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

 
Date: June 15th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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


There are no maneuvers



Coasting Arc #1 (Orbit 3174)
---------------------------------------

Vector Time (GMT): 2020/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6022416
23                 A    =         6800787
31  meter
 Y    =        2190768
42  meter          E    =           
0014927
 Z    =        2258415
51                 I    =           51
63110
 XDOT =      -3534
123084                 Wp   =          100
93968
 YDOT =      -4080
691791  meter/sec      RA   =          356
21098  deg
 ZDOT =      -5438
019087                 TA   =           53
97739
                                          MA   =           53
83914
                                          Ha   =            228
972  n
mi
                                          Hp   =            221
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19758583
43                 X    =        -6057436
57
 Y    =        7187560
43  feet           Y    =         2123225
37  meter
 Z    =        7409499
71                 Z    =         2229076
12
 XDOT =     -11594
892009                 XDOT =       -3461
814068
 YDOT =     -13388
096426  feet/sec       YDOT =       -4119
807885  meter/sec
 ZDOT =     -17841
269969                 ZDOT =       -5455
011402

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4838280
46                 X    =         1474707
88
 Y    =       20509463
17  feet           Y    =         6251284
37  meter
 Z    =        7274358
60                 Z    =         2217224
50
 XDOT =     -13135
607202                 XDOT =       -4003
733075
 YDOT =       9487
312791  feet/sec       YDOT =        2891
732939  meter/sec
 ZDOT =     -17919
096846                 ZDOT =       -5461
740719


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   20167
53669763  
00016717  00000-0  10270-3 0  9008
2 25544  51
6418 356
6428 0002131  45
8857 314
2468 15
49486482 31750


Satellite: ISS
Catalog Number: 25544
Epoch time:      20167
53669763   =   yrday
fracday
Element set:     900
Inclination:       51
6418  deg
RA of node:       356
6428  deg
Eccentricity:     
0002131     
Arg of perigee:    45
8857  deg
Mean anomaly:     314
2468  deg
Mean motion:   15
49486482  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3175
Checksum:              332


Coasting Arc #2 (Orbit 3189)
---------------------------------------

Vector Time (GMT): 2020/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5899591
48                 A    =         6801132
29  meter
 Y    =       -2619550
32  meter          E    =           
0008542
 Z    =       -2135237
94                 I    =           51
59740
 XDOT =       3690
341653                 Wp   =           44
93720
 YDOT =       3843
636424  meter/sec      RA   =          351
25855  deg
 ZDOT =       5500
227275                 TA   =          291
43791
                                          MA   =          291
52900
                                          Ha   =            229
130  n
mi
                                          Hp   =            221
405

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19355615
11                 X    =         5938817
42
 Y    =       -8594325
18  feet           Y    =        -2553357
26  meter
 Z    =       -7005373
82                 Z    =        -2106484
98
 XDOT =      12107
420121                 XDOT =        3620
369610
 YDOT =      12610
355721  feet/sec       YDOT =        3884
512457  meter/sec
 ZDOT =      18045
365074                 ZDOT =        5517
984179

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6630368
76                 X    =        -2020936
40
 Y    =      -20158841
92  feet           Y    =        -6144415
02  meter
 Z    =       -6872905
24                 Z    =        -2094861
52
 XDOT =      12266
476570                 XDOT =        3738
822058
 YDOT =     -10192
502273  feet/sec       YDOT =       -3106
674693  meter/sec
 ZDOT =      18126
721781                 ZDOT =        5525
024799


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   20168
50414951  
00016717  00000-0  10270-3 0  9014
2 25544  51
6409 351
8532 0002159  58
0050 302
1310 15
49441877 31902


Satellite: ISS
Catalog Number: 25544
Epoch time:      20168
50414951   =   yrday
fracday
Element set:     901
Inclination:       51
6409  deg
RA of node:       351
8532  deg
Eccentricity:     
0002159     
Arg of perigee:    58
0050  deg
Mean anomaly:     302
1310  deg
Mean motion:   15
49441877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3190
Checksum:              280


Coasting Arc #3 (Orbit 3205)
---------------------------------------

Vector Time (GMT): 2020/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5764830
41                 A    =         6801301
91  meter
 Y    =        3011615
37  meter          E    =           
0015204
 Z    =        1967177
88                 I    =           51
56494
 XDOT =      -3807
198260                 Wp   =          105
34734
 YDOT =      -3625
535200  meter/sec      RA   =          346
30478  deg
 ZDOT =      -5574
483862                 TA   =           52
96262
                                          MA   =           52
82364
                                          Ha   =            229
041  n
mi
                                          Hp   =            221
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18913485
60                 X    =        -5807634
22
 Y    =        9880627
84  feet           Y    =         2946909
29  meter
 Z    =        6453995
67                 Z    =         1939070
91
 XDOT =     -12490
807938                 XDOT =       -3739
295668
 YDOT =     -11894
800524  feet/sec       YDOT =       -3667
729471  meter/sec
 ZDOT =     -18288
989048                 ZDOT =       -5592
813499

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8294625
92                 X    =         2528201
98
 Y    =       19702817
14  feet           Y    =         6005418
67  meter
 Z    =        6324474
83                 Z    =         1927699
93
 XDOT =     -11432
196584                 XDOT =       -3484
533519
 YDOT =      10744
904205  feet/sec       YDOT =        3275
046802  meter/sec
 ZDOT =     -18372
992091                 ZDOT =       -5600
087989


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   20169
53609307  
00016717  00000-0  10270-3 0  9020
2 25544  51
6406 346
7449 0002169  55
8924 304
2432 15
49483541 32065


Satellite: ISS
Catalog Number: 25544
Epoch time:      20169
53609307   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       346
7449  deg
Eccentricity:     
0002169     
Arg of perigee:    55
8924  deg
Mean anomaly:     304
2432  deg
Mean motion:   15
49483541  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3206
Checksum:              309


Coasting Arc #4 (Orbit 3220)
---------------------------------------

Vector Time (GMT): 2020/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5577162
99                 A    =         6801608
87  meter
 Y    =       -3425616
62  meter          E    =           
0009354
 Z    =       -1840201
23                 I    =           51
53242
 XDOT =       3932
643929                 Wp   =           45
27946
 YDOT =       3392
151436  meter/sec      RA   =          341
34844  deg
 ZDOT =       5628
237635                 TA   =          294
49682
                                          MA   =          294
59433
                                          Ha   =            229
204  n
mi
                                          Hp   =            221
290

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18297778
84                 X    =         5623993
45
 Y    =      -11238899
68  feet           Y    =        -3362986
65  meter
 Z    =       -6037405
61                 Z    =        -1812996
23
 XDOT =      12902
375095                 XDOT =        3867
080676
 YDOT =      11129
105760  feet/sec       YDOT =        3435
761492  meter/sec
 ZDOT =      18465
346573                 ZDOT =        5647
182353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10027775
38                 X    =        -3056465
94
 Y    =      -19027972
76  feet           Y    =        -5799726
10  meter
 Z    =       -5912006
15                 Z    =        -1801979
48
 XDOT =      10546
777793                 XDOT =        3214
657871
 YDOT =     -11297
289422  feet/sec       YDOT =       -3443
413816  meter/sec
 ZDOT =      18552
193257                 ZDOT =        5654
708505


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   20170
50354346  
00016717  00000-0  10270-3 0  9030
2 25544  51
6399 341
9559 0002255  69
5799 290
5593 15
49443347 32215


Satellite: ISS
Catalog Number: 25544
Epoch time:      20170
50354346   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       341
9559  deg
Eccentricity:     
0002255     
Arg of perigee:    69
5799  deg
Mean anomaly:     290
5593  deg
Mean motion:   15
49443347  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3221
Checksum:              329


Coasting Arc #5 (Orbit 3236)
---------------------------------------

Vector Time (GMT): 2020/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5381521
11                 A    =         6801780
32  meter
 Y    =        3799414
99  meter          E    =           
0015376
 Z    =        1667191
22                 I    =           51
50190
 XDOT =      -4022
408302                 Wp   =          110
08106
 YDOT =      -3183
041975  meter/sec      RA   =          336
39022  deg
 ZDOT =      -5692
360283                 TA   =           51
64932
                                          MA   =           51
51125
                                          Ha   =            229
092  n
mi
                                          Hp   =            221
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17655909
14                 X    =        -5431705
63
 Y    =       12465272
28  feet           Y    =         3738954
07  meter
 Z    =        5469787
47                 Z    =         1640928
61
 XDOT =     -13196
877630                 XDOT =       -3958
865275
 YDOT =     -10443
051098  feet/sec       YDOT =       -3227
667022  meter/sec
 ZDOT =     -18675
722713                 ZDOT =       -5711
745940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11609285
94                 X    =         3538510
35
 Y    =       18266051
41  feet           Y    =         5567492
47  meter
 Z    =        5348697
19                 Z    =         1630282
90
 XDOT =      -9722
351999                 XDOT =       -2963
372889
 YDOT =      11710
848160  feet/sec       YDOT =        3569
466519  meter/sec
 ZDOT =     -18764
611978                 ZDOT =       -5719
453731


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   20171
53548593  
00016717  00000-0  10270-3 0  9044
2 25544  51
6401 336
8475 0002140  67
7107 292
4270 15
49472465 32378


Satellite: ISS
Catalog Number: 25544
Epoch time:      20171
53548593   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       336
8475  deg
Eccentricity:     
0002140     
Arg of perigee:    67
7107  deg
Mean anomaly:     292
4270  deg
Mean motion:   15
49472465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3237
Checksum:              306


Coasting Arc #6 (Orbit 3251)
---------------------------------------

Vector Time (GMT): 2020/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5131793
27                 A    =         6801992
90  meter
 Y    =       -4186824
01  meter          E    =           
0010177
 Z    =       -1535771
23                 I    =           51
47371
 XDOT =       4121
130916                 Wp   =           45
60096
 YDOT =       2957
743606  meter/sec      RA   =          331
42945  deg
 ZDOT =       5737
944678                 TA   =          297
61639
                                          MA   =          297
71968
                                          Ha   =            229
223  n
mi
                                          Hp   =            221
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16836592
11                 X    =         5185690
09
 Y    =      -13736299
24  feet           Y    =        -4129134
97  meter
 Z    =       -5038619
52                 Z    =        -1510712
90
 XDOT =      13520
770723                 XDOT =        4059
878570
 YDOT =       9703
883223  feet/sec       YDOT =        3003
485362  meter/sec
 ZDOT =      18825
277816                 ZDOT =        5757
815391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13217188
79                 X    =        -4028599
14
 Y    =      -17280452
05  feet           Y    =        -5267081
78  meter
 Z    =       -4923041
21                 Z    =        -1500542
96
 XDOT =       8847
585679                 XDOT =        2696
744115
 YDOT =     -12127
075788  feet/sec       YDOT =       -3696
332700  meter/sec
 ZDOT =      18916
416011                 ZDOT =        5765
723600


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   20172
50293266  
00016717  00000-0  10270-3 0  9057
2 25544  51
6417 332
0584 0002322  77
0130 283
1279 15
49455558 32523


Satellite: ISS
Catalog Number: 25544
Epoch time:      20172
50293266   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:       332
0584  deg
Eccentricity:     
0002322     
Arg of perigee:    77
0130  deg
Mean anomaly:     283
1279  deg
Mean motion:   15
49455558  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3252
Checksum:              294


Coasting Arc #7 (Orbit 3267)
---------------------------------------

Vector Time (GMT): 2020/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4879119
82                 A    =         6802187
48  meter
 Y    =        4531152
38  meter          E    =           
0015534
 Z    =        1357222
58                 I    =           51
44425
 XDOT =      -4188
671094                 Wp   =          114
19917
 YDOT =      -2761
738813  meter/sec      RA   =          326
46725  deg
 ZDOT =      -5791
508410                 TA   =           51
00357
                                          MA   =           50
86533
                                          Ha   =            229
183  n
mi
                                          Hp   =            221
209

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16007610
95                 X    =        -4936018
48
 Y    =       14865985
49  feet           Y    =         4476272
16  meter
 Z    =        4452829
99                 Z    =         1333384
56
 XDOT =     -13742
359231                 XDOT =       -4129
345447
 YDOT =      -9060
822876  feet/sec       YDOT =       -2808
246572  meter/sec
 ZDOT =     -19001
011843                 ZDOT =       -5811
711781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14653040
62                 X    =         4466246
78
 Y    =       16232589
26  feet           Y    =         4947693
21  meter
 Z    =        4342841
73                 Z    =         1323698
16
 XDOT =      -8057
238598                 XDOT =       -2455
846325
 YDOT =      12423
153952  feet/sec       YDOT =        3786
577325  meter/sec
 ZDOT =     -19093
697803                 ZDOT =       -5819
759090


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   20173
53487230  
00016717  00000-0  10270-3 0  9068
2 25544  51
6406 326
9501 0002303  78
0376 282
1032 15
49463718 32684


Satellite: ISS
Catalog Number: 25544
Epoch time:      20173
53487230   =   yrday
fracday
Element set:     906
Inclination:       51
6406  deg
RA of node:       326
9501  deg
Eccentricity:     
0002303     
Arg of perigee:    78
0376  deg
Mean anomaly:     282
1032  deg
Mean motion:   15
49463718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3268
Checksum:              296


Coasting Arc #8 (Orbit 3282)
---------------------------------------

Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4571107
55                 A    =         6802345
34  meter
 Y    =       -4881742
15  meter          E    =           
0010935
 Z    =       -1222600
57                 I    =           51
41860
 XDOT =       4267
504014                 Wp   =           46
66570
 YDOT =       2546
457705  meter/sec      RA   =          321
50372  deg
 ZDOT =       5828
016460                 TA   =          300
03462
                                          MA   =          300
14306
                                          Ha   =            229
238  n
mi
                                          Hp   =            221
169

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14997072
00                 X    =         4631295
56
 Y    =      -16016214
41  feet           Y    =        -4830287
98  meter
 Z    =       -4011156
71                 Z    =        -1200250
93
 XDOT =      14000
997421                 XDOT =        4210
402644
 YDOT =       8354
520029  feet/sec       YDOT =        2593
859462  meter/sec
 ZDOT =      19120
788911                 ZDOT =        5848
608029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16076246
45                 X    =        -4900039
92
 Y    =      -14960032
11  feet           Y    =        -4559817
79  meter
 Z    =       -3907993
12                 Z    =        -1191156
30
 XDOT =       7209
272665                 XDOT =        2197
386308
 YDOT =     -12731
318410  feet/sec       YDOT =       -3880
505851  meter/sec
 ZDOT =      19215
281148                 ZDOT =        5856
817694


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   20174
50231674  
00016717  00000-0  10270-3 0  9076
2 25544  51
6419 322
1621 0002350  84
6836 275
4582 15
49455188 32839


Satellite: ISS
Catalog Number: 25544
Epoch time:      20174
50231674   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:       322
1621  deg
Eccentricity:     
0002350     
Arg of perigee:    84
6836  deg
Mean anomaly:     275
4582  deg
Mean motion:   15
49455188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3283
Checksum:              309


Coasting Arc #9 (Orbit 3298)
---------------------------------------

Vector Time (GMT): 2020/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4265410
51                 A    =         6802501
06  meter
 Y    =        5187127
61  meter          E    =           
0015360
 Z    =        1040579
84                 I    =           51
39351
 XDOT =      -4320
457367                 Wp   =          118
56038
 YDOT =      -2363
288334  meter/sec      RA   =          316
53768  deg
 ZDOT =      -5870
294301                 TA   =           50
13969
                                          MA   =           50
00468
                                          Ha   =            229
166  n
mi
                                          Hp   =            221
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13994128
96                 X    =        -4328151
98
 Y    =       17018135
21  feet           Y    =         5139077
73  meter
 Z    =        3413975
84                 Z    =         1019709
05
 XDOT =     -14174
728893                 XDOT =       -4265
195080
 YDOT =      -7753
570651  feet/sec       YDOT =       -2411
292581  meter/sec
 ZDOT =     -19259
495739                 ZDOT =       -5891
147410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17311524
55                 X    =         5276552
68
 Y    =       13653294
46  feet           Y    =         4161524
15  meter
 Z    =        3317600
11                 Z    =         1011204
51
 XDOT =      -6459
701802                 XDOT =       -1968
917109
 YDOT =      12941
957036  feet/sec       YDOT =        3944
708505  meter/sec
 ZDOT =     -19355
210009                 ZDOT =       -5899
468011


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   20175
53425512  
00016717  00000-0  10270-3 0  9087
2 25544  51
6418 317
0537 0002243  86
6474 273
4932 15
49461520 32999


Satellite: ISS
Catalog Number: 25544
Epoch time:      20175
53425512   =   yrday
fracday
Element set:     908
Inclination:       51
6418  deg
RA of node:       317
0537  deg
Eccentricity:     
0002243     
Arg of perigee:    86
6474  deg
Mean anomaly:     273
4932  deg
Mean motion:   15
49461520  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3299
Checksum:              310


Coasting Arc #10 (Orbit 3313)
---------------------------------------

Vector Time (GMT): 2020/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3906217
92                 A    =         6802609
19  meter
 Y    =       -5490446
50  meter          E    =           
0011736
 Z    =        -901937
87                 I    =           51
37176
 XDOT =       4384
133904                 Wp   =           47
70525
 YDOT =       2159
639116  meter/sec      RA   =          311
57046  deg
 ZDOT =       5897
853745                 TA   =          302
51700
                                          MA   =          302
63035
                                          Ha   =            229
227  n
mi
                                          Hp   =            221
150

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12815675
58                 X    =         3971704
44
 Y    =      -18013275
93  feet           Y    =        -5446398
07  meter
 Z    =       -2959113
73                 Z    =         -882805
23
 XDOT =      14383
641418                 XDOT =        4331
010373
 YDOT =       7085
430169  feet/sec       YDOT =        2208
367496  meter/sec
 ZDOT =      19349
913862                 ZDOT =        5919
021216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18492847
60                 X    =        -5636619
95
 Y    =      -12134642
35  feet           Y    =        -3698638
99  meter
 Z    =       -2870722
42                 Z    =         -874996
19
 XDOT =       5649
364727                 XDOT =        1721
926369
 YDOT =     -13164
436454  feet/sec       YDOT =       -4012
520231  meter/sec
 ZDOT =      19447
094365                 ZDOT =        5927
474363


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   20176
50169588  
00016717  00000-0  10270-3 0  9094
2 25544  51
6434 312
2656 0002353  88
4606 271
6814 15
49459340 33149


Satellite: ISS
Catalog Number: 25544
Epoch time:      20176
50169588   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:       312
2656  deg
Eccentricity:     
0002353     
Arg of perigee:    88
4606  deg
Mean anomaly:     271
6814  deg
Mean motion:   15
49459340  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3314
Checksum:              317


Coasting Arc #11 (Orbit 3329)
---------------------------------------

Vector Time (GMT): 2020/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3555663
96                 A    =         6802719
04  meter
 Y    =        5747358
07  meter          E    =           
0015134
 Z    =         715742
67                 I    =           51
34971
 XDOT =      -4427
427411                 Wp   =          122
09675
 YDOT =      -1990
280303  meter/sec      RA   =          306
60196  deg
 ZDOT =      -5928
312175                 TA   =           50
15313
                                          MA   =           50
02009
                                          Ha   =            229
188  n
mi
                                          Hp   =            221
162

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11665564
16                 X    =        -3623144
97
 Y    =       18856161
66  feet           Y    =         5707218
68  meter
 Z    =        2348237
11                 Z    =          698307
95
 XDOT =     -14525
680481                 XDOT =       -4376
046562
 YDOT =      -6529
791019  feet/sec       YDOT =       -2039
502703  meter/sec
 ZDOT =     -19449
843093                 ZDOT =       -5949
694077

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19476254
36                 X    =         5936362
33
 Y    =       10615446
62  feet           Y    =         3235588
13  meter
 Z    =        2267652
16                 Z    =          691180
38
 XDOT =      -4946
902587                 XDOT =       -1507
815908
 YDOT =      13313
229485  feet/sec       YDOT =        4057
872347  meter/sec
 ZDOT =     -19548
026572                 ZDOT =       -5958
238499


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   20177
53363085  
00016717  00000-0  10270-3 0  9108
2 25544  51
6424 307
1579 0002337  92
0316 268
1102 15
49465299 33305


Satellite: ISS
Catalog Number: 25544
Epoch time:      20177
53363085   =   yrday
fracday
Element set:     910
Inclination:       51
6424  deg
RA of node:       307
1579  deg
Eccentricity:     
0002337     
Arg of perigee:    92
0316  deg
Mean anomaly:     268
1102  deg
Mean motion:   15
49465299  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3330
Checksum:              297


Coasting Arc #12 (Orbit 3344)
---------------------------------------

Vector Time (GMT): 2020/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3152847
57                 A    =         6802809
86  meter
 Y    =       -5995257
28  meter          E    =           
0012426
 Z    =        -574610
25                 I    =           51
33122
 XDOT =       4482
347142                 Wp   =           49
72629
 YDOT =       1796
249663  meter/sec      RA   =          301
63197  deg
 ZDOT =       5946
201687                 TA   =          304
05874
                                          MA   =          304
17665
                                          Ha   =            229
222  n
mi
                                          Hp   =            221
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10343988
10                 X    =         3222445
09
 Y    =      -19669479
27  feet           Y    =        -5959610
67  meter
 Z    =       -1885204
25                 Z    =         -559126
96
 XDOT =      14705
863326                 XDOT =        4433
044980
 YDOT =       5893
207555  feet/sec       YDOT =        1846
097982  meter/sec
 ZDOT =      19508
535717                 ZDOT =        5967
855368

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20370759
69                 X    =        -6209007
55
 Y    =       -8898512
52  feet           Y    =        -2712266
62  meter
 Z    =       -1813594
32                 Z    =         -552783
55
 XDOT =       4169
847093                 XDOT =        1270
969394
 YDOT =     -13477
225733  feet/sec       YDOT =       -4107
858403  meter/sec
 ZDOT =      19607
985880                 ZDOT =        5976
514096


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   20178
50106955  
00016717  00000-0  10270-3 0  9118
2 25544  51
6428 302
3699 0002353  94
6255 265
5164 15
49457278 33450


Satellite: ISS
Catalog Number: 25544
Epoch time:      20178
50106955   =   yrday
fracday
Element set:     911
Inclination:       51
6428  deg
RA of node:       302
3699  deg
Eccentricity:     
0002353     
Arg of perigee:    94
6255  deg
Mean anomaly:     265
5164  deg
Mean motion:   15
49457278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3345
Checksum:              322


Coasting Arc #13 (Orbit 3360)
---------------------------------------

Vector Time (GMT): 2020/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2765403
71                 A    =         6802850
84  meter
 Y    =        6196338
03  meter          E    =           
0014702
 Z    =         385797
78                 I    =           51
31485
 XDOT =      -4522
004327                 Wp   =          126
01275
 YDOT =      -1637
361805  meter/sec      RA   =          296
66043  deg
 ZDOT =      -5964
488131                 TA   =           49
81699
                                          MA   =           49
68837
                                          Ha   =            229
148  n
mi
                                          Hp   =            221
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9072846
81                 X    =        -2836361
44
 Y    =       20329193
02  feet           Y    =         6165016
52  meter
 Z    =        1265740
75                 Z    =          372193
07
 XDOT =     -14835
972202                 XDOT =       -4474
387022
 YDOT =      -5371
921933  feet/sec       YDOT =       -1687
663124  meter/sec
 ZDOT =     -19568
530612                 ZDOT =       -5986
338566

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21063196
33                 X    =         6420062
24
 Y    =        7217328
54  feet           Y    =         2199841
74  meter
 Z    =        1202774
54                 Z    =          366605
68
 XDOT =      -3503
516974                 XDOT =       -1067
871974
 YDOT =      13589
722841  feet/sec       YDOT =        4142
147522  meter/sec
 ZDOT =     -19668
898278                 ZDOT =       -5995
080195


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   20179
53300201  
00016717  00000-0  10270-3 0  9123
2 25544  51
6428 297
2619 0002278  99
3207 260
8201 15
49469471 33615


Satellite: ISS
Catalog Number: 25544
Epoch time:      20179
53300201   =   yrday
fracday
Element set:     912
Inclination:       51
6428  deg
RA of node:       297
2619  deg
Eccentricity:     
0002278     
Arg of perigee:    99
3207  deg
Mean anomaly:     260
8201  deg
Mean motion:   15
49469471  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3361
Checksum:              302


Coasting Arc #14 (Orbit 3375)
---------------------------------------

Vector Time (GMT): 2020/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2329713
06                 A    =         6802897
29  meter
 Y    =       -6381453
15  meter          E    =           
0013154
 Z    =        -241475
86                 I    =           51
30181
 XDOT =       4571
831200                 Wp   =           51
99851
 YDOT =       1451
799802  meter/sec      RA   =          291
68765  deg
 ZDOT =       5972
678791                 TA   =          305
39270
                                          MA   =          305
51551
                                          Ha   =            229
212  n
mi
                                          Hp   =            221
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7643415
54                 X    =         2402072
16
 Y    =      -20936526
07  feet           Y    =        -6354996
02  meter
 Z    =        -792243
64                 Z    =         -229984
08
 XDOT =      14999
446195                 XDOT =        4526
245283
 YDOT =       4763
122709  feet/sec       YDOT =        1502
669710  meter/sec
 ZDOT =      19595
402858                 ZDOT =        5994
776268

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21634761
49                 X    =        -6594275
30
 Y    =       -5364564
44  feet           Y    =        -1635119
24  meter
 Z    =        -738998
44                 Z    =         -225246
72
 XDOT =       2755
069094                 XDOT =         839
745060
 YDOT =     -13712
330345  feet/sec       YDOT =       -4179
518289  meter/sec
 ZDOT =      19696
919802                 ZDOT =        6003
621156


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   20180
50043687  
00016717  00000-0  10270-3 0  9135
2 25544  51
6437 292
4734 0002385  98
0730 262
0691 15
49464429 33767


Satellite: ISS
Catalog Number: 25544
Epoch time:      20180
50043687   =   yrday
fracday
Element set:     913
Inclination:       51
6437  deg
RA of node:       292
4734  deg
Eccentricity:     
0002385     
Arg of perigee:    98
0730  deg
Mean anomaly:     262
0691  deg
Mean motion:   15
49464429  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3376
Checksum:              316


Coasting Arc #15 (Orbit 3391)
---------------------------------------

Vector Time (GMT): 2020/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1916282
08                 A    =         6802918
94  meter
 Y    =        6520805
58  meter          E    =           
0014258
 Z    =          49990
98                 I    =           51
28959
 XDOT =      -4611
912065                 Wp   =          129
04297
 YDOT =      -1300
714075  meter/sec      RA   =          286
71434  deg
 ZDOT =      -5978
101909                 TA   =           50
41696
                                          MA   =           50
29113
                                          Ha   =            229
184  n
mi
                                          Hp   =            221
152

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6287014
70                 X    =        -1989300
08
 Y    =       21393719
09  feet           Y    =         6498968
07  meter
 Z    =         164012
41                 Z    =           40505
91
 XDOT =     -15130
945094                 XDOT =       -4567
986190
 YDOT =      -4267
434629  feet/sec       YDOT =       -1352
041424  meter/sec
 ZDOT =     -19613
195241                 ZDOT =       -6000
398202

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22008629
00                 X    =         6708230
12
 Y    =        3584762
15  feet           Y    =         1092635
50  meter
 Z    =         120000
37                 Z    =           36576
11
 XDOT =      -2113
224015                 XDOT =        -644
110680
 YDOT =      13805
774052  feet/sec       YDOT =        4207
999931  meter/sec
 ZDOT =     -19715
637324                 ZDOT =       -6009
326256


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   20181
53236619  
00016717  00000-0  10270-3 0  9149
2 25544  51
6428 287
3655 0002389 103
8430 256
2986 15
49465054 33923


Satellite: ISS
Catalog Number: 25544
Epoch time:      20181
53236619   =   yrday
fracday
Element set:     914
Inclination:       51
6428  deg
RA of node:       287
3655  deg
Eccentricity:     
0002389     
Arg of perigee:   103
8430  deg
Mean anomaly:     256
2986  deg
Mean motion:   15
49465054  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3392
Checksum:              326
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