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

 
Date: July 10th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 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


200/11:54:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 212 7

201/17:45:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 212 7

Coasting Arc #1 (Orbit 2536)
---------------------------------------

Vector Time (GMT): 2017/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1445369
59                 A    =         6784971
04  meter
 Y    =       -5811261
57  meter          E    =           
0008452
 Z    =       -3188186
11                 I    =           51
28105
 XDOT =       4659
336105                 Wp   =           44
55155
 YDOT =      -3772
308059  meter/sec      RA   =          281
29901  deg
 ZDOT =       4777
287013                 TA   =          278
41188
                                          MA   =          278
50768
                                          Ha   =            222
164  n
mi
                                          Hp   =            213
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4742026
23                 X    =        -1364792
70
 Y    =      -19065818
80  feet           Y    =        -5826973
76  meter
 Z    =      -10459928
18                 Z    =        -3195012
16
 XDOT =      15286
535779                 XDOT =        4677
967378
 YDOT =     -12376
338776  feet/sec       YDOT =       -3720
100605  meter/sec
 ZDOT =      15673
513823                 ZDOT =        4799
965098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16736361
04                 X    =        -5101242
84
 Y    =       10260444
87  feet           Y    =         3127383
60  meter
 Z    =      -10489034
62                 Z    =        -3197057
75
 XDOT =     -15664
459430                 XDOT =       -4774
527234
 YDOT =      -9471
030311  feet/sec       YDOT =       -2886
770039  meter/sec
 ZDOT =      15774
284318                 ZDOT =        4808
001860


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   17191
50660012  
00016717  00000-0  10270-3 0  9006
2 25544  51
6422 282
0934 0005386  15
6589 344
4729 15
54135393 25375


Satellite: ISS
Catalog Number: 25544
Epoch time:      17191
50660012   =   yrday
fracday
Element set:     900
Inclination:       51
6422  deg
RA of node:       282
0934  deg
Eccentricity:     
0005386     
Arg of perigee:    15
6589  deg
Mean anomaly:     344
4729  deg
Mean motion:   15
54135393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2537
Checksum:              305


Coasting Arc #2 (Orbit 2552)
---------------------------------------

Vector Time (GMT): 2017/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         601929
88                 A    =         6788126
93  meter
 Y    =        6554688
59  meter          E    =           
0014475
 Z    =        1643497
28                 I    =           51
28517
 XDOT =      -4791
148998                 Wp   =           94
47007
 YDOT =       1875
853667  meter/sec      RA   =          276
29839  deg
 ZDOT =      -5684
346043                 TA   =           67
44249
                                          MA   =           67
28937
                                          Ha   =            222
295  n
mi
                                          Hp   =            213
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1974835
58                 X    =          520605
72
 Y    =       21504883
84  feet           Y    =         6560964
90  meter
 Z    =        5392051
43                 Z    =         1646224
39
 XDOT =     -15718
992774                 XDOT =       -4784
157874
 YDOT =       6154
375548  feet/sec       YDOT =        1822
315475  meter/sec
 ZDOT =     -18649
429276                 ZDOT =       -5707
602420

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19744581
40                 X    =         6018148
41
 Y    =       -8740357
13  feet           Y    =        -2664060
85  meter
 Z    =        5402951
55                 Z    =         1646819
63
 XDOT =      10196
442213                 XDOT =        3107
875586
 YDOT =      11356
293520  feet/sec       YDOT =        3461
398265  meter/sec
 ZDOT =     -18752
416723                 ZDOT =       -5715
736617


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   17192
53542046  
00016717  00000-0  10270-3 0  9017
2 25544  51
6411 276
9652 0005403  21
2354 338
9022 15
54147215 25533


Satellite: ISS
Catalog Number: 25544
Epoch time:      17192
53542046   =   yrday
fracday
Element set:     901
Inclination:       51
6411  deg
RA of node:       276
9652  deg
Eccentricity:     
0005403     
Arg of perigee:    21
2354  deg
Mean anomaly:     338
9022  deg
Mean motion:   15
54147215  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2553
Checksum:              284


Coasting Arc #3 (Orbit 2568)
---------------------------------------

Vector Time (GMT): 2017/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         180848
12                 A    =         6789333
87  meter
 Y    =       -6777576
96  meter          E    =           
0017438
 Z    =          33286
12                 I    =           51
28615
 XDOT =       4796
084550                 Wp   =           38
94247
 YDOT =        165
712817  meter/sec      RA   =          271
30301  deg
 ZDOT =       5986
681843                 TA   =          321
41803
                                          MA   =          321
54252
                                          Ha   =            222
387  n
mi
                                          Hp   =            213
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         593333
73                 X    =          256461
65
 Y    =      -22236144
87  feet           Y    =        -6775131
81  meter
 Z    =         109206
44                 Z    =           34347
67
 XDOT =      15735
185533                 XDOT =        4764
795152
 YDOT =        543
677221  feet/sec       YDOT =         219
170413  meter/sec
 ZDOT =      19641
344628                 ZDOT =        6009
903388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21133246
22                 X    =        -6441413
45
 Y    =        6941381
51  feet           Y    =         2115733
09  meter
 Z    =         115050
69                 Z    =           35067
45
 XDOT =      -4243
690639                 XDOT =       -1293
476907
 YDOT =     -13334
897080  feet/sec       YDOT =       -4064
476630  meter/sec
 ZDOT =      19743
827883                 ZDOT =        6017
918739


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   17193
56423760  
00016717  00000-0  10270-3 0  9023
2 25544  51
6409 271
8366 0005545  23
8358 336
3051 15
54128649 25696


Satellite: ISS
Catalog Number: 25544
Epoch time:      17193
56423760   =   yrday
fracday
Element set:     902
Inclination:       51
6409  deg
RA of node:       271
8366  deg
Eccentricity:     
0005545     
Arg of perigee:    23
8358  deg
Mean anomaly:     336
3051  deg
Mean motion:   15
54128649  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2569
Checksum:              323


Coasting Arc #4 (Orbit 2583)
---------------------------------------

Vector Time (GMT): 2017/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -988887
05                 A    =         6787913
63  meter
 Y    =        6483993
17  meter          E    =           
0007275
 Z    =       -1751832
22                 I    =           51
28139
 XDOT =      -4677
419056                 Wp   =           97
90896
 YDOT =      -2232
268807  meter/sec      RA   =          266
30748  deg
 ZDOT =      -5643
049663                 TA   =          101
40409
                                          MA   =          101
32236
                                          Ha   =            222
425  n
mi
                                          Hp   =            213
451

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3244380
10                 X    =        -1052809
86
 Y    =       21272943
48  feet           Y    =         6472577
48  meter
 Z    =       -5747481
03                 Z    =        -1756790
65
 XDOT =     -15345
863045                 XDOT =       -4624
698835
 YDOT =      -7323
716559  feet/sec       YDOT =       -2284
279700  meter/sec
 ZDOT =     -18513
942464                 ZDOT =       -5665
642902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21033025
23                 X    =         6410866
09
 Y    =       -4517886
25  feet           Y    =        -1377051
73  meter
 Z    =       -5770460
82                 Z    =        -1758836
46
 XDOT =      -1801
822758                 XDOT =        -549
195577
 YDOT =      15297
030959  feet/sec       YDOT =        4662
535036  meter/sec
 ZDOT =     -18613
308416                 ZDOT =       -5673
336405


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   17194
52874805  
00016717  00000-0  10270-3 0  9031
2 25544  51
6402 267
0285 0005511  27
8110 332
3337 15
54162310 25842


Satellite: ISS
Catalog Number: 25544
Epoch time:      17194
52874805   =   yrday
fracday
Element set:     903
Inclination:       51
6402  deg
RA of node:       267
0285  deg
Eccentricity:     
0005511     
Arg of perigee:    27
8110  deg
Mean anomaly:     332
3337  deg
Mean motion:   15
54162310  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2584
Checksum:              287


Coasting Arc #5 (Orbit 2599)
---------------------------------------

Vector Time (GMT): 2017/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1764978
44                 A    =         6784681
93  meter
 Y    =       -5679024
38  meter          E    =           
0016494
 Z    =        3246299
39                 I    =           51
27372
 XDOT =       4456
726451                 Wp   =           71
14015
 YDOT =       4092
743224  meter/sec      RA   =          261
30496  deg
 ZDOT =       4722
237784                 TA   =          326
75106
                                          MA   =          326
85458
                                          Ha   =            222
425  n
mi
                                          Hp   =            213
327

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5790611
69                 X    =         1812582
87
 Y    =      -18631969
75  feet           Y    =        -5659021
21  meter
 Z    =       10650588
56                 Z    =         3254988
29
 XDOT =      14621
805943                 XDOT =        4387
691043
 YDOT =      13427
635250  feet/sec       YDOT =        4142
195081  meter/sec
 ZDOT =      15492
906114                 ZDOT =        4743
719498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19426463
90                 X    =        -5921186
20
 Y    =        1566941
44  feet           Y    =          477603
75  meter
 Z    =       10689888
30                 Z    =         3258277
95
 XDOT =       7228
941396                 XDOT =        2203
381338
 YDOT =     -17037
490618  feet/sec       YDOT =       -5193
027140  meter/sec
 ZDOT =      15587
065992                 ZDOT =        4750
937715


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   17195
55755595  
00016717  00000-0  10270-3 0  9040
2 25544  51
6402 261
8993 0005588  31
5106 328
6380 15
54177095 26002


Satellite: ISS
Catalog Number: 25544
Epoch time:      17195
55755595   =   yrday
fracday
Element set:     904
Inclination:       51
6402  deg
RA of node:       261
8993  deg
Eccentricity:     
0005588     
Arg of perigee:    31
5106  deg
Mean anomaly:     328
6380  deg
Mean motion:   15
54177095  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2600
Checksum:              326


Coasting Arc #6 (Orbit 2614)
---------------------------------------

Vector Time (GMT): 2017/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2570193
25                 A    =         6780877
60  meter
 Y    =        4458683
80  meter          E    =           
0014236
 Z    =       -4430073
91                 I    =           51
26578
 XDOT =      -4068
685438                 Wp   =           56
88917
 YDOT =      -5598
406480  meter/sec      RA   =          256
29309  deg
 ZDOT =      -3274
073974                 TA   =          179
86607
                                          MA   =          179
86569
                                          Ha   =            222
589  n
mi
                                          Hp   =            213
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8432392
55                 X    =        -2598341
46
 Y    =       14628227
70  feet           Y    =         4429785
02  meter
 Z    =      -14534363
23                 Z    =        -4442627
13
 XDOT =     -13348
705506                 XDOT =       -3989
876477
 YDOT =     -18367
475329  feet/sec       YDOT =       -5643
464454  meter/sec
 ZDOT =     -10741
712513                 ZDOT =       -3293
647121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16710060
34                 X    =         5093226
39
 Y    =        2056410
53  feet           Y    =          626793
93  meter
 Z    =      -14590512
79                 Z    =        -4447188
30
 XDOT =     -11682
770553                 XDOT =       -3560
908465
 YDOT =      18112
663001  feet/sec       YDOT =        5520
739683  meter/sec
 ZDOT =     -10827
213342                 ZDOT =       -3300
134627


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   17196
52206324  
00016717  00000-0  10270-3 0  9050
2 25544  51
6392 257
0914 0005601  35
6521 324
5005 15
54159680 26157


Satellite: ISS
Catalog Number: 25544
Epoch time:      17196
52206324   =   yrday
fracday
Element set:     905
Inclination:       51
6392  deg
RA of node:       257
0914  deg
Eccentricity:     
0005601     
Arg of perigee:    35
6521  deg
Mean anomaly:     324
5005  deg
Mean motion:   15
54159680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2615
Checksum:              291


Coasting Arc #7 (Orbit 2630)
---------------------------------------

Vector Time (GMT): 2017/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3342629
77                 A    =         6777932
69  meter
 Y    =       -2920483
37  meter          E    =           
0007563
 Z    =        5115519
17                 I    =           51
26548
 XDOT =       3522
427755                 Wp   =           76
97621
 YDOT =       6652
233140  meter/sec      RA   =          251
27129  deg
 ZDOT =       1495
952106                 TA   =          358
55184
                                          MA   =          358
55403
                                          Ha   =            222
472  n
mi
                                          Hp   =            213
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10966633
10                 X    =         3350190
39
 Y    =       -9581638
34  feet           Y    =        -2883061
84  meter
 Z    =       16783199
38                 Z    =         5131774
74
 XDOT =      11556
521505                 XDOT =        3440
512372
 YDOT =      21824
911875  feet/sec       YDOT =        6691
165213  meter/sec
 ZDOT =       4907
979350                 ZDOT =        1512
864320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13130887
70                 X    =        -4002294
57
 Y    =       -6101189
64  feet           Y    =        -1859642
60  meter
 Z    =       16855440
94                 Z    =         5137538
40
 XDOT =      14923
747073                 XDOT =        4548
758108
 YDOT =     -18354
565621  feet/sec       YDOT =       -5594
471601  meter/sec
 ZDOT =       4981
576940                 ZDOT =        1518
384651


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   17197
55086521  
00016717  00000-0  10270-3 0  9060
2 25544  51
6397 251
9622 0005656  38
2758 321
8796 15
54187486 26312


Satellite: ISS
Catalog Number: 25544
Epoch time:      17197
55086521   =   yrday
fracday
Element set:     906
Inclination:       51
6397  deg
RA of node:       251
9622  deg
Eccentricity:     
0005656     
Arg of perigee:    38
2758  deg
Mean anomaly:     321
8796  deg
Mean motion:   15
54187486  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2631
Checksum:              346


Coasting Arc #8 (Orbit 2645)
---------------------------------------

Vector Time (GMT): 2017/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4080122
19                 A    =         6777335
54  meter
 Y    =        1244658
80  meter          E    =           
0018946
 Z    =       -5282437
48                 I    =           51
27494
 XDOT =      -2747
255106                 Wp   =           79
50382
 YDOT =      -7131
053132  meter/sec      RA   =          246
24542  deg
 ZDOT =        446
486341                 TA   =          194
75604
                                          MA   =          194
81142
                                          Ha   =            222
741  n
mi
                                          Hp   =            212
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13386227
66                 X    =        -4068077
63
 Y    =        4083526
26  feet           Y    =         1199099
83  meter
 Z    =      -17330831
64                 Z    =        -5302228
06
 XDOT =      -9013
304152                 XDOT =       -2669
478414
 YDOT =     -23395
843608  feet/sec       YDOT =       -7161
339959  meter/sec
 ZDOT =       1464
850201                 ZDOT =         433
329461

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9243445
40                 X    =         2817402
16
 Y    =       10362508
61  feet           Y    =         3158492
62  meter
 Z    =      -17418413
69                 Z    =        -5309132
49
 XDOT =     -16748
757623                 XDOT =       -5105
021324
 YDOT =      17280
472633  feet/sec       YDOT =        5267
088058  meter/sec
 ZDOT =       1407
894703                 ZDOT =         429
126306


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   17198
51536576  
00016717  00000-0  10270-3 0  9078
2 25544  51
6401 247
1539 0005830  41
5465 318
6130 15
54157640 26469


Satellite: ISS
Catalog Number: 25544
Epoch time:      17198
51536576   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:       247
1539  deg
Eccentricity:     
0005830     
Arg of perigee:    41
5465  deg
Mean anomaly:     318
6130  deg
Mean motion:   15
54157640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2646
Checksum:              311


Coasting Arc #9 (Orbit 2661)
---------------------------------------

Vector Time (GMT): 2017/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4698754
24                 A    =         6778950
50  meter
 Y    =         468850
58  meter          E    =           
0012521
 Z    =        4857895
02                 I    =           51
29410
 XDOT =       1740
664460                 Wp   =           52
82737
 YDOT =       7091
543807  meter/sec      RA   =          241
22250  deg
 ZDOT =      -2356
425422                 TA   =           60
41047
                                          MA   =           60
28577
                                          Ha   =            222
601  n
mi
                                          Hp   =            212
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15415860
37                 X    =         4669564
99
 Y    =        1538223
69  feet           Y    =          521231
60  meter
 Z    =       15937975
78                 Z    =         4880649
21
 XDOT =       5710
841405                 XDOT =        1672
681913
 YDOT =      23266
219839  feet/sec       YDOT =        7110
629193  meter/sec
 ZDOT =      -7731
054533                 ZDOT =       -2348
134321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5233198
14                 X    =        -1595078
79
 Y    =      -14471281
94  feet           Y    =        -4410846
73  meter
 Z    =       16038378
69                 Z    =         4888497
83
 XDOT =      17430
737508                 XDOT =        5312
888792
 YDOT =     -14874
404239  feet/sec       YDOT =       -4533
718412  meter/sec
 ZDOT =      -7695
564021                 ZDOT =       -2345
607914


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   17199
54416236  
00016717  00000-0  10270-3 0  9083
2 25544  51
6393 242
0256 0005834  45
5056 314
6573 15
54205935 26629


Satellite: ISS
Catalog Number: 25544
Epoch time:      17199
54416236   =   yrday
fracday
Element set:     908
Inclination:       51
6393  deg
RA of node:       242
0256  deg
Eccentricity:     
0005834     
Arg of perigee:    45
5056  deg
Mean anomaly:     314
6573  deg
Mean motion:   15
54205935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2662
Checksum:              316


Coasting Arc #10 (Orbit 2676)
---------------------------------------

Vector Time (GMT): 2017/200/11:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4625309
27                 A    =         6778654
80  meter
 Y    =         234816
04  meter          E    =           
0016651
 Z    =       -4964200
92                 I    =           51
31002
 XDOT =      -2590
907237                 Wp   =           88
28194
 YDOT =      -6893
575912  meter/sec      RA   =          236
23525  deg
 ZDOT =       2094
552064                 TA   =          202
19888
                                          MA   =          202
27105
                                          Ha   =            222
831  n
mi
                                          Hp   =            212
681

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15174899
19                 X    =        -4603477
72
 Y    =         770393
85  feet           Y    =          183215
29  meter
 Z    =      -16286748
44                 Z    =        -4986616
12
 XDOT =      -8500
351827                 XDOT =       -2523
803162
 YDOT =     -22616
718870  feet/sec       YDOT =       -6922
174215  meter/sec
 ZDOT =       6871
889975                 ZDOT =        2082
128537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7118442
49                 X    =         2169701
27
 Y    =       13302758
66  feet           Y    =         4054680
84  meter
 Z    =      -16385775
39                 Z    =        -4994384
34
 XDOT =     -15846
095292                 XDOT =       -4829
889845
 YDOT =      16851
160657  feet/sec       YDOT =        5136
233768  meter/sec
 ZDOT =       6818
105644                 ZDOT =        2078
158600


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   17200
50865827  
00016717  00000-0  10270-3 0  9097
2 25544  51
6400 237
2169 0005932  48
7400 311
4263 15
54172544 26770


Satellite: ISS
Catalog Number: 25544
Epoch time:      17200
50865827   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       237
2169  deg
Eccentricity:     
0005932     
Arg of perigee:    48
7400  deg
Mean anomaly:     311
4263  deg
Mean motion:   15
54172544  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2677
Checksum:              301


Coasting Arc #11 (Orbit 2692)
---------------------------------------

Vector Time (GMT): 2017/201/11:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 901991
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5247325
90                 A    =         6781876
35  meter
 Y    =        1319559
32  meter          E    =           
0016175
 Z    =        4080104
10                 I    =           51
33962
 XDOT =       1334
378030                 Wp   =           67
95409
 YDOT =       6525
390212  meter/sec      RA   =          231
22058  deg
 ZDOT =      -3808
392509                 TA   =           61
59775
                                          MA   =           61
43480
                                          Ha   =            222
753  n
mi
                                          Hp   =            212
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17215636
17                 X    =         5212361
25
 Y    =        4329262
85  feet           Y    =         1378042
49  meter
 Z    =       13386168
31                 Z    =         4105509
04
 XDOT =       4377
880676                 XDOT =        1279
809394
 YDOT =      21408
760537  feet/sec       YDOT =        6540
007472  meter/sec
 ZDOT =     -12494
726081                 ZDOT =       -3802
042323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3681227
15                 X    =        -1122038
04
 Y    =      -17278833
93  feet           Y    =        -5266588
58  meter
 Z    =       13498170
70                 Z    =         4114242
43
 XDOT =      15975
552373                 XDOT =        4869
348363
 YDOT =     -13189
334785  feet/sec       YDOT =       -4020
109242  meter/sec
 ZDOT =     -12467
692528                 ZDOT =       -3800
152682


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   17201
53744816  
00016717  00000-0  10270-3 0  9107
2 25544  51
6394 232
0882 0006030  52
3158 307
8536 15
54220650 26930


Satellite: ISS
Catalog Number: 25544
Epoch time:      17201
53744816   =   yrday
fracday
Element set:     910
Inclination:       51
6394  deg
RA of node:       232
0882  deg
Eccentricity:     
0006030     
Arg of perigee:    52
3158  deg
Mean anomaly:     307
8536  deg
Mean motion:   15
54220650  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2693
Checksum:              291


Coasting Arc #12 (Orbit 2696)
---------------------------------------

Vector Time (GMT): 2017/201/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          73207
54                 A    =         6781253
17  meter
 Y    =       -5247364
48  meter          E    =           
0014100
 Z    =        4282126
40                 I    =           51
34163
 XDOT =       6147
915354                 Wp   =           87
18131
 YDOT =       2961
434436  meter/sec      RA   =          230
05041  deg
 ZDOT =       3514
525350                 TA   =          326
87658
                                          MA   =          326
96479
                                          Ha   =            222
787  n
mi
                                          Hp   =            212
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         240182
21                 X    =          111079
21
 Y    =      -17215762
72  feet           Y    =        -5246334
58  meter
 Z    =       14048971
12                 Z    =         4282573
37
 XDOT =      20170
325963                 XDOT =        6097
271189
 YDOT =       9715
992243  feet/sec       YDOT =        3029
901006  meter/sec
 ZDOT =      11530
594981                 ZDOT =        3544
267130

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6923120
84                 X    =         2110167
23
 Y    =       15761733
43  feet           Y    =         4804176
35  meter
 Z    =       14051758
62                 Z    =         4282976
03
 XDOT =     -21162
466247                 XDOT =       -6450
319712
 YDOT =      -1128
364037  feet/sec       YDOT =        -343
925359  meter/sec
 ZDOT =      11661
502376                 ZDOT =        3554
425924


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   17201
79464574  
00016717  00000-0  10270-3 0  9116
2 25544  51
6387 230
8064 0005938  51
9403 308
2285 15
54224183 26979


Satellite: ISS
Catalog Number: 25544
Epoch time:      17201
79464574   =   yrday
fracday
Element set:     911
Inclination:       51
6387  deg
RA of node:       230
8064  deg
Eccentricity:     
0005938     
Arg of perigee:    51
9403  deg
Mean anomaly:     308
2285  deg
Mean motion:   15
54224183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2697
Checksum:              319


Coasting Arc #13 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2017/202/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1464801
24                 A    =         6778206
32  meter
 Y    =        4272272
30  meter          E    =           
0019012
 Z    =       -5071565
21                 I    =           51
35227
 XDOT =      -6161
736688                 Wp   =           70
11369
 YDOT =      -4190
107885  meter/sec      RA   =          225
03533  deg
 ZDOT =      -1749
087171                 TA   =          182
86722
                                          MA   =          182
87814
                                          Ha   =            222
939  n
mi
                                          Hp   =            212
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4805778
34                 X    =        -1487831
20
 Y    =       14016641
42  feet           Y    =         4255763
75  meter
 Z    =      -16638993
47                 Z    =        -5078736
08
 XDOT =     -20215
671547                 XDOT =       -6105
927752
 YDOT =     -13747
073115  feet/sec       YDOT =       -4258
700349  meter/sec
 ZDOT =      -5738
474970                 ZDOT =       -1778
883542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1715498
46                 X    =         -522883
93
 Y    =      -14681341
88  feet           Y    =        -4474873
00  meter
 Z    =      -16671326
03                 Z    =        -5081420
17
 XDOT =      23039
615199                 XDOT =        7022
474713
 YDOT =       3976
513135  feet/sec       YDOT =        1212
041203  meter/sec
 ZDOT =      -5869
458893                 ZDOT =       -1789
011071


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   17202
75913572  
00016717  00000-0  10270-3 0  9121
2 25544  51
6381 225
9977 0006103  55
0477 305
1248 15
54203175 27123


Satellite: ISS
Catalog Number: 25544
Epoch time:      17202
75913572   =   yrday
fracday
Element set:     912
Inclination:       51
6381  deg
RA of node:       225
9977  deg
Eccentricity:     
0006103     
Arg of perigee:    55
0477  deg
Mean anomaly:     305
1248  deg
Mean motion:   15
54203175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              298


Coasting Arc #14 (Orbit 2727)
---------------------------------------

Vector Time (GMT): 2017/203/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2887560
95                 A    =         6777045
93  meter
 Y    =       -3092573
59  meter          E    =           
0008183
 Z    =        5287660
25                 I    =           51
37275
 XDOT =       5774
403884                 Wp   =           64
91512
 YDOT =       5051
766143  meter/sec      RA   =          220
01681  deg
 ZDOT =       -195
116316                 TA   =           26
97102
                                          MA   =           26
92851
                                          Ha   =            222
737  n
mi
                                          Hp   =            212
600

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9473625
15                 X    =         2896243
93
 Y    =      -10146238
82  feet           Y    =        -3060234
96  meter
 Z    =       17347966
70                 Z    =         5301707
62
 XDOT =      18944
894633                 XDOT =        5718
432302
 YDOT =      16574
035902  feet/sec       YDOT =        5116
026512  meter/sec
 ZDOT =       -640
145393                 ZDOT =        -167
201949

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3924494
62                 X    =        -1196185
96
 Y    =       13233312
67  feet           Y    =         4033513
70  meter
 Z    =       17410498
61                 Z    =         5306719
98
 XDOT =     -23351
816316                 XDOT =       -7117
633613
 YDOT =      -6228
620253  feet/sec       YDOT =       -1898
483453  meter/sec
 ZDOT =       -517
579391                 ZDOT =        -157
758198


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   17203
78791984  
00016717  00000-0  10270-3 0  9137
2 25544  51
6382 220
8694 0005908  57
4204 302
7519 15
54233105 27287


Satellite: ISS
Catalog Number: 25544
Epoch time:      17203
78791984   =   yrday
fracday
Element set:     913
Inclination:       51
6382  deg
RA of node:       220
8694  deg
Eccentricity:     
0005908     
Arg of perigee:    57
4204  deg
Mean anomaly:     302
7519  deg
Mean motion:   15
54233105  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2728
Checksum:              318


Coasting Arc #15 (Orbit 2742)
---------------------------------------

Vector Time (GMT): 2017/204/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4234968
68                 A    =         6778555
05  meter
 Y    =        1873224
33  meter          E    =           
0017527
 Z    =       -4965615
88                 I    =           51
40363
 XDOT =      -4899
384841                 Wp   =           91
72853
 YDOT =      -5489
789436  meter/sec      RA   =          214
99881  deg
 ZDOT =       2113
480028                 TA   =          198
92374
                                          MA   =          198
98896
                                          Ha   =            222
968  n
mi
                                          Hp   =            212
365

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13894254
21                 X    =        -4231480
83
 Y    =        6145749
13  feet           Y    =         1825885
99  meter
 Z    =      -16291390
69                 Z    =        -4986178
96
 XDOT =     -16074
097249                 XDOT =       -4847
898462
 YDOT =     -18011
120197  feet/sec       YDOT =       -5544
289996  meter/sec
 ZDOT =       6933
989592                 ZDOT =        2089
805409

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9461704
36                 X    =         2883927
49
 Y    =      -11760895
28  feet           Y    =        -3584720
88  meter
 Z    =      -16382534
48                 Z    =        -4993396
51
 XDOT =      21705
992666                 XDOT =        6615
986565
 YDOT =       7975
442370  feet/sec       YDOT =        2430
914834  meter/sec
 ZDOT =       6830
195255                 ZDOT =        2081
843514


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   17204
75240322  
00016717  00000-0  10270-3 0  9141
2 25544  51
6387 216
0598 0006101  61
3029 298
8737 15
54209282 27430


Satellite: ISS
Catalog Number: 25544
Epoch time:      17204
75240322   =   yrday
fracday
Element set:     914
Inclination:       51
6387  deg
RA of node:       216
0598  deg
Eccentricity:     
0006101     
Arg of perigee:    61
3029  deg
Mean anomaly:     298
8737  deg
Mean motion:   15
54209282  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2743
Checksum:              305


Coasting Arc #16 (Orbit 2758)
---------------------------------------

Vector Time (GMT): 2017/205/17:45:30
000
Vector Time (MET): N/A
Weight (LBS)     : 887557
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5376580
10                 A    =         6781939
14  meter
 Y    =        -645195
05  meter          E    =           
0016552
 Z    =        4072793
25                 I    =           51
44200
 XDOT =       3587
635491                 Wp   =           72
80992
 YDOT =       5597
031120  meter/sec      RA   =          209
99124  deg
 ZDOT =      -3831
758478                 TA   =           56
95592
                                          MA   =           56
79704
                                          Ha   =            222
919  n
mi
                                          Hp   =            212
430

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17639698
50                 X    =         5363612
08
 Y    =       -2116781
65  feet           Y    =         -585143
25  meter
 Z    =       13362182
58                 Z    =         4098878
87
 XDOT =      11770
457648                 XDOT =        3543
393748
 YDOT =      18362
962993  feet/sec       YDOT =        5636
903373  meter/sec
 ZDOT =     -12571
386083                 ZDOT =       -3814
438349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14477877
14                 X    =        -4412856
95
 Y    =       10145644
75  feet           Y    =         3092392
52  meter
 Z    =       13477559
77                 Z    =         4107960
22
 XDOT =     -18373
238187                 XDOT =       -5600
163000
 YDOT =      -9542
875959  feet/sec       YDOT =       -2908
668592  meter/sec
 ZDOT =     -12495
664913                 ZDOT =       -3808
678665


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
78118210  
00016717  00000-0  10270-3 0  9156
2 25544  51
6384 210
9312 0006121  65
2993 294
8796 15
54205900 27590


Satellite: ISS
Catalog Number: 25544
Epoch time:      17205
78118210   =   yrday
fracday
Element set:     915
Inclination:       51
6384  deg
RA of node:       210
9312  deg
Eccentricity:     
0006121     
Arg of perigee:    65
2993  deg
Mean anomaly:     294
8796  deg
Mean motion:   15
54205900  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2759
Checksum:              310
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