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

 
Date: April 12th 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) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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


108/10:36:05 758 0 2 0 9 0 9
N/A -0 8 -0 1 220 9
000/00:02:11 515 -0 3 -0 0 214 8

Coasting Arc #1 (Orbit 2813)
---------------------------------------

Vector Time (GMT): 2018/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3092962
20                 A    =         6778511
92  meter
 Y    =       -3467089
65  meter          E    =           
0012284
 Z    =       -4947078
75                 I    =           51
56937
 XDOT =       6747
110162                 Wp   =           63
32671
 YDOT =      -2882
727536  meter/sec      RA   =          350
60878  deg
 ZDOT =      -2196
872494                 TA   =          185
18786
                                          MA   =          185
20060
                                          Ha   =            220
600  n
mi
                                          Hp   =            214
695

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10147513
79                 X    =        -3029932
08
 Y    =      -11374966
05  feet           Y    =        -3501325
27  meter
 Z    =      -16230573
33                 Z    =        -4961949
92
 XDOT =      22136
188197                 XDOT =        6789
515401
 YDOT =      -9457
767506  feet/sec       YDOT =       -2807
039783  meter/sec
 ZDOT =      -7207
586923                 ZDOT =       -2163
994136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13168217
52                 X    =        -4013672
70
 Y    =       -7537885
14  feet           Y    =        -2297547
39  meter
 Z    =      -16296371
82                 Z    =        -4967134
13
 XDOT =      17407
137864                 XDOT =        5305
695621
 YDOT =     -15136
728834  feet/sec       YDOT =       -4613
674949  meter/sec
 ZDOT =      -7060
456969                 ZDOT =       -2152
027284


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   18101
51984524  
00016717  00000-0  10270-3 0  9006
2 25544  51
6426 351
0710 0002247 334
4062  25
6980 15
54258655 28141


Satellite: ISS
Catalog Number: 25544
Epoch time:      18101
51984524   =   yrday
fracday
Element set:     900
Inclination:       51
6426  deg
RA of node:       351
0710  deg
Eccentricity:     
0002247     
Arg of perigee:   334
4062  deg
Mean anomaly:      25
6980  deg
Mean motion:   15
54258655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2814
Checksum:              291


Coasting Arc #2 (Orbit 2829)
---------------------------------------

Vector Time (GMT): 2018/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1330573
00                 A    =         6776956
40  meter
 Y    =        4006166
49  meter          E    =           
0002152
 Z    =        5300310
29                 I    =           51
53224
 XDOT =      -7371
111949                 Wp   =           42
83480
 YDOT =       2105
705392  meter/sec      RA   =          345
60308  deg
 ZDOT =        260
335887                 TA   =           44
68939
                                          MA   =           44
67205
                                          Ha   =            220
556  n
mi
                                          Hp   =            214
776

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4365396
97                 X    =         1259929
89
 Y    =       13143590
85  feet           Y    =         4020651
38  meter
 Z    =       17389469
47                 Z    =         5306601
82
 XDOT =     -24183
438154                 XDOT =       -7395
375263
 YDOT =       6908
482257  feet/sec       YDOT =        2023
140903  meter/sec
 ZDOT =        854
120363                 ZDOT =         224
470381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8445638
55                 X    =         2574230
63
 Y    =       10932831
10  feet           Y    =         3332326
92  meter
 Z    =       17416908
83                 Z    =         5308673
81
 XDOT =     -19629
446033                 XDOT =       -5983
055151
 YDOT =      14066
255653  feet/sec       YDOT =        4287
394723  meter/sec
 ZDOT =        693
800812                 ZDOT =         211
470487


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   18102
54860269  
00016717  00000-0  10270-3 0  9010
2 25544  51
6429 345
9421 0002209 334
4899  25
6144 15
54266985 28306


Satellite: ISS
Catalog Number: 25544
Epoch time:      18102
54860269   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:       345
9421  deg
Eccentricity:     
0002209     
Arg of perigee:   334
4899  deg
Mean anomaly:      25
6144  deg
Mean motion:   15
54266985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2830
Checksum:              320


Coasting Arc #3 (Orbit 2844)
---------------------------------------

Vector Time (GMT): 2018/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         470988
25                 A    =         6777953
02  meter
 Y    =       -4460164
41  meter          E    =           
0012116
 Z    =       -5092569
15                 I    =           51
50370
 XDOT =       7376
823469                 Wp   =           93
45859
 YDOT =      -1162
500834  meter/sec      RA   =          340
59381  deg
 ZDOT =       1703
179334                 TA   =          193
03140
                                          MA   =          193
06273
                                          Ha   =            220
648  n
mi
                                          Hp   =            214
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1545237
04                 X    =          545565
17
 Y    =      -14633085
33  feet           Y    =        -4454481
01  meter
 Z    =      -16707904
04                 Z    =        -5090099
66
 XDOT =      24202
176737                 XDOT =        7381
001418
 YDOT =      -3813
979114  feet/sec       YDOT =       -1079
984585  meter/sec
 ZDOT =       5587
858708                 ZDOT =        1739
023832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3637423
09                 X    =        -1108686
56
 Y    =      -14271482
15  feet           Y    =        -4349947
76  meter
 Z    =      -16696195
73                 Z    =        -5089000
46
 XDOT =      20204
830255                 XDOT =        6158
432262
 YDOT =     -11863
443834  feet/sec       YDOT =       -3615
977681  meter/sec
 ZDOT =       5747
922323                 ZDOT =        1751
966724


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   18103
51305830  
00016717  00000-0  10270-3 0  9027
2 25544  51
6428 341
1334 0002355 338
9093  21
1962 15
54271339 28457


Satellite: ISS
Catalog Number: 25544
Epoch time:      18103
51305830   =   yrday
fracday
Element set:     902
Inclination:       51
6428  deg
RA of node:       341
1334  deg
Eccentricity:     
0002355     
Arg of perigee:   338
9093  deg
Mean anomaly:      21
1962  deg
Mean motion:   15
54271339  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2845
Checksum:              288


Coasting Arc #4 (Orbit 2860)
---------------------------------------

Vector Time (GMT): 2018/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2182624
08                 A    =         6780989
30  meter
 Y    =        4756268
19  meter          E    =           
0010142
 Z    =        4308181
47                 I    =           51
48262
 XDOT =      -6827
035358                 Wp   =           57
96910
 YDOT =         43
376074  meter/sec      RA   =          335
58858  deg
 ZDOT =      -3495
301636                 TA   =           67
70736
                                          MA   =           67
59986
                                          Ha   =            220
709  n
mi
                                          Hp   =            214
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7160840
15                 X    =        -2256574
82
 Y    =       15604554
41  feet           Y    =         4731447
52  meter
 Z    =       14134453
63                 Z    =         4297398
86
 XDOT =     -22398
409966                 XDOT =       -6810
034509
 YDOT =        142
309953  feet/sec       YDOT =         -32
873822  meter/sec
 ZDOT =     -11467
525052                 ZDOT =       -3528
424022

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -958221
24                 X    =         -292065
83
 Y    =       17182533
45  feet           Y    =         5237236
20  meter
 Z    =       14085626
92                 Z    =         4293299
09
 XDOT =     -19429
313034                 XDOT =       -5922
054613
 YDOT =       8468
806476  feet/sec       YDOT =        2581
292214  meter/sec
 ZDOT =     -11615
259729                 ZDOT =       -3540
331166


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   18104
54180493  
00016717  00000-0  10270-3 0  9038
2 25544  51
6419 336
0043 0002500 342
8005  17
3062 15
54306699 28610


Satellite: ISS
Catalog Number: 25544
Epoch time:      18104
54180493   =   yrday
fracday
Element set:     903
Inclination:       51
6419  deg
RA of node:       336
0043  deg
Eccentricity:     
0002500     
Arg of perigee:   342
8005  deg
Mean anomaly:      17
3062  deg
Mean motion:   15
54306699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2861
Checksum:              282


Coasting Arc #5 (Orbit 2875)
---------------------------------------

Vector Time (GMT): 2018/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3614626
77                 A    =         6784982
43  meter
 Y    =       -4848472
09  meter          E    =           
0005202
 Z    =       -3074696
00                 I    =           51
46513
 XDOT =       5778
073389                 Wp   =           43
76433
 YDOT =       1212
760789  meter/sec      RA   =          330
59128  deg
 ZDOT =       4888
975146                 TA   =          280
82886
                                          MA   =          280
88741
                                          Ha   =            220
774  n
mi
                                          Hp   =            214
698

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11859011
71                 X    =         3683510
51
 Y    =      -15907060
67  feet           Y    =        -4807665
97  meter
 Z    =      -10087585
30                 Z    =        -3056969
42
 XDOT =      18956
933692                 XDOT =        5740
334141
 YDOT =       3978
873981  feet/sec       YDOT =        1277
164607  meter/sec
 ZDOT =      16039
944705                 ZDOT =        4916
951629

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4854497
07                 X    =         1479650
71
 Y    =      -19279736
53  feet           Y    =        -5876463
69  meter
 Z    =      -10007783
61                 Z    =        -3050372
45
 XDOT =      17518
872985                 XDOT =        5339
752486
 YDOT =      -3964
771081  feet/sec       YDOT =       -1208
462225  meter/sec
 ZDOT =      16164
524254                 ZDOT =        4926
946993


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   18105
50625314  
00016717  00000-0  10270-3 0  9042
2 25544  51
6410 331
1956 0002430 344
0386  16
0689 15
54265417 28767


Satellite: ISS
Catalog Number: 25544
Epoch time:      18105
50625314   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       331
1956  deg
Eccentricity:     
0002430     
Arg of perigee:   344
0386  deg
Mean anomaly:      16
0689  deg
Mean motion:   15
54265417  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2876
Checksum:              293


Coasting Arc #6 (Orbit 2891)
---------------------------------------

Vector Time (GMT): 2018/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4714288
28                 A    =         6788024
16  meter
 Y    =        4649539
09  meter          E    =           
0012440
 Z    =        1472160
46                 I    =           51
44773
 XDOT =      -4355
358338                 Wp   =          109
78461
 YDOT =      -2581
023805  meter/sec      RA   =          325
60197  deg
 ZDOT =      -5759
876224                 TA   =           54
10292
                                          MA   =           53
98750
                                          Ha   =            220
823  n
mi
                                          Hp   =            214
587

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15466825
05                 X    =        -4773081
42
 Y    =       15254393
32  feet           Y    =         4596492
04  meter
 Z    =        4829922
78                 Z    =         1449116
55
 XDOT =     -14289
233392                 XDOT =       -4298
194003
 YDOT =      -8467
925871  feet/sec       YDOT =       -2629
409220  meter/sec
 ZDOT =     -18897
231707                 ZDOT =       -5780
894371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8056160
86                 X    =        -2455517
83
 Y    =       20199166
02  feet           Y    =         6156705
80  meter
 Z    =        4726448
08                 Z    =         1440621
37
 XDOT =     -14901
185538                 XDOT =       -4541
881352
 YDOT =      -1471
575952  feet/sec       YDOT =        -448
536350  meter/sec
 ZDOT =     -18990
562914                 ZDOT =       -5788
323576


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   18106
53499223  
00016717  00000-0  10270-3 0  9055
2 25544  51
6415 326
0658 0002456 349
4935  10
6166 15
54275282 28920


Satellite: ISS
Catalog Number: 25544
Epoch time:      18106
53499223   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       326
0658  deg
Eccentricity:     
0002456     
Arg of perigee:   349
4935  deg
Mean anomaly:      10
6166  deg
Mean motion:   15
54275282  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2892
Checksum:              319


Coasting Arc #7 (Orbit 2907)
---------------------------------------

Vector Time (GMT): 2018/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928509
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5367273
10                 A    =         6788831
63  meter
 Y    =       -4136126
91  meter          E    =           
0014173
 Z    =         261789
77                 I    =           51
42239
 XDOT =       2733
624020                 Wp   =           39
68801
 YDOT =       3937
082243  meter/sec      RA   =          320
61549  deg
 ZDOT =       5989
512159                 TA   =          323
14256
                                          MA   =          323
23990
                                          Ha   =            220
834  n
mi
                                          Hp   =            214
470

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17609163
72                 X    =         5411853
83
 Y    =      -13569970
18  feet           Y    =        -4075857
09  meter
 Z    =         858890
32                 Z    =          287971
12
 XDOT =       8968
582742                 XDOT =        2660
300871
 YDOT =      12916
936492  feet/sec       YDOT =        3967
241852  meter/sec
 ZDOT =      19650
630444                 ZDOT =        6002
613109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10323661
67                 X    =         3146652
08
 Y    =      -19683326
43  feet           Y    =        -5999477
89  meter
 Z    =         976268
72                 Z    =          297566
71
 XDOT =      11992
162898                 XDOT =        3655
211251
 YDOT =       7291
411723  feet/sec       YDOT =        2222
422293  meter/sec
 ZDOT =      19708
446353                 ZDOT =        6007
134449


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   18107
56372568  
00016717  00000-0  10270-3 0  9062
2 25544  51
6398 320
9352 0002466 352
6101   7
5015 15
54288165 29086


Satellite: ISS
Catalog Number: 25544
Epoch time:      18107
56372568   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:       320
9352  deg
Eccentricity:     
0002466     
Arg of perigee:   352
6101  deg
Mean anomaly:       7
5015  deg
Mean motion:   15
54288165  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2908
Checksum:              312


Coasting Arc #8 (Orbit 2921)
---------------------------------------

Vector Time (GMT): 2018/108/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4985398
99                 A    =         6780254
26  meter
 Y    =        -286255
75  meter          E    =           
0010546
 Z    =       -4597021
32                 I    =           51
36928
 XDOT =       3113
092443                 Wp   =           57
39504
 YDOT =      -6331
296472  meter/sec      RA   =          315
92000  deg
 ZDOT =      -2981
286285                 TA   =          182
71679
                                          MA   =          182
72252
                                          Ha   =            220
878  n
mi
                                          Hp   =            214
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16356295
90                 X    =        -4959497
14
 Y    =        -939159
27  feet           Y    =         -341861
23  meter
 Z    =      -15082090
94                 Z    =        -4621176
20
 XDOT =      10213
557885                 XDOT =        3198
141149
 YDOT =     -20771
970052  feet/sec       YDOT =       -6296
008286  meter/sec
 ZDOT =      -9781
122982                 ZDOT =       -2965
956902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16277023
76                 X    =        -4961236
84
 Y    =         458049
46  feet           Y    =          139613
48  meter
 Z    =      -15189752
83                 Z    =        -4629836
66
 XDOT =       8490
972815                 XDOT =        2588
048514
 YDOT =     -20391
110203  feet/sec       YDOT =       -6215
210390  meter/sec
 ZDOT =      -9711
804037                 ZDOT =       -2960
157870


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   18108
46386708  
00016717  00000-0  10270-3 0  9074
2 25544  51
6402 316
4479 0002263 339
4819  20
6242 15
54130189 29222


Satellite: ISS
Catalog Number: 25544
Epoch time:      18108
46386708   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:       316
4479  deg
Eccentricity:     
0002263     
Arg of perigee:   339
4819  deg
Mean anomaly:      20
6242  deg
Mean motion:   15
54130189  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2922
Checksum:              310


Coasting Arc #9 (Orbit 2937)
---------------------------------------

Vector Time (GMT): 2018/109/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4005664
88                 A    =         6777797
49  meter
 Y    =        1716193
21  meter          E    =           
0002635
 Z    =        5188843
11                 I    =           51
33884
 XDOT =      -4217
236139                 Wp   =           89
50193
 YDOT =       6299
402067  meter/sec      RA   =          310
90356  deg
 ZDOT =       1171
606413                 TA   =          349
21531
                                          MA   =          349
22096
                                          Ha   =            220
827  n
mi
                                          Hp   =            214
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13141945
13                 X    =         3960971
13
 Y    =        5630555
15  feet           Y    =         1760737
46  meter
 Z    =       17023763
49                 Z    =         5208193
00
 XDOT =     -13836
076571                 XDOT =       -4293
055478
 YDOT =      20667
329615  feet/sec       YDOT =        6251
818108  meter/sec
 ZDOT =       3843
853061                 ZDOT =        1150
935985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13539682
43                 X    =         4126895
21
 Y    =        4260840
03  feet           Y    =         1298704
04  meter
 Z    =       17109781
94                 Z    =         5215061
54
 XDOT =     -11349
442953                 XDOT =       -3459
310212
 YDOT =      20997
295037  feet/sec       YDOT =        6399
975527  meter/sec
 ZDOT =       3750
729482                 ZDOT =        1143
222346


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   18109
49269903  
00016717  00000-0  10270-3 0  9086
2 25544  51
6410 311
3188 0002257 344
3626  15
7456 15
54121727 29383


Satellite: ISS
Catalog Number: 25544
Epoch time:      18109
49269903   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:       311
3188  deg
Eccentricity:     
0002257     
Arg of perigee:   344
3626  deg
Mean anomaly:      15
7456  deg
Mean motion:   15
54121727  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2938
Checksum:              313


Coasting Arc #10 (Orbit 2952)
---------------------------------------

Vector Time (GMT): 2018/110/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2901693
04                 A    =         6777485
63  meter
 Y    =       -3167023
84  meter          E    =           
0013952
 Z    =       -5254573
99                 I    =           51
31634
 XDOT =       4947
275098                 Wp   =           86
79132
 YDOT =      -5795
894749  meter/sec      RA   =          305
88016  deg
 ZDOT =        763
818325                 TA   =          190
53460
                                          MA   =          190
56386
                                          Ha   =            220
938  n
mi
                                          Hp   =            214
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9519990
30                 X    =        -2840538
58
 Y    =      -10390498
16  feet           Y    =        -3199130
59  meter
 Z    =      -17239415
97                 Z    =        -5268521
08
 XDOT =      16231
217513                 XDOT =        5008
008406
 YDOT =     -19015
402719  feet/sec       YDOT =       -5740
231339  meter/sec
 ZDOT =       2505
965634                 ZDOT =         787
998253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10585189
70                 X    =        -3226365
82
 Y    =       -9187757
24  feet           Y    =        -2800428
41  meter
 Z    =      -17301127
31                 Z    =        -5273383
60
 XDOT =      13144
735610                 XDOT =        4006
515414
 YDOT =     -20052
019985  feet/sec       YDOT =       -6111
855691  meter/sec
 ZDOT =       2614
655184                 ZDOT =         796
946900


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   18110
45722297  
00016717  00000-0  10270-3 0  9095
2 25544  51
6401 306
5090 0002330 346
9185  13
1907 15
54156145 29533


Satellite: ISS
Catalog Number: 25544
Epoch time:      18110
45722297   =   yrday
fracday
Element set:     909
Inclination:       51
6401  deg
RA of node:       306
5090  deg
Eccentricity:     
0002330     
Arg of perigee:   346
9185  deg
Mean anomaly:      13
1907  deg
Mean motion:   15
54156145  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2953
Checksum:              292


Coasting Arc #11 (Orbit 2968)
---------------------------------------

Vector Time (GMT): 2018/111/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1736818
12                 A    =         6779580
39  meter
 Y    =        4511478
71  meter          E    =           
0008571
 Z    =        4750324
22                 I    =           51
30484
 XDOT =      -5342
460107                 Wp   =           46
21745
 YDOT =       4834
605142  meter/sec      RA   =          300
86030  deg
 ZDOT =      -2629
402049                 TA   =           69
88377
                                          MA   =           69
79157
                                          Ha   =            220
910  n
mi
                                          Hp   =            214
728

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5698222
19                 X    =         1663165
69
 Y    =       14801439
34  feet           Y    =         4530489
13  meter
 Z    =       15585053
22                 Z    =         4758582
32
 XDOT =     -17527
756256                 XDOT =       -5383
352562
 YDOT =      15861
565428  feet/sec       YDOT =        4774
633467  meter/sec
 ZDOT =      -8626
647142                 ZDOT =       -2655
453344

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7571551
01                 X    =         2307808
75
 Y    =       13895893
90  feet           Y    =         4235468
46  meter
 Z    =       15621202
72                 Z    =         4761342
59
 XDOT =     -14117
793570                 XDOT =       -4303
103480
 YDOT =      17553
980129  feet/sec       YDOT =        5350
453143  meter/sec
 ZDOT =      -8743
530165                 ZDOT =       -2665
027994


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   18111
48604546  
00016717  00000-0  10270-3 0  9107
2 25544  51
6399 301
3808 0002375 348
6146  11
4953 15
54171792 29698


Satellite: ISS
Catalog Number: 25544
Epoch time:      18111
48604546   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       301
3808  deg
Eccentricity:     
0002375     
Arg of perigee:   348
6146  deg
Mean anomaly:      11
4953  deg
Mean motion:   15
54171792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2969
Checksum:              319


Coasting Arc #12 (Orbit 2983)
---------------------------------------

Vector Time (GMT): 2018/112/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -638292
87                 A    =         6783210
91  meter
 Y    =       -5606781
51  meter          E    =           
0005522
 Z    =       -3768022
55                 I    =           51
30001
 XDOT =       5407
323982                 Wp   =           80
09264
 YDOT =      -3436
779771  meter/sec      RA   =          295
84615  deg
 ZDOT =       4204
118393                 TA   =          234
54626
                                          MA   =          234
59781
                                          Ha   =            220
985  n
mi
                                          Hp   =            214
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2094136
71                 X    =         -557245
72
 Y    =      -18394952
46  feet           Y    =        -5613466
16  meter
 Z    =      -12362278
71                 Z    =        -3770926
35
 XDOT =      17740
564244                 XDOT =        5424
931630
 YDOT =     -11275
524183  feet/sec       YDOT =       -3376
212925  meter/sec
 ZDOT =      13793
039347                 ZDOT =        4230
428158

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4823285
11                 X    =        -1470137
30
 Y    =      -17866049
55  feet           Y    =        -5445571
90  meter
 Z    =      -12374401
55                 Z    =        -3771717
59
 XDOT =      14397
922091                 XDOT =        4388
486653
 YDOT =     -13507
856706  feet/sec       YDOT =       -4117
194724  meter/sec
 ZDOT =      13910
861497                 ZDOT =        4240
030584


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   18112
45056466  
00016717  00000-0  10270-3 0  9118
2 25544  51
6390 296
5719 0002283 350
9319   9
1792 15
54158723 29842


Satellite: ISS
Catalog Number: 25544
Epoch time:      18112
45056466   =   yrday
fracday
Element set:     911
Inclination:       51
6390  deg
RA of node:       296
5719  deg
Eccentricity:     
0002283     
Arg of perigee:   350
9319  deg
Mean anomaly:       9
1792  deg
Mean motion:   15
54158723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2984
Checksum:              324


Coasting Arc #13 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2018/113/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -394139
35                 A    =         6786756
93  meter
 Y    =        6346415
01  meter          E    =           
0013050
 Z    =        2358580
69                 I    =           51
29927
 XDOT =      -5228
200355                 Wp   =           96
12534
 YDOT =       1674
474637  meter/sec      RA   =          290
84174  deg
 ZDOT =      -5355
085554                 TA   =           57
41165
                                          MA   =           57
28572
                                          Ha   =            221
015  n
mi
                                          Hp   =            214
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1293108
09                 X    =         -476534
16
 Y    =       20821571
55  feet           Y    =         6341546
80  meter
 Z    =        7738125
62                 Z    =         2356465
90
 XDOT =     -17152
888305                 XDOT =       -5220
523986
 YDOT =       5493
683193  feet/sec       YDOT =        1616
052162  meter/sec
 ZDOT =     -17569
178328                 ZDOT =       -5380
463761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2237843
89                 X    =          682094
82
 Y    =       20745170
25  feet           Y    =         6323127
89  meter
 Z    =        7727776
14                 Z    =         2355426
17
 XDOT =     -14332
859953                 XDOT =       -4368
655714
 YDOT =       8162
714783  feet/sec       YDOT =        2487
995466  meter/sec
 ZDOT =     -17682
584860                 ZDOT =       -5389
651865


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   18113
47937818  
00016717  00000-0  10270-3 0  9121
2 25544  51
6394 291
4425 0002557 354
5835   5
5289 15
54204974 30002


Satellite: ISS
Catalog Number: 25544
Epoch time:      18113
47937818   =   yrday
fracday
Element set:     912
Inclination:       51
6394  deg
RA of node:       291
4425  deg
Eccentricity:     
0002557     
Arg of perigee:   354
5835  deg
Mean anomaly:       5
5289  deg
Mean motion:   15
54204974  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3000
Checksum:              317


Coasting Arc #14 (Orbit 3014)
---------------------------------------

Vector Time (GMT): 2018/114/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1270994
28                 A    =         6789016
37  meter
 Y    =       -6622379
62  meter          E    =           
0012331
 Z    =        -730521
32                 I    =           51
29341
 XDOT =       4857
487041                 Wp   =           33
11387
 YDOT =        284
657489  meter/sec      RA   =          285
84457  deg
 ZDOT =       5928
384495                 TA   =          318
95295
                                          MA   =          319
04568
                                          Ha   =            221
117  n
mi
                                          Hp   =            214
562

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4169928
75                 X    =         1348501
57
 Y    =      -21726967
26  feet           Y    =        -6607733
14  meter
 Z    =       -2396723
48                 Z    =         -724158
80
 XDOT =      15936
637275                 XDOT =        4825
145888
 YDOT =        933
915647  feet/sec       YDOT =         338
796608  meter/sec
 ZDOT =      19450
080364                 ZDOT =        5951
901964

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          26297
33                 X    =            8015
43
 Y    =      -22126644
05  feet           Y    =        -6744201
11  meter
 Z    =       -2367409
35                 Z    =         -721586
37
 XDOT =      14088
236649                 XDOT =        4294
094531
 YDOT =      -2055
034203  feet/sec       YDOT =        -626
374425  meter/sec
 ZDOT =      19554
907298                 ZDOT =        5960
335744


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   18114
44388981  
00016717  00000-0  10270-3 0  9131
2 25544  51
6372 286
6337 0002287    
2560 359
8593 15
54159719 30151


Satellite: ISS
Catalog Number: 25544
Epoch time:      18114
44388981   =   yrday
fracday
Element set:     913
Inclination:       51
6372  deg
RA of node:       286
6337  deg
Eccentricity:     
0002287     
Arg of perigee:      
2560  deg
Mean anomaly:     359
8593  deg
Mean motion:   15
54159719  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3015
Checksum:              326


Coasting Arc #15 (Orbit 3030)
---------------------------------------

Vector Time (GMT): 2018/115/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2050128
49                 A    =         6788697
50  meter
 Y    =        6389427
85  meter          E    =           
0008061
 Z    =       -1011392
30                 I    =           51
28454
 XDOT =      -4348
050968                 Wp   =          129
68015
 YDOT =      -2318
830646  meter/sec      RA   =          280
85014  deg
 ZDOT =      -5871
822566                 TA   =           61
33171
                                          MA   =           61
25069
                                          Ha   =            221
147  n
mi
                                          Hp   =            214
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6726143
34                 X    =        -2116511
62
 Y    =       20962689
78  feet           Y    =         6366130
68  meter
 Z    =       -3318216
22                 Z    =        -1021512
69
 XDOT =     -14265
259082                 XDOT =       -4293
275688
 YDOT =      -7607
712094  feet/sec       YDOT =       -2367
147557  meter/sec
 ZDOT =     -19264
509731                 ZDOT =       -5892
810819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2267326
09                 X    =         -691080
99
 Y    =       21891255
33  feet           Y    =         6672454
63  meter
 Z    =       -3364238
15                 Z    =        -1025419
79
 XDOT =     -13800
315447                 XDOT =       -4206
336148
 YDOT =      -4386
139607  feet/sec       YDOT =       -1336
895352  meter/sec
 ZDOT =     -19357
774740                 ZDOT =       -5900
249741


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   18115
47269698  
00016717  00000-0  10270-3 0  9149
2 25544  51
6370 281
5045 0002417   4
1236 355
9936 15
54191078 30317


Satellite: ISS
Catalog Number: 25544
Epoch time:      18115
47269698   =   yrday
fracday
Element set:     914
Inclination:       51
6370  deg
RA of node:       281
5045  deg
Eccentricity:     
0002417     
Arg of perigee:     4
1236  deg
Mean anomaly:     355
9936  deg
Mean motion:   15
54191078  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3031
Checksum:              310


Coasting Arc #16 (Orbit 3045)
---------------------------------------

Vector Time (GMT): 2018/116/10:37:11
515
Vector Time (MET): N/A
Weight (LBS)     : 928421
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2685716
60                 A    =         6786213
53  meter
 Y    =       -5648535
47  meter          E    =           
0014510
 Z    =        2613526
97                 I    =           51
27076
 XDOT =       3762
008049                 Wp   =           69
12051
 YDOT =       4203
498575  meter/sec      RA   =          275
84985  deg
 ZDOT =       5200
624492                 TA   =          320
49854
                                          MA   =          320
60422
                                          Ha   =            221
109  n
mi
                                          Hp   =            214
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8811406
17                 X    =         2735985
23
 Y    =      -18531940
50  feet           Y    =        -5618220
72  meter
 Z    =        8574563
54                 Z    =         2626695
76
 XDOT =      12342
546091                 XDOT =        3689
461703
 YDOT =      13791
005822  feet/sec       YDOT =        4245
162602  meter/sec
 ZDOT =      17062
416311                 ZDOT =        5218
722713

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4428821
00                 X    =         1349904
64
 Y    =      -20010880
99  feet           Y    =        -6099316
53  meter
 Z    =        8634061
85                 Z    =         2631662
05
 XDOT =      13523
443623                 XDOT =        4121
945616
 YDOT =      10415
273711  feet/sec       YDOT =        3174
575427  meter/sec
 ZDOT =      17142
540130                 ZDOT =        5225
046232


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   18116
50149958  
00016717  00000-0  10270-3 0  9151
2 25544  51
6367 276
3741 0002202   8
1942 351
9246 15
54190719 30465


Satellite: ISS
Catalog Number: 25544
Epoch time:      18116
50149958   =   yrday
fracday
Element set:     915
Inclination:       51
6367  deg
RA of node:       276
3741  deg
Eccentricity:     
0002202     
Arg of perigee:     8
1942  deg
Mean anomaly:     351
9246  deg
Mean motion:   15
54190719  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3046
Checksum:              310
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