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

 
Date: June 14th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16989 6378 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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


168/10:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 216 7

168/10:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 2
000/00:00:00 000 0 0 0 0 216 7

175/23:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 216 2

175/23:25:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 216 3

176/18:02:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 216 3

Coasting Arc #1 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2019/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5544905
17                 A    =         6795668
45  meter
 Y    =       -3223607
68  meter          E    =           
0009666
 Z    =       -2256952
01                 I    =           51
75079
 XDOT =       4177
194900                 Wp   =           80
64382
 YDOT =      -3382
380051  meter/sec      RA   =           14
06725  deg
 ZDOT =      -5449
932453                 TA   =          124
35960
                                          MA   =          124
26812
                                          Ha   =            228
168  n
mi
                                          Hp   =            217
014

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18191946
09                 X    =        -5497482
64
 Y    =      -10576140
67  feet           Y    =        -3285349
22  meter
 Z    =       -7404698
18                 Z    =        -2283772
59
 XDOT =      13704
707676                 XDOT =        4241
180157
 YDOT =     -11097
047411  feet/sec       YDOT =       -3335
309193  meter/sec
 ZDOT =     -17880
355816                 ZDOT =       -5429
486094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13110654
51                 X    =        -3996127
50
 Y    =       16404326
41  feet           Y    =         5000038
69  meter
 Z    =       -7525956
59                 Z    =        -2293911
57
 XDOT =      -7766
029962                 XDOT =       -2367
085932
 YDOT =     -14339
873319  feet/sec       YDOT =       -4370
793388  meter/sec
 ZDOT =     -17787
173570                 ZDOT =       -5421
530504


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   19165
52770381  
00016717  00000-0  10270-3 0  9002
2 25544  51
6418  14
5055 0007873  43
8324 316
3451 15
51186134 14830


Satellite: ISS
Catalog Number: 25544
Epoch time:      19165
52770381   =   yrday
fracday
Element set:     900
Inclination:       51
6418  deg
RA of node:        14
5055  deg
Eccentricity:     
0007873     
Arg of perigee:    43
8324  deg
Mean anomaly:     316
3451  deg
Mean motion:   15
51186134  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1483
Checksum:              296


Coasting Arc #2 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2019/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5270367
21                 A    =         6794203
19  meter
 Y    =        3150033
41  meter          E    =           
0020177
 Z    =        2882785
95                 I    =           51
71350
 XDOT =      -4741
567407                 Wp   =           68
49155
 YDOT =       3283
943929  meter/sec      RA   =            9
11257  deg
 ZDOT =       5059
023712                 TA   =          324
29098
                                          MA   =          324
42577
                                          Ha   =            228
093  n
mi
                                          Hp   =            216
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17291231
02                 X    =         5220747
86
 Y    =       10334755
28  feet           Y    =         3208692
44  meter
 Z    =        9457959
16                 Z    =         2908267
62
 XDOT =     -15556
323514                 XDOT =       -4802
511113
 YDOT =      10774
094254  feet/sec       YDOT =        3230
578816  meter/sec
 ZDOT =      16597
846824                 ZDOT =        5035
843290

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12469449
43                 X    =         3800688
19
 Y    =      -15751652
77  feet           Y    =        -4801103
76  meter
 Z    =        9573144
42                 Z    =         2917894
42
 XDOT =       7517
544144                 XDOT =        2291
347455
 YDOT =      16016
171360  feet/sec       YDOT =        4881
729031  meter/sec
 ZDOT =      16492
275431                 ZDOT =        5026
845551


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   19166
55848163  
00016717  00000-0  10270-3 0  9011
2 25544  51
6417   9
3887 0007834  47
2492 312
9318 15
51218633 14996


Satellite: ISS
Catalog Number: 25544
Epoch time:      19166
55848163   =   yrday
fracday
Element set:     901
Inclination:       51
6417  deg
RA of node:         9
3887  deg
Eccentricity:     
0007834     
Arg of perigee:    47
2492  deg
Mean anomaly:     312
9318  deg
Mean motion:   15
51218633  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1499
Checksum:              331


Coasting Arc #3 (Orbit 1513)
---------------------------------------

Vector Time (GMT): 2019/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4918898
06                 A    =         6792573
82  meter
 Y    =       -3131057
28  meter          E    =           
0012639
 Z    =       -3499635
29                 I    =           51
67332
 XDOT =       5262
834114                 Wp   =           63
91453
 YDOT =      -3210
119897  meter/sec      RA   =            4
15431  deg
 ZDOT =      -4532
448803                 TA   =          157
08022
                                          MA   =          157
02376
                                          Ha   =            228
304  n
mi
                                          Hp   =            216
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16138117
01                 X    =        -4866520
74
 Y    =      -10272497
64  feet           Y    =        -3185770
35  meter
 Z    =      -11481743
08                 Z    =        -3523402
92
 XDOT =      17266
516122                 XDOT =        5320
355667
 YDOT =     -10531
889427  feet/sec       YDOT =       -3150
944757  meter/sec
 ZDOT =     -14870
238855                 ZDOT =       -4506
744671

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12004490
11                 X    =        -3658968
58
 Y    =       14811390
29  feet           Y    =         4514511
76  meter
 Z    =      -11589149
55                 Z    =        -3532372
78
 XDOT =      -7445
263099                 XDOT =       -2269
316193
 YDOT =     -17559
321727  feet/sec       YDOT =       -5352
081262  meter/sec
 ZDOT =     -14753
230428                 ZDOT =       -4496
784634


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   19167
52483547  
00016717  00000-0  10270-3 0  9021
2 25544  51
6401   4
5920 0008052  51
3769 308
8102 15
51206940 15141


Satellite: ISS
Catalog Number: 25544
Epoch time:      19167
52483547   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:         4
5920  deg
Eccentricity:     
0008052     
Arg of perigee:    51
3769  deg
Mean anomaly:     308
8102  deg
Mean motion:   15
51206940  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1514
Checksum:              286


Coasting Arc #4 (Orbit 1528)
---------------------------------------

Vector Time (GMT): 2019/168/10:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6787339
94                 A    =         6797801
30  meter
 Y    =          40740
14  meter          E    =           
0020381
 Z    =         121585
52                 I    =           51
66165
 XDOT =       -147
893878                 Wp   =           49
50966
 YDOT =       4756
378181  meter/sec      RA   =          359
53220  deg
 ZDOT =       6012
611181                 TA   =          311
79876
                                          MA   =          311
97270
                                          Ha   =            228
337  n
mi
                                          Hp   =            216
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22268175
66                 X    =         6785789
33
 Y    =         133661
86  feet           Y    =          116632
23  meter
 Z    =         398902
62                 Z    =          154552
16
 XDOT =       -485
216135                 XDOT =        -230
276021
 YDOT =      15604
915292  feet/sec       YDOT =        4754
262554  meter/sec
 ZDOT =      19726
414636                 ZDOT =        6011
693583

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11831627
86                 X    =         3606280
17
 Y    =      -18861612
92  feet           Y    =        -5749019
62  meter
 Z    =         548430
75                 Z    =          167161
69
 XDOT =      11569
557865                 XDOT =        3526
401237
 YDOT =       7875
934770  feet/sec       YDOT =        2400
584918  meter/sec
 ZDOT =      19721
637328                 ZDOT =        6011
155058


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   19168
49118742  
00016717  00000-0  10270-3 0  9031
2 25544  51
6420 359
7977 0008021  54
6491 305
5409 15
51216362 15292


Satellite: ISS
Catalog Number: 25544
Epoch time:      19168
49118742   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:       359
7977  deg
Eccentricity:     
0008021     
Arg of perigee:    54
6491  deg
Mean anomaly:     305
5409  deg
Mean motion:   15
51216362  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1529
Checksum:              317


Coasting Arc #5 (Orbit 1543)
---------------------------------------

Vector Time (GMT): 2019/169/10:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6671960
90                 A    =         6797174
02  meter
 Y    =        -359498
50  meter          E    =           
0012431
 Z    =       -1248567
28                 I    =           51
62625
 XDOT =       1339
887324                 Wp   =          102
65754
 YDOT =      -4770
901118  meter/sec      RA   =          354
57502  deg
 ZDOT =      -5838
084099                 TA   =           90
89282
                                          MA   =           90
75039
                                          Ha   =            228
324  n
mi
                                          Hp   =            216
710

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21889635
51                 X    =        -6661380
19
 Y    =       -1179457
01  feet           Y    =         -434049
63  meter
 Z    =       -4096349
35                 Z    =        -1280951
45
 XDOT =       4395
955787                 XDOT =        1421
495400
 YDOT =     -15652
562723  feet/sec       YDOT =       -4755
460136  meter/sec
 ZDOT =     -19153
819221                 ZDOT =       -5831
378155

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12118210
07                 X    =        -3693630
43
 Y    =       18233805
35  feet           Y    =         5557663
87  meter
 Z    =       -4243190
65                 Z    =        -1293324
51
 XDOT =      -9857
897771                 XDOT =       -3004
687240
 YDOT =     -10963
444507  feet/sec       YDOT =       -3341
657886  meter/sec
 ZDOT =     -19122
786027                 ZDOT =       -5828
625181


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   19169
45753898  
00016717  00000-0  10270-3 0  9046
2 25544  51
6421 355
0016 0007865  57
8267 302
3646 15
51188800 15447


Satellite: ISS
Catalog Number: 25544
Epoch time:      19169
45753898   =   yrday
fracday
Element set:     904
Inclination:       51
6421  deg
RA of node:       355
0016  deg
Eccentricity:     
0007865     
Arg of perigee:    57
8267  deg
Mean anomaly:     302
3646  deg
Mean motion:   15
51188800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1544
Checksum:              327


Coasting Arc #6 (Orbit 1559)
---------------------------------------

Vector Time (GMT): 2019/170/10:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6494577
70                 A    =         6796105
49  meter
 Y    =         366044
09  meter          E    =           
0021744
 Z    =        1930900
62                 I    =           51
58982
 XDOT =      -1950
447105                 Wp   =           65
06108
 YDOT =       4869
038138  meter/sec      RA   =          349
61318  deg
 ZDOT =       5596
812105                 TA   =          316
23332
                                          MA   =          316
40547
                                          Ha   =            228
247  n
mi
                                          Hp   =            216
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21307669
61                 X    =         6480622
62
 Y    =        1200932
06  feet           Y    =          438592
62  meter
 Z    =        6334975
79                 Z    =         1962414
81
 XDOT =      -6399
104675                 XDOT =       -2031
935134
 YDOT =      15974
534572  feet/sec       YDOT =        4846
770206  meter/sec
 ZDOT =      18362
244438                 ZDOT =        5587
140612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11527313
26                 X    =         3513525
08
 Y    =      -17909473
29  feet           Y    =        -5458807
46  meter
 Z    =        6477866
62                 Z    =         1974453
74
 XDOT =       9378
988429                 XDOT =        2858
715673
 YDOT =      12709
239915  feet/sec       YDOT =        3873
776326  meter/sec
 ZDOT =      18317
751619                 ZDOT =        5583
250694


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   19170
48830930  
00016717  00000-0  10270-3 0  9055
2 25544  51
6419 349
8846 0007855  61
4917 298
7024 15
51237515 15602


Satellite: ISS
Catalog Number: 25544
Epoch time:      19170
48830930   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:       349
8846  deg
Eccentricity:     
0007855     
Arg of perigee:    61
4917  deg
Mean anomaly:     298
7024  deg
Mean motion:   15
51237515  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1560
Checksum:              331


Coasting Arc #7 (Orbit 1574)
---------------------------------------

Vector Time (GMT): 2019/171/10:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6251787
90                 A    =         6794800
66  meter
 Y    =        -452262
68  meter          E    =           
0011306
 Z    =       -2633806
37                 I    =           51
55131
 XDOT =       2549
314168                 Wp   =           86
50360
 YDOT =      -4991
803032  meter/sec      RA   =          344
64896  deg
 ZDOT =      -5212
784368                 TA   =          123
14215
                                          MA   =          123
03361
                                          Ha   =            228
408  n
mi
                                          Hp   =            216
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20511115
14                 X    =        -6233472
48
 Y    =       -1483801
45  feet           Y    =         -522071
69  meter
 Z    =       -8641097
00                 Z    =        -2664130
51
 XDOT =       8363
891626                 XDOT =        2630
265029
 YDOT =     -16377
306536  feet/sec       YDOT =       -4962
841295  meter/sec
 ZDOT =     -17102
310917                 ZDOT =       -5200
205117

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11078092
73                 X    =        -3376602
66
 Y    =       17256550
90  feet           Y    =         5259796
72  meter
 Z    =       -8778575
11                 Z    =        -2675709
69
 XDOT =      -9076
920806                 XDOT =       -2766
645462
 YDOT =     -14467
074011  feet/sec       YDOT =       -4409
564159  meter/sec
 ZDOT =     -17044
620739                 ZDOT =       -5195
200401


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   19171
45465756  
00016717  00000-0  10270-3 0  9064
2 25544  51
6405 345
0884 0008018  64
7751 295
4230 15
51209513 15757


Satellite: ISS
Catalog Number: 25544
Epoch time:      19171
45465756   =   yrday
fracday
Element set:     906
Inclination:       51
6405  deg
RA of node:       345
0884  deg
Eccentricity:     
0008018     
Arg of perigee:    64
7751  deg
Mean anomaly:     295
4230  deg
Mean motion:   15
51209513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1575
Checksum:              315


Coasting Arc #8 (Orbit 1590)
---------------------------------------

Vector Time (GMT): 2019/172/10:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5941045
29                 A    =         6793242
07  meter
 Y    =         537461
03  meter          E    =           
0020224
 Z    =        3228871
96                 I    =           51
51419
 XDOT =      -3068
021691                 Wp   =           79
97708
 YDOT =       5173
222837  meter/sec      RA   =          339
68067  deg
 ZDOT =       4761
980752                 TA   =          317
47694
                                          MA   =          317
63340
                                          Ha   =            228
245  n
mi
                                          Hp   =            216
471

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19491618
40                 X    =         5918909
81
 Y    =        1763323
59  feet           Y    =          603773
69  meter
 Z    =       10593411
93                 Z    =         3257677
34
 XDOT =     -10065
687963                 XDOT =       -3148
772926
 YDOT =      16972
515870  feet/sec       YDOT =        5138
461821  meter/sec
 ZDOT =      15623
296431                 ZDOT =        4746
882291

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10549740
11                 X    =         3215560
78
 Y    =      -16399755
42  feet           Y    =        -4998645
45  meter
 Z    =       10723986
21                 Z    =         3268671
00
 XDOT =       9145
352956                 XDOT =        2787
503581
 YDOT =      16100
744138  feet/sec       YDOT =        4907
506813  meter/sec
 ZDOT =      15554
167036                 ZDOT =        4740
910113


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   19172
48542626  
00016717  00000-0  10270-3 0  9071
2 25544  51
6402 339
9724 0007799  69
0892 291
1094 15
51232982 15913


Satellite: ISS
Catalog Number: 25544
Epoch time:      19172
48542626   =   yrday
fracday
Element set:     907
Inclination:       51
6402  deg
RA of node:       339
9724  deg
Eccentricity:     
0007799     
Arg of perigee:    69
0892  deg
Mean anomaly:     291
1094  deg
Mean motion:   15
51232982  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1591
Checksum:              338


Coasting Arc #9 (Orbit 1605)
---------------------------------------

Vector Time (GMT): 2019/173/10:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5585098
54                 A    =         6791529
21  meter
 Y    =        -717489
38  meter          E    =           
0014253
 Z    =       -3812273
33                 I    =           51
47740
 XDOT =       3532
888703                 Wp   =           73
26105
 YDOT =      -5348
263253  meter/sec      RA   =          334
70761  deg
 ZDOT =      -4178
211241                 TA   =          152
51112
                                          MA   =          152
43566
                                          Ha   =            228
444  n
mi
                                          Hp   =            216
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18323814
12                 X    =        -5558142
58
 Y    =       -2353967
77  feet           Y    =         -779794
61  meter
 Z    =      -12507458
44                 Z    =        -3839337
98
 XDOT =      11590
842200                 XDOT =        3612
727145
 YDOT =     -17546
795451  feet/sec       YDOT =       -5308
309031  meter/sec
 ZDOT =     -13708
042130                 ZDOT =       -4160
856810

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10266218
40                 X    =        -3129143
37
 Y    =       15258601
36  feet           Y    =         4650821
69  meter
 Z    =      -12630110
41                 Z    =        -3849657
65
 XDOT =      -9354
126395                 XDOT =       -2851
137725
 YDOT =     -17550
377177  feet/sec       YDOT =       -5349
354964  meter/sec
 ZDOT =     -13628
671414                 ZDOT =       -4154
019047


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   19173
45177197  
00016717  00000-0  10270-3 0  9087
2 25544  51
6400 335
1756 0008035  72
4556 287
7473 15
51227178 16063


Satellite: ISS
Catalog Number: 25544
Epoch time:      19173
45177197   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       335
1756  deg
Eccentricity:     
0008035     
Arg of perigee:    72
4556  deg
Mean anomaly:     287
7473  deg
Mean motion:   15
51227178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1606
Checksum:              324


Coasting Arc #10 (Orbit 1621)
---------------------------------------

Vector Time (GMT): 2019/174/10:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5185698
69                 A    =         6789928
68  meter
 Y    =         916213
23  meter          E    =           
0017033
 Z    =        4272096
79                 I    =           51
44223
 XDOT =      -3916
818730                 Wp   =           93
06526
 YDOT =       5561
041567  meter/sec      RA   =          329
73089  deg
 ZDOT =       3548
651501                 TA   =          320
60895
                                          MA   =          320
73269
                                          Ha   =            228
315  n
mi
                                          Hp   =            216
376

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17013447
14                 X    =         5154316
65
 Y    =        3005948
91  feet           Y    =          974027
35  meter
 Z    =       14016065
59                 Z    =         4297210
63
 XDOT =     -12850
455150                 XDOT =       -3995
949992
 YDOT =      18244
887031  feet/sec       YDOT =        5516
798062  meter/sec
 ZDOT =      11642
557417                 ZDOT =        3529
433743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10019970
05                 X    =         3054086
87
 Y    =      -13960336
77  feet           Y    =        -4255110
65  meter
 Z    =       14129840
92                 Z    =         4306775
51
 XDOT =       9853
415969                 XDOT =        3003
321187
 YDOT =      18810
566227  feet/sec       YDOT =        5733
460586  meter/sec
 ZDOT =      11554
724123                 ZDOT =        3521
879913


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   19174
48253694  
00016717  00000-0  10270-3 0  9099
2 25544  51
6399 330
0593 0007923  76
2581 283
9451 15
51224118 16221


Satellite: ISS
Catalog Number: 25544
Epoch time:      19174
48253694   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       330
0593  deg
Eccentricity:     
0007923     
Arg of perigee:    76
2581  deg
Mean anomaly:     283
9451  deg
Mean motion:   15
51224118  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1622
Checksum:              324


Coasting Arc #11 (Orbit 1636)
---------------------------------------

Vector Time (GMT): 2019/175/10:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4772212
27                 A    =         6788387
87  meter
 Y    =       -1212038
33  meter          E    =           
0018962
 Z    =       -4691455
59                 I    =           51
40827
 XDOT =       4215
806559                 Wp   =           74
70435
 YDOT =      -5728
416960  meter/sec      RA   =          324
75053  deg
 ZDOT =      -2813
087019                 TA   =          167
24936
                                          MA   =          167
20133
                                          Ha   =            228
551  n
mi
                                          Hp   =            216
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15656864
40                 X    =        -4735515
91
 Y    =       -3976503
71  feet           Y    =        -1265198
84  meter
 Z    =      -15391914
66                 Z    =        -4714548
05
 XDOT =      13831
386347                 XDOT =        4293
214343
 YDOT =     -18794
018896  feet/sec       YDOT =       -5680
839721  meter/sec
 ZDOT =      -9229
288120                 ZDOT =       -2792
421000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10092185
00                 X    =        -3076097
99
 Y    =       12484704
23  feet           Y    =         3805337
85  meter
 Z    =      -15496482
95                 Z    =        -4723328
00
 XDOT =     -10392
996491                 XDOT =       -3167
785330
 YDOT =     -19721
078089  feet/sec       YDOT =       -6010
984601  meter/sec
 ZDOT =      -9134
882075                 ZDOT =       -2784
312057


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   19175
44887910  
00016717  00000-0  10270-3 0  9102
2 25544  51
6393 325
2633 0008207  80
8728 279
3352 15
51227115 16371


Satellite: ISS
Catalog Number: 25544
Epoch time:      19175
44887910   =   yrday
fracday
Element set:     910
Inclination:       51
6393  deg
RA of node:       325
2633  deg
Eccentricity:     
0008207     
Arg of perigee:    80
8728  deg
Mean anomaly:     279
3352  deg
Mean motion:   15
51227115  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1637
Checksum:              317


Coasting Arc #12 (Orbit 1645)
---------------------------------------

Vector Time (GMT): 2019/175/23:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931521
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5573073
91                 A    =         6797557
66  meter
 Y    =       -3847672
92  meter          E    =           
0020359
 Z    =         491267
53                 I    =           51
42474
 XDOT =       2355
936675                 Wp   =           62
66568
 YDOT =       4197
373122  meter/sec      RA   =          322
06180  deg
 ZDOT =       5966
549098                 TA   =          302
64437
                                          MA   =          302
84065
                                          Ha   =            228
489  n
mi
                                          Hp   =            216
168

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18284363
21                 X    =         5613299
19
 Y    =      -12623598
81  feet           Y    =        -3785126
04  meter
 Z    =        1611770
10                 Z    =          518436
56
 XDOT =       7729
451034                 XDOT =        2279
843338
 YDOT =      13770
909194  feet/sec       YDOT =        4223
292738  meter/sec
 ZDOT =      19575
292316                 ZDOT =        5977
808937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9055306
26                 X    =         2760057
35
 Y    =       20279563
63  feet           Y    =         6181210
99  meter
 Z    =        1735429
39                 Z    =          528958
88
 XDOT =     -13453
936779                 XDOT =       -4100
759930
 YDOT =       4280
702475  feet/sec       YDOT =        1304
758114  meter/sec
 ZDOT =      19625
844845                 ZDOT =        5981
957509


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   19176
02868161  
00016717  00000-0  10270-3 0  9115
2 25544  51
6394 322
3891 0008167  83
1218 277
0862 15
51263029 16466


Satellite: ISS
Catalog Number: 25544
Epoch time:      19176
02868161   =   yrday
fracday
Element set:     911
Inclination:       51
6394  deg
RA of node:       322
3891  deg
Eccentricity:     
0008167     
Arg of perigee:    83
1218  deg
Mean anomaly:     277
0862  deg
Mean motion:   15
51263029  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1646
Checksum:              315


Coasting Arc #13 (Orbit 1645)
---------------------------------------

Vector Time (GMT): 2019/175/23:25:30
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4579965
79                 A    =         6787762
17  meter
 Y    =        1311270
62  meter          E    =           
0014180
 Z    =        4823804
58                 I    =           51
39184
 XDOT =      -4292
394428                 Wp   =           98
95390
 YDOT =       5857
825976  meter/sec      RA   =          322
02220  deg
 ZDOT =       2474
663658                 TA   =          326
62268
                                          MA   =          326
71200
                                          Ha   =            228
346  n
mi
                                          Hp   =            216
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15026134
48                 X    =         4541531
17
 Y    =        4302068
95  feet           Y    =         1362271
57  meter
 Z    =       15826130
51                 Z    =         4845959
01
 XDOT =     -14082
658884                 XDOT =       -4369
599767
 YDOT =      19218
589159  feet/sec       YDOT =        5809
393458  meter/sec
 ZDOT =       8118
975257                 ZDOT =        2453
626058

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6011948
45                 X    =        -1832441
89
 Y    =       14316570
43  feet           Y    =         4363690
67  meter
 Z    =       15926431
13                 Z    =         4854376
21
 XDOT =     -16397
356649                 XDOT =       -4997
914307
 YDOT =     -15841
233247  feet/sec       YDOT =       -4828
407894  meter/sec
 ZDOT =       8022
877136                 ZDOT =        2445
372951


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   19176
02868284  
00016717  00000-0  10270-3 0  9122
2 25544  51
6396 322
3889 0008029  81
3689 278
8371 15
51235808 16462


Satellite: ISS
Catalog Number: 25544
Epoch time:      19176
02868284   =   yrday
fracday
Element set:     912
Inclination:       51
6396  deg
RA of node:       322
3889  deg
Eccentricity:     
0008029     
Arg of perigee:    81
3689  deg
Mean anomaly:     278
8371  deg
Mean motion:   15
51235808  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1646
Checksum:              348


Coasting Arc #14 (Orbit 1657)
---------------------------------------

Vector Time (GMT): 2019/176/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3784571
66                 A    =         6786235
73  meter
 Y    =        2174906
67  meter          E    =           
0011361
 Z    =        5186621
75                 I    =           51
36880
 XDOT =      -4954
145329                 Wp   =           97
61251
 YDOT =       5732
491752  meter/sec      RA   =          318
15104  deg
 ZDOT =       1207
378896                 TA   =          340
74416
                                          MA   =          340
78706
                                          Ha   =            228
349  n
mi
                                          Hp   =            216
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12416573
68                 X    =         3734776
31
 Y    =        7135520
58  feet           Y    =         2216949
42  meter
 Z    =       17016475
57                 Z    =         5204885
02
 XDOT =     -16253
757642                 XDOT =       -5023
744248
 YDOT =      18807
387639  feet/sec       YDOT =        5676
701743  meter/sec
 ZDOT =       3961
216849                 ZDOT =        1183
145167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12681068
90                 X    =        -3865189
80
 Y    =       -6439033
87  feet           Y    =        -1962617
52  meter
 Z    =       17099027
21                 Z    =         5211783
49
 XDOT =      14735
511296                 XDOT =        4491
383843
 YDOT =     -18762
143884  feet/sec       YDOT =       -5718
701456  meter/sec
 ZDOT =       3850
653330                 ZDOT =        1173
679135


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   19176
80175379  
00016717  00000-0  10270-3 0  9135
2 25544  51
6417 318
5512 0007980  85
6466 274
5596 15
51234676 16588


Satellite: ISS
Catalog Number: 25544
Epoch time:      19176
80175379   =   yrday
fracday
Element set:     913
Inclination:       51
6417  deg
RA of node:       318
5512  deg
Eccentricity:     
0007980     
Arg of perigee:    85
6466  deg
Mean anomaly:     274
5596  deg
Mean motion:   15
51234676  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1658
Checksum:              347


Coasting Arc #15 (Orbit 1672)
---------------------------------------

Vector Time (GMT): 2019/177/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3374143
08                 A    =         6785924
18  meter
 Y    =       -2601430
90  meter          E    =           
0022859
 Z    =       -5301624
48                 I    =           51
34402
 XDOT =       5010
819031                 Wp   =           87
40914
 YDOT =      -5764
808992  meter/sec      RA   =          313
16220  deg
 ZDOT =       -360
696566                 TA   =          179
12983
                                          MA   =          179
12584
                                          Ha   =            228
554  n
mi
                                          Hp   =            216
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11070023
24                 X    =        -3319050
03
 Y    =       -8534878
28  feet           Y    =        -2638854
29  meter
 Z    =      -17393781
12                 Z    =        -5317881
29
 XDOT =      16439
694983                 XDOT =        5076
662424
 YDOT =     -18913
415328  feet/sec       YDOT =       -5708
406306  meter/sec
 ZDOT =      -1183
387683                 ZDOT =        -336
196618

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11546607
66                 X    =         3519406
02
 Y    =        7714045
61  feet           Y    =         2351241
10  meter
 Z    =      -17467184
52                 Z    =        -5323997
84
 XDOT =     -14460
747574                 XDOT =       -4407
635861
 YDOT =      19221
267769  feet/sec       YDOT =        5858
642416  meter/sec
 ZDOT =      -1071
627830                 ZDOT =        -326
632163


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   19177
76809162  
00016717  00000-0  10270-3 0  9146
2 25544  51
6424 313
7549 0008067  88
3405 271
8670 15
51205274 16735


Satellite: ISS
Catalog Number: 25544
Epoch time:      19177
76809162   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       313
7549  deg
Eccentricity:     
0008067     
Arg of perigee:    88
3405  deg
Mean anomaly:     271
8670  deg
Mean motion:   15
51205274  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1673
Checksum:              325


Coasting Arc #16 (Orbit 1688)
---------------------------------------

Vector Time (GMT): 2019/178/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2975482
01                 A    =         6785833
19  meter
 Y    =        3046532
15  meter          E    =           
0010754
 Z    =        5273995
81                 I    =           51
32138
 XDOT =      -5034
405981                 Wp   =           85
27470
 YDOT =       5768
814851  meter/sec      RA   =          308
17242  deg
 ZDOT =       -490
319081                 TA   =            9
43104
                                          MA   =            9
41086
                                          Ha   =            228
410  n
mi
                                          Hp   =            216
216

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9762080
09                 X    =         2915575
48
 Y    =        9995184
21  feet           Y    =         3079470
45  meter
 Z    =       17303135
85                 Z    =         5288304
50
 XDOT =     -16517
079990                 XDOT =       -5096
158650
 YDOT =      18926
557909  feet/sec       YDOT =        5712
171374  meter/sec
 ZDOT =      -1608
658403                 ZDOT =        -514
923652

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10507200
18                 X    =        -3202594
61
 Y    =       -9086456
47  feet           Y    =        -2769551
93  meter
 Z    =       17367656
11                 Z    =         5293661
58
 XDOT =      14070
550839                 XDOT =        4288
703896
 YDOT =     -19570
697802  feet/sec       YDOT =       -5965
148690  meter/sec
 ZDOT =      -1720
880410                 ZDOT =        -524
524349


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   19178
79884824  
00016717  00000-0  10270-3 0  9159
2 25544  51
6416 308
6395 0008138  91
6750 268
5333 15
51247010 16897


Satellite: ISS
Catalog Number: 25544
Epoch time:      19178
79884824   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       308
6395  deg
Eccentricity:     
0008138     
Arg of perigee:    91
6750  deg
Mean anomaly:     268
5333  deg
Mean motion:   15
51247010  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1689
Checksum:              340


Coasting Arc #17 (Orbit 1703)
---------------------------------------

Vector Time (GMT): 2019/179/18:02:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916289
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2644129
43                 A    =         6786487
59  meter
 Y    =       -3532202
30  meter          E    =           
0021956
 Z    =       -5175935
91                 I    =           51
30403
 XDOT =       4969
195000                 Wp   =           98
09079
 YDOT =      -5659
360805  meter/sec      RA   =          303
18067  deg
 ZDOT =       1325
412276                 TA   =          184
72965
                                          MA   =          184
75042
                                          Ha   =            228
553  n
mi
                                          Hp   =            216
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8674965
31                 X    =        -2579292
91
 Y    =      -11588590
23  feet           Y    =        -3561407
53  meter
 Z    =      -16981417
03                 Z    =        -5188623
18
 XDOT =      16303
133203                 XDOT =        5025
672135
 YDOT =     -18567
456710  feet/sec       YDOT =       -5603
476193  meter/sec
 ZDOT =       4348
465473                 ZDOT =        1349
687197

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9754134
43                 X    =         2973060
18
 Y    =       10604914
65  feet           Y    =         3232377
99  meter
 Z    =      -17038533
32                 Z    =        -5193344
96
 XDOT =     -13415
338441                 XDOT =       -4088
995157
 YDOT =      19493
901130  feet/sec       YDOT =        5941
741064  meter/sec
 ZDOT =       4459
169980                 ZDOT =        1359
155010


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   19179
76518327  
00016717  00000-0  10270-3 0  9160
2 25544  51
6423 303
8432 0008092  94
9665 265
2410 15
51209277 17045


Satellite: ISS
Catalog Number: 25544
Epoch time:      19179
76518327   =   yrday
fracday
Element set:     916
Inclination:       51
6423  deg
RA of node:       303
8432  deg
Eccentricity:     
0008092     
Arg of perigee:    94
9665  deg
Mean anomaly:     265
2410  deg
Mean motion:   15
51209277  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1704
Checksum:              319
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