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

 
Date: February 1st 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 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


037/00:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 7

040/08:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 5

042/12:24:39 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 6

043/19:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 6

Coasting Arc #1 (Orbit 1726)
---------------------------------------

Vector Time (GMT): 2018/031/14:37:35
785
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -539493
40                 A    =         6777934
88  meter
 Y    =       -4268978
22  meter          E    =           
0016819
 Z    =       -5251448
91                 I    =           51
49171
 XDOT =       7323
165394                 Wp   =           89
21638
 YDOT =      -2039
562629  meter/sec      RA   =          338
98102  deg
 ZDOT =        908
413248                 TA   =          189
48919
                                          MA   =          189
52100
                                          Ha   =            222
163  n
mi
                                          Hp   =            213
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1769991
45                 X    =         -466208
40
 Y    =      -14005834
06  feet           Y    =        -4274601
39  meter
 Z    =      -17229163
09                 Z    =        -5253891
56
 XDOT =      24026
133182                 XDOT =        7341
015603
 YDOT =      -6691
478441  feet/sec       YDOT =       -1957
570176  meter/sec
 ZDOT =       2980
358426                 ZDOT =         944
028948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         974093
36                 X    =          296903
66
 Y    =      -14071166
54  feet           Y    =        -4288891
56  meter
 Z    =      -17239307
77                 Z    =        -5254541
01
 XDOT =      23804
960715                 XDOT =        7255
752026
 YDOT =      -2187
091870  feet/sec       YDOT =        -666
625602  meter/sec
 ZDOT =       3139
255010                 ZDOT =         956
844927


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   18031
62390151  
00016717  00000-0  10270-3 0  9007
2 25544  51
6427 339
5082 0003196  52
5921 307
5522 15
54034170 17271


Satellite: ISS
Catalog Number: 25544
Epoch time:      18031
62390151   =   yrday
fracday
Element set:     900
Inclination:       51
6427  deg
RA of node:       339
5082  deg
Eccentricity:     
0003196     
Arg of perigee:    52
5921  deg
Mean anomaly:     307
5522  deg
Mean motion:   15
54034170  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1727
Checksum:              282


Coasting Arc #2 (Orbit 1742)
---------------------------------------

Vector Time (GMT): 2018/032/14:37:35
785
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1120345
15                 A    =         6780109
82  meter
 Y    =        4730351
10  meter          E    =           
0010974
 Z    =        4720523
31                 I    =           51
46832
 XDOT =      -7094
618604                 Wp   =           60
15445
 YDOT =       1049
183574  meter/sec      RA   =          333
97495  deg
 ZDOT =      -2725
050823                 TA   =           56
90245
                                          MA   =           56
79715
                                          Ha   =            222
161  n
mi
                                          Hp   =            213
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3675673
06                 X    =        -1196087
09
 Y    =       15519524
60  feet           Y    =         4717399
22  meter
 Z    =       15487281
20                 Z    =         4714897
17
 XDOT =     -23276
307757                 XDOT =       -7092
587105
 YDOT =       3442
203328  feet/sec       YDOT =         969
857989  meter/sec
 ZDOT =      -8940
455457                 ZDOT =       -2759
508098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6343483
53                 X    =        -1933493
78
 Y    =       14660362
61  feet           Y    =         4468478
52  meter
 Z    =       15461438
49                 Z    =         4712646
45
 XDOT =     -22395
562902                 XDOT =       -6826
167573
 YDOT =        -64
472316  feet/sec       YDOT =         -19
651162  meter/sec
 ZDOT =      -9094
017221                 ZDOT =       -2771
856449


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   18032
65280135  
00016717  00000-0  10270-3 0  9012
2 25544  51
6422 334
3810 0003141  54
7139 305
4307 15
54055380 17435


Satellite: ISS
Catalog Number: 25544
Epoch time:      18032
65280135   =   yrday
fracday
Element set:     901
Inclination:       51
6422  deg
RA of node:       334
3810  deg
Eccentricity:     
0003141     
Arg of perigee:    54
7139  deg
Mean anomaly:     305
4307  deg
Mean motion:   15
54055380  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1743
Checksum:              271


Coasting Arc #3 (Orbit 1757)
---------------------------------------

Vector Time (GMT): 2018/033/14:37:35
785
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2584026
27                 A    =         6783689
69  meter
 Y    =       -5036483
34  meter          E    =           
0008263
 Z    =       -3745006
90                 I    =           51
45201
 XDOT =       6373
901878                 Wp   =           86
24797
 YDOT =        117
132496  meter/sec      RA   =          328
97380  deg
 ZDOT =       4249
065667                 TA   =          228
88219
                                          MA   =          228
95355
                                          Ha   =            222
157  n
mi
                                          Hp   =            213
868

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8477776
48                 X    =         2658344
32
 Y    =      -16523895
46  feet           Y    =        -5007171
62  meter
 Z    =      -12286768
04                 Z    =        -3732274
20
 XDOT =      20911
751567                 XDOT =        6351
479189
 YDOT =        384
292967  feet/sec       YDOT =         188
284662  meter/sec
 ZDOT =      13940
504158                 ZDOT =        4279
972571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10968290
62                 X    =         3343134
98
 Y    =      -15033910
24  feet           Y    =        -4582335
84  meter
 Z    =      -12229252
95                 Z    =        -3727476
30
 XDOT =      19423
214205                 XDOT =        5920
195690
 YDOT =       2742
063592  feet/sec       YDOT =         835
780983  meter/sec
 ZDOT =      14078
057185                 ZDOT =        4290
991830


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   18033
61739178  
00016717  00000-0  10270-3 0  9026
2 25544  51
6431 329
5733 0003063  57
5245 302
6203 15
54043343 17583


Satellite: ISS
Catalog Number: 25544
Epoch time:      18033
61739178   =   yrday
fracday
Element set:     902
Inclination:       51
6431  deg
RA of node:       329
5733  deg
Eccentricity:     
0003063     
Arg of perigee:    57
5245  deg
Mean anomaly:     302
6203  deg
Mean motion:   15
54043343  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1758
Checksum:              293


Coasting Arc #4 (Orbit 1773)
---------------------------------------

Vector Time (GMT): 2018/034/14:37:35
785
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3810323
88                 A    =         6787336
27  meter
 Y    =        5091071
86  meter          E    =           
0016273
 Z    =        2354478
07                 I    =           51
43592
 XDOT =      -5280
223985                 Wp   =           98
94825
 YDOT =      -1454
685416  meter/sec      RA   =          323
98140  deg
 ZDOT =      -5370
384076                 TA   =           54
68817
                                          MA   =           54
53611
                                          Ha   =            222
276  n
mi
                                          Hp   =            213
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12501062
60                 X    =        -3878406
98
 Y    =       16702991
67  feet           Y    =         5048081
67  meter
 Z    =        7724665
57                 Z    =         2335803
59
 XDOT =     -17323
569505                 XDOT =       -5237
478976
 YDOT =      -4772
589946  feet/sec       YDOT =       -1513
493836  meter/sec
 ZDOT =     -17619
370328                 ZDOT =       -5395
929067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14688827
84                 X    =        -4477154
73
 Y    =       14859167
58  feet           Y    =         4529074
28  meter
 Z    =        7640708
76                 Z    =         2328888
03
 XDOT =     -15322
866462                 XDOT =       -4670
409698
 YDOT =      -5978
855267  feet/sec       YDOT =       -1822
355085  meter/sec
 ZDOT =     -17732
828990                 ZDOT =       -5404
966276


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   18034
64628473  
00016717  00000-0  10270-3 0  9036
2 25544  51
6427 324
4456 0003188  63
5564 296
5915 15
54024262 17741


Satellite: ISS
Catalog Number: 25544
Epoch time:      18034
64628473   =   yrday
fracday
Element set:     903
Inclination:       51
6427  deg
RA of node:       324
4456  deg
Eccentricity:     
0003188     
Arg of perigee:    63
5564  deg
Mean anomaly:     296
5915  deg
Mean motion:   15
54024262  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1774
Checksum:              321


Coasting Arc #5 (Orbit 1788)
---------------------------------------

Vector Time (GMT): 2018/035/14:37:35
785
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4663442
57                 A    =         6789292
24  meter
 Y    =       -4866600
62  meter          E    =           
0013301
 Z    =        -767970
14                 I    =           51
41641
 XDOT =       3937
248708                 Wp   =           45
05729
 YDOT =       2848
183965  meter/sec      RA   =          318
99425  deg
 ZDOT =       5932
071558                 TA   =          306
61591
                                          MA   =          306
73818
                                          Ha   =            222
171  n
mi
                                          Hp   =            213
739

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15300008
43                 X    =         4721245
94
 Y    =      -15966537
46  feet           Y    =        -4814127
65  meter
 Z    =       -2519587
07                 Z    =         -745176
47
 XDOT =      12917
482637                 XDOT =        3876
292600
 YDOT =       9344
435580  feet/sec       YDOT =        2891
872551  meter/sec
 ZDOT =      19462
177028                 ZDOT =        5951
048738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17089634
76                 X    =         5208920
67
 Y    =      -14052391
49  feet           Y    =        -4283168
93  meter
 Z    =       -2417348
26                 Z    =         -736807
75
 XDOT =      10574
832502                 XDOT =        3223
208946
 YDOT =       9540
543663  feet/sec       YDOT =        2907
957709  meter/sec
 ZDOT =      19546
173048                 ZDOT =        5957
673545


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   18035
61086700  
00016717  00000-0  10270-3 0  9046
2 25544  51
6421 319
6379 0003064  64
2534 295
8935 15
54061142 17891


Satellite: ISS
Catalog Number: 25544
Epoch time:      18035
61086700   =   yrday
fracday
Element set:     904
Inclination:       51
6421  deg
RA of node:       319
6379  deg
Eccentricity:     
0003064     
Arg of perigee:    64
2534  deg
Mean anomaly:     295
8935  deg
Mean motion:   15
54061142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1789
Checksum:              311


Coasting Arc #6 (Orbit 1804)
---------------------------------------

Vector Time (GMT): 2018/036/14:37:35
785
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5181013
09                 A    =         6789248
64  meter
 Y    =        4279816
71  meter          E    =           
0011096
 Z    =        -942821
03                 I    =           51
39189
 XDOT =      -2444
495912                 Wp   =          126
45066
 YDOT =      -4246
016480  meter/sec      RA   =          314
00889  deg
 ZDOT =      -5896
103749                 TA   =           63
79093
                                          MA   =           63
67689
                                          Ha   =            222
179  n
mi
                                          Hp   =            213
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16998074
46                 X    =        -5223906
45
 Y    =       14041393
40  feet           Y    =         4221639
18  meter
 Z    =       -3093244
85                 Z    =         -968092
63
 XDOT =      -8019
999711                 XDOT =       -2368
194422
 YDOT =     -13930
500264  feet/sec       YDOT =       -4272
926241  meter/sec
 ZDOT =     -19344
172404                 ZDOT =       -5907
792494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18304183
59                 X    =        -5579115
16
 Y    =       12261291
51  feet           Y    =         3737241
65  meter
 Z    =       -3206403
16                 Z    =         -977311
68
 XDOT =      -5556
001194                 XDOT =       -1693
469164
 YDOT =     -13320
839767  feet/sec       YDOT =       -4060
191961  meter/sec
 ZDOT =     -19395
506426                 ZDOT =       -5911
750359


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   18036
63975336  
00016717  00000-0  10270-3 0  9052
2 25544  51
6422 314
5100 0002926  70
0525 290
0943 15
54015645 18051


Satellite: ISS
Catalog Number: 25544
Epoch time:      18036
63975336   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       314
5100  deg
Eccentricity:     
0002926     
Arg of perigee:    70
0525  deg
Mean anomaly:     290
0943  deg
Mean motion:   15
54015645  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1805
Checksum:              287


Coasting Arc #7 (Orbit 1810)
---------------------------------------

Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4188555
95                 A    =         6778332
87  meter
 Y    =       -1484768
88  meter          E    =           
0016521
 Z    =       -5133130
61                 I    =           51
34612
 XDOT =       4071
045879                 Wp   =           78
16740
 YDOT =      -6308
237428  meter/sec      RA   =          312
01937  deg
 ZDOT =      -1498
021750                 TA   =          177
32632
                                          MA   =          177
31748
                                          Ha   =            222
133  n
mi
                                          Hp   =            213
655

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13741981
46                 X    =        -4146707
89
 Y    =       -4871288
96  feet           Y    =        -1531374
49  meter
 Z    =      -16840979
70                 Z    =        -5153375
13
 XDOT =      13356
449734                 XDOT =        4148
560220
 YDOT =     -20696
317021  feet/sec       YDOT =       -6262
278875  meter/sec
 ZDOT =      -4914
769522                 ZDOT =       -1478
057697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6806019
32                 X    =         2074474
69
 Y    =       12775564
21  feet           Y    =         3893991
97  meter
 Z    =      -16930834
83                 Z    =        -5160518
46
 XDOT =     -22898
290075                 XDOT =       -6979
398815
 YDOT =       5807
934540  feet/sec       YDOT =        1770
258448  meter/sec
 ZDOT =      -4824
909973                 ZDOT =       -1470
632560


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   18037
02558326  
00016717  00000-0  10270-3 0  9063
2 25544  51
6418 312
5830 0002773  76
9702 283
1760 15
54039890 18111


Satellite: ISS
Catalog Number: 25544
Epoch time:      18037
02558326   =   yrday
fracday
Element set:     906
Inclination:       51
6418  deg
RA of node:       312
5830  deg
Eccentricity:     
0002773     
Arg of perigee:    76
9702  deg
Mean anomaly:     283
1760  deg
Mean motion:   15
54039890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1811
Checksum:              308


Coasting Arc #8 (Orbit 1826)
---------------------------------------

Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3099896
91                 A    =         6777498
46  meter
 Y    =        2904637
26  meter          E    =           
0005506
 Z    =        5276404
82                 I    =           51
32291
 XDOT =      -4863
337270                 Wp   =           74
63196
 YDOT =       5921
234056  meter/sec      RA   =          306
99895  deg
 ZDOT =       -400
609809                 TA   =           19
21315
                                          MA   =           19
19239
                                          Ha   =            221
967  n
mi
                                          Hp   =            213
691

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10170265
44                 X    =         3041556
43
 Y    =        9529649
80  feet           Y    =         2938976
46  meter
 Z    =       17311039
44                 Z    =         5291321
02
 XDOT =     -15955
830938                 XDOT =       -4927
242734
 YDOT =      19426
620920  feet/sec       YDOT =        5866
491547  meter/sec
 ZDOT =      -1314
336644                 ZDOT =        -424
389368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1264692
38                 X    =         -385478
24
 Y    =      -13797194
59  feet           Y    =        -4205384
91  meter
 Z    =       17376955
60                 Z    =         5296496
07
 XDOT =      23795
520037                 XDOT =        7252
874507
 YDOT =      -3978
326807  feet/sec       YDOT =       -1212
594011  meter/sec
 ZDOT =      -1421
101135                 ZDOT =        -433
151626


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   18038
05446199  
00016717  00000-0  10270-3 0  9072
2 25544  51
6420 307
4544 0002847  78
7035 281
4437 15
54096346 18278


Satellite: ISS
Catalog Number: 25544
Epoch time:      18038
05446199   =   yrday
fracday
Element set:     907
Inclination:       51
6420  deg
RA of node:       307
4544  deg
Eccentricity:     
0002847     
Arg of perigee:    78
7035  deg
Mean anomaly:     281
4437  deg
Mean motion:   15
54096346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1827
Checksum:              324


Coasting Arc #9 (Orbit 1841)
---------------------------------------

Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1978933
22                 A    =         6779237
31  meter
 Y    =       -4252885
24  meter          E    =           
0014934
 Z    =       -4908144
51                 I    =           51
30824
 XDOT =       5287
090502                 Wp   =          101
58398
 YDOT =      -5058
575013  meter/sec      RA   =          301
97961  deg
 ZDOT =       2254
414359                 TA   =          190
56264
                                          MA   =          190
59404
                                          Ha   =            222
163  n
mi
                                          Hp   =            213
570

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6492563
05                 X    =        -1907388
37
 Y    =      -13953035
56  feet           Y    =        -4274615
15  meter
 Z    =      -16102836
30                 Z    =        -4917583
45
 XDOT =      17346
097446                 XDOT =        5332
313300
 YDOT =     -16596
374716  feet/sec       YDOT =       -4999
198214  meter/sec
 ZDOT =       7396
372569                 ZDOT =        2280
206862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4158042
47                 X    =        -1267371
34
 Y    =       14772217
32  feet           Y    =         4502571
84  meter
 Z    =      -16144168
97                 Z    =        -4920742
70
 XDOT =     -22848
903311                 XDOT =       -6964
345729
 YDOT =       1767
780158  feet/sec       YDOT =         538
819392  meter/sec
 ZDOT =       7511
947171                 ZDOT =        2289
641498


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   18039
01903639  
00016717  00000-0  10270-3 0  9087
2 25544  51
6407 302
6475 0003004  82
1056 278
0438 15
54078523 18428


Satellite: ISS
Catalog Number: 25544
Epoch time:      18039
01903639   =   yrday
fracday
Element set:     908
Inclination:       51
6407  deg
RA of node:       302
6475  deg
Eccentricity:     
0003004     
Arg of perigee:    82
1056  deg
Mean anomaly:     278
0438  deg
Mean motion:   15
54078523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1842
Checksum:              299


Coasting Arc #10 (Orbit 1857)
---------------------------------------

Vector Time (GMT): 2018/040/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         861085
89                 A    =         6782573
92  meter
 Y    =        5393749
03  meter          E    =           
0013682
 Z    =        4011299
70                 I    =           51
30365
 XDOT =      -5424
133959                 Wp   =           79
38006
 YDOT =       3775
240425  meter/sec      RA   =          296
96488  deg
 ZDOT =      -3898
134451                 TA   =           51
29535
                                          MA   =           51
17308
                                          Ha   =            222
067  n
mi
                                          Hp   =            213
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2825084
96                 X    =          781223
04
 Y    =       17696027
01  feet           Y    =         5402931
83  meter
 Z    =       13160432
09                 Z    =         4015288
41
 XDOT =     -17795
715089                 XDOT =       -5447
011779
 YDOT =      12385
959400  feet/sec       YDOT =        3714
456037  meter/sec
 ZDOT =     -12789
155022                 ZDOT =       -3924
538278

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9097149
11                 X    =         2772811
05
 Y    =      -15424883
64  feet           Y    =        -4701504
53  meter
 Z    =       13177340
12                 Z    =         4016453
27
 XDOT =      20424
285221                 XDOT =        6225
322135
 YDOT =        980
403501  feet/sec       YDOT =         298
826987  meter/sec
 ZDOT =     -12907
240595                 ZDOT =       -3934
126933


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   18040
04791095  
00016717  00000-0  10270-3 0  9094
2 25544  51
6414 297
5188 0002874  83
8829 276
2651 15
54096562 18586


Satellite: ISS
Catalog Number: 25544
Epoch time:      18040
04791095   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       297
5188  deg
Eccentricity:     
0002874     
Arg of perigee:    83
8829  deg
Mean anomaly:     276
2651  deg
Mean motion:   15
54096562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1858
Checksum:              344


Coasting Arc #11 (Orbit 1862)
---------------------------------------

Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4458340
94                 A    =         6778310
04  meter
 Y    =        -167613
20  meter          E    =           
0016737
 Z    =       -5118030
88                 I    =           51
28253
 XDOT =       2040
689437                 Wp   =           78
48267
 YDOT =      -7215
666274  meter/sec      RA   =          295
28234  deg
 ZDOT =      -1542
366377                 TA   =          176
55908
                                          MA   =          176
54756
                                          Ha   =            222
207  n
mi
                                          Hp   =            213
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14627102
83                 X    =        -4431274
97
 Y    =        -549912
07  feet           Y    =         -217318
19  meter
 Z    =      -16791439
89                 Z    =        -5139621
89
 XDOT =       6695
175317                 XDOT =        2128
717191
 YDOT =     -23673
445780  feet/sec       YDOT =       -7192
353720  meter/sec
 ZDOT =      -5060
257142                 ZDOT =       -1532
239627

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1874087
67                 X    =          571221
92
 Y    =      -14405115
41  feet           Y    =        -4390679
18  meter
 Z    =      -16887493
59                 Z    =        -5147308
05
 XDOT =      21910
364758                 XDOT =        6678
279178
 YDOT =       8724
730371  feet/sec       YDOT =        2659
297817  meter/sec
 ZDOT =      -5014
071643                 ZDOT =       -1528
289037


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   18040
36943557  
00016717  00000-0  10270-3 0  9103
2 25544  51
6398 295
9170 0003080  80
0608 280
0892 15
54067631 18635


Satellite: ISS
Catalog Number: 25544
Epoch time:      18040
36943557   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       295
9170  deg
Eccentricity:     
0003080     
Arg of perigee:    80
0608  deg
Mean anomaly:     280
0892  deg
Mean motion:   15
54067631  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1863
Checksum:              312


Coasting Arc #12 (Orbit 1878)
---------------------------------------

Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3828101
48                 A    =         6777520
35  meter
 Y    =        1846551
27  meter          E    =           
0005685
 Z    =        5274515
98                 I    =           51
26698
 XDOT =      -2921
900662                 Wp   =           77
27412
 YDOT =       7085
929207  meter/sec      RA   =          290
25882  deg
 ZDOT =       -358
511667                 TA   =           16
16879
                                          MA   =           16
15066
                                          Ha   =            222
052  n
mi
                                          Hp   =            213
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12559388
07                 X    =         3781547
96
 Y    =        6058239
08  feet           Y    =         1889099
51  meter
 Z    =       17304842
46                 Z    =         5292998
16
 XDOT =      -9586
288262                 XDOT =       -2999
178848
 YDOT =      23247
799235  feet/sec       YDOT =        7052
822415  meter/sec
 ZDOT =      -1176
219380                 ZDOT =        -372
892798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6965675
63                 X    =        -2123137
93
 Y    =       11961455
43  feet           Y    =         3645851
61  meter
 Z    =       17386805
60                 Z    =         5299498
35
 XDOT =     -21601
307874                 XDOT =       -6584
078640
 YDOT =     -10767
659357  feet/sec       YDOT =       -3281
982572  meter/sec
 ZDOT =      -1241
303683                 ZDOT =        -378
349363


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   18041
39830619  
00016717  00000-0  10270-3 0  9112
2 25544  51
6398 290
7894 0003088  81
2699 278
8803 15
54083926 18791


Satellite: ISS
Catalog Number: 25544
Epoch time:      18041
39830619   =   yrday
fracday
Element set:     911
Inclination:       51
6398  deg
RA of node:       290
7894  deg
Eccentricity:     
0003088     
Arg of perigee:    81
2699  deg
Mean anomaly:     278
8803  deg
Mean motion:   15
54083926  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1879
Checksum:              357


Coasting Arc #13 (Orbit 1893)
---------------------------------------

Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3143485
41                 A    =         6779183
63  meter
 Y    =       -3469401
53  meter          E    =           
0015208
 Z    =       -4917005
80                 I    =           51
26154
 XDOT =       3585
780059                 Wp   =          102
06131
 YDOT =      -6390
483996  meter/sec      RA   =          285
23479  deg
 ZDOT =       2219
379364                 TA   =          189
73963
                                          MA   =          189
76914
                                          Ha   =            222
214  n
mi
                                          Hp   =            213
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10313272
34                 X    =        -3080572
24
 Y    =      -11382550
94  feet           Y    =        -3504202
44  meter
 Z    =      -16131908
78                 Z    =        -4932122
60
 XDOT =      11764
370271                 XDOT =        3646
193316
 YDOT =     -20966
154844  feet/sec       YDOT =       -6350
047520  meter/sec
 ZDOT =       7281
428358                 ZDOT =        2236
944321

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11946921
76                 X    =         3641421
75
 Y    =       -9541443
04  feet           Y    =        -2908231
84  meter
 Z    =      -16198656
07                 Z    =        -4937350
37
 XDOT =      19568
170319                 XDOT =        5964
378313
 YDOT =      12020
441311  feet/sec       YDOT =        3663
830512  meter/sec
 ZDOT =       7360
561902                 ZDOT =        2243
499268


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   18042
36287167  
00016717  00000-0  10270-3 0  9125
2 25544  51
6394 285
9815 0003113  85
5851 274
5658 15
54073477 18940


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
36287167   =   yrday
fracday
Element set:     912
Inclination:       51
6394  deg
RA of node:       285
9815  deg
Eccentricity:     
0003113     
Arg of perigee:    85
5851  deg
Mean anomaly:     274
5658  deg
Mean motion:   15
54073477  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1894
Checksum:              339


Coasting Arc #14 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2018/042/12:24:39
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1074524
00                 A    =         6785250
23  meter
 Y    =        5914370
84  meter          E    =           
0015980
 Z    =        3132547
57                 I    =           51
28246
 XDOT =      -4873
391875                 Wp   =           92
52339
 YDOT =       3448
591114  meter/sec      RA   =          284
39590  deg
 ZDOT =      -4818
764360                 TA   =           51
15635
                                          MA   =           51
01384
                                          Ha   =            222
153  n
mi
                                          Hp   =            213
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3525341
20                 X    =          993092
08
 Y    =       19404103
79  feet           Y    =         5925931
63  meter
 Z    =       10277387
03                 Z    =         3137569
26
 XDOT =     -15988
818488                 XDOT =       -4888
186209
 YDOT =      11314
275308  feet/sec       YDOT =        3394
010709  meter/sec
 ZDOT =     -15809
594356                 ZDOT =       -4842
473116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7729113
52                 X    =        -2355833
80
 Y    =       18131922
58  feet           Y    =         5526610
00  meter
 Z    =       10298841
99                 Z    =         3139087
04
 XDOT =     -18163
566763                 XDOT =       -5536
255149
 YDOT =       1335
778188  feet/sec       YDOT =         407
145192  meter/sec
 ZDOT =     -15915
622792                 ZDOT =       -4851
081827


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   18042
55578354  
00016717  00000-0  10270-3 0  9138
2 25544  51
6413 285
0215 0003095  84
5062 275
6443 15
54094387 18979


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
55578354   =   yrday
fracday
Element set:     913
Inclination:       51
6413  deg
RA of node:       285
0215  deg
Eccentricity:     
0003095     
Arg of perigee:    84
5062  deg
Mean anomaly:     275
6443  deg
Mean motion:   15
54094387  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1897
Checksum:              321


Coasting Arc #15 (Orbit 1911)
---------------------------------------

Vector Time (GMT): 2018/043/12:24:39
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -249776
49                 A    =         6788308
10  meter
 Y    =       -6578191
70  meter          E    =           
0009975
 Z    =       -1647061
75                 I    =           51
28540
 XDOT =       4884
898655                 Wp   =           50
67463
 YDOT =      -1601
856306  meter/sec      RA   =          279
39487  deg
 ZDOT =       5686
211786                 TA   =          291
20157
                                          MA   =          291
30811
                                          Ha   =            222
128  n
mi
                                          Hp   =            213
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -819476
69                 X    =         -168198
43
 Y    =      -21581993
78  feet           Y    =        -6580528
78  meter
 Z    =       -5403745
88                 Z    =        -1648076
77
 XDOT =      16026
570392                 XDOT =        4874
827998
 YDOT =      -5255
434076  feet/sec       YDOT =       -1547
286204  meter/sec
 ZDOT =      18655
550480                 ZDOT =        5709
915969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10838877
06                 X    =         3303689
73
 Y    =      -18679787
45  feet           Y    =        -5693599
21  meter
 Z    =       -5407286
93                 Z    =        -1648141
06
 XDOT =      14894
395000                 XDOT =        4539
811596
 YDOT =       3239
405426  feet/sec       YDOT =         987
370774  meter/sec
 ZDOT =      18761
279379                 ZDOT =        5718
437955


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   18043
52034547  
00016717  00000-0  10270-3 0  9148
2 25544  51
6413 280
2135 0002916  87
4675 272
6811 15
54081742 19125


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
52034547   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:       280
2135  deg
Eccentricity:     
0002916     
Arg of perigee:    87
4675  deg
Mean anomaly:     272
6811  deg
Mean motion:   15
54081742  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1912
Checksum:              297


Coasting Arc #16 (Orbit 1916)
---------------------------------------

Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3616303
32                 A    =         6778989
77  meter
 Y    =        2867972
64  meter          E    =           
0008721
 Z    =        4958779
15                 I    =           51
25152
 XDOT =      -2639
490203                 Wp   =           71
18496
 YDOT =       6903
614758  meter/sec      RA   =          277
98455  deg
 ZDOT =      -2062
134511                 TA   =           39
00294
                                          MA   =           38
94007
                                          Ha   =            222
149  n
mi
                                          Hp   =            213
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11864512
22                 X    =         3559877
53
 Y    =        9409359
05  feet           Y    =         2908097
25  meter
 Z    =       16268960
47                 Z    =         4976208
38
 XDOT =      -8659
744761                 XDOT =       -2706
475590
 YDOT =      22649
654718  feet/sec       YDOT =        6873
723579  meter/sec
 ZDOT =      -6765
533171                 ZDOT =       -2075
118800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13010951
02                 X    =         3965737
87
 Y    =       -7582995
06  feet           Y    =        -2311296
90  meter
 Z    =       16346103
57                 Z    =         4982292
37
 XDOT =      17478
899113                 XDOT =        5327
568450
 YDOT =      15239
213628  feet/sec       YDOT =        4644
912314  meter/sec
 ZDOT =      -6824
337300                 ZDOT =       -2080
058009


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   18043
84186768  
00016717  00000-0  10270-3 0  9157
2 25544  51
6403 278
6054 0003198  99
8326 260
3188 15
54056196 19179


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
84186768   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:       278
6054  deg
Eccentricity:     
0003198     
Arg of perigee:    99
8326  deg
Mean anomaly:     260
3188  deg
Mean motion:   15
54056196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1917
Checksum:              340


Coasting Arc #17 (Orbit 1931)
---------------------------------------

Vector Time (GMT): 2018/044/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3100275
65                 A    =         6782136
81  meter
 Y    =       -4395349
55  meter          E    =           
0010773
 Z    =       -4142350
84                 I    =           51
25847
 XDOT =       3292
971639                 Wp   =          107
43847
 YDOT =      -5826
713058  meter/sec      RA   =          272
96639  deg
 ZDOT =       3722
885450                 TA   =          201
09171
                                          MA   =          201
13617
                                          Ha   =            222
175  n
mi
                                          Hp   =            213
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10171508
05                 X    =        -3030774
40
 Y    =      -14420438
14  feet           Y    =        -4429630
50  meter
 Z    =      -13590389
89                 Z    =        -4157241
56
 XDOT =      10803
712728                 XDOT =        3339
799421
 YDOT =     -19116
512657  feet/sec       YDOT =       -5789
626821  meter/sec
 ZDOT =      12214
191110                 ZDOT =        3738
995112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17008233
92                 X    =        -5184109
70
 Y    =        4510018
80  feet           Y    =         1374653
73  meter
 Z    =      -13656025
00                 Z    =        -4162356
42
 XDOT =     -13935
911000                 XDOT =       -4247
665673
 YDOT =     -15400
046836  feet/sec       YDOT =       -4693
934276  meter/sec
 ZDOT =      12286
731715                 ZDOT =        3744
995827


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   18044
80642533  
00016717  00000-0  10270-3 0  9162
2 25544  51
6400 273
7984 0003085 102
4731 257
6767 15
54080375 19325


Satellite: ISS
Catalog Number: 25544
Epoch time:      18044
80642533   =   yrday
fracday
Element set:     916
Inclination:       51
6400  deg
RA of node:       273
7984  deg
Eccentricity:     
0003085     
Arg of perigee:   102
4731  deg
Mean anomaly:     257
6767  deg
Mean motion:   15
54080375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1932
Checksum:              311


Coasting Arc #18 (Orbit 1947)
---------------------------------------

Vector Time (GMT): 2018/045/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920849
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2500197
04                 A    =         6785975
50  meter
 Y    =        5610731
00  meter          E    =           
0016455
 Z    =        2866011
53                 I    =           51
26975
 XDOT =      -3880
029299                 Wp   =          100
55611
 YDOT =       4307
490310  meter/sec      RA   =          267
95706  deg
 ZDOT =      -5026
217863                 TA   =           46
62334
                                          MA   =           46
48640
                                          Ha   =            222
169  n
mi
                                          Hp   =            213
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8202746
21                 X    =         2423349
30
 Y    =       18407910
09  feet           Y    =         5638260
39  meter
 Z    =        9402924
96                 Z    =         2877969
36
 XDOT =     -12729
754918                 XDOT =       -3903
494368
 YDOT =      14132
186056  feet/sec       YDOT =        4263
969691  meter/sec
 ZDOT =     -16490
216087                 ZDOT =       -5045
122430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20059548
06                 X    =         6114150
25
 Y    =       -1661954
30  feet           Y    =         -506563
67  meter
 Z    =        9455349
63                 Z    =         2881990
57
 XDOT =       9096
417428                 XDOT =        2772
588032
 YDOT =      15090
142429  feet/sec       YDOT =        4599
475412  meter/sec
 ZDOT =     -16574
965983                 ZDOT =       -5052
049631


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   18045
83528664  
00016717  00000-0  10270-3 0  9175
2 25544  51
6393 268
6698 0003183 108
0226 252
1274 15
54071020 19488


Satellite: ISS
Catalog Number: 25544
Epoch time:      18045
83528664   =   yrday
fracday
Element set:     917
Inclination:       51
6393  deg
RA of node:       268
6698  deg
Eccentricity:     
0003183     
Arg of perigee:   108
0226  deg
Mean anomaly:     252
1274  deg
Mean motion:   15
54071020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1948
Checksum:              317
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