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

 
Date: July 6th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 438 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


190/12:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 216 1

191/01:39:12 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 216 1

191/20:25:30 000 -0 0 0 2 0 2
N/A -0 2 0 0 220 1
000/00:01:00 000 0 0 -0 0 216 0

193/18:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 215 9

197/12:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 215 7

199/12:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 215 5

Coasting Arc #1 (Orbit 151)
---------------------------------------

Vector Time (GMT): 2018/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3988443
38                 A    =         6783059
54  meter
 Y    =       -3856067
71  meter          E    =           
0007449
 Z    =        3898083
63                 I    =           51
26745
 XDOT =       2030
843729                 Wp   =          103
93677
 YDOT =       6193
637988  meter/sec      RA   =          281
66277  deg
 ZDOT =       4040
680364                 TA   =          303
53980
                                          MA   =          303
61093
                                          Ha   =            219
678  n
mi
                                          Hp   =            216
153

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13085444
16                 X    =         4012331
80
 Y    =      -12651140
77  feet           Y    =        -3811332
96  meter
 Z    =       12788988
29                 Z    =         3917515
71
 XDOT =       6662
873128                 XDOT =        1941
806414
 YDOT =      20320
334605  feet/sec       YDOT =        6215
850084  meter/sec
 ZDOT =      13256
825342                 ZDOT =        4050
329760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15343007
55                 X    =        -4676548
70
 Y    =       -9676120
80  feet           Y    =        -2949281
62  meter
 Z    =       12876460
64                 Z    =         3924745
20
 XDOT =      17510
774771                 XDOT =        5337
284150
 YDOT =     -10032
461954  feet/sec       YDOT =       -3057
894404  meter/sec
 ZDOT =      13299
093997                 ZDOT =        4053
563850


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   18187
55581090  
00016717  00000-0  10270-3 0  9005
2 25544  51
6406 282
1722 0003730 270
9546  89
1179 15
54038025  1520


Satellite: ISS
Catalog Number: 25544
Epoch time:      18187
55581090   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:       282
1722  deg
Eccentricity:     
0003730     
Arg of perigee:   270
9546  deg
Mean anomaly:      89
1179  deg
Mean motion:   15
54038025  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             152
Checksum:              299


Coasting Arc #2 (Orbit 166)
---------------------------------------

Vector Time (GMT): 2018/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4168613
79                 A    =         6779747
03  meter
 Y    =        2321764
39  meter          E    =           
0008310
 Z    =       -4824240
64                 I    =           51
25005
 XDOT =      -1148
883240                 Wp   =           61
91701
 YDOT =      -7165
685692  meter/sec      RA   =          276
64677  deg
 ZDOT =      -2455
289116                 TA   =          183
81642
                                          MA   =          183
82276
                                          Ha   =            219
807  n
mi
                                          Hp   =            216
136

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13676554
42                 X    =        -4170832
99
 Y    =        7617337
24  feet           Y    =         2275136
15  meter
 Z    =      -15827561
15                 Z    =        -4844495
45
 XDOT =      -3769
301970                 XDOT =       -1056
742703
 YDOT =     -23509
467494  feet/sec       YDOT =       -7178
017864  meter/sec
 ZDOT =      -8055
410486                 ZDOT =       -2460
646905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10777391
68                 X    =         3284948
98
 Y    =       11226450
90  feet           Y    =         3421822
24  meter
 Z    =      -15918488
87                 Z    =        -4851955
41
 XDOT =     -21007
242203                 XDOT =       -6403
007424
 YDOT =       8709
524898  feet/sec       YDOT =        2654
663189  meter/sec
 ZDOT =      -8078
357690                 ZDOT =       -2462
283424


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   18188
52041518  
00016717  00000-0  10270-3 0  9010
2 25544  51
6403 277
3651 0003854 275
3432  84
7281 15
53996309  1672


Satellite: ISS
Catalog Number: 25544
Epoch time:      18188
52041518   =   yrday
fracday
Element set:     901
Inclination:       51
6403  deg
RA of node:       277
3651  deg
Eccentricity:     
0003854     
Arg of perigee:   275
3432  deg
Mean anomaly:      84
7281  deg
Mean motion:   15
53996309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             167
Checksum:              316


Coasting Arc #3 (Orbit 182)
---------------------------------------

Vector Time (GMT): 2018/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4238401
50                 A    =         6777725
10  meter
 Y    =        -596243
62  meter          E    =           
0001181
 Z    =        5256258
63                 I    =           51
24185
 XDOT =        290
794777                 Wp   =          244
80661
 YDOT =       7636
365816  meter/sec      RA   =          271
62232  deg
 ZDOT =        631
364979                 TA   =          199
13004
                                          MA   =          199
13447
                                          Ha   =            219
645  n
mi
                                          Hp   =            216
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13905516
73                 X    =         4219221
72
 Y    =       -1956179
85  feet           Y    =         -548954
74  meter
 Z    =       17244943
02                 Z    =         5276800
67
 XDOT =        954
051107                 XDOT =         202
314385
 YDOT =      25053
693622  feet/sec       YDOT =        7639
122886  meter/sec
 ZDOT =       2071
407410                 ZDOT =         632
563540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5572683
65                 X    =        -1698553
98
 Y    =      -12765374
21  feet           Y    =        -3890886
06  meter
 Z    =       17336911
87                 Z    =         5284290
74
 XDOT =      22958
412669                 XDOT =        6997
724181
 YDOT =      -7201
679284  feet/sec       YDOT =       -2195
071846  meter/sec
 ZDOT =       2075
697568                 ZDOT =         632
672619


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   18189
54932176  
00016717  00000-0  10270-3 0  9023
2 25544  51
6412 272
2366 0003812 281
5298  78
5426 15
54044470  1836


Satellite: ISS
Catalog Number: 25544
Epoch time:      18189
54932176   =   yrday
fracday
Element set:     902
Inclination:       51
6412  deg
RA of node:       272
2366  deg
Eccentricity:     
0003812     
Arg of perigee:   281
5298  deg
Mean anomaly:      78
5426  deg
Mean motion:   15
54044470  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             183
Checksum:              313


Coasting Arc #4 (Orbit 197)
---------------------------------------

Vector Time (GMT): 2018/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4230156
09                 A    =         6778200
09  meter
 Y    =       -1177489
84  meter          E    =           
0010333
 Z    =       -5172803
86                 I    =           51
24206
 XDOT =        562
338404                 Wp   =           96
93717
 YDOT =      -7535
938300  meter/sec      RA   =          266
59656  deg
 ZDOT =       1256
491476                 TA   =          185
19948
                                          MA   =          185
21022
                                          Ha   =            219
929  n
mi
                                          Hp   =            215
993

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13878464
85                 X    =        -4191547
93
 Y    =       -3863155
63  feet           Y    =        -1224577
79  meter
 Z    =      -16971141
28                 Z    =        -5193258
88
 XDOT =       1844
942269                 XDOT =         640
462172
 YDOT =     -24724
207022  feet/sec       YDOT =       -7529
213198  meter/sec
 ZDOT =       4122
347363                 ZDOT =        1259
411848

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         204637
55                 X    =           62373
52
 Y    =       14296340
03  feet           Y    =         4357524
44  meter
 Z    =      -17062478
71                 Z    =        -5200643
51
 XDOT =     -23179
322754                 XDOT =       -7065
057576
 YDOT =       5264
920581  feet/sec       YDOT =        1604
747793  meter/sec
 ZDOT =       4136
455361                 ZDOT =        1260
791594


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   18190
51392250  
00016717  00000-0  10270-3 0  9036
2 25544  51
6399 267
4297 0003761 287
1916  72
8824 15
54018618  1981


Satellite: ISS
Catalog Number: 25544
Epoch time:      18190
51392250   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       267
4297  deg
Eccentricity:     
0003761     
Arg of perigee:   287
1916  deg
Mean anomaly:      72
8824  deg
Mean motion:   15
54018618  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             198
Checksum:              331


Coasting Arc #5 (Orbit 198)
---------------------------------------

Vector Time (GMT): 2018/190/12:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944270
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4254969
14                 A    =         6777779
13  meter
 Y    =         577825
26  meter          E    =           
0002709
 Z    =        5245066
35                 I    =           51
24112
 XDOT =       -121
121682                 Wp   =          340
68592
 YDOT =       7631
083940  meter/sec      RA   =          266
44462  deg
 ZDOT =       -740
020320                 TA   =          116
43736
                                          MA   =          116
40957
                                          Ha   =            219
734  n
mi
                                          Hp   =            216
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13959872
50                 X    =         4222713
74
 Y    =        1895752
17  feet           Y    =          625226
20  meter
 Z    =       17208222
92                 Z    =         5265657
25
 XDOT =       -397
380847                 XDOT =        -202
850931
 YDOT =      25036
364632  feet/sec       YDOT =        7629
272598  meter/sec
 ZDOT =      -2427
888188                 ZDOT =        -740
806152

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4775105
67                 X    =        -1455452
21
 Y    =      -13133716
79  feet           Y    =        -4003156
88  meter
 Z    =       17300251
50                 Z    =         5273116
66
 XDOT =      21370
132450                 XDOT =        6513
616371
 YDOT =     -10984
136444  feet/sec       YDOT =       -3347
964788  meter/sec
 ZDOT =      -2432
460655                 ZDOT =        -741
414008


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   18190
57822825  
00016717  00000-0  10270-3 0  9049
2 25544  51
6401 267
1095 0003825 286
8693  73
2040 15
54043301  1990


Satellite: ISS
Catalog Number: 25544
Epoch time:      18190
57822825   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       267
1095  deg
Eccentricity:     
0003825     
Arg of perigee:   286
8693  deg
Mean anomaly:      73
2040  deg
Mean motion:   15
54043301  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             199
Checksum:              303


Coasting Arc #6 (Orbit 206)
---------------------------------------

Vector Time (GMT): 2018/191/01:39:12
000
Vector Time (MET): N/A
Weight (LBS)     : 959630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2582702
87                 A    =         6783276
51  meter
 Y    =        4942212
48  meter          E    =           
0004168
 Z    =       -3867154
82                 I    =           51
26037
 XDOT =      -3860
718925                 Wp   =           37
71774
 YDOT =      -5211
243895  meter/sec      RA   =          263
78495  deg
 ZDOT =      -4080
651595                 TA   =          189
21904
                                          MA   =          189
22669
                                          Ha   =            220
043  n
mi
                                          Hp   =            216
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8473434
63                 X    =        -2618991
53
 Y    =       16214607
89  feet           Y    =         4913128
58  meter
 Z    =      -12687515
82                 Z    =        -3879788
10
 XDOT =     -12666
400671                 XDOT =       -3782
336799
 YDOT =     -17097
256872  feet/sec       YDOT =       -5253
978256  meter/sec
 ZDOT =     -13387
964549                 ZDOT =       -4099
215999

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17673520
81                 X    =        -5386889
14
 Y    =        4572163
97  feet           Y    =         1393595
58  meter
 Z    =      -12744710
26                 Z    =        -3884587
69
 XDOT =       4674
058156                 XDOT =        1424
652926
 YDOT =     -19488
652435  feet/sec       YDOT =       -5940
141262  meter/sec
 ZDOT =     -13470
293866                 ZDOT =       -4105
745570


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   18191
09268209  
00016717  00000-0  10270-3 0  9058
2 25544  51
6400 264
5477 0003960 293
7031  66
3706 15
54011901  2070


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
09268209   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       264
5477  deg
Eccentricity:     
0003960     
Arg of perigee:   293
7031  deg
Mean anomaly:      66
3706  deg
Mean motion:   15
54011901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             207
Checksum:              292


Coasting Arc #7 (Orbit 218)
---------------------------------------

Vector Time (GMT): 2018/191/20:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959612
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4347412
00                 A    =         6778847
91  meter
 Y    =       -1292534
49  meter          E    =           
0009376
 Z    =       -5046500
77                 I    =           51
24739
 XDOT =        129
115690                 Wp   =           98
02051
 YDOT =      -7446
095912  meter/sec      RA   =          259
82266  deg
 ZDOT =       1797
493223                 TA   =          189
47985
                                          MA   =          189
49756
                                          Ha   =            220
118  n
mi
                                          Hp   =            216
033

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14263162
73                 X    =        -4308122
28
 Y    =       -4240598
73  feet           Y    =        -1340929
76  meter
 Z    =      -16556761
04                 Z    =        -5067523
69
 XDOT =        423
607907                 XDOT =         203
639146
 YDOT =     -24429
448530  feet/sec       YDOT =       -7444
235652  meter/sec
 ZDOT =       5897
287476                 ZDOT =        1798
300234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11698438
43                 X    =         3565684
03
 Y    =       -9024947
70  feet           Y    =        -2750804
06  meter
 Z    =      -16650636
09                 Z    =        -5075113
88
 XDOT =      18964
375026                 XDOT =        5780
341508
 YDOT =      13703
066663  feet/sec       YDOT =        4176
694719  meter/sec
 ZDOT =       5901
912269                 ZDOT =        1798
902860


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   18191
86436195  
00016717  00000-0  10270-3 0  9065
2 25544  51
6387 260
7002 0003967 296
7107  63
3639 15
53983054  2191


Satellite: ISS
Catalog Number: 25544
Epoch time:      18191
86436195   =   yrday
fracday
Element set:     906
Inclination:       51
6387  deg
RA of node:       260
7002  deg
Eccentricity:     
0003967     
Arg of perigee:   296
7107  deg
Mean anomaly:      63
3639  deg
Mean motion:   15
53983054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             219
Checksum:              330


Coasting Arc #8 (Orbit 234)
---------------------------------------

Vector Time (GMT): 2018/192/20:26:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959612
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4362138
96                 A    =         6781801
63  meter
 Y    =        2915665
83  meter          E    =           
0007750
 Z    =        4295024
47                 I    =           51
26445
 XDOT =      -1066
298109                 Wp   =           48
82580
 YDOT =       6745
355846  meter/sec      RA   =          254
80377  deg
 ZDOT =      -3486
971703                 TA   =           76
87818
                                          MA   =           76
79170
                                          Ha   =            220
189  n
mi
                                          Hp   =            216
115

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14311479
54                 X    =         4308348
22
 Y    =        9565832
77  feet           Y    =         2964144
79  meter
 Z    =       14091287
62                 Z    =         4316083
88
 XDOT =      -3498
353376                 XDOT =       -1124
709572
 YDOT =      22130
432564  feet/sec       YDOT =        6733
105751  meter/sec
 ZDOT =     -11440
195876                 ZDOT =       -3492
292102

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15957208
72                 X    =        -4863757
22
 Y    =        6248026
25  feet           Y    =         1904398
40  meter
 Z    =       14185120
65                 Z    =         4323624
77
 XDOT =     -15794
836159                 XDOT =       -4814
266061
 YDOT =     -14242
596219  feet/sec       YDOT =       -4341
143327  meter/sec
 ZDOT =     -11464
905551                 ZDOT =       -3494
503212


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   18192
89328883  
00016717  00000-0  10270-3 0  9074
2 25544  51
6389 255
5725 0004022 301
9734  58
1027 15
53991179  2353


Satellite: ISS
Catalog Number: 25544
Epoch time:      18192
89328883   =   yrday
fracday
Element set:     907
Inclination:       51
6389  deg
RA of node:       255
5725  deg
Eccentricity:     
0004022     
Arg of perigee:   301
9734  deg
Mean anomaly:      58
1027  deg
Mean motion:   15
53991179  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             235
Checksum:              331


Coasting Arc #9 (Orbit 248)
---------------------------------------

Vector Time (GMT): 2018/193/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959612
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3327151
35                 A    =         6778494
08  meter
 Y    =        2929177
18  meter          E    =           
0011398
 Z    =       -5138149
73                 I    =           51
26011
 XDOT =      -3599
591244                 Wp   =           64
38474
 YDOT =      -6607
584559  meter/sec      RA   =          250
21287  deg
 ZDOT =      -1433
658999                 TA   =          191
71788
                                          MA   =          191
74443
                                          Ha   =            220
380  n
mi
                                          Hp   =            215
938

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10915850
89                 X    =        -3334700
89
 Y    =        9610161
34  feet           Y    =         2891929
30  meter
 Z    =      -16857446
63                 Z    =        -5154329
50
 XDOT =     -11809
682558                 XDOT =       -3518
472034
 YDOT =     -21678
427031  feet/sec       YDOT =       -6647
383871  meter/sec
 ZDOT =      -4703
605641                 ZDOT =       -1450
948367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4855179
80                 X    =         1479858
80
 Y    =      -13619065
97  feet           Y    =        -4151091
31  meter
 Z    =      -16930232
71                 Z    =        -5160334
93
 XDOT =      19755
614102                 XDOT =        6021
511178
 YDOT =      12994
643164  feet/sec       YDOT =        3960
767236  meter/sec
 ZDOT =      -4780
098352                 ZDOT =       -1456
973978


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   18193
79359901  
00016717  00000-0  10270-3 0  9080
2 25544  51
6370 251
0848 0003983 305
4995  54
5786 15
53979796  2491


Satellite: ISS
Catalog Number: 25544
Epoch time:      18193
79359901   =   yrday
fracday
Element set:     908
Inclination:       51
6370  deg
RA of node:       251
0848  deg
Eccentricity:     
0003983     
Arg of perigee:   305
4995  deg
Mean anomaly:      54
5786  deg
Mean motion:   15
53979796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             249
Checksum:              365


Coasting Arc #10 (Orbit 264)
---------------------------------------

Vector Time (GMT): 2018/194/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959612
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4050408
11                 A    =         6777823
53  meter
 Y    =       -1316849
70  meter          E    =           
0003452
 Z    =        5273210
19                 I    =           51
27027
 XDOT =       2886
297195                 Wp   =          350
10028
 YDOT =       7090
316442  meter/sec      RA   =          245
18943  deg
 ZDOT =       -443
069871                 TA   =          104
16658
                                          MA   =          104
12822
                                          Ha   =            220
329  n
mi
                                          Hp   =            216
021

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13288740
52                 X    =         4039218
50
 Y    =       -4320373
03  feet           Y    =        -1271618
57  meter
 Z    =       17300558
38                 Z    =         5292857
91
 XDOT =       9469
478985                 XDOT =        2808
948969
 YDOT =      23262
193051  feet/sec       YDOT =        7122
160592  meter/sec
 ZDOT =      -1453
641309                 ZDOT =        -429
236350

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9300534
79                 X    =        -2834803
00
 Y    =       10281062
53  feet           Y    =         3133667
86  meter
 Z    =       17388656
47                 Z    =         5300062
49
 XDOT =     -19013
413390                 XDOT =       -5795
288401
 YDOT =     -14826
417308  feet/sec       YDOT =       -4519
091996  meter/sec
 ZDOT =      -1392
649172                 ZDOT =        -424
479468


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   18194
82252467  
00016717  00000-0  10270-3 0  9095
2 25544  51
6371 245
9573 0004039 309
3044  50
7750 15
53986235  2653


Satellite: ISS
Catalog Number: 25544
Epoch time:      18194
82252467   =   yrday
fracday
Element set:     909
Inclination:       51
6371  deg
RA of node:       245
9573  deg
Eccentricity:     
0004039     
Arg of perigee:   309
3044  deg
Mean anomaly:      50
7750  deg
Mean motion:   15
53986235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             265
Checksum:              322


Coasting Arc #11 (Orbit 279)
---------------------------------------

Vector Time (GMT): 2018/195/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 959612
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4686761
15                 A    =         6779453
30  meter
 Y    =        -281744
16  meter          E    =           
0008732
 Z    =       -4898205
40                 I    =           51
29073
 XDOT =      -1946
691254                 Wp   =           94
72535
 YDOT =      -7053
353636  meter/sec      RA   =          240
16694  deg
 ZDOT =       2271
167394                 TA   =          197
58656
                                          MA   =          197
61681
                                          Ha   =            220
506  n
mi
                                          Hp   =            215
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15376512
97                 X    =        -4659469
94
 Y    =        -924357
48  feet           Y    =         -334001
58  meter
 Z    =      -16070227
70                 Z    =        -4920905
29
 XDOT =      -6386
782329                 XDOT =       -1878
705912
 YDOT =     -23140
924004  feet/sec       YDOT =       -7074
743020  meter/sec
 ZDOT =       7451
336594                 ZDOT =        2261
875545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13602098
04                 X    =         4145919
48
 Y    =       -6999994
80  feet           Y    =        -2133598
42  meter
 Z    =      -16171790
50                 Z    =        -4929161
74
 XDOT =      16837
907928                 XDOT =        5132
194336
 YDOT =      15619
343149  feet/sec       YDOT =        4760
775792  meter/sec
 ZDOT =       7410
639030                 ZDOT =        2258
762776


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   18195
78713977  
00016717  00000-0  10270-3 0  9101
2 25544  51
6372 241
1491 0004103 312
6536  47
4271 15
53986851  2808


Satellite: ISS
Catalog Number: 25544
Epoch time:      18195
78713977   =   yrday
fracday
Element set:     910
Inclination:       51
6372  deg
RA of node:       241
1491  deg
Eccentricity:     
0004103     
Arg of perigee:   312
6536  deg
Mean anomaly:      47
4271  deg
Mean motion:   15
53986851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             280
Checksum:              313


Coasting Arc #12 (Orbit 295)
---------------------------------------

Vector Time (GMT): 2018/196/18:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944898
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5162000
40                 A    =         6782723
05  meter
 Y    =        1780142
82  meter          E    =           
0009364
 Z    =        4020969
36                 I    =           51
31906
 XDOT =        775
307299                 Wp   =           55
30279
 YDOT =       6562
735149  meter/sec      RA   =          235
15305  deg
 ZDOT =      -3889
028989                 TA   =           75
26894
                                          MA   =           75
16519
                                          Ha   =            220
621  n
mi
                                          Hp   =            215
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16935696
85                 X    =         5122179
40
 Y    =        5840363
59  feet           Y    =         1837644
86  meter
 Z    =       13192156
68                 Z    =         4045947
44
 XDOT =       2543
659116                 XDOT =         720
753786
 YDOT =      21531
283297  feet/sec       YDOT =        6571
100492  meter/sec
 ZDOT =     -12759
281461                 ZDOT =       -3885
394810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17404745
94                 X    =        -5304966
56
 Y    =        3878905
60  feet           Y    =         1182290
43  meter
 Z    =       13303743
18                 Z    =         4054980
92
 XDOT =     -13262
734867                 XDOT =       -4042
481588
 YDOT =     -15671
239498  feet/sec       YDOT =       -4776
593799  meter/sec
 ZDOT =     -12743
823102                 ZDOT =       -3884
317281


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   18196
81606125  
00016717  00000-0  10270-3 0  9113
2 25544  51
6371 236
0208 0004167 318
2421  41
8413 15
54003060  2967


Satellite: ISS
Catalog Number: 25544
Epoch time:      18196
81606125   =   yrday
fracday
Element set:     911
Inclination:       51
6371  deg
RA of node:       236
0208  deg
Eccentricity:     
0004167     
Arg of perigee:   318
2421  deg
Mean anomaly:      41
8413  deg
Mean motion:   15
54003060  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             296
Checksum:              274


Coasting Arc #13 (Orbit 307)
---------------------------------------

Vector Time (GMT): 2018/197/12:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944898
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -737252
60                 A    =         6784031
59  meter
 Y    =       -5644937
37  meter          E    =           
0009653
 Z    =        3679754
25                 I    =           51
33769
 XDOT =       6019
359846                 Wp   =           78
07047
 YDOT =       2024
127481  meter/sec      RA   =          231
41783  deg
 ZDOT =       4303
492793                 TA   =          325
97345
                                          MA   =          326
03531
                                          Ha   =            220
816  n
mi
                                          Hp   =            215
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2418807
73                 X    =         -691948
49
 Y    =      -18520135
73  feet           Y    =        -5652928
79  meter
 Z    =       12072684
56                 Z    =         3676282
64
 XDOT =      19748
555926                 XDOT =        5975
374473
 YDOT =       6640
838191  feet/sec       YDOT =        2091
193872  meter/sec
 ZDOT =      14119
070843                 ZDOT =        4332
625455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13806968
34                 X    =        -4208363
95
 Y    =       12592544
50  feet           Y    =         3838207
56  meter
 Z    =       12057828
12                 Z    =         3675226
01
 XDOT =      -4803
543188                 XDOT =       -1464
119964
 YDOT =     -18934
958820  feet/sec       YDOT =       -5771
375448  meter/sec
 ZDOT =      14249
236701                 ZDOT =        4343
167346


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   18197
58775244  
00016717  00000-0  10270-3 0  9128
2 25544  51
6371 232
1737 0003826 322
7325  37
3561 15
53979380  3089


Satellite: ISS
Catalog Number: 25544
Epoch time:      18197
58775244   =   yrday
fracday
Element set:     912
Inclination:       51
6371  deg
RA of node:       232
1737  deg
Eccentricity:     
0003826     
Arg of perigee:   322
7325  deg
Mean anomaly:      37
3561  deg
Mean motion:   15
53979380  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             308
Checksum:              321


Coasting Arc #14 (Orbit 322)
---------------------------------------

Vector Time (GMT): 2018/198/12:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944898
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -534732
26                 A    =         6780382
38  meter
 Y    =        4877517
97  meter          E    =           
0010248
 Z    =       -4689292
18                 I    =           51
34842
 XDOT =      -6287
499382                 Wp   =           49
59536
 YDOT =      -3371
564539  meter/sec      RA   =          226
40978  deg
 ZDOT =      -2787
432953                 TA   =          192
61802
                                          MA   =          192
64370
                                          Ha   =            220
827  n
mi
                                          Hp   =            215
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1754370
94                 X    =         -566456
57
 Y    =       16002355
54  feet           Y    =         4871361
11  meter
 Z    =      -15384816
87                 Z    =        -4691966
46
 XDOT =     -20628
278812                 XDOT =       -6235
790683
 YDOT =     -11061
563447  feet/sec       YDOT =       -3441
586420  meter/sec
 ZDOT =      -9145
121237                 ZDOT =       -2817
849509

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13963027
83                 X    =         4255930
88
 Y    =       -7987532
92  feet           Y    =        -2434600
03  meter
 Z    =      -15397368
67                 Z    =        -4693117
97
 XDOT =       2422
535517                 XDOT =         738
388826
 YDOT =      22141
082854  feet/sec       YDOT =        6748
602054  meter/sec
 ZDOT =      -9280
890635                 ZDOT =       -2828
815465


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   18198
55236386  
00016717  00000-0  10270-3 0  9136
2 25544  51
6384 227
3666 0003911 323
2771  36
8113 15
54000463  3238


Satellite: ISS
Catalog Number: 25544
Epoch time:      18198
55236386   =   yrday
fracday
Element set:     913
Inclination:       51
6384  deg
RA of node:       227
3666  deg
Eccentricity:     
0003911     
Arg of perigee:   323
2771  deg
Mean anomaly:      36
8113  deg
Mean motion:   15
54000463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             323
Checksum:              298


Coasting Arc #15 (Orbit 338)
---------------------------------------

Vector Time (GMT): 2018/199/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944898
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3662999
85                 A    =         6788074
48  meter
 Y    =       -5349067
63  meter          E    =           
0013934
 Z    =        1983967
31                 I    =           51
39733
 XDOT =       5094
468718                 Wp   =           51
49366
 YDOT =      -1420
508545  meter/sec      RA   =          221
45540  deg
 ZDOT =       5558
050085                 TA   =          330
49650
                                          MA   =          330
57507
                                          Ha   =            220
996  n
mi
                                          Hp   =            215
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12017716
03                 X    =        -3612549
79
 Y    =      -17549434
49  feet           Y    =        -5389747
85  meter
 Z    =        6509079
09                 Z    =         1966296
22
 XDOT =      16714
136214                 XDOT =        5082
976905
 YDOT =      -4660
461105  feet/sec       YDOT =       -1363
603222  meter/sec
 ZDOT =      18235
072456                 ZDOT =        5582
768921

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8185988
40                 X    =        -2495089
26
 Y    =       19657400
70  feet           Y    =         5991575
73  meter
 Z    =        6430587
21                 Z    =         1960042
98
 XDOT =     -11489
660921                 XDOT =       -3502
048649
 YDOT =     -10805
750243  feet/sec       YDOT =       -3293
592674  meter/sec
 ZDOT =      18345
910009                 ZDOT =        5591
833371


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   18199
58128182  
00016717  00000-0  10270-3 0  9145
2 25544  51
6383 222
2378 0004032 329
5178  30
5740 15
54001129  3390


Satellite: ISS
Catalog Number: 25544
Epoch time:      18199
58128182   =   yrday
fracday
Element set:     914
Inclination:       51
6383  deg
RA of node:       222
2378  deg
Eccentricity:     
0004032     
Arg of perigee:   329
5178  deg
Mean anomaly:      30
5740  deg
Mean motion:   15
54001129  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             339
Checksum:              299


Coasting Arc #16 (Orbit 353)
---------------------------------------

Vector Time (GMT): 2018/200/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944898
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2543329
97                 A    =         6784795
84  meter
 Y    =        5279013
70  meter          E    =           
0004628
 Z    =       -3426304
39                 I    =           51
41057
 XDOT =      -6147
311941                 Wp   =           40
54739
 YDOT =         -5
884573  meter/sec      RA   =          216
46234  deg
 ZDOT =      -4572
227543                 TA   =          179
67671
                                          MA   =          179
67642
                                          Ha   =            221
077  n
mi
                                          Hp   =            215
498

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8344258
43                 X    =         2500752
57
 Y    =       17319598
74  feet           Y    =         5307217
10  meter
 Z    =      -11241156
14                 Z    =        -3414053
02
 XDOT =     -20168
346262                 XDOT =       -6124
580022
 YDOT =        -19
306343  feet/sec       YDOT =         -74
500701  meter/sec
 ZDOT =     -15000
746531                 ZDOT =       -4602
033532

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9685662
65                 X    =         2952189
97
 Y    =      -16643309
70  feet           Y    =        -5072880
80  meter
 Z    =      -11186908
52                 Z    =        -3409769
72
 XDOT =       9956
015655                 XDOT =        3034
593572
 YDOT =      15966
423132  feet/sec       YDOT =        4866
565771  meter/sec
 ZDOT =     -15134
206042                 ZDOT =       -4612
906001


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   18200
54589154  
00016717  00000-0  10270-3 0  9155
2 25544  51
6371 217
4304 0004016 332
2768  27
8170 15
53994012  3544


Satellite: ISS
Catalog Number: 25544
Epoch time:      18200
54589154   =   yrday
fracday
Element set:     915
Inclination:       51
6371  deg
RA of node:       217
4304  deg
Eccentricity:     
0004016     
Arg of perigee:   332
2768  deg
Mean anomaly:      27
8170  deg
Mean motion:   15
53994012  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             354
Checksum:              293


Coasting Arc #17 (Orbit 369)
---------------------------------------

Vector Time (GMT): 2018/201/12:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944898
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1157652
27                 A    =         6781123
43  meter
 Y    =       -4924870
64  meter          E    =           
0006613
 Z    =        4509505
57                 I    =           51
42468
 XDOT =       6880
431132                 Wp   =           86
75277
 YDOT =       1267
428984  meter/sec      RA   =          211
46070  deg
 ZDOT =       3146
845360                 TA   =          331
58083
                                          MA   =          331
61689
                                          Ha   =            221
194  n
mi
                                          Hp   =            215
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3798071
75                 X    =        -1124399
59
 Y    =      -16157712
08  feet           Y    =        -4937630
68  meter
 Z    =       14794965
77                 Z    =         4503962
57
 XDOT =      22573
592953                 XDOT =        6850
461436
 YDOT =       4158
231575  feet/sec       YDOT =        1344
202936  meter/sec
 ZDOT =      10324
295801                 ZDOT =        3180
195135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11029552
13                 X    =        -3361807
49
 Y    =       12432345
53  feet           Y    =         3789378
92  meter
 Z    =       14770706
99                 Z    =         4502111
49
 XDOT =      -8545
079378                 XDOT =       -2604
540195
 YDOT =     -20038
483326  feet/sec       YDOT =       -6107
729718  meter/sec
 ZDOT =      10473
494538                 ZDOT =        3192
321135


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   18201
57480843  
00016717  00000-0  10270-3 0  9165
2 25544  51
6363 212
3017 0004129 336
2208  23
8753 15
53990832  3705


Satellite: ISS
Catalog Number: 25544
Epoch time:      18201
57480843   =   yrday
fracday
Element set:     916
Inclination:       51
6363  deg
RA of node:       212
3017  deg
Eccentricity:     
0004129     
Arg of perigee:   336
2208  deg
Mean anomaly:      23
8753  deg
Mean motion:   15
53990832  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             370
Checksum:              294
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