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

 
Date: August 13th 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) : 72 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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


238/15:14:30 000 0 0 0 0 0 0
N/A 0 0 0 0 223 4
000/00:00:00 000 0 0 0 0 213 0

Coasting Arc #1 (Orbit 742)
---------------------------------------

Vector Time (GMT): 2018/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -424311
70                 A    =         6790111
37  meter
 Y    =        6765017
82  meter          E    =           
0018095
 Z    =         211493
96                 I    =           52
04111
 XDOT =      -4699
244584                 Wp   =           48
56159
 YDOT =       -493
727047  meter/sec      RA   =           92
19418  deg
 ZDOT =       6043
477368                 TA   =          313
70528
                                          MA   =          313
85504
                                          Ha   =            223
286  n
mi
                                          Hp   =            213
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1392098
76                 X    =         -500955
77
 Y    =       22194940
35  feet           Y    =         6759844
34  meter
 Z    =         693877
83                 Z    =          209246
48
 XDOT =     -15417
469107                 XDOT =       -4722
729745
 YDOT =      -1619
839393  feet/sec       YDOT =        -546
408375  meter/sec
 ZDOT =      19827
681653                 ZDOT =        6020
593525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15053793
86                 X    =         4588396
37
 Y    =      -16369228
92  feet           Y    =        -4989340
98  meter
 Z    =         682947
68                 Z    =          208162
45
 XDOT =       9871
145840                 XDOT =        3008
725252
 YDOT =       9945
547107  feet/sec       YDOT =        3031
402758  meter/sec
 ZDOT =      19724
984365                 ZDOT =        6012
175234


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   18225
56391584  
00016717  00000-0  10270-3 0  9006
2 25544  51
6410  92
7675 0005610  51
0745 309
0907 15
53854872  7439


Satellite: ISS
Catalog Number: 25544
Epoch time:      18225
56391584   =   yrday
fracday
Element set:     900
Inclination:       51
6410  deg
RA of node:        92
7675  deg
Eccentricity:     
0005610     
Arg of perigee:    51
0745  deg
Mean anomaly:     309
0907  deg
Mean motion:   15
53854872  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             743
Checksum:              309


Coasting Arc #2 (Orbit 757)
---------------------------------------

Vector Time (GMT): 2018/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1121636
98                 A    =         6788840
92  meter
 Y    =       -6440686
25  meter          E    =           
0009410
 Z    =       -1831744
86                 I    =           52
03592
 XDOT =       4550
623470                 Wp   =          105
03946
 YDOT =       2399
702413  meter/sec      RA   =           87
25081  deg
 ZDOT =      -5677
840649                 TA   =           94
97197
                                          MA   =           94
86453
                                          Ha   =            223
370  n
mi
                                          Hp   =            213
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3679911
34                 X    =         1202472
65
 Y    =      -21130860
41  feet           Y    =        -6427691
43  meter
 Z    =       -6009661
61                 Z    =        -1826099
82
 XDOT =      14929
867029                 XDOT =        4551
030627
 YDOT =       7873
039412  feet/sec       YDOT =        2450
592674  meter/sec
 ZDOT =     -18628
086120                 ZDOT =       -5655
734776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15945069
95                 X    =        -4860057
32
 Y    =       14357000
01  feet           Y    =         4376013
60  meter
 Z    =       -5983505
40                 Z    =        -1823772
45
 XDOT =      -5964
453217                 XDOT =       -1817
965340
 YDOT =     -14309
935045  feet/sec       YDOT =       -4361
668202  meter/sec
 ZDOT =     -18529
121384                 ZDOT =       -5647
676198


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   18226
52863097  
00016717  00000-0  10270-3 0  9017
2 25544  51
6403  87
9598 0005574  54
5024 305
6648 15
53809585  7589


Satellite: ISS
Catalog Number: 25544
Epoch time:      18226
52863097   =   yrday
fracday
Element set:     901
Inclination:       51
6403  deg
RA of node:        87
9598  deg
Eccentricity:     
0005574     
Arg of perigee:    54
5024  deg
Mean anomaly:     305
6648  deg
Mean motion:   15
53809585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             758
Checksum:              340


Coasting Arc #3 (Orbit 773)
---------------------------------------

Vector Time (GMT): 2018/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1779195
27                 A    =         6785795
40  meter
 Y    =        5683169
19  meter          E    =           
0017939
 Z    =        3233771
97                 I    =           52
02233
 XDOT =      -4345
073958                 Wp   =           77
68961
 YDOT =      -4108
289110  meter/sec      RA   =           82
30157  deg
 ZDOT =       4810
772608                 TA   =          319
56761
                                          MA   =          319
70080
                                          Ha   =            223
453  n
mi
                                          Hp   =            213
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5837254
83                 X    =        -1858321
57
 Y    =       18645568
19  feet           Y    =         5662830
70  meter
 Z    =       10609488
09                 Z    =         3224936
95
 XDOT =     -14255
491989                 XDOT =       -4322
178912
 YDOT =     -13478
638812  feet/sec       YDOT =       -4156
750526  meter/sec
 ZDOT =      15783
374697                 ZDOT =        4789
721778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15945779
25                 X    =         4860273
51
 Y    =      -11327771
83  feet           Y    =        -3452704
86  meter
 Z    =       10569091
93                 Z    =         3221459
22
 XDOT =       2520
953835                 XDOT =         768
386729
 YDOT =      18244
662937  feet/sec       YDOT =        5560
973263  meter/sec
 ZDOT =      15689
369807                 ZDOT =        4782
119917


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   18227
55765815  
00016717  00000-0  10270-3 0  9021
2 25544  51
6393  82
8318 0005683  57
3161 302
8539 15
53830083  7748


Satellite: ISS
Catalog Number: 25544
Epoch time:      18227
55765815   =   yrday
fracday
Element set:     902
Inclination:       51
6393  deg
RA of node:        82
8318  deg
Eccentricity:     
0005683     
Arg of perigee:    57
3161  deg
Mean anomaly:     302
8539  deg
Mean motion:   15
53830083  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             774
Checksum:              323


Coasting Arc #4 (Orbit 788)
---------------------------------------

Vector Time (GMT): 2018/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2482400
29                 A    =         6782125
71  meter
 Y    =       -4559003
32  meter          E    =           
0014261
 Z    =       -4379414
25                 I    =           52
00452
 XDOT =       4016
711081                 Wp   =           65
91370
 YDOT =       5516
894534  meter/sec      RA   =           77
34301  deg
 ZDOT =      -3469
557323                 TA   =          168
99588
                                          MA   =          168
96465
                                          Ha   =            223
363  n
mi
                                          Hp   =            213
372

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8144357
92                 X    =         2554468
53
 Y    =      -14957359
98  feet           Y    =        -4530840
58  meter
 Z    =      -14368157
00                 Z    =        -4367180
54
 XDOT =      13178
185961                 XDOT =        3971
574240
 YDOT =      18100
047685  feet/sec       YDOT =        5561
559694  meter/sec
 ZDOT =     -11383
062082                 ZDOT =       -3450
155511

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15464053
90                 X    =        -4713443
63
 Y    =        7246288
52  feet           Y    =         2208668
74  meter
 Z    =      -14312632
84                 Z    =        -4362490
49
 XDOT =        462
291250                 XDOT =         140
906373
 YDOT =     -21305
168890  feet/sec       YDOT =       -6493
815478  meter/sec
 ZDOT =     -11296
653584                 ZDOT =       -3443
220012


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   18228
52236915  
00016717  00000-0  10270-3 0  9034
2 25544  51
6392  78
0242 0005544  60
6071 299
5634 15
53839547  7891


Satellite: ISS
Catalog Number: 25544
Epoch time:      18228
52236915   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:        78
0242  deg
Eccentricity:     
0005544     
Arg of perigee:    60
6071  deg
Mean anomaly:     299
5634  deg
Mean motion:   15
53839547  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             789
Checksum:              329


Coasting Arc #5 (Orbit 804)
---------------------------------------

Vector Time (GMT): 2018/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3165527
05                 A    =         6779342
08  meter
 Y    =        3162533
76  meter          E    =           
0009657
 Z    =        5084744
71                 I    =           51
98704
 XDOT =      -3580
012872                 Wp   =           93
64890
 YDOT =      -6536
470092  meter/sec      RA   =           72
37536  deg
 ZDOT =       1833
120002                 TA   =          338
68360
                                          MA   =          338
72380
                                          Ha   =            223
623  n
mi
                                          Hp   =            213
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10385587
43                 X    =        -3225354
94
 Y    =       10375766
94  feet           Y    =         3126800
23  meter
 Z    =       16682233
30                 Z    =         5069222
42
 XDOT =     -11745
449054                 XDOT =       -3515
558449
 YDOT =     -21445
111852  feet/sec       YDOT =       -6576
143853  meter/sec
 ZDOT =       6014
173235                 ZDOT =        1815
886336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14552525
36                 X    =         4435609
73
 Y    =       -2464849
93  feet           Y    =         -751286
26  meter
 Z    =       16612115
88                 Z    =         5063372
92
 XDOT =      -2851
423754                 XDOT =        -869
113960
 YDOT =      23262
158245  feet/sec       YDOT =        7090
305833  meter/sec
 ZDOT =       5937
647722                 ZDOT =        1809
795026


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   18229
55139361  
00016717  00000-0  10270-3 0  9046
2 25544  51
6395  72
8960 0005713  64
8309 295
3436 15
53814412  8058


Satellite: ISS
Catalog Number: 25544
Epoch time:      18229
55139361   =   yrday
fracday
Element set:     904
Inclination:       51
6395  deg
RA of node:        72
8960  deg
Eccentricity:     
0005713     
Arg of perigee:    64
8309  deg
Mean anomaly:     295
3436  deg
Mean motion:   15
53814412  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             805
Checksum:              318


Coasting Arc #6 (Orbit 819)
---------------------------------------

Vector Time (GMT): 2018/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3855899
71                 A    =         6778173
97  meter
 Y    =       -1624789
75  meter          E    =           
0020266
 Z    =       -5349877
93                 I    =           51
97060
 XDOT =       2951
701005                 Wp   =           84
07985
 YDOT =       7060
953619  meter/sec      RA   =           67
40164  deg
 ZDOT =        -15
046845                 TA   =          185
76545
                                          MA   =          185
78882
                                          Ha   =            223
450  n
mi
                                          Hp   =            213
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12650589
61                 X    =         3899768
69
 Y    =       -5330675
03  feet           Y    =        -1581425
16  meter
 Z    =      -17552092
95                 Z    =        -5331040
88
 XDOT =       9684
058414                 XDOT =        2872
597183
 YDOT =      23165
858330  feet/sec       YDOT =        7093
519285  meter/sec
 ZDOT =        -49
366291                 ZDOT =           -
900777

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13562304
38                 X    =        -4133790
37
 Y    =       -2736268
23  feet           Y    =         -834014
56  meter
 Z    =      -17467289
92                 Z    =        -5324029
97
 XDOT =       4757
938437                 XDOT =        1450
219636
 YDOT =     -23625
320460  feet/sec       YDOT =       -7200
997676  meter/sec
 ZDOT =         13
209634                 ZDOT =           4
026296


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   18230
51610087  
00016717  00000-0  10270-3 0  9054
2 25544  51
6378  68
0883 0005671  69
0579 291
1180 15
53849937  8206


Satellite: ISS
Catalog Number: 25544
Epoch time:      18230
51610087   =   yrday
fracday
Element set:     905
Inclination:       51
6378  deg
RA of node:        68
0883  deg
Eccentricity:     
0005671     
Arg of perigee:    69
0579  deg
Mean anomaly:     291
1180  deg
Mean motion:   15
53849937  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             820
Checksum:              324


Coasting Arc #7 (Orbit 835)
---------------------------------------

Vector Time (GMT): 2018/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4470234
41                 A    =         6779302
32  meter
 Y    =          41631
94  meter          E    =           
0010862
 Z    =        5089392
90                 I    =           51
96124
 XDOT =      -2134
679585                 Wp   =           63
83081
 YDOT =      -7145
655484  meter/sec      RA   =           62
42793  deg
 ZDOT =      -1808
880679                 TA   =           43
62694
                                          MA   =           43
54111
                                          Ha   =            223
591  n
mi
                                          Hp   =            213
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14666123
39                 X    =        -4495089
10
 Y    =         136587
72  feet           Y    =           -8496
31  meter
 Z    =       16697483
27                 Z    =         5067617
87
 XDOT =      -7003
541947                 XDOT =       -2045
829722
 YDOT =     -23443
751588  feet/sec       YDOT =       -7169
030150  meter/sec
 ZDOT =      -5934
647896                 ZDOT =       -1819
034356

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12455587
66                 X    =         3796463
12
 Y    =        7951609
51  feet           Y    =         2423650
58  meter
 Z    =       16599699
43                 Z    =         5059588
39
 XDOT =      -6384
515029                 XDOT =       -1946
000181
 YDOT =      22535
811201  feet/sec       YDOT =        6868
915254  meter/sec
 ZDOT =      -5979
270081                 ZDOT =       -1822
481521


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   18231
54512200  
00016717  00000-0  10270-3 0  9067
2 25544  51
6384  62
9609 0005513  72
7129 287
4626 15
53834942  8369


Satellite: ISS
Catalog Number: 25544
Epoch time:      18231
54512200   =   yrday
fracday
Element set:     906
Inclination:       51
6384  deg
RA of node:        62
9609  deg
Eccentricity:     
0005513     
Arg of perigee:    72
7129  deg
Mean anomaly:     287
4626  deg
Mean motion:   15
53834942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             836
Checksum:              310


Coasting Arc #8 (Orbit 850)
---------------------------------------

Vector Time (GMT): 2018/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4981859
98                 A    =         6782100
52  meter
 Y    =        1420302
82  meter          E    =           
0013801
 Z    =       -4390122
60                 I    =           51
95394
 XDOT =       1106
488540                 Wp   =           97
15623
 YDOT =       6747
478245  meter/sec      RA   =           57
45708  deg
 ZDOT =       3446
187953                 TA   =          207
66258
                                          MA   =          207
73607
                                          Ha   =            223
500  n
mi
                                          Hp   =            213
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16344684
98                 X    =         4986932
18
 Y    =        4659786
15  feet           Y    =         1476041
83  meter
 Z    =      -14403289
38                 Z    =        -4365910
37
 XDOT =       3630
211744                 XDOT =        1014
214548
 YDOT =      22137
395816  feet/sec       YDOT =        6759
335795  meter/sec
 ZDOT =      11306
390921                 ZDOT =        3451
338787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11450409
32                 X    =        -3490084
76
 Y    =      -12683254
80  feet           Y    =        -3865856
06  meter
 Z    =      -14294763
13                 Z    =        -4357043
80
 XDOT =       7828
834790                 XDOT =        2386
228844
 YDOT =     -19807
522215  feet/sec       YDOT =       -6037
332771  meter/sec
 ZDOT =      11328
590012                 ZDOT =        3452
954236


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   18232
50982723  
00016717  00000-0  10270-3 0  9076
2 25544  51
6379  58
1526 0005651  76
9672 283
2111 15
53853264  8518


Satellite: ISS
Catalog Number: 25544
Epoch time:      18232
50982723   =   yrday
fracday
Element set:     907
Inclination:       51
6379  deg
RA of node:        58
1526  deg
Eccentricity:     
0005651     
Arg of perigee:    76
9672  deg
Mean anomaly:     283
2111  deg
Mean motion:   15
53853264  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             851
Checksum:              318


Coasting Arc #9 (Orbit 866)
---------------------------------------

Vector Time (GMT): 2018/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5291605
22                 A    =         6785736
99  meter
 Y    =       -2727200
16  meter          E    =           
0018206
 Z    =        3241578
59                 I    =           51
94726
 XDOT =        134
901917                 Wp   =           89
02567
 YDOT =      -5988
518730  meter/sec      RA   =           52
49477  deg
 ZDOT =      -4794
556701                 TA   =           53
57906
                                          MA   =           53
41132
                                          Ha   =            223
501  n
mi
                                          Hp   =            213
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17360909
51                 X    =        -5276461
30
 Y    =       -8947507
09  feet           Y    =        -2786289
91  meter
 Z    =       10635100
37                 Z    =         3215910
90
 XDOT =        442
591591                 XDOT =         225
146286
 YDOT =     -19647
371163  feet/sec       YDOT =       -5986
505524  meter/sec
 ZDOT =     -15730
172905                 ZDOT =       -4793
682284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10299440
48                 X    =         3139269
46
 Y    =       16667658
72  feet           Y    =         5080302
38  meter
 Z    =       10520223
41                 Z    =         3206564
10
 XDOT =      -9407
117553                 XDOT =       -2867
289430
 YDOT =      15787
587718  feet/sec       YDOT =        4812
056737  meter/sec
 ZDOT =     -15725
411690                 ZDOT =       -4793
105483


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   18233
53884293  
00016717  00000-0  10270-3 0  9084
2 25544  51
6377  53
0247 0005512  79
7050 280
4724 15
53864892  8672


Satellite: ISS
Catalog Number: 25544
Epoch time:      18233
53884293   =   yrday
fracday
Element set:     908
Inclination:       51
6377  deg
RA of node:        53
0247  deg
Eccentricity:     
0005512     
Arg of perigee:    79
7050  deg
Mean anomaly:     280
4724  deg
Mean motion:   15
53864892  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             867
Checksum:              330


Coasting Arc #10 (Orbit 881)
---------------------------------------

Vector Time (GMT): 2018/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923006
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5364764
08                 A    =         6788752
80  meter
 Y    =        3727961
85  meter          E    =           
0011994
 Z    =       -1840358
26                 I    =           51
93562
 XDOT =      -1498
081675                 Wp   =           58
52065
 YDOT =       4937
302522  meter/sec      RA   =           47
53987  deg
 ZDOT =       5667
583345                 TA   =          281
33409
                                          MA   =          281
46883
                                          Ha   =            223
560  n
mi
                                          Hp   =            213
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17600932
03                 X    =         5331617
61
 Y    =       12230845
97  feet           Y    =         3787769
03  meter
 Z    =       -6037920
80                 Z    =        -1814378
99
 XDOT =      -4914
966124                 XDOT =       -1580
710318
 YDOT =      16198
499088  feet/sec       YDOT =        4920
087897  meter/sec
 ZDOT =      18594
433548                 ZDOT =        5660
105639

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9117428
64                 X    =        -2778992
25
 Y    =      -19433162
01  feet           Y    =        -5923227
78  meter
 Z    =       -5921790
13                 Z    =        -1804961
63
 XDOT =      11072
624240                 XDOT =        3374
935868
 YDOT =     -10816
813644  feet/sec       YDOT =       -3296
964799  meter/sec
 ZDOT =      18560
162179                 ZDOT =        5657
137432


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   18234
50354676  
00016717  00000-0  10270-3 0  9090
2 25544  51
6370  48
2175 0005702  85
3715 274
8089 15
53849609  8820


Satellite: ISS
Catalog Number: 25544
Epoch time:      18234
50354676   =   yrday
fracday
Element set:     909
Inclination:       51
6370  deg
RA of node:        48
2175  deg
Eccentricity:     
0005702     
Arg of perigee:    85
3715  deg
Mean anomaly:     274
8089  deg
Mean motion:   15
53849609  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             882
Checksum:              334


Coasting Arc #11 (Orbit 897)
---------------------------------------

Vector Time (GMT): 2018/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5102757
01                 A    =         6789963
04  meter
 Y    =       -4465657
90  meter          E    =           
0016797
 Z    =         211218
27                 I    =           51
91790
 XDOT =       2966
686825                 Wp   =          118
22886
 YDOT =      -3692
034013  meter/sec      RA   =           42
58930  deg
 ZDOT =      -6030
957910                 TA   =           59
50427
                                          MA   =           59
33853
                                          Ha   =            223
405  n
mi
                                          Hp   =            212
980

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16741328
79                 X    =        -5053467
52
 Y    =      -14651108
61  feet           Y    =        -4522444
87  meter
 Z    =         692973
31                 Z    =          186551
02
 XDOT =       9733
224490                 XDOT =        3037
046378
 YDOT =     -12112
972483  feet/sec       YDOT =       -3658
465092  meter/sec
 ZDOT =     -19786
607317                 ZDOT =       -6016
376123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7489650
61                 X    =         2282845
51
 Y    =       20951675
62  feet           Y    =         6386070
73  meter
 Z    =         582844
10                 Z    =          177650
88
 XDOT =     -12987
787982                 XDOT =       -3958
677777
 YDOT =       5230
026011  feet/sec       YDOT =        1594
111928  meter/sec
 ZDOT =     -19720
609814                 ZDOT =       -6010
841871


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   18235
53255891  
00016717  00000-0  10270-3 0  9105
2 25544  51
6378  43
0891 0005637  85
9157 274
2640 15
53906072  8981


Satellite: ISS
Catalog Number: 25544
Epoch time:      18235
53255891   =   yrday
fracday
Element set:     910
Inclination:       51
6378  deg
RA of node:        43
0891  deg
Eccentricity:     
0005637     
Arg of perigee:    85
9157  deg
Mean anomaly:     274
2640  deg
Mean motion:   15
53906072  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             898
Checksum:              330


Coasting Arc #12 (Orbit 913)
---------------------------------------

Vector Time (GMT): 2018/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4527276
19                 A    =         6789250
92  meter
 Y    =        4857359
87  meter          E    =           
0019017
 Z    =        1379224
76                 I    =           51
89019
 XDOT =      -4370
720922                 Wp   =           69
67207
 YDOT =       2402
261317  meter/sec      RA   =           37
63768  deg
 ZDOT =       5828
033405                 TA   =          305
30727
                                          MA   =          305
48496
                                          Ha   =            223
531  n
mi
                                          Hp   =            212
927

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14853268
34                 X    =         4465923
95
 Y    =       15936220
04  feet           Y    =         4907643
99  meter
 Z    =        4525015
62                 Z    =         1401067
18
 XDOT =     -14339
635570                 XDOT =       -4425
567816
 YDOT =       7881
434768  feet/sec       YDOT =        2353
078339  meter/sec
 ZDOT =      19120
844503                 ZDOT =        5806
669098

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5547164
86                 X    =        -1690775
85
 Y    =      -21045684
71  feet           Y    =        -6414724
70  meter
 Z    =        4622399
08                 Z    =         1408907
24
 XDOT =      14939
526584                 XDOT =        4553
567703
 YDOT =        282
016250  feet/sec       YDOT =          85
958553  meter/sec
 ZDOT =      19024
576652                 ZDOT =        5798
690963


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   18236
56157157  
00016717  00000-0  10270-3 0  9116
2 25544  51
6378  37
9611 0005813  93
1046 267
0771 15
53867996  9142


Satellite: ISS
Catalog Number: 25544
Epoch time:      18236
56157157   =   yrday
fracday
Element set:     911
Inclination:       51
6378  deg
RA of node:        37
9611  deg
Eccentricity:     
0005813     
Arg of perigee:    93
1046  deg
Mean anomaly:     267
0771  deg
Mean motion:   15
53867996  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             914
Checksum:              332


Coasting Arc #13 (Orbit 928)
---------------------------------------

Vector Time (GMT): 2018/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3570817
96                 A    =         6786445
93  meter
 Y    =       -4994203
76  meter          E    =           
0010281
 Z    =       -2897314
57                 I    =           51
85426
 XDOT =       5641
625648                 Wp   =          103
45195
 YDOT =      -1106
048607  meter/sec      RA   =           32
68045  deg
 ZDOT =      -5063
942395                 TA   =          109
41386
                                          MA   =          109
30272
                                          Ha   =            223
509  n
mi
                                          Hp   =            212
900

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11715282
02                 X    =        -3500632
64
 Y    =      -16385182
93  feet           Y    =        -5033742
79  meter
 Z    =       -9505625
24                 Z    =        -2914489
39
 XDOT =      18509
270499                 XDOT =        5678
171999
 YDOT =      -3628
768396  feet/sec       YDOT =       -1042
755890  meter/sec
 ZDOT =     -16613
984235                 ZDOT =       -5036
449042

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2882164
47                 X    =          878483
73
 Y    =       19898665
01  feet           Y    =         6065113
09  meter
 Z    =       -9582026
01                 Z    =        -2920601
53
 XDOT =     -16770
801072                 XDOT =       -5111
740167
 YDOT =      -5484
392527  feet/sec       YDOT =       -1671
642842  meter/sec
 ZDOT =     -16490
386708                 ZDOT =       -5026
269869


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   18237
52626846  
00016717  00000-0  10270-3 0  9120
2 25544  51
6379  33
1541 0005841  95
6251 264
5568 15
53875913  9299


Satellite: ISS
Catalog Number: 25544
Epoch time:      18237
52626846   =   yrday
fracday
Element set:     912
Inclination:       51
6379  deg
RA of node:        33
1541  deg
Eccentricity:     
0005841     
Arg of perigee:    95
6251  deg
Mean anomaly:     264
5568  deg
Mean motion:   15
53875913  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             929
Checksum:              333


Coasting Arc #14 (Orbit 944)
---------------------------------------

Vector Time (GMT): 2018/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2342377
29                 A    =         6782861
75  meter
 Y    =        4866187
49  meter          E    =           
0016200
 Z    =        4092481
26                 I    =           51
81492
 XDOT =      -6635
124320                 Wp   =          102
00135
 YDOT =        -61
164415  meter/sec      RA   =           27
71210  deg
 ZDOT =       3854
258306                 TA   =          308
20750
                                          MA   =          308
35326
                                          Ha   =            223
407  n
mi
                                          Hp   =            212
974

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7684964
87                 X    =         2267909
37
 Y    =       15965182
06  feet           Y    =         4891965
43  meter
 Z    =       13426775
78                 Z    =         4103678
38
 XDOT =     -21768
780576                 XDOT =       -6652
668862
 YDOT =       -200
670653  feet/sec       YDOT =        -135
460855  meter/sec
 ZDOT =      12645
204416                 ZDOT =        3821
985122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         230611
47                 X    =           70290
38
 Y    =      -17679332
24  feet           Y    =        -5388660
47  meter
 Z    =       13476351
92                 Z    =         4107592
06
 XDOT =      18231
634410                 XDOT =        5557
002168
 YDOT =       9806
642777  feet/sec       YDOT =        2989
064719  meter/sec
 ZDOT =      12500
322024                 ZDOT =        3810
098153


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   18238
55527603  
00016717  00000-0  10270-3 0  9136
2 25544  51
6388  28
0260 0005695 100
8819 259
2975 15
53889436  9452


Satellite: ISS
Catalog Number: 25544
Epoch time:      18238
55527603   =   yrday
fracday
Element set:     913
Inclination:       51
6388  deg
RA of node:        28
0260  deg
Eccentricity:     
0005695     
Arg of perigee:   100
8819  deg
Mean anomaly:     259
2975  deg
Mean motion:   15
53889436  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             945
Checksum:              342


Coasting Arc #15 (Orbit 946)
---------------------------------------

Vector Time (GMT): 2018/238/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1517974
03                 A    =         6778025
93  meter
 Y    =        3918190
38  meter          E    =           
0008146
 Z    =        5311600
00                 I    =           51
79791
 XDOT =      -6959
105595                 Wp   =          101
93363
 YDOT =      -3213
551671  meter/sec      RA   =           27
01987  deg
 ZDOT =        379
588237                 TA   =          344
44531
                                          MA   =          344
47033
                                          Ha   =            223
439  n
mi
                                          Hp   =            212
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4980229
75                 X    =        -1587476
02
 Y    =       12854955
31  feet           Y    =         3900827
04  meter
 Z    =       17426509
20                 Z    =         5304057
31
 XDOT =     -22831
711271                 XDOT =       -6924
497368
 YDOT =     -10543
148528  feet/sec       YDOT =       -3291
179682  meter/sec
 ZDOT =       1245
368233                 ZDOT =         345
868132

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -228520
23                 X    =          -69652
97
 Y    =      -13827466
94  feet           Y    =        -4214611
92  meter
 Z    =       17392087
96                 Z    =         5301108
41
 XDOT =      24128
456797                 XDOT =        7354
353632
 YDOT =        986
651036  feet/sec       YDOT =         300
731236  meter/sec
 ZDOT =       1094
440796                 ZDOT =         333
585555


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   18238
68390078  
00016717  00000-0  10270-3 0  9145
2 25544  51
6419  27
3863 0005584 101
2652 258
9128 15
53905846  9477


Satellite: ISS
Catalog Number: 25544
Epoch time:      18238
68390078   =   yrday
fracday
Element set:     914
Inclination:       51
6419  deg
RA of node:        27
3863  deg
Eccentricity:     
0005584     
Arg of perigee:   101
2652  deg
Mean anomaly:     258
9128  deg
Mean motion:   15
53905846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             947
Checksum:              336


Coasting Arc #16 (Orbit 961)
---------------------------------------

Vector Time (GMT): 2018/239/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3053409
84                 A    =         6778801
51  meter
 Y    =       -3163599
21  meter          E    =           
0019402
 Z    =       -5176753
68                 I    =           51
77039
 XDOT =       6453
256678                 Wp   =          101
37695
 YDOT =       3848
509308  meter/sec      RA   =           22
03385  deg
 ZDOT =       1455
338277                 TA   =          182
62687
                                          MA   =          182
63708
                                          Ha   =            223
438  n
mi
                                          Hp   =            213
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10017748
82                 X    =         3113704
73
 Y    =      -10379262
49  feet           Y    =        -3129117
10  meter
 Z    =      -16984100
00                 Z    =        -5161774
81
 XDOT =      21172
101962                 XDOT =        6402
672799
 YDOT =      12626
342873  feet/sec       YDOT =        3920
391367  meter/sec
 ZDOT =       4774
731880                 ZDOT =        1486
562378

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5138017
82                 X    =        -1566067
83
 Y    =       13563922
13  feet           Y    =         4134283
47  meter
 Z    =      -16916406
92                 Z    =        -5156120
83
 XDOT =     -23435
349509                 XDOT =       -7143
094530
 YDOT =      -2752
001035  feet/sec       YDOT =        -838
809915  meter/sec
 ZDOT =       4914
351331                 ZDOT =        1497
894286


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   18239
64859395  
00016717  00000-0  10270-3 0  9155
2 25544  51
6420  22
5802 0005699 102
9457 257
2332 15
53888884  9625


Satellite: ISS
Catalog Number: 25544
Epoch time:      18239
64859395   =   yrday
fracday
Element set:     915
Inclination:       51
6420  deg
RA of node:        22
5802  deg
Eccentricity:     
0005699     
Arg of perigee:   102
9457  deg
Mean anomaly:     257
2332  deg
Mean motion:   15
53888884  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             962
Checksum:              344
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