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

 
Date: March 5th 2018

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) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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


069/22:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 1
000/00:00:00 000 0 0 0 0 214 5

072/21:25:56 618 -0 5 0 7 0 7
N/A 0 4 -0 1 220 9
000/00:01:53 236 0 2 0 0 215 1

073/06:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 215 1

077/07:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 215 3

Coasting Arc #1 (Orbit 2238)
---------------------------------------

Vector Time (GMT): 2018/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         462443
88                 A    =         6777280
06  meter
 Y    =       -4233062
00  meter          E    =           
0003899
 Z    =        5269140
32                 I    =           51
65274
 XDOT =       7631
818594                 Wp   =          109
46067
 YDOT =       -127
910913  meter/sec      RA   =          174
44239  deg
 ZDOT =       -773
367544                 TA   =          347
91952
                                          MA   =          347
92887
                                          Ha   =            221
429  n
mi
                                          Hp   =            214
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1517204
34                 X    =          484150
26
 Y    =      -13887998
67  feet           Y    =        -4227768
56  meter
 Z    =       17287205
79                 Z    =         5271439
98
 XDOT =      25038
774915                 XDOT =        7636
438301
 YDOT =       -419
655227  feet/sec       YDOT =         -42
540943  meter/sec
 ZDOT =      -2537
295091                 ZDOT =        -736
283882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5555469
69                 X    =         1693307
16
 Y    =      -12804074
40  feet           Y    =        -3902681
88  meter
 Z    =       17297928
65                 Z    =         5272408
65
 XDOT =      23064
665305                 XDOT =        7030
109985
 YDOT =       6806
482429  feet/sec       YDOT =        2074
615844  meter/sec
 ZDOT =      -2371
958833                 ZDOT =        -722
973052


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   18064
54701166  
00016717  00000-0  10270-3 0  9006
2 25544  51
6410 175
3858 0002848 160
8601 199
2659 15
54209707 22397


Satellite: ISS
Catalog Number: 25544
Epoch time:      18064
54701166   =   yrday
fracday
Element set:     900
Inclination:       51
6410  deg
RA of node:       175
3858  deg
Eccentricity:     
0002848     
Arg of perigee:   160
8601  deg
Mean anomaly:     199
2659  deg
Mean motion:   15
54209707  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2239
Checksum:              317


Coasting Arc #2 (Orbit 2253)
---------------------------------------

Vector Time (GMT): 2018/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2251023
88                 A    =         6779363
21  meter
 Y    =        4261101
57  meter          E    =           
0013235
 Z    =       -4780922
81                 I    =           51
69203
 XDOT =      -7140
351201                 Wp   =          119
34232
 YDOT =       -798
753766  meter/sec      RA   =          169
44815  deg
 ZDOT =       2649
218816                 TA   =          176
82185
                                          MA   =          176
81343
                                          Ha   =            221
402  n
mi
                                          Hp   =            214
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7385248
96                 X    =        -2275282
31
 Y    =       13979992
01  feet           Y    =         4235792
88  meter
 Z    =      -15685442
29                 Z    =        -4791916
85
 XDOT =     -23426
349086                 XDOT =       -7143
757068
 YDOT =      -2620
583221  feet/sec       YDOT =        -878
620817  meter/sec
 ZDOT =       8691
662781                 ZDOT =        2614
525503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10991414
27                 X    =        -3350183
07
 Y    =       11296715
22  feet           Y    =         3443238
80  meter
 Z    =      -15734936
17                 Z    =        -4796008
54
 XDOT =     -20916
092118                 XDOT =       -6375
224878
 YDOT =      -8456
092824  feet/sec       YDOT =       -2577
417093  meter/sec
 ZDOT =       8537
069791                 ZDOT =        2602
098872


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   18065
51150713  
00016717  00000-0  10270-3 0  9011
2 25544  51
6406 170
5790 0002929 163
8903 196
2344 15
54210246 22547


Satellite: ISS
Catalog Number: 25544
Epoch time:      18065
51150713   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:       170
5790  deg
Eccentricity:     
0002929     
Arg of perigee:   163
8903  deg
Mean anomaly:     196
2344  deg
Mean motion:   15
54210246  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2254
Checksum:              292


Coasting Arc #3 (Orbit 2269)
---------------------------------------

Vector Time (GMT): 2018/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3824416
48                 A    =         6783088
44  meter
 Y    =       -4141758
52  meter          E    =           
0012186
 Z    =        3760490
31                 I    =           51
73642
 XDOT =       6128
609033                 Wp   =           97
28162
 YDOT =       1782
700943  meter/sec      RA   =          164
46274  deg
 ZDOT =      -4259
041661                 TA   =           37
74646
                                          MA   =           37
66104
                                          Ha   =            221
341  n
mi
                                          Hp   =            214
261

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12547298
15                 X    =         3852180
13
 Y    =      -13588446
59  feet           Y    =        -4098835
66  meter
 Z    =       12337566
63                 Z    =         3779135
73
 XDOT =      20106
985017                 XDOT =        6128
906962
 YDOT =       5848
756375  feet/sec       YDOT =        1851
236505  meter/sec
 ZDOT =     -13973
233795                 ZDOT =       -4229
270630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15679759
72                 X    =         4779190
76
 Y    =       -9703385
31  feet           Y    =        -2957591
84  meter
 Z    =       12421174
29                 Z    =         3785973
92
 XDOT =      17152
416538                 XDOT =        5228
056561
 YDOT =       9956
433904  feet/sec       YDOT =        3034
721054  meter/sec
 ZDOT =     -13840
683024                 ZDOT =       -4218
640186


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   18066
54029898  
00016717  00000-0  10270-3 0  9025
2 25544  51
6407 165
4498 0002916 166
7306 193
3924 15
54181761 22700


Satellite: ISS
Catalog Number: 25544
Epoch time:      18066
54029898   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:       165
4498  deg
Eccentricity:     
0002916     
Arg of perigee:   166
7306  deg
Mean anomaly:     193
3924  deg
Mean motion:   15
54181761  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2270
Checksum:              329


Coasting Arc #4 (Orbit 2284)
---------------------------------------

Vector Time (GMT): 2018/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5047828
39                 A    =         6786757
92  meter
 Y    =        3874110
43  meter          E    =           
0004590
 Z    =       -2361921
20                 I    =           51
78029
 XDOT =      -4665
737393                 Wp   =           74
49092
 YDOT =      -2793
851667  meter/sec      RA   =          159
49040  deg
 ZDOT =       5398
827636                 TA   =          259
21779
                                          MA   =          259
26946
                                          Ha   =            221
254  n
mi
                                          Hp   =            214
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16561116
76                 X    =        -5079301
68
 Y    =       12710336
06  feet           Y    =         3817485
96  meter
 Z    =       -7749085
31                 Z    =        -2386518
41
 XDOT =     -15307
537380                 XDOT =       -4660
373509
 YDOT =      -9166
180010  feet/sec       YDOT =       -2845
996692  meter/sec
 ZDOT =      17712
689093                 ZDOT =        5376
176521

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19198489
56                 X    =        -5851699
62
 Y    =        8094579
80  feet           Y    =         2467227
92  meter
 Z    =       -7859219
46                 Z    =        -2395490
09
 XDOT =     -11996
894535                 XDOT =       -3656
653454
 YDOT =     -11385
175261  feet/sec       YDOT =       -3470
201420  meter/sec
 ZDOT =      17611
990441                 ZDOT =        5368
134686


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   18067
50478587  
00016717  00000-0  10270-3 0  9036
2 25544  51
6409 160
6416 0002604 172
2324 187
8869 15
54174787 22857


Satellite: ISS
Catalog Number: 25544
Epoch time:      18067
50478587   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:       160
6416  deg
Eccentricity:     
0002604     
Arg of perigee:   172
2324  deg
Mean anomaly:     187
8869  deg
Mean motion:   15
54174787  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2285
Checksum:              337


Coasting Arc #5 (Orbit 2300)
---------------------------------------

Vector Time (GMT): 2018/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5842938
07                 A    =         6788929
93  meter
 Y    =       -3373260
08  meter          E    =           
0015301
 Z    =         677259
98                 I    =           51
81701
 XDOT =       2909
218074                 Wp   =          135
31621
 YDOT =       3824
074552  meter/sec      RA   =          154
52914  deg
 ZDOT =      -5980
741286                 TA   =           37
38357
                                          MA   =           37
27721
                                          Ha   =            221
262  n
mi
                                          Hp   =            214
374

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19169744
34                 X    =         5876934
78
 Y    =      -11067126
25  feet           Y    =        -3307730
19  meter
 Z    =        2221981
56                 Z    =          705725
55
 XDOT =       9544
678722                 XDOT =        2895
291069
 YDOT =      12546
176352  feet/sec       YDOT =        3856
529086  meter/sec
 ZDOT =     -19621
854614                 ZDOT =       -5966
643559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21235455
88                 X    =         6472566
95
 Y    =       -6199487
60  feet           Y    =        -1889603
82  meter
 Z    =        2349329
82                 Z    =          716075
73
 XDOT =       5964
689608                 XDOT =        1818
037392
 YDOT =      12935
239313  feet/sec       YDOT =        3942
660943  meter/sec
 ZDOT =     -19559
413390                 ZDOT =       -5961
709201


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   18068
53357098  
00016717  00000-0  10270-3 0  9044
2 25544  51
6399 155
5131 0002782 173
7238 186
3950 15
54192430 23018


Satellite: ISS
Catalog Number: 25544
Epoch time:      18068
53357098   =   yrday
fracday
Element set:     904
Inclination:       51
6399  deg
RA of node:       155
5131  deg
Eccentricity:     
0002782     
Arg of perigee:   173
7238  deg
Mean anomaly:     186
3950  deg
Mean motion:   15
54192430  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2301
Checksum:              316


Coasting Arc #6 (Orbit 2316)
---------------------------------------

Vector Time (GMT): 2018/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6152492
24                 A    =         6788702
20  meter
 Y    =        2659060
68  meter          E    =           
0012370
 Z    =        1047792
12                 I    =           51
84598
 XDOT =      -1046
673427                 Wp   =           66
70927
 YDOT =      -4770
913445  meter/sec      RA   =          149
57177  deg
 ZDOT =       5911
078914                 TA   =          304
61818
                                          MA   =          304
73477
                                          Ha   =            221
163  n
mi
                                          Hp   =            214
516

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20185341
98                 X    =        -6186858
88
 Y    =        8723952
37  feet           Y    =         2590067
21  meter
 Z    =        3437638
18                 Z    =         1017822
08
 XDOT =      -3433
967937                 XDOT =       -1021
958601
 YDOT =     -15652
603165  feet/sec       YDOT =       -4782
479425  meter/sec
 ZDOT =      19393
303523                 ZDOT =        5906
054982

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21635272
84                 X    =        -6594431
16
 Y    =        4046437
07  feet           Y    =         1233354
02  meter
 Z    =        3303641
68                 Z    =         1006949
98
 XDOT =        277
296478                 XDOT =          84
519967
 YDOT =     -14473
599350  feet/sec       YDOT =       -4411
553082  meter/sec
 ZDOT =      19371
443192                 ZDOT =        5904
415885


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   18069
56235228  
00016717  00000-0  10270-3 0  9059
2 25544  51
6404 150
3839 0002628 178
1178 181
9985 15
54196990 23175


Satellite: ISS
Catalog Number: 25544
Epoch time:      18069
56235228   =   yrday
fracday
Element set:     905
Inclination:       51
6404  deg
RA of node:       150
3839  deg
Eccentricity:     
0002628     
Arg of perigee:   178
1178  deg
Mean anomaly:     181
9985  deg
Mean motion:   15
54196990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2317
Checksum:              338


Coasting Arc #7 (Orbit 2322)
---------------------------------------

Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          41067
95                 A    =         6778616
77  meter
 Y    =        4617572
78  meter          E    =           
0013384
 Z    =       -4974814
06                 I    =           51
82445
 XDOT =      -6936
277761                 Wp   =          115
09963
 YDOT =       2407
621885  meter/sec      RA   =          147
38002  deg
 ZDOT =       2176
518079                 TA   =          176
10030
                                          MA   =          176
08986
                                          Ha   =            221
068  n
mi
                                          Hp   =            214
462

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         134737
37                 X    =           13594
70
 Y    =       15149516
99  feet           Y    =         4617878
03  meter
 Z    =      -16321568
43                 Z    =        -4974681
65
 XDOT =     -22756
816802                 XDOT =       -6973
257188
 YDOT =       7899
021931  feet/sec       YDOT =        2329
849062  meter/sec
 ZDOT =       7140
807345                 ZDOT =        2142
734424

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8589028
20                 X    =         2617935
80
 Y    =      -12480242
17  feet           Y    =        -3803977
81  meter
 Z    =      -16321512
34                 Z    =        -4974796
96
 XDOT =      22247
437453                 XDOT =        6781
018936
 YDOT =       6165
622031  feet/sec       YDOT =        1879
281595  meter/sec
 ZDOT =       6989
818813                 ZDOT =        2130
496774


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   18069
94814526  
00016717  00000-0  10270-3 0  9066
2 25544  51
6400 148
4623 0002213 177
1132 183
0033 15
54212630 23233


Satellite: ISS
Catalog Number: 25544
Epoch time:      18069
94814526   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       148
4623  deg
Eccentricity:     
0002213     
Arg of perigee:   177
1132  deg
Mean anomaly:     183
0033  deg
Mean motion:   15
54212630  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2323
Checksum:              273


Coasting Arc #8 (Orbit 2338)
---------------------------------------

Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1507230
87                 A    =         6782015
64  meter
 Y    =       -5199781
79  meter          E    =           
0010375
 Z    =        4076016
13                 I    =           51
86302
 XDOT =       6512
518306                 Wp   =           89
40452
 YDOT =      -1164
707833  meter/sec      RA   =          142
40199  deg
 ZDOT =      -3885
396348                 TA   =           40
71377
                                          MA   =           40
63627
                                          Ha   =            221
049  n
mi
                                          Hp   =            214
488

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4944983
19                 X    =         1545465
35
 Y    =      -17059651
54  feet           Y    =        -5182712
78  meter
 Z    =       13372756
33                 Z    =         4083430
92
 XDOT =      21366
529874                 XDOT =        6543
931326
 YDOT =      -3821
219923  feet/sec       YDOT =       -1091
705051  meter/sec
 ZDOT =     -12747
363346                 ZDOT =       -3853
684819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13658143
87                 X    =        -4163002
25
 Y    =       11315367
19  feet           Y    =         3448923
92  meter
 Z    =       13406444
44                 Z    =         4086284
26
 XDOT =     -19022
566675                 XDOT =       -5798
078323
 YDOT =      -7992
344890  feet/sec       YDOT =       -2436
066722  meter/sec
 ZDOT =     -12605
744095                 ZDOT =       -3842
230800


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   18070
97692217  
00016717  00000-0  10270-3 0  9073
2 25544  51
6401 143
3340 0002192 178
6696 181
4463 15
54205275 23394


Satellite: ISS
Catalog Number: 25544
Epoch time:      18070
97692217   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:       143
3340  deg
Eccentricity:     
0002192     
Arg of perigee:   178
6696  deg
Mean anomaly:     181
4463  deg
Mean motion:   15
54205275  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2339
Checksum:              311


Coasting Arc #9 (Orbit 2353)
---------------------------------------

Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2814250
23                 A    =         6785761
76  meter
 Y    =        5524316
30  meter          E    =           
0003947
 Z    =       -2761409
73                 I    =           51
90163
 XDOT =      -5654
383967                 Wp   =           86
58491
 YDOT =       -303
062207  meter/sec      RA   =          137
43511  deg
 ZDOT =       5162
875487                 TA   =          242
28279
                                          MA   =          242
32283
                                          Ha   =            220
947  n
mi
                                          Hp   =            214
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9233104
44                 X    =        -2862402
20
 Y    =       18124397
31  feet           Y    =         5492575
93  meter
 Z    =       -9059743
20                 Z    =        -2775197
63
 XDOT =     -18551
128502                 XDOT =       -5675
652963
 YDOT =       -994
298580  feet/sec       YDOT =        -366
411871  meter/sec
 ZDOT =      16938
567872                 ZDOT =        5135
357225

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17649278
02                 X    =         5379499
94
 Y    =      -10055674
98  feet           Y    =        -3064969
74  meter
 Z    =       -9121914
72                 Z    =        -2780359
61
 XDOT =      14284
600317                 XDOT =        4353
946177
 YDOT =       9836
841994  feet/sec       YDOT =        2998
269440  meter/sec
 ZDOT =      16815
814642                 ZDOT =        5125
460303


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   18071
94139804  
00016717  00000-0  10270-3 0  9080
2 25544  51
6405 138
5254 0002177 183
7524 176
3613 15
54227463 23548


Satellite: ISS
Catalog Number: 25544
Epoch time:      18071
94139804   =   yrday
fracday
Element set:     908
Inclination:       51
6405  deg
RA of node:       138
5254  deg
Eccentricity:     
0002177     
Arg of perigee:   183
7524  deg
Mean anomaly:     176
3613  deg
Mean motion:   15
54227463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2354
Checksum:              312


Coasting Arc #10 (Orbit 2368)
---------------------------------------

Vector Time (GMT): 2018/072/21:26:53
236
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1118863
81                 A    =         6779129
19  meter
 Y    =        4509420
81  meter          E    =           
0012140
 Z    =       -4947847
64                 I    =           51
90049
 XDOT =      -6118
018887                 Wp   =          116
42654
 YDOT =       4009
322652  meter/sec      RA   =          132
68125  deg
 ZDOT =       2269
624519                 TA   =          175
70062
                                          MA   =          175
69018
                                          Ha   =            220
878  n
mi
                                          Hp   =            215
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3670813
04                 X    =         1092388
76
 Y    =       14794687
69  feet           Y    =         4521784
17  meter
 Z    =      -16233095
92                 Z    =        -4942477
44
 XDOT =     -20072
240443                 XDOT =       -6173
421992
 YDOT =      13153
945710  feet/sec       YDOT =        3940
597215  meter/sec
 ZDOT =       7446
274667                 ZDOT =        2239
770788

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8397100
06                 X    =         2559436
10
 Y    =      -12751727
14  feet           Y    =        -3886726
43  meter
 Z    =      -16209664
43                 Z    =        -4940705
72
 XDOT =      22342
223717                 XDOT =        6809
909789
 YDOT =       5412
950409  feet/sec       YDOT =        1649
867285  meter/sec
 ZDOT =       7312
578012                 ZDOT =        2228
873778


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   18072
90587236  
00016717  00000-0  10270-3 0  9094
2 25544  51
6404 133
7165 0002095 205
3156 154
7894 15
54085050 23697


Satellite: ISS
Catalog Number: 25544
Epoch time:      18072
90587236   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:       133
7165  deg
Eccentricity:     
0002095     
Arg of perigee:   205
3156  deg
Mean anomaly:     154
7894  deg
Mean motion:   15
54085050  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2369
Checksum:              315


Coasting Arc #11 (Orbit 2374)
---------------------------------------

Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -572474
60                 A    =         6782718
35  meter
 Y    =        5458897
25  meter          E    =           
0007151
 Z    =       -3992957
52                 I    =           51
92044
 XDOT =      -6114
668339                 Wp   =          128
67888
 YDOT =       2289
154437  meter/sec      RA   =          130
73625  deg
 ZDOT =       4006
722489                 TA   =          182
96028
                                          MA   =          182
96451
                                          Ha   =            220
941  n
mi
                                          Hp   =            215
076

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1878197
52                 X    =         -614079
54
 Y    =       17909767
90  feet           Y    =         5452262
39  meter
 Z    =      -13100254
33                 Z    =        -3995840
00
 XDOT =     -20061
247832                 XDOT =       -6159
274083
 YDOT =       7510
349202  feet/sec       YDOT =        2220
527042  meter/sec
 ZDOT =      13145
414989                 ZDOT =        3976
911423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17975614
24                 X    =        -5478967
22
 Y    =        -900297
30  feet           Y    =         -274410
62  meter
 Z    =      -13113765
01                 Z    =        -3997075
58
 XDOT =      -8568
076697                 XDOT =       -2611
549777
 YDOT =     -18439
002066  feet/sec       YDOT =       -5620
207830  meter/sec
 ZDOT =      13012
106572                 ZDOT =        3966
090083


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   18073
29169538  
00016717  00000-0  10270-3 0  9100
2 25544  51
6398 131
7890 0002556 202
5449 157
5591 15
54075644 23758


Satellite: ISS
Catalog Number: 25544
Epoch time:      18073
29169538   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       131
7890  deg
Eccentricity:     
0002556     
Arg of perigee:   202
5449  deg
Mean anomaly:     157
5591  deg
Mean motion:   15
54075644  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2375
Checksum:              332


Coasting Arc #12 (Orbit 2390)
---------------------------------------

Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1748470
80                 A    =         6786466
71  meter
 Y    =       -5985944
63  meter          E    =           
0013273
 Z    =        2658877
34                 I    =           51
95348
 XDOT =       5561
822627                 Wp   =          113
26451
 YDOT =       -708
431894  meter/sec      RA   =          125
77484  deg
 ZDOT =      -5236
776961                 TA   =           36
86541
                                          MA   =           36
77424
                                          Ha   =            220
932  n
mi
                                          Hp   =            215
089

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5736452
75                 X    =         1802362
07
 Y    =      -19638925
94  feet           Y    =        -5966090
37  meter
 Z    =        8723350
86                 Z    =         2667502
32
 XDOT =      18247
449563                 XDOT =        5594
768279
 YDOT =      -2324
251621  feet/sec       YDOT =        -646
052208  meter/sec
 ZDOT =     -17181
026774                 ZDOT =       -5209
679843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19973818
51                 X    =         6088019
88
 Y    =        4353766
26  feet           Y    =         1327027
96  meter
 Z    =        8762559
32                 Z    =         2670828
08
 XDOT =       3864
758546                 XDOT =        1177
978405
 YDOT =      16707
522951  feet/sec       YDOT =        5092
452996  meter/sec
 ZDOT =     -17060
006918                 ZDOT =       -5199
890109


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   18074
32055633  
00016717  00000-0  10270-3 0  9116
2 25544  51
6397 126
6603 0002563 203
7818 156
3217 15
54073021 23910


Satellite: ISS
Catalog Number: 25544
Epoch time:      18074
32055633   =   yrday
fracday
Element set:     911
Inclination:       51
6397  deg
RA of node:       126
6603  deg
Eccentricity:     
0002563     
Arg of perigee:   203
7818  deg
Mean anomaly:     156
3217  deg
Mean motion:   15
54073021  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2391
Checksum:              290


Coasting Arc #13 (Orbit 2405)
---------------------------------------

Vector Time (GMT): 2018/075/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2683102
36                 A    =         6788944
00  meter
 Y    =        6139452
65  meter          E    =           
0007070
 Z    =       -1076636
49                 I    =           51
98029
 XDOT =      -4760
836987                 Wp   =           41
98118
 YDOT =      -1047
985274  meter/sec      RA   =          120
82389  deg
 ZDOT =       5915
968838                 TA   =          306
40067
                                          MA   =          306
46586
                                          Ha   =            220
827  n
mi
                                          Hp   =            215
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8802829
26                 X    =        -2746326
30
 Y    =       20142561
17  feet           Y    =         6109094
69  meter
 Z    =       -3532271
95                 Z    =        -1089824
31
 XDOT =     -15619
543920                 XDOT =       -4777
500610
 YDOT =      -3438
271897  feet/sec       YDOT =       -1101
316592  meter/sec
 ZDOT =      19409
346583                 ZDOT =        5892
802299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20808384
93                 X    =        -6342395
73
 Y    =       -7056846
52  feet           Y    =        -2150926
82  meter
 Z    =       -3591873
12                 Z    =        -1094802
93
 XDOT =       1587
647281                 XDOT =         483
914891
 YDOT =     -14462
951304  feet/sec       YDOT =       -4408
307558  meter/sec
 ZDOT =      19306
073436                 ZDOT =        5884
491183


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   18075
28511135  
00016717  00000-0  10270-3 0  9127
2 25544  51
6397 121
8528 0002460 208
2961 151
8059 15
54084620 24066


Satellite: ISS
Catalog Number: 25544
Epoch time:      18075
28511135   =   yrday
fracday
Element set:     912
Inclination:       51
6397  deg
RA of node:       121
8528  deg
Eccentricity:     
0002460     
Arg of perigee:   208
2961  deg
Mean anomaly:     151
8059  deg
Mean motion:   15
54084620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2406
Checksum:              297


Coasting Arc #14 (Orbit 2421)
---------------------------------------

Vector Time (GMT): 2018/076/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3393056
12                 A    =         6789242
46  meter
 Y    =       -5837419
07  meter          E    =           
0011693
 Z    =        -646389
07                 I    =           51
99735
 XDOT =       3815
224541                 Wp   =          151
39335
 YDOT =       2875
933612  meter/sec      RA   =          115
87781  deg
 ZDOT =      -5999
629766                 TA   =           35
55300
                                          MA   =           35
47514
                                          Ha   =            220
771  n
mi
                                          Hp   =            215
188

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11132073
90                 X    =         3461219
34
 Y    =      -19151637
36  feet           Y    =        -5799094
55  meter
 Z    =       -2120699
05                 Z    =         -629740
53
 XDOT =      12517
140881                 XDOT =        3811
924305
 YDOT =       9435
477730  feet/sec       YDOT =        2918
578761  meter/sec
 ZDOT =     -19683
824691                 ZDOT =       -5981
105322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20180545
85                 X    =         6151030
38
 Y    =        9152399
86  feet           Y    =         2789651
48  meter
 Z    =       -2045676
72                 Z    =         -623522
26
 XDOT =      -7439
573220                 XDOT =       -2267
581918
 YDOT =      12064
233903  feet/sec       YDOT =        3677
178494  meter/sec
 ZDOT =     -19601
490918                 ZDOT =       -5974
534432


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   18076
31396810  
00016717  00000-0  10270-3 0  9134
2 25544  51
6397 116
7241 0002507 212
9448 147
1549 15
54101742 24220


Satellite: ISS
Catalog Number: 25544
Epoch time:      18076
31396810   =   yrday
fracday
Element set:     913
Inclination:       51
6397  deg
RA of node:       116
7241  deg
Eccentricity:     
0002507     
Arg of perigee:   212
9448  deg
Mean anomaly:     147
1549  deg
Mean motion:   15
54101742  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2422
Checksum:              298


Coasting Arc #15 (Orbit 2437)
---------------------------------------

Vector Time (GMT): 2018/077/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3852362
77                 A    =         6787232
87  meter
 Y    =        5097393
63  meter          E    =           
0012041
 Z    =        2275160
57                 I    =           52
00486
 XDOT =      -2819
664257                 Wp   =           78
69027
 YDOT =      -4580
621943  meter/sec      RA   =          110
93007  deg
 ZDOT =       5466
232662                 TA   =          306
50261
                                          MA   =          306
61346
                                          Ha   =            220
716  n
mi
                                          Hp   =            215
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12638985
48                 X    =        -3920128
38
 Y    =       16723732
39  feet           Y    =         5053935
29  meter
 Z    =        7464437
57                 Z    =         2256281
89
 XDOT =      -9250
866984                 XDOT =       -2794
784895
 YDOT =     -15028
287214  feet/sec       YDOT =       -4612
013466  meter/sec
 ZDOT =      17933
834194                 ZDOT =        5452
596867

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18106805
26                 X    =        -5518954
24
 Y    =      -10622193
96  feet           Y    =        -3237644
72  meter
 Z    =        7379539
69                 Z    =         2249283
70
 XDOT =      13039
533589                 XDOT =        3974
449838
 YDOT =      -9759
221659  feet/sec       YDOT =       -2974
610762  meter/sec
 ZDOT =      17873
534285                 ZDOT =        5447
853250


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   18077
34282168  
00016717  00000-0  10270-3 0  9149
2 25544  51
6405 111
5953 0002375 215
2685 144
8311 15
54112822 24384


Satellite: ISS
Catalog Number: 25544
Epoch time:      18077
34282168   =   yrday
fracday
Element set:     914
Inclination:       51
6405  deg
RA of node:       111
5953  deg
Eccentricity:     
0002375     
Arg of perigee:   215
2685  deg
Mean anomaly:     144
8311  deg
Mean motion:   15
54112822  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2438
Checksum:              297


Coasting Arc #16 (Orbit 2437)
---------------------------------------

Vector Time (GMT): 2018/077/07:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2755512
09                 A    =         6778963
99  meter
 Y    =        3709064
84  meter          E    =           
0011705
 Z    =       -4971070
04                 I    =           51
97809
 XDOT =      -4137
118898                 Wp   =          116
84893
 YDOT =       6051
122916  meter/sec      RA   =          110
65869  deg
 ZDOT =       2220
558786                 TA   =          174
75116
                                          MA   =          174
73888
                                          Ha   =            220
626  n
mi
                                          Hp   =            215
271

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9040394
01                 X    =         2737978
27
 Y    =       12168847
92  feet           Y    =         3739780
12  meter
 Z    =      -16309284
92                 Z    =        -4957727
90
 XDOT =     -13573
224732                 XDOT =       -4215
262980
 YDOT =      19852
765473  feet/sec       YDOT =        6004
422198  meter/sec
 ZDOT =       7285
297855                 ZDOT =        2200
271512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7404106
69                 X    =        -2256771
72
 Y    =       13300862
21  feet           Y    =         4054102
80  meter
 Z    =      -16250188
51                 Z    =        -4953057
46
 XDOT =     -22704
130864                 XDOT =       -6920
219087
 YDOT =      -3844
868301  feet/sec       YDOT =       -1171
915858  meter/sec
 ZDOT =       7193
993956                 ZDOT =        2192
729358


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   18077
34282150  
00016717  00000-0  10270-3 0  9151
2 25544  51
6406 111
5969 0002324 218
0409 142
0579 15
54123482 24381


Satellite: ISS
Catalog Number: 25544
Epoch time:      18077
34282150   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:       111
5969  deg
Eccentricity:     
0002324     
Arg of perigee:   218
0409  deg
Mean anomaly:     142
0579  deg
Mean motion:   15
54123482  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2438
Checksum:              296


Coasting Arc #17 (Orbit 2453)
---------------------------------------

Vector Time (GMT): 2018/078/07:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1893714
46                 A    =         6782347
02  meter
 Y    =       -5065026
20  meter          E    =           
0008867
 Z    =        4086699
71                 I    =           51
99945
 XDOT =       4513
566042                 Wp   =           85
85536
 YDOT =      -4831
866514  meter/sec      RA   =          105
69056  deg
 ZDOT =      -3889
199579                 TA   =           44
22533
                                          MA   =           44
15450
                                          Ha   =            220
673  n
mi
                                          Hp   =            215
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6212973
93                 X    =        -1856786
25
 Y    =      -16617540
03  feet           Y    =        -5085995
97  meter
 Z    =       13407807
44                 Z    =         4077591
10
 XDOT =      14808
287541                 XDOT =        4586
153513
 YDOT =     -15852
580425  feet/sec       YDOT =       -4780
987393  meter/sec
 ZDOT =     -12759
841138                 ZDOT =       -3867
097269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12408630
02                 X    =         3782150
43
 Y    =      -12721682
52  feet           Y    =        -3877568
83  meter
 Z    =       13367785
05                 Z    =         4074500
88
 XDOT =      19727
809452                 XDOT =        6013
036321
 YDOT =       5911
589870  feet/sec       YDOT =        1801
852592  meter/sec
 ZDOT =     -12660
573608                 ZDOT =       -3858
942836


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   18078
37167413  
00016717  00000-0  10270-3 0  9160
2 25544  51
6401 106
4681 0002262 222
5964 137
5014 15
54106373 24548


Satellite: ISS
Catalog Number: 25544
Epoch time:      18078
37167413   =   yrday
fracday
Element set:     916
Inclination:       51
6401  deg
RA of node:       106
4681  deg
Eccentricity:     
0002262     
Arg of perigee:   222
5964  deg
Mean anomaly:     137
5014  deg
Mean motion:   15
54106373  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2454
Checksum:              292


Coasting Arc #18 (Orbit 2468)
---------------------------------------

Vector Time (GMT): 2018/079/07:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904716
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1071847
48                 A    =         6786135
20  meter
 Y    =        6087807
58  meter          E    =           
0002423
 Z    =       -2801024
48                 I    =           52
01947
 XDOT =      -4695
272825                 Wp   =           69
71601
 YDOT =       3192
823810  meter/sec      RA   =          100
73324  deg
 ZDOT =       5147
059859                 TA   =          258
70777
                                          MA   =          258
73501
                                          Ha   =            220
511  n
mi
                                          Hp   =            215
415

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3516559
99                 X    =         1017298
25
 Y    =       19973121
99  feet           Y    =         6099488
36  meter
 Z    =       -9189712
87                 Z    =        -2795951
07
 XDOT =     -15404
438403                 XDOT =       -4755
628680
 YDOT =      10475
143734  feet/sec       YDOT =        3139
981224  meter/sec
 ZDOT =      16886
679327                 ZDOT =        5124
104775

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16397272
20                 X    =        -4997888
57
 Y    =       11950845
08  feet           Y    =         3642617
58  meter
 Z    =       -9167845
18                 Z    =        -2794359
21
 XDOT =     -15335
082278                 XDOT =       -4674
133078
 YDOT =      -8176
432025  feet/sec       YDOT =       -2492
176481  meter/sec
 ZDOT =      16783
800898                 ZDOT =        5115
702514


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   18079
33622127  
00016717  00000-0  10270-3 0  9176
2 25544  51
6398 101
6602 0002377 229
8078 130
2867 15
54087804 24695


Satellite: ISS
Catalog Number: 25544
Epoch time:      18079
33622127   =   yrday
fracday
Element set:     917
Inclination:       51
6398  deg
RA of node:       101
6602  deg
Eccentricity:     
0002377     
Arg of perigee:   229
8078  deg
Mean anomaly:     130
2867  deg
Mean motion:   15
54087804  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2469
Checksum:              325
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