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

 
Date: April 18th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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


107/20:46:03 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 217 3

109/09:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 1
000/00:00:00 000 0 0 0 0 217 4

114/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 2
000/00:00:00 000 0 0 0 0 217 2

116/09:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 5

118/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 4

118/11:34:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 217 4

Coasting Arc #1 (Orbit 581)
---------------------------------------

Vector Time (GMT): 2019/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3197009
99                 A    =         6782054
96  meter
 Y    =       -2850428
47  meter          E    =           
0014323
 Z    =       -5270867
82                 I    =           51
29417
 XDOT =       4476
154759                 Wp   =           99
64607
 YDOT =      -6178
816131  meter/sec      RA   =          302
15391  deg
 ZDOT =        625
559191                 TA   =          176
36979
                                          MA   =          176
35939
                                          Ha   =            223
334  n
mi
                                          Hp   =            217
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10488877
93                 X    =        -3139295
00
 Y    =       -9351799
44  feet           Y    =        -2885857
40  meter
 Z    =      -17292873
43                 Z    =        -5286257
37
 XDOT =      14685
547109                 XDOT =        4541
876725
 YDOT =     -20271
706466  feet/sec       YDOT =       -6128
393109  meter/sec
 ZDOT =       2052
359551                 ZDOT =         647
462914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13313337
14                 X    =        -4057905
16
 Y    =       -4222279
68  feet           Y    =        -1286950
85  meter
 Z    =      -17362131
00                 Z    =        -5291977
53
 XDOT =       4660
028080                 XDOT =        1420
376559
 YDOT =     -23554
838096  feet/sec       YDOT =       -7179
514652  meter/sec
 ZDOT =       2152
026208                 ZDOT =         655
937588


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   19107
51498939  
00016717  00000-0  10270-3 0  9003
2 25544  51
6369 302
8076 0001260 201
8913 158
2185 15
52565965  5825


Satellite: ISS
Catalog Number: 25544
Epoch time:      19107
51498939   =   yrday
fracday
Element set:     900
Inclination:       51
6369  deg
RA of node:       302
8076  deg
Eccentricity:     
0001260     
Arg of perigee:   201
8913  deg
Mean anomaly:     158
2185  deg
Mean motion:   15
52565965  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             582
Checksum:              322


Coasting Arc #2 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2019/107/20:46:03
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1908313
93                 A    =         6792354
63  meter
 Y    =        6235553
02  meter          E    =           
0014035
 Z    =        1874535
65                 I    =           51
32495
 XDOT =      -5240
993928                 Wp   =          118
71763
 YDOT =         86
432376  meter/sec      RA   =          300
31867  deg
 ZDOT =      -5597
643508                 TA   =           40
55778
                                          MA   =           40
45329
                                          Ha   =            223
291  n
mi
                                          Hp   =            217
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6260872
46                 X    =        -1987005
34
 Y    =       20457851
11  feet           Y    =         6213773
08  meter
 Z    =        6150051
35                 Z    =         1865074
08
 XDOT =     -17194
861970                 XDOT =       -5214
380479
 YDOT =        283
570786  feet/sec       YDOT =          27
972260  meter/sec
 ZDOT =     -18364
972138                 ZDOT =       -5623
037838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13988883
13                 X    =         4263811
58
 Y    =      -16203876
99  feet           Y    =        -4938941
71  meter
 Z    =        6106623
20                 Z    =         1861298
75
 XDOT =      14565
494382                 XDOT =        4439
562688
 YDOT =       5578
632898  feet/sec       YDOT =        1700
367307  meter/sec
 ZDOT =     -18479
763462                 ZDOT =       -5632
631903


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   19107
90119169  
00016717  00000-0  10270-3 0  9012
2 25544  51
6396 300
8881 0001322 202
3049 157
8045 15
52585656  5887


Satellite: ISS
Catalog Number: 25544
Epoch time:      19107
90119169   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:       300
8881  deg
Eccentricity:     
0001322     
Arg of perigee:   202
3049  deg
Mean anomaly:     157
8045  deg
Mean motion:   15
52585656  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             588
Checksum:              313


Coasting Arc #3 (Orbit 602)
---------------------------------------

Vector Time (GMT): 2019/108/20:46:03
000
Vector Time (MET): N/A
Weight (LBS)     : 930220
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2347743
10                 A    =         6793772
37  meter
 Y    =       -6328731
96  meter          E    =           
0009243
 Z    =        -731535
10                 I    =           51
31246
 XDOT =       4739
441511                 Wp   =           41
55426
 YDOT =       1078
980784  meter/sec      RA   =          295
33177  deg
 ZDOT =       5925
835261                 TA   =          310
51183
                                          MA   =          310
59232
                                          Ha   =            223
349  n
mi
                                          Hp   =            217
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7702569
21                 X    =         2421891
72
 Y    =      -20763556
29  feet           Y    =        -6302063
31  meter
 Z    =       -2400049
54                 Z    =         -719949
94
 XDOT =      15549
348788                 XDOT =        4698
239029
 YDOT =       3539
963201  feet/sec       YDOT =        1131
750598  meter/sec
 ZDOT =      19441
716737                 ZDOT =        5948
757813

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15132789
27                 X    =        -4612474
17
 Y    =       16177306
33  feet           Y    =         4930842
97  meter
 Z    =       -2347025
59                 Z    =         -715373
40
 XDOT =     -11678
500823                 XDOT =       -3559
607051
 YDOT =      -8113
128159  feet/sec       YDOT =       -2472
881463  meter/sec
 ZDOT =      19545
208980                 ZDOT =        5957
379697


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   19108
86669675  
00016717  00000-0  10270-3 0  9021
2 25544  51
6387 296
0863 0001281 208
3269 151
7814 15
52525619  6035


Satellite: ISS
Catalog Number: 25544
Epoch time:      19108
86669675   =   yrday
fracday
Element set:     902
Inclination:       51
6387  deg
RA of node:       296
0863  deg
Eccentricity:     
0001281     
Arg of perigee:   208
3269  deg
Mean anomaly:     151
7814  deg
Mean motion:   15
52525619  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             603
Checksum:              330


Coasting Arc #4 (Orbit 611)
---------------------------------------

Vector Time (GMT): 2019/109/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4331397
83                 A    =         6782334
83  meter
 Y    =         448853
51  meter          E    =           
0003887
 Z    =        5198086
47                 I    =           51
26856
 XDOT =      -2088
501118                 Wp   =          140
05403
 YDOT =       7294
202842  meter/sec      RA   =          292
69807  deg
 ZDOT =       1107
037063                 TA   =          299
26081
                                          MA   =          299
29966
                                          Ha   =            223
098  n
mi
                                          Hp   =            217
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14210622
81                 X    =         4300806
93
 Y    =        1472616
50  feet           Y    =          497119
53  meter
 Z    =       17054089
47                 Z    =         5219052
74
 XDOT =      -6852
037788                 XDOT =       -2175
289194
 YDOT =      23931
111687  feet/sec       YDOT =        7270
362570  meter/sec
 ZDOT =       3632
011361                 ZDOT =        1096
680494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13542273
82                 X    =         4127685
06
 Y    =        4180633
20  feet           Y    =         1274257
00  meter
 Z    =       17148804
43                 Z    =         5226955
59
 XDOT =     -11083
803088                 XDOT =       -3378
343181
 YDOT =      21154
979738  feet/sec       YDOT =        6448
037824  meter/sec
 ZDOT =       3584
445681                 ZDOT =        1092
539043


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   19109
44599842  
00016717  00000-0  10270-3 0  9035
2 25544  51
6401 293
2065 0001146 217
6843 142
4229 15
52552829  6126


Satellite: ISS
Catalog Number: 25544
Epoch time:      19109
44599842   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:       293
2065  deg
Eccentricity:     
0001146     
Arg of perigee:   217
6843  deg
Mean anomaly:     142
4229  deg
Mean motion:   15
52552829  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             612
Checksum:              305


Coasting Arc #5 (Orbit 626)
---------------------------------------

Vector Time (GMT): 2019/110/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3961641
67                 A    =         6781875
83  meter
 Y    =       -1555274
12  meter          E    =           
0014059
 Z    =       -5292410
59                 I    =           51
25472
 XDOT =       2510
566608                 Wp   =           95
23198
 YDOT =      -7228
209558  meter/sec      RA   =          287
68636  deg
 ZDOT =        244
160668                 TA   =          177
11564
                                          MA   =          177
10752
                                          Ha   =            223
147  n
mi
                                          Hp   =            217
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12997512
04                 X    =        -3918247
69
 Y    =       -5102605
37  feet           Y    =        -1599333
56  meter
 Z    =      -17363551
81                 Z    =        -5311549
62
 XDOT =       8236
767088                 XDOT =        2590
021895
 YDOT =     -23714
598289  feet/sec       YDOT =       -7199
690373  meter/sec
 ZDOT =        801
052061                 ZDOT =         256
549550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11773306
89                 X    =        -3588503
94
 Y    =       -7304470
06  feet           Y    =        -2226402
47  meter
 Z    =      -17449893
81                 Z    =        -5318727
63
 XDOT =      11768
623457                 XDOT =        3587
076430
 YDOT =     -21023
228514  feet/sec       YDOT =       -6407
880051  meter/sec
 ZDOT =        857
786270                 ZDOT =         261
453255


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   19110
41149768  
00016717  00000-0  10270-3 0  9043
2 25544  51
6393 288
4027 0001141 225
9766 134
1292 15
52585861  6277


Satellite: ISS
Catalog Number: 25544
Epoch time:      19110
41149768   =   yrday
fracday
Element set:     904
Inclination:       51
6393  deg
RA of node:       288
4027  deg
Eccentricity:     
0001141     
Arg of perigee:   225
9766  deg
Mean anomaly:     134
1292  deg
Mean motion:   15
52585861  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             627
Checksum:              314


Coasting Arc #6 (Orbit 642)
---------------------------------------

Vector Time (GMT): 2019/111/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3598638
12                 A    =         6782712
88  meter
 Y    =        2651478
79  meter          E    =           
0003784
 Z    =        5099181
77                 I    =           51
24824
 XDOT =      -2862
414925                 Wp   =           56
71569
 YDOT =       6935
175913  meter/sec      RA   =          282
67674  deg
 ZDOT =      -1583
177686                 TA   =           48
65262
                                          MA   =           48
62007
                                          Ha   =            223
001  n
mi
                                          Hp   =            217
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11806555
51                 X    =         3543951
66
 Y    =        8699077
41  feet           Y    =         2691415
59  meter
 Z    =       16729598
99                 Z    =         5116530
04
 XDOT =      -9391
125083                 XDOT =       -2932
062965
 YDOT =      22753
201814  feet/sec       YDOT =        6902
776936  meter/sec
 ZDOT =      -5194
152514                 ZDOT =       -1597
251726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10149842
39                 X    =         3093671
96
 Y    =       10460822
16  feet           Y    =         3188458
60  meter
 Z    =       16807738
76                 Z    =         5122998
77
 XDOT =     -12116
600514                 XDOT =       -3693
139837
 YDOT =      20220
535485  feet/sec       YDOT =        6163
219216  meter/sec
 ZDOT =      -5258
464914                 ZDOT =       -1602
780106


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   19111
44136280  
00016717  00000-0  10270-3 0  9053
2 25544  51
6391 283
2811 0001167 229
0500 131
0551 15
52579332  6436


Satellite: ISS
Catalog Number: 25544
Epoch time:      19111
44136280   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       283
2811  deg
Eccentricity:     
0001167     
Arg of perigee:   229
0500  deg
Mean anomaly:     131
0551  deg
Mean motion:   15
52579332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             643
Checksum:              273


Coasting Arc #7 (Orbit 657)
---------------------------------------

Vector Time (GMT): 2019/112/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3278189
00                 A    =         6784558
24  meter
 Y    =       -3693850
79  meter          E    =           
0010011
 Z    =       -4661680
18                 I    =           51
24731
 XDOT =       3154
144724                 Wp   =          115
39956
 YDOT =      -6375
761227  meter/sec      RA   =          277
66797  deg
 ZDOT =       2834
578287                 TA   =          182
93598
                                          MA   =          182
94186
                                          Ha   =            223
086  n
mi
                                          Hp   =            217
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10755213
24                 X    =        -3213995
47
 Y    =      -12118933
05  feet           Y    =        -3730150
82  meter
 Z    =      -15294226
30                 Z    =        -4677448
75
 XDOT =      10348
243844                 XDOT =        3211
436862
 YDOT =     -20917
851793  feet/sec       YDOT =       -6340
169060  meter/sec
 ZDOT =       9299
797531                 ZDOT =        2850
039263

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8807743
15                 X    =        -2684600
11
 Y    =      -13520096
78  feet           Y    =        -4120925
50  meter
 Z    =      -15365127
79                 Z    =        -4683290
95
 XDOT =      12188
291925                 XDOT =        3714
991379
 YDOT =     -18587
049099  feet/sec       YDOT =       -5665
332565  meter/sec
 ZDOT =       9370
315141                 ZDOT =        2856
072055


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   19112
40686029  
00016717  00000-0  10270-3 0  9062
2 25544  51
6382 278
4784 0001244 232
3030 127
8009 15
52583945  6584


Satellite: ISS
Catalog Number: 25544
Epoch time:      19112
40686029   =   yrday
fracday
Element set:     906
Inclination:       51
6382  deg
RA of node:       278
4784  deg
Eccentricity:     
0001244     
Arg of perigee:   232
3030  deg
Mean anomaly:     127
8009  deg
Mean motion:   15
52583945  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             658
Checksum:              310


Coasting Arc #8 (Orbit 673)
---------------------------------------

Vector Time (GMT): 2019/113/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2969623
00                 A    =         6787036
85  meter
 Y    =        4633373
78  meter          E    =           
0009686
 Z    =        3964846
68                 I    =           51
25345
 XDOT =      -3438
442192                 Wp   =           81
16404
 YDOT =       5597
311361  meter/sec      RA   =          272
66357  deg
 ZDOT =      -3955
972834                 TA   =           50
29001
                                          MA   =           50
20467
                                          Ha   =            222
899  n
mi
                                          Hp   =            217
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9742857
61                 X    =         2898331
34
 Y    =       15201357
53  feet           Y    =         4666183
46  meter
 Z    =       13008027
17                 Z    =         3979099
13
 XDOT =     -11280
978319                 XDOT =       -3481
561221
 YDOT =      18363
882418  feet/sec       YDOT =        5558
619302  meter/sec
 ZDOT =     -12978
913498                 ZDOT =       -3972
780281

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7661235
01                 X    =         2335144
43
 Y    =       16298521
55  feet           Y    =         4967789
37  meter
 Z    =       13071992
56                 Z    =         3984343
33
 XDOT =     -12231
663592                 XDOT =       -3728
211063
 YDOT =      16246
080836  feet/sec       YDOT =        4951
805439  meter/sec
 ZDOT =     -13055
433674                 ZDOT =       -3979
296184


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   19113
43672022  
00016717  00000-0  10270-3 0  9075
2 25544  51
6392 273
3560 0001286 244
4783 115
6236 15
52605276  6743


Satellite: ISS
Catalog Number: 25544
Epoch time:      19113
43672022   =   yrday
fracday
Element set:     907
Inclination:       51
6392  deg
RA of node:       273
3560  deg
Eccentricity:     
0001286     
Arg of perigee:   244
4783  deg
Mean anomaly:     115
6236  deg
Mean motion:   15
52605276  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             674
Checksum:              302


Coasting Arc #9 (Orbit 688)
---------------------------------------

Vector Time (GMT): 2019/114/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2698070
44                 A    =         6789751
54  meter
 Y    =       -5414555
03  meter          E    =           
0003413
 Z    =       -3085043
65                 I    =           51
25999
 XDOT =       3712
789552                 Wp   =           80
31891
 YDOT =      -4615
253731  meter/sec      RA   =          267
66392  deg
 ZDOT =       4858
325724                 TA   =          244
05871
                                          MA   =          244
09388
                                          Ha   =            223
068  n
mi
                                          Hp   =            217
403

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8851937
14                 X    =        -2622337
27
 Y    =      -17764288
16  feet           Y    =        -5444303
19  meter
 Z    =      -10121534
29                 Z    =        -3097966
20
 XDOT =      12181
068085                 XDOT =        3740
523448
 YDOT =     -15141
908567  feet/sec       YDOT =       -4573
579803  meter/sec
 ZDOT =      15939
388857                 ZDOT =        4876
428429

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6794678
04                 X    =        -2071017
87
 Y    =      -18616762
11  feet           Y    =        -5674389
09  meter
 Z    =      -10179425
33                 Z    =        -3102688
84
 XDOT =      12295
239377                 XDOT =        3747
588962
 YDOT =     -13238
694361  feet/sec       YDOT =       -4035
154041  meter/sec
 ZDOT =      16021
663120                 ZDOT =        4883
402919


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   19114
40221366  
00016717  00000-0  10270-3 0  9085
2 25544  51
6373 268
5535 0001170 237
6162 122
4877 15
52582846  6897


Satellite: ISS
Catalog Number: 25544
Epoch time:      19114
40221366   =   yrday
fracday
Element set:     908
Inclination:       51
6373  deg
RA of node:       268
5535  deg
Eccentricity:     
0001170     
Arg of perigee:   237
6162  deg
Mean anomaly:     122
4877  deg
Mean motion:   15
52582846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             689
Checksum:              316


Coasting Arc #10 (Orbit 689)
---------------------------------------

Vector Time (GMT): 2019/114/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4042682
12                 A    =         6782568
83  meter
 Y    =        1853082
57  meter          E    =           
0012871
 Z    =       -5132633
36                 I    =           51
23596
 XDOT =      -1510
208952                 Wp   =           81
60701
 YDOT =      -7360
606928  meter/sec      RA   =          267
43914  deg
 ZDOT =      -1469
293478                 TA   =          174
15245
                                          MA   =          174
13741
                                          Ha   =            223
168  n
mi
                                          Hp   =            217
191

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13263392
78                 X    =        -4038171
67
 Y    =        6079667
24  feet           Y    =         1807899
85  meter
 Z    =      -16839348
30                 Z    =        -5152260
34
 XDOT =      -4954
753780                 XDOT =       -1420
651242
 YDOT =     -24148
972861  feet/sec       YDOT =       -7376
994347  meter/sec
 ZDOT =      -4820
516659                 ZDOT =       -1476
412276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11516471
56                 X    =        -3510220
53
 Y    =        8789138
07  feet           Y    =         2678929
28  meter
 Z    =      -16928246
44                 Z    =        -5159729
52
 XDOT =      -9408
132140                 XDOT =       -2867
598676
 YDOT =     -21664
310941  feet/sec       YDOT =       -6603
281975  meter/sec
 ZDOT =      -4851
986266                 ZDOT =       -1478
885414


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   19114
46658098  
00016717  00000-0  10270-3 0  9098
2 25544  51
6372 268
2325 0001076 222
6869 137
4199 15
52588548  6903


Satellite: ISS
Catalog Number: 25544
Epoch time:      19114
46658098   =   yrday
fracday
Element set:     909
Inclination:       51
6372  deg
RA of node:       268
2325  deg
Eccentricity:     
0001076     
Arg of perigee:   222
6869  deg
Mean anomaly:     137
4199  deg
Mean motion:   15
52588548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             690
Checksum:              345


Coasting Arc #11 (Orbit 705)
---------------------------------------

Vector Time (GMT): 2019/115/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4188624
16                 A    =         6781975
10  meter
 Y    =        -702896
35  meter          E    =           
0001920
 Z    =        5285995
67                 I    =           51
23509
 XDOT =       1111
320936                 Wp   =          121
84768
 YDOT =       7585
596656  meter/sec      RA   =          262
42766  deg
 ZDOT =        127
040604                 TA   =          326
92874
                                          MA   =          326
94075
                                          Ha   =            223
066  n
mi
                                          Hp   =            217
446

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13742205
24                 X    =         4170496
28
 Y    =       -2306090
40  feet           Y    =         -656157
73  meter
 Z    =       17342505
48                 Z    =         5306298
49
 XDOT =       3646
066063                 XDOT =        1025
796946
 YDOT =      24887
128138  feet/sec       YDOT =        7597
546027  meter/sec
 ZDOT =        416
799883                 ZDOT =         132
231500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12708520
37                 X    =         3873557
01
 Y    =       -5428224
74  feet           Y    =        -1654522
90  meter
 Z    =       17434352
31                 Z    =         5313990
58
 XDOT =       8967
758648                 XDOT =        2733
372836
 YDOT =      22417
800281  feet/sec       YDOT =        6832
945526  meter/sec
 ZDOT =        439
551162                 ZDOT =         133
975194


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   19115
49643898  
00016717  00000-0  10270-3 0  9106
2 25544  51
6361 263
1101 0001083 227
0482 133
0579 15
52542608  7064


Satellite: ISS
Catalog Number: 25544
Epoch time:      19115
49643898   =   yrday
fracday
Element set:     910
Inclination:       51
6361  deg
RA of node:       263
1101  deg
Eccentricity:     
0001083     
Arg of perigee:   227
0482  deg
Mean anomaly:     133
0579  deg
Mean motion:   15
52542608  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             706
Checksum:              294


Coasting Arc #12 (Orbit 720)
---------------------------------------

Vector Time (GMT): 2019/116/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4082831
17                 A    =         6781972
81  meter
 Y    =       -1183107
88  meter          E    =           
0001848
 Z    =        5283220
18                 I    =           51
24079
 XDOT =       1837
086458                 Wp   =          125
16262
 YDOT =       7440
142188  meter/sec      RA   =          257
60293  deg
 ZDOT =        245
328632                 TA   =          322
47933
                                          MA   =          322
49223
                                          Ha   =            222
995  n
mi
                                          Hp   =            217
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13395115
38                 X    =         4070094
55
 Y    =       -3881587
55  feet           Y    =        -1137522
13  meter
 Z    =       17333399
54                 Z    =         5303022
14
 XDOT =       6027
186541                 XDOT =        1752
560462
 YDOT =      24409
915315  feet/sec       YDOT =        7460
213155  meter/sec
 ZDOT =        804
883963                 ZDOT =         254
047381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13136737
56                 X    =         4004077
61
 Y    =       -4336669
99  feet           Y    =        -1321817
01  meter
 Z    =       17423030
65                 Z    =         5310539
74
 XDOT =       6544
805406                 XDOT =        1994
856688
 YDOT =      23229
513897  feet/sec       YDOT =        7080
355836  meter/sec
 ZDOT =        843
616486                 ZDOT =         257
134305


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   19116
46192637  
00016717  00000-0  10270-3 0  9115
2 25544  51
6365 258
3086 0001087 240
1379 119
9665 15
52548885  7210


Satellite: ISS
Catalog Number: 25544
Epoch time:      19116
46192637   =   yrday
fracday
Element set:     911
Inclination:       51
6365  deg
RA of node:       258
3086  deg
Eccentricity:     
0001087     
Arg of perigee:   240
1379  deg
Mean anomaly:     119
9665  deg
Mean motion:   15
52548885  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             721
Checksum:              329


Coasting Arc #13 (Orbit 735)
---------------------------------------

Vector Time (GMT): 2019/117/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4363461
18                 A    =         6782213
72  meter
 Y    =          42874
79  meter          E    =           
0013491
 Z    =       -5203938
41                 I    =           51
25115
 XDOT =      -1399
127455                 Wp   =          101
42030
 YDOT =      -7444
445660  meter/sec      RA   =          252
59180  deg
 ZDOT =       1111
660798                 TA   =          179
31068
                                          MA   =          179
30882
                                          Ha   =            223
102  n
mi
                                          Hp   =            217
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14315817
52                 X    =        -4338338
42
 Y    =         140665
31  feet           Y    =           -5779
98  meter
 Z    =      -17073288
74                 Z    =        -5225073
49
 XDOT =      -4590
313173                 XDOT =       -1321
177402
 YDOT =     -24424
034318  feet/sec       YDOT =       -7459
655846  meter/sec
 ZDOT =       3647
181095                 ZDOT =        1105
053612

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14174862
03                 X    =        -4320497
95
 Y    =         873808
24  feet           Y    =          266336
75  meter
 Z    =      -17168848
30                 Z    =        -5233064
96
 XDOT =      -5807
953492                 XDOT =       -1770
264224
 YDOT =     -23118
786942  feet/sec       YDOT =       -7046
606260  meter/sec
 ZDOT =       3617
974618                 ZDOT =        1102
758664


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   19117
42741031  
00016717  00000-0  10270-3 0  9121
2 25544  51
6373 253
5065 0001003 237
2576 122
8480 15
52600472  7362


Satellite: ISS
Catalog Number: 25544
Epoch time:      19117
42741031   =   yrday
fracday
Element set:     912
Inclination:       51
6373  deg
RA of node:       253
5065  deg
Eccentricity:     
0001003     
Arg of perigee:   237
2576  deg
Mean anomaly:     122
8480  deg
Mean motion:   15
52600472  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             736
Checksum:              277


Coasting Arc #14 (Orbit 751)
---------------------------------------

Vector Time (GMT): 2019/118/09:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 945825
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4633590
65                 A    =         6783839
63  meter
 Y    =        1057476
94  meter          E    =           
0005917
 Z    =        4837365
79                 I    =           51
26594
 XDOT =        881
424371                 Wp   =           59
77553
 YDOT =       7223
140945  meter/sec      RA   =          247
58309  deg
 ZDOT =      -2418
165163                 TA   =           54
09762
                                          MA   =           54
04271
                                          Ha   =            222
999  n
mi
                                          Hp   =            217
436

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15202069
05                 X    =         4597923
97
 Y    =        3469412
53  feet           Y    =         1109093
58  meter
 Z    =       15870622
68                 Z    =         4859787
46
 XDOT =       2891
812240                 XDOT =         812
333777
 YDOT =      23697
968979  feet/sec       YDOT =        7232
611332  meter/sec
 ZDOT =      -7933
612740                 ZDOT =       -2414
051355

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15298591
91                 X    =         4663010
81
 Y    =        2422305
96  feet           Y    =          738318
86  meter
 Z    =       15971910
04                 Z    =         4868238
18
 XDOT =       4747
086551                 XDOT =        1446
911981
 YDOT =      22322
671693  feet/sec       YDOT =        6803
950332  meter/sec
 ZDOT =      -7915
640325                 ZDOT =       -2412
687171


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   19118
45725952  
00016717  00000-0  10270-3 0  9130
2 25544  51
6360 248
3839 0001020 238
7577 121
3475 15
52563401  7521


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
45725952   =   yrday
fracday
Element set:     913
Inclination:       51
6360  deg
RA of node:       248
3839  deg
Eccentricity:     
0001020     
Arg of perigee:   238
7577  deg
Mean anomaly:     121
3475  deg
Mean motion:   15
52563401  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             752
Checksum:              305


Coasting Arc #15 (Orbit 752)
---------------------------------------

Vector Time (GMT): 2019/118/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2171610
60                 A    =         6793612
83  meter
 Y    =       -6405536
03  meter          E    =           
0011894
 Z    =         572843
86                 I    =           51
30166
 XDOT =       4719
406128                 Wp   =           50
78071
 YDOT =      -1061
315959  meter/sec      RA   =          247
38181  deg
 ZDOT =       5947
542146                 TA   =          315
42701
                                          MA   =          315
52261
                                          Ha   =            223
049  n
mi
                                          Hp   =            217
391

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7124706
69                 X    =        -2102603
24
 Y    =      -21015538
15  feet           Y    =        -6429434
65  meter
 Z    =        1879409
00                 Z    =          562462
60
 XDOT =      15483
615905                 XDOT =        4702
033380
 YDOT =      -3482
007739  feet/sec       YDOT =       -1008
637370  meter/sec
 ZDOT =      19512
933549                 ZDOT =        5970
425118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13968221
10                 X    =        -4257513
79
 Y    =      -17247471
71  feet           Y    =        -5257029
38  meter
 Z    =        1833026
46                 Z    =          558706
46
 XDOT =      11941
936231                 XDOT =        3639
902163
 YDOT =      -7559
536172  feet/sec       YDOT =       -2304
146625  meter/sec
 ZDOT =      19616
490956                 ZDOT =        5979
106443


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   19118
52162368  
00016717  00000-0  10270-3 0  9145
2 25544  51
6381 248
0637 0001135 235
6031 124
5014 15
52611332  7537


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
52162368   =   yrday
fracday
Element set:     914
Inclination:       51
6381  deg
RA of node:       248
0637  deg
Eccentricity:     
0001135     
Arg of perigee:   235
6031  deg
Mean anomaly:     124
5014  deg
Mean motion:   15
52611332  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             753
Checksum:              276


Coasting Arc #16 (Orbit 752)
---------------------------------------

Vector Time (GMT): 2019/118/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4517107
93                 A    =         6788924
95  meter
 Y    =        3770520
43  meter          E    =           
0011464
 Z    =        3375789
91                 I    =           51
28592
 XDOT =      -1509
191715                 Wp   =           93
63635
 YDOT =       5942
867879  meter/sec      RA   =          247
23136  deg
 ZDOT =      -4605
479259                 TA   =           46
73755
                                          MA   =           46
64195
                                          Ha   =            223
001  n
mi
                                          Hp   =            217
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14819907
89                 X    =         4458211
42
 Y    =       12370473
84  feet           Y    =         3820704
59  meter
 Z    =       11075426
21                 Z    =         3397589
32
 XDOT =      -4951
416387                 XDOT =       -1553
163471
 YDOT =      19497
598029  feet/sec       YDOT =        5925
745161  meter/sec
 ZDOT =     -15109
840089                 ZDOT =       -4612
917189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18887398
79                 X    =         5756879
15
 Y    =        3706579
69  feet           Y    =         1129765
49  meter
 Z    =       11173665
15                 Z    =         3405733
14
 XDOT =       5444
355152                 XDOT =        1659
439450
 YDOT =      18035
818738  feet/sec       YDOT =        5497
317551  meter/sec
 ZDOT =     -15143
986457                 ZDOT =       -4615
887072


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   19118
52162464  
00016717  00000-0  10270-3 0  9153
2 25544  51
6379 248
0637 0001183 235
9063 124
1976 15
52579587  7533


Satellite: ISS
Catalog Number: 25544
Epoch time:      19118
52162464   =   yrday
fracday
Element set:     915
Inclination:       51
6379  deg
RA of node:       248
0637  deg
Eccentricity:     
0001183     
Arg of perigee:   235
9063  deg
Mean anomaly:     124
1976  deg
Mean motion:   15
52579587  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             753
Checksum:              330


Coasting Arc #17 (Orbit 767)
---------------------------------------

Vector Time (GMT): 2019/119/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4511810
37                 A    =         6791328
58  meter
 Y    =       -4482953
40  meter          E    =           
0004463
 Z    =       -2377768
75                 I    =           51
30920
 XDOT =       2188
909547                 Wp   =           41
91541
 YDOT =      -5033
791278  meter/sec      RA   =          242
23826  deg
 ZDOT =       5346
154739                 TA   =          291
42828
                                          MA   =          291
47588
                                          Ha   =            222
989  n
mi
                                          Hp   =            217
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14802527
47                 X    =        -4449795
46
 Y    =      -14707852
37  feet           Y    =        -4533060
91  meter
 Z    =       -7801078
58                 Z    =        -2399534
84
 XDOT =       7181
461767                 XDOT =        2219
067388
 YDOT =     -16515
063247  feet/sec       YDOT =       -5009
144659  meter/sec
 ZDOT =      17539
877754                 ZDOT =        5356
861006

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20116619
61                 X    =        -6131545
66
 Y    =       -5405372
92  feet           Y    =        -1647557
66  meter
 Z    =       -7899121
93                 Z    =        -2407652
36
 XDOT =      -2496
048958                 XDOT =        -760
795722
 YDOT =     -16370
876614  feet/sec       YDOT =       -4989
843192  meter/sec
 ZDOT =      17588
714188                 ZDOT =        5361
040084


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   19119
48710429  
00016717  00000-0  10270-3 0  9160
2 25544  51
6391 243
2619 0001183 246
8682 113
2345 15
52596875  7686


Satellite: ISS
Catalog Number: 25544
Epoch time:      19119
48710429   =   yrday
fracday
Element set:     916
Inclination:       51
6391  deg
RA of node:       243
2619  deg
Eccentricity:     
0001183     
Arg of perigee:   246
8682  deg
Mean anomaly:     113
2345  deg
Mean motion:   15
52596875  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             768
Checksum:              330


Coasting Arc #18 (Orbit 783)
---------------------------------------

Vector Time (GMT): 2019/120/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4396581
86                 A    =         6793092
80  meter
 Y    =        5022277
91  meter          E    =           
0013037
 Z    =        1225655
37                 I    =           51
33221
 XDOT =      -2956
235051                 Wp   =          125
50874
 YDOT =       4017
926430  meter/sec      RA   =          237
25027  deg
 ZDOT =      -5823
207770                 TA   =           41
11693
                                          MA   =           41
01876
                                          Ha   =            222
967  n
mi
                                          Hp   =            217
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14424481
18                 X    =         4334140
97
 Y    =       16477289
73  feet           Y    =         5071094
46  meter
 Z    =        4021179
03                 Z    =         1246860
70
 XDOT =      -9698
933893                 XDOT =       -2972
658828
 YDOT =      13182
173328  feet/sec       YDOT =        3984
775785  meter/sec
 ZDOT =     -19105
012369                 ZDOT =       -5837
608127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20811476
78                 X    =         6343338
12
 Y    =        6758119
20  feet           Y    =         2059874
73  meter
 Z    =        4116658
11                 Z    =         1254757
39
 XDOT =       -960
546063                 XDOT =        -292
774440
 YDOT =      14706
509809  feet/sec       YDOT =        4482
544190  meter/sec
 ZDOT =     -19170
462427                 ZDOT =       -5843
156948


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   19120
51694615  
00016717  00000-0  10270-3 0  9175
2 25544  51
6397 238
1396 0001179 249
9350 110
1675 15
52606682  7846


Satellite: ISS
Catalog Number: 25544
Epoch time:      19120
51694615   =   yrday
fracday
Element set:     917
Inclination:       51
6397  deg
RA of node:       238
1396  deg
Eccentricity:     
0001179     
Arg of perigee:   249
9350  deg
Mean anomaly:     110
1675  deg
Mean motion:   15
52606682  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             784
Checksum:              325


Coasting Arc #19 (Orbit 798)
---------------------------------------

Vector Time (GMT): 2019/121/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4177948
81                 A    =         6793748
93  meter
 Y    =       -5350023
48  meter          E    =           
0011146
 Z    =         -37541
52                 I    =           51
35396
 XDOT =       3756
499910                 Wp   =           42
31818
 YDOT =      -2968
194834  meter/sec      RA   =          232
26633  deg
 ZDOT =       5987
189169                 TA   =          317
27611
                                          MA   =          317
36271
                                          Ha   =            223
001  n
mi
                                          Hp   =            217
425

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13707181
14                 X    =        -4117630
46
 Y    =      -17552570
48  feet           Y    =        -5396406
97  meter
 Z    =        -123167
70                 Z    =          -57690
01
 XDOT =      12324
474771                 XDOT =        3760
329177
 YDOT =      -9738
172027  feet/sec       YDOT =       -2926
165476  meter/sec
 ZDOT =      19643
009084                 ZDOT =        6005
446393

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20904842
05                 X    =        -6371795
86
 Y    =       -7677015
05  feet           Y    =        -2339954
19  meter
 Z    =        -213856
58                 Z    =          -65183
48
 XDOT =       4658
768923                 XDOT =        1419
992768
 YDOT =     -13180
393837  feet/sec       YDOT =       -4017
384041  meter/sec
 ZDOT =      19725
813764                 ZDOT =        6012
428035


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   19121
48242001  
00016717  00000-0  10270-3 0  9181
2 25544  51
6403 233
3381 0001022 259
6787 100
4250 15
52608178  7993


Satellite: ISS
Catalog Number: 25544
Epoch time:      19121
48242001   =   yrday
fracday
Element set:     918
Inclination:       51
6403  deg
RA of node:       233
3381  deg
Eccentricity:     
0001022     
Arg of perigee:   259
6787  deg
Mean anomaly:     100
4250  deg
Mean motion:   15
52608178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             799
Checksum:              288


Coasting Arc #20 (Orbit 813)
---------------------------------------

Vector Time (GMT): 2019/122/11:34:30
000
Vector Time (MET): N/A
Weight (LBS)     : 965966
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3792979
52                 A    =         6793143
48  meter
 Y    =        5504262
82  meter          E    =           
0008832
 Z    =       -1185243
99                 I    =           51
37302
 XDOT =      -4585
981442                 Wp   =          148
64734
 YDOT =       1909
032062  meter/sec      RA   =          227
28416  deg
 ZDOT =      -5837
430459                 TA   =           44
26606
                                          MA   =           44
19545
                                          Ha   =            222
984  n
mi
                                          Hp   =            217
433

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12444158
54                 X    =         3736904
73
 Y    =       18058605
04  feet           Y    =         5546365
02  meter
 Z    =       -3888595
77                 Z    =        -1166955
15
 XDOT =     -15045
870873                 XDOT =       -4578
632548
 YDOT =       6263
228551  feet/sec       YDOT =        1857
789401  meter/sec
 ZDOT =     -19151
674734                 ZDOT =       -5859
689932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20269435
19                 X    =         6178123
85
 Y    =        8411506
15  feet           Y    =         2563827
07  meter
 Z    =       -3806315
33                 Z    =        -1160164
91
 XDOT =      -8525
016375                 XDOT =       -2598
424991
 YDOT =      11871
985274  feet/sec       YDOT =        3618
581112  meter/sec
 ZDOT =     -19252
498240                 ZDOT =       -5868
161463


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   19122
51225655  
00016717  00000-0  10270-3 0  9193
2 25544  51
6401 228
2164 0001109 259
3496 100
7531 15
52620800  8142


Satellite: ISS
Catalog Number: 25544
Epoch time:      19122
51225655   =   yrday
fracday
Element set:     919
Inclination:       51
6401  deg
RA of node:       228
2164  deg
Eccentricity:     
0001109     
Arg of perigee:   259
3496  deg
Mean anomaly:     100
7531  deg
Mean motion:   15
52620800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             814
Checksum:              279
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