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

 
Date: February 20th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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


057/06:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 213 9

058/23:08:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 213 9

060/14:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 214 1

063/17:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 2020)
---------------------------------------

Vector Time (GMT): 2018/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1760482
69                 A    =         6788457
90  meter
 Y    =        6387814
33  meter          E    =           
0010993
 Z    =       -1459685
07                 I    =           51
31116
 XDOT =      -5065
768289                 Wp   =          134
88037
 YDOT =         89
080807  meter/sec      RA   =          244
43041  deg
 ZDOT =      -5754
125273                 TA   =           61
11883
                                          MA   =           61
00857
                                          Ha   =            222
011  n
mi
                                          Hp   =            213
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5775861
86                 X    =         1696011
86
 Y    =       20957396
09  feet           Y    =         6407140
62  meter
 Z    =       -4788993
02                 Z    =        -1451290
64
 XDOT =     -16619
974701                 XDOT =       -5038
437819
 YDOT =        292
259867  feet/sec       YDOT =          32
584121  meter/sec
 ZDOT =     -18878
363756                 ZDOT =       -5778
666284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5992718
98                 X    =        -1826580
74
 Y    =       20904760
61  feet           Y    =         6371771
03  meter
 Z    =       -4752450
77                 Z    =        -1448546
99
 XDOT =     -12694
173053                 XDOT =       -3869
183947
 YDOT =      -7929
851799  feet/sec       YDOT =       -2417
018828  meter/sec
 ZDOT =     -18987
618442                 ZDOT =       -5787
426101


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   18050
52937749  
00016717  00000-0  10270-3 0  9007
2 25544  51
6373 245
2698 0002861 111
4643 248
6815 15
54120953 20214


Satellite: ISS
Catalog Number: 25544
Epoch time:      18050
52937749   =   yrday
fracday
Element set:     900
Inclination:       51
6373  deg
RA of node:       245
2698  deg
Eccentricity:     
0002861     
Arg of perigee:   111
4643  deg
Mean anomaly:     248
6815  deg
Mean motion:   15
54120953  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2021
Checksum:              305


Coasting Arc #2 (Orbit 2036)
---------------------------------------

Vector Time (GMT): 2018/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -789483
10                 A    =         6785514
52  meter
 Y    =       -6035674
02  meter          E    =           
0015615
 Z    =        2984617
73                 I    =           51
31582
 XDOT =       5610
602081                 Wp   =           89
31643
 YDOT =       1720
270386  meter/sec      RA   =          239
43163  deg
 ZDOT =       4940
672070                 TA   =          305
01524
                                          MA   =          305
16169
                                          Ha   =            221
949  n
mi
                                          Hp   =            213
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2590167
64                 X    =         -736429
42
 Y    =      -19802080
13  feet           Y    =        -6044205
63  meter
 Z    =        9792052
93                 Z    =         2980912
20
 XDOT =      18407
487141                 XDOT =        5566
949645
 YDOT =       5643
931712  feet/sec       YDOT =        1782
768405  meter/sec
 ZDOT =      16209
554034                 ZDOT =        4967
819931

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7762121
24                 X    =         2365894
55
 Y    =      -18408926
72  feet           Y    =        -5611040
86  meter
 Z    =        9776325
37                 Z    =         2979823
97
 XDOT =      11560
699253                 XDOT =        3523
701132
 YDOT =      13585
802397  feet/sec       YDOT =        4140
952571  meter/sec
 ZDOT =      16330
188587                 ZDOT =        4977
441481


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   18051
55821540  
00016717  00000-0  10270-3 0  9013
2 25544  51
6365 240
1401 0002908 119
1781 240
9663 15
54146361 20375


Satellite: ISS
Catalog Number: 25544
Epoch time:      18051
55821540   =   yrday
fracday
Element set:     901
Inclination:       51
6365  deg
RA of node:       240
1401  deg
Eccentricity:     
0002908     
Arg of perigee:   119
1781  deg
Mean anomaly:     240
9663  deg
Mean motion:   15
54146361  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2037
Checksum:              282


Coasting Arc #3 (Orbit 2051)
---------------------------------------

Vector Time (GMT): 2018/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -391329
24                 A    =         6781682
18  meter
 Y    =        5286661
86  meter          E    =           
0010403
 Z    =       -4239352
95                 I    =           51
32020
 XDOT =      -5901
254178                 Wp   =           83
19053
 YDOT =      -3310
374821  meter/sec      RA   =          234
42488  deg
 ZDOT =      -3589
843159                 TA   =          149
94391
                                          MA   =          149
88416
                                          Ha   =            222
014  n
mi
                                          Hp   =            213
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1283888
57                 X    =         -429824
67
 Y    =       17344691
14  feet           Y    =         5282070
14  meter
 Z    =      -13908638
28                 Z    =        -4241347
83
 XDOT =     -19361
070137                 XDOT =       -5846
360661
 YDOT =     -10860
809781  feet/sec       YDOT =       -3376
060082  meter/sec
 ZDOT =     -11777
700653                 ZDOT =       -3618
375544

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9581251
86                 X    =        -2920365
57
 Y    =       14505883
73  feet           Y    =         4421393
36  meter
 Z    =      -13918184
12                 Z    =        -4242262
52
 XDOT =     -10372
332283                 XDOT =       -3161
486880
 YDOT =     -18252
901023  feet/sec       YDOT =       -5563
484232  meter/sec
 ZDOT =     -11904
309804                 ZDOT =       -3628
433628


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   18052
52275003  
00016717  00000-0  10270-3 0  9029
2 25544  51
6361 235
3316 0003086 119
2616 240
8846 15
54138186 20523


Satellite: ISS
Catalog Number: 25544
Epoch time:      18052
52275003   =   yrday
fracday
Element set:     902
Inclination:       51
6361  deg
RA of node:       235
3316  deg
Eccentricity:     
0003086     
Arg of perigee:   119
2616  deg
Mean anomaly:     240
8846  deg
Mean motion:   15
54138186  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2052
Checksum:              286


Coasting Arc #4 (Orbit 2067)
---------------------------------------

Vector Time (GMT): 2018/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1659530
29                 A    =         6778637
29  meter
 Y    =       -4236994
14  meter          E    =           
0008684
 Z    =        5019467
48                 I    =           51
33015
 XDOT =       5884
360651                 Wp   =          124
02173
 YDOT =       4547
696598  meter/sec      RA   =          229
40921  deg
 ZDOT =       1886
163474                 TA   =          307
58577
                                          MA   =          307
66460
                                          Ha   =            221
948  n
mi
                                          Hp   =            213
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5444653
17                 X    =         1682404
43
 Y    =      -13900899
42  feet           Y    =        -4218307
89  meter
 Z    =       16468069
14                 Z    =         5027584
69
 XDOT =      19305
645182                 XDOT =        5823
907824
 YDOT =      14920
264430  feet/sec       YDOT =        4613
161680  meter/sec
 ZDOT =       6188
200375                 ZDOT =        1914
600284

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11326211
76                 X    =         3452229
35
 Y    =       -9663702
24  feet           Y    =        -2945496
44  meter
 Z    =       16504736
90                 Z    =         5030643
81
 XDOT =       9094
931567                 XDOT =        2772
135142
 YDOT =      21483
579974  feet/sec       YDOT =        6548
195176  meter/sec
 ZDOT =       6314
245316                 ZDOT =        1924
581972


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   18053
55158171  
00016717  00000-0  10270-3 0  9030
2 25544  51
6365 230
2021 0002963 123
2363 236
9074 15
54107784 20687


Satellite: ISS
Catalog Number: 25544
Epoch time:      18053
55158171   =   yrday
fracday
Element set:     903
Inclination:       51
6365  deg
RA of node:       230
2021  deg
Eccentricity:     
0002963     
Arg of perigee:   123
2363  deg
Mean anomaly:     236
9074  deg
Mean motion:   15
54107784  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2068
Checksum:              291


Coasting Arc #5 (Orbit 2082)
---------------------------------------

Vector Time (GMT): 2018/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2994976
61                 A    =         6777309
84  meter
 Y    =        3001950
20  meter          E    =           
0017563
 Z    =       -5301969
10                 I    =           51
34873
 XDOT =      -5451
473933                 Wp   =           96
54110
 YDOT =      -5374
869210  meter/sec      RA   =          224
38905  deg
 ZDOT =         34
339938                 TA   =          173
79888
                                          MA   =          173
77711
                                          Ha   =            222
001  n
mi
                                          Hp   =            213
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9826038
75                 X    =        -3002568
70
 Y    =        9848917
98  feet           Y    =         2968415
59  meter
 Z    =      -17394911
76                 Z    =        -5316536
13
 XDOT =     -17885
413165                 XDOT =       -5391
132330
 YDOT =     -17634
085336  feet/sec       YDOT =       -5435
493943  meter/sec
 ZDOT =        112
663837                 ZDOT =           8
005654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13163998
20                 X    =        -4012386
65
 Y    =        4241183
09  feet           Y    =         1292712
61  meter
 Z    =      -17460145
91                 Z    =        -5321852
47
 XDOT =      -7395
626292                 XDOT =       -2254
186894
 YDOT =     -22946
052590  feet/sec       YDOT =       -6993
956829  meter/sec
 ZDOT =         -3
936064                 ZDOT =          -1
199712


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   18054
51610522  
00016717  00000-0  10270-3 0  9041
2 25544  51
6370 225
3938 0003210 126
3264 233
8185 15
54146022 20839


Satellite: ISS
Catalog Number: 25544
Epoch time:      18054
51610522   =   yrday
fracday
Element set:     904
Inclination:       51
6370  deg
RA of node:       225
3938  deg
Eccentricity:     
0003210     
Arg of perigee:   126
3264  deg
Mean anomaly:     233
8185  deg
Mean motion:   15
54146022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2083
Checksum:              274


Coasting Arc #6 (Orbit 2098)
---------------------------------------

Vector Time (GMT): 2018/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4241794
40                 A    =         6778614
78  meter
 Y    =       -1691024
47  meter          E    =           
0007242
 Z    =        5003812
13                 I    =           51
37571
 XDOT =       4620
374788                 Wp   =           81
65096
 YDOT =       5807
340125  meter/sec      RA   =          219
37031  deg
 ZDOT =      -1950
720281                 TA   =           27
35819
                                          MA   =           27
32007
                                          Ha   =            221
887  n
mi
                                          Hp   =            213
764

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13916648
30                 X    =         4236083
05
 Y    =       -5547980
54  feet           Y    =        -1643621
54  meter
 Z    =       16416706
45                 Z    =         5024403
23
 XDOT =      15158
709935                 XDOT =        4564
567599
 YDOT =      19052
953166  feet/sec       YDOT =        5858
696213  meter/sec
 ZDOT =      -6400
000923                 ZDOT =       -1928
412156

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14831007
01                 X    =         4520490
94
 Y    =        1211766
17  feet           Y    =          369346
33  meter
 Z    =       16508612
67                 Z    =         5031825
14
 XDOT =       5167
354260                 XDOT =        1575
009578
 YDOT =      22756
672946  feet/sec       YDOT =        6936
233914  meter/sec
 ZDOT =      -6301
362253                 ZDOT =       -1920
655215


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   18055
54492760  
00016717  00000-0  10270-3 0  9058
2 25544  51
6356 220
2645 0003214 130
9822 229
1609 15
54112285 20997


Satellite: ISS
Catalog Number: 25544
Epoch time:      18055
54492760   =   yrday
fracday
Element set:     905
Inclination:       51
6356  deg
RA of node:       220
2645  deg
Eccentricity:     
0003214     
Arg of perigee:   130
9822  deg
Mean anomaly:     229
1609  deg
Mean motion:   15
54112285  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2099
Checksum:              299


Coasting Arc #7 (Orbit 2113)
---------------------------------------

Vector Time (GMT): 2018/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5314248
38                 A    =         6781648
93  meter
 Y    =         429082
10  meter          E    =           
0011047
 Z    =       -4203027
78                 I    =           51
41424
 XDOT =      -3360
063301                 Wp   =          117
34010
 YDOT =      -5830
531642  meter/sec      RA   =          214
35999  deg
 ZDOT =       3655
626902                 TA   =          190
28650
                                          MA   =          190
30912
                                          Ha   =            221
893  n
mi
                                          Hp   =            213
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17435198
10                 X    =        -5298235
77
 Y    =        1407749
68  feet           Y    =          369743
91  meter
 Z    =      -13789461
22                 Z    =        -4228803
25
 XDOT =     -11023
829728                 XDOT =       -3312
371809
 YDOT =     -19129
040821  feet/sec       YDOT =       -5867
839385  meter/sec
 ZDOT =      11993
526582                 ZDOT =        3639
421193

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16252211
29                 X    =        -4953674
00
 Y    =       -6217132
21  feet           Y    =        -1894981
90  meter
 Z    =      -13904316
87                 Z    =        -4238035
78
 XDOT =      -2212
491197                 XDOT =        -674
367317
 YDOT =     -20861
636640  feet/sec       YDOT =       -6358
626848  meter/sec
 ZDOT =      11922
048729                 ZDOT =        3633
840453


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   18056
50944246  
00016717  00000-0  10270-3 0  9067
2 25544  51
6374 215
4561 0003164 134
9202 225
2208 15
54156151 21140


Satellite: ISS
Catalog Number: 25544
Epoch time:      18056
50944246   =   yrday
fracday
Element set:     906
Inclination:       51
6374  deg
RA of node:       215
4561  deg
Eccentricity:     
0003164     
Arg of perigee:   134
9202  deg
Mean anomaly:     225
2208  deg
Mean motion:   15
54156151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2114
Checksum:              281


Coasting Arc #8 (Orbit 2126)
---------------------------------------

Vector Time (GMT): 2018/057/06:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1694926
81                 A    =         6781511
41  meter
 Y    =       -4964820
79  meter          E    =           
0012311
 Z    =        4290335
02                 I    =           51
43786
 XDOT =       6778
775823                 Wp   =          112
28948
 YDOT =        735
053417  meter/sec      RA   =          210
46118  deg
 ZDOT =       3515
938372                 TA   =          301
76865
                                          MA   =          301
88854
                                          Ha   =            221
806  n
mi
                                          Hp   =            213
902

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5560783
51                 X    =        -1660122
64
 Y    =      -16288782
13  feet           Y    =        -4983579
85  meter
 Z    =       14075902
31                 Z    =         4282186
56
 XDOT =      22240
078160                 XDOT =        6752
974212
 YDOT =       2411
592574  feet/sec       YDOT =         810
714222  meter/sec
 ZDOT =      11535
230880                 ZDOT =        3548
803963

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17029830
09                 X    =         5190692
21
 Y    =       -2689893
43  feet           Y    =         -819879
52  meter
 Z    =       14040196
68                 Z    =         4279451
95
 XDOT =      -6482
802118                 XDOT =       -1975
958085
 YDOT =      20147
834707  feet/sec       YDOT =        6141
060019  meter/sec
 ZDOT =      11681
543180                 ZDOT =        3560
534361


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   18057
34535155  
00016717  00000-0  10270-3 0  9076
2 25544  51
6401 211
2936 0002603 130
7675 229
3704 15
54143713 21276


Satellite: ISS
Catalog Number: 25544
Epoch time:      18057
34535155   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:       211
2936  deg
Eccentricity:     
0002603     
Arg of perigee:   130
7675  deg
Mean anomaly:     229
3704  deg
Mean motion:   15
54143713  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2127
Checksum:              286


Coasting Arc #9 (Orbit 2141)
---------------------------------------

Vector Time (GMT): 2018/058/06:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 920932
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          60149
90                 A    =         6778284
11  meter
 Y    =        4507005
73  meter          E    =           
0014667
 Z    =       -5075438
06                 I    =           51
45488
 XDOT =      -7211
632915                 Wp   =           85
45586
 YDOT =      -1880
606517  meter/sec      RA   =          205
45244  deg
 ZDOT =      -1758
710495                 TA   =          167
48558
                                          MA   =          167
44912
                                          Ha   =            221
657  n
mi
                                          Hp   =            213
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         197342
20                 X    =           34400
10
 Y    =       14786764
20  feet           Y    =         4507534
10  meter
 Z    =      -16651699
69                 Z    =        -5075208
68
 XDOT =     -23660
212976                 XDOT =       -7181
524796
 YDOT =      -6169
968887  feet/sec       YDOT =       -1961
083705  meter/sec
 ZDOT =      -5770
047556                 ZDOT =       -1793
668053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14645058
83                 X    =        -4463813
93
 Y    =       -2055724
68  feet           Y    =         -626584
88  meter
 Z    =      -16651206
87                 Z    =        -5075287
85
 XDOT =       9710
309902                 XDOT =        2959
702458
 YDOT =     -21266
600107  feet/sec       YDOT =       -6482
059713  meter/sec
 ZDOT =      -5925
567529                 ZDOT =       -1806
112983


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   18058
30985719  
00016717  00000-0  10270-3 0  9089
2 25544  51
6387 206
4842 0002553 135
3188 224
8170 15
54180714 21421


Satellite: ISS
Catalog Number: 25544
Epoch time:      18058
30985719   =   yrday
fracday
Element set:     908
Inclination:       51
6387  deg
RA of node:       206
4842  deg
Eccentricity:     
0002553     
Arg of perigee:   135
3188  deg
Mean anomaly:     224
8170  deg
Mean motion:   15
54180714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2142
Checksum:              314


Coasting Arc #10 (Orbit 2152)
---------------------------------------

Vector Time (GMT): 2018/058/23:08:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1305431
53                 A    =         6779511
36  meter
 Y    =       -4630033
25  meter          E    =           
0010127
 Z    =        4772193
25                 I    =           51
47704
 XDOT =       7182
818758                 Wp   =          124
19475
 YDOT =        673
889329  meter/sec      RA   =          202
09274  deg
 ZDOT =       2609
122351                 TA   =          299
98824
                                          MA   =          300
08871
                                          Ha   =            221
689  n
mi
                                          Hp   =            213
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4282911
84                 X    =        -1276740
45
 Y    =      -15190397
80  feet           Y    =        -4644470
72  meter
 Z    =       15656802
01                 Z    =         4765922
09
 XDOT =      23565
678341                 XDOT =        7162
075881
 YDOT =       2210
922996  feet/sec       YDOT =         754
096750  meter/sec
 ZDOT =       8560
112700                 ZDOT =        2643
962697

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5383870
70                 X    =        -1641003
79
 Y    =       14864817
94  feet           Y    =         4530796
51  meter
 Z    =       15629398
33                 Z    =         4763840
61
 XDOT =     -16630
417726                 XDOT =       -5068
951323
 YDOT =     -15219
892501  feet/sec       YDOT =       -4639
023234  meter/sec
 ZDOT =       8715
267001                 ZDOT =        2656
413382


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   18059
01716070  
00016717  00000-0  10270-3 0  9091
2 25544  51
6365 202
9580 0002698 139
6292 220
5062 15
54190440 21532


Satellite: ISS
Catalog Number: 25544
Epoch time:      18059
01716070   =   yrday
fracday
Element set:     909
Inclination:       51
6365  deg
RA of node:       202
9580  deg
Eccentricity:     
0002698     
Arg of perigee:   139
6292  deg
Mean anomaly:     220
5062  deg
Mean motion:   15
54190440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2153
Checksum:              297


Coasting Arc #11 (Orbit 2167)
---------------------------------------

Vector Time (GMT): 2018/059/23:08:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -449372
27                 A    =         6777432
09  meter
 Y    =        4250285
30  meter          E    =           
0016233
 Z    =       -5273891
68                 I    =           51
50187
 XDOT =      -7434
458863                 Wp   =           92
53167
 YDOT =      -1681
866161  meter/sec      RA   =          197
08356  deg
 ZDOT =       -724
600226                 TA   =          170
53839
                                          MA   =          170
50777
                                          Ha   =            221
681  n
mi
                                          Hp   =            213
893

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1474318
47                 X    =         -471249
56
 Y    =       13944505
58  feet           Y    =         4245137
27  meter
 Z    =      -17302794
22                 Z    =        -5276128
07
 XDOT =     -24391
269234                 XDOT =       -7411
579602
 YDOT =      -5517
933600  feet/sec       YDOT =       -1764
875534  meter/sec
 ZDOT =      -2377
297330                 ZDOT =        -760
657614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9117381
91                 X    =         2778978
01
 Y    =      -10636465
95  feet           Y    =        -3241994
82  meter
 Z    =      -17313245
73                 Z    =        -5277077
30
 XDOT =      16016
091510                 XDOT =        4881
704692
 YDOT =      17845
448066  feet/sec       YDOT =        5439
292571  meter/sec
 ZDOT =      -2537
779906                 ZDOT =        -773
515315


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   18059
98166162  
00016717  00000-0  10270-3 0  9100
2 25544  51
6375 198
1487 0002728 140
5071 219
6281 15
54171330 21680


Satellite: ISS
Catalog Number: 25544
Epoch time:      18059
98166162   =   yrday
fracday
Element set:     910
Inclination:       51
6375  deg
RA of node:       198
1487  deg
Eccentricity:     
0002728     
Arg of perigee:   140
5071  deg
Mean anomaly:     219
6281  deg
Mean motion:   15
54171330  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2168
Checksum:              314


Coasting Arc #12 (Orbit 2177)
---------------------------------------

Vector Time (GMT): 2018/060/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3795379
92                 A    =         6782960
82  meter
 Y    =        4096001
71  meter          E    =           
0007532
 Z    =       -3856039
41                 I    =           51
54391
 XDOT =      -6183
024881                 Wp   =           98
54693
 YDOT =       1847
518203  meter/sec      RA   =          193
92319  deg
 ZDOT =      -4131
279628                 TA   =          127
97392
                                          MA   =          127
90586
                                          Ha   =            221
666  n
mi
                                          Hp   =            214
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12452033
87                 X    =         3768025
41
 Y    =       13438325
82  feet           Y    =         4138290
87  meter
 Z    =      -12651047
92                 Z    =        -3837670
11
 XDOT =     -20285
514703                 XDOT =       -6183
157694
 YDOT =       6061
411426  feet/sec       YDOT =        1778
374156  meter/sec
 ZDOT =     -13554
067021                 ZDOT =       -4161
314437

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15538388
02                 X    =         4736100
67
 Y    =        9810868
03  feet           Y    =         2990352
58  meter
 Z    =      -12569651
07                 Z    =        -3831229
65
 XDOT =     -17277
253414                 XDOT =       -5266
106841
 YDOT =       9860
308885  feet/sec       YDOT =        3005
422148  meter/sec
 ZDOT =     -13688
123409                 ZDOT =       -4172
140015


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   18060
62465832  
00016717  00000-0  10270-3 0  9110
2 25544  51
6410 194
9410 0002975 150
6464 209
4857 15
54179389 21781


Satellite: ISS
Catalog Number: 25544
Epoch time:      18060
62465832   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:       194
9410  deg
Eccentricity:     
0002975     
Arg of perigee:   150
6464  deg
Mean anomaly:     209
4857  deg
Mean motion:   15
54179389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2178
Checksum:              325


Coasting Arc #13 (Orbit 2193)
---------------------------------------

Vector Time (GMT): 2018/061/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2219387
74                 A    =         6779252
87  meter
 Y    =       -4218032
92  meter          E    =           
0009867
 Z    =        4816731
80                 I    =           51
56458
 XDOT =       7190
134779                 Wp   =          129
11318
 YDOT =       -894
820365  meter/sec      RA   =          188
92698  deg
 ZDOT =       2519
810970                 TA   =          296
04301
                                          MA   =          296
14456
                                          Ha   =            221
571  n
mi
                                          Hp   =            213
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7281455
84                 X    =        -2195452
28
 Y    =      -13838690
67  feet           Y    =        -4242717
16  meter
 Z    =       15802925
86                 Z    =         4806009
71
 XDOT =      23589
681034                 XDOT =        7187
366853
 YDOT =      -2935
762353  feet/sec       YDOT =        -814
430473  meter/sec
 ZDOT =       8267
096359                 ZDOT =        2554
730843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10855790
38                 X    =        -3308844
91
 Y    =      -11321393
08  feet           Y    =        -3450760
61  meter
 Z    =       15755611
65                 Z    =         4802310
43
 XDOT =      21035
690129                 XDOT =        6411
678351
 YDOT =      -8405
009371  feet/sec       YDOT =       -2561
846856  meter/sec
 ZDOT =       8422
829144                 ZDOT =        2567
278323


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   18061
65344832  
00016717  00000-0  10270-3 0  9121
2 25544  51
6414 189
8125 0002897 153
5615 206
5686 15
54225877 21944


Satellite: ISS
Catalog Number: 25544
Epoch time:      18061
65344832   =   yrday
fracday
Element set:     912
Inclination:       51
6414  deg
RA of node:       189
8125  deg
Eccentricity:     
0002897     
Arg of perigee:   153
5615  deg
Mean anomaly:     206
5686  deg
Mean motion:   15
54225877  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2194
Checksum:              329


Coasting Arc #14 (Orbit 2208)
---------------------------------------

Vector Time (GMT): 2018/062/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         407547
73                 A    =         6777333
32  meter
 Y    =        4232737
22  meter          E    =           
0015719
 Z    =       -5290738
79                 I    =           51
58986
 XDOT =      -7632
197082                 Wp   =           95
15847
 YDOT =        -33
048610  meter/sec      RA   =          183
92498  deg
 ZDOT =       -617
314420                 TA   =          168
95349
                                          MA   =          168
91894
                                          Ha   =            221
493  n
mi
                                          Hp   =            214
124

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1337098
86                 X    =          385885
05
 Y    =       13886933
12  feet           Y    =         4237172
80  meter
 Z    =      -17358066
89                 Z    =        -5288812
32
 XDOT =     -25040
016673                 XDOT =       -7628
261745
 YDOT =       -108
427198  feet/sec       YDOT =        -118
375171  meter/sec
 ZDOT =      -2025
309776                 ZDOT =        -654
378843

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5378835
72                 X    =         1639469
13
 Y    =       12883499
36  feet           Y    =         3926890
60  meter
 Z    =      -17349951
06                 Z    =        -5288265
08
 XDOT =     -23063
245862                 XDOT =       -7029
677339
 YDOT =       6692
040263  feet/sec       YDOT =        2039
733872  meter/sec
 ZDOT =      -2190
512115                 ZDOT =        -667
668093


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   18062
61793673  
00016717  00000-0  10270-3 0  9130
2 25544  51
6408 185
0049 0002816 157
5013 202
6263 15
54187366 22092


Satellite: ISS
Catalog Number: 25544
Epoch time:      18062
61793673   =   yrday
fracday
Element set:     913
Inclination:       51
6408  deg
RA of node:       185
0049  deg
Eccentricity:     
0002816     
Arg of perigee:   157
5013  deg
Mean anomaly:     202
6263  deg
Mean motion:   15
54187366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2209
Checksum:              306


Coasting Arc #15 (Orbit 2224)
---------------------------------------

Vector Time (GMT): 2018/063/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1439102
49                 A    =         6777545
54  meter
 Y    =       -4126799
83  meter          E    =           
0004360
 Z    =        5176317
65                 I    =           51
62516
 XDOT =       7496
359244                 Wp   =           92
38386
 YDOT =        924
941287  meter/sec      RA   =          178
92216  deg
 ZDOT =      -1345
905473                 TA   =           10
55116
                                          MA   =           10
54202
                                          Ha   =            221
288  n
mi
                                          Hp   =            214
107

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4721464
86                 X    =         1459998
98
 Y    =      -13539369
51  feet           Y    =        -4110589
21  meter
 Z    =       16982669
45                 Z    =         5183359
58
 XDOT =      24594
354474                 XDOT =        7491
996785
 YDOT =       3034
584274  feet/sec       YDOT =        1008
746145  meter/sec
 ZDOT =      -4415
700372                 ZDOT =       -1309
501898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         280586
15                 X    =           85522
66
 Y    =      -14298435
45  feet           Y    =        -4358163
13  meter
 Z    =       17014518
32                 Z    =         5186025
19
 XDOT =      23338
970598                 XDOT =        7113
718238
 YDOT =      -4606
641763  feet/sec       YDOT =       -1404
104409  meter/sec
 ZDOT =      -4253
527349                 ZDOT =       -1296
475136


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   18063
64671548  
00016717  00000-0  10270-3 0  9141
2 25544  51
6417 179
8758 0002696 161
3082 198
8170 15
54250255 22254


Satellite: ISS
Catalog Number: 25544
Epoch time:      18063
64671548   =   yrday
fracday
Element set:     914
Inclination:       51
6417  deg
RA of node:       179
8758  deg
Eccentricity:     
0002696     
Arg of perigee:   161
3082  deg
Mean anomaly:     198
8170  deg
Mean motion:   15
54250255  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2225
Checksum:              329


Coasting Arc #16 (Orbit 2226)
---------------------------------------

Vector Time (GMT): 2018/063/17:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3748675
55                 A    =         6780642
74  meter
 Y    =       -3438476
21  meter          E    =           
0011367
 Z    =        4478132
90                 I    =           51
63748
 XDOT =       6392
700565                 Wp   =          120
29198
 YDOT =      -2743
503203  meter/sec      RA   =          178
35678  deg
 ZDOT =       3233
072397                 TA   =          297
13592
                                          MA   =          297
25179
                                          Ha   =            221
583  n
mi
                                          Hp   =            214
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12298804
29                 X    =        -3731699
15
 Y    =      -11281089
93  feet           Y    =        -3480300
92  meter
 Z    =       14692037
08                 Z    =         4459965
06
 XDOT =      20973
427051                 XDOT =        6407
199650
 YDOT =      -9000
994760  feet/sec       YDOT =       -2671
934099  meter/sec
 ZDOT =      10607
192903                 ZDOT =        3264
161191

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15858952
71                 X    =        -4833808
79
 Y    =        5420260
35  feet           Y    =         1652095
35  meter
 Z    =       14611431
38                 Z    =         4453564
29
 XDOT =       2589
639363                 XDOT =         789
322078
 YDOT =     -21495
731148  feet/sec       YDOT =       -6551
898854  meter/sec
 ZDOT =      10746
083092                 ZDOT =        3275
406126


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   18063
77531416  
00016717  00000-0  10270-3 0  9155
2 25544  51
6403 179
2357 0002720 151
3417 208
7885 15
54220336 22270


Satellite: ISS
Catalog Number: 25544
Epoch time:      18063
77531416   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:       179
2357  deg
Eccentricity:     
0002720     
Arg of perigee:   151
3417  deg
Mean anomaly:     208
7885  deg
Mean motion:   15
54220336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2227
Checksum:              299


Coasting Arc #17 (Orbit 2241)
---------------------------------------

Vector Time (GMT): 2018/064/17:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905824
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2050476
35                 A    =         6777804
06  meter
 Y    =        3882417
06  meter          E    =           
0014587
 Z    =       -5176062
51                 I    =           51
66174
 XDOT =      -7266
196116                 Wp   =           89
58740
 YDOT =       1965
990994  meter/sec      RA   =          173
36180  deg
 ZDOT =      -1407
169624                 TA   =          166
88282
                                          MA   =          166
84485
                                          Ha   =            221
424  n
mi
                                          Hp   =            214
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6727284
62                 X    =         2032052
11
 Y    =       12737588
79  feet           Y    =         3905243
21  meter
 Z    =      -16981832
38                 Z    =        -5166147
33
 XDOT =     -23839
226102                 XDOT =       -7280
805087
 YDOT =       6450
101685  feet/sec       YDOT =        1884
653526  meter/sec
 ZDOT =      -4616
698242                 ZDOT =       -1442
501753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14456052
13                 X    =         4406204
69
 Y    =         -99035
71  feet           Y    =          -30186
09  meter
 Z    =      -16938060
88                 Z    =        -5162720
96
 XDOT =      -5423
703877                 XDOT =       -1653
144942
 YDOT =      23010
197509  feet/sec       YDOT =        7013
508201  meter/sec
 ZDOT =      -4774
434181                 ZDOT =       -1455
247538


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   18064
73978877  
00016717  00000-0  10270-3 0  9169
2 25544  51
6412 174
4277 0002640 156
3134 203
8141 15
54215141 22426


Satellite: ISS
Catalog Number: 25544
Epoch time:      18064
73978877   =   yrday
fracday
Element set:     916
Inclination:       51
6412  deg
RA of node:       174
4277  deg
Eccentricity:     
0002640     
Arg of perigee:   156
3134  deg
Mean anomaly:     203
8141  deg
Mean motion:   15
54215141  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2242
Checksum:              299
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