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

 
Date: September 5th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 596 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


255/21:17:02 000 0 0 0 0 0 0
N/A 0 0 0 0 219 3
000/00:00:00 000 0 0 0 0 216 2

256/02:57:42 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 3

256/23:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 2

Coasting Arc #1 (Orbit 3407)
---------------------------------------

Vector Time (GMT): 2017/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2619031
66                 A    =         6779152
09  meter
 Y    =       -3819947
47  meter          E    =           
0010660
 Z    =       -4959858
95                 I    =           51
64736
 XDOT =       7063
128492                 Wp   =          126
38294
 YDOT =       2013
833328  meter/sec      RA   =            2
35791  deg
 ZDOT =       2175
735178                 TA   =          164
86801
                                          MA   =          164
83610
                                          Ha   =            220
415  n
mi
                                          Hp   =            215
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8592623
54                 X    =         2685644
93
 Y    =      -12532636
05  feet           Y    =        -3790287
62  meter
 Z    =      -16272503
10                 Z    =        -4946974
56
 XDOT =      23172
993740                 XDOT =        7029
515807
 YDOT =       6607
064725  feet/sec       YDOT =        2092
630281  meter/sec
 ZDOT =       7138
238774                 ZDOT =        2209
963431

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11994645
51                 X    =        -3655967
95
 Y    =        9428881
11  feet           Y    =         2873922
96  meter
 Z    =      -16214782
86                 Z    =        -4942265
81
 XDOT =     -19480
411919                 XDOT =       -5937
629553
 YDOT =     -12229
231872  feet/sec       YDOT =       -3727
469875  meter/sec
 ZDOT =       7289
447028                 ZDOT =        2221
823454


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   17247
51221155  
00016717  00000-0  10270-3 0  9000
2 25544  51
6427   2
8847 0004419 228
1037 131
9740 15
54073479 34082


Satellite: ISS
Catalog Number: 25544
Epoch time:      17247
51221155   =   yrday
fracday
Element set:     900
Inclination:       51
6427  deg
RA of node:         2
8847  deg
Eccentricity:     
0004419     
Arg of perigee:   228
1037  deg
Mean anomaly:     131
9740  deg
Mean motion:   15
54073479  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3408
Checksum:              296


Coasting Arc #2 (Orbit 3423)
---------------------------------------

Vector Time (GMT): 2017/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4165728
16                 A    =         6782562
31  meter
 Y    =        3438358
99  meter          E    =           
0007044
 Z    =        4095785
53                 I    =           51
62543
 XDOT =      -6046
790679                 Wp   =           93
07123
 YDOT =      -2757
685663  meter/sec      RA   =          357
36646  deg
 ZDOT =      -3829
691441                 TA   =           36
51116
                                          MA   =           36
46315
                                          Ha   =            220
468  n
mi
                                          Hp   =            216
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13667087
14                 X    =        -4223762
30
 Y    =       11280705
34  feet           Y    =         3391450
89  meter
 Z    =       13437616
58                 Z    =         4075408
65
 XDOT =     -19838
552098                 XDOT =       -5996
901541
 YDOT =      -9047
525140  feet/sec       YDOT =       -2825
026431  meter/sec
 ZDOT =     -12564
604465                 ZDOT =       -3858
943099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16341755
24                 X    =         4980967
00
 Y    =       -7030162
38  feet           Y    =        -2142793
49  meter
 Z    =       13346796
46                 Z    =         4068103
56
 XDOT =      15963
533085                 XDOT =        4865
684884
 YDOT =      12975
279072  feet/sec       YDOT =        3954
865061  meter/sec
 ZDOT =     -12693
638817                 ZDOT =       -3869
021111


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   17248
54109168  
00016717  00000-0  10270-3 0  9014
2 25544  51
6424 357
7566 0004345 230
9320 129
1446 15
54040232 34244


Satellite: ISS
Catalog Number: 25544
Epoch time:      17248
54109168   =   yrday
fracday
Element set:     901
Inclination:       51
6424  deg
RA of node:       357
7566  deg
Eccentricity:     
0004345     
Arg of perigee:   230
9320  deg
Mean anomaly:     129
1446  deg
Mean motion:   15
54040232  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3424
Checksum:              292


Coasting Arc #3 (Orbit 3438)
---------------------------------------

Vector Time (GMT): 2017/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5400007
03                 A    =         6786261
12  meter
 Y    =       -2982914
01  meter          E    =           
0000340
 Z    =       -2827834
99                 I    =           51
60596
 XDOT =       4572
791285                 Wp   =           79
68797
 YDOT =       3455
777090  meter/sec      RA   =          352
38315  deg
 ZDOT =       5087
446846                 TA   =          248
19419
                                          MA   =          248
19780
                                          Ha   =            220
144  n
mi
                                          Hp   =            216
229

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17716558
50                 X    =         5446697
55
 Y    =       -9786463
28  feet           Y    =        -2922266
70  meter
 Z    =       -9277673
84                 Z    =        -2801489
91
 XDOT =      15002
596081                 XDOT =        4509
095890
 YDOT =      11337
851345  feet/sec       YDOT =        3506
557589  meter/sec
 ZDOT =      16691
098576                 ZDOT =        5109
504769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19712479
34                 X    =        -6008363
70
 Y    =        4819704
95  feet           Y    =         1469046
07  meter
 Z    =       -9160520
89                 Z    =        -2792126
77
 XDOT =     -11074
312274                 XDOT =       -3375
450381
 YDOT =     -13389
112497  feet/sec       YDOT =       -4081
001489  meter/sec
 ZDOT =      16788
154865                 ZDOT =        5117
029603


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   17249
50566088  
00016717  00000-0  10270-3 0  9020
2 25544  51
6430 352
9496 0004415 238
1915 121
8808 15
54046572 34398


Satellite: ISS
Catalog Number: 25544
Epoch time:      17249
50566088   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:       352
9496  deg
Eccentricity:     
0004415     
Arg of perigee:   238
1915  deg
Mean anomaly:     121
8808  deg
Mean motion:   15
54046572  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3439
Checksum:              322


Coasting Arc #4 (Orbit 3454)
---------------------------------------

Vector Time (GMT): 2017/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6214224
23                 A    =         6788895
55  meter
 Y    =        2407814
27  meter          E    =           
0012285
 Z    =        1254564
60                 I    =           51
58262
 XDOT =      -2781
439254                 Wp   =          139
50257
 YDOT =      -4123
945888  meter/sec      RA   =          347
40643  deg
 ZDOT =      -5839
450947                 TA   =           26
83991
                                          MA   =           26
77640
                                          Ha   =            220
089  n
mi
                                          Hp   =            216
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20387874
78                 X    =        -6246781
23
 Y    =        7899653
12  feet           Y    =         2338140
69  meter
 Z    =        4116025
58                 Z    =         1224298
59
 XDOT =      -9125
456870                 XDOT =       -2706
752402
 YDOT =     -13530
006195  feet/sec       YDOT =       -4154
632936  meter/sec
 ZDOT =     -19158
303633                 ZDOT =       -5852
780363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21724412
91                 X    =         6621601
05
 Y    =       -2684799
39  feet           Y    =         -818326
85  meter
 Z    =        3981627
83                 Z    =         1213600
16
 XDOT =       5233
486140                 XDOT =        1595
166575
 YDOT =      13733
175136  feet/sec       YDOT =        4185
871781  meter/sec
 ZDOT =     -19216
598942                 ZDOT =       -5857
219357


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   17250
53453068  
00016717  00000-0  10270-3 0  9039
2 25544  51
6429 347
8217 0004370 239
9292 120
1427 15
54063800 34557


Satellite: ISS
Catalog Number: 25544
Epoch time:      17250
53453068   =   yrday
fracday
Element set:     903
Inclination:       51
6429  deg
RA of node:       347
8217  deg
Eccentricity:     
0004370     
Arg of perigee:   239
9292  deg
Mean anomaly:     120
1427  deg
Mean motion:   15
54063800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3455
Checksum:              300


Coasting Arc #5 (Orbit 3470)
---------------------------------------

Vector Time (GMT): 2017/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6550038
37                 A    =         6789378
78  meter
 Y    =       -1715089
41  meter          E    =           
0008946
 Z    =         430725
98                 I    =           51
55312
 XDOT =        837
758286                 Wp   =           41
95800
 YDOT =       4718
999739  meter/sec      RA   =          342
43189  deg
 ZDOT =       5985
172609                 TA   =          322
69160
                                          MA   =          322
75370
                                          Ha   =            219
885  n
mi
                                          Hp   =            216
143

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21489627
21                 X    =         6566637
89
 Y    =       -5626933
75  feet           Y    =        -1641749
55  meter
 Z    =        1413142
99                 Z    =          462584
56
 XDOT =       2748
550807                 XDOT =         755
853870
 YDOT =      15482
282609  feet/sec       YDOT =        4727
910884  meter/sec
 ZDOT =      19636
393074                 ZDOT =        5989
042681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22196492
23                 X    =        -6765490
83
 Y    =         602354
14  feet           Y    =          183597
54  meter
 Z    =        1554457
02                 Z    =          473798
50
 XDOT =       1008
546505                 XDOT =         307
404975
 YDOT =     -14055
714199  feet/sec       YDOT =       -4284
181688  meter/sec
 ZDOT =      19652
712613                 ZDOT =        5990
146804


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   17251
56339401  
00016717  00000-0  10270-3 0  9048
2 25544  51
6432 342
6936 0004224 246
8636 113
2072 15
54078952 34710


Satellite: ISS
Catalog Number: 25544
Epoch time:      17251
56339401   =   yrday
fracday
Element set:     904
Inclination:       51
6432  deg
RA of node:       342
6936  deg
Eccentricity:     
0004224     
Arg of perigee:   246
8636  deg
Mean anomaly:     113
2072  deg
Mean motion:   15
54078952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3471
Checksum:              302


Coasting Arc #6 (Orbit 3485)
---------------------------------------

Vector Time (GMT): 2017/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6396303
41                 A    =         6787523
30  meter
 Y    =         855058
75  meter          E    =           
0006271
 Z    =       -2091527
29                 I    =           51
51485
 XDOT =       1105
684100                 Wp   =          177
74105
 YDOT =      -5208
425571  meter/sec      RA   =          337
45403  deg
 ZDOT =      -5517
409313                 TA   =           25
45512
                                          MA   =           25
42424
                                          Ha   =            219
717  n
mi
                                          Hp   =            216
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20985247
42                 X    =        -6395229
86
 Y    =        2805310
84  feet           Y    =          783536
69  meter
 Z    =       -6861966
17                 Z    =        -2122596
17
 XDOT =       3627
572506                 XDOT =        1190
644909
 YDOT =     -17088
010404  feet/sec       YDOT =       -5195
586634  meter/sec
 ZDOT =     -18101
736590                 ZDOT =       -5511
831275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21061391
65                 X    =         6419512
18
 Y    =        1661323
24  feet           Y    =          506371
32  meter
 Z    =       -6999624
60                 Z    =        -2133485
58
 XDOT =      -7134
933126                 XDOT =       -2174
727617
 YDOT =      14383
794645  feet/sec       YDOT =        4384
180608  meter/sec
 ZDOT =     -18076
155864                 ZDOT =       -5509
612307


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   17252
52794996  
00016717  00000-0  10270-3 0  9050
2 25544  51
6418 337
8867 0004300 249
1318 110
9374 15
54085173 34869


Satellite: ISS
Catalog Number: 25544
Epoch time:      17252
52794996   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:       337
8867  deg
Eccentricity:     
0004300     
Arg of perigee:   249
1318  deg
Mean anomaly:     110
9374  deg
Mean motion:   15
54085173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3486
Checksum:              333


Coasting Arc #7 (Orbit 3501)
---------------------------------------

Vector Time (GMT): 2017/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5794455
94                 A    =         6783998
58  meter
 Y    =         139645
33  meter          E    =           
0008124
 Z    =        3520006
04                 I    =           51
47411
 XDOT =      -2864
276311                 Wp   =          101
96979
 YDOT =       5520
757545  meter/sec      RA   =          332
46514  deg
 ZDOT =       4485
576013                 TA   =          299
59792
                                          MA   =          299
67885
                                          Ha   =            219
553  n
mi
                                          Hp   =            216
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19010682
23                 X    =         5775365
15
 Y    =         458153
97  feet           Y    =          204336
49  meter
 Z    =       11548576
24                 Z    =         3548107
52
 XDOT =      -9397
231990                 XDOT =       -2947
586894
 YDOT =      18112
721605  feet/sec       YDOT =        5488
261879  meter/sec
 ZDOT =      14716
456734                 ZDOT =        4471
459256

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18488125
90                 X    =        -5635180
77
 Y    =       -4113108
20  feet           Y    =        -1253675
38  meter
 Z    =       11672921
61                 Z    =         3557906
51
 XDOT =      12518
188564                 XDOT =        3815
543874
 YDOT =     -14587
226259  feet/sec       YDOT =       -4446
186564  meter/sec
 ZDOT =      14653
037059                 ZDOT =        4466
245696


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   17253
55680306  
00016717  00000-0  10270-3 0  9064
2 25544  51
6423 332
7577 0004314 254
2258 105
8419 15
54116106 35025


Satellite: ISS
Catalog Number: 25544
Epoch time:      17253
55680306   =   yrday
fracday
Element set:     906
Inclination:       51
6423  deg
RA of node:       332
7577  deg
Eccentricity:     
0004314     
Arg of perigee:   254
2258  deg
Mean anomaly:     105
8419  deg
Mean motion:   15
54116106  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3502
Checksum:              293


Coasting Arc #8 (Orbit 3516)
---------------------------------------

Vector Time (GMT): 2017/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4819561
94                 A    =         6780345
07  meter
 Y    =       -1277186
36  meter          E    =           
0006192
 Z    =       -4601146
33                 I    =           51
43236
 XDOT =       4324
525626                 Wp   =           63
59893
 YDOT =      -5578
817178  meter/sec      RA   =          327
46476  deg
 ZDOT =      -2981
662297                 TA   =          176
55676
                                          MA   =          176
55250
                                          Ha   =            219
553  n
mi
                                          Hp   =            216
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15812211
09                 X    =        -4782571
61
 Y    =       -4190243
97  feet           Y    =        -1330875
53  meter
 Z    =      -15095624
44                 Z    =        -4624468
50
 XDOT =      14188
076200                 XDOT =        4401
071600
 YDOT =     -18303
205963  feet/sec       YDOT =       -5530
029626  meter/sec
 ZDOT =      -9782
356617                 ZDOT =       -2960
468568

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14726191
27                 X    =         4488543
10
 Y    =        6899515
91  feet           Y    =         2102972
45  meter
 Z    =      -15198618
76                 Z    =        -4632539
00
 XDOT =     -16756
212333                 XDOT =       -5107
293519
 YDOT =      14426
759102  feet/sec       YDOT =        4397
276174  meter/sec
 ZDOT =      -9687
614406                 ZDOT =       -2952
784871


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   17254
52135017  
00016717  00000-0  10270-3 0  9077
2 25544  51
6414 327
9502 0004254 259
2410 100
8264 15
54092012 35175


Satellite: ISS
Catalog Number: 25544
Epoch time:      17254
52135017   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       327
9502  deg
Eccentricity:     
0004254     
Arg of perigee:   259
2410  deg
Mean anomaly:     100
8264  deg
Mean motion:   15
54092012  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3517
Checksum:              276


Coasting Arc #9 (Orbit 3532)
---------------------------------------

Vector Time (GMT): 2017/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3585384
44                 A    =         6777774
04  meter
 Y    =        2474109
88  meter          E    =           
0002818
 Z    =        5193784
09                 I    =           51
39709
 XDOT =      -5387
143245                 Wp   =          199
75534
 YDOT =       5327
508169  meter/sec      RA   =          322
45337  deg
 ZDOT =       1178
639220                 TA   =          238
88701
                                          MA   =          238
91465
                                          Ha   =            219
343  n
mi
                                          Hp   =            216
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11763072
30                 X    =         3532222
79
 Y    =        8117158
39  feet           Y    =         2513907
16  meter
 Z    =       17039974
04                 Z    =         5211071
61
 XDOT =     -17674
354479                 XDOT =       -5452
041760
 YDOT =      17478
701343  feet/sec       YDOT =        5266
902664  meter/sec
 ZDOT =       3866
926575                 ZDOT =        1152
312034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10206274
00                 X    =        -3110872
31
 Y    =       -9873772
95  feet           Y    =        -3009525
99  meter
 Z    =       17116057
50                 Z    =         5216974
32
 XDOT =      19541
738610                 XDOT =        5956
321928
 YDOT =     -13686
398797  feet/sec       YDOT =       -4171
614353  meter/sec
 ZDOT =       3749
517123                 ZDOT =        1142
852819


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   17255
55019512  
00016717  00000-0  10270-3 0  9083
2 25544  51
6414 322
8218 0004251 263
6900  96
3769 15
54131176 35335


Satellite: ISS
Catalog Number: 25544
Epoch time:      17255
55019512   =   yrday
fracday
Element set:     908
Inclination:       51
6414  deg
RA of node:       322
8218  deg
Eccentricity:     
0004251     
Arg of perigee:   263
6900  deg
Mean anomaly:      96
3769  deg
Mean motion:   15
54131176  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3533
Checksum:              302


Coasting Arc #10 (Orbit 3538)
---------------------------------------

Vector Time (GMT): 2017/255/21:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 909096
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3194093
70                 A    =         6777397
82  meter
 Y    =        2822793
83  meter          E    =           
0001950
 Z    =        5270514
60                 I    =           51
38509
 XDOT =      -5588
387428                 Wp   =          234
90532
 YDOT =       5216
595250  meter/sec      RA   =          320
51605  deg
 ZDOT =        591
874178                 TA   =          209
41966
                                          MA   =          209
43063
                                          Ha   =            219
310  n
mi
                                          Hp   =            216
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10479310
04                 X    =         3136689
37
 Y    =        9261134
61  feet           Y    =         2858191
69  meter
 Z    =       17291714
55                 Z    =         5285891
01
 XDOT =     -18334
604422                 XDOT =       -5649
180490
 YDOT =      17114
813813  feet/sec       YDOT =        5153
762212  meter/sec
 ZDOT =       1941
844415                 ZDOT =         564
579442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -321671
71                 X    =          -98045
54
 Y    =       13897474
55  feet           Y    =         4235950
24  meter
 Z    =       17359282
07                 Z    =         5291109
17
 XDOT =     -23914
168591                 XDOT =       -7289
038587
 YDOT =      -2830
948419  feet/sec       YDOT =        -862
873078  meter/sec
 ZDOT =       1820
175032                 ZDOT =         554
789350


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   17255
93601235  
00016717  00000-0  10270-3 0  9095
2 25544  51
6406 320
9005 0004211 270
0881  89
9789 15
54146614 35394


Satellite: ISS
Catalog Number: 25544
Epoch time:      17255
93601235   =   yrday
fracday
Element set:     909
Inclination:       51
6406  deg
RA of node:       320
9005  deg
Eccentricity:     
0004211     
Arg of perigee:   270
0881  deg
Mean anomaly:      89
9789  deg
Mean motion:   15
54146614  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3539
Checksum:              313


Coasting Arc #11 (Orbit 3541)
---------------------------------------

Vector Time (GMT): 2017/256/02:57:42
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2968658
85                 A    =         6786208
08  meter
 Y    =       -5446410
53  meter          E    =           
0002625
 Z    =       -2748553
67                 I    =           51
40691
 XDOT =       5678
567884                 Wp   =          354
66110
 YDOT =        510
313492  meter/sec      RA   =          319
30342  deg
 ZDOT =       5124
262849                 TA   =          334
11931
                                          MA   =          334
13243
                                          Ha   =            219
462  n
mi
                                          Hp   =            216
277

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9739694
39                 X    =         3042692
60
 Y    =      -17868800
96  feet           Y    =        -5412799
16  meter
 Z    =       -9017564
54                 Z    =        -2733952
68
 XDOT =      18630
472060                 XDOT =        5647
548117
 YDOT =       1674
256862  feet/sec       YDOT =         573
641935  meter/sec
 ZDOT =      16811
885986                 ZDOT =        5151
772317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2525810
75                 X    =         -769867
12
 Y    =      -20222600
69  feet           Y    =        -6163848
69  meter
 Z    =       -8952031
41                 Z    =        -2728579
17
 XDOT =      14516
848651                 XDOT =        4424
735469
 YDOT =      -9306
035319  feet/sec       YDOT =       -2836
479565  meter/sec
 ZDOT =      16933
536367                 ZDOT =        5161
341885


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   17256
12891958  
00016717  00000-0  10270-3 0  9102
2 25544  51
6393 319
9371 0004286 269
8981  90
1681 15
54115513 35425


Satellite: ISS
Catalog Number: 25544
Epoch time:      17256
12891958   =   yrday
fracday
Element set:     910
Inclination:       51
6393  deg
RA of node:       319
9371  deg
Eccentricity:     
0004286     
Arg of perigee:   269
8981  deg
Mean anomaly:      90
1681  deg
Mean motion:   15
54115513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3542
Checksum:              331


Coasting Arc #12 (Orbit 3554)
---------------------------------------

Vector Time (GMT): 2017/256/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2059374
57                 A    =         6785070
49  meter
 Y    =       -5630141
88  meter          E    =           
0001324
 Z    =       -3176430
91                 I    =           51
38645
 XDOT =       5956
756035                 Wp   =           12
50416
 YDOT =       -525
807265  meter/sec      RA   =          315
12681  deg
 ZDOT =       4795
565360                 TA   =          310
68397
                                          MA   =          310
69548
                                          Ha   =            219
490  n
mi
                                          Hp   =            216
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6756478
26                 X    =         2137608
82
 Y    =      -18471594
08  feet           Y    =        -5606675
26  meter
 Z    =      -10421361
25                 Z    =        -3166236
81
 XDOT =      19543
162845                 XDOT =        5938
898506
 YDOT =      -1725
089451  feet/sec       YDOT =        -459
294377  meter/sec
 ZDOT =      15733
482153                 ZDOT =        4824
458113

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13435932
12                 X    =         4095272
11
 Y    =      -14397337
43  feet           Y    =        -4388308
45  meter
 Z    =      -10375305
28                 Z    =        -3162393
05
 XDOT =      17544
460201                 XDOT =        5347
551469
 YDOT =       4946
416133  feet/sec       YDOT =        1507
667637  meter/sec
 ZDOT =      15861
427117                 ZDOT =        4834
562985


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   17256
96485342  
00016717  00000-0  10270-3 0  9111
2 25544  51
6428 315
7719 0004155 274
5760  85
4918 15
54134394 35559


Satellite: ISS
Catalog Number: 25544
Epoch time:      17256
96485342   =   yrday
fracday
Element set:     911
Inclination:       51
6428  deg
RA of node:       315
7719  deg
Eccentricity:     
0004155     
Arg of perigee:   274
5760  deg
Mean anomaly:      85
4918  deg
Mean motion:   15
54134394  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3555
Checksum:              334


Coasting Arc #13 (Orbit 3570)
---------------------------------------

Vector Time (GMT): 2017/257/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3147659
56                 A    =         6788288
88  meter
 Y    =        5777575
66  meter          E    =           
0010218
 Z    =        1648884
02                 I    =           51
37411
 XDOT =      -5018
762248                 Wp   =          123
56881
 YDOT =      -1103
901296  meter/sec      RA   =          310
13330  deg
 ZDOT =      -5692
678144                 TA   =           38
30157
                                          MA   =           38
22904
                                          Ha   =            219
617  n
mi
                                          Hp   =            216
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10326967
07                 X    =        -3220041
45
 Y    =       18955300
73  feet           Y    =         5741971
76  meter
 Z    =        5409724
47                 Z    =         1633417
60
 XDOT =     -16465
755406                 XDOT =       -4978
392971
 YDOT =      -3621
723412  feet/sec       YDOT =       -1159
799101  meter/sec
 ZDOT =     -18676
765565                 ZDOT =       -5716
959550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16650950
98                 X    =        -5075209
86
 Y    =       13763777
69  feet           Y    =         4195199
44  meter
 Z    =        5340322
89                 Z    =         1627730
42
 XDOT =     -12831
642463                 XDOT =       -3911
084623
 YDOT =      -8209
370556  feet/sec       YDOT =       -2502
216146  meter/sec
 ZDOT =     -18784
032138                 ZDOT =       -5725
372996


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   17257
99369044  
00016717  00000-0  10270-3 0  9126
2 25544  51
6424 310
6439 0004004 277
8419  82
2279 15
54100420 35714


Satellite: ISS
Catalog Number: 25544
Epoch time:      17257
99369044   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:       310
6439  deg
Eccentricity:     
0004004     
Arg of perigee:   277
8419  deg
Mean anomaly:      82
2279  deg
Mean motion:   15
54100420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3571
Checksum:              304


Coasting Arc #14 (Orbit 3586)
---------------------------------------

Vector Time (GMT): 2017/258/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3926486
84                 A    =         6789295
64  meter
 Y    =       -5530703
05  meter          E    =           
0010544
 Z    =          33936
43                 I    =           51
35724
 XDOT =       3885
899706                 Wp   =           26
27964
 YDOT =       2799
854963  meter/sec      RA   =          305
14340  deg
 ZDOT =       5990
179174                 TA   =          334
08739
                                          MA   =          334
14015
                                          Ha   =            219
554  n
mi
                                          Hp   =            216
136

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12882174
69                 X    =         3987875
97
 Y    =      -18145351
20  feet           Y    =        -5486451
14  meter
 Z    =         111340
01                 Z    =           53159
45
 XDOT =      12749
014782                 XDOT =        3825
204999
 YDOT =       9185
875863  feet/sec       YDOT =        2842
970786  meter/sec
 ZDOT =      19652
818811                 ZDOT =        6008
907945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18479488
57                 X    =         5632548
12
 Y    =      -12397022
28  feet           Y    =        -3778612
39  meter
 Z    =         197312
03                 Z    =           60140
71
 XDOT =       7636
826521                 XDOT =        2327
704723
 YDOT =      11718
653733  feet/sec       YDOT =        3571
845658  meter/sec
 ZDOT =      19735
237785                 ZDOT =        6015
300477


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   17259
02252215  
00016717  00000-0  10270-3 0  9134
2 25544  51
6420 305
5151 0004205 283
3815  76
6868 15
54140297 35873


Satellite: ISS
Catalog Number: 25544
Epoch time:      17259
02252215   =   yrday
fracday
Element set:     913
Inclination:       51
6420  deg
RA of node:       305
5151  deg
Eccentricity:     
0004205     
Arg of perigee:   283
3815  deg
Mean anomaly:      76
6868  deg
Mean motion:   15
54140297  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3587
Checksum:              301


Coasting Arc #15 (Orbit 3601)
---------------------------------------

Vector Time (GMT): 2017/259/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4419338
41                 A    =         6788078
18  meter
 Y    =        4848439
37  meter          E    =           
0004792
 Z    =       -1732092
60                 I    =           51
33514
 XDOT =      -2655
951684                 Wp   =          173
84383
 YDOT =      -4439
783078  meter/sec      RA   =          300
15297  deg
 ZDOT =      -5657
373500                 TA   =           25
23919
                                          MA   =           25
21578
                                          Ha   =            219
616  n
mi
                                          Hp   =            216
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14499141
75                 X    =        -4464812
90
 Y    =       15906953
31  feet           Y    =         4798764
90  meter
 Z    =       -5682718
50                 Z    =        -1753671
09
 XDOT =      -8713
752243                 XDOT =       -2578
626907
 YDOT =     -14566
217448  feet/sec       YDOT =       -4469
051891  meter/sec
 ZDOT =     -18560
936681                 ZDOT =       -5670
086994

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18992638
04                 X    =        -5788956
07
 Y    =       10071372
72  feet           Y    =         3069754
41  meter
 Z    =       -5778989
23                 Z    =        -1761435
92
 XDOT =      -2418
297859                 XDOT =        -737
097187
 YDOT =     -15231
281985  feet/sec       YDOT =       -4642
494749  meter/sec
 ZDOT =     -18616
478428                 ZDOT =       -5674
302625


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   17259
98705111  
00016717  00000-0  10270-3 0  9148
2 25544  51
6422 300
7079 0004288 284
9782  75
0895 15
54105551 36027


Satellite: ISS
Catalog Number: 25544
Epoch time:      17259
98705111   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       300
7079  deg
Eccentricity:     
0004288     
Arg of perigee:   284
9782  deg
Mean anomaly:      75
0895  deg
Mean motion:   15
54105551  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3602
Checksum:              319


Coasting Arc #16 (Orbit 3617)
---------------------------------------

Vector Time (GMT): 2017/260/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4625252
41                 A    =         6784806
53  meter
 Y    =       -3757981
60  meter          E    =           
0009019
 Z    =        3233050
41                 I    =           51
30836
 XDOT =       1441
404190                 Wp   =           75
47410
 YDOT =       5857
515450  meter/sec      RA   =          295
15299  deg
 ZDOT =       4737
581801                 TA   =          322
18352
                                          MA   =          322
24685
                                          Ha   =            219
661  n
mi
                                          Hp   =            216
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15174712
62                 X    =         4651226
93
 Y    =      -12329335
95  feet           Y    =        -3706113
29  meter
 Z    =       10607120
78                 Z    =         3255581
80
 XDOT =       4729
016372                 XDOT =        1352
784066
 YDOT =      19217
570373  feet/sec       YDOT =        5873
139224  meter/sec
 ZDOT =      15543
247378                 ZDOT =        4744
367770

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18272302
52                 X    =         5569397
81
 Y    =       -6802172
05  feet           Y    =        -2073302
04  meter
 Z    =       10707420
57                 Z    =         3263621
79
 XDOT =      -2310
311956                 XDOT =        -704
183084
 YDOT =      18352
114428  feet/sec       YDOT =        5593
724478  meter/sec
 ZDOT =      15572
344730                 ZDOT =        4746
450674


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   17261
01587675  
00016717  00000-0  10270-3 0  9159
2 25544  51
6416 295
5781 0004293 293
0763  66
9937 15
54130379 36186


Satellite: ISS
Catalog Number: 25544
Epoch time:      17261
01587675   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       295
5781  deg
Eccentricity:     
0004293     
Arg of perigee:   293
0763  deg
Mean anomaly:      66
9937  deg
Mean motion:   15
54130379  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3618
Checksum:              339


Coasting Arc #17 (Orbit 3632)
---------------------------------------

Vector Time (GMT): 2017/261/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924327
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4611956
43                 A    =         6780942
98  meter
 Y    =        2310891
97  meter          E    =           
0006934
 Z    =       -4408258
94                 I    =           51
28083
 XDOT =       -293
927540                 Wp   =           42
49978
 YDOT =      -6903
851995  meter/sec      RA   =          290
14267  deg
 ZDOT =      -3309
657211                 TA   =          193
87305
                                          MA   =          193
89211
                                          Ha   =            219
817  n
mi
                                          Hp   =            215
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15131090
64                 X    =        -4616041
59
 Y    =        7581666
58  feet           Y    =         2259294
53  meter
 Z    =      -14462791
79                 Z    =        -4430672
51
 XDOT =       -964
329198                 XDOT =        -200
628354
 YDOT =     -22650
433053  feet/sec       YDOT =       -6906
617642  meter/sec
 ZDOT =     -10858
455418                 ZDOT =       -3310
857537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16634224
82                 X    =        -5070111
73
 Y    =        2616289
65  feet           Y    =          797445
09  meter
 Z    =      -14562331
93                 Z    =        -4438598
77
 XDOT =       6271
261247                 XDOT =        1911
480428
 YDOT =     -20625
234470  feet/sec       YDOT =       -6286
571466  meter/sec
 ZDOT =     -10862
687302                 ZDOT =       -3310
947090


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   17261
98039732  
00016717  00000-0  10270-3 0  9162
2 25544  51
6398 290
7699 0004346 295
4977  64
5726 15
54143466 36330


Satellite: ISS
Catalog Number: 25544
Epoch time:      17261
98039732   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       290
7699  deg
Eccentricity:     
0004346     
Arg of perigee:   295
4977  deg
Mean anomaly:      64
5726  deg
Mean motion:   15
54143466  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3633
Checksum:              356
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