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

 
Date: June 10th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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


165/09:20:13 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 7

167/11:41:08 000 0 0 0 0 0 0
N/A 0 0 0 0 219 7
000/00:00:00 000 0 0 0 0 216 6

167/16:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 216 4

Coasting Arc #1 (Orbit 2054)
---------------------------------------

Vector Time (GMT): 2017/160/11:33:58
253
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -781215
87                 A    =         6789216
72  meter
 Y    =       -6648818
49  meter          E    =           
0008596
 Z    =       -1096439
47                 I    =           52
02438
 XDOT =       4861
620917                 Wp   =          171
31357
 YDOT =        402
141180  meter/sec      RA   =           75
95343  deg
 ZDOT =      -5916
788963                 TA   =           20
51827
                                          MA   =           20
48376
                                          Ha   =            219
675  n
mi
                                          Hp   =            216
590

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2563044
21                 X    =         -701482
96
 Y    =      -21813708
95  feet           Y    =        -6657108
61  meter
 Z    =       -3597242
35                 Z    =        -1100041
68
 XDOT =      15950
199858                 XDOT =        4885
503875
 YDOT =       1319
360826  feet/sec       YDOT =         456
641486  meter/sec
 ZDOT =     -19412
037281                 ZDOT =       -5893
114418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21424035
00                 X    =        -6530045
87
 Y    =       -4828229
40  feet           Y    =        -1471644
32  meter
 Z    =       -3611948
47                 Z    =        -1100921
89
 XDOT =       6215
485948                 XDOT =        1894
480117
 YDOT =     -13170
766264  feet/sec       YDOT =       -4014
449557  meter/sec
 ZDOT =     -19307
553902                 ZDOT =       -5884
942429


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   17160
51196400  
00016717  00000-0  10270-3 0  9008
2 25544  51
6417  76
5897 0004697 256
9367 103
1262 15
53990213 20557


Satellite: ISS
Catalog Number: 25544
Epoch time:      17160
51196400   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:        76
5897  deg
Eccentricity:     
0004697     
Arg of perigee:   256
9367  deg
Mean anomaly:     103
1262  deg
Mean motion:   15
53990213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2055
Checksum:              309


Coasting Arc #2 (Orbit 2070)
---------------------------------------

Vector Time (GMT): 2017/161/11:33:58
253
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -47605
34                 A    =         6786720
60  meter
 Y    =        6239885
85  meter          E    =           
0008935
 Z    =        2657750
66                 I    =           52
00741
 XDOT =      -5113
513341                 Wp   =           75
52674
 YDOT =      -2276
863889  meter/sec      RA   =           71
00595  deg
 ZDOT =       5241
535420                 TA   =          314
28957
                                          MA   =          314
36283
                                          Ha   =            219
581  n
mi
                                          Hp   =            216
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -156185
50                 X    =         -130287
98
 Y    =       20472066
45  feet           Y    =         6238890
80  meter
 Z    =        8719654
41                 Z    =         2657319
50
 XDOT =     -16776
618573                 XDOT =       -5113
133781
 YDOT =      -7470
025882  feet/sec       YDOT =       -2334
045303  meter/sec
 ZDOT =      17196
638516                 ZDOT =        5216
695973

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19364156
81                 X    =         5902194
99
 Y    =        6649244
04  feet           Y    =         2026689
58  meter
 Z    =        8716608
09                 Z    =         2656822
15
 XDOT =     -11921
909584                 XDOT =       -3633
798041
 YDOT =      12265
474846  feet/sec       YDOT =        3738
516733  meter/sec
 ZDOT =      17087
350118                 ZDOT =        5208
224316


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   17161
54088048  
00016717  00000-0  10270-3 0  9011
2 25544  51
6418  71
4617 0004644 261
8240  98
2386 15
53997071 20717


Satellite: ISS
Catalog Number: 25544
Epoch time:      17161
54088048   =   yrday
fracday
Element set:     901
Inclination:       51
6418  deg
RA of node:        71
4617  deg
Eccentricity:     
0004644     
Arg of perigee:   261
8240  deg
Mean anomaly:      98
2386  deg
Mean motion:   15
53997071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2071
Checksum:              312


Coasting Arc #3 (Orbit 2085)
---------------------------------------

Vector Time (GMT): 2017/162/11:33:58
253
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         994400
54                 A    =         6782976
23  meter
 Y    =       -5409924
21  meter          E    =           
0002511
 Z    =       -3971871
06                 I    =           51
98448
 XDOT =       5198
501056                 Wp   =           47
83299
 YDOT =       3922
176353  meter/sec      RA   =           66
04980  deg
 ZDOT =      -4040
727362                 TA   =          180
16000
                                          MA   =          180
16008
                                          Ha   =            219
499  n
mi
                                          Hp   =            216
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3262468
96                 X    =         1074115
29
 Y    =      -17749095
17  feet           Y    =        -5398357
85  meter
 Z    =      -13031073
04                 Z    =        -3966847
73
 XDOT =      17055
449659                 XDOT =        5173
883828
 YDOT =      12868
032655  feet/sec       YDOT =        3980
172463  meter/sec
 ZDOT =     -13256
979535                 ZDOT =       -4015
533774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15941524
24                 X    =        -4858976
59
 Y    =       -8493859
48  feet           Y    =        -2588928
37  meter
 Z    =      -13007886
20                 Z    =        -3964803
71
 XDOT =      16778
045064                 XDOT =        5113
948136
 YDOT =     -11356
431294  feet/sec       YDOT =       -3461
440259  meter/sec
 ZDOT =     -13146
431742                 ZDOT =       -4007
032395


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   17162
50548604  
00016717  00000-0  10270-3 0  9028
2 25544  51
6426  66
6548 0004613 266
3535  93
7090 15
54022488 20868


Satellite: ISS
Catalog Number: 25544
Epoch time:      17162
50548604   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:        66
6548  deg
Eccentricity:     
0004613     
Arg of perigee:   266
3535  deg
Mean anomaly:      93
7090  deg
Mean motion:   15
54022488  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2086
Checksum:              310


Coasting Arc #4 (Orbit 2101)
---------------------------------------

Vector Time (GMT): 2017/163/11:33:58
253
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2011716
93                 A    =         6779605
41  meter
 Y    =        4254925
59  meter          E    =           
0003870
 Z    =        4879965
42                 I    =           51
95846
 XDOT =      -5066
221505                 Wp   =          159
96131
 YDOT =      -5208
462808  meter/sec      RA   =           61
08270  deg
 ZDOT =       2448
736222                 TA   =          266
09353
                                          MA   =          266
13777
                                          Ha   =            219
534  n
mi
                                          Hp   =            216
553

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6600121
15                 X    =        -2082851
60
 Y    =       13959729
63  feet           Y    =         4232030
78  meter
 Z    =       16010385
24                 Z    =         4870020
94
 XDOT =     -16621
461631                 XDOT =       -5019
497342
 YDOT =     -17088
132571  feet/sec       YDOT =       -5264
855825  meter/sec
 ZDOT =       8033
911488                 ZDOT =        2424
238812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11503112
16                 X    =         3506148
59
 Y    =       10370338
18  feet           Y    =         3160879
08  meter
 Z    =       15965668
88                 Z    =         4866335
87
 XDOT =     -20340
449369                 XDOT =       -6199
768968
 YDOT =      10337
913580  feet/sec       YDOT =        3150
996059  meter/sec
 ZDOT =       7926
681886                 ZDOT =        2416
052639


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   17163
53439734  
00016717  00000-0  10270-3 0  9036
2 25544  51
6420  61
5270 0004672 268
8950  91
1667 15
54018274 21020


Satellite: ISS
Catalog Number: 25544
Epoch time:      17163
53439734   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:        61
5270  deg
Eccentricity:     
0004672     
Arg of perigee:   268
8950  deg
Mean anomaly:      91
1667  deg
Mean motion:   15
54018274  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2102
Checksum:              300


Coasting Arc #5 (Orbit 2116)
---------------------------------------

Vector Time (GMT): 2017/164/11:33:58
253
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3072990
50                 A    =         6777727
07  meter
 Y    =       -2888453
94  meter          E    =           
0010003
 Z    =       -5314412
64                 I    =           51
93658
 XDOT =       4645
527093                 Wp   =           81
36595
 YDOT =       6061
566412  meter/sec      RA   =           56
10710  deg
 ZDOT =       -607
839375                 TA   =          182
84758
                                          MA   =          182
85328
                                          Ha   =            219
403  n
mi
                                          Hp   =            216
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10081989
83                 X    =         3130876
33
 Y    =       -9476554
93  feet           Y    =        -2853765
32  meter
 Z    =      -17435737
02                 Z    =        -5299344
81
 XDOT =      15241
230621                 XDOT =        4580
352383
 YDOT =      19887
028910  feet/sec       YDOT =        6113
151509  meter/sec
 ZDOT =      -1994
223670                 ZDOT =        -585
430375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6430692
19                 X    =        -1960074
98
 Y    =      -12346376
48  feet           Y    =        -3763175
55  meter
 Z    =      -17368641
96                 Z    =        -5293962
07
 XDOT =      22322
975617                 XDOT =        6804
042968
 YDOT =      -8957
019965  feet/sec       YDOT =       -2730
099685  meter/sec
 ZDOT =      -1896
383972                 ZDOT =        -578
017835


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   17164
49899828  
00016717  00000-0  10270-3 0  9047
2 25544  51
6429  56
7197 0004774 273
7597  86
3010 15
54038084 21173


Satellite: ISS
Catalog Number: 25544
Epoch time:      17164
49899828   =   yrday
fracday
Element set:     904
Inclination:       51
6429  deg
RA of node:        56
7197  deg
Eccentricity:     
0004774     
Arg of perigee:   273
7597  deg
Mean anomaly:      86
3010  deg
Mean motion:   15
54038084  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2117
Checksum:              344


Coasting Arc #6 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5025435
58                 A    =         6781131
09  meter
 Y    =         648935
49  meter          E    =           
0004969
 Z    =       -4511465
93                 I    =           51
92883
 XDOT =       2041
108385                 Wp   =          122
14269
 YDOT =       6642
939919  meter/sec      RA   =           51
57571  deg
 ZDOT =       3229
193720                 TA   =          180
22017
                                          MA   =          180
22039
                                          Ha   =            219
539  n
mi
                                          Hp   =            216
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16487649
54                 X    =         5039719
94
 Y    =        2129053
43  feet           Y    =          705213
72  meter
 Z    =      -14801397
42                 Z    =        -4487019
22
 XDOT =       6696
549818                 XDOT =        1950
987792
 YDOT =      21794
422307  feet/sec       YDOT =        6665
260694  meter/sec
 ZDOT =      10594
467585                 ZDOT =        3238
890674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13738508
68                 X    =         4187497
44
 Y    =       -9529429
39  feet           Y    =        -2904570
08  meter
 Z    =      -14693542
00                 Z    =        -4478591
60
 XDOT =      18825
794509                 XDOT =        5738
102166
 YDOT =      10741
278248  feet/sec       YDOT =        3273
941610  meter/sec
 ZDOT =      10636
043891                 ZDOT =        3241
866178


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   17165
39929034  
00016717  00000-0  10270-3 0  9051
2 25544  51
6411  52
2314 0004699 277
8756  82
1863 15
54025563 21318


Satellite: ISS
Catalog Number: 25544
Epoch time:      17165
39929034   =   yrday
fracday
Element set:     905
Inclination:       51
6411  deg
RA of node:        52
2314  deg
Eccentricity:     
0004699     
Arg of perigee:   277
8756  deg
Mean anomaly:      82
1863  deg
Mean motion:   15
54025563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2131
Checksum:              313


Coasting Arc #7 (Orbit 2146)
---------------------------------------

Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5529419
18                 A    =         6784871
28  meter
 Y    =       -1984671
04  meter          E    =           
0007934
 Z    =        3388287
19                 I    =           51
92026
 XDOT =       -691
720527                 Wp   =           84
32956
 YDOT =      -6048
902472  meter/sec      RA   =           46
61016  deg
 ZDOT =      -4661
822057                 TA   =           56
27244
                                          MA   =           56
19685
                                          Ha   =            219
633  n
mi
                                          Hp   =            216
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18141139
04                 X    =        -5523273
70
 Y    =       -6511387
93  feet           Y    =        -2046470
75  meter
 Z    =       11116427
78                 Z    =         3361441
76
 XDOT =      -2269
424300                 XDOT =        -601
383917
 YDOT =     -19845
480550  feet/sec       YDOT =       -6056
132164  meter/sec
 ZDOT =     -15294
691788                 ZDOT =       -4664
963439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17754754
17                 X    =        -5411649
07
 Y    =        7673436
34  feet           Y    =         2338863
40  meter
 Z    =       10998233
68                 Z    =         3352261
63
 XDOT =     -14572
378764                 XDOT =       -4441
661047
 YDOT =     -11729
451855  feet/sec       YDOT =       -3575
136925  meter/sec
 ZDOT =     -15307
419157                 ZDOT =       -4665
701359


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   17166
42819322  
00016717  00000-0  10270-3 0  9065
2 25544  51
6410  47
1040 0004735 281
8957  78
1665 15
54023235 21471


Satellite: ISS
Catalog Number: 25544
Epoch time:      17166
42819322   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:        47
1040  deg
Eccentricity:     
0004735     
Arg of perigee:   281
8957  deg
Mean anomaly:      78
1665  deg
Mean motion:   15
54023235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2147
Checksum:              300


Coasting Arc #8 (Orbit 2161)
---------------------------------------

Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5733085
48                 A    =         6788081
25  meter
 Y    =        3063639
32  meter          E    =           
0006724
 Z    =       -1940456
72                 I    =           51
90847
 XDOT =       -847
925153                 Wp   =          357
84566
 YDOT =       5144
237118  meter/sec      RA   =           41
65155  deg
 ZDOT =       5622
558037                 TA   =          340
84217
                                          MA   =          340
86745
                                          Ha   =            219
693  n
mi
                                          Hp   =            216
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18809335
55                 X    =         5707826
74
 Y    =       10051310
10  feet           Y    =         3127609
52  meter
 Z    =       -6366327
83                 Z    =        -1912668
26
 XDOT =      -2781
906670                 XDOT =        -932
697944
 YDOT =      16877
418365  feet/sec       YDOT =        5134
280523  meter/sec
 ZDOT =      18446
712721                 ZDOT =        5618
233666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20538842
69                 X    =         6260239
25
 Y    =       -5875051
15  feet           Y    =        -1790715
59  meter
 Z    =       -6244179
99                 Z    =        -1903226
06
 XDOT =       9216
046569                 XDOT =        2809
050994
 YDOT =      12655
411120  feet/sec       YDOT =        3857
369309  meter/sec
 ZDOT =      18426
633121                 ZDOT =        5616
437775


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   17167
39278726  
00016717  00000-0  10270-3 0  9070
2 25544  51
6415  42
2960 0004832 285
2268  74
8350 15
54028641 21621


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
39278726   =   yrday
fracday
Element set:     907
Inclination:       51
6415  deg
RA of node:        42
2960  deg
Eccentricity:     
0004832     
Arg of perigee:   285
2268  deg
Mean anomaly:      74
8350  deg
Mean motion:   15
54028641  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2162
Checksum:              315


Coasting Arc #9 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2017/167/11:41:08
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5605550
96                 A    =         6789088
02  meter
 Y    =       -3615700
68  meter          E    =           
0009273
 Z    =        1235848
86                 I    =           51
91058
 XDOT =       1690
119475                 Wp   =          130
32833
 YDOT =      -4634
689524  meter/sec      RA   =           41
17266  deg
 ZDOT =      -5870
517047                 TA   =           36
28859
                                          MA   =           36
22574
                                          Ha   =            219
659  n
mi
                                          Hp   =            216
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18390915
22                 X    =        -5570705
77
 Y    =      -11862535
05  feet           Y    =        -3678191
04  meter
 Z    =        4054622
25                 Z    =         1208703
15
 XDOT =       5545
011401                 XDOT =        1770
336245
 YDOT =     -15205
674292  feet/sec       YDOT =       -4615
340398  meter/sec
 ZDOT =     -19260
226532                 ZDOT =       -5862
112572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15060294
05                 X    =        -4590377
63
 Y    =       15908660
55  feet           Y    =         4848959
74  meter
 Z    =        3935419
22                 Z    =         1199515
78
 XDOT =     -12737
977811                 XDOT =       -3882
535637
 YDOT =      -7284
278714  feet/sec       YDOT =       -2220
248152  meter/sec
 ZDOT =     -19222
223422                 ZDOT =       -5858
933699


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   17167
52139968  
00016717  00000-0  10270-3 0  9080
2 25544  51
6428  41
6563 0004768 284
6201  75
4422 15
54001844 21640


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
52139968   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:        41
6563  deg
Eccentricity:     
0004768     
Arg of perigee:   284
6201  deg
Mean anomaly:      75
4422  deg
Mean motion:   15
54001844  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2164
Checksum:              314


Coasting Arc #10 (Orbit 2166)
---------------------------------------

Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3171033
41                 A    =         6786551
49  meter
 Y    =       -5388062
25  meter          E    =           
0001805
 Z    =       -2637146
00                 I    =           51
89446
 XDOT =       5546
342344                 Wp   =          194
84111
 YDOT =       -697
706245  meter/sec      RA   =           40
20402  deg
 ZDOT =      -5244
587412                 TA   =           14
75732
                                          MA   =           14
75206
                                          Ha   =            219
588  n
mi
                                          Hp   =            216
441

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10403652
91                 X    =        -3097737
05
 Y    =      -17677369
60  feet           Y    =        -5423112
83  meter
 Z    =       -8652053
81                 Z    =        -2652372
36
 XDOT =      18196
661235                 XDOT =        5579
207688
 YDOT =      -2289
062484  feet/sec       YDOT =        -635
499047  meter/sec
 ZDOT =     -17206
651613                 ZDOT =       -5217
565243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         753735
14                 X    =          229738
47
 Y    =       20469660
59  feet           Y    =         6239152
55  meter
 Z    =       -8718274
13                 Z    =        -2657329
95
 XDOT =     -15721
647276                 XDOT =       -4791
958090
 YDOT =      -6697
471384  feet/sec       YDOT =       -2041
389278  meter/sec
 ZDOT =     -17087
172706                 ZDOT =       -5208
170241


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   17167
71431690  
00016717  00000-0  10270-3 0  9099
2 25544  51
6394  40
6892 0004655 284
3892  75
6743 15
54053825 21671


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
71431690   =   yrday
fracday
Element set:     909
Inclination:       51
6394  deg
RA of node:        40
6892  deg
Eccentricity:     
0004655     
Arg of perigee:   284
3892  deg
Mean anomaly:      75
6743  deg
Mean motion:   15
54053825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2167
Checksum:              334


Coasting Arc #11 (Orbit 2182)
---------------------------------------

Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1935107
99                 A    =         6782897
13  meter
 Y    =        5161989
18  meter          E    =           
0006383
 Z    =        3946873
80                 I    =           51
85654
 XDOT =      -6475
108255                 Wp   =           96
02172
 YDOT =       -676
721099  meter/sec      RA   =           35
23838  deg
 ZDOT =       4053
461090                 TA   =          311
72575
                                          MA   =          311
78032
                                          Ha   =            219
613  n
mi
                                          Hp   =            216
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6348779
50                 X    =         1858069
43
 Y    =       16935660
04  feet           Y    =         5183197
78  meter
 Z    =       12949061
04                 Z    =         3956087
31
 XDOT =     -21243
793486                 XDOT =       -6486
749515
 YDOT =      -2220
213578  feet/sec       YDOT =        -749
195587  meter/sec
 ZDOT =      13298
756857                 ZDOT =        4021
978601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2184764
03                 X    =          665916
08
 Y    =      -17925419
07  feet           Y    =        -5463667
73  meter
 Z    =       12988761
34                 Z    =         3958974
46
 XDOT =      16640
645587                 XDOT =        5072
068775
 YDOT =      11578
671775  feet/sec       YDOT =        3529
179157  meter/sec
 ZDOT =      13159
848481                 ZDOT =        4011
121817


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   17168
74321286  
00016717  00000-0  10270-3 0  9104
2 25544  51
6392  35
5601 0004658 285
8445  74
2194 15
54054133 21839


Satellite: ISS
Catalog Number: 25544
Epoch time:      17168
74321286   =   yrday
fracday
Element set:     910
Inclination:       51
6392  deg
RA of node:        35
5601  deg
Eccentricity:     
0004658     
Arg of perigee:   285
8445  deg
Mean anomaly:      74
2194  deg
Mean motion:   15
54054133  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2183
Checksum:              307


Coasting Arc #12 (Orbit 2197)
---------------------------------------

Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -453388
82                 A    =         6779499
31  meter
 Y    =       -4700635
61  meter          E    =           
0008753
 Z    =       -4872241
34                 I    =           51
81851
 XDOT =       7015
870051                 Wp   =           53
73695
 YDOT =       1863
863970  meter/sec      RA   =           30
26333  deg
 ZDOT =      -2449
097610                 TA   =          192
25590
                                          MA   =          192
27721
                                          Ha   =            219
790  n
mi
                                          Hp   =            216
363

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1487496
13                 X    =         -377124
28
 Y    =      -15422032
84  feet           Y    =        -4705278
86  meter
 Z    =      -15985043
78                 Z    =        -4874258
96
 XDOT =      23017
946363                 XDOT =        7006
402984
 YDOT =       6115
039272  feet/sec       YDOT =        1942
267467  meter/sec
 ZDOT =      -8035
097147                 ZDOT =       -2415
039314

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5583792
52                 X    =        -1701939
96
 Y    =       14443582
11  feet           Y    =         4402403
83  meter
 Z    =      -15993047
34                 Z    =        -4874680
83
 XDOT =     -16930
507990                 XDOT =       -5160
418835
 YDOT =     -15283
362789  feet/sec       YDOT =       -4658
368978  meter/sec
 ZDOT =      -7885
051292                 ZDOT =       -2403
363634


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   17169
70780256  
00016717  00000-0  10270-3 0  9118
2 25544  51
6397  30
7539 0004529 290
7125  69
3542 15
54049399 21984


Satellite: ISS
Catalog Number: 25544
Epoch time:      17169
70780256   =   yrday
fracday
Element set:     911
Inclination:       51
6397  deg
RA of node:        30
7539  deg
Eccentricity:     
0004529     
Arg of perigee:   290
7125  deg
Mean anomaly:      69
3542  deg
Mean motion:   15
54049399  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2198
Checksum:              336


Coasting Arc #13 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1166630
47                 A    =         6777750
06  meter
 Y    =        4063276
03  meter          E    =           
0001807
 Z    =        5299126
67                 I    =           51
78409
 XDOT =      -7101
820287                 Wp   =          296
17436
 YDOT =      -2826
723710  meter/sec      RA   =           25
27647  deg
 ZDOT =        604
915896                 TA   =          148
06820
                                          MA   =          148
05725
                                          Ha   =            219
989  n
mi
                                          Hp   =            216
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3827527
78                 X    =        -1237721
16
 Y    =       13330958
12  feet           Y    =         4049831
97  meter
 Z    =       17385586
20                 Z    =         5293287
23
 XDOT =     -23299
935325                 XDOT =       -7072
621707
 YDOT =      -9274
027920  feet/sec       YDOT =       -2905
977878  meter/sec
 ZDOT =       1984
632205                 ZDOT =         570
487792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9256181
73                 X    =         2821284
19
 Y    =      -10373564
48  feet           Y    =        -3161862
45  meter
 Z    =       17359011
50                 Z    =         5291026
71
 XDOT =      16364
793531                 XDOT =        4987
989068
 YDOT =      17664
489979  feet/sec       YDOT =        5384
136546  meter/sec
 ZDOT =       1833
150988                 ZDOT =         558
744421


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   17170
73669619  
00016717  00000-0  10270-3 0  9123
2 25544  51
6401  25
6245 0004642 294
5980  65
4689 15
54025970 22141


Satellite: ISS
Catalog Number: 25544
Epoch time:      17170
73669619   =   yrday
fracday
Element set:     912
Inclination:       51
6401  deg
RA of node:        25
6245  deg
Eccentricity:     
0004642     
Arg of perigee:   294
5980  deg
Mean anomaly:      65
4689  deg
Mean motion:   15
54025970  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              318


Coasting Arc #14 (Orbit 2228)
---------------------------------------

Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2793617
94                 A    =         6778157
73  meter
 Y    =       -3339493
71  meter          E    =           
0009695
 Z    =       -5203303
06                 I    =           51
75670
 XDOT =       6662
042860                 Wp   =           91
35405
 YDOT =       3553
463332  meter/sec      RA   =           20
28775  deg
 ZDOT =       1298
048478                 TA   =          191
09347
                                          MA   =          191
11487
                                          Ha   =            220
024  n
mi
                                          Hp   =            216
368

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9165413
18                 X    =         2856028
75
 Y    =      -10956344
18  feet           Y    =        -3307904
01  meter
 Z    =      -17071204
26                 Z    =        -5189581
19
 XDOT =      21857
095998                 XDOT =        6615
506616
 YDOT =      11658
344265  feet/sec       YDOT =        3627
702458  meter/sec
 ZDOT =       4258
689231                 ZDOT =        1330
298335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12963012
87                 X    =        -3951126
32
 Y    =        6172019
07  feet           Y    =         1881231
41  meter
 Z    =      -17009960
88                 Z    =        -5184636
08
 XDOT =     -14650
831352                 XDOT =       -4465
573396
 YDOT =     -18660
469179  feet/sec       YDOT =       -5687
711006  meter/sec
 ZDOT =       4400
398952                 ZDOT =        1341
241600


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   17171
70128002  
00016717  00000-0  10270-3 0  9138
2 25544  51
6410  20
8179 0004579 298
3529  61
7161 15
54056388 22291


Satellite: ISS
Catalog Number: 25544
Epoch time:      17171
70128002   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:        20
8179  deg
Eccentricity:     
0004579     
Arg of perigee:   298
3529  deg
Mean anomaly:      61
7161  deg
Mean motion:   15
54056388  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2229
Checksum:              303


Coasting Arc #15 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4301055
49                 A    =         6780896
79  meter
 Y    =        2562723
21  meter          E    =           
0007165
 Z    =        4572572
35                 I    =           51
73392
 XDOT =      -5714
090487                 Wp   =           35
56540
 YDOT =      -4081
318151  meter/sec      RA   =           15
29968  deg
 ZDOT =      -3079
276304                 TA   =           85
23952
                                          MA   =           85
15771
                                          Ha   =            220
269  n
mi
                                          Hp   =            216
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14111074
45                 X    =        -4351604
40
 Y    =        8407884
55  feet           Y    =         2514342
62  meter
 Z    =       15001877
79                 Z    =         4551556
53
 XDOT =     -18747
016032                 XDOT =       -5653
069676
 YDOT =     -13390
151415  feet/sec       YDOT =       -4144
875368  meter/sec
 ZDOT =     -10102
612546                 ZDOT =       -3106
886210

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16376389
21                 X    =         4991523
43
 Y    =       -2102246
83  feet           Y    =         -640764
83  meter
 Z    =       14908578
64                 Z    =         4544134
77
 XDOT =      11705
918373                 XDOT =        3567
963920
 YDOT =      18494
493031  feet/sec       YDOT =        5637
121476  meter/sec
 ZDOT =     -10223
721305                 ZDOT =       -3116
190254


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   17172
73016925  
00016717  00000-0  10270-3 0  9143
2 25544  51
6403  15
6891 0004519 302
0099  58
0614 15
54017133 22450


Satellite: ISS
Catalog Number: 25544
Epoch time:      17172
73016925   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:        15
6891  deg
Eccentricity:     
0004519     
Arg of perigee:   302
0099  deg
Mean anomaly:      58
0614  deg
Mean motion:   15
54017133  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              287


Coasting Arc #16 (Orbit 2259)
---------------------------------------

Vector Time (GMT): 2017/173/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5528728
62                 A    =         6784525
04  meter
 Y    =       -1797893
62  meter          E    =           
0002814
 Z    =       -3495605
70                 I    =           51
71502
 XDOT =       4307
714034                 Wp   =           23
22082
 YDOT =       4426
854776  meter/sec      RA   =           10
31910  deg
 ZDOT =       4540
085230                 TA   =          295
74735
                                          MA   =          295
77639
                                          Ha   =            220
360  n
mi
                                          Hp   =            216
312

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18138873
41                 X    =         5565402
27
 Y    =       -5898601
11  feet           Y    =        -1735862
02  meter
 Z    =      -11468522
64                 Z    =        -3468659
88
 XDOT =      14132
920059                 XDOT =        4235
837978
 YDOT =      14523
801760  feet/sec       YDOT =        4474
623949  meter/sec
 ZDOT =      14895
292749                 ZDOT =        4560
837033

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19089455
09                 X    =        -5818465
91
 Y    =       -1458703
58  feet           Y    =         -444612
85  meter
 Z    =      -11349190
43                 Z    =        -3459233
24
 XDOT =      -7574
488491                 XDOT =       -2308
704092
 YDOT =     -17374
851302  feet/sec       YDOT =       -5295
854677  meter/sec
 ZDOT =      14986
045393                 ZDOT =        4567
746636


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   17173
69474936  
00016717  00000-0  10270-3 0  9150
2 25544  51
6408  10
8817 0004729 305
6984  54
3728 15
54035190 22600


Satellite: ISS
Catalog Number: 25544
Epoch time:      17173
69474936   =   yrday
fracday
Element set:     915
Inclination:       51
6408  deg
RA of node:        10
8817  deg
Eccentricity:     
0004729     
Arg of perigee:   305
6984  deg
Mean anomaly:      54
3728  deg
Mean motion:   15
54035190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2260
Checksum:              324


Coasting Arc #17 (Orbit 2275)
---------------------------------------

Vector Time (GMT): 2017/174/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6386009
14                 A    =         6787866
85  meter
 Y    =        1026326
79  meter          E    =           
0009594
 Z    =        2046816
57                 I    =           51
69460
 XDOT =      -2532
027228                 Wp   =          102
75999
 YDOT =      -4641
940264  meter/sec      RA   =            5
34549  deg
 ZDOT =      -5552
394106                 TA   =           54
62856
                                          MA   =           54
53895
                                          Ha   =            220
386  n
mi
                                          Hp   =            216
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20951473
57                 X    =        -6406953
62
 Y    =        3367213
86  feet           Y    =          954796
65  meter
 Z    =        6715277
46                 Z    =         2015744
58
 XDOT =      -8307
175946                 XDOT =       -2452
960817
 YDOT =     -15229
462808  feet/sec       YDOT =       -4669
812074  meter/sec
 ZDOT =     -18216
516095                 ZDOT =       -5564
502676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20781629
01                 X    =         6334240
52
 Y    =        4500302
67  feet           Y    =         1371692
25  meter
 Z    =        6577879
37                 Z    =         2004937
63
 XDOT =       2414
464441                 XDOT =         735
928762
 YDOT =      15650
708725  feet/sec       YDOT =        4770
336019  meter/sec
 ZDOT =     -18269
059801                 ZDOT =       -5568
409427


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   17174
72363343  
00016717  00000-0  10270-3 0  9165
2 25544  51
6413   5
7528 0004664 309
2816  50
7922 15
54045726 22769


Satellite: ISS
Catalog Number: 25544
Epoch time:      17174
72363343   =   yrday
fracday
Element set:     916
Inclination:       51
6413  deg
RA of node:         5
7528  deg
Eccentricity:     
0004664     
Arg of perigee:   309
2816  deg
Mean anomaly:      50
7922  deg
Mean motion:   15
54045726  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2276
Checksum:              308
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