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

 
Date: December 8th 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) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


344/23:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 4

348/03:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 6

354/01:42:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 214 1

Coasting Arc #1 (Orbit 2545)
---------------------------------------

Vector Time (GMT): 2018/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944383
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2093215
25                 A    =         6778577
76  meter
 Y    =        4013298
14  meter          E    =           
0017103
 Z    =       -5060881
01                 I    =           51
31279
 XDOT =      -5448
202278                 Wp   =           88
29597
 YDOT =      -5076
354275  meter/sec      RA   =          233
99227  deg
 ZDOT =      -1776
876743                 TA   =          164
43214
                                          MA   =          164
37948
                                          Ha   =            222
756  n
mi
                                          Hp   =            213
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6867504
10                 X    =        -2113354
10
 Y    =       13166988
65  feet           Y    =         3989778
35  meter
 Z    =      -16603940
31                 Z    =        -5071097
69
 XDOT =     -17874
679390                 XDOT =       -5382
400902
 YDOT =     -16654
705626  feet/sec       YDOT =       -5136
911730  meter/sec
 ZDOT =      -5829
648107                 ZDOT =       -1803
183338

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11025210
82                 X    =        -3360484
26
 Y    =       -9870868
04  feet           Y    =        -3008640
58  meter
 Z    =      -16650337
14                 Z    =        -5075022
76
 XDOT =      19909
508610                 XDOT =        6068
418224
 YDOT =     -12231
683117  feet/sec       YDOT =       -3728
217014  meter/sec
 ZDOT =      -5947
413702                 ZDOT =       -1812
771696


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   18341
51925259  
00016717  00000-0  10270-3 0  9002
2 25544  51
6411 234
9405 0004967 120
2902 239
8743 15
54082537 25462


Satellite: ISS
Catalog Number: 25544
Epoch time:      18341
51925259   =   yrday
fracday
Element set:     900
Inclination:       51
6411  deg
RA of node:       234
9405  deg
Eccentricity:     
0004967     
Arg of perigee:   120
2902  deg
Mean anomaly:     239
8743  deg
Mean motion:   15
54082537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2546
Checksum:              308


Coasting Arc #2 (Orbit 2561)
---------------------------------------

Vector Time (GMT): 2018/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3270567
28                 A    =         6777430
76  meter
 Y    =       -2687435
10  meter          E    =           
0006976
 Z    =        5287250
44                 I    =           51
32972
 XDOT =       4971
856600                 Wp   =          112
45606
 YDOT =       5844
527434  meter/sec      RA   =          228
97152  deg
 ZDOT =       -107
286392                 TA   =          338
55537
                                          MA   =          338
58458
                                          Ha   =            222
576  n
mi
                                          Hp   =            213
167

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10730207
61                 X    =         3274692
95
 Y    =       -8817044
30  feet           Y    =        -2650838
95  meter
 Z    =       17346622
17                 Z    =         5303147
54
 XDOT =      16311
865486                 XDOT =        4906
653085
 YDOT =      19174
958774  feet/sec       YDOT =        5899
761627  meter/sec
 ZDOT =       -351
989474                 ZDOT =         -83
292244

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6054176
41                 X    =         1845312
97
 Y    =       12398718
23  feet           Y    =         3779129
32  meter
 Z    =       17418428
76                 Z    =         5309137
09
 XDOT =     -21586
147837                 XDOT =       -6579
457861
 YDOT =      10872
561583  feet/sec       YDOT =        3313
956770  meter/sec
 ZDOT =       -244
687204                 ZDOT =         -74
580660


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   18342
54812683  
00016717  00000-0  10270-3 0  9013
2 25544  51
6412 229
8120 0004914 124
5855 235
5762 15
54098494 25627


Satellite: ISS
Catalog Number: 25544
Epoch time:      18342
54812683   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:       229
8120  deg
Eccentricity:     
0004914     
Arg of perigee:   124
5855  deg
Mean anomaly:     235
5762  deg
Mean motion:   15
54098494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2562
Checksum:              314


Coasting Arc #3 (Orbit 2576)
---------------------------------------

Vector Time (GMT): 2018/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4401278
71                 A    =         6778775
85  meter
 Y    =        1312123
28  meter          E    =           
0017505
 Z    =       -5001983
07                 I    =           51
35561
 XDOT =      -4094
344425                 Wp   =          111
01372
 YDOT =      -6154
805465  meter/sec      RA   =          223
95255  deg
 ZDOT =       1987
602228                 TA   =          178
40654
                                          MA   =          178
40095
                                          Ha   =            222
688  n
mi
                                          Hp   =            213
078

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14439890
77                 X    =        -4391327
01
 Y    =        4304866
41  feet           Y    =         1262961
41  meter
 Z    =      -16410705
60                 Z    =        -5023338
73
 XDOT =     -13432
888534                 XDOT =       -4034
870139
 YDOT =     -20192
931316  feet/sec       YDOT =       -6200
258981  meter/sec
 ZDOT =       6521
004684                 ZDOT =        1967
856887

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1047929
77                 X    =         -319409
00
 Y    =      -14925705
98  feet           Y    =        -4549355
18  meter
 Z    =      -16506929
53                 Z    =        -5031312
12
 XDOT =      21572
675147                 XDOT =        6575
351385
 YDOT =      -8630
758395  feet/sec       YDOT =       -2630
655159  meter/sec
 ZDOT =       6432
827502                 ZDOT =        1960
725823


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   18343
51269631  
00016717  00000-0  10270-3 0  9021
2 25544  51
6401 225
0043 0004900 126
8690 233
2912 15
54080003 25779


Satellite: ISS
Catalog Number: 25544
Epoch time:      18343
51269631   =   yrday
fracday
Element set:     902
Inclination:       51
6401  deg
RA of node:       225
0043  deg
Eccentricity:     
0004900     
Arg of perigee:   126
8690  deg
Mean anomaly:     233
2912  deg
Mean motion:   15
54080003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2577
Checksum:              274


Coasting Arc #4 (Orbit 2592)
---------------------------------------

Vector Time (GMT): 2018/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5332691
72                 A    =         6781831
98  meter
 Y    =          19807
55  meter          E    =           
0013392
 Z    =        4177988
08                 I    =           51
39062
 XDOT =       2867
480566                 Wp   =           91
88912
 YDOT =       6094
598740  meter/sec      RA   =          218
94194  deg
 ZDOT =      -3679
098702                 TA   =           35
99658
                                          MA   =           35
90646
                                          Ha   =            222
420  n
mi
                                          Hp   =            213
271

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17495707
76                 X    =         5311779
40
 Y    =          64985
39  feet           Y    =           79323
97  meter
 Z    =       13707309
97                 Z    =         4203841
70
 XDOT =       9407
744640                 XDOT =        2816
987087
 YDOT =      19995
402689  feet/sec       YDOT =        6126
383021  meter/sec
 ZDOT =     -12070
533800                 ZDOT =       -3665
291351

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3598193
14                 X    =        -1096729
27
 Y    =       17028041
80  feet           Y    =         5190147
14  meter
 Z    =       13823644
90                 Z    =         4213446
96
 XDOT =     -20262
718212                 XDOT =       -6176
076511
 YDOT =       5493
270532  feet/sec       YDOT =        1674
348858  meter/sec
 ZDOT =     -12009
047078                 ZDOT =       -3660
357549


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   18344
54156738  
00016717  00000-0  10270-3 0  9039
2 25544  51
6399 219
8762 0004769 130
4422 229
7147 15
54112528 25937


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
54156738   =   yrday
fracday
Element set:     903
Inclination:       51
6399  deg
RA of node:       219
8762  deg
Eccentricity:     
0004769     
Arg of perigee:   130
4422  deg
Mean anomaly:     229
7147  deg
Mean motion:   15
54112528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2593
Checksum:              330


Coasting Arc #5 (Orbit 2599)
---------------------------------------

Vector Time (GMT): 2018/344/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4018729
25                 A    =         6787717
07  meter
 Y    =        5056295
21  meter          E    =           
0011726
 Z    =       -2076235
58                 I    =           51
42027
 XDOT =      -5029
867068                 Wp   =          138
21488
 YDOT =       1742
930690  meter/sec      RA   =          216
66408  deg
 ZDOT =      -5517
714548                 TA   =           64
83160
                                          MA   =           64
71003
                                          Ha   =            222
716  n
mi
                                          Hp   =            213
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13184807
25                 X    =         3971974
92
 Y    =       16588895
06  feet           Y    =         5100974
26  meter
 Z    =       -6811796
54                 Z    =        -2056826
95
 XDOT =     -16502
188543                 XDOT =       -5022
181027
 YDOT =       5718
276542  feet/sec       YDOT =        1686
726844  meter/sec
 ZDOT =     -18102
738017                 ZDOT =       -5542
129034

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20570521
99                 X    =         6269895
10
 Y    =       -5201860
19  feet           Y    =        -1585526
99  meter
 Z    =       -6724985
46                 Z    =        -2049775
57
 XDOT =      -1934
841084                 XDOT =        -589
739562
 YDOT =      15780
156695  feet/sec       YDOT =        4809
791761  meter/sec
 ZDOT =     -18212
789176                 ZDOT =       -5551
258141


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   18344
99169895  
00016717  00000-0  10270-3 0  9047
2 25544  51
6384 217
6297 0005142 135
9748 224
1815 15
54068828 26000


Satellite: ISS
Catalog Number: 25544
Epoch time:      18344
99169895   =   yrday
fracday
Element set:     904
Inclination:       51
6384  deg
RA of node:       217
6297  deg
Eccentricity:     
0005142     
Arg of perigee:   135
9748  deg
Mean anomaly:     224
1815  deg
Mean motion:   15
54068828  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2600
Checksum:              341


Coasting Arc #6 (Orbit 2615)
---------------------------------------

Vector Time (GMT): 2018/345/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2882130
69                 A    =         6784340
97  meter
 Y    =       -5047242
95  meter          E    =           
0016156
 Z    =        3489973
99                 I    =           51
43679
 XDOT =       6192
350541                 Wp   =          104
89101
 YDOT =       -403
434414  meter/sec      RA   =          211
67115  deg
 ZDOT =       4508
818458                 TA   =          296
28391
                                          MA   =          296
44981
                                          Ha   =            222
643  n
mi
                                          Hp   =            213
402

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9455809
34                 X    =        -2842429
22
 Y    =      -16559196
04  feet           Y    =        -5079251
32  meter
 Z    =       11450045
90                 Z    =         3476069
52
 XDOT =      20316
110699                 XDOT =        6174
500210
 YDOT =      -1323
603719  feet/sec       YDOT =        -334
287529  meter/sec
 ZDOT =      14792
711477                 ZDOT =        4538
855301

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18981964
61                 X    =        -5785702
81
 Y    =        2172936
63  feet           Y    =          662311
09  meter
 Z    =       11387985
81                 Z    =         3471058
07
 XDOT =       6972
819688                 XDOT =        2125
315441
 YDOT =     -17695
686200  feet/sec       YDOT =       -5393
645154  meter/sec
 ZDOT =      14927
941931                 ZDOT =        4550
036701


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   18346
02056598  
00016717  00000-0  10270-3 0  9059
2 25544  51
6388 212
5008 0005075 138
8282 221
3254 15
54087623 26165


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
02056598   =   yrday
fracday
Element set:     905
Inclination:       51
6388  deg
RA of node:       212
5008  deg
Eccentricity:     
0005075     
Arg of perigee:   138
8282  deg
Mean anomaly:     221
3254  deg
Mean motion:   15
54087623  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2616
Checksum:              308


Coasting Arc #7 (Orbit 2630)
---------------------------------------

Vector Time (GMT): 2018/346/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1407304
25                 A    =         6780632
90  meter
 Y    =        4799102
60  meter          E    =           
0012632
 Z    =       -4589386
22                 I    =           51
45235
 XDOT =      -6992
484297                 Wp   =           92
87123
 YDOT =       -824
614860  meter/sec      RA   =          206
67068  deg
 ZDOT =      -3014
305512                 TA   =          146
95515
                                          MA   =          146
87615
                                          Ha   =            222
621  n
mi
                                          Hp   =            213
482

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4617139
93                 X    =         1375827
51
 Y    =       15745087
29  feet           Y    =         4814664
48  meter
 Z    =      -15057041
40                 Z    =        -4582626
05
 XDOT =     -22941
221447                 XDOT =       -6968
101662
 YDOT =      -2705
429331  feet/sec       YDOT =        -902
673072  meter/sec
 ZDOT =      -9889
453778                 ZDOT =       -3048
213343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16353373
34                 X    =         4984508
19
 Y    =        1641262
00  feet           Y    =          500256
66  meter
 Z    =      -15027098
52                 Z    =        -4580259
63
 XDOT =     -11103
129446                 XDOT =       -3384
233855
 YDOT =      18922
834716  feet/sec       YDOT =        5767
680021  meter/sec
 ZDOT =     -10042
002176                 ZDOT =       -3060
802263


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   18346
98512964  
00016717  00000-0  10270-3 0  9069
2 25544  51
6381 207
6932 0005120 141
3259 218
8261 15
54065904 26317


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
98512964   =   yrday
fracday
Element set:     906
Inclination:       51
6381  deg
RA of node:       207
6932  deg
Eccentricity:     
0005120     
Arg of perigee:   141
3259  deg
Mean anomaly:     218
8261  deg
Mean motion:   15
54065904  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2631
Checksum:              310


Coasting Arc #8 (Orbit 2646)
---------------------------------------

Vector Time (GMT): 2018/347/23:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         222164
81                 A    =         6778012
68  meter
 Y    =       -4354125
17  meter          E    =           
0009107
 Z    =        5185510
71                 I    =           51
47391
 XDOT =       7340
894098                 Wp   =          136
24019
 YDOT =       1856
500835  meter/sec      RA   =          201
66345  deg
 ZDOT =       1236
589574                 TA   =          301
82621
                                          MA   =          301
91485
                                          Ha   =            222
501  n
mi
                                          Hp   =            213
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         728887
17                 X    =          245648
93
 Y    =      -14285187
56  feet           Y    =        -4351509
86  meter
 Z    =       17012830
40                 Z    =         5186646
61
 XDOT =      24084
298222                 XDOT =        7313
581911
 YDOT =       6090
882005  feet/sec       YDOT =        1938
439009  meter/sec
 ZDOT =       4057
052408                 ZDOT =        1272
182821

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13071985
55                 X    =        -3984341
19
 Y    =       -5790699
55  feet           Y    =        -1765005
22  meter
 Z    =       17018379
80                 Z    =         5187202
16
 XDOT =      14035
717532                 XDOT =        4278
086704
 YDOT =     -19215
928152  feet/sec       YDOT =       -5857
014901  meter/sec
 ZDOT =       4217
106437                 ZDOT =        1285
374042


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   18348
01399390  
00016717  00000-0  10270-3 0  9072
2 25544  51
6380 202
5648 0005036 145
3812 214
7669 15
54088491 26479


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
01399390   =   yrday
fracday
Element set:     907
Inclination:       51
6380  deg
RA of node:       202
5648  deg
Eccentricity:     
0005036     
Arg of perigee:   145
3812  deg
Mean anomaly:     214
7669  deg
Mean motion:   15
54088491  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2647
Checksum:              325


Coasting Arc #9 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4441004
74                 A    =         6780352
34  meter
 Y    =       -2239005
52  meter          E    =           
0010397
 Z    =        4599168
29                 I    =           51
48601
 XDOT =       5397
417719                 Wp   =           92
80764
 YDOT =       4568
283060  meter/sec      RA   =          200
63071  deg
 ZDOT =      -2982
502384                 TA   =           26
99989
                                          MA   =           26
94583
                                          Ha   =            222
351  n
mi
                                          Hp   =            213
555

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14570225
53                 X    =         4443371
58
 Y    =       -7345818
63  feet           Y    =        -2189330
23  meter
 Z    =       15089134
83                 Z    =         4620746
69
 XDOT =      17708
063383                 XDOT =        5360
420145
 YDOT =      14987
805316  feet/sec       YDOT =        4628
434094  meter/sec
 ZDOT =      -9785
112809                 ZDOT =       -2956
373172

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15860764
33                 X    =        -4834360
97
 Y    =       -3426470
71  feet           Y    =        -1044388
27  meter
 Z    =       15186506
06                 Z    =         4628847
05
 XDOT =      -4589
243516                 XDOT =       -1398
801424
 YDOT =     -21683
272486  feet/sec       YDOT =       -6609
061454  meter/sec
 ZDOT =      -9667
932577                 ZDOT =       -2946
785849


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   18348
20690643  
00016717  00000-0  10270-3 0  9089
2 25544  51
6359 201
6035 0004875 144
0787 216
0694 15
54083573 26505


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
20690643   =   yrday
fracday
Element set:     908
Inclination:       51
6359  deg
RA of node:       201
6035  deg
Eccentricity:     
0004875     
Arg of perigee:   144
0787  deg
Mean anomaly:     216
0694  deg
Mean motion:   15
54083573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              318


Coasting Arc #10 (Orbit 2664)
---------------------------------------

Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5630134
10                 A    =         6784076
76  meter
 Y    =        1350993
87  meter          E    =           
0009213
 Z    =       -3546973
94                 I    =           51
53068
 XDOT =      -3962
548878                 Wp   =          120
67887
 YDOT =      -4794
982849  meter/sec      RA   =          195
63409  deg
 ZDOT =       4467
493837                 TA   =          197
46975
                                          MA   =          197
50146
                                          Ha   =            222
450  n
mi
                                          Hp   =            213
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18471568
57                 X    =        -5627593
53
 Y    =        4432394
60  feet           Y    =         1288048
23  meter
 Z    =      -11637053
62                 Z    =        -3574316
92
 XDOT =     -13000
488446                 XDOT =       -3930
336253
 YDOT =     -15731
571027  feet/sec       YDOT =       -4839
114993  meter/sec
 ZDOT =      14657
132012                 ZDOT =        4448
323093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17206537
82                 X    =         5244552
73
 Y    =        7867421
64  feet           Y    =         2397990
12  meter
 Z    =      -11760302
59                 Z    =        -3584540
23
 XDOT =       1168
408904                 XDOT =         356
131034
 YDOT =      19206
230054  feet/sec       YDOT =        5854
058920  meter/sec
 ZDOT =      14571
285771                 ZDOT =        4441
327903


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   18349
17146463  
00016717  00000-0  10270-3 0  9093
2 25544  51
6368 196
7956 0004824 145
9892 214
1571 15
54064032 26650


Satellite: ISS
Catalog Number: 25544
Epoch time:      18349
17146463   =   yrday
fracday
Element set:     909
Inclination:       51
6368  deg
RA of node:       196
7956  deg
Eccentricity:     
0004824     
Arg of perigee:   145
9892  deg
Mean anomaly:     214
1571  deg
Mean motion:   15
54064032  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2665
Checksum:              337


Coasting Arc #11 (Orbit 2680)
---------------------------------------

Vector Time (GMT): 2018/350/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6427084
87                 A    =         6787508
94  meter
 Y    =        -484099
11  meter          E    =           
0017792
 Z    =        2096891
12                 I    =           51
57437
 XDOT =       2176
335816                 Wp   =          120
09862
 YDOT =       4865
859521  meter/sec      RA   =          190
64963  deg
 ZDOT =      -5520
927428                 TA   =           36
64124
                                          MA   =           36
51970
                                          Ha   =            222
267  n
mi
                                          Hp   =            213
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21086236
44                 X    =         6421834
91
 Y    =       -1588251
68  feet           Y    =         -412256
45  meter
 Z    =        6879564
03                 Z    =         2128098
96
 XDOT =       7140
209371                 XDOT =        2148
580475
 YDOT =      15964
106039  feet/sec       YDOT =        4890
041940  meter/sec
 ZDOT =     -18113
278963                 ZDOT =       -5510
422660

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17732448
78                 X    =        -5404850
39
 Y    =      -11434951
63  feet           Y    =        -3485373
26  meter
 Z    =        7020146
25                 Z    =         2139740
58
 XDOT =       3013
404495                 XDOT =         918
485690
 YDOT =     -15816
229956  feet/sec       YDOT =       -4820
786891  meter/sec
 ZDOT =     -18066
449995                 ZDOT =       -5506
653958


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   18350
20032513  
00016717  00000-0  10270-3 0  9101
2 25544  51
6366 191
6666 0004733 149
8991 210
2435 15
54088163 26817


Satellite: ISS
Catalog Number: 25544
Epoch time:      18350
20032513   =   yrday
fracday
Element set:     910
Inclination:       51
6366  deg
RA of node:       191
6666  deg
Eccentricity:     
0004733     
Arg of perigee:   149
8991  deg
Mean anomaly:     210
2435  deg
Mean motion:   15
54088163  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2681
Checksum:              302


Coasting Arc #12 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2018/351/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6764488
75                 A    =         6789294
35  meter
 Y    =        -299836
82  meter          E    =           
0010152
 Z    =        -467790
40                 I    =           51
61312
 XDOT =       -194
366794                 Wp   =           67
93319
 YDOT =      -4784
079406  meter/sec      RA   =          185
67541  deg
 ZDOT =       5984
980724                 TA   =          287
02235
                                          MA   =          287
13356
                                          Ha   =            222
258  n
mi
                                          Hp   =            213
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22193204
57                 X    =        -6758360
85
 Y    =        -983716
61  feet           Y    =         -375447
75  meter
 Z    =       -1534745
42                 Z    =         -500635
25
 XDOT =       -637
686332                 XDOT =        -169
927461
 YDOT =     -15695
798576  feet/sec       YDOT =       -4786
116646  meter/sec
 ZDOT =      19635
763529                 ZDOT =        5984
095636

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17332338
10                 X    =         5282896
65
 Y    =       13878769
66  feet           Y    =         4230248
99  meter
 Z    =       -1682640
70                 Z    =         -512868
89
 XDOT =      -7624
555991                 XDOT =       -2323
964666
 YDOT =      11862
868354  feet/sec       YDOT =        3615
802274  meter/sec
 ZDOT =      19632
243646                 ZDOT =        5983
907863


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   18351
16488067  
00016717  00000-0  10270-3 0  9117
2 25544  51
6365 186
8591 0004831 154
3390 205
8004 15
54100086 26969


Satellite: ISS
Catalog Number: 25544
Epoch time:      18351
16488067   =   yrday
fracday
Element set:     911
Inclination:       51
6365  deg
RA of node:       186
8591  deg
Eccentricity:     
0004831     
Arg of perigee:   154
3390  deg
Mean anomaly:     205
8004  deg
Mean motion:   15
54100086  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2696
Checksum:              310


Coasting Arc #13 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2018/352/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6578341
56                 A    =         6788801
17  meter
 Y    =        1073417
71  meter          E    =           
0013655
 Z    =       -1254204
43                 I    =           51
64590
 XDOT =      -1858
136129                 Wp   =          147
96134
 YDOT =       4603
667355  meter/sec      RA   =          180
70465  deg
 ZDOT =      -5846
389535                 TA   =           45
67823
                                          MA   =           45
56636
                                          Ha   =            222
199  n
mi
                                          Hp   =            213
944

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21582485
43                 X    =         6571941
70
 Y    =        3521711
65  feet           Y    =         1146945
60  meter
 Z    =       -4114843
94                 Z    =        -1222264
35
 XDOT =      -6096
247143                 XDOT =       -1881
078629
 YDOT =      15103
895522  feet/sec       YDOT =        4582
760509  meter/sec
 ZDOT =     -19181
068029                 ZDOT =       -5855
471194

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15638717
70                 X    =        -4766681
15
 Y    =      -15323155
55  feet           Y    =        -4670497
81  meter
 Z    =       -3971080
89                 Z    =        -1210385
46
 XDOT =      12458
928145                 XDOT =        3797
481299
 YDOT =      -7769
572072  feet/sec       YDOT =       -2368
165567  meter/sec
 ZDOT =     -19222
423775                 ZDOT =       -5858
994767


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   18352
19373712  
00016717  00000-0  10270-3 0  9122
2 25544  51
6379 181
7298 0004629 158
2915 201
8435 15
54096143 27124


Satellite: ISS
Catalog Number: 25544
Epoch time:      18352
19373712   =   yrday
fracday
Element set:     912
Inclination:       51
6379  deg
RA of node:       181
7298  deg
Eccentricity:     
0004629     
Arg of perigee:   158
2915  deg
Mean anomaly:     201
8435  deg
Mean motion:   15
54096143  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              320


Coasting Arc #14 (Orbit 2727)
---------------------------------------

Vector Time (GMT): 2018/353/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964842
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5910762
94                 A    =         6786129
43  meter
 Y    =       -1783985
95  meter          E    =           
0014823
 Z    =        2806551
35                 I    =           51
66952
 XDOT =       3742
596487                 Wp   =           98
10624
 YDOT =      -4327
551900  meter/sec      RA   =          175
73223  deg
 ZDOT =       5106
188247                 TA   =          293
73250
                                          MA   =          293
88792
                                          Ha   =            222
124  n
mi
                                          Hp   =            214
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19392266
86                 X    =        -5904007
48
 Y    =       -5852972
29  feet           Y    =        -1850046
69  meter
 Z    =        9207845
63                 Z    =         2777854
89
 XDOT =      12278
859865                 XDOT =        3765
906824
 YDOT =     -14198
004920  feet/sec       YDOT =       -4285
569700  meter/sec
 ZDOT =      16752
586113                 ZDOT =        5124
424891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12806793
54                 X    =         3903510
67
 Y    =       15769087
99  feet           Y    =         4806418
02  meter
 Z    =        9078745
67                 Z    =         2767201
68
 XDOT =     -16890
691289                 XDOT =       -5148
282705
 YDOT =       3977
036751  feet/sec       YDOT =        1212
200802  meter/sec
 ZDOT =      16835
165138                 ZDOT =        5131
358334


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   18353
22259077  
00016717  00000-0  10270-3 0  9135
2 25544  51
6372 176
6016 0004679 161
8651 198
2670 15
54113821 27280


Satellite: ISS
Catalog Number: 25544
Epoch time:      18353
22259077   =   yrday
fracday
Element set:     913
Inclination:       51
6372  deg
RA of node:       176
6016  deg
Eccentricity:     
0004679     
Arg of perigee:   161
8651  deg
Mean anomaly:     198
2670  deg
Mean motion:   15
54113821  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2728
Checksum:              319


Coasting Arc #15 (Orbit 2741)
---------------------------------------

Vector Time (GMT): 2018/354/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949610
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2960818
37                 A    =         6778970
90  meter
 Y    =       -3521886
03  meter          E    =           
0010191
 Z    =        4975428
88                 I    =           51
67379
 XDOT =       6841
374690                 Wp   =          141
11054
 YDOT =      -2749
678057  meter/sec      RA   =          171
20809  deg
 ZDOT =       2114
737228                 TA   =          288
25910
                                          MA   =          288
36998
                                          Ha   =            222
086  n
mi
                                          Hp   =            214
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9713971
04                 X    =        -2945383
84
 Y    =      -11554744
20  feet           Y    =        -3554910
21  meter
 Z    =       16323585
56                 Z    =         4961083
21
 XDOT =      22445
455021                 XDOT =        6861
341520
 YDOT =      -9021
253468  feet/sec       YDOT =       -2673
061640  meter/sec
 ZDOT =       6938
114264                 ZDOT =        2148
018769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6745242
78                 X    =        -2055950
00
 Y    =       13581961
60  feet           Y    =         4139781
90  meter
 Z    =       16259299
23                 Z    =         4955834
40
 XDOT =     -16130
235825                 XDOT =       -4916
495879
 YDOT =     -16536
276018  feet/sec       YDOT =       -5040
256930  meter/sec
 ZDOT =       7088
336674                 ZDOT =        2160
525018


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   18354
12283756  
00016717  00000-0  10270-3 0  9147
2 25544  51
6354 172
1141 0004623 165
8324 194
2959 15
54104856 27420


Satellite: ISS
Catalog Number: 25544
Epoch time:      18354
12283756   =   yrday
fracday
Element set:     914
Inclination:       51
6354  deg
RA of node:       172
1141  deg
Eccentricity:     
0004623     
Arg of perigee:   165
8324  deg
Mean anomaly:     194
2959  deg
Mean motion:   15
54104856  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2742
Checksum:              311


Coasting Arc #16 (Orbit 2756)
---------------------------------------

Vector Time (GMT): 2018/355/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949610
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1233462
05                 A    =         6777492
45  meter
 Y    =        4026357
70  meter          E    =           
0016261
 Z    =       -5323962
76                 I    =           51
70204
 XDOT =      -7391
410714                 Wp   =          104
70914
 YDOT =       1987
680605  meter/sec      RA   =          166
21221  deg
 ZDOT =       -213
800579                 TA   =          163
27876
                                          MA   =          163
22508
                                          Ha   =            221
965  n
mi
                                          Hp   =            214
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4046791
50                 X    =         1214207
71
 Y    =       13209834
97  feet           Y    =         4040044
18  meter
 Z    =      -17467069
43                 Z    =        -5318017
22
 XDOT =     -24250
035150                 XDOT =       -7412
049631
 YDOT =       6521
261829  feet/sec       YDOT =        1904
909342  meter/sec
 ZDOT =       -701
445469                 ZDOT =        -249
755628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10340451
11                 X    =         3151769
50
 Y    =       -9212629
54  feet           Y    =        -2808009
48  meter
 Z    =      -17440679
57                 Z    =        -5315919
13
 XDOT =      15216
342903                 XDOT =        4637
941317
 YDOT =      18685
721217  feet/sec       YDOT =        5695
407827  meter/sec
 ZDOT =       -863
666481                 ZDOT =        -263
245543


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   18355
08738586  
00016717  00000-0  10270-3 0  9150
2 25544  51
6360 167
3051 0004620 168
4042 191
7218 15
54090581 27571


Satellite: ISS
Catalog Number: 25544
Epoch time:      18355
08738586   =   yrday
fracday
Element set:     915
Inclination:       51
6360  deg
RA of node:       167
3051  deg
Eccentricity:     
0004620     
Arg of perigee:   168
4042  deg
Mean anomaly:     191
7218  deg
Mean motion:   15
54090581  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2757
Checksum:              315


Coasting Arc #17 (Orbit 2772)
---------------------------------------

Vector Time (GMT): 2018/356/01:42:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949610
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         514616
31                 A    =         6778325
12  meter
 Y    =       -4426259
22  meter          E    =           
0004989
 Z    =        5103262
78                 I    =           51
73745
 XDOT =       7400
162726                 Wp   =          108
67002
 YDOT =      -1099
940811  meter/sec      RA   =          161
21885  deg
 ZDOT =      -1700
460472                 TA   =          357
72487
                                          MA   =          357
72714
                                          Ha   =            221
847  n
mi
                                          Hp   =            214
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1688373
73                 X    =          539284
71
 Y    =      -14521847
84  feet           Y    =        -4420367
26  meter
 Z    =       16742988
13                 Z    =         5105821
87
 XDOT =      24278
749101                 XDOT =        7420
172541
 YDOT =      -3608
729695  feet/sec       YDOT =       -1017
074913  meter/sec
 ZDOT =      -5578
938555                 ZDOT =       -1664
464494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13810751
42                 X    =        -4209517
03
 Y    =        4753576
70  feet           Y    =         1448890
18  meter
 Z    =       16754968
69                 Z    =         5106914
46
 XDOT =     -13268
466932                 XDOT =       -4044
228721
 YDOT =     -19459
819828  feet/sec       YDOT =       -5931
353084  meter/sec
 ZDOT =      -5416
591956                 ZDOT =       -1650
977228


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   18356
11623433  
00016717  00000-0  10270-3 0  9160
2 25544  51
6364 162
1763 0004499 172
4744 187
6476 15
54101463 27736


Satellite: ISS
Catalog Number: 25544
Epoch time:      18356
11623433   =   yrday
fracday
Element set:     916
Inclination:       51
6364  deg
RA of node:       162
1763  deg
Eccentricity:     
0004499     
Arg of perigee:   172
4744  deg
Mean anomaly:     187
6476  deg
Mean motion:   15
54101463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2773
Checksum:              320
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