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

 
Date: August 20th 2018

ISS TRAJECTORY DATA

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

242/21:52:00 000 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 850)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4981939
08                 A    =         6782090
13  meter
 Y    =        1420794
77  meter          E    =           
0013759
 Z    =       -4389800
41                 I    =           51
95394
 XDOT =       1106
045275                 Wp   =           97
00608
 YDOT =       6747
349334  meter/sec      RA   =           57
45629  deg
 ZDOT =       3446
688333                 TA   =          207
81820
                                          MA   =          207
89184
                                          Ha   =            223
483  n
mi
                                          Hp   =            213
199

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16344944
48                 X    =         4987004
20
 Y    =        4661400
15  feet           Y    =         1476534
62  meter
 Z    =      -14402232
33                 Z    =        -4365587
82
 XDOT =       3628
757464                 XDOT =        1013
770328
 YDOT =      22136
972881  feet/sec       YDOT =        6759
201922  meter/sec
 ZDOT =      11308
032589                 ZDOT =        3451
837012

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11449765
40                 X    =        -3489888
49
 Y    =      -12684756
26  feet           Y    =        -3866313
71  meter
 Z    =      -14293704
50                 Z    =        -4356721
13
 XDOT =       7829
741726                 XDOT =        2386
505278
 YDOT =     -19806
432367  feet/sec       YDOT =       -6037
000585  meter/sec
 ZDOT =      11330
222017                 ZDOT =        3453
451671


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
50982610  
00016717  00000-0  10270-3 0  9004
2 25544  51
6379  58
1519 0005626  76
4843 283
6936 15
53857206  8516


Satellite: ISS
Catalog Number: 25544
Epoch time:      18232
50982610   =   yrday
fracday
Element set:     900
Inclination:       51
6379  deg
RA of node:        58
1519  deg
Eccentricity:     
0005626     
Arg of perigee:    76
4843  deg
Mean anomaly:     283
6936  deg
Mean motion:   15
53857206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             851
Checksum:              324


Coasting Arc #2 (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    =       -5291620
38                 A    =         6785728
62  meter
 Y    =       -2729016
98  meter          E    =           
0018176
 Z    =        3240083
10                 I    =           51
94727
 XDOT =        136
945387                 Wp   =           88
90681
 YDOT =      -5987
396621  meter/sec      RA   =           52
49395  deg
 ZDOT =      -4795
841717                 TA   =           53
71831
                                          MA   =           53
55055
                                          Ha   =            223
483  n
mi
                                          Hp   =            213
128

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17360959
25                 X    =        -5276448
88
 Y    =       -8953467
78  feet           Y    =        -2788106
75  meter
 Z    =       10630193
89                 Z    =         3214415
40
 XDOT =        449
295890                 XDOT =         227
183298
 YDOT =     -19643
689702  feet/sec       YDOT =       -5985
360599  meter/sec
 ZDOT =     -15734
388836                 ZDOT =       -4794
957389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10296374
54                 X    =         3138334
96
 Y    =       16672770
91  feet           Y    =         5081860
57  meter
 Z    =       10515317
16                 Z    =         3205068
67
 XDOT =      -9410
605857                 XDOT =       -2868
352665
 YDOT =      15781
180700  feet/sec       YDOT =        4810
103877  meter/sec
 ZDOT =     -15729
583273                 ZDOT =       -4794
376982


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
53883908  
00016717  00000-0  10270-3 0  9019
2 25544  51
6376  53
0241 0005488  79
1987 280
9783 15
53869190  8676


Satellite: ISS
Catalog Number: 25544
Epoch time:      18233
53883908   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:        53
0241  deg
Eccentricity:     
0005488     
Arg of perigee:    79
1987  deg
Mean anomaly:     280
9783  deg
Mean motion:   15
53869190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             867
Checksum:              349


Coasting Arc #3 (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    =        5363935
71                 A    =         6788744
45  meter
 Y    =        3730632
36  meter          E    =           
0012000
 Z    =       -1837157
73                 I    =           51
93563
 XDOT =      -1501
860951                 Wp   =           58
23178
 YDOT =       4934
685656  meter/sec      RA   =           47
53903  deg
 ZDOT =       5668
938799                 TA   =          281
65935
                                          MA   =          281
79400
                                          Ha   =            223
543  n
mi
                                          Hp   =            213
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17598214
26                 X    =         5330743
89
 Y    =       12239607
49  feet           Y    =         3790430
03  meter
 Z    =       -6027420
39                 Z    =        -1811182
60
 XDOT =      -4927
365325                 XDOT =       -1584
466635
 YDOT =      16189
913569  feet/sec       YDOT =        4917
428897  meter/sec
 ZDOT =      18598
880575                 ZDOT =        5661
442791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9110619
26                 X    =        -2776916
75
 Y    =      -19439341
04  feet           Y    =        -5925111
15  meter
 Z    =       -5911308
65                 Z    =        -1801766
88
 XDOT =      11078
613055                 XDOT =        3376
761259
 YDOT =     -10803
646134  feet/sec       YDOT =       -3292
951342  meter/sec
 ZDOT =      18564
527389                 ZDOT =        5658
467948


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
50354018  
00016717  00000-0  10270-3 0  9023
2 25544  51
6370  48
2168 0005675  84
8885 275
2915 15
53854174  8829


Satellite: ISS
Catalog Number: 25544
Epoch time:      18234
50354018   =   yrday
fracday
Element set:     902
Inclination:       51
6370  deg
RA of node:        48
2168  deg
Eccentricity:     
0005675     
Arg of perigee:    84
8885  deg
Mean anomaly:     275
2915  deg
Mean motion:   15
53854174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             882
Checksum:              326


Coasting Arc #4 (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    =       -5100405
26                 A    =         6789949
32  meter
 Y    =       -4468616
81  meter          E    =           
0016739
 Z    =         206279
11                 I    =           51
91790
 XDOT =       2971
977933                 Wp   =          118
15605
 YDOT =      -3687
373806  meter/sec      RA   =           42
58845  deg
 ZDOT =      -6031
154056                 TA   =           59
63013
                                          MA   =           59
46475
                                          Ha   =            223
388  n
mi
                                          Hp   =            212
982

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16733613
06                 X    =        -5051058
86
 Y    =      -14660816
31  feet           Y    =        -4525377
16  meter
 Z    =         676768
73                 Z    =          181623
42
 XDOT =       9750
583769                 XDOT =        3042
285934
 YDOT =     -12097
683091  feet/sec       YDOT =       -3653
746005  meter/sec
 ZDOT =     -19787
250839                 ZDOT =       -6016
546692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7478089
37                 X    =         2279321
64
 Y    =       20956345
02  feet           Y    =         6387493
96  meter
 Z    =         566691
85                 Z    =          172727
68
 XDOT =     -12995
165673                 XDOT =       -3960
926497
 YDOT =       5209
059128  feet/sec       YDOT =        1587
721222  meter/sec
 ZDOT =     -19721
139151                 ZDOT =       -6011
003213


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
53254918  
00016717  00000-0  10270-3 0  9036
2 25544  51
6378  43
0884 0005613  85
4068 274
7726 15
53911023  8985


Satellite: ISS
Catalog Number: 25544
Epoch time:      18235
53254918   =   yrday
fracday
Element set:     903
Inclination:       51
6378  deg
RA of node:        43
0884  deg
Eccentricity:     
0005613     
Arg of perigee:    85
4068  deg
Mean anomaly:     274
7726  deg
Mean motion:   15
53911023  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             898
Checksum:              325


Coasting Arc #5 (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    =        4522452
93                 A    =         6789228
11  meter
 Y    =        4859930
13  meter          E    =           
0019017
 Z    =        1385701
13                 I    =           51
89016
 XDOT =      -4377
131943                 Wp   =           69
55957
 YDOT =       2395
443463  meter/sec      RA   =           37
63680  deg
 ZDOT =       5826
095012                 TA   =          305
49190
                                          MA   =          305
66918
                                          Ha   =            223
513  n
mi
                                          Hp   =            212
929

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14837444
01                 X    =         4461040
86
 Y    =       15944652
65  feet           Y    =         4910159
98  meter
 Z    =        4546263
54                 Z    =         1407519
97
 XDOT =     -14360
669105                 XDOT =       -4431
892706
 YDOT =       7859
066481  feet/sec       YDOT =        2346
189274  meter/sec
 ZDOT =      19114
484947                 ZDOT =        5804
699773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5529109
07                 X    =        -1685272
45
 Y    =      -21045585
93  feet           Y    =        -6414694
59  meter
 Z    =        4643540
78                 Z    =         1415351
23
 XDOT =      14947
483169                 XDOT =        4555
992870
 YDOT =        310
327021  feet/sec       YDOT =          94
587676  meter/sec
 ZDOT =      19018
079176                 ZDOT =        5796
710533


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
56155848  
00016717  00000-0  10270-3 0  9043
2 25544  51
6378  37
9604 0005785  92
6216 267
5599 15
53873187  9147


Satellite: ISS
Catalog Number: 25544
Epoch time:      18236
56155848   =   yrday
fracday
Element set:     904
Inclination:       51
6378  deg
RA of node:        37
9604  deg
Eccentricity:     
0005785     
Arg of perigee:    92
6216  deg
Mean anomaly:     267
5599  deg
Mean motion:   15
53873187  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             914
Checksum:              354


Coasting Arc #6 (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    =       -3562997
19                 A    =         6786412
37  meter
 Y    =       -4995694
04  meter          E    =           
0010246
 Z    =       -2904400
70                 I    =           51
85420
 XDOT =       5647
978111                 Wp   =          103
04731
 YDOT =      -1097
200565  meter/sec      RA   =           32
67951  deg
 ZDOT =      -5058
728634                 TA   =          109
90903
                                          MA   =          109
79861
                                          Ha   =            223
491  n
mi
                                          Hp   =            212
899

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11689623
32                 X    =        -3492761
36
 Y    =      -16390072
32  feet           Y    =        -5035145
34  meter
 Z    =       -9528873
68                 Z    =        -2921537
40
 XDOT =      18530
111912                 XDOT =        5684
399723
 YDOT =      -3599
739385  feet/sec       YDOT =       -1033
837507  meter/sec
 ZDOT =     -16596
878720                 ZDOT =       -5031
204727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2856967
34                 X    =          870803
65
 Y    =       19891227
45  feet           Y    =         6062846
13  meter
 Z    =       -9605103
12                 Z    =        -2927635
43
 XDOT =     -16776
524483                 XDOT =       -5113
484662
 YDOT =      -5517
847278  feet/sec       YDOT =       -1681
839850  meter/sec
 ZDOT =     -16473
145272                 ZDOT =       -5021
014679


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
52625199  
00016717  00000-0  10270-3 0  9052
2 25544  51
6379  33
1534 0005814  95
1399 265
0417 15
53881465  9297


Satellite: ISS
Catalog Number: 25544
Epoch time:      18237
52625199   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:        33
1534  deg
Eccentricity:     
0005814     
Arg of perigee:    95
1399  deg
Mean anomaly:     265
0417  deg
Mean motion:   15
53881465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             929
Checksum:              333


Coasting Arc #7 (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    =        2330903
42                 A    =         6782821
13  meter
 Y    =        4866013
11  meter          E    =           
0016146
 Z    =        4099156
06                 I    =           51
81483
 XDOT =      -6640
331656                 Wp   =          101
91793
 YDOT =        -71
854650  meter/sec      RA   =           27
71107  deg
 ZDOT =       3845
155865                 TA   =          308
40380
                                          MA   =          308
54868
                                          Ha   =            223
389  n
mi
                                          Hp   =            212
973

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7647320
92                 X    =         2256405
88
 Y    =       15964609
96  feet           Y    =         4891662
58  meter
 Z    =       13448674
72                 Z    =         4110297
37
 XDOT =     -21785
865012                 XDOT =       -6657
712056
 YDOT =       -235
743601  feet/sec       YDOT =        -146
208405  meter/sec
 ZDOT =      12615
340766                 ZDOT =        3812
857786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         264268
98                 X    =           80549
19
 Y    =      -17662142
82  feet           Y    =        -5383421
13  meter
 Z    =       13498000
34                 Z    =         4114190
50
 XDOT =      18232
560143                 XDOT =        5557
284332
 YDOT =       9843
115101  feet/sec       YDOT =        3000
181483  meter/sec
 ZDOT =      12470
348130                 ZDOT =        3800
962110


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
55525573  
00016717  00000-0  10270-3 0  9062
2 25544  51
6389  28
0252 0005666 100
3825 259
7966 15
53895409  9456


Satellite: ISS
Catalog Number: 25544
Epoch time:      18238
55525573   =   yrday
fracday
Element set:     906
Inclination:       51
6389  deg
RA of node:        28
0252  deg
Eccentricity:     
0005666     
Arg of perigee:   100
3825  deg
Mean anomaly:     259
7966  deg
Mean motion:   15
53895409  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             945
Checksum:              342


Coasting Arc #8 (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    =       -1530320
49                 A    =         6778005
66  meter
 Y    =        3912471
46  meter          E    =           
0008106
 Z    =        5312260
36                 I    =           51
79789
 XDOT =      -6955
687195                 Wp   =          101
42766
 YDOT =      -3222
348646  meter/sec      RA   =           27
01874  deg
 ZDOT =        367
464744                 TA   =          345
06723
                                          MA   =          345
09115
                                          Ha   =            223
421  n
mi
                                          Hp   =            212
997

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5020736
51                 X    =        -1599760
82
 Y    =       12836192
46  feet           Y    =         3894970
40  meter
 Z    =       17428675
71                 Z    =         5304657
84
 XDOT =     -22820
496045                 XDOT =       -6920
921962
 YDOT =     -10572
009993  feet/sec       YDOT =       -3299
937552  meter/sec
 ZDOT =       1205
592993                 ZDOT =         333
761626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -183902
05                 X    =          -56053
34
 Y    =      -13825692
58  feet           Y    =        -4214071
10  meter
 Z    =       17393986
71                 Z    =         5301687
15
 XDOT =      24129
064071                 XDOT =        7354
538729
 YDOT =       1014
457012  feet/sec       YDOT =         309
206497  meter/sec
 ZDOT =       1054
743077                 ZDOT =         321
485690


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
68387999  
00016717  00000-0  10270-3 0  9075
2 25544  51
6419  27
3855 0005556 100
7515 259
4263 15
53911891  9472


Satellite: ISS
Catalog Number: 25544
Epoch time:      18238
68387999   =   yrday
fracday
Element set:     907
Inclination:       51
6419  deg
RA of node:        27
3855  deg
Eccentricity:     
0005556     
Arg of perigee:   100
7515  deg
Mean anomaly:     259
4263  deg
Mean motion:   15
53911891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             947
Checksum:              351


Coasting Arc #9 (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    =        3066949
89                 A    =         6778796
16  meter
 Y    =       -3155502
84  meter          E    =           
0019355
 Z    =       -5173638
07                 I    =           51
77042
 XDOT =       6445
137282                 Wp   =          101
29659
 YDOT =       3856
896240  meter/sec      RA   =           22
03267  deg
 ZDOT =       1469
269175                 TA   =          182
84362
                                          MA   =          182
85464
                                          Ha   =            223
420  n
mi
                                          Hp   =            213
075

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10062171
55                 X    =         3127138
10
 Y    =      -10352699
61  feet           Y    =        -3120869
92  meter
 Z    =      -16973878
19                 Z    =        -5158593
69
 XDOT =      21145
463522                 XDOT =        6394
392553
 YDOT =      12653
859056  feet/sec       YDOT =        3928
686605  meter/sec
 ZDOT =       4820
436926                 ZDOT =        1500
453444

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5189291
52                 X    =        -1581696
05
 Y    =       13557296
54  feet           Y    =         4132263
99  meter
 Z    =      -16905892
18                 Z    =        -5152915
94
 XDOT =     -23422
133345                 XDOT =       -7139
066244
 YDOT =      -2784
255126  feet/sec       YDOT =        -848
640962  meter/sec
 ZDOT =       4959
876367                 ZDOT =        1511
770317


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
64856931  
00016717  00000-0  10270-3 0  9080
2 25544  51
6420  22
5794 0005672 102
4349 257
7439 15
53895441  9621


Satellite: ISS
Catalog Number: 25544
Epoch time:      18239
64856931   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:        22
5794  deg
Eccentricity:     
0005672     
Arg of perigee:   102
4349  deg
Mean anomaly:     257
7439  deg
Mean motion:   15
53895441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             962
Checksum:              335


Coasting Arc #10 (Orbit 977)
---------------------------------------

Vector Time (GMT): 2018/240/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4466237
54                 A    =         6781457
72  meter
 Y    =        2354751
53  meter          E    =           
0013916
 Z    =        4516381
71                 I    =           51
74812
 XDOT =      -5497
904642                 Wp   =           82
08346
 YDOT =      -4308
458559  meter/sec      RA   =           17
04812  deg
 ZDOT =      -3180
271807                 TA   =           39
81538
                                          MA   =           39
71336
                                          Ha   =            223
525  n
mi
                                          Hp   =            213
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14653010
29                 X    =        -4514175
05
 Y    =        7725562
77  feet           Y    =         2304539
30  meter
 Z    =       14817525
28                 Z    =         4494569
88
 XDOT =     -18037
744889                 XDOT =       -5433
869730
 YDOT =     -14135
362728  feet/sec       YDOT =       -4369
582156  meter/sec
 ZDOT =     -10433
962622                 ZDOT =       -3206
822558

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10209546
30                 X    =         3111869
71
 Y    =      -13155302
41  feet           Y    =        -4009736
17  meter
 Z    =       14719282
22                 Z    =         4486437
22
 XDOT =      21256
860746                 XDOT =        6479
091155
 YDOT =       4652
053625  feet/sec       YDOT =        1417
945945  meter/sec
 ZDOT =     -10552
525927                 ZDOT =       -3216
409903


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   18240
67756853  
00016717  00000-0  10270-3 0  9098
2 25544  51
6420  17
4519 0005653 105
7773 254
4004 15
53893937  9782


Satellite: ISS
Catalog Number: 25544
Epoch time:      18240
67756853   =   yrday
fracday
Element set:     909
Inclination:       51
6420  deg
RA of node:        17
4519  deg
Eccentricity:     
0005653     
Arg of perigee:   105
7773  deg
Mean anomaly:     254
4004  deg
Mean motion:   15
53893937  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             978
Checksum:              334


Coasting Arc #11 (Orbit 992)
---------------------------------------

Vector Time (GMT): 2018/241/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5613811
29                 A    =         6785046
15  meter
 Y    =       -1598925
74  meter          E    =           
0010309
 Z    =       -3469773
63                 I    =           51
72780
 XDOT =       4117
192415                 Wp   =          100
55128
 YDOT =       4565
298490  meter/sec      RA   =           12
07074  deg
 ZDOT =       4567
219588                 TA   =          218
84224
                                          MA   =          218
91637
                                          Ha   =            223
375  n
mi
                                          Hp   =            213
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18418016
04                 X    =         5648127
91
 Y    =       -5245819
35  feet           Y    =        -1535956
63  meter
 Z    =      -11383771
76                 Z    =        -3442420
38
 XDOT =      13507
849132                 XDOT =        4043
650985
 YDOT =      14978
013420  feet/sec       YDOT =        4610
928978  meter/sec
 ZDOT =      14984
316233                 ZDOT =        4587
040345

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14427270
14                 X    =        -4397431
94
 Y    =       12703583
61  feet           Y    =         3872052
28  meter
 Z    =      -11260774
16                 Z    =        -3432283
96
 XDOT =     -17627
667712                 XDOT =       -5372
913119
 YDOT =      -6687
239820  feet/sec       YDOT =       -2038
270697  meter/sec
 ZDOT =      15072
624496                 ZDOT =        4594
135946


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   18241
64225311  
00016717  00000-0  10270-3 0  9108
2 25544  51
6417  12
6458 0005550 110
0985 250
0765 15
53885601  9939


Satellite: ISS
Catalog Number: 25544
Epoch time:      18241
64225311   =   yrday
fracday
Element set:     910
Inclination:       51
6417  deg
RA of node:        12
6458  deg
Eccentricity:     
0005550     
Arg of perigee:   110
0985  deg
Mean anomaly:     250
0765  deg
Mean motion:   15
53885601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             993
Checksum:              291


Coasting Arc #12 (Orbit 1008)
---------------------------------------

Vector Time (GMT): 2018/242/15:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6407432
41                 A    =         6788312
51  meter
 Y    =         833725
73  meter          E    =           
0019562
 Z    =        2050821
26                 I    =           51
70645
 XDOT =      -2402
912311                 Wp   =          111
19255
 YDOT =      -4718
170912  meter/sec      RA   =            7
09968  deg
 ZDOT =      -5553
663954                 TA   =           46
13558
                                          MA   =           45
97412
                                          Ha   =            223
408  n
mi
                                          Hp   =            213
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21021759
89                 X    =        -6426240
94
 Y    =        2735320
62  feet           Y    =          761968
37  meter
 Z    =        6728416
21                 Z    =         2019650
51
 XDOT =      -7883
570574                 XDOT =       -2322
997126
 YDOT =     -15479
563359  feet/sec       YDOT =       -4744
595551  meter/sec
 ZDOT =     -18220
682264                 ZDOT =       -5565
141962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17629617
96                 X    =         5373507
55
 Y    =      -11851473
14  feet           Y    =        -3612329
01  meter
 Z    =        6588407
04                 Z    =         2008146
47
 XDOT =      12992
179447                 XDOT =        3960
016296
 YDOT =       9102
525668  feet/sec       YDOT =        2774
449823  meter/sec
 ZDOT =     -18271
517843                 ZDOT =       -5569
158638


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   18242
67124702  
00016717  00000-0  10270-3 0  9115
2 25544  51
6419   7
5183 0005624 112
0371 248
1379 15
53891925 10096


Satellite: ISS
Catalog Number: 25544
Epoch time:      18242
67124702   =   yrday
fracday
Element set:     911
Inclination:       51
6419  deg
RA of node:         7
5183  deg
Eccentricity:     
0005624     
Arg of perigee:   112
0371  deg
Mean anomaly:     248
1379  deg
Mean motion:   15
53891925  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1009
Checksum:              295


Coasting Arc #13 (Orbit 1012)
---------------------------------------

Vector Time (GMT): 2018/242/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -472891
17                 A    =         6778276
27  meter
 Y    =       -4244850
89  meter          E    =           
0019879
 Z    =       -5280487
58                 I    =           51
66106
 XDOT =       7610
955518                 Wp   =           90
75820
 YDOT =        135
703837  meter/sec      RA   =            5
75045  deg
 ZDOT =       -793
526925                 TA   =          171
66227
                                          MA   =          171
62919
                                          Ha   =            223
421  n
mi
                                          Hp   =            213
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1551480
23                 X    =         -399739
15
 Y    =      -13926676
15  feet           Y    =        -4249730
48  meter
 Z    =      -17324434
32                 Z    =        -5282606
72
 XDOT =      24970
326503                 XDOT =        7612
726909
 YDOT =        445
222562  feet/sec       YDOT =         220
824658  meter/sec
 ZDOT =      -2603
434793                 ZDOT =        -756
551316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10397787
58                 X    =         3169245
65
 Y    =       -9377467
70  feet           Y    =        -2858252
15  meter
 Z    =      -17333336
01                 Z    =        -5283200
82
 XDOT =      13699
745981                 XDOT =        4175
682575
 YDOT =      19678
634418  feet/sec       YDOT =        5998
047770  meter/sec
 ZDOT =      -2437
517316                 ZDOT =        -742
955278


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   18242
92849552  
00016717  00000-0  10270-3 0  9121
2 25544  51
6391   6
2374 0005686 109
4820 250
6947 15
53876969 10135


Satellite: ISS
Catalog Number: 25544
Epoch time:      18242
92849552   =   yrday
fracday
Element set:     912
Inclination:       51
6391  deg
RA of node:         6
2374  deg
Eccentricity:     
0005686     
Arg of perigee:   109
4820  deg
Mean anomaly:     250
6947  deg
Mean motion:   15
53876969  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1013
Checksum:              330


Coasting Arc #14 (Orbit 1028)
---------------------------------------

Vector Time (GMT): 2018/243/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1242522
15                 A    =         6778451
68  meter
 Y    =        4123182
39  meter          E    =           
0008325
 Z    =        5227583
17                 I    =           51
62795
 XDOT =      -7544
206014                 Wp   =           89
98162
 YDOT =       -934
456759  meter/sec      RA   =             
75419  deg
 ZDOT =      -1054
657214                 TA   =           10
12183
                                          MA   =           10
10507
                                          Ha   =            223
386  n
mi
                                          Hp   =            213
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4076516
23                 X    =        -1313929
24
 Y    =       13527501
28  feet           Y    =         4108888
72  meter
 Z    =       17150863
41                 Z    =         5221373
72
 XDOT =     -24751
332066                 XDOT =       -7528
072985
 YDOT =      -3065
803016  feet/sec       YDOT =       -1018
731159  meter/sec
 ZDOT =      -3460
161464                 ZDOT =       -1091
265140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13314276
69                 X    =        -4058191
54
 Y    =        4828727
07  feet           Y    =         1471796
01  meter
 Z    =       17122407
02                 Z    =         5218909
66
 XDOT =     -12135
031724                 XDOT =       -3698
757669
 YDOT =     -20591
479646  feet/sec       YDOT =       -6276
282996  meter/sec
 ZDOT =      -3624
299948                 ZDOT =       -1104
686624


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   18243
95748621  
00016717  00000-0  10270-3 0  9131
2 25544  51
6384   1
1102 0005569 113
0496 247
1244 15
53886089 10292


Satellite: ISS
Catalog Number: 25544
Epoch time:      18243
95748621   =   yrday
fracday
Element set:     913
Inclination:       51
6384  deg
RA of node:         1
1102  deg
Eccentricity:     
0005569     
Arg of perigee:   113
0496  deg
Mean anomaly:     247
1244  deg
Mean motion:   15
53886089  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1029
Checksum:              307


Coasting Arc #15 (Orbit 1043)
---------------------------------------

Vector Time (GMT): 2018/244/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2881523
64                 A    =         6780766
85  meter
 Y    =       -3955881
95  meter          E    =           
0016162
 Z    =       -4708970
80                 I    =           51
60265
 XDOT =       6916
843323                 Wp   =          111
29359
 YDOT =       1710
372450  meter/sec      RA   =          355
75851  deg
 ZDOT =       2797
752378                 TA   =          186
49375
                                          MA   =          186
51472
                                          Ha   =            223
317  n
mi
                                          Hp   =            213
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9453817
72                 X    =         2948418
99
 Y    =      -12978615
33  feet           Y    =        -3923284
94  meter
 Z    =      -15449379
26                 Z    =        -4694810
67
 XDOT =      22693
055522                 XDOT =        6883
613360
 YDOT =       5611
458169  feet/sec       YDOT =        1787
535711  meter/sec
 ZDOT =       9178
977617                 ZDOT =        2831
271276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16110513
54                 X    =         4910484
53
 Y    =        -497167
96  feet           Y    =         -151536
79  meter
 Z    =      -15385272
90                 Z    =        -4689431
18
 XDOT =       9522
864657                 XDOT =        2902
569147
 YDOT =      20092
723009  feet/sec       YDOT =        6124
261973  meter/sec
 ZDOT =       9329
131548                 ZDOT =        2843
519296


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   18244
92216224  
00016717  00000-0  10270-3 0  9149
2 25544  51
6386 356
3031 0005516 116
3408 243
8311 15
53877935 10446


Satellite: ISS
Catalog Number: 25544
Epoch time:      18244
92216224   =   yrday
fracday
Element set:     914
Inclination:       51
6386  deg
RA of node:       356
3031  deg
Eccentricity:     
0005516     
Arg of perigee:   116
3408  deg
Mean anomaly:     243
8311  deg
Mean motion:   15
53877935  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1044
Checksum:              299


Coasting Arc #16 (Orbit 1059)
---------------------------------------

Vector Time (GMT): 2018/245/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4313376
94                 A    =         6784217
13  meter
 Y    =        3681027
31  meter          E    =           
0016581
 Z    =        3708695
47                 I    =           51
58236
 XDOT =      -5844
872416                 Wp   =           95
12728
 YDOT =      -2503
422920  meter/sec      RA   =          350
76794  deg
 ZDOT =      -4298
000394                 TA   =           40
55785
                                          MA   =           40
43442
                                          Ha   =            223
297  n
mi
                                          Hp   =            213
227

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14151499
15                 X    =        -4372233
53
 Y    =       12076861
24  feet           Y    =         3632463
15  meter
 Z    =       12167636
05                 Z    =         3687599
51
 XDOT =     -19176
090605                 XDOT =       -5795
566610
 YDOT =      -8213
329791  feet/sec       YDOT =       -2568
508767  meter/sec
 ZDOT =     -14101
051163                 ZDOT =       -4326
272952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18349606
92                 X    =        -5592960
19
 Y    =       -3422670
52  feet           Y    =        -1043229
97  meter
 Z    =       12072453
16                 Z    =         3679683
72
 XDOT =      -5914
725961                 XDOT =       -1802
808473
 YDOT =     -18649
523795  feet/sec       YDOT =       -5684
374853  meter/sec
 ZDOT =     -14227
542851                 ZDOT =       -4336
555061


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   18245
95114588  
00016717  00000-0  10270-3 0  9154
2 25544  51
6394 351
1751 0005439 119
0987 241
0711 15
53909662 10608


Satellite: ISS
Catalog Number: 25544
Epoch time:      18245
95114588   =   yrday
fracday
Element set:     915
Inclination:       51
6394  deg
RA of node:       351
1751  deg
Eccentricity:     
0005439     
Arg of perigee:   119
0987  deg
Mean anomaly:     241
0711  deg
Mean motion:   15
53909662  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1060
Checksum:              316


Coasting Arc #17 (Orbit 1074)
---------------------------------------

Vector Time (GMT): 2018/246/21:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907880
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5410884
92                 A    =         6787660
12  meter
 Y    =       -3330452
74  meter          E    =           
0008754
 Z    =       -2393540
76                 I    =           51
56066
 XDOT =       4381
798310                 Wp   =           82
32491
 YDOT =       3279
247908  meter/sec      RA   =          345
78500  deg
 ZDOT =       5360
706866                 TA   =          250
92644
                                          MA   =          251
02126
                                          Ha   =            223
240  n
mi
                                          Hp   =            213
330

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17752247
13                 X    =         5459351
36
 Y    =      -10926682
21  feet           Y    =        -3269673
52  meter
 Z    =       -7852824
01                 Z    =        -2367138
84
 XDOT =      14375
978707                 XDOT =        4318
763755
 YDOT =      10758
687362  feet/sec       YDOT =        3327
895846  meter/sec
 ZDOT =      17587
620951                 ZDOT =        5381
838928

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19826592
41                 X    =         6043145
37
 Y    =        6579868
57  feet           Y    =         2005543
94  meter
 Z    =       -7733891
01                 Z    =        -2357289
98
 XDOT =       1433
978945                 XDOT =         437
076782
 YDOT =      16391
833672  feet/sec       YDOT =        4996
230903  meter/sec
 ZDOT =      17681
959864                 ZDOT =        5389
461366


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   18246
91581526  
00016717  00000-0  10270-3 0  9162
2 25544  51
6388 346
3681 0005434 122
0167 238
1514 15
53890727 10753


Satellite: ISS
Catalog Number: 25544
Epoch time:      18246
91581526   =   yrday
fracday
Element set:     916
Inclination:       51
6388  deg
RA of node:       346
3681  deg
Eccentricity:     
0005434     
Arg of perigee:   122
0167  deg
Mean anomaly:     238
1514  deg
Mean motion:   15
53890727  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1075
Checksum:              319
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