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

 
Date: September 18th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13923 1181 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


268/13:57:43 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 3

268/17:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

271/11:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

272/00:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 4

Coasting Arc #1 (Orbit 2941)
---------------------------------------

Vector Time (GMT): 2019/259/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3951644
92                 A    =         6791341
20  meter
 Y    =        2783081
27  meter          E    =           
0014757
 Z    =        4763438
80                 I    =           51
24177
 XDOT =      -1776
528038                 Wp   =           57
16530
 YDOT =       6991
478586  meter/sec      RA   =          267
45542  deg
 ZDOT =      -2597
309082                 TA   =           58
65578
                                          MA   =           58
51144
                                          Ha   =            229
710  n
mi
                                          Hp   =            218
674

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12964714
32                 X    =         3897091
77
 Y    =        9130844
06  feet           Y    =         2826966
82  meter
 Z    =       15628080
07                 Z    =         4782501
70
 XDOT =      -5828
504062                 XDOT =       -1841
960396
 YDOT =      22937
921871  feet/sec       YDOT =        6971
246069  meter/sec
 ZDOT =      -8521
355255                 ZDOT =       -2606
098483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11880792
81                 X    =        -3621265
65
 Y    =      -10372677
50  feet           Y    =        -3161592
10  meter
 Z    =       15714558
25                 Z    =         4789797
35
 XDOT =       7280
791532                 XDOT =        2219
185259
 YDOT =     -21378
466391  feet/sec       YDOT =       -6516
156556  meter/sec
 ZDOT =      -8561
811537                 ZDOT =       -2609
640157


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   19259
54378625  
00016717  00000-0  10270-3 0  9003
2 25544  51
6402 268
1623 0007360  53
0142 307
1681 15
50108694 29421


Satellite: ISS
Catalog Number: 25544
Epoch time:      19259
54378625   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:       268
1623  deg
Eccentricity:     
0007360     
Arg of perigee:    53
0142  deg
Mean anomaly:     307
1681  deg
Mean motion:   15
50108694  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2942
Checksum:              298


Coasting Arc #2 (Orbit 2956)
---------------------------------------

Vector Time (GMT): 2019/260/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4109311
84                 A    =         6792124
14  meter
 Y    =       -2848666
57  meter          E    =           
0015791
 Z    =       -4610361
71                 I    =           51
24596
 XDOT =       1479
920744                 Wp   =           87
81628
 YDOT =      -6900
222415  meter/sec      RA   =          262
47291  deg
 ZDOT =       2953
856747                 TA   =          211
81284
                                          MA   =          211
90832
                                          Ha   =            229
886  n
mi
                                          Hp   =            218
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13481994
21                 X    =        -4054757
05
 Y    =       -9346018
92  feet           Y    =        -2894315
20  meter
 Z    =      -15125858
63                 Z    =        -4630190
59
 XDOT =       4855
383019                 XDOT =        1542
622722
 YDOT =     -22638
524983  feet/sec       YDOT =       -6883
322024  meter/sec
 ZDOT =       9691
131059                 ZDOT =        2961
198661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12558474
79                 X    =         3827823
12
 Y    =       10424361
82  feet           Y    =         3177345
48  meter
 Z    =      -15215821
65                 Z    =        -4637782
44
 XDOT =      -5890
753225                 XDOT =       -1795
501583
 YDOT =      21246
929701  feet/sec       YDOT =        6476
064173  meter/sec
 ZDOT =       9724
985701                 ZDOT =        2964
175642


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   19260
51083497  
00016717  00000-0  10270-3 0  9013
2 25544  51
6396 263
3717 0007352  56
0021 304
1827 15
50062270 29578


Satellite: ISS
Catalog Number: 25544
Epoch time:      19260
51083497   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:       263
3717  deg
Eccentricity:     
0007352     
Arg of perigee:    56
0021  deg
Mean anomaly:     304
1827  deg
Mean motion:   15
50062270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2957
Checksum:              295


Coasting Arc #3 (Orbit 2972)
---------------------------------------

Vector Time (GMT): 2019/261/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4261297
05                 A    =         6792787
84  meter
 Y    =        2935647
18  meter          E    =           
0016509
 Z    =        4391559
37                 I    =           51
25322
 XDOT =      -1230
669092                 Wp   =           65
32505
 YDOT =       6794
786892  meter/sec      RA   =          257
48937  deg
 ZDOT =      -3331
295622                 TA   =           58
61207
                                          MA   =           58
45069
                                          Ha   =            229
751  n
mi
                                          Hp   =            218
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13980633
37                 X    =         4206821
10
 Y    =        9631388
38  feet           Y    =         2982995
77  meter
 Z    =       14408003
19                 Z    =         4412126
83
 XDOT =      -4037
628253                 XDOT =       -1290
377138
 YDOT =      22292
607915  feet/sec       YDOT =        6780
690563  meter/sec
 ZDOT =     -10929
447578                 ZDOT =       -3337
419390

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13219535
15                 X    =        -4029314
31
 Y    =      -10524624
99  feet           Y    =        -3207905
70  meter
 Z    =       14501326
38                 Z    =         4420004
28
 XDOT =       4654
176789                 XDOT =        1418
593085
 YDOT =     -21018
946867  feet/sec       YDOT =       -6406
575005  meter/sec
 ZDOT =     -10957
744603                 ZDOT =       -3339
920555


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   19261
54235133  
00016717  00000-0  10270-3 0  9024
2 25544  51
6387 258
2599 0007275  59
2253 300
9613 15
50107562 29734


Satellite: ISS
Catalog Number: 25544
Epoch time:      19261
54235133   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:       258
2599  deg
Eccentricity:     
0007275     
Arg of perigee:    59
2253  deg
Mean anomaly:     300
9613  deg
Mean motion:   15
50107562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2973
Checksum:              312


Coasting Arc #4 (Orbit 2987)
---------------------------------------

Vector Time (GMT): 2019/262/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4460887
65                 A    =         6793633
61  meter
 Y    =       -2958237
42  meter          E    =           
0014138
 Z    =       -4195496
40                 I    =           51
26484
 XDOT =        980
445679                 Wp   =           87
37371
 YDOT =      -6649
087495  meter/sec      RA   =          252
50814  deg
 ZDOT =       3657
164281                 TA   =          220
36138
                                          MA   =          220
46639
                                          Ha   =            229
965  n
mi
                                          Hp   =            218
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14635458
18                 X    =        -4407096
61
 Y    =       -9705503
36  feet           Y    =        -3007821
72  meter
 Z    =      -13764751
96                 Z    =        -4217035
14
 XDOT =       3216
685297                 XDOT =        1036
960144
 YDOT =     -21814
591519  feet/sec       YDOT =       -6637
807237  meter/sec
 ZDOT =      11998
570476                 ZDOT =        3662
064659

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14053380
29                 X    =         4283470
31
 Y    =       10401703
37  feet           Y    =         3170439
19  meter
 Z    =      -13862499
70                 Z    =        -4225289
91
 XDOT =      -3433
812068                 XDOT =       -1046
625918
 YDOT =      20610
884520  feet/sec       YDOT =        6282
197602  meter/sec
 ZDOT =      12021
284908                 ZDOT =        3664
087640


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   19262
50939719  
00016717  00000-0  10270-3 0  9033
2 25544  51
6395 253
4689 0007440  62
8760 297
3148 15
50070352 29881


Satellite: ISS
Catalog Number: 25544
Epoch time:      19262
50939719   =   yrday
fracday
Element set:     903
Inclination:       51
6395  deg
RA of node:       253
4689  deg
Eccentricity:     
0007440     
Arg of perigee:    62
8760  deg
Mean anomaly:     297
3148  deg
Mean motion:   15
50070352  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2988
Checksum:              338


Coasting Arc #5 (Orbit 3003)
---------------------------------------

Vector Time (GMT): 2019/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4650825
14                 A    =         6794407
78  meter
 Y    =        3000078
52  meter          E    =           
0018219
 Z    =        3929864
18                 I    =           51
27824
 XDOT =       -787
821849                 Wp   =           74
16567
 YDOT =       6491
327631  meter/sec      RA   =          247
52699  deg
 ZDOT =      -4002
735582                 TA   =           57
92621
                                          MA   =           57
74943
                                          Ha   =            229
840  n
mi
                                          Hp   =            218
435

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15258612
66                 X    =         4597842
42
 Y    =        9842777
31  feet           Y    =         3051791
26  meter
 Z    =       12893255
17                 Z    =         3952327
57
 XDOT =      -2584
717354                 XDOT =        -840
907916
 YDOT =      21297
006665  feet/sec       YDOT =        6482
220650  meter/sec
 ZDOT =     -13132
334585                 ZDOT =       -4006
691795

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14854613
61                 X    =        -4527686
23
 Y    =      -10315345
39  feet           Y    =        -3144117
27  meter
 Z    =       12995216
76                 Z    =         3960942
07
 XDOT =       2411
780981                 XDOT =         735
110843
 YDOT =     -20124
066038  feet/sec       YDOT =       -6133
815328  meter/sec
 ZDOT =     -13150
736018                 ZDOT =       -4008
344338


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   19263
54090895  
00016717  00000-0  10270-3 0  9042
2 25544  51
6388 248
3574 0007369  65
4656 294
7262 15
50110812 30046


Satellite: ISS
Catalog Number: 25544
Epoch time:      19263
54090895   =   yrday
fracday
Element set:     904
Inclination:       51
6388  deg
RA of node:       248
3574  deg
Eccentricity:     
0007369     
Arg of perigee:    65
4656  deg
Mean anomaly:     294
7262  deg
Mean motion:   15
50110812  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3004
Checksum:              322


Coasting Arc #6 (Orbit 3018)
---------------------------------------

Vector Time (GMT): 2019/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4877693
84                 A    =         6795282
08  meter
 Y    =       -2967379
52  meter          E    =           
0012698
 Z    =       -3694576
90                 I    =           51
29424
 XDOT =        597
981061                 Wp   =           83
35122
 YDOT =      -6308
290080  meter/sec      RA   =          242
54858  deg
 ZDOT =       4291
374125                 TA   =          232
52725
                                          MA   =          232
64280
                                          Ha   =            230
006  n
mi
                                          Hp   =            218
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16002932
55                 X    =        -4826202
87
 Y    =       -9735497
10  feet           Y    =        -3021637
54  meter
 Z    =      -12121315
29                 Z    =        -3718145
96
 XDOT =       1961
880121                 XDOT =         647
632446
 YDOT =     -20696
489763  feet/sec       YDOT =       -6301
325286  meter/sec
 ZDOT =      14079
311434                 ZDOT =        4294
399704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15780806
20                 X    =         4809989
73
 Y    =        9961643
71  feet           Y    =         3036309
00  meter
 Z    =      -12228321
60                 Z    =        -3727192
42
 XDOT =      -1434
625060                 XDOT =        -437
273718
 YDOT =      19516
247553  feet/sec       YDOT =        5948
552254  meter/sec
 ZDOT =      14093
459624                 ZDOT =        4295
686494


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   19264
50795171  
00016717  00000-0  10270-3 0  9059
2 25544  51
6384 243
5667 0007458  69
1814 291
0135 15
50075173 30193


Satellite: ISS
Catalog Number: 25544
Epoch time:      19264
50795171   =   yrday
fracday
Element set:     905
Inclination:       51
6384  deg
RA of node:       243
5667  deg
Eccentricity:     
0007458     
Arg of perigee:    69
1814  deg
Mean anomaly:     291
0135  deg
Mean motion:   15
50075173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3019
Checksum:              316


Coasting Arc #7 (Orbit 3034)
---------------------------------------

Vector Time (GMT): 2019/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5089156
20                 A    =         6796098
89  meter
 Y    =        2951823
28  meter          E    =           
0019499
 Z    =        3387474
30                 I    =           51
31360
 XDOT =       -472
952921                 Wp   =           83
61145
 YDOT =       6118
197350  meter/sec      RA   =          237
57045  deg
 ZDOT =      -4595
818570                 TA   =           56
65310
                                          MA   =           56
46659
                                          Ha   =            229
889  n
mi
                                          Hp   =            218
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16696706
70                 X    =         5039315
27
 Y    =        9684459
56  feet           Y    =         3008455
21  meter
 Z    =       11113760
83                 Z    =         3412074
52
 XDOT =      -1551
682811                 XDOT =        -519
009170
 YDOT =      20072
825953  feet/sec       YDOT =        6112
650835  meter/sec
 ZDOT =     -15078
144915                 ZDOT =       -4598
228014

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16650215
24                 X    =        -5074985
61
 Y    =       -9635532
82  feet           Y    =        -2936910
40  meter
 Z    =       11225475
10                 Z    =         3421524
81
 XDOT =        687
521447                 XDOT =         209
556537
 YDOT =     -18861
999938  feet/sec       YDOT =       -5749
137581  meter/sec
 ZDOT =     -15089
468887                 ZDOT =       -4599
270117


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   19265
53946146  
00016717  00000-0  10270-3 0  9064
2 25544  51
6383 238
4552 0007339  72
4297 287
7655 15
50108886 30353


Satellite: ISS
Catalog Number: 25544
Epoch time:      19265
53946146   =   yrday
fracday
Element set:     906
Inclination:       51
6383  deg
RA of node:       238
4552  deg
Eccentricity:     
0007339     
Arg of perigee:    72
4297  deg
Mean anomaly:     287
7655  deg
Mean motion:   15
50108886  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3035
Checksum:              341


Coasting Arc #8 (Orbit 3049)
---------------------------------------

Vector Time (GMT): 2019/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5325088
09                 A    =         6796910
35  meter
 Y    =       -2857995
13  meter          E    =           
0011959
 Z    =       -3116936
40                 I    =           51
33569
 XDOT =        352
392966                 Wp   =           76
45263
 YDOT =      -5917
594220  meter/sec      RA   =          232
59480  deg
 ZDOT =       4842
417123                 TA   =          247
60008
                                          MA   =          247
72681
                                          Ha   =            230
011  n
mi
                                          Hp   =            218
281

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17470761
45                 X    =        -5277593
02
 Y    =       -9376624
45  feet           Y    =        -2917278
54  meter
 Z    =      -10226169
30                 Z    =        -3142688
29
 XDOT =       1156
144902                 XDOT =         395
017218
 YDOT =     -19414
679201  feet/sec       YDOT =       -5913
415064  meter/sec
 ZDOT =      15887
195286                 ZDOT =        4844
232595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17587139
34                 X    =         5360560
07
 Y    =        9024132
52  feet           Y    =         2750555
59  meter
 Z    =      -10343147
13                 Z    =        -3152591
24
 XDOT =          1
059609                 XDOT =            
322969
 YDOT =      18148
467572  feet/sec       YDOT =        5531
652916  meter/sec
 ZDOT =      15895
794069                 ZDOT =        4845
038032


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   19266
50649942  
00016717  00000-0  10270-3 0  9077
2 25544  51
6390 233
6641 0007429  75
6946 284
5029 15
50086410 30508


Satellite: ISS
Catalog Number: 25544
Epoch time:      19266
50649942   =   yrday
fracday
Element set:     907
Inclination:       51
6390  deg
RA of node:       233
6641  deg
Eccentricity:     
0007429     
Arg of perigee:    75
6946  deg
Mean anomaly:     284
5029  deg
Mean motion:   15
50086410  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3050
Checksum:              319


Coasting Arc #9 (Orbit 3065)
---------------------------------------

Vector Time (GMT): 2019/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5538747
88                 A    =         6797712
31  meter
 Y    =        2781768
40  meter          E    =           
0020443
 Z    =        2772433
65                 I    =           51
35957
 XDOT =       -302
642179                 Wp   =           92
73580
 YDOT =       5716
436275  meter/sec      RA   =          227
62024  deg
 ZDOT =      -5099
378703                 TA   =           55
74649
                                          MA   =           55
55303
                                          Ha   =            229
956  n
mi
                                          Hp   =            218
276

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18171745
00                 X    =         5493762
77
 Y    =        9126536
73  feet           Y    =         2843455
16  meter
 Z    =        9095910
94                 Z    =         2799229
40
 XDOT =       -992
920536                 XDOT =        -341
772627
 YDOT =      18754
712188  feet/sec       YDOT =        5712
832930  meter/sec
 ZDOT =     -16730
245088                 ZDOT =       -5100
944081

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18438502
70                 X    =        -5620055
62
 Y    =       -8443808
20  feet           Y    =        -2573672
74  meter
 Z    =        9217662
74                 Z    =         2809543
60
 XDOT =       -437
199019                 XDOT =        -133
258261
 YDOT =     -17428
944406  feet/sec       YDOT =       -5312
342255  meter/sec
 ZDOT =     -16737
681969                 ZDOT =       -5101
645464


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   19267
53800420  
00016717  00000-0  10270-3 0  9082
2 25544  51
6388 228
5524 0007403  78
7472 281
4510 15
50108696 30667


Satellite: ISS
Catalog Number: 25544
Epoch time:      19267
53800420   =   yrday
fracday
Element set:     908
Inclination:       51
6388  deg
RA of node:       228
5524  deg
Eccentricity:     
0007403     
Arg of perigee:    78
7472  deg
Mean anomaly:     281
4510  deg
Mean motion:   15
50108696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3066
Checksum:              313


Coasting Arc #10 (Orbit 3080)
---------------------------------------

Vector Time (GMT): 2019/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5764452
81                 A    =         6798421
37  meter
 Y    =       -2624759
15  meter          E    =           
0012172
 Z    =       -2472499
55                 I    =           51
38480
 XDOT =        252
324282                 Wp   =           68
96658
 YDOT =      -5520
961666  meter/sec      RA   =          222
64857  deg
 ZDOT =       5298
130078                 TA   =          263
29783
                                          MA   =          263
43638
                                          Ha   =            230
000  n
mi
                                          Hp   =            218
275

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18912246
75                 X    =        -5722663
59
 Y    =       -8611414
52  feet           Y    =        -2688987
81  meter
 Z    =       -8111875
17                 Z    =        -2500399
34
 XDOT =        827
835571                 XDOT =         288
307245
 YDOT =     -18113
391293  feet/sec       YDOT =       -5517
938487  meter/sec
 ZDOT =      17382
316530                 ZDOT =        5299
443497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19298914
09                 X    =         5882309
02
 Y    =        7570213
25  feet           Y    =         2307401
00  meter
 Z    =       -8238679
65                 Z    =        -2511149
56
 XDOT =        830
687664                 XDOT =         253
193600
 YDOT =      16716
848078  feet/sec       YDOT =        5095
295294  meter/sec
 ZDOT =      17388
583160                 ZDOT =        5300
040147


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   19268
50503878  
00016717  00000-0  10270-3 0  9098
2 25544  51
6385 223
7614 0007366  82
1634 278
0352 15
50092403 30819


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
50503878   =   yrday
fracday
Element set:     909
Inclination:       51
6385  deg
RA of node:       223
7614  deg
Eccentricity:     
0007366     
Arg of perigee:    82
1634  deg
Mean anomaly:     278
0352  deg
Mean motion:   15
50092403  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3081
Checksum:              311


Coasting Arc #11 (Orbit 3082)
---------------------------------------

Vector Time (GMT): 2019/268/13:57:43
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         845977
59                 A    =         6790586
13  meter
 Y    =       -4569501
28  meter          E    =           
0012832
 Z    =        4941337
96                 I    =           51
36261
 XDOT =       6454
194258                 Wp   =          101
86061
 YDOT =       3536
944882  meter/sec      RA   =          222
28123  deg
 ZDOT =       2158
450275                 TA   =          326
98172
                                          MA   =          327
06178
                                          Ha   =            229
879  n
mi
                                          Hp   =            218
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2775517
01                 X    =          873010
01
 Y    =      -14991802
10  feet           Y    =        -4559889
51  meter
 Z    =       16211738
73                 Z    =         4945513
33
 XDOT =      21175
178011                 XDOT =        6403
678917
 YDOT =      11604
149874  feet/sec       YDOT =        3608
837918  meter/sec
 ZDOT =       7081
529772                 ZDOT =        2189
679294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5839695
24                 X    =         1779939
11
 Y    =       14061702
03  feet           Y    =         4286006
78  meter
 Z    =       16230976
35                 Z    =         4947201
59
 XDOT =     -23024
213005                 XDOT =       -7017
780124
 YDOT =       1196
144448  feet/sec       YDOT =         364
584828  meter/sec
 ZDOT =       7223
436012                 ZDOT =        2201
703296


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   19268
63397568  
00016717  00000-0  10270-3 0  9101
2 25544  51
6402 223
1232 0007214  83
3648 276
8324 15
50141077 30838


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
63397568   =   yrday
fracday
Element set:     910
Inclination:       51
6402  deg
RA of node:       223
1232  deg
Eccentricity:     
0007214     
Arg of perigee:    83
3648  deg
Mean anomaly:     276
8324  deg
Mean motion:   15
50141077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3083
Checksum:              303


Coasting Arc #12 (Orbit 3084)
---------------------------------------

Vector Time (GMT): 2019/268/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916975
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1033340
32                 A    =         6790369
93  meter
 Y    =       -4446644
79  meter          E    =           
0012351
 Z    =        5017001
64                 I    =           51
36632
 XDOT =       6450
266929                 Wp   =          101
47848
 YDOT =       3676
842395  meter/sec      RA   =          221
63689  deg
 ZDOT =       1923
850618                 TA   =          329
75606
                                          MA   =          329
82729
                                          Ha   =            229
977  n
mi
                                          Hp   =            218
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3390224
14                 X    =         1058617
48
 Y    =      -14588729
64  feet           Y    =        -4434947
59  meter
 Z    =       16459979
15                 Z    =         5022082
89
 XDOT =      21162
293075                 XDOT =        6399
327057
 YDOT =      12063
131218  feet/sec       YDOT =        3748
689132  meter/sec
 ZDOT =       6311
845858                 ZDOT =        1955
059505

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13728970
76                 X    =         4184590
29
 Y    =        5922054
47  feet           Y    =         1805042
20  meter
 Z    =       16483330
93                 Z    =         5024119
27
 XDOT =     -15331
511062                 XDOT =       -4673
044572
 YDOT =      17520
967103  feet/sec       YDOT =        5340
390773  meter/sec
 ZDOT =       6453
656367                 ZDOT =        1967
074461


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   19268
76291422  
00016717  00000-0  10270-3 0  9118
2 25544  51
6418 222
4849 0007335  83
5061 276
6924 15
50103655 30852


Satellite: ISS
Catalog Number: 25544
Epoch time:      19268
76291422   =   yrday
fracday
Element set:     911
Inclination:       51
6418  deg
RA of node:       222
4849  deg
Eccentricity:     
0007335     
Arg of perigee:    83
5061  deg
Mean anomaly:     276
6924  deg
Mean motion:   15
50103655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3085
Checksum:              314


Coasting Arc #13 (Orbit 3099)
---------------------------------------

Vector Time (GMT): 2019/269/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932083
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1082714
06                 A    =         6789813
45  meter
 Y    =        4317004
20  meter          E    =           
0020715
 Z    =       -5146159
76                 I    =           51
39082
 XDOT =      -6652
813179                 Wp   =           81
31672
 YDOT =      -3456
589791  meter/sec      RA   =          216
66150  deg
 ZDOT =      -1502
101267                 TA   =          174
13492
                                          MA   =          174
11063
                                          Ha   =            229
913  n
mi
                                          Hp   =            218
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3552211
49                 X    =        -1105910
47
 Y    =       14163399
61  feet           Y    =         4304766
36  meter
 Z    =      -16883726
25                 Z    =        -5151475
90
 XDOT =     -21826
814893                 XDOT =       -6606
369790
 YDOT =     -11340
517686  feet/sec       YDOT =       -3530
726697  meter/sec
 ZDOT =      -4928
153764                 ZDOT =       -1534
304919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13382757
87                 X    =        -4079064
60
 Y    =       -5770370
02  feet           Y    =        -1758808
78  meter
 Z    =      -16908132
02                 Z    =        -5153598
64
 XDOT =      14422
511092                 XDOT =        4395
981381
 YDOT =     -18600
368144  feet/sec       YDOT =       -5669
392210  meter/sec
 ZDOT =      -5074
525386                 ZDOT =       -1546
715338


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   19269
72994529  
00016717  00000-0  10270-3 0  9124
2 25544  51
6422 217
6929 0007162  86
0362 274
1607 15
50132777 31008


Satellite: ISS
Catalog Number: 25544
Epoch time:      19269
72994529   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:       217
6929  deg
Eccentricity:     
0007162     
Arg of perigee:    86
0362  deg
Mean anomaly:     274
1607  deg
Mean motion:   15
50132777  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3100
Checksum:              316


Coasting Arc #14 (Orbit 3115)
---------------------------------------

Vector Time (GMT): 2019/270/17:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932083
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1134869
14                 A    =         6789482
12  meter
 Y    =       -4187534
32  meter          E    =           
0010672
 Z    =        5213696
44                 I    =           51
41771
 XDOT =       6874
009711                 Wp   =          101
71949
 YDOT =       3223
053715  meter/sec      RA   =          211
68800  deg
 ZDOT =       1088
400285                 TA   =          337
79822
                                          MA   =          337
84440
                                          Ha   =            229
927  n
mi
                                          Hp   =            218
336

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3723323
93                 X    =         1156285
75
 Y    =      -13738629
66  feet           Y    =        -4174723
08  meter
 Z    =       17105303
28                 Z    =         5219261
70
 XDOT =      22552
525297                 XDOT =        6832
170853
 YDOT =      10574
323212  feet/sec       YDOT =        3299
689929  meter/sec
 ZDOT =       3570
867078                 ZDOT =        1121
689684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13034500
57                 X    =         3972915
77
 Y    =        5642778
65  feet           Y    =         1719918
93  meter
 Z    =       17130829
83                 Z    =         5221476
93
 XDOT =     -13446
473526                 XDOT =       -4098
485131
 YDOT =      19720
409622  feet/sec       YDOT =        6010
780853  meter/sec
 ZDOT =       3722
211480                 ZDOT =        1134
530059


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   19270
76144317  
00016717  00000-0  10270-3 0  9133
2 25544  51
6428 212
5816 0007224  89
7705 270
4273 15
50113868 31168


Satellite: ISS
Catalog Number: 25544
Epoch time:      19270
76144317   =   yrday
fracday
Element set:     913
Inclination:       51
6428  deg
RA of node:       212
5816  deg
Eccentricity:     
0007224     
Arg of perigee:    89
7705  deg
Mean anomaly:     270
4273  deg
Mean motion:   15
50113868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3116
Checksum:              305


Coasting Arc #15 (Orbit 3126)
---------------------------------------

Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6257540
91                 A    =         6800616
17  meter
 Y    =       -2493556
52  meter          E    =           
0015413
 Z    =        -910528
47                 I    =           51
47415
 XDOT =       1051
135424                 Wp   =           61
95827
 YDOT =      -4763
580209  meter/sec      RA   =          207
90486  deg
 ZDOT =       5905
294964                 TA   =          288
18269
                                          MA   =          288
35044
                                          Ha   =            229
973  n
mi
                                          Hp   =            218
268

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20529989
86                 X    =        -6224769
30
 Y    =       -8180959
71  feet           Y    =        -2563349
63  meter
 Z    =       -2987298
12                 Z    =         -940845
50
 XDOT =       3448
607035                 XDOT =        1075
640251
 YDOT =     -15628
543992  feet/sec       YDOT =       -4751
687945  meter/sec
 ZDOT =      19374
327310                 ZDOT =        5910
461101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19684143
47                 X    =         5999726
93
 Y    =       10005018
39  feet           Y    =         3049529
61  meter
 Z    =       -3125162
15                 Z    =         -952549
42
 XDOT =      -3990
036449                 XDOT =       -1216
163110
 YDOT =      13827
287305  feet/sec       YDOT =        4214
557171  meter/sec
 ZDOT =      19398
060473                 ZDOT =        5912
528832


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   19271
47059738  
00016717  00000-0  10270-3 0  9145
2 25544  51
6401 209
0670 0007360  92
4877 267
7117 15
50120658 31273


Satellite: ISS
Catalog Number: 25544
Epoch time:      19271
47059738   =   yrday
fracday
Element set:     914
Inclination:       51
6401  deg
RA of node:       209
0670  deg
Eccentricity:     
0007360     
Arg of perigee:    92
4877  deg
Mean anomaly:     267
7117  deg
Mean motion:   15
50120658  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3127
Checksum:              312


Coasting Arc #16 (Orbit 3135)
---------------------------------------

Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         251173
21                 A    =         6790347
44  meter
 Y    =        4557219
42  meter          E    =           
0019698
 Z    =       -5045272
62                 I    =           51
45902
 XDOT =      -7207
030717                 Wp   =           84
25847
 YDOT =      -1705
711641  meter/sec      RA   =          205
13291  deg
 ZDOT =      -1904
011254                 TA   =          167
20434
                                          MA   =          167
15428
                                          Ha   =            229
960  n
mi
                                          Hp   =            218
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         824059
10                 X    =          224701
73
 Y    =       14951507
28  feet           Y    =         4559879
59  meter
 Z    =      -16552731
68                 Z    =        -5044117
35
 XDOT =     -23645
113901                 XDOT =       -7178
172608
 YDOT =      -5596
166802  feet/sec       YDOT =       -1786
144619  meter/sec
 ZDOT =      -6246
756084                 ZDOT =       -1938
950291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5475302
99                 X    =         1668872
35
 Y    =       13943272
46  feet           Y    =         4249909
45  meter
 Z    =      -16547682
00                 Z    =        -5043733
47
 XDOT =     -23164
748313                 XDOT =       -7060
615286
 YDOT =       1511
789123  feet/sec       YDOT =         460
793325  meter/sec
 ZDOT =      -6405
701145                 ZDOT =       -1952
457709


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   19272
05081307  
00016717  00000-0  10270-3 0  9158
2 25544  51
6427 206
1897 0007218  98
8582 261
3386 15
50109808 31367


Satellite: ISS
Catalog Number: 25544
Epoch time:      19272
05081307   =   yrday
fracday
Element set:     915
Inclination:       51
6427  deg
RA of node:       206
1897  deg
Eccentricity:     
0007218     
Arg of perigee:    98
8582  deg
Mean anomaly:     261
3386  deg
Mean motion:   15
50109808  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3136
Checksum:              319


Coasting Arc #17 (Orbit 3151)
---------------------------------------

Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -186609
15                 A    =         6789729
32  meter
 Y    =       -4424409
49  meter          E    =           
0011818
 Z    =        5138340
12                 I    =           51
48864
 XDOT =       7382
157046                 Wp   =          111
91963
 YDOT =       1439
193665  meter/sec      RA   =          200
16488  deg
 ZDOT =       1500
227746                 TA   =          323
56317
                                          MA   =          323
64354
                                          Ha   =            229
886  n
mi
                                          Hp   =            218
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -612234
74                 X    =         -162079
80
 Y    =      -14515779
16  feet           Y    =        -4426358
57  meter
 Z    =       16858071
24                 Z    =         5137493
69
 XDOT =      24219
675348                 XDOT =        7358
227534
 YDOT =       4721
763993  feet/sec       YDOT =        1521
612522  meter/sec
 ZDOT =       4922
007041                 ZDOT =        1536
029699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5375076
50                 X    =        -1638323
32
 Y    =      -13502384
72  feet           Y    =        -4115526
86  meter
 Z    =       16854417
87                 Z    =         5137226
57
 XDOT =      23430
208297                 XDOT =        7141
527489
 YDOT =      -2950
837140  feet/sec       YDOT =        -899
415160  meter/sec
 ZDOT =       5084
907686                 ZDOT =        1549
879863


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   19273
08230513  
00016717  00000-0  10270-3 0  9168
2 25544  51
6432 201
0788 0007225 102
6400 257
5559 15
50156662 31524


Satellite: ISS
Catalog Number: 25544
Epoch time:      19273
08230513   =   yrday
fracday
Element set:     916
Inclination:       51
6432  deg
RA of node:       201
0788  deg
Eccentricity:     
0007225     
Arg of perigee:   102
6400  deg
Mean anomaly:     257
5559  deg
Mean motion:   15
50156662  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3152
Checksum:              286


Coasting Arc #18 (Orbit 3166)
---------------------------------------

Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965355
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          73421
50                 A    =         6789474
24  meter
 Y    =        4337176
68  meter          E    =           
0020922
 Z    =       -5241235
89                 I    =           51
51907
 XDOT =      -7483
139428                 Wp   =           89
86278
 YDOT =      -1155
797914  meter/sec      RA   =          195
19888  deg
 ZDOT =      -1064
907196                 TA   =          169
91032
                                          MA   =          169
86825
                                          Ha   =            229
893  n
mi
                                          Hp   =            218
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         240884
18                 X    =           50375
92
 Y    =       14229582
29  feet           Y    =         4337868
41  meter
 Z    =      -17195655
79                 Z    =        -5240935
59
 XDOT =     -24550
982376                 XDOT =       -7464
485981
 YDOT =      -3791
987907  feet/sec       YDOT =       -1239
375456  meter/sec
 ZDOT =      -3493
790012                 ZDOT =       -1101
212682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5162267
11                 X    =         1573459
02
 Y    =       13263873
67  feet           Y    =         4042828
70  meter
 Z    =      -17194483
68                 Z    =        -5240878
63
 XDOT =     -23391
775083                 XDOT =       -7129
813045
 YDOT =       4376
203606  feet/sec       YDOT =        1333
866859  meter/sec
 ZDOT =      -3659
013190                 ZDOT =       -1115
267220


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   19274
04932723  
00016717  00000-0  10270-3 0  9178
2 25544  51
6432 196
2879 0007139 105
4210 254
7730 15
50118276 31679


Satellite: ISS
Catalog Number: 25544
Epoch time:      19274
04932723   =   yrday
fracday
Element set:     917
Inclination:       51
6432  deg
RA of node:       196
2879  deg
Eccentricity:     
0007139     
Arg of perigee:   105
4210  deg
Mean anomaly:     254
7730  deg
Mean motion:   15
50118276  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3167
Checksum:              311
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