    =           
0014833
 Z    =       -4371109
52                 I    =           51
55640
 XDOT =      -6684
111295                 Wp   =           73
20429
 YDOT =       1501
512880  meter/sec      RA   =          190
67370  deg
 ZDOT =      -3418
282910                 TA   =          162
06812
                                          MA   =          162
01573
                                          Ha   =            223
050  n
mi
                                          Hp   =            212
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10363487
67                 X    =         3133646
55
 Y    =       13537959
25  feet           Y    =         4161553
18  meter
 Z    =      -14340910
50                 Z    =        -4355826
32
 XDOT =     -21929
499000                 XDOT =       -6683
800706
 YDOT =       4926
223361  feet/sec       YDOT =        1426
768380  meter/sec
 ZDOT =     -11214
838945                 ZDOT =       -3450
751065

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7304935
99                 X    =        -2226544
49
 Y    =      -15467156
60  feet           Y    =        -4714389
33  meter
 Z    =      -14273924
06                 Z    =        -4350692
05
 XDOT =      21275
513529                 XDOT =        6484
776524
 YDOT =        417
634516  feet/sec       YDOT =         127
295001  meter/sec
 ZDOT =     -11358
600657                 ZDOT =       -3462
101480


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   17209
63907315  
00016717  00000-0  10270-3 0  9055
2 25544  51
6384 191
6949 0006168  77
3782 282
8060 15
54248344 28199


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
63907315   =   yrday
fracday
Element set:     905
Inclination:       51
6384  deg
RA of node:       191
6949  deg
Eccentricity:     
0006168     
Arg of perigee:    77
3782  deg
Mean anomaly:     282
8060  deg
Mean motion:   15
54248344  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2819
Checksum:              338


Coasting Arc #7 (Orbit 2819)
---------------------------------------

Vector Time (GMT): 2017/209/15:41:12
000
Vector Time (MET): N/A
Weight (LBS)     : 887043
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -164402
61                 A    =         6777170
58  meter
 Y    =       -4271491
87  meter          E    =           
0008727
 Z    =        5251549
79                 I    =           51
54570
 XDOT =       7595
246764                 Wp   =           93
28230
 YDOT =        732
359198  meter/sec      RA   =          190
47372  deg
 ZDOT =        831
774742                 TA   =          348
75392
                                          MA   =          348
77341
                                          Ha   =            222
924  n
mi
                                          Hp   =            212
295

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -539378
63                 X    =         -142134
57
 Y    =      -14014080
95  feet           Y    =        -4273205
89  meter
 Z    =       17229494
05                 Z    =         5250805
22
 XDOT =      24918
788597                 XDOT =        7582
452537
 YDOT =       2402
753274  feet/sec       YDOT =         817
222863  meter/sec
 ZDOT =       2728
919756                 ZDOT =         868
638562

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         879760
34                 X    =          268150
95
 Y    =       14000143
26  feet           Y    =         4267243
67  meter
 Z    =       17226806
73                 Z    =         5250730
69
 XDOT =     -23915
238102                 XDOT =       -7289
364574
 YDOT =      -2062
260270  feet/sec       YDOT =        -628
576930  meter/sec
 ZDOT =       2891
800198                 ZDOT =         881
420700


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   17209
70336944  
00016717  00000-0  10270-3 0  9068
2 25544  51
6389 191
3754 0005947  77
7175 282
4643 15
54275533 28204


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
70336944   =   yrday
fracday
Element set:     906
Inclination:       51
6389  deg
RA of node:       191
3754  deg
Eccentricity:     
0005947     
Arg of perigee:    77
7175  deg
Mean anomaly:     282
4643  deg
Mean motion:   15
54275533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2820
Checksum:              336


Coasting Arc #8 (Orbit 2823)
---------------------------------------

Vector Time (GMT): 2017/209/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3740166
72                 A    =         6779604
97  meter
 Y    =       -3160952
13  meter          E    =           
0013604
 Z    =        4679554
58                 I    =           51
56052
 XDOT =       6331
416623                 Wp   =           70
49087
 YDOT =       3289
848922  meter/sec      RA   =          189
12721  deg
 ZDOT =      -2827
044414                 TA   =           47
61924
                                          MA   =           47
50417
                                          Ha   =            222
853  n
mi
                                          Hp   =            212
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12270888
18                 X    =         3752504
63
 Y    =      -10370577
86  feet           Y    =        -3119058
12  meter
 Z    =       15352869
37                 Z    =         4697752
87
 XDOT =      20772
364249                 XDOT =        6307
890333
 YDOT =      10793
467592  feet/sec       YDOT =        3360
519616  meter/sec
 ZDOT =      -9275
080097                 ZDOT =       -2796
345821

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11602008
64                 X    =         3536292
23
 Y    =       11001185
38  feet           Y    =         3353161
30  meter
 Z    =       15433777
74                 Z    =         4704215
45
 XDOT =      -7719
098559                 XDOT =       -2352
781241
 YDOT =      21014
162386  feet/sec       YDOT =        6405
116695  meter/sec
 ZDOT =      -9139
815318                 ZDOT =       -2785
815709


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   17209
96055868  
00016717  00000-0  10270-3 0  9070
2 25544  51
6373 190
0905 0005845  79
4600 280
7211 15
54237503 28241


Satellite: ISS
Catalog Number: 25544
Epoch time:      17209
96055868   =   yrday
fracday
Element set:     907
Inclination:       51
6373  deg
RA of node:       190
0905  deg
Eccentricity:     
0005845     
Arg of perigee:    79
4600  deg
Mean anomaly:     280
7211  deg
Mean motion:   15
54237503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2824
Checksum:              315


Coasting Arc #9 (Orbit 2838)
---------------------------------------

Vector Time (GMT): 2017/210/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5151203
25                 A    =         6783270
74  meter
 Y    =        2516569
48  meter          E    =           
0011461
 Z    =       -3635865
34                 I    =           51
60491
 XDOT =      -4965
439370                 Wp   =           92
06350
 YDOT =      -3843
606162  meter/sec      RA   =          184
13256  deg
 ZDOT =       4386
118668                 TA   =          224
83087
                                          MA   =          224
92352
                                          Ha   =            222
968  n
mi
                                          Hp   =            212
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16900273
14                 X    =        -5161300
27
 Y    =        8256461
55  feet           Y    =         2458908
84  meter
 Z    =      -11928692
07                 Z    =        -3660912
53
 XDOT =     -16290
811580                 XDOT =       -4943
395522
 YDOT =     -12610
256436  feet/sec       YDOT =       -3899
009909  meter/sec
 ZDOT =      14390
153111                 ZDOT =        4362
051797

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10264862
96                 X    =        -3128730
23
 Y    =      -15676665
21  feet           Y    =        -4778247
56  meter
 Z    =      -12039802
35                 Z    =        -3669731
76
 XDOT =       9351
337777                 XDOT =        2850
287754
 YDOT =     -17064
688755  feet/sec       YDOT =       -5201
317132  meter/sec
 ZDOT =      14284
275118                 ZDOT =        4353
847056


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   17210
92501846  
00016717  00000-0  10270-3 0  9081
2 25544  51
6369 185
2808 0005997  83
9320 276
2516 15
54249962 28397


Satellite: ISS
Catalog Number: 25544
Epoch time:      17210
92501846   =   yrday
fracday
Element set:     908
Inclination:       51
6369  deg
RA of node:       185
2808  deg
Eccentricity:     
0005997     
Arg of perigee:    83
9320  deg
Mean anomaly:     276
2516  deg
Mean motion:   15
54249962  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2839
Checksum:              342


Coasting Arc #10 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2017/211/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6176391
53                 A    =         6786849
63  meter
 Y    =       -1789416
47  meter          E    =           
0019413
 Z    =        2145887
17                 I    =           51
64956
 XDOT =       3171
988183                 Wp   =          102
74720
 YDOT =       4306
036462  meter/sec      RA   =          179
15180  deg
 ZDOT =      -5501
282822                 TA   =           53
44662
                                          MA   =           53
26807
                                          Ha   =            222
852  n
mi
                                          Hp   =            212
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20263751
74                 X    =         6185518
64
 Y    =       -5870788
93  feet           Y    =        -1720296
89  meter
 Z    =        7040312
25                 Z    =         2175912
04
 XDOT =      10406
785376                 XDOT =        3150
323515
 YDOT =      14127
416214  feet/sec       YDOT =        4341
386817  meter/sec
 ZDOT =     -18048
828157                 ZDOT =       -5485
926903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8647515
25                 X    =         2635762
65
 Y    =       19194149
58  feet           Y    =         5850376
79  meter
 Z    =        7173346
23                 Z    =         2186435
93
 XDOT =     -11110
550565                 XDOT =       -3386
495812
 YDOT =      11771
212770  feet/sec       YDOT =        3587
865652  meter/sec
 ZDOT =     -17981
526108                 ZDOT =       -5480
769158


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   17211
95376870  
00016717  00000-0  10270-3 0  9093
2 25544  51
6367 180
1511 0005862  85
9606 274
2216 15
54285682 28552


Satellite: ISS
Catalog Number: 25544
Epoch time:      17211
95376870   =   yrday
fracday
Element set:     909
Inclination:       51
6367  deg
RA of node:       180
1511  deg
Eccentricity:     
0005862     
Arg of perigee:    85
9606  deg
Mean anomaly:     274
2216  deg
Mean motion:   15
54285682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              329


Coasting Arc #11 (Orbit 2869)
---------------------------------------

Vector Time (GMT): 2017/212/22:00:48
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6684664
64                 A    =         6788836
08  meter
 Y    =        1057271
71  meter          E    =           
0015577
 Z    =        -473503
42                 I    =           51
68767
 XDOT =      -1147
902905                 Wp   =           59
59578
 YDOT =      -4642
825593  meter/sec      RA   =          174
18121  deg
 ZDOT =       5993
253125                 TA   =          295
30102
                                          MA   =          295
46232
                                          Ha   =            223
001  n
mi
                                          Hp   =            212
237

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21931314
44                 X    =        -6693690
49
 Y    =        3468739
19  feet           Y    =          982468
80  meter
 Z    =       -1553488
92                 Z    =         -505997
08
 XDOT =      -3766
085645                 XDOT =       -1125
012344
 YDOT =     -15232
367432  feet/sec       YDOT =       -4655
534475  meter/sec
 ZDOT =      19662
903953                 ZDOT =        5987
732423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6872582
73                 X    =        -2094763
22
 Y    =      -21102479
04  feet           Y    =        -6432035
61  meter
 Z    =       -1697355
98                 Z    =         -517354
10
 XDOT =      12889
877216                 XDOT =        3928
834575
 YDOT =      -5740
243064  feet/sec       YDOT =       -1749
626086  meter/sec
 ZDOT =      19639
142583                 ZDOT =        5986
010659


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   17212
91822225  
00016717  00000-0  10270-3 0  9102
2 25544  51
6359 175
3423 0006101  92
3582 267
8269 15
54257915 28704


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
91822225   =   yrday
fracday
Element set:     910
Inclination:       51
6359  deg
RA of node:       175
3423  deg
Eccentricity:     
0006101     
Arg of perigee:    92
3582  deg
Mean anomaly:     267
8269  deg
Mean motion:   15
54257915  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2870
Checksum:              310


Coasting Arc #12 (Orbit 2870)
---------------------------------------

Vector Time (GMT): 2017/212/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2678566
65                 A    =         6779385
55  meter
 Y    =        4057418
41  meter          E    =           
0017148
 Z    =       -4740914
50                 I    =           51
65936
 XDOT =      -7004
169832                 Wp   =          103
90252
 YDOT =      -1429
201916  meter/sec      RA   =          173
89633  deg
 ZDOT =       2738
431574                 TA   =          193
21008
                                          MA   =          193
25504
                                          Ha   =            223
049  n
mi
                                          Hp   =            212
125

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8787948
32                 X    =        -2700709
84
 Y    =       13311740
18  feet           Y    =         4027341
24  meter
 Z    =      -15554181
45                 Z    =        -4753979
67
 XDOT =     -22979
559817                 XDOT =       -7000
969409
 YDOT =      -4688
982663  feet/sec       YDOT =       -1507
509519  meter/sec
 ZDOT =       8984
355558                 ZDOT =        2704
415468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15842533
32                 X    =        -4828804
15
 Y    =       -1275025
15  feet           Y    =         -388627
67  meter
 Z    =      -15612542
13                 Z    =        -4758702
84
 XDOT =      -6975
752886                 XDOT =       -2126
209480
 YDOT =     -21324
765203  feet/sec       YDOT =       -6499
788434  meter/sec
 ZDOT =       8834
105278                 ZDOT =        2692
635289


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   17212
98251949  
00016717  00000-0  10270-3 0  9119
2 25544  51
6374 175
0215 0006177  93
7769 266
4090 15
54256638 28711


Satellite: ISS
Catalog Number: 25544
Epoch time:      17212
98251949   =   yrday
fracday
Element set:     911
Inclination:       51
6374  deg
RA of node:       175
0215  deg
Eccentricity:     
0006177     
Arg of perigee:    93
7769  deg
Mean anomaly:     266
4090  deg
Mean motion:   15
54256638  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2871
Checksum:              334


Coasting Arc #13 (Orbit 2886)
---------------------------------------

Vector Time (GMT): 2017/213/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4253793
63                 A    =         6783173
08  meter
 Y    =       -3786677
72  meter          E    =           
0017787
 Z    =        3669532
42                 I    =           51
70448
 XDOT =       5866
355214                 Wp   =           89
62930
 YDOT =       2353
180463  meter/sec      RA   =          168
90778  deg
 ZDOT =      -4353
760755                 TA   =           46
72970
                                          MA   =           46
58143
                                          Ha   =            222
980  n
mi
                                          Hp   =            212
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13956015
84                 X    =         4277996
48
 Y    =      -12423483
34  feet           Y    =        -3738973
77  meter
 Z    =       12039148
37                 Z    =         3690254
45
 XDOT =      19246
572224                 XDOT =        5860
753580
 YDOT =       7720
408343  feet/sec       YDOT =        2418
750931  meter/sec
 ZDOT =     -14283
991978                 ZDOT =       -4325
277553

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17646427
82                 X    =         5378631
20
 Y    =        5957207
64  feet           Y    =         1815756
89  meter
 Z    =       12131350
80                 Z    =         3697635
72
 XDOT =       3243
407622                 XDOT =         988
590643
 YDOT =      19346
159608  feet/sec       YDOT =        5896
709449  meter/sec
 ZDOT =     -14158
328068                 ZDOT =       -4315
458395


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   17214
01126319  
00016717  00000-0  10270-3 0  9128
2 25544  51
6375 169
8909 0006148  97
7873 262
3978 15
54249035 28871


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
01126319   =   yrday
fracday
Element set:     912
Inclination:       51
6375  deg
RA of node:       169
8909  deg
Eccentricity:     
0006148     
Arg of perigee:    97
7873  deg
Mean anomaly:     262
3978  deg
Mean motion:   15
54249035  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2887
Checksum:              343


Coasting Arc #14 (Orbit 2901)
---------------------------------------

Vector Time (GMT): 2017/214/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5431698
43                 A    =         6786707
46  meter
 Y    =        3400253
60  meter          E    =           
0010688
 Z    =       -2237893
54                 I    =           51
74954
 XDOT =      -4276
388857                 Wp   =           73
31834
 YDOT =      -3251
183330  meter/sec      RA   =          163
93384  deg
 ZDOT =       5464
175119                 TA   =          261
85784
                                          MA   =          261
97909
                                          Ha   =            222
994  n
mi
                                          Hp   =            212
161

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17820532
90                 X    =        -5458446
80
 Y    =       11155687
67  feet           Y    =         3339363
23  meter
 Z    =       -7342170
41                 Z    =        -2264343
55
 XDOT =     -14030
147169                 XDOT =       -4266
257441
 YDOT =     -10666
611975  feet/sec       YDOT =       -3298
948482  meter/sec
 ZDOT =      17927
083725                 ZDOT =        5443
426384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18631018
47                 X    =        -5678734
43
 Y    =       -9652286
64  feet           Y    =        -2942016
97  meter
 Z    =       -7459674
26                 Z    =        -2273708
72
 XDOT =       1306
119596                 XDOT =         398
105253
 YDOT =     -16243
904698  feet/sec       YDOT =       -4951
142152  meter/sec
 ZDOT =      17835
749586                 ZDOT =        5436
336474


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   17214
97570485  
00016717  00000-0  10270-3 0  9131
2 25544  51
6387 165
0826 0006196 100
3813 259
8038 15
54274209 29025


Satellite: ISS
Catalog Number: 25544
Epoch time:      17214
97570485   =   yrday
fracday
Element set:     913
Inclination:       51
6387  deg
RA of node:       165
0826  deg
Eccentricity:     
0006196     
Arg of perigee:   100
3813  deg
Mean anomaly:     259
8038  deg
Mean motion:   15
54274209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2902
Checksum:              320


Coasting Arc #15 (Orbit 2917)
---------------------------------------

Vector Time (GMT): 2017/215/23:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6158890
54                 A    =         6788755
18  meter
 Y    =       -2792375
16  meter          E    =           
0018754
 Z    =         503268
09                 I    =           51
78667
 XDOT =       2382
041228                 Wp   =          121
76648
 YDOT =       4144
746513  meter/sec      RA   =          158
96999  deg
 ZDOT =      -5999
609296                 TA   =           52
81339
                                          MA   =           52
64233
                                          Ha   =            222
972  n
mi
                                          Hp   =            212
214

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20206333
80                 X    =         6187213
28
 Y    =       -9161335
84  feet           Y    =        -2723343
93  meter
 Z    =        1651142
04                 Z    =          533254
31
 XDOT =       7815
095891                 XDOT =        2364
659320
 YDOT =      13598
249714  feet/sec       YDOT =        4171
287292  meter/sec
 ZDOT =     -19683
757532                 ZDOT =       -5988
080193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18359330
37                 X    =         5595923
90
 Y    =       12437998
26  feet           Y    =         3791101
87  meter
 Z    =        1784224
72                 Z    =          543831
69
 XDOT =      -6539
532349                 XDOT =       -1993
249460
 YDOT =      12536
369314  feet/sec       YDOT =        3821
085367  meter/sec
 ZDOT =     -19633
334451                 ZDOT =       -5984
240341


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   17216
00443901  
00016717  00000-0  10270-3 0  9140
2 25544  51
6379 159
9529 0006117 104
5750 255
6082 15
54284109 29187


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
00443901   =   yrday
fracday
Element set:     914
Inclination:       51
6379  deg
RA of node:       159
9529  deg
Eccentricity:     
0006117     
Arg of perigee:   104
5750  deg
Mean anomaly:     255
6082  deg
Mean motion:   15
54284109  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2918
Checksum:              311


Coasting Arc #16 (Orbit 2919)
---------------------------------------

Vector Time (GMT): 2017/216/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         802029
16                 A    =         6777085
47  meter
 Y    =        4174557
15  meter          E    =           
0020534
 Z    =       -5295986
93                 I    =           51
75384
 XDOT =      -7265
855246                 Wp   =           98
05876
 YDOT =       2297
394031  meter/sec      RA   =          158
24123  deg
 ZDOT =        710
123062                 TA   =          178
72883
                                          MA   =          178
72360
                                          Ha   =            222
914  n
mi
                                          Hp   =            212
325

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2631329
25                 X    =          781013
51
 Y    =       13696053
66  feet           Y    =         4183408
80  meter
 Z    =      -17375285
21                 Z    =        -5292141
76
 XDOT =     -23838
107761                 XDOT =       -7294
454686
 YDOT =       7537
381990  feet/sec       YDOT =        2215
982348  meter/sec
 ZDOT =       2329
800072                 ZDOT =         674
758934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1420441
96                 X    =          432950
71
 Y    =       13894546
07  feet           Y    =         4235057
64  meter
 Z    =      -17358866
60                 Z    =        -5290982
54
 XDOT =     -23452
058021                 XDOT =       -7148
187285
 YDOT =       5114
124349  feet/sec       YDOT =        1558
785101  meter/sec
 ZDOT =       2172
988176                 ZDOT =         662
326796


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   17216
13302956  
00016717  00000-0  10270-3 0  9159
2 25544  51
6398 159
3148 0005936 103
7973 256
3840 15
54273591 29201


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
13302956   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:       159
3148  deg
Eccentricity:     
0005936     
Arg of perigee:   103
7973  deg
Mean anomaly:     256
3840  deg
Mean motion:   15
54273591  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2920
Checksum:              324


Coasting Arc #17 (Orbit 2935)
---------------------------------------

Vector Time (GMT): 2017/217/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         953608
27                 A    =         6778996
80  meter
 Y    =       -4697566
87  meter          E    =           
0012176
 Z    =        4783910
08                 I    =           51
79190
 XDOT =       7098
653278                 Wp   =           81
72284
 YDOT =      -1252
756196  meter/sec      RA   =          153
25097  deg
 ZDOT =      -2637
728229                 TA   =           34
25016
                                          MA   =           34
17169
                                          Ha   =            222
773  n
mi
                                          Hp   =            212
294

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3128636
04                 X    =          982829
31
 Y    =      -15411964
79  feet           Y    =        -4686739
86  meter
 Z    =       15695243
03                 Z    =         4788613
04
 XDOT =      23289
544876                 XDOT =        7124
946928
 YDOT =      -4110
092507  feet/sec       YDOT =       -1173
227065  meter/sec
 ZDOT =      -8653
964006                 ZDOT =       -2603
181935

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4228715
14                 X    =         1288912
38
 Y    =      -15124816
76  feet           Y    =        -4610044
15  meter
 Z    =       15716728
74                 Z    =         4790458
92
 XDOT =      22493
839822                 XDOT =        6856
122378
 YDOT =      -2569
902544  feet/sec       YDOT =        -783
306295  meter/sec
 ZDOT =      -8500
897743                 ZDOT =       -2591
073632


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   17217
16175704  
00016717  00000-0  10270-3 0  9163
2 25544  51
6408 154
1850 0005832 107
4212 252
7572 15
54325039 29362


Satellite: ISS
Catalog Number: 25544
Epoch time:      17217
16175704   =   yrday
fracday
Element set:     916
Inclination:       51
6408  deg
RA of node:       154
1850  deg
Eccentricity:     
0005832     
Arg of perigee:   107
4212  deg
Mean anomaly:     252
7572  deg
Mean motion:   15
54325039  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2936
Checksum:              299


Coasting Arc #18 (Orbit 2950)
---------------------------------------

Vector Time (GMT): 2017/218/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2521496
52                 A    =         6782675
25  meter
 Y    =        5048420
44  meter          E    =           
0012035
 Z    =       -3776003
36                 I    =           51
83248
 XDOT =      -6364
770632                 Wp   =          107
21684
 YDOT =           
198151  meter/sec      RA   =          148
27230  deg
 ZDOT =       4258
187255                 TA   =          207
76375
                                          MA   =          207
82804
                                          Ha   =            222
835  n
mi
                                          Hp   =            212
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8272626
36                 X    =        -2559420
26
 Y    =       16563059
19  feet           Y    =         5020011
48  meter
 Z    =      -12388462
48                 Z    =        -3788343
66
 XDOT =     -20881
793413                 XDOT =       -6384
983606
 YDOT =           
650101  feet/sec       YDOT =         -71
090254  meter/sec
 ZDOT =      13970
430628                 ZDOT =        4227
220655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9194493
04                 X    =        -2802481
48
 Y    =       16026797
72  feet           Y    =         4884967
94  meter
 Z    =      -12443806
97                 Z    =        -3792872
36
 XDOT =     -19764
554868                 XDOT =       -6024
236324
 YDOT =       -617
679608  feet/sec       YDOT =        -188
268744  meter/sec
 ZDOT =      13833
367056                 ZDOT =        4216
410279


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   17218
12618579  
00016717  00000-0  10270-3 0  9173
2 25544  51
6404 149
3769 0006032 110
2853 249
8949 15
54322268 29512


Satellite: ISS
Catalog Number: 25544
Epoch time:      17218
12618579   =   yrday
fracday
Element set:     917
Inclination:       51
6404  deg
RA of node:       149
3769  deg
Eccentricity:     
0006032     
Arg of perigee:   110
2853  deg
Mean anomaly:     249
8949  deg
Mean motion:   15
54322268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2951
Checksum:              329


Coasting Arc #19 (Orbit 2966)
---------------------------------------

Vector Time (GMT): 2017/219/02:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3819154
27                 A    =         6786444
47  meter
 Y    =       -5101982
39  meter          E    =           
0019754
 Z    =        2304669
05                 I    =           51
87242
 XDOT =       5219
501296                 Wp   =          109
12451
 YDOT =       1435
424759  meter/sec      RA   =          143
30619  deg
 ZDOT =      -5440
126798                 TA   =           45
26116
                                          MA   =           45
10054
                                          Ha   =            222
766  n
mi
                                          Hp   =            212
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12530033
70                 X    =         3864727
42
 Y    =      -16738787
36  feet           Y    =        -5059019
26  meter
 Z    =        7561250
17                 Z    =         2323331
48
 XDOT =      17124
348084                 XDOT =        5229
487004
 YDOT =       4709
398814  feet/sec       YDOT =        1493
848768  meter/sec
 ZDOT =     -17848
185032                 ZDOT =       -5414
748298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13209971
80                 X    =         4026399
40
 Y    =      -16168427
03  feet           Y    =        -4928136
56  meter
 Z    =        7644597
00                 Z    =         2330073
17
 XDOT =      15836
213062                 XDOT =        4826
877741
 YDOT =       4504
244673  feet/sec       YDOT =        1372
893776  meter/sec
 ZDOT =     -17736
047502                 ZDOT =       -5405
947279


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   17219
15490358  
00016717  00000-0  10270-3 0  9181
2 25544  51
6405 144
2478 0005953 112
7017 247
4766 15
54330121 29679


Satellite: ISS
Catalog Number: 25544
Epoch time:      17219
15490358   =   yrday
fracday
Element set:     918
Inclination:       51
6405  deg
RA of node:       144
2478  deg
Eccentricity:     
0005953     
Arg of perigee:   112
7017  deg
Mean anomaly:     247
4766  deg
Mean motion:   15
54330121  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2967
Checksum:              314


Coasting Arc #20 (Orbit 2968)
---------------------------------------

Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -46014
46                 A    =         6778795
22  meter
 Y    =       -4740199
46  meter          E    =           
0011941
 Z    =        4835898
70                 I    =           51
84916
 XDOT =       6748
371195                 Wp   =           84
25664
 YDOT =      -2647
495972  meter/sec      RA   =          142
70355  deg
 ZDOT =      -2524
384524                 TA   =           30
49876
                                          MA   =           30
42937
                                          Ha   =            222
892  n
mi
                                          Hp   =            212
216

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -150966
09                 X    =          -16494
82
 Y    =      -15551835
51  feet           Y    =        -4740549
11  meter
 Z    =       15865809
37                 Z    =         4835746
74
 XDOT =      22140
325444                 XDOT =        6789
736616
 YDOT =      -8686
010407  feet/sec       YDOT =       -2571
799739  meter/sec
 ZDOT =      -8282
101456                 ZDOT =       -2491
503306

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10460651
44                 X    =        -3188406
56
 Y    =      -11508990
80  feet           Y    =        -3507940
40  meter
 Z    =       15865818
22                 Z    =         4835901
39
 XDOT =      10090
406696                 XDOT =        3075
555961
 YDOT =     -20416
892294  feet/sec       YDOT =       -6223
068771  meter/sec
 ZDOT =      -8136
162448                 ZDOT =       -2479
902314


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   17219
28349288  
00016717  00000-0  10270-3 0  9191
2 25544  51
6396 143
6074 0006157 111
8770 248
3038 15
54329823 29697


Satellite: ISS
Catalog Number: 25544
Epoch time:      17219
28349288   =   yrday
fracday
Element set:     919
Inclination:       51
6396  deg
RA of node:       143
6074  deg
Eccentricity:     
0006157     
Arg of perigee:   111
8770  deg
Mean anomaly:     248
3038  deg
Mean motion:   15
54329823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2969
Checksum:              342


Coasting Arc #21 (Orbit 2983)
---------------------------------------

Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1446275
67                 A    =         6782477
38  meter
 Y    =        5400226
14  meter          E    =           
0012327
 Z    =       -3853819
90                 I    =           51
88775
 XDOT =      -6288
254996                 Wp   =          110
38967
 YDOT =       1290
473982  meter/sec      RA   =          137
72799  deg
 ZDOT =       4174
800706                 TA   =          203
44425
                                          MA   =          203
50050
                                          Ha   =            222
834  n
mi
                                          Hp   =            212
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4744998
93                 X    =        -1487835
36
 Y    =       17717277
38  feet           Y    =         5383820
57  meter
 Z    =      -12643766
07                 Z    =        -3860946
20
 XDOT =     -20630
757862                 XDOT =       -6322
496776
 YDOT =       4233
838525  feet/sec       YDOT =        1219
962942  meter/sec
 ZDOT =      13696
852709                 ZDOT =        4144
171795

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8479148
28                 X    =         2584444
40
 Y    =       16238917
13  feet           Y    =         4949621
94  meter
 Z    =      -12676094
34                 Z    =        -3863673
55
 XDOT =     -11286
444109                 XDOT =       -3440
108164
 YDOT =      16462
056597  feet/sec       YDOT =        5017
634851  meter/sec
 ZDOT =      13561
063928                 ZDOT =        4133
412285


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   17220
24791021  
00016717  00000-0  10270-3 0  9207
2 25544  51
6407 138
7993 0006065 115
2830 244
8952 15
54311882 29847


Satellite: ISS
Catalog Number: 25544
Epoch time:      17220
24791021   =   yrday
fracday
Element set:     920
Inclination:       51
6407  deg
RA of node:       138
7993  deg
Eccentricity:     
0006065     
Arg of perigee:   115
2830  deg
Mean anomaly:     244
8952  deg
Mean motion:   15
54311882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2984
Checksum:              308
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