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

 
Date: February 20th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


050/05:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 214 5

054/08:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 2
000/00:00:00 000 0 0 0 0 214 1

057/02:24:38 197 -2 8 2 8 2 8
N/A -0 0 -0 3 224 4
000/00:07:16 395 -0 3 -0 2 215 6

057/14:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 6

060/17:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 224 6
000/00:00:00 000 0 0 0 0 215 5

061/07:48:58 000 0 0 0 0 0 0
N/A 0 0 0 0 224 3
000/00:00:00 000 0 0 0 0 215 5

062/10:55:42 000 0 0 0 0 0 0
N/A 0 0 0 0 224 4
000/00:00:00 000 0 0 0 0 215 5

Coasting Arc #1 (Orbit 3680)
---------------------------------------

Vector Time (GMT): 2019/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1900558
39                 A    =         6788364
37  meter
 Y    =        5865565
19  meter          E    =           
0008014
 Z    =       -2849572
46                 I    =           51
34539
 XDOT =      -5730
497433                 Wp   =           74
17926
 YDOT =       -589
862092  meter/sec      RA   =          230
35213  deg
 ZDOT =      -5045
935751                 TA   =          138
31475
                                          MA   =          138
25365
                                          Ha   =            224
051  n
mi
                                          Hp   =            214
515

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6235427
78                 X    =         1848667
95
 Y    =       19243980
30  feet           Y    =         5886528
34  meter
 Z    =       -9348991
03                 Z    =        -2840466
75
 XDOT =     -18800
844595                 XDOT =       -5698
965922
 YDOT =      -1935
243085  feet/sec       YDOT =        -653
768363  meter/sec
 ZDOT =     -16554
907320                 ZDOT =       -5073
694913

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5103671
76                 X    =        -1555599
15
 Y    =       19593906
34  feet           Y    =         5972222
65  meter
 Z    =       -9308401
55                 Z    =        -2837200
79
 XDOT =     -13248
271307                 XDOT =       -4038
073094
 YDOT =     -11359
744957  feet/sec       YDOT =       -3462
450263  meter/sec
 ZDOT =     -16680
150836                 ZDOT =       -5084
109975


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   19049
52645881  
00016717  00000-0  10270-3 0  9009
2 25544  51
6347 231
2748 0005718  39
0062 321
1502 15
53287921 36811


Satellite: ISS
Catalog Number: 25544
Epoch time:      19049
52645881   =   yrday
fracday
Element set:     900
Inclination:       51
6347  deg
RA of node:       231
2748  deg
Eccentricity:     
0005718     
Arg of perigee:    39
0062  deg
Mean anomaly:     321
1502  deg
Mean motion:   15
53287921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3681
Checksum:              304


Coasting Arc #2 (Orbit 3692)
---------------------------------------

Vector Time (GMT): 2019/050/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2506581
09                 A    =         6779922
77  meter
 Y    =       -3467036
99  meter          E    =           
0007015
 Z    =        5253805
86                 I    =           51
33749
 XDOT =       5645
718657                 Wp   =           66
01658
 YDOT =       5147
652613  meter/sec      RA   =          226
59465  deg
 ZDOT =        705
478539                 TA   =           17
23284
                                          MA   =           17
20904
                                          Ha   =            223
911  n
mi
                                          Hp   =            214
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8223691
24                 X    =         2519644
90
 Y    =      -11374793
26  feet           Y    =        -3438933
32  meter
 Z    =       17236895
88                 Z    =         5266013
43
 XDOT =      18522
699007                 XDOT =        5584
309839
 YDOT =      16888
624057  feet/sec       YDOT =        5210
443661  meter/sec
 ZDOT =       2314
562136                 ZDOT =         732
753047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5267885
36                 X    =         1605651
46
 Y    =       12936441
52  feet           Y    =         3943027
38  meter
 Z    =       17292294
92                 Z    =         5270691
49
 XDOT =     -23227
979145                 XDOT =       -7079
888043
 YDOT =       6209
824184  feet/sec       YDOT =        1892
754411  meter/sec
 ZDOT =       2437
242771                 ZDOT =         742
871597


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   19050
29850955  
00016717  00000-0  10270-3 0  9016
2 25544  51
6385 227
4343 0005661  40
0533 320
1036 15
53305162 36935


Satellite: ISS
Catalog Number: 25544
Epoch time:      19050
29850955   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:       227
4343  deg
Eccentricity:     
0005661     
Arg of perigee:    40
0533  deg
Mean anomaly:     320
1036  deg
Mean motion:   15
53305162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3693
Checksum:              285


Coasting Arc #3 (Orbit 3707)
---------------------------------------

Vector Time (GMT): 2019/051/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3550031
96                 A    =         6780051
45  meter
 Y    =        2454612
36  meter          E    =           
0018525
 Z    =       -5244515
48                 I    =           51
36283
 XDOT =      -5177
973961                 Wp   =           82
51417
 YDOT =      -5563
136145  meter/sec      RA   =          221
58331  deg
 ZDOT =        906
376870                 TA   =          196
17616
                                          MA   =          196
23537
                                          Ha   =            224
119  n
mi
                                          Hp   =            214
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11647086
50                 X    =        -3551742
08
 Y    =        8053190
17  feet           Y    =         2414903
42  meter
 Z    =      -17206415
61                 Z    =        -5261764
06
 XDOT =     -16988
103548                 XDOT =       -5119
783116
 YDOT =     -18251
759006  feet/sec       YDOT =       -5620
714424  meter/sec
 ZDOT =       2973
677396                 ZDOT =         881
366748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -871361
47                 X    =         -265590
98
 Y    =      -14037683
58  feet           Y    =        -4278685
96  meter
 Z    =      -17284484
45                 Z    =        -5268310
86
 XDOT =      23413
727966                 XDOT =        7136
504284
 YDOT =      -4955
757439  feet/sec       YDOT =       -1510
514867  meter/sec
 ZDOT =       2861
227271                 ZDOT =         872
102072


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   19051
26357124  
00016717  00000-0  10270-3 0  9025
2 25544  51
6398 222
6292 0005800  43
3373 316
8234 15
53290395 37082


Satellite: ISS
Catalog Number: 25544
Epoch time:      19051
26357124   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       222
6292  deg
Eccentricity:     
0005800     
Arg of perigee:    43
3373  deg
Mean anomaly:     316
8234  deg
Mean motion:   15
53290395  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3708
Checksum:              301


Coasting Arc #4 (Orbit 3723)
---------------------------------------

Vector Time (GMT): 2019/052/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4543809
91                 A    =         6781681
46  meter
 Y    =       -1423631
63  meter          E    =           
0012773
 Z    =        4822916
97                 I    =           51
39422
 XDOT =       4437
072370                 Wp   =           53
78969
 YDOT =       5749
393736  meter/sec      RA   =          216
57610  deg
 ZDOT =      -2471
193808                 TA   =           60
61837
                                          MA   =           60
49089
                                          Ha   =            224
008  n
mi
                                          Hp   =            214
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14907512
83                 X    =         4535965
18
 Y    =       -4670707
43  feet           Y    =        -1372862
92  meter
 Z    =       15823218
41                 Z    =         4844969
65
 XDOT =      14557
324047                 XDOT =        4384
454649
 YDOT =      18862
840342  feet/sec       YDOT =        5798
717715  meter/sec
 ZDOT =      -8107
591233                 ZDOT =       -2449
769107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3458933
19                 X    =        -1054282
84
 Y    =       15130131
13  feet           Y    =         4611663
97  meter
 Z    =       15922895
48                 Z    =         4853298
54
 XDOT =     -22558
762728                 XDOT =       -6875
910880
 YDOT =       3315
018886  feet/sec       YDOT =        1010
417756  meter/sec
 ZDOT =      -8011
320813                 ZDOT =       -2441
850584


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   19052
29296672  
00016717  00000-0  10270-3 0  9030
2 25544  51
6398 217
5041 0005851  45
9800 314
1834 15
53320976 37240


Satellite: ISS
Catalog Number: 25544
Epoch time:      19052
29296672   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       217
5041  deg
Eccentricity:     
0005851     
Arg of perigee:    45
9800  deg
Mean anomaly:     314
1834  deg
Mean motion:   15
53320976  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3724
Checksum:              314


Coasting Arc #5 (Orbit 3738)
---------------------------------------

Vector Time (GMT): 2019/053/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5401936
78                 A    =         6784611
57  meter
 Y    =         501472
02  meter          E    =           
0011522
 Z    =       -4083170
19                 I    =           51
43141
 XDOT =      -3415
365952                 Wp   =           83
77603
 YDOT =      -5684
780701  meter/sec      RA   =          211
57666  deg
 ZDOT =       3830
830219                 TA   =          225
94894
                                          MA   =          226
04390
                                          Ha   =            224
159  n
mi
                                          Hp   =            214
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17722889
69                 X    =        -5387309
51
 Y    =        1645249
41  feet           Y    =          441145
12  meter
 Z    =      -13396227
66                 Z    =        -4109374
79
 XDOT =     -11205
268870                 XDOT =       -3370
150981
 YDOT =     -18650
855319  feet/sec       YDOT =       -5722
720470  meter/sec
 ZDOT =      12568
340613                 ZDOT =        3814
350425

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7223880
57                 X    =         2201838
80
 Y    =      -16169048
01  feet           Y    =        -4928325
83  meter
 Z    =      -13514585
30                 Z    =        -4119245
60
 XDOT =      20610
950139                 XDOT =        6282
217602
 YDOT =      -1206
089905  feet/sec       YDOT =        -367
616203  meter/sec
 ZDOT =      12494
374092                 ZDOT =        3808
285223


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   19053
25802585  
00016717  00000-0  10270-3 0  9044
2 25544  51
6401 212
6996 0005776  49
2181 310
9472 15
53282192 37390


Satellite: ISS
Catalog Number: 25544
Epoch time:      19053
25802585   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       212
6996  deg
Eccentricity:     
0005776     
Arg of perigee:    49
2181  deg
Mean anomaly:     310
9472  deg
Mean motion:   15
53282192  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3739
Checksum:              318


Coasting Arc #6 (Orbit 3754)
---------------------------------------

Vector Time (GMT): 2019/054/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6070888
97                 A    =         6787855
07  meter
 Y    =         365986
43  meter          E    =           
0017833
 Z    =        3001251
09                 I    =           51
47184
 XDOT =       2127
329672                 Wp   =           83
74409
 YDOT =       5465
282170  meter/sec      RA   =          206
58632  deg
 ZDOT =      -4942
377941                 TA   =           61
80715
                                          MA   =           61
62716
                                          Ha   =            224
211  n
mi
                                          Hp   =            214
114

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19917614
73                 X    =         6051767
01
 Y    =        1200742
89  feet           Y    =          433768
75  meter
 Z    =        9846624
31                 Z    =         3030694
27
 XDOT =       6979
428059                 XDOT =        2090
064209
 YDOT =      17930
715780  feet/sec       YDOT =        5488
862579  meter/sec
 ZDOT =     -16215
150724                 ZDOT =       -4932
135402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10503242
46                 X    =        -3201388
30
 Y    =       16887855
38  feet           Y    =         5147418
32  meter
 Z    =        9979549
52                 Z    =         3041766
70
 XDOT =     -17910
747575                 XDOT =       -5459
195861
 YDOT =      -1532
412823  feet/sec       YDOT =        -467
079429  meter/sec
 ZDOT =     -16169
318742                 ZDOT =       -4928
408353


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   19054
28741967  
00016717  00000-0  10270-3 0  9055
2 25544  51
6408 207
5747 0005871  53
5163 306
6529 15
53288711 37554


Satellite: ISS
Catalog Number: 25544
Epoch time:      19054
28741967   =   yrday
fracday
Element set:     905
Inclination:       51
6408  deg
RA of node:       207
5747  deg
Eccentricity:     
0005871     
Arg of perigee:    53
5163  deg
Mean anomaly:     306
6529  deg
Mean motion:   15
53288711  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3755
Checksum:              333


Coasting Arc #7 (Orbit 3755)
---------------------------------------

Vector Time (GMT): 2019/054/08:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2186036
34                 A    =         6779801
54  meter
 Y    =        3636457
46  meter          E    =           
0019581
 Z    =       -5304702
70                 I    =           51
44543
 XDOT =      -6746
984757                 Wp   =           81
82737
 YDOT =      -3597
802561  meter/sec      RA   =          206
17047  deg
 ZDOT =        317
774178                 TA   =          191
19453
                                          MA   =          191
23815
                                          Ha   =            224
196  n
mi
                                          Hp   =            214
102

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7172035
25                 X    =        -2200770
84
 Y    =       11930634
72  feet           Y    =         3611928
75  meter
 Z    =      -17403880
26                 Z    =        -5315357
65
 XDOT =     -22135
776762                 XDOT =       -6707
795214
 YDOT =     -11803
814176  feet/sec       YDOT =       -3673
032904  meter/sec
 ZDOT =       1042
566200                 ZDOT =         285
095888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12287409
14                 X    =        -3745202
31
 Y    =       -6411781
07  feet           Y    =        -1954310
87  meter
 Z    =      -17452272
71                 Z    =        -5319452
72
 XDOT =      10143
287184                 XDOT =        3091
673934
 YDOT =     -21842
020027  feet/sec       YDOT =       -6657
447704  meter/sec
 ZDOT =        895
278939                 ZDOT =         272
881021


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   19054
35175494  
00016717  00000-0  10270-3 0  9060
2 25544  51
6387 207
2522 0005720  52
6294 307
5379 15
53299271 37563


Satellite: ISS
Catalog Number: 25544
Epoch time:      19054
35175494   =   yrday
fracday
Element set:     906
Inclination:       51
6387  deg
RA of node:       207
2522  deg
Eccentricity:     
0005720     
Arg of perigee:    52
6294  deg
Mean anomaly:     307
5379  deg
Mean motion:   15
53299271  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3756
Checksum:              327


Coasting Arc #8 (Orbit 3771)
---------------------------------------

Vector Time (GMT): 2019/055/08:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3471536
46                 A    =         6780945
73  meter
 Y    =       -2941796
14  meter          E    =           
0011344
 Z    =        5021117
44                 I    =           51
47968
 XDOT =       6225
746782                 Wp   =           56
44229
 YDOT =       4051
128003  meter/sec      RA   =          201
16799  deg
 ZDOT =      -1921
623527                 TA   =           52
27963
                                          MA   =           52
17686
                                          Ha   =            224
138  n
mi
                                          Hp   =            214
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11389555
33                 X    =         3479784
94
 Y    =       -9651562
15  feet           Y    =        -2902928
44  meter
 Z    =       16473482
41                 Z    =         5038000
94
 XDOT =      20425
678420                 XDOT =        6189
317286
 YDOT =      13291
102371  feet/sec       YDOT =        4120
544797  meter/sec
 ZDOT =      -6304
539129                 ZDOT =       -1891
470376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10419393
30                 X    =         3175831
08
 Y    =       10572867
68  feet           Y    =         3222610
07  meter
 Z    =       16549953
39                 Z    =         5044425
79
 XDOT =     -11048
142544                 XDOT =       -3367
473847
 YDOT =      20591
192877  feet/sec       YDOT =        6276
195589  meter/sec
 ZDOT =      -6168
672090                 ZDOT =       -1880
211253


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   19055
38114524  
00016717  00000-0  10270-3 0  9072
2 25544  51
6387 202
1269 0005731  56
3831 303
7867 15
53296011 37722


Satellite: ISS
Catalog Number: 25544
Epoch time:      19055
38114524   =   yrday
fracday
Element set:     907
Inclination:       51
6387  deg
RA of node:       202
1269  deg
Eccentricity:     
0005731     
Arg of perigee:    56
3831  deg
Mean anomaly:     303
7867  deg
Mean motion:   15
53296011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3772
Checksum:              308


Coasting Arc #9 (Orbit 3786)
---------------------------------------

Vector Time (GMT): 2019/056/08:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900744
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4630985
20                 A    =         6783443
62  meter
 Y    =        2300851
65  meter          E    =           
0013579
 Z    =       -4402425
46                 I    =           51
51768
 XDOT =      -5342
124802                 Wp   =           92
26189
 YDOT =      -4332
997673  meter/sec      RA   =          196
17190  deg
 ZDOT =       3363
373425                 TA   =          211
83258
                                          MA   =          211
91473
                                          Ha   =            224
254  n
mi
                                          Hp   =            213
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15193521
00                 X    =        -4634985
49
 Y    =        7548725
89  feet           Y    =         2249042
07  meter
 Z    =      -14443653
10                 Z    =        -4424930
67
 XDOT =     -17526
656174                 XDOT =       -5309
612179
 YDOT =     -14215
871632  feet/sec       YDOT =       -4392
555025  meter/sec
 ZDOT =      11034
689713                 ZDOT =        3337
502942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8838868
84                 X    =        -2694087
22
 Y    =      -14378769
62  feet           Y    =        -4382648
98  meter
 Z    =      -14545474
89                 Z    =        -4433460
75
 XDOT =      11573
220507                 XDOT =        3527
517611
 YDOT =     -18131
092610  feet/sec       YDOT =       -5526
357028  meter/sec
 ZDOT =      10918
169169                 ZDOT =        3327
857963


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   19056
34619830  
00016717  00000-0  10270-3 0  9080
2 25544  51
6368 197
3218 0005724  60
8763 299
2962 15
53295329 37878


Satellite: ISS
Catalog Number: 25544
Epoch time:      19056
34619830   =   yrday
fracday
Element set:     908
Inclination:       51
6368  deg
RA of node:       197
3218  deg
Eccentricity:     
0005724     
Arg of perigee:    60
8763  deg
Mean anomaly:     299
2962  deg
Mean motion:   15
53295329  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3787
Checksum:              352


Coasting Arc #10 (Orbit 3798)
---------------------------------------

Vector Time (GMT): 2019/057/02:28:16
395
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1496900
10                 A    =         6781411
57  meter
 Y    =        3980623
32  meter          E    =           
0017772
 Z    =       -5297466
64                 I    =           51
53262
 XDOT =      -7353
510186                 Wp   =           86
36807
 YDOT =      -2051
202599  meter/sec      RA   =          192
36900  deg
 ZDOT =        539
226238                 TA   =          188
77927
                                          MA   =          188
81040
                                          Ha   =            224
363  n
mi
                                          Hp   =            215
585

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4911089
57                 X    =        -1515569
46
 Y    =       13059787
79  feet           Y    =         3963779
25  meter
 Z    =      -17380139
89                 Z    =        -5304783
50
 XDOT =     -24125
689586                 XDOT =       -7332
645765
 YDOT =      -6729
667320  feet/sec       YDOT =       -2133
317995  meter/sec
 ZDOT =       1769
114955                 ZDOT =         503
556862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2013237
45                 X    =          613634
78
 Y    =      -13764568
11  feet           Y    =        -4195440
36  meter
 Z    =      -17413490
74                 Z    =        -5307631
98
 XDOT =      24000
506705                 XDOT =        7315
354444
 YDOT =       1486
957930  feet/sec       YDOT =         453
224777  meter/sec
 ZDOT =       1608
147134                 ZDOT =         490
163246


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   19057
11824273  
00016717  00000-0  10270-3 0  9096
2 25544  51
6392 193
4790 0003766  53
3997 306
7501 15
52765296 37997


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
11824273   =   yrday
fracday
Element set:     909
Inclination:       51
6392  deg
RA of node:       193
4790  deg
Eccentricity:     
0003766     
Arg of perigee:    53
3997  deg
Mean anomaly:     306
7501  deg
Mean motion:   15
52765296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3799
Checksum:              347


Coasting Arc #11 (Orbit 3806)
---------------------------------------

Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2331713
02                 A    =         6781960
38  meter
 Y    =        3754178
94  meter          E    =           
0016572
 Z    =       -5158886
37                 I    =           51
55214
 XDOT =      -7115
502873                 Wp   =           93
35836
 YDOT =      -2408
776561  meter/sec      RA   =          189
78711  deg
 ZDOT =       1466
300702                 TA   =          190
78283
                                          MA   =          190
81841
                                          Ha   =            224
280  n
mi
                                          Hp   =            215
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7649977
09                 X    =        -2348461
33
 Y    =       12316860
04  feet           Y    =         3728010
19  meter
 Z    =      -16925480
21                 Z    =        -5170253
68
 XDOT =     -23344
825698                 XDOT =       -7095
160801
 YDOT =      -7902
810241  feet/sec       YDOT =       -2488
233270  meter/sec
 ZDOT =       4810
697842                 ZDOT =        1431
786230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3292996
86                 X    =        -1003705
44
 Y    =       14058195
38  feet           Y    =         4284937
95  meter
 Z    =      -16977113
58                 Z    =        -5174624
22
 XDOT =     -23650
358923                 XDOT =       -7208
629400
 YDOT =         69
245417  feet/sec       YDOT =          21
106003  meter/sec
 ZDOT =       4654
962094                 ZDOT =        1418
832446


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   19057
63311040  
00016717  00000-0  10270-3 0  9108
2 25544  51
6399 190
9153 0003457  59
5158 300
6335 15
52777616 38070


Satellite: ISS
Catalog Number: 25544
Epoch time:      19057
63311040   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       190
9153  deg
Eccentricity:     
0003457     
Arg of perigee:    59
5158  deg
Mean anomaly:     300
6335  deg
Mean motion:   15
52777616  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3807
Checksum:              312


Coasting Arc #12 (Orbit 3822)
---------------------------------------

Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3477277
32                 A    =         6783769
54  meter
 Y    =       -3441728
43  meter          E    =           
0011361
 Z    =        4692830
86                 I    =           51
59180
 XDOT =       6568
945356                 Wp   =           62
86623
 YDOT =       2788
692499  meter/sec      RA   =          184
79921  deg
 ZDOT =      -2811
887790                 TA   =           55
08041
                                          MA   =           54
97371
                                          Ha   =            224
194  n
mi
                                          Hp   =            215
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11408390
16                 X    =         3492710
45
 Y    =      -11291759
95  feet           Y    =        -3402756
59  meter
 Z    =       15396426
70                 Z    =         4709759
54
 XDOT =      21551
657993                 XDOT =        6550
931575
 YDOT =       9149
253605  feet/sec       YDOT =        2862
050189  meter/sec
 ZDOT =      -9225
353642                 ZDOT =       -2780
022680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6946390
82                 X    =         2117259
92
 Y    =      -14388669
99  feet           Y    =        -4385666
61  meter
 Z    =       15473170
15                 Z    =         4716222
26
 XDOT =      22371
917659                 XDOT =        6818
960502
 YDOT =        998
145492  feet/sec       YDOT =         304
234746  meter/sec
 ZDOT =      -9081
592832                 ZDOT =       -2768
069495


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   19058
66284614  
00016717  00000-0  10270-3 0  9119
2 25544  51
6403 185
7920 0003518  61
1827 298
9678 15
52797260 38234


Satellite: ISS
Catalog Number: 25544
Epoch time:      19058
66284614   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       185
7920  deg
Eccentricity:     
0003518     
Arg of perigee:    61
1827  deg
Mean anomaly:     298
9678  deg
Mean motion:   15
52797260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3823
Checksum:              337


Coasting Arc #13 (Orbit 3837)
---------------------------------------

Vector Time (GMT): 2019/059/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4485446
59                 A    =         6786374
30  meter
 Y    =        3174217
14  meter          E    =           
0009977
 Z    =       -3991700
32                 I    =           51
63248
 XDOT =      -5747
143349                 Wp   =           94
74459
 YDOT =      -3130
160470  meter/sec      RA   =          179
81988  deg
 ZDOT =       3976
684245                 TA   =          216
69934
                                          MA   =          216
76771
                                          Ha   =            224
315  n
mi
                                          Hp   =            215
452

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14716032
12                 X    =        -4501219
11
 Y    =       10414098
22  feet           Y    =         3123969
38  meter
 Z    =      -13096129
66                 Z    =        -4013526
99
 XDOT =     -18855
457182                 XDOT =       -5731
030046
 YDOT =     -10269
555348  feet/sec       YDOT =       -3194
338773  meter/sec
 ZDOT =      13046
864320                 ZDOT =        3948
806559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10119129
80                 X    =        -3084310
76
 Y    =       14833035
10  feet           Y    =         4521109
10  meter
 Z    =      -13194996
67                 Z    =        -4021834
98
 XDOT =     -20244
173809                 XDOT =       -6170
424177
 YDOT =      -2338
920971  feet/sec       YDOT =        -712
903112  meter/sec
 ZDOT =      12921
124667                 ZDOT =        3938
358798


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   19059
62822340  
00016717  00000-0  10270-3 0  9121
2 25544  51
6390 180
9905 0003568  66
8494 293
3034 15
52793528 38380


Satellite: ISS
Catalog Number: 25544
Epoch time:      19059
62822340   =   yrday
fracday
Element set:     912
Inclination:       51
6390  deg
RA of node:       180
9905  deg
Eccentricity:     
0003568     
Arg of perigee:    66
8494  deg
Mean anomaly:     293
3034  deg
Mean motion:   15
52793528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3838
Checksum:              335


Coasting Arc #14 (Orbit 3853)
---------------------------------------

Vector Time (GMT): 2019/060/14:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5342313
96                 A    =         6789241
75  meter
 Y    =       -2883081
82  meter          E    =           
0016270
 Z    =        3025702
13                 I    =           51
67577
 XDOT =       4702
680716                 Wp   =           90
48513
 YDOT =       3500
467786  meter/sec      RA   =          174
84728  deg
 ZDOT =      -4944
938409                 TA   =           54
86177
                                          MA   =           54
70940
                                          Ha   =            224
282  n
mi
                                          Hp   =            215
505

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17527276
76                 X    =         5359459
47
 Y    =       -9458929
84  feet           Y    =        -2823244
31  meter
 Z    =        9926844
27                 Z    =         3051694
33
 XDOT =      15428
742508                 XDOT =        4687
207251
 YDOT =      11484
474363  feet/sec       YDOT =        3552
969684  meter/sec
 ZDOT =     -16223
551211                 ZDOT =       -4922
132782

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12848426
31                 X    =         3916200
34
 Y    =      -15140818
74  feet           Y    =        -4614921
55  meter
 Z    =       10044529
40                 Z    =         3061572
56
 XDOT =      17537
419553                 XDOT =        5345
405480
 YDOT =       4138
391740  feet/sec       YDOT =        1261
381802  meter/sec
 ZDOT =     -16120
742036                 ZDOT =       -4913
602173


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   19060
65795605  
00016717  00000-0  10270-3 0  9130
2 25544  51
6395 175
8675 0003563  67
8809 292
2721 15
52794988 38548


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
65795605   =   yrday
fracday
Element set:     913
Inclination:       51
6395  deg
RA of node:       175
8675  deg
Eccentricity:     
0003563     
Arg of perigee:    67
8809  deg
Mean anomaly:     292
2721  deg
Mean motion:   15
52794988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3854
Checksum:              362


Coasting Arc #15 (Orbit 3855)
---------------------------------------

Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6096829
50                 A    =         6790587
04  meter
 Y    =       -1454657
05  meter          E    =           
0017641
 Z    =        2590520
46                 I    =           51
68217
 XDOT =       3316
488588                 Wp   =           74
72513
 YDOT =      -4499
566329  meter/sec      RA   =          174
35631  deg
 ZDOT =       5253
483229                 TA   =          314
40734
                                          MA   =          314
55162
                                          Ha   =            224
643  n
mi
                                          Hp   =            215
481

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20002721
45                 X    =        -6092693
03
 Y    =       -4772496
89  feet           Y    =        -1522812
80  meter
 Z    =        8499082
88                 Z    =         2560915
10
 XDOT =      10880
868070                 XDOT =        3341
039558
 YDOT =     -14762
356722  feet/sec       YDOT =       -4462
341498  meter/sec
 ZDOT =      17235
837367                 ZDOT =        5269
653003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14104673
14                 X    =        -4299104
37
 Y    =       15039896
08  feet           Y    =         4584160
33  meter
 Z    =        8365388
42                 Z    =         2549770
39
 XDOT =      -6368
107771                 XDOT =       -1940
999249
 YDOT =     -15646
620799  feet/sec       YDOT =       -4769
090020  meter/sec
 ZDOT =      17309
251380                 ZDOT =        5275
859821


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   19060
78667435  
00016717  00000-0  10270-3 0  9144
2 25544  51
6386 175
2277 0004020  68
1329 292
0250 15
52751267 38560


Satellite: ISS
Catalog Number: 25544
Epoch time:      19060
78667435   =   yrday
fracday
Element set:     914
Inclination:       51
6386  deg
RA of node:       175
2277  deg
Eccentricity:     
0004020     
Arg of perigee:    68
1329  deg
Mean anomaly:     292
0250  deg
Mean motion:   15
52751267  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3856
Checksum:              318


Coasting Arc #16 (Orbit 3864)
---------------------------------------

Vector Time (GMT): 2019/061/07:48:58
000
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4360202
40                 A    =         6787348
17  meter
 Y    =       -3631924
83  meter          E    =           
0015109
 Z    =        3712829
83                 I    =           51
68964
 XDOT =       5810
091522                 Wp   =           81
15357
 YDOT =       2555
529681  meter/sec      RA   =          171
33183  deg
 ZDOT =      -4306
063344                 TA   =           54
59940
                                          MA   =           54
45836
                                          Ha   =            224
322  n
mi
                                          Hp   =            215
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14305126
00                 X    =         4382457
09
 Y    =      -11915763
89  feet           Y    =        -3583041
36  meter
 Z    =       12181200
24                 Z    =         3734063
85
 XDOT =      19061
980059                 XDOT =        5801
999052
 YDOT =       8384
283731  feet/sec       YDOT =        2620
456690  meter/sec
 ZDOT =     -14127
504410                 ZDOT =       -4277
860529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13375913
28                 X    =         4076978
37
 Y    =       12858964
69  feet           Y    =         3919412
44  meter
 Z    =       12277445
55                 Z    =         3742165
40
 XDOT =      -5336
201110                 XDOT =       -1626
474098
 YDOT =      18971
388042  feet/sec       YDOT =        5782
479075  meter/sec
 ZDOT =     -14000
218845                 ZDOT =       -4267
266704


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   19061
36589592  
00016717  00000-0  10270-3 0  9157
2 25544  51
6366 172
3430 0003566  70
0388 290
1148 15
52770346 38652


Satellite: ISS
Catalog Number: 25544
Epoch time:      19061
36589592   =   yrday
fracday
Element set:     915
Inclination:       51
6366  deg
RA of node:       172
3430  deg
Eccentricity:     
0003566     
Arg of perigee:    70
0388  deg
Mean anomaly:     290
1148  deg
Mean motion:   15
52770346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3865
Checksum:              323


Coasting Arc #17 (Orbit 3879)
---------------------------------------

Vector Time (GMT): 2019/062/07:48:58
000
Vector Time (MET): N/A
Weight (LBS)     : 900452
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5162233
80                 A    =         6790007
52  meter
 Y    =        3467094
47  meter          E    =           
0008507
 Z    =       -2728551
04                 I    =           51
73199
 XDOT =      -4766
244574                 Wp   =           66
73079
 YDOT =      -3040
463428  meter/sec      RA   =          166
36450  deg
 ZDOT =       5170
060662                 TA   =          262
48727
                                          MA   =          262
58392
                                          Ha   =            224
457  n
mi
                                          Hp   =            215
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16936462
59                 X    =        -5187366
69
 Y    =       11374981
85  feet           Y    =         3409226
04  meter
 Z    =       -8951939
09                 Z    =        -2753687
93
 XDOT =     -15637
285349                 XDOT =       -4757
003715
 YDOT =      -9975
273715  feet/sec       YDOT =       -3093
710869  meter/sec
 ZDOT =      16962
141281                 ZDOT =        5146
931238

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13389500
21                 X    =        -4081119
67
 Y    =      -15326553
66  feet           Y    =        -4671533
56  meter
 Z    =       -9065827
46                 Z    =        -2763264
21
 XDOT =       6815
175933                 XDOT =        2077
265624
 YDOT =     -15894
601245  feet/sec       YDOT =       -4844
674460  meter/sec
 ZDOT =      16857
807495                 ZDOT =        5138
259724


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   19062
33126677  
00016717  00000-0  10270-3 0  9167
2 25544  51
6372 167
5402 0003827  76
0266 284
1311 15
52783012 38801


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
33126677   =   yrday
fracday
Element set:     916
Inclination:       51
6372  deg
RA of node:       167
5402  deg
Eccentricity:     
0003827     
Arg of perigee:    76
0266  deg
Mean anomaly:     284
1311  deg
Mean motion:   15
52783012  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3880
Checksum:              302


Coasting Arc #18 (Orbit 3881)
---------------------------------------

Vector Time (GMT): 2019/062/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935669
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5498450
13                 A    =         6791008
58  meter
 Y    =        3261371
63  meter          E    =           
0009152
 Z    =       -2288611
95                 I    =           51
74211
 XDOT =      -4238
357357                 Wp   =           57
45091
 YDOT =      -3345
106167  meter/sec      RA   =          165
72334  deg
 ZDOT =       5436
485864                 TA   =          277
13040
                                          MA   =          277
23446
                                          Ha   =            224
438  n
mi
                                          Hp   =            215
455

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18039534
56                 X    =        -5523394
52
 Y    =       10700038
15  feet           Y    =         3199744
48  meter
 Z    =       -7508569
40                 Z    =        -2315381
55
 XDOT =     -13905
371906                 XDOT =       -4227
043243
 YDOT =     -10974
757765  feet/sec       YDOT =       -3392
438782  meter/sec
 ZDOT =      17836
239712                 ZDOT =        5415
925723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20841418
90                 X    =        -6352464
48
 Y    =       -1927501
56  feet           Y    =         -587502
48  meter
 Z    =       -7629825
27                 Z    =        -2325570
74
 XDOT =      -5028
229307                 XDOT =       -1532
604293
 YDOT =     -15603
698165  feet/sec       YDOT =       -4756
007201  meter/sec
 ZDOT =      17743
541232                 ZDOT =        5408
231367


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   19062
45998253  
00016717  00000-0  10270-3 0  9178
2 25544  51
6400 166
9003 0003694  75
8649 284
2913 15
52762522 38821


Satellite: ISS
Catalog Number: 25544
Epoch time:      19062
45998253   =   yrday
fracday
Element set:     917
Inclination:       51
6400  deg
RA of node:       166
9003  deg
Eccentricity:     
0003694     
Arg of perigee:    75
8649  deg
Mean anomaly:     284
2913  deg
Mean motion:   15
52762522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3882
Checksum:              333


Coasting Arc #19 (Orbit 3897)
---------------------------------------

Vector Time (GMT): 2019/063/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935669
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6005468
66                 A    =         6792763
40  meter
 Y    =       -2977528
17  meter          E    =           
0016572
 Z    =        1057711
54                 I    =           51
77960
 XDOT =       2977
119473                 Wp   =          115
27441
 YDOT =       3884
574199  meter/sec      RA   =          160
76587  deg
 ZDOT =      -5902
849927                 TA   =           53
28248
                                          MA   =           53
13037
                                          Ha   =            224
454  n
mi
                                          Hp   =            215
438

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19702981
17                 X    =         6033180
23
 Y    =       -9768793
21  feet           Y    =        -2910215
78  meter
 Z    =        3470182
21                 Z    =         1086950
74
 XDOT =       9767
452338                 XDOT =        2962
131900
 YDOT =      12744
666007  feet/sec       YDOT =        3917
782104  meter/sec
 ZDOT =     -19366
305534                 ZDOT =       -5888
425283

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21720960
14                 X    =         6620548
65
 Y    =        3301535
50  feet           Y    =         1006308
02  meter
 Z    =        3602597
16                 Z    =         1098071
62
 XDOT =       1026
680426                 XDOT =         312
932194
 YDOT =      14531
997159  feet/sec       YDOT =        4429
352734  meter/sec
 ZDOT =     -19301
374048                 ZDOT =       -5883
058810


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   19063
48970845  
00016717  00000-0  10270-3 0  9180
2 25544  51
6397 161
7777 0003650  82
6567 277
5000 15
52773634 38989


Satellite: ISS
Catalog Number: 25544
Epoch time:      19063
48970845   =   yrday
fracday
Element set:     918
Inclination:       51
6397  deg
RA of node:       161
7777  deg
Eccentricity:     
0003650     
Arg of perigee:    82
6567  deg
Mean anomaly:     277
5000  deg
Mean motion:   15
52773634  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3898
Checksum:              353


Coasting Arc #20 (Orbit 3912)
---------------------------------------

Vector Time (GMT): 2019/064/10:55:42
000
Vector Time (MET): N/A
Weight (LBS)     : 935669
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6247236
78                 A    =         6793228
89  meter
 Y    =        2645780
76  meter          E    =           
0015518
 Z    =         185770
13                 I    =           51
81381
 XDOT =      -1688
530471                 Wp   =           55
48120
 YDOT =      -4434
337834  meter/sec      RA   =          155
81269  deg
 ZDOT =       6022
484571                 TA   =          306
51446
                                          MA   =          306
65727
                                          Ha   =            224
454  n
mi
                                          Hp   =            215
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20496183
67                 X    =        -6277260
70
 Y    =        8680383
07  feet           Y    =         2575751
94  meter
 Z    =         609482
07                 Z    =          155350
87
 XDOT =      -5539
798133                 XDOT =       -1668
072202
 YDOT =     -14548
352475  feet/sec       YDOT =       -4453
105146  meter/sec
 ZDOT =      19758
807649                 ZDOT =        6014
332655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21844933
99                 X    =        -6658335
88
 Y    =       -4288401
03  feet           Y    =        -1307104
63  meter
 Z    =         471740
92                 Z    =          143786
63
 XDOT =       3134
625473                 XDOT =         955
433844
 YDOT =     -13635
378213  feet/sec       YDOT =       -4156
063279  meter/sec
 ZDOT =      19722
272425                 ZDOT =        6011
348635


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   19064
51943109  
00016717  00000-0  10270-3 0  9199
2 25544  51
6412 156
6554 0003710  83
3814 276
7761 15
52785667 39135


Satellite: ISS
Catalog Number: 25544
Epoch time:      19064
51943109   =   yrday
fracday
Element set:     919
Inclination:       51
6412  deg
RA of node:       156
6554  deg
Eccentricity:     
0003710     
Arg of perigee:    83
3814  deg
Mean anomaly:     276
7761  deg
Mean motion:   15
52785667  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3913
Checksum:              328
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