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

 
Date: June 17th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 408 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


172/07:16:36 447 1 2 1 2 1 3
N/A 0 1 -0 1 220 4
000/00:03:12 895 0 4 -0 0 216 0

179/14:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 216 0

180/09:42:42 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 9

Coasting Arc #1 (Orbit 3824)
---------------------------------------

Vector Time (GMT): 2018/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4923129
48                 A    =         6787493
90  meter
 Y    =       -4216209
77  meter          E    =           
0008585
 Z    =       -2000281
95                 I    =           51
82821
 XDOT =       4532
343729                 Wp   =          156
38495
 YDOT =      -2648
050607  meter/sec      RA   =           26
53708  deg
 ZDOT =      -5589
455259                 TA   =           45
64469
                                          MA   =           45
57438
                                          Ha   =            220
885  n
mi
                                          Hp   =            214
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16151999
61                 X    =        -4865900
49
 Y    =      -13832709
22  feet           Y    =        -4270943
25  meter
 Z    =       -6562604
84                 Z    =        -2024058
50
 XDOT =      14869
894123                 XDOT =        4588
768629
 YDOT =      -8687
830076  feet/sec       YDOT =       -2597
050310  meter/sec
 ZDOT =     -18338
107806                 ZDOT =       -5567
302214

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15731433
67                 X    =        -4794940
98
 Y    =       14260232
28  feet           Y    =         4346518
80  meter
 Z    =       -6668319
74                 Z    =        -2032503
86
 XDOT =      -5715
058841                 XDOT =       -1741
949935
 YDOT =     -14809
216581  feet/sec       YDOT =       -4513
849214  meter/sec
 ZDOT =     -18238
516168                 ZDOT =       -5559
099728


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   18166
52817284  
00016717  00000-0  10270-3 0  9006
2 25544  51
6411  26
9891 0002986 198
2153 161
8893 15
54156291 38252


Satellite: ISS
Catalog Number: 25544
Epoch time:      18166
52817284   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:        26
9891  deg
Eccentricity:     
0002986     
Arg of perigee:   198
2153  deg
Mean anomaly:     161
8893  deg
Mean motion:   15
54156291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3825
Checksum:              332


Coasting Arc #2 (Orbit 3840)
---------------------------------------

Vector Time (GMT): 2018/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3784634
50                 A    =         6784037
25  meter
 Y    =        4431053
12  meter          E    =           
0011600
 Z    =        3466684
45                 I    =           51
78564
 XDOT =      -5969
783503                 Wp   =          104
19105
 YDOT =       1510
252701  meter/sec      RA   =           21
56943  deg
 ZDOT =       4571
352931                 TA   =          296
40472
                                          MA   =          296
52373
                                          Ha   =            220
788  n
mi
                                          Hp   =            214
901

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12416779
86                 X    =         3717964
79
 Y    =       14537575
84  feet           Y    =         4473002
16  meter
 Z    =       11373636
65                 Z    =         3484907
56
 XDOT =     -19585
903881                 XDOT =       -6008
432915
 YDOT =       4954
897314  feet/sec       YDOT =        1443
277608  meter/sec
 ZDOT =      14997
877069                 ZDOT =        4542
260403

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15780260
91                 X    =         4809823
52
 Y    =      -10707749
24  feet           Y    =        -3263721
97  meter
 Z    =       11454458
35                 Z    =         3491318
91
 XDOT =       2031
690235                 XDOT =         619
259184
 YDOT =      18952
634773  feet/sec       YDOT =        5776
763079  meter/sec
 ZDOT =      14867
416360                 ZDOT =        4531
588506


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   18167
55697055  
00016717  00000-0  10270-3 0  9013
2 25544  51
6399  21
8595 0002815 201
4358 158
6677 15
54171331 38411


Satellite: ISS
Catalog Number: 25544
Epoch time:      18167
55697055   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:        21
8595  deg
Eccentricity:     
0002815     
Arg of perigee:   201
4358  deg
Mean anomaly:     158
6677  deg
Mean motion:   15
54171331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3841
Checksum:              328


Coasting Arc #3 (Orbit 3855)
---------------------------------------

Vector Time (GMT): 2018/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2265453
22                 A    =         6780172
57  meter
 Y    =       -4452820
23  meter          E    =           
0008302
 Z    =       -4591359
33                 I    =           51
74131
 XDOT =       7013
853735                 Wp   =           83
54419
 YDOT =       -423
397041  meter/sec      RA   =           16
58935  deg
 ZDOT =      -3053
961582                 TA   =          155
96880
                                          MA   =          155
93004
                                          Ha   =            220
693  n
mi
                                          Hp   =            214
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7432589
29                 X    =        -2193190
02
 Y    =      -14608990
25  feet           Y    =        -4477749
38  meter
 Z    =      -15063514
86                 Z    =        -4602189
13
 XDOT =      23011
331151                 XDOT =        7032
901373
 YDOT =      -1389
097902  feet/sec       YDOT =        -344
856357  meter/sec
 ZDOT =     -10019
558996                 ZDOT =       -3019
844860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15212779
50                 X    =        -4636855
19
 Y    =        5983072
70  feet           Y    =         1823640
56  meter
 Z    =      -15111242
20                 Z    =        -4605906
62
 XDOT =       1136
423478                 XDOT =         346
381876
 YDOT =     -21999
077413  feet/sec       YDOT =       -6705
318796  meter/sec
 ZDOT =      -9866
797011                 ZDOT =       -3007
399729


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   18168
52146584  
00016717  00000-0  10270-3 0  9028
2 25544  51
6394  17
0506 0002936 206
8757 153
2244 15
54187578 38568


Satellite: ISS
Catalog Number: 25544
Epoch time:      18168
52146584   =   yrday
fracday
Element set:     902
Inclination:       51
6394  deg
RA of node:        17
0506  deg
Eccentricity:     
0002936     
Arg of perigee:   206
8757  deg
Mean anomaly:     153
2244  deg
Mean motion:   15
54187578  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3856
Checksum:              330


Coasting Arc #4 (Orbit 3871)
---------------------------------------

Vector Time (GMT): 2018/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         532465
11                 A    =         6777712
41  meter
 Y    =        4306163
42  meter          E    =           
0005120
 Z    =        5205939
06                 I    =           51
70140
 XDOT =      -7549
783416                 Wp   =          157
15899
 YDOT =       -558
529254  meter/sec      RA   =           11
59786  deg
 ZDOT =       1229
172291                 TA   =          281
02865
                                          MA   =          281
08623
                                          Ha   =            220
691  n
mi
                                          Hp   =            215
068

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1746932
76                 X    =          458985
39
 Y    =       14127832
75  feet           Y    =         4311706
34  meter
 Z    =       17079852
55                 Z    =         5208347
61
 XDOT =     -24769
630629                 XDOT =       -7548
947285
 YDOT =      -1832
445059  feet/sec       YDOT =        -642
951607  meter/sec
 ZDOT =       4032
717491                 ZDOT =        1192
500394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14210876
91                 X    =         4331475
28
 Y    =        -595450
17  feet           Y    =         -181493
21  meter
 Z    =       17089915
50                 Z    =         5209006
24
 XDOT =      -3685
102321                 XDOT =       -1123
219187
 YDOT =      23558
983239  feet/sec       YDOT =        7180
778091  meter/sec
 ZDOT =       3868
690842                 ZDOT =        1179
176969


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   18169
55025990  
00016717  00000-0  10270-3 0  9030
2 25544  51
6400  11
9209 0002855 208
6358 151
4638 15
54161966 38724


Satellite: ISS
Catalog Number: 25544
Epoch time:      18169
55025990   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:        11
9209  deg
Eccentricity:     
0002855     
Arg of perigee:   208
6358  deg
Mean anomaly:     151
4638  deg
Mean motion:   15
54161966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3872
Checksum:              318


Coasting Arc #5 (Orbit 3886)
---------------------------------------

Vector Time (GMT): 2018/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1307791
53                 A    =         6777358
05  meter
 Y    =       -4053959
71  meter          E    =           
0013586
 Z    =       -5283066
23                 I    =           51
66606
 XDOT =       7483
738704                 Wp   =          106
72135
 YDOT =       1451
850306  meter/sec      RA   =            6
59941  deg
 ZDOT =        736
229914                 TA   =          170
33104
                                          MA   =          170
30487
                                          Ha   =            220
612  n
mi
                                          Hp   =            215
090

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4290654
64                 X    =         1378688
97
 Y    =      -13300392
73  feet           Y    =        -4038938
13  meter
 Z    =      -17332894
47                 Z    =        -5276541
70
 XDOT =      24552
948504                 XDOT =        7463
371324
 YDOT =       4763
288406  feet/sec       YDOT =        1535
424676  meter/sec
 ZDOT =       2415
452473                 ZDOT =         772
533713

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13034152
61                 X    =        -3972809
72
 Y    =       -5143502
75  feet           Y    =        -1567739
64  meter
 Z    =      -17303024
01                 Z    =        -5273961
72
 XDOT =       5755
231681                 XDOT =        1754
194616
 YDOT =     -23280
622202  feet/sec       YDOT =       -7095
933647  meter/sec
 ZDOT =       2577
673306                 ZDOT =         785
674824


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   18170
51475056  
00016717  00000-0  10270-3 0  9041
2 25544  51
6382   7
1114 0002893 211
1340 148
9642 15
54198747 38876


Satellite: ISS
Catalog Number: 25544
Epoch time:      18170
51475056   =   yrday
fracday
Element set:     904
Inclination:       51
6382  deg
RA of node:         7
1114  deg
Eccentricity:     
0002893     
Arg of perigee:   211
1340  deg
Mean anomaly:     148
9642  deg
Mean motion:   15
54198747  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3887
Checksum:              311


Coasting Arc #6 (Orbit 3902)
---------------------------------------

Vector Time (GMT): 2018/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3060444
56                 A    =         6779525
30  meter
 Y    =        3700446
27  meter          E    =           
0004986
 Z    =        4781972
91                 I    =           51
64077
 XDOT =      -6843
011930                 Wp   =           75
78208
 YDOT =      -2267
144906  meter/sec      RA   =            1
60295  deg
 ZDOT =      -2621
622910                 TA   =           40
07615
                                          MA   =           40
03937
                                          Ha   =            220
574  n
mi
                                          Hp   =            215
212

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10040828
61                 X    =        -3124824
70
 Y    =       12140571
77  feet           Y    =         3665861
86  meter
 Z    =       15688887
50                 Z    =         4766950
37
 XDOT =     -22450
826542                 XDOT =       -6804
417107
 YDOT =      -7438
139456  feet/sec       YDOT =       -2343
452147  meter/sec
 ZDOT =      -8601
125033                 ZDOT =       -2654
770207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11738779
86                 X    =         3577980
10
 Y    =       10608330
61  feet           Y    =         3233419
17  meter
 Z    =       15621052
53                 Z    =         4761296
81
 XDOT =      -7529
134171                 XDOT =       -2294
880095
 YDOT =      21231
630393  feet/sec       YDOT =        6471
400944  meter/sec
 ZDOT =      -8749
074573                 ZDOT =       -2666
717930


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   18171
54353996  
00016717  00000-0  10270-3 0  9054
2 25544  51
6387   1
9828 0003021 217
7469 142
3472 15
54189479 39033


Satellite: ISS
Catalog Number: 25544
Epoch time:      18171
54353996   =   yrday
fracday
Element set:     905
Inclination:       51
6387  deg
RA of node:         1
9828  deg
Eccentricity:     
0003021     
Arg of perigee:   217
7469  deg
Mean anomaly:     142
3472  deg
Mean motion:   15
54189479  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3903
Checksum:              331


Coasting Arc #7 (Orbit 3914)
---------------------------------------

Vector Time (GMT): 2018/172/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3137512
10                 A    =         6780709
96  meter
 Y    =       -3818727
78  meter          E    =           
0008715
 Z    =       -4650897
77                 I    =           51
61976
 XDOT =       6788
405717                 Wp   =          126
52914
 YDOT =       2025
602362  meter/sec      RA   =          357
59396  deg
 ZDOT =       2915
045031                 TA   =          172
51784
                                          MA   =          172
50483
                                          Ha   =            220
411  n
mi
                                          Hp   =            215
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10293674
88                 X    =         3202572
55
 Y    =      -12528634
44  feet           Y    =        -3783277
76  meter
 Z    =      -15258850
94                 Z    =        -4635499
17
 XDOT =      22271
672300                 XDOT =        6751
090622
 YDOT =       6645
677040  feet/sec       YDOT =        2101
306088  meter/sec
 ZDOT =       9563
796033                 ZDOT =        2947
930253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5981823
70                 X    =         1823259
86
 Y    =      -15141378
77  feet           Y    =        -4615092
25  meter
 Z    =      -15189318
28                 Z    =        -4629704
21
 XDOT =      22069
437831                 XDOT =        6726
764651
 YDOT =      -1026
691568  feet/sec       YDOT =        -312
935590  meter/sec
 ZDOT =       9710
603989                 ZDOT =        2959
792096


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   18172
31513167  
00016717  00000-0  10270-3 0  9069
2 25544  51
6424 358
1385 0003261 237
8388 122
2448 15
53972724 39154


Satellite: ISS
Catalog Number: 25544
Epoch time:      18172
31513167   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:       358
1385  deg
Eccentricity:     
0003261     
Arg of perigee:   237
8388  deg
Mean anomaly:     122
2448  deg
Mean motion:   15
53972724  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3915
Checksum:              317


Coasting Arc #8 (Orbit 3930)
---------------------------------------

Vector Time (GMT): 2018/173/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4557351
80                 A    =         6784323
36  meter
 Y    =        3481452
80  meter          E    =           
0009348
 Z    =        3615739
49                 I    =           51
59856
 XDOT =      -5629
122576                 Wp   =           94
65937
 YDOT =      -2787
710673  meter/sec      RA   =          352
60529  deg
 ZDOT =      -4401
815831                 TA   =           42
45488
                                          MA   =           42
38261
                                          Ha   =            220
466  n
mi
                                          Hp   =            215
908

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14951941
61                 X    =        -4613507
03
 Y    =       11422089
23  feet           Y    =         3430175
01  meter
 Z    =       11862662
36                 Z    =         3593465
37
 XDOT =     -18468
249921                 XDOT =       -5576
149534
 YDOT =      -9146
032392  feet/sec       YDOT =       -2850
362778  meter/sec
 ZDOT =     -14441
652990                 ZDOT =       -4429
031812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10463069
51                 X    =        -3189143
59
 Y    =       15713589
15  feet           Y    =         4789501
97  meter
 Z    =       11762428
80                 Z    =         3585188
30
 XDOT =     -19208
348389                 XDOT =       -5854
704589
 YDOT =      -1866
510040  feet/sec       YDOT =        -568
912260  meter/sec
 ZDOT =     -14562
959073                 ZDOT =       -4438
789925


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   18173
34406918  
00016717  00000-0  10270-3 0  9079
2 25544  51
6420 353
0110 0003086 241
1238 118
9605 15
53974910 39311


Satellite: ISS
Catalog Number: 25544
Epoch time:      18173
34406918   =   yrday
fracday
Element set:     907
Inclination:       51
6420  deg
RA of node:       353
0110  deg
Eccentricity:     
0003086     
Arg of perigee:   241
1238  deg
Mean anomaly:     118
9605  deg
Mean motion:   15
53974910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3931
Checksum:              294


Coasting Arc #9 (Orbit 3945)
---------------------------------------

Vector Time (GMT): 2018/174/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5628141
98                 A    =         6787670
52  meter
 Y    =       -3056659
56  meter          E    =           
0003410
 Z    =       -2243045
22                 I    =           51
57703
 XDOT =       4082
885296                 Wp   =           20
42796
 YDOT =       3526
103053  meter/sec      RA   =          347
62316  deg
 ZDOT =       5445
089743                 TA   =          314
61721
                                          MA   =          314
64502
                                          Ha   =            220
264  n
mi
                                          Hp   =            215
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18465032
75                 X    =         5672799
66
 Y    =      -10028410
64  feet           Y    =        -2993471
85  meter
 Z    =       -7359072
24                 Z    =        -2215597
44
 XDOT =      13395
292966                 XDOT =        4016
702536
 YDOT =      11568
579570  feet/sec       YDOT =        3571
390028  meter/sec
 ZDOT =      17864
467660                 ZDOT =        5464
762702

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13941320
51                 X    =         4249314
49
 Y    =      -15778644
51  feet           Y    =        -4809330
85  meter
 Z    =       -7235769
38                 Z    =        -2205462
51
 XDOT =      15292
742414                 XDOT =        4661
227888
 YDOT =       5288
229005  feet/sec       YDOT =        1611
852201  meter/sec
 ZDOT =      17951
897339                 ZDOT =        5471
738309


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   18174
30869561  
00016717  00000-0  10270-3 0  9084
2 25544  51
6417 348
2033 0003221 246
0691 114
0125 15
53988642 39462


Satellite: ISS
Catalog Number: 25544
Epoch time:      18174
30869561   =   yrday
fracday
Element set:     908
Inclination:       51
6417  deg
RA of node:       348
2033  deg
Eccentricity:     
0003221     
Arg of perigee:   246
0691  deg
Mean anomaly:     114
0125  deg
Mean motion:   15
53988642  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3946
Checksum:              310


Coasting Arc #10 (Orbit 3961)
---------------------------------------

Vector Time (GMT): 2018/175/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6279286
68                 A    =         6789721
77  meter
 Y    =        2486062
60  meter          E    =           
0011852
 Z    =         629850
30                 I    =           51
55170
 XDOT =      -2284
731431                 Wp   =          142
19746
 YDOT =      -4247
024894  meter/sec      RA   =          342
64713  deg
 ZDOT =      -5963
951203                 TA   =           30
99302
                                          MA   =           30
92313
                                          Ha   =            220
274  n
mi
                                          Hp   =            216
081

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20601334
24                 X    =        -6309679
31
 Y    =        8156373
35  feet           Y    =         2415673
27  meter
 Z    =        2066437
99                 Z    =          599274
09
 XDOT =      -7495
838028                 XDOT =       -2208
100394
 YDOT =     -13933
808707  feet/sec       YDOT =       -4272
145092  meter/sec
 ZDOT =     -19566
769040                 ZDOT =       -5974
864106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16301858
00                 X    =        -4968806
32
 Y    =       15024613
81  feet           Y    =         4579502
29  meter
 Z    =        1929240
89                 Z    =          588032
62
 XDOT =     -10789
290010                 XDOT =       -3288
575595
 YDOT =      -9165
109432  feet/sec       YDOT =       -2793
525355  meter/sec
 ZDOT =     -19614
886030                 ZDOT =       -5978
617262


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   18175
33763043  
00016717  00000-0  10270-3 0  9097
2 25544  51
6419 343
0757 0003265 247
6428 112
4378 15
53943729 39620


Satellite: ISS
Catalog Number: 25544
Epoch time:      18175
33763043   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       343
0757  deg
Eccentricity:     
0003265     
Arg of perigee:   247
6428  deg
Mean anomaly:     112
4378  deg
Mean motion:   15
53943729  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3962
Checksum:              331


Coasting Arc #11 (Orbit 3977)
---------------------------------------

Vector Time (GMT): 2018/176/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6466431
65                 A    =         6789228
09  meter
 Y    =       -1776154
24  meter          E    =           
0010549
 Z    =        1024013
98                 I    =           51
51937
 XDOT =        406
304167                 Wp   =           50
14794
 YDOT =       4894
264318  meter/sec      RA   =          337
66936  deg
 ZDOT =       5889
667988                 TA   =          320
97020
                                          MA   =          321
04627
                                          Ha   =            220
064  n
mi
                                          Hp   =            216
009

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21215326
95                 X    =         6480838
37
 Y    =       -5827277
69  feet           Y    =        -1703761
74  meter
 Z    =        3359625
92                 Z    =         1055460
48
 XDOT =       1333
018919                 XDOT =         322
935990
 YDOT =      16057
297630  feet/sec       YDOT =        4898
340887  meter/sec
 ZDOT =      19323
057705                 ZDOT =        5891
439909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17451758
18                 X    =         5319295
89
 Y    =      -13361000
53  feet           Y    =        -4072432
96  meter
 Z    =        3500592
88                 Z    =         1066980
71
 XDOT =       6174
718990                 XDOT =        1882
054348
 YDOT =      13157
579877  feet/sec       YDOT =        4010
430346  meter/sec
 ZDOT =      19330
175426                 ZDOT =        5891
837470


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   18176
36655898  
00016717  00000-0  10270-3 0  9101
2 25544  51
6418 337
9465 0003308 256
2991 103
7793 15
53998026 39787


Satellite: ISS
Catalog Number: 25544
Epoch time:      18176
36655898   =   yrday
fracday
Element set:     910
Inclination:       51
6418  deg
RA of node:       337
9465  deg
Eccentricity:     
0003308     
Arg of perigee:   256
2991  deg
Mean anomaly:     103
7793  deg
Mean motion:   15
53998026  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3978
Checksum:              362


Coasting Arc #12 (Orbit 3992)
---------------------------------------

Vector Time (GMT): 2018/177/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6206113
07                 A    =         6786862
16  meter
 Y    =         877317
06  meter          E    =           
0003667
 Z    =       -2598184
59                 I    =           51
47989
 XDOT =       1421
615047                 Wp   =          168
07458
 YDOT =      -5420
416730  meter/sec      RA   =          332
68696  deg
 ZDOT =      -5230
842952                 TA   =           41
22907
                                          MA   =           41
20138
                                          Ha   =            220
026  n
mi
                                          Hp   =            216
071

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20361263
34                 X    =        -6202841
60
 Y    =        2878336
81  feet           Y    =          807934
73  meter
 Z    =       -8524227
67                 Z    =        -2628323
67
 XDOT =       4664
091363                 XDOT =        1507
530661
 YDOT =     -17783
519455  feet/sec       YDOT =       -5404
038030  meter/sec
 ZDOT =     -17161
558240                 ZDOT =       -5223
729427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17556734
82                 X    =        -5351292
77
 Y    =       10597535
47  feet           Y    =         3230128
81  meter
 Z    =       -8659193
36                 Z    =        -2639322
14
 XDOT =      -1794
126478                 XDOT =        -546
849751
 YDOT =     -16955
423355  feet/sec       YDOT =       -5168
013039  meter/sec
 ZDOT =     -17128
844448                 ZDOT =       -5220
871788


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   18177
33118061  
00016717  00000-0  10270-3 0  9116
2 25544  51
6406 333
1391 0003365 259
1839 100
8935 15
53960700 39937


Satellite: ISS
Catalog Number: 25544
Epoch time:      18177
33118061   =   yrday
fracday
Element set:     911
Inclination:       51
6406  deg
RA of node:       333
1391  deg
Eccentricity:     
0003365     
Arg of perigee:   259
1839  deg
Mean anomaly:     100
8935  deg
Mean motion:   15
53960700  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3993
Checksum:              307


Coasting Arc #13 (Orbit 4008)
---------------------------------------

Vector Time (GMT): 2018/178/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5547259
14                 A    =         6783237
62  meter
 Y    =         166271
05  meter          E    =           
0007946
 Z    =        3895335
68                 I    =           51
43921
 XDOT =      -3033
264295                 Wp   =          105
13677
 YDOT =       5752
098602  meter/sec      RA   =          327
69365  deg
 ZDOT =       4065
098884                 TA   =          302
14571
                                          MA   =          302
22278
                                          Ha   =            219
942  n
mi
                                          Hp   =            216
090

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18199669
11                 X    =         5526066
14
 Y    =         545508
68  feet           Y    =          228185
17  meter
 Z    =       12779972
69                 Z    =         3922230
83
 XDOT =      -9951
654511                 XDOT =       -3117
106454
 YDOT =      18871
714573  feet/sec       YDOT =        5717
709080  meter/sec
 ZDOT =      13336
938596                 ZDOT =        4050
161697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16766600
53                 X    =         5110459
84
 Y    =       -6878793
59  feet           Y    =        -2096656
29  meter
 Z    =       12900253
59                 Z    =         3931997
30
 XDOT =      -1984
181632                 XDOT =        -604
778561
 YDOT =      20102
974898  feet/sec       YDOT =        6127
386749  meter/sec
 ZDOT =      13269
178821                 ZDOT =        4044
445705


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   18178
36010871  
00016717  00000-0  10270-3 0  9121
2 25544  51
6408 328
0107 0003284 265
8269  94
2509 15
53968674 40098


Satellite: ISS
Catalog Number: 25544
Epoch time:      18178
36010871   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:       328
0107  deg
Eccentricity:     
0003284     
Arg of perigee:   265
8269  deg
Mean anomaly:      94
2509  deg
Mean motion:   15
53968674  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4009
Checksum:              323


Coasting Arc #14 (Orbit 4023)
---------------------------------------

Vector Time (GMT): 2018/179/07:18:12
895
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4576037
43                 A    =         6779738
49  meter
 Y    =       -1354143
21  meter          E    =           
0008530
 Z    =       -4823844
79                 I    =           51
40005
 XDOT =       4339
145855                 Wp   =           65
34296
 YDOT =      -5803
343074  meter/sec      RA   =          322
68766  deg
 ZDOT =      -2487
113384                 TA   =          180
11266
                                          MA   =          180
11285
                                          Ha   =            219
946  n
mi
                                          Hp   =            215
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15013246
15                 X    =        -4537123
37
 Y    =       -4442727
07  feet           Y    =        -1405097
23  meter
 Z    =      -15826262
43                 Z    =        -4845979
18
 XDOT =      14236
042830                 XDOT =        4415
798948
 YDOT =     -19039
839480  feet/sec       YDOT =       -5754
390743  meter/sec
 ZDOT =      -8159
820813                 ZDOT =       -2465
850235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15388568
57                 X    =        -4690435
70
 Y    =        2278287
21  feet           Y    =          694421
94  meter
 Z    =      -15925053
56                 Z    =        -4853956
33
 XDOT =       5061
883656                 XDOT =        1542
862138
 YDOT =     -22175
282152  feet/sec       YDOT =       -6759
026000  meter/sec
 ZDOT =      -8063
763532                 ZDOT =       -2457
835125


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   18179
32472431  
00016717  00000-0  10270-3 0  9133
2 25544  51
6404 323
2020 0003411 269
3468  90
7294 15
53996588 40241


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
32472431   =   yrday
fracday
Element set:     913
Inclination:       51
6404  deg
RA of node:       323
2020  deg
Eccentricity:     
0003411     
Arg of perigee:   269
3468  deg
Mean anomaly:      90
7294  deg
Mean motion:   15
53996588  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4024
Checksum:              308


Coasting Arc #15 (Orbit 4028)
---------------------------------------

Vector Time (GMT): 2018/179/14:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          40358
66                 A    =         6780171
32  meter
 Y    =        4836687
63  meter          E    =           
0004769
 Z    =        4749543
10                 I    =           51
39473
 XDOT =      -6684
205987                 Wp   =           49
62936
 YDOT =       2664
612556  meter/sec      RA   =          321
15270  deg
 ZDOT =      -2651
912828                 TA   =           66
65966
                                          MA   =           66
60949
                                          Ha   =            220
078  n
mi
                                          Hp   =            216
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         132410
30                 X    =          -36800
12
 Y    =       15868397
74  feet           Y    =         4836706
74  meter
 Z    =       15582490
48                 Z    =         4749552
55
 XDOT =     -21929
809668                 XDOT =       -6700
624132
 YDOT =       8742
167179  feet/sec       YDOT =        2589
773799  meter/sec
 ZDOT =      -8700
501403                 ZDOT =       -2684
421596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11631593
57                 X    =         3545309
72
 Y    =      -10795958
63  feet           Y    =        -3290608
19  meter
 Z    =       15581748
85                 Z    =         4749317
05
 XDOT =      20480
239790                 XDOT =        6242
377088
 YDOT =       9274
881641  feet/sec       YDOT =        2826
983924  meter/sec
 ZDOT =      -8846
350645                 ZDOT =       -2696
367677


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   18179
64626465  
00016717  00000-0  10270-3 0  9147
2 25544  51
6418 321
5964 0003163 260
8487  99
2308 15
53986514 40298


Satellite: ISS
Catalog Number: 25544
Epoch time:      18179
64626465   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:       321
5964  deg
Eccentricity:     
0003163     
Arg of perigee:   260
8487  deg
Mean anomaly:      99
2308  deg
Mean motion:   15
53986514  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4029
Checksum:              339


Coasting Arc #16 (Orbit 4040)
---------------------------------------

Vector Time (GMT): 2018/180/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1472345
54                 A    =         6778599
84  meter
 Y    =       -4209910
69  meter          E    =           
0010619
 Z    =       -5114282
75                 I    =           51
36536
 XDOT =       6273
357506                 Wp   =          106
39954
 YDOT =      -4104
829808  meter/sec      RA   =          317
14965  deg
 ZDOT =       1572
712849                 TA   =          178
83996
                                          MA   =          178
83749
                                          Ha   =            220
089  n
mi
                                          Hp   =            215
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4830530
00                 X    =        -1400317
49
 Y    =      -13812042
93  feet           Y    =        -4225971
91  meter
 Z    =      -16779142
89                 Z    =        -5121260
57
 XDOT =      20581
881581                 XDOT =        6311
153257
 YDOT =     -13467
289395  feet/sec       YDOT =       -4034
465724  meter/sec
 ZDOT =       5159
819057                 ZDOT =        1603
277500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14421086
04                 X    =        -4395547
02
 Y    =       -2261226
49  feet           Y    =         -689221
83  meter
 Z    =      -16809679
31                 Z    =        -5123590
25
 XDOT =      -2505
706689                 XDOT =        -763
739399
 YDOT =     -23403
780248  feet/sec       YDOT =       -7133
472219  meter/sec
 ZDOT =       5297
199088                 ZDOT =        1614
586282


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   18180
41795601  
00016717  00000-0  10270-3 0  9154
2 25544  51
6378 317
7501 0003051 266
1993  93
8811 15
53997681 40414


Satellite: ISS
Catalog Number: 25544
Epoch time:      18180
41795601   =   yrday
fracday
Element set:     915
Inclination:       51
6378  deg
RA of node:       317
7501  deg
Eccentricity:     
0003051     
Arg of perigee:   266
1993  deg
Mean anomaly:      93
8811  deg
Mean motion:   15
53997681  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4041
Checksum:              322


Coasting Arc #17 (Orbit 4056)
---------------------------------------

Vector Time (GMT): 2018/181/09:42:42
000
Vector Time (MET): N/A
Weight (LBS)     : 922905
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         115127
03                 A    =         6781502
69  meter
 Y    =        5140135
05  meter          E    =           
0006402
 Z    =        4419061
09                 I    =           51
35073
 XDOT =      -6250
477677                 Wp   =           60
07200
 YDOT =       2979
589720  meter/sec      RA   =          312
13699  deg
 ZDOT =      -3296
210347                 TA   =           63
35207
                                          MA   =           63
28652
                                          Ha   =            220
066  n
mi
                                          Hp   =            216
075

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         377713
34                 X    =           36174
86
 Y    =       16863960
13  feet           Y    =         5140980
37  meter
 Z    =       14498231
93                 Z    =         4419429
35
 XDOT =     -20506
816525                 XDOT =       -6267
320662
 YDOT =       9775
556825  feet/sec       YDOT =        2909
598890  meter/sec
 ZDOT =     -10814
338409                 ZDOT =       -3326
613106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15182073
62                 X    =         4627496
04
 Y    =        7349580
90  feet           Y    =         2240152
26  meter
 Z    =       14499063
73                 Z    =         4419314
62
 XDOT =         51
857624                 XDOT =          15
806204
 YDOT =      21539
902159  feet/sec       YDOT =        6565
362178  meter/sec
 ZDOT =     -10950
806666                 ZDOT =       -3337
805872


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   18181
44687688  
00016717  00000-0  10270-3 0  9164
2 25544  51
6373 312
6221 0003176 269
4727  90
6061 15
53970766 40575


Satellite: ISS
Catalog Number: 25544
Epoch time:      18181
44687688   =   yrday
fracday
Element set:     916
Inclination:       51
6373  deg
RA of node:       312
6221  deg
Eccentricity:     
0003176     
Arg of perigee:   269
4727  deg
Mean anomaly:      90
6061  deg
Mean motion:   15
53970766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4057
Checksum:              333
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