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

 
Date: October 23rd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15204 0235 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


297/21:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 2
000/00:00:00 000 0 0 0 0 220 7

301/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 8
000/00:00:00 000 0 0 0 0 221 1

304/19:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 3
000/00:00:00 000 0 0 0 0 221 8

305/15:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 2
000/00:00:00 000 0 0 0 0 221 9

306/13:59:43 634 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 222 1

308/07:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 3

308/09:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 2

Coasting Arc #1 (Orbit 3515)
---------------------------------------

Vector Time (GMT): 2019/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4181269
78                 A    =         6788889
83  meter
 Y    =         146877
47  meter          E    =           
0006852
 Z    =        5344110
73                 I    =           52
00493
 XDOT =       -582
670275                 Wp   =          159
15471
 YDOT =      -7638
217872  meter/sec      RA   =           84
16474  deg
 ZDOT =       -252
085311                 TA   =          293
20114
                                          MA   =          293
27330
                                          Ha   =            228
659  n
mi
                                          Hp   =            220
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13718076
71                 X    =        -4208560
43
 Y    =         481881
47  feet           Y    =           99967
16  meter
 Z    =       17533171
67                 Z    =         5323733
20
 XDOT =      -1911
647884                 XDOT =        -495
989698
 YDOT =     -25059
769921  feet/sec       YDOT =       -7644
249049  meter/sec
 ZDOT =       -827
051546                 ZDOT =        -254
704934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11647176
61                 X    =         3550059
43
 Y    =       -7484193
08  feet           Y    =        -2281182
05  meter
 Z    =       17440185
73                 Z    =         5315768
61
 XDOT =      13896
166569                 XDOT =        4235
551570
 YDOT =      19719
057607  feet/sec       YDOT =        6010
368759  meter/sec
 ZDOT =       -838
432295                 ZDOT =        -255
554163


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   19296
54792676  
00016717  00000-0  10270-3 0  9000
2 25544  51
6398  84
7954 0006912 180
3487 179
7660 15
50179317 35160


Satellite: ISS
Catalog Number: 25544
Epoch time:      19296
54792676   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:        84
7954  deg
Eccentricity:     
0006912     
Arg of perigee:   180
3487  deg
Mean anomaly:     179
7660  deg
Mean motion:   15
50179317  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3516
Checksum:              354


Coasting Arc #2 (Orbit 3530)
---------------------------------------

Vector Time (GMT): 2019/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4235189
19                 A    =         6788923
17  meter
 Y    =          28641
17  meter          E    =           
0016311
 Z    =       -5318798
97                 I    =           52
00162
 XDOT =        864
515683                 Wp   =          120
56528
 YDOT =       7567
596399  meter/sec      RA   =           79
23167  deg
 ZDOT =        722
729773                 TA   =          156
35691
                                          MA   =          156
28187
                                          Ha   =            228
367  n
mi
                                          Hp   =            220
651

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13894977
65                 X    =         4260390
22
 Y    =          93967
09  feet           Y    =           76142
66  meter
 Z    =      -17450127
85                 Z    =        -5298164
56
 XDOT =       2836
337542                 XDOT =         776
317709
 YDOT =      24828
072174  feet/sec       YDOT =        7576
770917  meter/sec
 ZDOT =       2371
160671                 ZDOT =         726
714678

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11969415
31                 X    =        -3648277
79
 Y    =        7286231
33  feet           Y    =         2220843
31  meter
 Z    =      -17355982
42                 Z    =        -5290103
44
 XDOT =     -14918
297565                 XDOT =       -4547
097098
 YDOT =     -18766
511849  feet/sec       YDOT =       -5720
032812  meter/sec
 ZDOT =       2388
763708                 ZDOT =         728
095178


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   19297
51489290  
00016717  00000-0  10270-3 0  9014
2 25544  51
6405  80
0041 0006898 183
8788 176
2310 15
50226081 35312


Satellite: ISS
Catalog Number: 25544
Epoch time:      19297
51489290   =   yrday
fracday
Element set:     901
Inclination:       51
6405  deg
RA of node:        80
0041  deg
Eccentricity:     
0006898     
Arg of perigee:   183
8788  deg
Mean anomaly:     176
2310  deg
Mean motion:   15
50226081  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3531
Checksum:              310


Coasting Arc #3 (Orbit 3537)
---------------------------------------

Vector Time (GMT): 2019/297/21:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3016698
75                 A    =         6791046
03  meter
 Y    =        3714631
71  meter          E    =           
0011549
 Z    =        4817759
36                 I    =           52
00426
 XDOT =      -3523
687080                 Wp   =          149
66544
 YDOT =      -6278
180466  meter/sec      RA   =           77
22393  deg
 ZDOT =       2621
827485                 TA   =          274
53319
                                          MA   =          274
66510
                                          Ha   =            228
239  n
mi
                                          Hp   =            220
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9897305
60                 X    =        -3081414
94
 Y    =       12187111
91  feet           Y    =         3680535
30  meter
 Z    =       15806297
13                 Z    =         4802947
77
 XDOT =     -11560
653148                 XDOT =       -3465
956304
 YDOT =     -20597
704942  feet/sec       YDOT =       -6317
261868  meter/sec
 ZDOT =       8601
796209                 ZDOT =        2604
851118

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9818017
31                 X    =        -2992531
68
 Y    =       12338141
07  feet           Y    =         3760665
40  meter
 Z    =       15738430
50                 Z    =         4797073
62
 XDOT =     -11029
294040                 XDOT =       -3361
728823
 YDOT =     -19702
953415  feet/sec       YDOT =       -6005
460201  meter/sec
 ZDOT =       8524
823852                 ZDOT =        2598
366310


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   19297
96614327  
00016717  00000-0  10270-3 0  9025
2 25544  51
6389  77
7712 0006454 186
3353 173
7717 15
50204940 35385


Satellite: ISS
Catalog Number: 25544
Epoch time:      19297
96614327   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:        77
7712  deg
Eccentricity:     
0006454     
Arg of perigee:   186
3353  deg
Mean anomaly:     173
7717  deg
Mean motion:   15
50204940  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3538
Checksum:              334


Coasting Arc #4 (Orbit 3552)
---------------------------------------

Vector Time (GMT): 2019/298/21:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2971196
89                 A    =         6790324
48  meter
 Y    =       -3524897
75  meter          E    =           
0011322
 Z    =       -4993970
95                 I    =           51
99341
 XDOT =       3794
887931                 Wp   =          105
12211
 YDOT =       6279
642454  meter/sec      RA   =           72
29036  deg
 ZDOT =      -2181
556835                 TA   =          143
71182
                                          MA   =          143
63498
                                          Ha   =            228
135  n
mi
                                          Hp   =            220
899

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9748021
29                 X    =         3034650
86
 Y    =      -11564625
18  feet           Y    =        -3491317
29  meter
 Z    =      -16384419
12                 Z    =        -4979383
36
 XDOT =      12450
419721                 XDOT =        3734
982081
 YDOT =      20602
501489  feet/sec       YDOT =        6321
744462  meter/sec
 ZDOT =      -7157
338696                 ZDOT =       -2163
268312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9479159
51                 X    =         2889247
82
 Y    =      -11878369
39  feet           Y    =        -3620526
99  meter
 Z    =      -16317583
77                 Z    =        -4973599
53
 XDOT =      12291
986437                 XDOT =        3746
597466
 YDOT =      19495
868777  feet/sec       YDOT =        5942
340803  meter/sec
 ZDOT =      -7074
393998                 ZDOT =       -2156
275290


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   19298
93310957  
00016717  00000-0  10270-3 0  9036
2 25544  51
6389  72
9788 0006454 189
3698 170
7333 15
50208963 35537


Satellite: ISS
Catalog Number: 25544
Epoch time:      19298
93310957   =   yrday
fracday
Element set:     903
Inclination:       51
6389  deg
RA of node:        72
9788  deg
Eccentricity:     
0006454     
Arg of perigee:   189
3698  deg
Mean anomaly:     170
7333  deg
Mean motion:   15
50208963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3553
Checksum:              357


Coasting Arc #5 (Orbit 3568)
---------------------------------------

Vector Time (GMT): 2019/299/21:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2931999
61                 A    =         6789765
35  meter
 Y    =        3363761
07  meter          E    =           
0009597
 Z    =        5117582
37                 I    =           51
98100
 XDOT =      -4086
330929                 Wp   =          163
29783
 YDOT =      -6240
371965  meter/sec      RA   =           67
35659  deg
 ZDOT =       1750
840773                 TA   =          269
78569
                                          MA   =          269
89566
                                          Ha   =            227
979  n
mi
                                          Hp   =            221
037

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9619421
29                 X    =        -2994255
20
 Y    =       11035961
51  feet           Y    =         3330625
62  meter
 Z    =       16789968
41                 Z    =         5103188
06
 XDOT =     -13406
597537                 XDOT =       -4024
750380
 YDOT =     -20473
661301  feet/sec       YDOT =       -6285
723769  meter/sec
 ZDOT =       5744
228259                 ZDOT =        1731
140438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9173910
23                 X    =        -2796207
84
 Y    =       11505442
81  feet           Y    =         3506858
97  meter
 Z    =       16724021
90                 Z    =         5097481
88
 XDOT =     -13603
561570                 XDOT =       -4146
365566
 YDOT =     -19113
320905  feet/sec       YDOT =       -5825
740212  meter/sec
 ZDOT =       5654
856905                 ZDOT =        1723
600385


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   19299
96453869  
00016717  00000-0  10270-3 0  9041
2 25544  51
6396  67
8675 0006414 194
4189 165
6780 15
50212878 35697


Satellite: ISS
Catalog Number: 25544
Epoch time:      19299
96453869   =   yrday
fracday
Element set:     904
Inclination:       51
6396  deg
RA of node:        67
8675  deg
Eccentricity:     
0006414     
Arg of perigee:   194
4189  deg
Mean anomaly:     165
6780  deg
Mean motion:   15
50212878  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3569
Checksum:              372


Coasting Arc #6 (Orbit 3583)
---------------------------------------

Vector Time (GMT): 2019/300/21:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2957399
10                 A    =         6789289
68  meter
 Y    =       -3175943
42  meter          E    =           
0012500
 Z    =       -5230891
90                 I    =           51
96656
 XDOT =       4353
691111                 Wp   =          106
93083
 YDOT =       6162
281697  meter/sec      RA   =           62
42062  deg
 ZDOT =      -1286
057553                 TA   =          150
78684
                                          MA   =          150
71687
                                          Ha   =            227
833  n
mi
                                          Hp   =            221
242

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9702752
96                 X    =         3018103
09
 Y    =      -10419761
89  feet           Y    =        -3142532
54  meter
 Z    =      -17161718
83                 Z    =        -5216377
97
 XDOT =      14283
763487                 XDOT =        4290
706234
 YDOT =      20217
459636  feet/sec       YDOT =        6210
615512  meter/sec
 ZDOT =      -4219
348928                 ZDOT =       -1265
061661

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9101391
84                 X    =         2774104
23
 Y    =      -11052467
22  feet           Y    =        -3368792
01  meter
 Z    =      -17095235
62                 Z    =        -5210627
82
 XDOT =      14822
582008                 XDOT =        4517
922996
 YDOT =      18553
890164  feet/sec       YDOT =        5655
225722  meter/sec
 ZDOT =      -4124
080560                 ZDOT =       -1257
019755


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   19300
93150062  
00016717  00000-0  10270-3 0  9051
2 25544  51
6406  63
0751 0006314 197
4463 162
6471 15
50216405 35840


Satellite: ISS
Catalog Number: 25544
Epoch time:      19300
93150062   =   yrday
fracday
Element set:     905
Inclination:       51
6406  deg
RA of node:        63
0751  deg
Eccentricity:     
0006314     
Arg of perigee:   197
4463  deg
Mean anomaly:     162
6471  deg
Mean motion:   15
50216405  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3584
Checksum:              285


Coasting Arc #7 (Orbit 3592)
---------------------------------------

Vector Time (GMT): 2019/301/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3182875
90                 A    =         6800608
60  meter
 Y    =        5998011
64  meter          E    =           
0007738
 Z    =         344905
99                 I    =           51
99751
 XDOT =      -4316
149960                 Wp   =           75
43108
 YDOT =       1937
760641  meter/sec      RA   =           59
77252  deg
 ZDOT =       6021
372104                 TA   =          288
26009
                                          MA   =          288
34429
                                          Ha   =            227
842  n
mi
                                          Hp   =            221
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10442506
24                 X    =         3113892
42
 Y    =       19678515
87  feet           Y    =         6033219
11  meter
 Z    =        1131581
34                 Z    =          360199
89
 XDOT =     -14160
596982                 XDOT =       -4366
747100
 YDOT =       6357
482419  feet/sec       YDOT =        1889
211715  meter/sec
 ZDOT =      19755
157822                 ZDOT =        6000
282298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15691242
87                 X    =        -4782690
83
 Y    =      -15808645
79  feet           Y    =        -4818475
24  meter
 Z    =        1200839
37                 Z    =          366015
84
 XDOT =      10683
681414                 XDOT =        3256
386095
 YDOT =      -9084
995187  feet/sec       YDOT =       -2769
106533  meter/sec
 ZDOT =      19658
776825                 ZDOT =        5991
995176


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   19301
51167735  
00016717  00000-0  10270-3 0  9062
2 25544  51
6422  60
1963 0006756 198
4559 161
6348 15
50235763 35938


Satellite: ISS
Catalog Number: 25544
Epoch time:      19301
51167735   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:        60
1963  deg
Eccentricity:     
0006756     
Arg of perigee:   198
4559  deg
Mean anomaly:     161
6348  deg
Mean motion:   15
50235763  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3593
Checksum:              324


Coasting Arc #8 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2019/302/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3374760
85                 A    =         6800386
92  meter
 Y    =       -5842452
71  meter          E    =           
0014635
 Z    =        -773769
09                 I    =           51
97842
 XDOT =       4456
230096                 Wp   =          163
97340
 YDOT =      -1787
911313  meter/sec      RA   =           54
84354  deg
 ZDOT =      -5976
316420                 TA   =           24
34235
                                          MA   =           24
27329
                                          Ha   =            227
674  n
mi
                                          Hp   =            221
333

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11072050
05                 X    =        -3305419
38
 Y    =      -19168151
95  feet           Y    =        -5879803
97  meter
 Z    =       -2538612
50                 Z    =         -789994
42
 XDOT =      14620
177479                 XDOT =        4504
922320
 YDOT =      -5865
850764  feet/sec       YDOT =       -1737
806398  meter/sec
 ZDOT =     -19607
337335                 ZDOT =       -5954
550805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16394776
48                 X    =         4997127
87
 Y    =       14860721
96  feet           Y    =         4529548
05  meter
 Z    =       -2612114
43                 Z    =         -796172
48
 XDOT =     -11162
225557                 XDOT =       -3402
246350
 YDOT =       8908
247112  feet/sec       YDOT =        2715
233720  meter/sec
 ZDOT =     -19507
883147                 ZDOT =       -5946
002783


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   19302
47863796  
00016717  00000-0  10270-3 0  9079
2 25544  51
6416  55
4049 0006704 202
8328 157
2525 15
50241487 36085


Satellite: ISS
Catalog Number: 25544
Epoch time:      19302
47863796   =   yrday
fracday
Element set:     907
Inclination:       51
6416  deg
RA of node:        55
4049  deg
Eccentricity:     
0006704     
Arg of perigee:   202
8328  deg
Mean anomaly:     157
2525  deg
Mean motion:   15
50241487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3608
Checksum:              318


Coasting Arc #9 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2019/303/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3570357
20                 A    =         6800043
06  meter
 Y    =        5665046
79  meter          E    =           
0008709
 Z    =        1171278
93                 I    =           51
95872
 XDOT =      -4605
415084                 Wp   =           81
96795
 YDOT =       1678
406311  meter/sec      RA   =           49
91282  deg
 ZDOT =       5884
437174                 TA   =          290
66907
                                          MA   =          290
76242
                                          Ha   =            227
557  n
mi
                                          Hp   =            221
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11713770
35                 X    =         3501054
07
 Y    =       18586111
52  feet           Y    =         5704585
53  meter
 Z    =        3842778
65                 Z    =         1188454
63
 XDOT =     -15109
629542                 XDOT =       -4652
425335
 YDOT =       5506
582386  feet/sec       YDOT =        1626
642361  meter/sec
 ZDOT =      19305
896240                 ZDOT =        5861
951026

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17059267
23                 X    =        -5199664
65
 Y    =      -13821471
82  feet           Y    =        -4212784
61  meter
 Z    =        3920615
19                 Z    =         1195003
51
 XDOT =      11639
664786                 XDOT =        3547
769827
 YDOT =      -8886
134325  feet/sec       YDOT =       -2708
493742  meter/sec
 ZDOT =      19203
161455                 ZDOT =        5853
123612


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   19303
51006043  
00016717  00000-0  10270-3 0  9080
2 25544  51
6431  50
2938 0006752 206
4382 153
6425 15
50243317 36246


Satellite: ISS
Catalog Number: 25544
Epoch time:      19303
51006043   =   yrday
fracday
Element set:     908
Inclination:       51
6431  deg
RA of node:        50
2938  deg
Eccentricity:     
0006752     
Arg of perigee:   206
4382  deg
Mean anomaly:     153
6425  deg
Mean motion:   15
50243317  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3624
Checksum:              280


Coasting Arc #10 (Orbit 3638)
---------------------------------------

Vector Time (GMT): 2019/304/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3707559
34                 A    =         6799541
70  meter
 Y    =       -5464503
94  meter          E    =           
0012083
 Z    =       -1589233
80                 I    =           51
93506
 XDOT =       4798
754616                 Wp   =          172
38115
 YDOT =      -1584
686964  meter/sec      RA   =           44
98055  deg
 ZDOT =      -5762
904823                 TA   =           24
90789
                                          MA   =           24
84962
                                          Ha   =            227
368  n
mi
                                          Hp   =            221
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12163908
61                 X    =        -3638458
32
 Y    =      -17928162
53  feet           Y    =        -5505578
06  meter
 Z    =       -5214021
64                 Z    =        -1607076
50
 XDOT =      15743
945590                 XDOT =        4844
112043
 YDOT =      -5199
104213  feet/sec       YDOT =       -1530
770102  meter/sec
 ZDOT =     -18907
168056                 ZDOT =       -5739
483605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17486343
28                 X    =         5329837
43
 Y    =       12757643
98  feet           Y    =         3888529
89  meter
 Z    =       -5294905
55                 Z    =        -1613887
21
 XDOT =     -12239
567620                 XDOT =       -3730
620211
 YDOT =       8995
782686  feet/sec       YDOT =        2741
914563  meter/sec
 ZDOT =     -18800
173218                 ZDOT =       -5730
292797


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   19304
47701704  
00016717  00000-0  10270-3 0  9093
2 25544  51
6435  45
5023 0006631 210
3173 149
7595 15
50245162 36390


Satellite: ISS
Catalog Number: 25544
Epoch time:      19304
47701704   =   yrday
fracday
Element set:     909
Inclination:       51
6435  deg
RA of node:        45
5023  deg
Eccentricity:     
0006631     
Arg of perigee:   210
3173  deg
Mean anomaly:     149
7595  deg
Mean motion:   15
50245162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3639
Checksum:              297


Coasting Arc #11 (Orbit 3644)
---------------------------------------

Vector Time (GMT): 2019/304/19:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5289541
39                 A    =         6793185
18  meter
 Y    =        -400644
42  meter          E    =           
0006868
 Z    =        4236377
10                 I    =           51
90210
 XDOT =      -2470
673848                 Wp   =          110
86383
 YDOT =      -6256
981568  meter/sec      RA   =           43
09755  deg
 ZDOT =      -3674
202931                 TA   =           16
67243
                                          MA   =           16
64986
                                          Ha   =            227
310  n
mi
                                          Hp   =            221
792

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17354138
40                 X    =        -5305246
55
 Y    =       -1314450
19  feet           Y    =         -459883
77  meter
 Z    =       13898875
00                 Z    =         4210643
76
 XDOT =      -8105
885328                 XDOT =       -2382
675206
 YDOT =     -20528
154752  feet/sec       YDOT =       -6284
118220  meter/sec
 ZDOT =     -12054
471560                 ZDOT =       -3685
991299

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15246807
62                 X    =        -4647226
96
 Y    =       -8583542
15  feet           Y    =        -2616263
65  meter
 Z    =       13781519
76                 Z    =         4200607
22
 XDOT =        805
341882                 XDOT =         245
468206
 YDOT =     -20883
115078  feet/sec       YDOT =       -6365
173476  meter/sec
 ZDOT =     -12107
656440                 ZDOT =       -3690
413683


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   19304
86379812  
00016717  00000-0  10270-3 0  9109
2 25544  51
6408  43
5895 0006188 213
8040 146
2716 15
50245219 36450


Satellite: ISS
Catalog Number: 25544
Epoch time:      19304
86379812   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:        43
5895  deg
Eccentricity:     
0006188     
Arg of perigee:   213
8040  deg
Mean anomaly:     146
2716  deg
Mean motion:   15
50245219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3645
Checksum:              313


Coasting Arc #12 (Orbit 3657)
---------------------------------------

Vector Time (GMT): 2019/305/15:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5819653
68                 A    =         6796531
09  meter
 Y    =       -1535420
73  meter          E    =           
0011148
 Z    =        3141727
46                 I    =           51
89432
 XDOT =      -1103
653239                 Wp   =          123
58002
 YDOT =      -5810
437018  meter/sec      RA   =           38
94522  deg
 ZDOT =      -4877
616102                 TA   =           20
39970
                                          MA   =           20
35521
                                          Ha   =            227
185  n
mi
                                          Hp   =            221
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19093351
97                 X    =        -5817312
68
 Y    =       -5037469
58  feet           Y    =        -1600487
24  meter
 Z    =       10307504
79                 Z    =         3113462
86
 XDOT =      -3620
909577                 XDOT =       -1014
904031
 YDOT =     -19063
113575  feet/sec       YDOT =       -5822
282425  meter/sec
 ZDOT =     -16002
677501                 ZDOT =       -4882
762007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2147008
81                 X    =          654408
28
 Y    =      -19696725
47  feet           Y    =        -6003561
92  meter
 Z    =       10178713
23                 Z    =         3102471
79
 XDOT =      16898
469952                 XDOT =        5150
653641
 YDOT =      -6450
627311  feet/sec       YDOT =       -1966
151205  meter/sec
 ZDOT =     -16025
593278                 ZDOT =       -4884
600831


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   19305
70182482  
00016717  00000-0  10270-3 0  9119
2 25544  51
6428  39
4366 0006220 216
1932 143
8799 15
50260673 36581


Satellite: ISS
Catalog Number: 25544
Epoch time:      19305
70182482   =   yrday
fracday
Element set:     911
Inclination:       51
6428  deg
RA of node:        39
4366  deg
Eccentricity:     
0006220     
Arg of perigee:   216
1932  deg
Mean anomaly:     143
8799  deg
Mean motion:   15
50260673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3658
Checksum:              314


Coasting Arc #13 (Orbit 3671)
---------------------------------------

Vector Time (GMT): 2019/306/13:59:43
634
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -587480
59                 A    =         6791383
56  meter
 Y    =       -4875437
52  meter          E    =           
0006197
 Z    =       -4695795
41                 I    =           51
85222
 XDOT =       6825
943651                 Wp   =          103
26698
 YDOT =       1942
840720  meter/sec      RA   =           34
44563  deg
 ZDOT =      -2875
720239                 TA   =          138
23232
                                          MA   =          138
18500
                                          Ha   =            227
057  n
mi
                                          Hp   =            222
064

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1927429
75                 X    =         -510108
46
 Y    =      -15995529
91  feet           Y    =        -4881574
36  meter
 Z    =      -15406152
92                 Z    =        -4698461
46
 XDOT =      22394
828251                 XDOT =        6817
679784
 YDOT =       6374
149343  feet/sec       YDOT =        2019
127136  meter/sec
 ZDOT =      -9434
777686                 ZDOT =       -2842
581863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15693560
14                 X    =         4783397
13
 Y    =        3594982
97  feet           Y    =         1095750
81  meter
 Z    =      -15417839
60                 Z    =        -4699357
51
 XDOT =     -13210
999433                 XDOT =       -4026
712627
 YDOT =      17920
194941  feet/sec       YDOT =        5462
075418  meter/sec
 ZDOT =      -9283
796917                 ZDOT =       -2829
701300


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   19306
60431507  
00016717  00000-0  10270-3 0  9125
2 25544  51
6424  34
9636 0006462 219
2083 140
8600 15
50226057 36728


Satellite: ISS
Catalog Number: 25544
Epoch time:      19306
60431507   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:        34
9636  deg
Eccentricity:     
0006462     
Arg of perigee:   219
2083  deg
Mean anomaly:     140
8600  deg
Mean motion:   15
50226057  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3672
Checksum:              287


Coasting Arc #14 (Orbit 3687)
---------------------------------------

Vector Time (GMT): 2019/307/13:59:43
634
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         526541
39                 A    =         6790582
63  meter
 Y    =        4700978
45  meter          E    =           
0008278
 Z    =        4873663
10                 I    =           51
82200
 XDOT =      -7038
349180                 Wp   =          168
82982
 YDOT =      -1765
048974  meter/sec      RA   =           29
50158  deg
 ZDOT =       2454
304833                 TA   =          257
07070
                                          MA   =          257
16317
                                          Ha   =            226
786  n
mi
                                          Hp   =            222
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1727498
01                 X    =          450260
71
 Y    =       15423157
64  feet           Y    =         4706439
97  meter
 Z    =       15989708
33                 Z    =         4876035
72
 XDOT =     -23091
696786                 XDOT =       -7030
010582
 YDOT =      -5790
843091  feet/sec       YDOT =       -1843
710203  meter/sec
 ZDOT =       8052
181211                 ZDOT =        2420
134952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15145642
91                 X    =        -4616391
96
 Y    =       -3337083
26  feet           Y    =        -1017142
98  meter
 Z    =       16000068
42                 Z    =         4876820
85
 XDOT =      12563
774850                 XDOT =        3829
438574
 YDOT =     -19025
668832  feet/sec       YDOT =       -5799
023860  meter/sec
 ZDOT =       7896
484314                 ZDOT =        2406
848419


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   19307
63572786  
00016717  00000-0  10270-3 0  9135
2 25544  51
6429  29
8520 0006390 223
9880 136
0762 15
50253586 36885


Satellite: ISS
Catalog Number: 25544
Epoch time:      19307
63572786   =   yrday
fracday
Element set:     913
Inclination:       51
6429  deg
RA of node:        29
8520  deg
Eccentricity:     
0006390     
Arg of perigee:   223
9880  deg
Mean anomaly:     136
0762  deg
Mean motion:   15
50253586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3688
Checksum:              334


Coasting Arc #15 (Orbit 3698)
---------------------------------------

Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1165988
19                 A    =         6791063
65  meter
 Y    =        4720512
49  meter          E    =           
0008398
 Z    =        4742431
89                 I    =           51
80116
 XDOT =      -7071
037600                 Wp   =          163
80387
 YDOT =      -1033
585924  meter/sec      RA   =           25
99746  deg
 ZDOT =       2758
272767                 TA   =          258
87777
                                          MA   =          258
97221
                                          Ha   =            226
709  n
mi
                                          Hp   =            222
269

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3825420
56                 X    =         1090079
02
 Y    =       15487245
70  feet           Y    =         4733126
87  meter
 Z    =       15559159
76                 Z    =         4747911
60
 XDOT =     -23198
942258                 XDOT =       -7072
352517
 YDOT =      -3391
029935  feet/sec       YDOT =       -1112
666659  meter/sec
 ZDOT =       9049
451336                 ZDOT =        2723
920711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5224368
94                 X    =         1592387
65
 Y    =      -15047614
63  feet           Y    =        -4586512
94  meter
 Z    =       15583688
18                 Z    =         4749908
16
 XDOT =      16656
744663                 XDOT =        5076
975773
 YDOT =      15023
381339  feet/sec       YDOT =        4579
126632  meter/sec
 ZDOT =       8892
856834                 ZDOT =        2710
542763


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   19308
34482369  
00016717  00000-0  10270-3 0  9142
2 25544  51
6412  26
3343 0006410 225
3627 134
7001 15
50265675 36995


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
34482369   =   yrday
fracday
Element set:     914
Inclination:       51
6412  deg
RA of node:        26
3343  deg
Eccentricity:     
0006410     
Arg of perigee:   225
3627  deg
Mean anomaly:     134
7001  deg
Mean motion:   15
50265675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3699
Checksum:              301


Coasting Arc #16 (Orbit 3699)
---------------------------------------

Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4640205
17                 A    =         6798070
12  meter
 Y    =       -4329502
34  meter          E    =           
0008221
 Z    =       -2422450
87                 I    =           51
82402
 XDOT =       4955
130123                 Wp   =          182
97432
 YDOT =      -2310
412914  meter/sec      RA   =           25
55157  deg
 ZDOT =      -5369
469635                 TA   =           24
00298
                                          MA   =           23
96469
                                          Ha   =            226
723  n
mi
                                          Hp   =            222
244

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15223770
26                 X    =        -4579679
50
 Y    =      -14204404
02  feet           Y    =        -4381053
93  meter
 Z    =       -7947673
46                 Z    =        -2444844
57
 XDOT =      16256
988592                 XDOT =        5006
679753
 YDOT =      -7580
094863  feet/sec       YDOT =       -2254
712830  meter/sec
 ZDOT =     -17616
370193                 ZDOT =       -5345
274028

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15153851
38                 X    =         4618893
90
 Y    =       14221879
24  feet           Y    =         4334828
79  meter
 Z    =       -8049392
96                 Z    =        -2453454
97
 XDOT =     -15346
937806                 XDOT =       -4677
746643
 YDOT =       6457
767707  feet/sec       YDOT =        1968
327597  meter/sec
 ZDOT =     -17505
773576                 ZDOT =       -5335
759786


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   19308
40928731  
00016717  00000-0  10270-3 0  9158
2 25544  51
6435  26
0154 0006441 224
8551 135
2079 15
50254952 37001


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
40928731   =   yrday
fracday
Element set:     915
Inclination:       51
6435  deg
RA of node:        26
0154  deg
Eccentricity:     
0006441     
Arg of perigee:   224
8551  deg
Mean anomaly:     135
2079  deg
Mean motion:   15
50254952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              293


Coasting Arc #17 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4656589
85                 A    =         6797209
37  meter
 Y    =        4092053
29  meter          E    =           
0008615
 Z    =        2783515
13                 I    =           51
79092
 XDOT =      -5165
039574                 Wp   =          102
88037
 YDOT =       2375
131541  meter/sec      RA   =           20
60888  deg
 ZDOT =       5133
725441                 TA   =          288
53954
                                          MA   =          288
63312
                                          Ha   =            226
590  n
mi
                                          Hp   =            222
339

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15277525
74                 X    =         4596964
30
 Y    =       13425371
70  feet           Y    =         4143793
17  meter
 Z    =        9132267
47                 Z    =         2805990
55
 XDOT =     -16945
667893                 XDOT =       -5216
152179
 YDOT =       7792
426315  feet/sec       YDOT =        2317
086612  meter/sec
 ZDOT =      16842
931236                 ZDOT =        5108
511193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15429467
96                 X    =        -4702901
84
 Y    =      -13179512
08  feet           Y    =        -4017115
28  meter
 Z    =        9234375
29                 Z    =         2814637
59
 XDOT =      15970
378961                 XDOT =        4867
771507
 YDOT =      -6941
622941  feet/sec       YDOT =       -2115
806672  meter/sec
 ZDOT =      16727
687313                 ZDOT =        5098
599093


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   19309
44069556  
00016717  00000-0  10270-3 0  9165
2 25544  51
6437  20
9043 0006430 228
3021 131
7580 15
50276704 37166


Satellite: ISS
Catalog Number: 25544
Epoch time:      19309
44069556   =   yrday
fracday
Element set:     916
Inclination:       51
6437  deg
RA of node:        20
9043  deg
Eccentricity:     
0006430     
Arg of perigee:   228
3021  deg
Mean anomaly:     131
7580  deg
Mean motion:   15
50276704  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              295


Coasting Arc #18 (Orbit 3730)
---------------------------------------

Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4614273
28                 A    =         6796359
36  meter
 Y    =       -3868566
55  meter          E    =           
0004921
 Z    =       -3145385
60                 I    =           51
75626
 XDOT =       5381
997935                 Wp   =          187
04586
 YDOT =      -2470
106889  meter/sec      RA   =           15
66396  deg
 ZDOT =      -4861
304722                 TA   =           29
07743
                                          MA   =           29
05004
                                          Ha   =            226
405  n
mi
                                          Hp   =            222
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15138691
88                 X    =        -4555392
17
 Y    =      -12692147
49  feet           Y    =        -3919837
42  meter
 Z    =      -10319506
55                 Z    =        -3167657
25
 XDOT =      17657
473540                 XDOT =        5432
833208
 YDOT =      -8104
025227  feet/sec       YDOT =       -2409
637387  meter/sec
 ZDOT =     -15949
162475                 ZDOT =       -4835
037167

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15482726
97                 X    =         4719135
18
 Y    =       12184294
07  feet           Y    =         3713772
83  meter
 Z    =      -10420698
56                 Z    =        -3176228
92
 XDOT =     -16596
688149                 XDOT =       -5058
670548
 YDOT =       7562
645649  feet/sec       YDOT =        2305
094394  meter/sec
 ZDOT =     -15829
112651                 ZDOT =       -4824
713536


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   19310
40764160  
00016717  00000-0  10270-3 0  9177
2 25544  51
6437  16
1131 0006451 232
2442 127
8124 15
50252735 37310


Satellite: ISS
Catalog Number: 25544
Epoch time:      19310
40764160   =   yrday
fracday
Element set:     917
Inclination:       51
6437  deg
RA of node:        16
1131  deg
Eccentricity:     
0006451     
Arg of perigee:   232
2442  deg
Mean anomaly:     127
8124  deg
Mean motion:   15
50252735  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3731
Checksum:              271


Coasting Arc #19 (Orbit 3746)
---------------------------------------

Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4558728
31                 A    =         6795349
98  meter
 Y    =        3650818
86  meter          E    =           
0007907
 Z    =        3471554
07                 I    =           51
72161
 XDOT =      -5572
688563                 Wp   =          119
10951
 YDOT =       2609
456263  meter/sec      RA   =           10
71549  deg
 ZDOT =       4562
049791                 TA   =          281
49901
                                          MA   =          281
58778
                                          Ha   =            226
223  n
mi
                                          Hp   =            222
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14956457
72                 X    =         4500701
84
 Y    =       11977752
18  feet           Y    =         3701473
40  meter
 Z    =       11389613
10                 Z    =         3493558
01
 XDOT =     -18283
098960                 XDOT =       -5623
614333
 YDOT =       8561
208212  feet/sec       YDOT =        2546
853857  meter/sec
 ZDOT =      14967
354957                 ZDOT =        4534
855606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15464759
91                 X    =        -4713658
82
 Y    =      -11212307
32  feet           Y    =        -3417511
27  meter
 Z    =       11489596
47                 Z    =         3502029
00
 XDOT =      17110
599562                 XDOT =        5215
310746
 YDOT =      -8351
215173  feet/sec       YDOT =       -2545
450385  meter/sec
 ZDOT =      14843
074722                 ZDOT =        4524
169175


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   19311
43904575  
00016717  00000-0  10270-3 0  9188
2 25544  51
6446  11
0017 0006425 236
3089 123
7449 15
50286178 37470


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
43904575   =   yrday
fracday
Element set:     918
Inclination:       51
6446  deg
RA of node:        11
0017  deg
Eccentricity:     
0006425     
Arg of perigee:   236
3089  deg
Mean anomaly:     123
7449  deg
Mean motion:   15
50286178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3747
Checksum:              312
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