[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: September 26th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 9 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


270/16:51:50 146 -1 0 1 5 1 5
N/A -0 9 -0 1 220 7
000/00:03:40 293 -0 5 -0 0 215 8

274/01:42:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 215 6

277/10:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 215 1

Coasting Arc #1 (Orbit 3734)
---------------------------------------

Vector Time (GMT): 2017/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3562146
60                 A    =         6785105
05  meter
 Y    =        4943221
87  meter          E    =           
0010601
 Z    =        2978853
03                 I    =           51
27694
 XDOT =      -2914
665306                 Wp   =           79
72361
 YDOT =       5088
052167  meter/sec      RA   =          257
30237  deg
 ZDOT =      -4941
015485                 TA   =           66
01488
                                          MA   =           65
90393
                                          Ha   =            220
412  n
mi
                                          Hp   =            215
297

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11686832
68                 X    =         3492135
43
 Y    =       16217919
52  feet           Y    =         4982665
04  meter
 Z    =        9773139
87                 Z    =         2995986
56
 XDOT =      -9562
550217                 XDOT =       -2947
343287
 YDOT =      16693
084539  feet/sec       YDOT =        5055
275230  meter/sec
 ZDOT =     -16210
680726                 ZDOT =       -4955
254043

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12626214
25                 X    =        -3848470
10
 Y    =      -15450180
76  feet           Y    =        -4709215
09  meter
 Z    =        9848241
60                 Z    =         3001744
04
 XDOT =       7253
395145                 XDOT =        2210
834840
 YDOT =     -16336
331593  feet/sec       YDOT =       -4979
313870  meter/sec
 ZDOT =     -16274
420784                 ZDOT =       -4960
443455


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   17268
53831645  
00016717  00000-0  10270-3 0  9006
2 25544  51
6374 258
0648 0004364 323
2299  36
8554 15
54267949 37359


Satellite: ISS
Catalog Number: 25544
Epoch time:      17268
53831645   =   yrday
fracday
Element set:     900
Inclination:       51
6374  deg
RA of node:       258
0648  deg
Eccentricity:     
0004364     
Arg of perigee:   323
2299  deg
Mean anomaly:      36
8554  deg
Mean motion:   15
54267949  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3735
Checksum:              339


Coasting Arc #2 (Orbit 3749)
---------------------------------------

Vector Time (GMT): 2017/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3058877
72                 A    =         6788065
67  meter
 Y    =       -5888081
87  meter          E    =           
0010626
 Z    =       -1402978
73                 I    =           51
29499
 XDOT =       3789
477884                 Wp   =           16
39161
 YDOT =      -3339
061052  meter/sec      RA   =          252
30259  deg
 ZDOT =       5772
136336                 TA   =          328
23606
                                          MA   =          328
30011
                                          Ha   =            220
466  n
mi
                                          Hp   =            215
163

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10035688
07                 X    =        -2985993
22
 Y    =      -19317853
91  feet           Y    =        -5921880
92  meter
 Z    =       -4602948
60                 Z    =        -1417660
49
 XDOT =      12432
670224                 XDOT =        3798
495960
 YDOT =     -10954
924712  feet/sec       YDOT =       -3296
633639  meter/sec
 ZDOT =      18937
455171                 ZDOT =        5790
566839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11527610
89                 X    =         3513615
80
 Y    =       18450317
65  feet           Y    =         5623656
82  meter
 Z    =       -4667077
91                 Z    =        -1422525
35
 XDOT =     -10041
297092                 XDOT =       -3060
587354
 YDOT =      11067
815774  feet/sec       YDOT =        3373
470248  meter/sec
 ZDOT =      19019
491527                 ZDOT =        5797
141017


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   17269
50277307  
00016717  00000-0  10270-3 0  9014
2 25544  51
6374 253
2569 0004107 327
1884  32
9013 15
54267314 37506


Satellite: ISS
Catalog Number: 25544
Epoch time:      17269
50277307   =   yrday
fracday
Element set:     901
Inclination:       51
6374  deg
RA of node:       253
2569  deg
Eccentricity:     
0004107     
Arg of perigee:   327
1884  deg
Mean anomaly:      32
9013  deg
Mean motion:   15
54267314  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3750
Checksum:              304


Coasting Arc #3 (Orbit 3765)
---------------------------------------

Vector Time (GMT): 2017/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904993
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2348468
35                 A    =         6788858
29  meter
 Y    =        6356700
53  meter          E    =           
0007267
 Z    =        -356637
34                 I    =           51
30946
 XDOT =      -4608
499536                 Wp   =          128
87784
 YDOT =       1372
526099  meter/sec      RA   =          247
30773  deg
 ZDOT =      -5969
997953                 TA   =           54
98290
                                          MA   =           54
91473
                                          Ha   =            220
674  n
mi
                                          Hp   =            215
066

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7704948
64                 X    =         2278943
87
 Y    =       20855316
69  feet           Y    =         6382573
94  meter
 Z    =       -1170070
02                 Z    =         -345398
43
 XDOT =     -15119
749133                 XDOT =       -4594
505344
 YDOT =       4503
038384  feet/sec       YDOT =        1321
068522  meter/sec
 ZDOT =     -19586
607457                 ZDOT =       -5992
350960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9711434
55                 X    =        -2960045
25
 Y    =      -20002760
23  feet           Y    =        -6096841
32  meter
 Z    =       -1121228
77                 Z    =         -341750
53
 XDOT =      13021
326853                 XDOT =        3968
900425
 YDOT =      -5235
110717  feet/sec       YDOT =       -1595
661747  meter/sec
 ZDOT =     -19685
725816                 ZDOT =       -6000
209229


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   17270
53151964  
00016717  00000-0  10270-3 0  9020
2 25544  51
6383 248
1267 0004351 331
8803  28
2114 15
54272269 37660


Satellite: ISS
Catalog Number: 25544
Epoch time:      17270
53151964   =   yrday
fracday
Element set:     902
Inclination:       51
6383  deg
RA of node:       248
1267  deg
Eccentricity:     
0004351     
Arg of perigee:   331
8803  deg
Mean anomaly:      28
2114  deg
Mean motion:   15
54272269  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3766
Checksum:              304


Coasting Arc #4 (Orbit 3768)
---------------------------------------

Vector Time (GMT): 2017/270/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2416064
91                 A    =         6779744
59  meter
 Y    =        4117226
12  meter          E    =           
0010529
 Z    =       -4823802
08                 I    =           51
28215
 XDOT =      -4613
126583                 Wp   =           49
57250
 YDOT =      -5596
867277  meter/sec      RA   =          246
30303  deg
 ZDOT =      -2463
365773                 TA   =          196
06933
                                          MA   =          196
10275
                                          Ha   =            220
655  n
mi
                                          Hp   =            215
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7926722
15                 X    =        -2438493
36
 Y    =       13507959
71  feet           Y    =         4090082
28  meter
 Z    =      -15826122
31                 Z    =        -4835593
47
 XDOT =     -15134
929733                 XDOT =       -4538
232120
 YDOT =     -18362
425449  feet/sec       YDOT =       -5648
035823  meter/sec
 ZDOT =      -8081
908703                 ZDOT =       -2485
592822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11805284
23                 X    =        -3598250
63
 Y    =      -10210792
13  feet           Y    =        -3112249
44  meter
 Z    =      -15878886
47                 Z    =        -4839884
60
 XDOT =      20115
131588                 XDOT =        6131
092108
 YDOT =     -10520
282358  feet/sec       YDOT =       -3206
582063  meter/sec
 ZDOT =      -8179
489470                 ZDOT =       -2493
108390


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   17270
72441108  
00016717  00000-0  10270-3 0  9034
2 25544  51
6415 247
1661 0004518 316
9115  43
1683 15
54015970 37692


Satellite: ISS
Catalog Number: 25544
Epoch time:      17270
72441108   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:       247
1661  deg
Eccentricity:     
0004518     
Arg of perigee:   316
9115  deg
Mean anomaly:      43
1683  deg
Mean motion:   15
54015970  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3769
Checksum:              300


Coasting Arc #5 (Orbit 3784)
---------------------------------------

Vector Time (GMT): 2017/271/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3345818
20                 A    =         6777790
42  meter
 Y    =       -2663796
00  meter          E    =           
0002113
 Z    =        5258157
59                 I    =           51
28911
 XDOT =       4116
353509                 Wp   =          353
56186
 YDOT =       6438
173908  meter/sec      RA   =          241
28187  deg
 ZDOT =        644
406879                 TA   =           90
26818
                                          MA   =           90
24397
                                          Ha   =            220
584  n
mi
                                          Hp   =            215
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10977093
84                 X    =         3349815
05
 Y    =       -8739488
19  feet           Y    =        -2626358
06  meter
 Z    =       17251173
18                 Z    =         5274420
56
 XDOT =      13505
096814                 XDOT =        4040
923960
 YDOT =      21122
617807  feet/sec       YDOT =        6483
784074  meter/sec
 ZDOT =       2114
195798                 ZDOT =         664
219344

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6762816
00                 X    =         2061306
32
 Y    =       12191721
52  feet           Y    =         3716036
72  meter
 Z    =       17323523
47                 Z    =         5280209
95
 XDOT =     -22220
736227                 XDOT =       -6772
880402
 YDOT =       9208
218037  feet/sec       YDOT =        2806
664858  meter/sec
 ZDOT =       2200
991306                 ZDOT =         670
862150


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   17271
75333042  
00016717  00000-0  10270-3 0  9046
2 25544  51
6407 242
0380 0004514 319
4661  40
6155 15
54027147 37858


Satellite: ISS
Catalog Number: 25544
Epoch time:      17271
75333042   =   yrday
fracday
Element set:     904
Inclination:       51
6407  deg
RA of node:       242
0380  deg
Eccentricity:     
0004514     
Arg of perigee:   319
4661  deg
Mean anomaly:      40
6155  deg
Mean motion:   15
54027147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3785
Checksum:              288


Coasting Arc #6 (Orbit 3799)
---------------------------------------

Vector Time (GMT): 2017/272/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4229662
85                 A    =         6778142
41  meter
 Y    =        1139916
25  meter          E    =           
0011210
 Z    =       -5181829
84                 I    =           51
30704
 XDOT =      -3338
905380                 Wp   =           83
20782
 YDOT =      -6782
606710  meter/sec      RA   =          236
25993  deg
 ZDOT =       1236
928469                 TA   =          198
71104
                                          MA   =          198
75228
                                          Ha   =            220
776  n
mi
                                          Hp   =            215
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13876846
62                 X    =        -4216924
40
 Y    =        3739882
70  feet           Y    =         1092688
11  meter
 Z    =      -17000754
08                 Z    =        -5202345
50
 XDOT =     -10954
413977                 XDOT =       -3268
820740
 YDOT =     -22252
646686  feet/sec       YDOT =       -6819
552667  meter/sec
 ZDOT =       4058
164269                 ZDOT =        1220
879743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1586643
12                 X    =         -483608
82
 Y    =      -14175149
88  feet           Y    =        -4320585
68  meter
 Z    =      -17091720
91                 Z    =        -5209556
53
 XDOT =      22637
644718                 XDOT =        6899
954110
 YDOT =      -7328
259130  feet/sec       YDOT =       -2233
653383  meter/sec
 ZDOT =       3988
055218                 ZDOT =        1215
559230


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   17272
71793873  
00016717  00000-0  10270-3 0  9056
2 25544  51
6409 237
2308 0004605 322
6003  37
4828 15
54025101 38000


Satellite: ISS
Catalog Number: 25544
Epoch time:      17272
71793873   =   yrday
fracday
Element set:     905
Inclination:       51
6409  deg
RA of node:       237
2308  deg
Eccentricity:     
0004605     
Arg of perigee:   322
6003  deg
Mean anomaly:      37
4828  deg
Mean motion:   15
54025101  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3800
Checksum:              290


Coasting Arc #7 (Orbit 3815)
---------------------------------------

Vector Time (GMT): 2017/273/16:53:40
293
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4991840
54                 A    =         6780522
19  meter
 Y    =         373208
31  meter          E    =           
0009003
 Z    =        4572911
64                 I    =           51
33492
 XDOT =       2269
289371                 Wp   =           34
50040
 YDOT =       6676
313533  meter/sec      RA   =          231
24261  deg
 ZDOT =      -3011
847246                 TA   =           85
75372
                                          MA   =           85
65084
                                          Ha   =            220
806  n
mi
                                          Hp   =            215
592

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16377429
59                 X    =         4965083
16
 Y    =        1224436
73  feet           Y    =          428881
27  meter
 Z    =       15002990
95                 Z    =         4597095
54
 XDOT =       7445
175102                 XDOT =        2209
094540
 YDOT =      21903
915790  feet/sec       YDOT =        6701
353443  meter/sec
 ZDOT =      -9881
388604                 ZDOT =       -3000
970479

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3429832
33                 X    =        -1045412
89
 Y    =       15960369
38  feet           Y    =         4864720
59  meter
 Z    =       15109998
10                 Z    =         4605527
42
 XDOT =     -21557
549299                 XDOT =       -6570
741026
 YDOT =       4709
005297  feet/sec       YDOT =        1435
304815  meter/sec
 ZDOT =      -9834
140040                 ZDOT =       -2997
445884


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   17273
74684601  
00016717  00000-0  10270-3 0  9069
2 25544  51
6414 232
1025 0004752 326
6065  33
4787 15
54063844 38164


Satellite: ISS
Catalog Number: 25544
Epoch time:      17273
74684601   =   yrday
fracday
Element set:     906
Inclination:       51
6414  deg
RA of node:       232
1025  deg
Eccentricity:     
0004752     
Arg of perigee:   326
6065  deg
Mean anomaly:      33
4787  deg
Mean motion:   15
54063844  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3816
Checksum:              307


Coasting Arc #8 (Orbit 3821)
---------------------------------------

Vector Time (GMT): 2017/274/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3495673
76                 A    =         6788955
85  meter
 Y    =       -5665510
40  meter          E    =           
0014172
 Z    =        1287243
65                 I    =           51
36947
 XDOT =       4744
584954                 Wp   =           42
18794
 YDOT =      -1600
652714  meter/sec      RA   =          229
43560  deg
 ZDOT =       5812
652401                 TA   =          331
87703
                                          MA   =          331
95351
                                          Ha   =            220
863  n
mi
                                          Hp   =            215
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11468745
95                 X    =        -3438313
54
 Y    =      -18587632
55  feet           Y    =        -5704280
57  meter
 Z    =        4223240
31                 Z    =         1270402
52
 XDOT =      15566
223602                 XDOT =        4733
896118
 YDOT =      -5251
485282  feet/sec       YDOT =       -1547
654754  meter/sec
 ZDOT =      19070
381894                 ZDOT =        5835
674403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20020892
01                 X    =        -6102367
89
 Y    =       -8764357
39  feet           Y    =        -2671376
13  meter
 Z    =        4149445
57                 Z    =         1264751
01
 XDOT =       9084
756427                 XDOT =        2769
033759
 YDOT =     -11633
031422  feet/sec       YDOT =       -3545
747977  meter/sec
 ZDOT =      19172
513895                 ZDOT =        5843
782235


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   17274
13268617  
00016717  00000-0  10270-3 0  9079
2 25544  51
6407 230
1743 0004160 326
2490  33
8397 15
54025346 38225


Satellite: ISS
Catalog Number: 25544
Epoch time:      17274
13268617   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:       230
1743  deg
Eccentricity:     
0004160     
Arg of perigee:   326
2490  deg
Mean anomaly:      33
8397  deg
Mean motion:   15
54025346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3822
Checksum:              298


Coasting Arc #9 (Orbit 3836)
---------------------------------------

Vector Time (GMT): 2017/275/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2501546
51                 A    =         6786224
09  meter
 Y    =        5633500
40  meter          E    =           
0002307
 Z    =       -2842197
32                 I    =           51
38197
 XDOT =      -5758
594793                 Wp   =           57
10374
 YDOT =          7
769802  meter/sec      RA   =          224
44381  deg
 ZDOT =      -5054
764017                 TA   =          155
30291
                                          MA   =          155
29186
                                          Ha   =            220
931  n
mi
                                          Hp   =            215
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8207173
58                 X    =         2452171
34
 Y    =       18482612
87  feet           Y    =         5661198
01  meter
 Z    =       -9324794
36                 Z    =        -2830166
08
 XDOT =     -18893
027537                 XDOT =       -5733
700017
 YDOT =         25
491475  feet/sec       YDOT =         -56
488098  meter/sec
 ZDOT =     -16583
871447                 ZDOT =       -5082
677133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17482810
33                 X    =         5328760
59
 Y    =       10212383
45  feet           Y    =         3112734
48  meter
 Z    =       -9272272
29                 Z    =        -2826188
59
 XDOT =     -14513
071006                 XDOT =       -4423
584043
 YDOT =       9681
108794  feet/sec       YDOT =        2950
801960  meter/sec
 ZDOT =     -16707
453279                 ZDOT =       -5092
431760


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   17275
09727970  
00016717  00000-0  10270-3 0  9088
2 25544  51
6403 225
3671 0004139 328
4443  31
6461 15
54031898 38378


Satellite: ISS
Catalog Number: 25544
Epoch time:      17275
09727970   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:       225
3671  deg
Eccentricity:     
0004139     
Arg of perigee:   328
4443  deg
Mean anomaly:      31
6461  deg
Mean motion:   15
54031898  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3837
Checksum:              320


Coasting Arc #10 (Orbit 3852)
---------------------------------------

Vector Time (GMT): 2017/276/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1243344
99                 A    =         6782391
31  meter
 Y    =       -5256038
91  meter          E    =           
0008428
 Z    =        4094218
46                 I    =           51
39438
 XDOT =       6509
593401                 Wp   =           81
76926
 YDOT =       1425
322876  meter/sec      RA   =          219
44398  deg
 ZDOT =       3801
110545                 TA   =          328
85733
                                          MA   =          328
90725
                                          Ha   =            220
935  n
mi
                                          Hp   =            215
379

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4079215
86                 X    =        -1204365
98
 Y    =      -17244222
14  feet           Y    =        -5269724
38  meter
 Z    =       13432475
27                 Z    =         4088273
98
 XDOT =      21356
933731                 XDOT =        6474
707214
 YDOT =       4676
256155  feet/sec       YDOT =        1497
923013  meter/sec
 ZDOT =      12470
835123                 ZDOT =        3832
647397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13624851
15                 X    =        -4152854
63
 Y    =      -11360223
63  feet           Y    =        -3462596
16  meter
 Z    =       13406839
35                 Z    =         4086404
63
 XDOT =      19041
140643                 XDOT =        5803
739668
 YDOT =      -7933
371850  feet/sec       YDOT =       -2418
091740  meter/sec
 ZDOT =      12610
285394                 ZDOT =        3843
614988


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   17276
12617147  
00016717  00000-0  10270-3 0  9098
2 25544  51
6410 220
2387 0004136 331
5255  28
5671 15
54076511 38534


Satellite: ISS
Catalog Number: 25544
Epoch time:      17276
12617147   =   yrday
fracday
Element set:     909
Inclination:       51
6410  deg
RA of node:       220
2387  deg
Eccentricity:     
0004136     
Arg of perigee:   331
5255  deg
Mean anomaly:      28
5671  deg
Mean motion:   15
54076511  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3853
Checksum:              296


Coasting Arc #11 (Orbit 3867)
---------------------------------------

Vector Time (GMT): 2017/277/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -223927
74                 A    =         6779208
06  meter
 Y    =        4637177
09  meter          E    =           
0012442
 Z    =       -4951249
27                 I    =           51
40969
 XDOT =      -6865
253105                 Wp   =           54
43321
 YDOT =      -2628
658388  meter/sec      RA   =          214
43644  deg
 ZDOT =      -2148
144669                 TA   =          194
51956
                                          MA   =          194
55533
                                          Ha   =            221
112  n
mi
                                          Hp   =            215
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -734671
06                 X    =         -251714
28
 Y    =       15213835
60  feet           Y    =         4634516
94  meter
 Z    =      -16244256
14                 Z    =        -4952405
17
 XDOT =     -22523
796275                 XDOT =       -6824
913776
 YDOT =      -8624
207309  feet/sec       YDOT =       -2705
205077  meter/sec
 ZDOT =      -7047
718729                 ZDOT =       -2181
395898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8779478
35                 X    =         2675985
00
 Y    =       12439276
40  feet           Y    =         3791491
45  meter
 Z    =      -16249970
93                 Z    =        -4952991
14
 XDOT =     -22166
261435                 XDOT =       -6756
276485
 YDOT =       6231
963992  feet/sec       YDOT =        1899
502625  meter/sec
 ZDOT =      -7194
618850                 ZDOT =       -2192
919825


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   17277
09075257  
00016717  00000-0  10270-3 0  9107
2 25544  51
6414 215
4315 0004285 335
0062  25
0882 15
54040662 38685


Satellite: ISS
Catalog Number: 25544
Epoch time:      17277
09075257   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       215
4315  deg
Eccentricity:     
0004285     
Arg of perigee:   335
0062  deg
Mean anomaly:      25
0882  deg
Mean motion:   15
54040662  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3868
Checksum:              296


Coasting Arc #12 (Orbit 3873)
---------------------------------------

Vector Time (GMT): 2017/277/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         596522
81                 A    =         6780117
12  meter
 Y    =        4843545
08  meter          E    =           
0011868
 Z    =       -4718028
92                 I    =           51
42122
 XDOT =      -6917
064789                 Wp   =           48
02482
 YDOT =      -1819
029460  meter/sec      RA   =          212
51844  deg
 ZDOT =      -2738
649017                 TA   =          194
73708
                                          MA   =          194
77170
                                          Ha   =            221
322  n
mi
                                          Hp   =            215
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1957095
82                 X    =          565234
78
 Y    =       15890895
94  feet           Y    =         4850040
21  meter
 Z    =      -15479097
52                 Z    =        -4715207
83
 XDOT =     -22693
782116                 XDOT =       -6882
906668
 YDOT =      -5967
944422  feet/sec       YDOT =       -1896
190189  meter/sec
 ZDOT =      -8985
068954                 ZDOT =       -2772
167108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1072835
43                 X    =         -327000
24
 Y    =      -15986469
70  feet           Y    =        -4872675
97  meter
 Z    =      -15467225
62                 Z    =        -4714410
37
 XDOT =      21056
539733                 XDOT =        6418
033311
 YDOT =       7434
106929  feet/sec       YDOT =        2265
915792  meter/sec
 ZDOT =      -9133
260166                 ZDOT =       -2783
817699


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   17277
47658341  
00016717  00000-0  10270-3 0  9111
2 25544  51
6393 213
5099 0004671 341
6908  18
4076 15
54063529 38745


Satellite: ISS
Catalog Number: 25544
Epoch time:      17277
47658341   =   yrday
fracday
Element set:     911
Inclination:       51
6393  deg
RA of node:       213
5099  deg
Eccentricity:     
0004671     
Arg of perigee:   341
6908  deg
Mean anomaly:      18
4076  deg
Mean motion:   15
54063529  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3874
Checksum:              330


Coasting Arc #13 (Orbit 3889)
---------------------------------------

Vector Time (GMT): 2017/278/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1006636
53                 A    =         6777741
87  meter
 Y    =       -4181660
14  meter          E    =           
0003169
 Z    =        5236308
97                 I    =           51
44186
 XDOT =       7061
526649                 Wp   =           32
58040
 YDOT =       2849
907056  meter/sec      RA   =          207
50883  deg
 ZDOT =        920
744813                 TA   =           48
60300
                                          MA   =           48
57576
                                          Ha   =            221
272  n
mi
                                          Hp   =            215
020

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3302613
30                 X    =         1027886
35
 Y    =      -13719357
40  feet           Y    =        -4170283
71  meter
 Z    =       17179491
37                 Z    =         5241251
15
 XDOT =      23167
738351                 XDOT =        7024
660804
 YDOT =       9350
088765  feet/sec       YDOT =        2928
667863  meter/sec
 ZDOT =       3020
816314                 ZDOT =         954
958106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3798665
25                 X    =        -1157833
17
 Y    =       13561983
93  feet           Y    =         4133692
70  meter
 Z    =       17201909
19                 Z    =         5243141
92
 XDOT =     -21718
274502                 XDOT =       -6619
730068
 YDOT =     -10096
709531  feet/sec       YDOT =       -3077
477065  meter/sec
 ZDOT =       3171
968659                 ZDOT =         966
816047


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   17278
50545737  
00016717  00000-0  10270-3 0  9121
2 25544  51
6394 208
3825 0004733 343
9357  16
1645 15
54098346 38907


Satellite: ISS
Catalog Number: 25544
Epoch time:      17278
50545737   =   yrday
fracday
Element set:     912
Inclination:       51
6394  deg
RA of node:       208
3825  deg
Eccentricity:     
0004733     
Arg of perigee:   343
9357  deg
Mean anomaly:      16
1645  deg
Mean motion:   15
54098346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3890
Checksum:              332


Coasting Arc #14 (Orbit 3904)
---------------------------------------

Vector Time (GMT): 2017/279/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2630255
67                 A    =         6777787
27  meter
 Y    =        3423357
09  meter          E    =           
0013589
 Z    =       -5236178
69                 I    =           51
47175
 XDOT =      -6676
353722                 Wp   =           78
72028
 YDOT =      -3619
819740  meter/sec      RA   =          202
49674  deg
 ZDOT =        991
882522                 TA   =          200
78089
                                          MA   =          200
83619
                                          Ha   =            221
438  n
mi
                                          Hp   =            214
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8629447
72                 X    =        -2642905
78
 Y    =       11231486
52  feet           Y    =         3393872
39  meter
 Z    =      -17179063
94                 Z    =        -5248987
06
 XDOT =     -21904
047643                 XDOT =       -6640
197904
 YDOT =     -11876
049016  feet/sec       YDOT =       -3694
277002  meter/sec
 ZDOT =       3254
207749                 ZDOT =         959
538503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8821315
35                 X    =         2688736
92
 Y    =      -10992310
02  feet           Y    =        -3350456
09  meter
 Z    =      -17236223
81                 Z    =        -5253601
02
 XDOT =      20789
447980                 XDOT =        6336
623744
 YDOT =      11829
295552  feet/sec       YDOT =        3605
569284  meter/sec
 ZDOT =       3111
417363                 ZDOT =         948
360012


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   17279
47002062  
00016717  00000-0  10270-3 0  9138
2 25544  51
6398 203
5744 0004695 347
8996  12
2043 15
54081951 39057


Satellite: ISS
Catalog Number: 25544
Epoch time:      17279
47002062   =   yrday
fracday
Element set:     913
Inclination:       51
6398  deg
RA of node:       203
5744  deg
Eccentricity:     
0004695     
Arg of perigee:   347
8996  deg
Mean anomaly:      12
2043  deg
Mean motion:   15
54081951  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3905
Checksum:              319


Coasting Arc #15 (Orbit 3920)
---------------------------------------

Vector Time (GMT): 2017/280/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4166329
04                 A    =         6780021
44  meter
 Y    =       -2588112
69  meter          E    =           
0010420
 Z    =        4679260
14                 I    =           51
51058
 XDOT =       5779
002038                 Wp   =           38
04310
 YDOT =       4175
778681  meter/sec      RA   =          197
49059  deg
 ZDOT =      -2824
482310                 TA   =           80
08522
                                          MA   =           79
96761
                                          Ha   =            221
446  n
mi
                                          Hp   =            214
755

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13669058
55                 X    =         4172230
28
 Y    =       -8491183
35  feet           Y    =        -2541488
45  meter
 Z    =       15351903
34                 Z    =         4699513
95
 XDOT =      18959
980441                 XDOT =        5745
598125
 YDOT =      13700
061290  feet/sec       YDOT =        4240
216348  meter/sec
 ZDOT =      -9266
674247                 ZDOT =       -2796
490655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13654138
29                 X    =        -4161781
35
 Y    =        8350764
17  feet           Y    =         2545312
92  meter
 Z    =       15441940
87                 Z    =         4706703
58
 XDOT =     -18270
371454                 XDOT =       -5568
809219
 YDOT =     -12897
368698  feet/sec       YDOT =       -3931
117979  meter/sec
 ZDOT =      -9143
217948                 ZDOT =       -2786
852831


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   17280
49887710  
00016717  00000-0  10270-3 0  9144
2 25544  51
6403 198
4464 0004745 351
7248   8
3826 15
54097350 39218


Satellite: ISS
Catalog Number: 25544
Epoch time:      17280
49887710   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:       198
4464  deg
Eccentricity:     
0004745     
Arg of perigee:   351
7248  deg
Mean anomaly:       8
3826  deg
Mean motion:   15
54097350  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3921
Checksum:              326


Coasting Arc #16 (Orbit 3935)
---------------------------------------

Vector Time (GMT): 2017/281/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5429123
48                 A    =         6783596
34  meter
 Y    =        1774010
29  meter          E    =           
0006409
 Z    =       -3661062
03                 I    =           51
55337
 XDOT =      -4405
045885                 Wp   =           54
95499
 YDOT =      -4515
998369  meter/sec      RA   =          192
49464  deg
 ZDOT =       4353
127778                 TA   =          261
49137
                                          MA   =          261
56400
                                          Ha   =            221
560  n
mi
                                          Hp   =            214
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17812084
90                 X    =        -5430773
35
 Y    =        5820243
74  feet           Y    =         1713288
58  meter
 Z    =      -12011358
37                 Z    =        -3687439
83
 XDOT =     -14452
250280                 XDOT =       -4375
365269
 YDOT =     -14816
267616  feet/sec       YDOT =       -4565
092264  meter/sec
 ZDOT =      14281
915281                 ZDOT =        4331
801399

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17691860
22                 X    =         5392479
00
 Y    =       -5942858
20  feet           Y    =        -1811383
18  meter
 Z    =      -12128431
64                 Z    =        -3696745
96
 XDOT =      14215
310012                 XDOT =        4332
826492
 YDOT =      13423
118860  feet/sec       YDOT =        4091
366629  meter/sec
 ZDOT =      14188
014863                 ZDOT =        4324
506930


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   17281
46342136  
00016717  00000-0  10270-3 0  9151
2 25544  51
6395 193
6386 0004797 355
6848   4
4263 15
54106793 39364


Satellite: ISS
Catalog Number: 25544
Epoch time:      17281
46342136   =   yrday
fracday
Element set:     915
Inclination:       51
6395  deg
RA of node:       193
6386  deg
Eccentricity:     
0004797     
Arg of perigee:   355
6848  deg
Mean anomaly:       4
4263  deg
Mean motion:   15
54106793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3936
Checksum:              339


Coasting Arc #17 (Orbit 3951)
---------------------------------------

Vector Time (GMT): 2017/282/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6336860
80                 A    =         6787156
72  meter
 Y    =        -946286
22  meter          E    =           
0013079
 Z    =        2228639
12                 I    =           51
59784
 XDOT =       2630
105458                 Wp   =           88
31736
 YDOT =       4705
881321  meter/sec      RA   =          187
51133  deg
 ZDOT =      -5452
189283                 TA   =           66
89727
                                          MA   =           66
75947
                                          Ha   =            221
647  n
mi
                                          Hp   =            214
455

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20790225
73                 X    =         6336145
57
 Y    =       -3104613
58  feet           Y    =         -875426
97  meter
 Z    =        7311808
12                 Z    =         2259420
66
 XDOT =       8628
954915                 XDOT =        2603
772241
 YDOT =      15439
243179  feet/sec       YDOT =        4735
145356  meter/sec
 ZDOT =     -17887
760116                 ZDOT =       -5439
477023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20660694
37                 X    =        -6297379
64
 Y    =        3604600
69  feet           Y    =         1098682
29  meter
 Z    =        7448302
59                 Z    =         2270242
63
 XDOT =      -8853
978994                 XDOT =       -2698
692797
 YDOT =     -13715
188979  feet/sec       YDOT =       -4180
389601  meter/sec
 ZDOT =     -17832
037041                 ZDOT =       -5435
204890


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   17282
49226046  
00016717  00000-0  10270-3 0  9167
2 25544  51
6399 188
5103 0004766 358
8612   1
2529 15
54125086 39522


Satellite: ISS
Catalog Number: 25544
Epoch time:      17282
49226046   =   yrday
fracday
Element set:     916
Inclination:       51
6399  deg
RA of node:       188
5103  deg
Eccentricity:     
0004766     
Arg of perigee:   358
8612  deg
Mean anomaly:       1
2529  deg
Mean motion:   15
54125086  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3952
Checksum:              323


Coasting Arc #18 (Orbit 3966)
---------------------------------------

Vector Time (GMT): 2017/283/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904841
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6752831
67                 A    =         6789151
63  meter
 Y    =         170800
31  meter          E    =           
0014776
 Z    =        -593257
06                 I    =           51
63693
 XDOT =       -639
104355                 Wp   =           29
22132
 YDOT =      -4764
979366  meter/sec      RA   =          182
53737  deg
 ZDOT =       5978
227756                 TA   =          324
37234
                                          MA   =          324
47088
                                          Ha   =            221
703  n
mi
                                          Hp   =            214
401

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22154959
54                 X    =        -6751357
91
 Y    =         560368
47  feet           Y    =           95293
75  meter
 Z    =       -1946381
41                 Z    =         -626057
31
 XDOT =      -2096
799066                 XDOT =        -614
813470
 YDOT =     -15633
134403  feet/sec       YDOT =       -4771
990152  meter/sec
 ZDOT =      19613
608123                 ZDOT =        5975
182359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22099579
75                 X    =         6735951
91
 Y    =       -1475748
82  feet           Y    =         -449808
24  meter
 Z    =       -2091742
35                 Z    =         -637563
07
 XDOT =       2762
615326                 XDOT =         842
045151
 YDOT =      13914
536164  feet/sec       YDOT =        4241
150623  meter/sec
 ZDOT =      19600
720333                 ZDOT =        5974
299557


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   17283
45678763  
00016717  00000-0  10270-3 0  9172
2 25544  51
6398 183
7020 0004834   1
7024 358
4145 15
54130585 39670


Satellite: ISS
Catalog Number: 25544
Epoch time:      17283
45678763   =   yrday
fracday
Element set:     917
Inclination:       51
6398  deg
RA of node:       183
7020  deg
Eccentricity:     
0004834     
Arg of perigee:     1
7024  deg
Mean anomaly:     358
4145  deg
Mean motion:   15
54130585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3967
Checksum:              326
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