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

 
Date: January 10th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


013/10:05:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 214 3

017/20:15:11 040 0 9 1 1 1 1
N/A 0 5 -0 1 221 6
000/00:00:22 080 -0 3 -0 0 214 4

018/18:52:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 214 3

Coasting Arc #1 (Orbit 1367)
---------------------------------------

Vector Time (GMT): 2018/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2869618
53                 A    =         6781925
70  meter
 Y    =       -4604161
56  meter          E    =           
0011217
 Z    =        4065134
05                 I    =           52
01473
 XDOT =       3447
421961                 Wp   =           60
93880
 YDOT =      -5619
943533  meter/sec      RA   =           93
87684  deg
 ZDOT =      -3918
130541                 TA   =           69
52597
                                          MA   =           69
40559
                                          Ha   =            220
928  n
mi
                                          Hp   =            214
613

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9414758
97                 X    =        -2837666
42
 Y    =      -15105516
92  feet           Y    =        -4636073
04  meter
 Z    =       13337053
98                 Z    =         4051272
04
 XDOT =      11310
439503                 XDOT =        3529
041542
 YDOT =     -18438
134951  feet/sec       YDOT =       -5580
935645  meter/sec
 ZDOT =     -12854
758993                 ZDOT =       -3901
186171

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11637872
96                 X    =         3547223
68
 Y    =      -13527686
88  feet           Y    =        -4123238
96  meter
 Z    =       13276028
68                 Z    =         4046533
54
 XDOT =      19990
068848                 XDOT =        6092
972985
 YDOT =       4613
288177  feet/sec       YDOT =        1406
130236  meter/sec
 ZDOT =     -12778
435824                 ZDOT =       -3894
867239


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   18008
54103844  
00016717  00000-0  10270-3 0  9003
2 25544  51
6416  94
5927 0003284 348
0807  12
0268 15
54285888 13689


Satellite: ISS
Catalog Number: 25544
Epoch time:      18008
54103844   =   yrday
fracday
Element set:     900
Inclination:       51
6416  deg
RA of node:        94
5927  deg
Eccentricity:     
0003284     
Arg of perigee:   348
0807  deg
Mean anomaly:      12
0268  deg
Mean motion:   15
54285888  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1368
Checksum:              316


Coasting Arc #2 (Orbit 1382)
---------------------------------------

Vector Time (GMT): 2018/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2238425
58                 A    =         6785822
12  meter
 Y    =        5793690
98  meter          E    =           
0006856
 Z    =       -2727505
22                 I    =           52
02789
 XDOT =      -3984
563769                 Wp   =           30
27489
 YDOT =       3982
278963  meter/sec      RA   =           88
91997  deg
 ZDOT =       5200
393469                 TA   =          299
05811
                                          MA   =          299
12676
                                          Ha   =            220
994  n
mi
                                          Hp   =            214
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7343915
94                 X    =         2186721
32
 Y    =       19008172
50  feet           Y    =         5818433
57  meter
 Z    =       -8948507
94                 Z    =        -2716757
17
 XDOT =     -13072
715778                 XDOT =       -4054
059197
 YDOT =      13065
219695  feet/sec       YDOT =        3937
332108  meter/sec
 ZDOT =      17061
658363                 ZDOT =        5180
869261

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15765746
37                 X    =        -4805399
49
 Y    =       12943078
35  feet           Y    =         3945050
28  meter
 Z    =       -8901543
77                 Z    =        -2713190
54
 XDOT =     -15573
267694                 XDOT =       -4746
731993
 YDOT =      -7321
594382  feet/sec       YDOT =       -2231
621968  meter/sec
 ZDOT =      16974
087200                 ZDOT =        5173
701778


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   18009
50548029  
00016717  00000-0  10270-3 0  9019
2 25544  51
6408  89
7847 0003295 349
5494  10
5589 15
54259663 13835


Satellite: ISS
Catalog Number: 25544
Epoch time:      18009
50548029   =   yrday
fracday
Element set:     901
Inclination:       51
6408  deg
RA of node:        89
7847  deg
Eccentricity:     
0003295     
Arg of perigee:   349
5494  deg
Mean anomaly:      10
5589  deg
Mean motion:   15
54259663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1383
Checksum:              338


Coasting Arc #3 (Orbit 1398)
---------------------------------------

Vector Time (GMT): 2018/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1518803
89                 A    =         6788409
19  meter
 Y    =       -6526826
17  meter          E    =           
0011840
 Z    =        1057329
11                 I    =           52
03542
 XDOT =       4437
372514                 Wp   =          110
86275
 YDOT =      -2000
325644  meter/sec      RA   =           83
97225  deg
 ZDOT =      -5924
579585                 TA   =           57
73559
                                          MA   =           57
62091
                                          Ha   =            221
033  n
mi
                                          Hp   =            214
454

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4982952
38                 X    =        -1450842
21
 Y    =      -21413471
70  feet           Y    =        -6543430
53  meter
 Z    =        3468927
52                 Z    =         1050116
10
 XDOT =      14558
308773                 XDOT =        4488
189284
 YDOT =      -6562
748175  feet/sec       YDOT =       -1950
419521  meter/sec
 ZDOT =     -19437
597064                 ZDOT =       -5902
901101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18598210
19                 X    =         5668734
47
 Y    =      -11734049
34  feet           Y    =        -3576538
24  meter
 Z    =        3437834
56                 Z    =         1047851
97
 XDOT =      10151
070466                 XDOT =        3094
046278
 YDOT =      10375
041837  feet/sec       YDOT =        3162
312752  meter/sec
 ZDOT =     -19340
733448                 ZDOT =       -5895
055555


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   18010
53421523  
00016717  00000-0  10270-3 0  9024
2 25544  51
6411  84
6555 0003314 355
6325   4
4798 15
54284979 13991


Satellite: ISS
Catalog Number: 25544
Epoch time:      18010
53421523   =   yrday
fracday
Element set:     902
Inclination:       51
6411  deg
RA of node:        84
6555  deg
Eccentricity:     
0003314     
Arg of perigee:   355
6325  deg
Mean anomaly:       4
4798  deg
Mean motion:   15
54284979  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1399
Checksum:              309


Coasting Arc #4 (Orbit 1414)
---------------------------------------

Vector Time (GMT): 2018/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         745541
56                 A    =         6788764
31  meter
 Y    =        6702764
66  meter          E    =           
0015666
 Z    =         696861
19                 I    =           52
03220
 XDOT =      -4785
527698                 Wp   =           42
11994
 YDOT =        -98
022979  meter/sec      RA   =           79
02801  deg
 ZDOT =       5996
293818                 TA   =          325
37131
                                          MA   =          325
47323
                                          Ha   =            221
247  n
mi
                                          Hp   =            214
362

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2446002
50                 X    =          667149
06
 Y    =       21990697
72  feet           Y    =         6710663
46  meter
 Z    =        2286290
01                 Z    =          700292
73
 XDOT =     -15700
550191                 XDOT =       -4813
202637
 YDOT =       -321
597701  feet/sec       YDOT =        -151
693096  meter/sec
 ZDOT =      19672
879979                 ZDOT =        5972
980243

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19820098
92                 X    =        -6041166
15
 Y    =        9832203
19  feet           Y    =         2996855
53  meter
 Z    =        2300499
00                 Z    =          701192
10
 XDOT =      -4416
566873                 XDOT =       -1346
169583
 YDOT =     -13532
392882  feet/sec       YDOT =       -4124
673351  meter/sec
 ZDOT =      19569
063161                 ZDOT =        5964
650452


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   18011
56294721  
00016717  00000-0  10270-3 0  9037
2 25544  51
6414  79
5260 0003555    
6843 359
4314 15
54253034 14153


Satellite: ISS
Catalog Number: 25544
Epoch time:      18011
56294721   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:        79
5260  deg
Eccentricity:     
0003555     
Arg of perigee:      
6843  deg
Mean anomaly:     359
4314  deg
Mean motion:   15
54253034  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1415
Checksum:              284


Coasting Arc #5 (Orbit 1429)
---------------------------------------

Vector Time (GMT): 2018/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         145984
76                 A    =         6786400
20  meter
 Y    =       -6344237
36  meter          E    =           
0004401
 Z    =       -2408263
48                 I    =           52
01672
 XDOT =       4995
637418                 Wp   =           94
76668
 YDOT =       2159
230288  meter/sec      RA   =           74
08159  deg
 ZDOT =      -5394
182638                 TA   =          111
98693
                                          MA   =          111
94016
                                          Ha   =            221
230  n
mi
                                          Hp   =            214
224

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         478952
61                 X    =          228614
89
 Y    =      -20814427
04  feet           Y    =        -6342142
69  meter
 Z    =       -7901126
89                 Z    =        -2407354
07
 XDOT =      16389
886543                 XDOT =        4997
323002
 YDOT =       7084
088873  feet/sec       YDOT =        2215
104709  meter/sec
 ZDOT =     -17697
449599                 ZDOT =       -5369
911445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19615251
69                 X    =         5978728
71
 Y    =       -6985122
76  feet           Y    =        -2129065
42  meter
 Z    =       -7896045
59                 Z    =        -2406714
69
 XDOT =      -1186
725551                 XDOT =        -361
713948
 YDOT =      16518
339488  feet/sec       YDOT =        5034
789876  meter/sec
 ZDOT =     -17589
699923                 ZDOT =       -5361
340537


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   18012
52737984  
00016717  00000-0  10270-3 0  9048
2 25544  51
6406  74
7180 0003443   5
6042 354
5148 15
54290229 14309


Satellite: ISS
Catalog Number: 25544
Epoch time:      18012
52737984   =   yrday
fracday
Element set:     904
Inclination:       51
6406  deg
RA of node:        74
7180  deg
Eccentricity:     
0003443     
Arg of perigee:     5
6042  deg
Mean anomaly:     354
5148  deg
Mean motion:   15
54290229  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1430
Checksum:              291


Coasting Arc #6 (Orbit 1443)
---------------------------------------

Vector Time (GMT): 2018/013/10:05:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904658
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4323815
52                 A    =         6784027
72  meter
 Y    =        3971524
92  meter          E    =           
0006151
 Z    =       -3399977
81                 I    =           52
00074
 XDOT =      -1703
756065                 Wp   =           55
82133
 YDOT =       5839
298452  meter/sec      RA   =           69
46873  deg
 ZDOT =       4663
572813                 TA   =          264
68771
                                          MA   =          264
75790
                                          Ha   =            221
254  n
mi
                                          Hp   =            214
283

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14185746
45                 X    =         4295598
68
 Y    =       13029937
40  feet           Y    =         4019719
27  meter
 Z    =      -11154782
83                 Z    =        -3379042
59
 XDOT =      -5589
750868                 XDOT =       -1791
579062
 YDOT =      19157
803319  feet/sec       YDOT =        5819
754489  meter/sec
 ZDOT =      15300
435737                 ZDOT =        4655
083744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14593760
47                 X    =        -4448178
19
 Y    =       12652823
28  feet           Y    =         3856580
54  meter
 Z    =      -11062190
99                 Z    =        -3371755
81
 XDOT =     -17447
827494                 XDOT =       -5318
097820
 YDOT =      -6808
346577  feet/sec       YDOT =       -2075
184037  meter/sec
 ZDOT =      15261
665397                 ZDOT =        4651
755613


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   18013
42751480  
00016717  00000-0  10270-3 0  9056
2 25544  51
6417  70
2294 0003302   5
3979 354
7209 15
54292963 14440


Satellite: ISS
Catalog Number: 25544
Epoch time:      18013
42751480   =   yrday
fracday
Element set:     905
Inclination:       51
6417  deg
RA of node:        70
2294  deg
Eccentricity:     
0003302     
Arg of perigee:     5
3979  deg
Mean anomaly:     354
7209  deg
Mean motion:   15
54292963  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1444
Checksum:              300


Coasting Arc #7 (Orbit 1459)
---------------------------------------

Vector Time (GMT): 2018/014/10:05:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904658
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4037981
05                 A    =         6787431
11  meter
 Y    =       -5129765
11  meter          E    =           
0013599
 Z    =        1840411
49                 I    =           51
99991
 XDOT =       2859
709682                 Wp   =           99
63069
 YDOT =      -4297
573466  meter/sec      RA   =           64
51521  deg
 ZDOT =      -5670
867777                 TA   =           60
22855
                                          MA   =           60
09335
                                          Ha   =            221
332  n
mi
                                          Hp   =            214
096

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13247969
31                 X    =        -3989258
18
 Y    =      -16829938
03  feet           Y    =        -5174648
30  meter
 Z    =        6038095
42                 Z    =         1820914
50
 XDOT =       9382
249613                 XDOT =        2935
099576
 YDOT =     -14099
650480  feet/sec       YDOT =       -4265
172257  meter/sec
 ZDOT =     -18605
209241                 ZDOT =       -5656
793668

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18059821
58                 X    =         5504633
62
 Y    =      -11559816
89  feet           Y    =        -3523432
19  meter
 Z    =        5952107
15                 Z    =         1814202
26
 XDOT =      12250
279957                 XDOT =        3733
885331
 YDOT =       9534
284933  feet/sec       YDOT =        2906
050048  meter/sec
 ZDOT =     -18541
807066                 ZDOT =       -5651
542794


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   18014
45623824  
00016717  00000-0  10270-3 0  9061
2 25544  51
6419  65
1002 0003459  11
2839 348
8391 15
54302148 14607


Satellite: ISS
Catalog Number: 25544
Epoch time:      18014
45623824   =   yrday
fracday
Element set:     906
Inclination:       51
6419  deg
RA of node:        65
1002  deg
Eccentricity:     
0003459     
Arg of perigee:    11
2839  deg
Mean anomaly:     348
8391  deg
Mean motion:   15
54302148  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1460
Checksum:              292


Coasting Arc #8 (Orbit 1474)
---------------------------------------

Vector Time (GMT): 2018/015/10:05:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904658
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3510390
08                 A    =         6788941
12  meter
 Y    =        5800398
59  meter          E    =           
0015201
 Z    =        -113525
17                 I    =           51
98909
 XDOT =      -3993
644156                 Wp   =           37
48409
 YDOT =       2526
707555  meter/sec      RA   =           59
56762  deg
 ZDOT =       6043
124825                 TA   =          321
29834
                                          MA   =          321
40716
                                          Ha   =            221
511  n
mi
                                          Hp   =            214
025

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11517027
81                 X    =         3445819
00
 Y    =       19030179
09  feet           Y    =         5839293
14  meter
 Z    =        -372457
92                 Z    =          -96629
52
 XDOT =     -13102
507072                 XDOT =       -4050
955590
 YDOT =       8289
722949  feet/sec       YDOT =        2481
726975  meter/sec
 ZDOT =      19826
525018                 ZDOT =        6023
586340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19907276
29                 X    =        -6067737
81
 Y    =        9926722
16  feet           Y    =         3025664
91  meter
 Z    =        -298175
25                 Z    =          -90883
81
 XDOT =      -6459
207692                 XDOT =       -1968
766504
 YDOT =     -12414
077831  feet/sec       YDOT =       -3783
810923  meter/sec
 ZDOT =      19739
072634                 ZDOT =        6016
469339


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   18015
42066382  
00016717  00000-0  10270-3 0  9070
2 25544  51
6414  60
2917 0003663  14
1618 345
9637 15
54261312 14751


Satellite: ISS
Catalog Number: 25544
Epoch time:      18015
42066382   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:        60
2917  deg
Eccentricity:     
0003663     
Arg of perigee:    14
1618  deg
Mean anomaly:     345
9637  deg
Mean motion:   15
54261312  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1475
Checksum:              295


Coasting Arc #9 (Orbit 1490)
---------------------------------------

Vector Time (GMT): 2018/016/10:05:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904658
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2672955
80                 A    =         6787612
84  meter
 Y    =       -6012480
35  meter          E    =           
0006540
 Z    =       -1664351
33                 I    =           51
96670
 XDOT =       5038
016469                 Wp   =          114
78249
 YDOT =       -657
094907  meter/sec      RA   =           54
61976  deg
 ZDOT =      -5737
618770                 TA   =           83
35714
                                          MA   =           83
28270
                                          Ha   =            221
451  n
mi
                                          Hp   =            213
882

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8769540
03                 X    =        -2597439
56
 Y    =      -19725985
40  feet           Y    =        -6041948
82  meter
 Z    =       -5460470
25                 Z    =        -1677152
43
 XDOT =      16528
925423                 XDOT =        5072
859718
 YDOT =      -2155
823185  feet/sec       YDOT =        -600
561130  meter/sec
 ZDOT =     -18824
208563                 ZDOT =       -5713
061650

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20248719
23                 X    =         6171809
62
 Y    =       -7442712
38  feet           Y    =        -2268538
73  meter
 Z    =       -5516472
57                 Z    =        -1681420
84
 XDOT =        535
983745                 XDOT =         163
367845
 YDOT =      15280
517321  feet/sec       YDOT =        4657
501679  meter/sec
 ZDOT =     -18714
713829                 ZDOT =       -5704
244775


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   18016
44938360  
00016717  00000-0  10270-3 0  9088
2 25544  51
6404  55
1626 0003521  19
4561 340
6725 15
54304847 14917


Satellite: ISS
Catalog Number: 25544
Epoch time:      18016
44938360   =   yrday
fracday
Element set:     908
Inclination:       51
6404  deg
RA of node:        55
1626  deg
Eccentricity:     
0003521     
Arg of perigee:    19
4561  deg
Mean anomaly:     340
6725  deg
Mean motion:   15
54304847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1491
Checksum:              299


Coasting Arc #10 (Orbit 1506)
---------------------------------------

Vector Time (GMT): 2018/017/10:05:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904658
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1572223
56                 A    =         6784358
03  meter
 Y    =        5750026
31  meter          E    =           
0014677
 Z    =        3222512
35                 I    =           51
93648
 XDOT =      -5876
105249                 Wp   =           73
92562
 YDOT =      -1098
133120  meter/sec      RA   =           49
66300  deg
 ZDOT =       4812
150081                 TA   =          323
23175
                                          MA   =          323
33234
                                          Ha   =            221
514  n
mi
                                          Hp   =            213
779

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5158213
78                 X    =         1492155
40
 Y    =       18864915
71  feet           Y    =         5767160
11  meter
 Z    =       10572547
07                 Z    =         3229955
39
 XDOT =     -19278
560528                 XDOT =       -5886
763354
 YDOT =      -3602
798950  feet/sec       YDOT =       -1163
903630  meter/sec
 ZDOT =      15787
893967                 ZDOT =        4783
580584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19085502
08                 X    =        -5817261
04
 Y    =        4189801
99  feet           Y    =         1277051
65  meter
 Z    =       10604722
30                 Z    =         3232319
36
 XDOT =       4820
346678                 XDOT =        1469
241667
 YDOT =     -17798
250317  feet/sec       YDOT =       -5424
906697  meter/sec
 ZDOT =      15660
824819                 ZDOT =        4773
419405


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   18017
47809888  
00016717  00000-0  10270-3 0  9095
2 25544  51
6408  50
0326 0003587  22
8394 337
2917 15
54313397 15079


Satellite: ISS
Catalog Number: 25544
Epoch time:      18017
47809888   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:        50
0326  deg
Eccentricity:     
0003587     
Arg of perigee:    22
8394  deg
Mean anomaly:     337
2917  deg
Mean motion:   15
54313397  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1507
Checksum:              328


Coasting Arc #11 (Orbit 1512)
---------------------------------------

Vector Time (GMT): 2018/017/20:15:22
080
Vector Time (MET): N/A
Weight (LBS)     : 904547
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1204958
53                 A    =         6778912
71  meter
 Y    =       -4459833
79  meter          E    =           
0014387
 Z    =       -4974234
57                 I    =           51
90864
 XDOT =       6083
329993                 Wp   =           61
81678
 YDOT =       4097
756207  meter/sec      RA   =           47
55371  deg
 ZDOT =      -2198
592345                 TA   =          186
77659
                                          MA   =          186
79606
                                          Ha   =            221
600  n
mi
                                          Hp   =            214
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3953276
01                 X    =         1278901
77
 Y    =      -14632000
63  feet           Y    =        -4445945
42  meter
 Z    =      -16319667
22                 Z    =        -4968202
06
 XDOT =      19958
431734                 XDOT =        6047
735048
 YDOT =      13444
082045  feet/sec       YDOT =        4165
585262  meter/sec
 ZDOT =      -7213
229477                 ZDOT =       -2169
128451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10674894
90                 X    =        -3253707
97
 Y    =      -10801459
20  feet           Y    =        -3292284
76  meter
 Z    =      -16292037
01                 Z    =        -4965812
88
 XDOT =      20825
664958                 XDOT =        6347
662679
 YDOT =      -9889
889626  feet/sec       YDOT =       -3014
438358  meter/sec
 ZDOT =      -7082
688447                 ZDOT =       -2158
803439


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   18017
86386876  
00016717  00000-0  10270-3 0  9107
2 25544  51
6421  48
1107 0003404  12
7116 347
4122 15
54125244 15137


Satellite: ISS
Catalog Number: 25544
Epoch time:      18017
86386876   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        48
1107  deg
Eccentricity:     
0003404     
Arg of perigee:    12
7116  deg
Mean anomaly:     347
4122  deg
Mean motion:   15
54125244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1513
Checksum:              278


Coasting Arc #12 (Orbit 1527)
---------------------------------------

Vector Time (GMT): 2018/018/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904547
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5094201
25                 A    =         6781063
67  meter
 Y    =          58714
88  meter          E    =           
0011612
 Z    =        4470740
93                 I    =           51
89197
 XDOT =      -2966
450642                 Wp   =           55
54436
 YDOT =      -6264
199135  meter/sec      RA   =           42
83455  deg
 ZDOT =      -3285
394405                 TA   =           67
49773
                                          MA   =           67
37484
                                          Ha   =            221
828  n
mi
                                          Hp   =            214
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16713258
69                 X    =        -5116195
26
 Y    =         192634
13  feet           Y    =            1624
89  meter
 Z    =       14667785
20                 Z    =         4445942
16
 XDOT =      -9732
449612                 XDOT =       -2880
223825
 YDOT =     -20551
834431  feet/sec       YDOT =       -6296
889770  meter/sec
 ZDOT =     -10778
853035                 ZDOT =       -3299
594907

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12702784
31                 X    =        -3871808
66
 Y    =       11010805
00  feet           Y    =         3356093
36  meter
 Z    =       14557317
43                 Z    =         4437070
35
 XDOT =     -19851
784038                 XDOT =       -6050
823775
 YDOT =      -8514
954551  feet/sec       YDOT =       -2595
358147  meter/sec
 ZDOT =     -10841
033394                 ZDOT =       -3304
346978


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   18018
82841525  
00016717  00000-0  10270-3 0  9112
2 25544  51
6402  43
3026 0003417  16
6908 343
4356 15
54097849 15289


Satellite: ISS
Catalog Number: 25544
Epoch time:      18018
82841525   =   yrday
fracday
Element set:     911
Inclination:       51
6402  deg
RA of node:        43
3026  deg
Eccentricity:     
0003417     
Arg of perigee:    16
6908  deg
Mean anomaly:     343
4356  deg
Mean motion:   15
54097849  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1528
Checksum:              305


Coasting Arc #13 (Orbit 1542)
---------------------------------------

Vector Time (GMT): 2018/019/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904547
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5788273
44                 A    =         6784753
19  meter
 Y    =        1183962
90  meter          E    =           
0006787
 Z    =       -3336684
15                 I    =           51
88034
 XDOT =       1510
891775                 Wp   =           57
28818
 YDOT =       5855
140174  meter/sec      RA   =           37
86472  deg
 ZDOT =       4709
114579                 TA   =          264
02450
                                          MA   =          264
10185
                                          Ha   =            221
774  n
mi
                                          Hp   =            214
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18990398
43                 X    =         5790811
37
 Y    =        3884392
73  feet           Y    =         1248705
60  meter
 Z    =      -10947126
48                 Z    =        -3308561
12
 XDOT =       4956
994014                 XDOT =        1422
431807
 YDOT =      19209
777474  feet/sec       YDOT =        5871
541293  meter/sec
 ZDOT =      15449
850980                 ZDOT =        4716
239087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16893285
51                 X    =         5149073
42
 Y    =       -9646918
88  feet           Y    =        -2940380
87  meter
 Z    =      -10822069
04                 Z    =        -3298566
64
 XDOT =      15612
279023                 XDOT =        4758
622646
 YDOT =      10012
382532  feet/sec       YDOT =        3051
774196  meter/sec
 ZDOT =      15480
580090                 ZDOT =        4718
480811


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   18019
79295932  
00016717  00000-0  10270-3 0  9125
2 25544  51
6408  38
4940 0003372  18
7439 341
3838 15
54114879 15439


Satellite: ISS
Catalog Number: 25544
Epoch time:      18019
79295932   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:        38
4940  deg
Eccentricity:     
0003372     
Arg of perigee:    18
7439  deg
Mean anomaly:     341
3838  deg
Mean motion:   15
54114879  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1543
Checksum:              328


Coasting Arc #14 (Orbit 1558)
---------------------------------------

Vector Time (GMT): 2018/020/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904547
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6129705
81                 A    =         6788070
12  meter
 Y    =       -2262191
50  meter          E    =           
0014249
 Z    =        1822168
39                 I    =           51
86542
 XDOT =        210
362438                 Wp   =          100
54775
 YDOT =      -5162
549280  meter/sec      RA   =           32
90378  deg
 ZDOT =      -5666
551647                 TA   =           59
48237
                                          MA   =           59
34178
                                          Ha   =            221
814  n
mi
                                          Hp   =            214
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20110583
35                 X    =        -6112804
76
 Y    =       -7421888
12  feet           Y    =        -2330643
58  meter
 Z    =        5978242
76                 Z    =         1792434
03
 XDOT =        690
165479                 XDOT =         295
600405
 YDOT =     -16937
497639  feet/sec       YDOT =       -5159
720239  meter/sec
 ZDOT =     -18591
048710                 ZDOT =       -5665
322802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19907865
75                 X    =        -6067917
48
 Y    =        8047247
67  feet           Y    =         2452801
09  meter
 Z    =        5846200
39                 Z    =         1781921
88
 XDOT =     -10196
164700                 XDOT =       -3107
791001
 YDOT =     -11637
181471  feet/sec       YDOT =       -3547
012912  meter/sec
 ZDOT =     -18584
689106                 ZDOT =       -5664
613239


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   18020
82180410  
00016717  00000-0  10270-3 0  9136
2 25544  51
6415  33
3653 0003366  22
9372 337
1931 15
54099423 15599


Satellite: ISS
Catalog Number: 25544
Epoch time:      18020
82180410   =   yrday
fracday
Element set:     913
Inclination:       51
6415  deg
RA of node:        33
3653  deg
Eccentricity:     
0003366     
Arg of perigee:    22
9372  deg
Mean anomaly:     337
1931  deg
Mean motion:   15
54099423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1559
Checksum:              289


Coasting Arc #15 (Orbit 1573)
---------------------------------------

Vector Time (GMT): 2018/021/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904547
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6046529
35                 A    =         6789375
51  meter
 Y    =        3066678
45  meter          E    =           
0015239
 Z    =        -158696
58                 I    =           51
84225
 XDOT =      -2025
355314                 Wp   =           39
70373
 YDOT =       4288
295552  meter/sec      RA   =           27
94705  deg
 ZDOT =       6029
295312                 TA   =          318
59087
                                          MA   =          318
70627
                                          Ha   =            221
877  n
mi
                                          Hp   =            214
057

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19837694
72                 X    =         6012558
39
 Y    =       10061281
00  feet           Y    =         3134104
94  meter
 Z    =        -520658
07                 Z    =         -129407
67
 XDOT =      -6644
866515                 XDOT =       -2102
444300
 YDOT =      14069
211129  feet/sec       YDOT =        4265
215649  meter/sec
 ZDOT =      19781
152598                 ZDOT =        6019
269747

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21349012
48                 X    =         6507179
01
 Y    =       -6253125
21  feet           Y    =        -1905952
56  meter
 Z    =        -390746
82                 Z    =         -119099
63
 XDOT =       4241
234723                 XDOT =        1292
728344
 YDOT =      13337
050843  feet/sec       YDOT =        4065
133097  meter/sec
 ZDOT =      19735
765646                 ZDOT =        6015
461369


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   18021
78634315  
00016717  00000-0  10270-3 0  9141
2 25544  51
6418  28
5571 0003519  25
1053 335
0270 15
54110862 15749


Satellite: ISS
Catalog Number: 25544
Epoch time:      18021
78634315   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:        28
5571  deg
Eccentricity:     
0003519     
Arg of perigee:    25
1053  deg
Mean anomaly:     335
0270  deg
Mean motion:   15
54110862  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1574
Checksum:              284


Coasting Arc #16 (Orbit 1589)
---------------------------------------

Vector Time (GMT): 2018/022/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904547
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5494766
75                 A    =         6788348
78  meter
 Y    =       -3665803
90  meter          E    =           
0007324
 Z    =       -1561697
00                 I    =           51
80955
 XDOT =       3830
476698                 Wp   =          117
39652
 YDOT =      -3297
605774  meter/sec      RA   =           22
99030  deg
 ZDOT =      -5760
828529                 TA   =           79
62586
                                          MA   =           79
54331
                                          Ha   =            221
845  n
mi
                                          Hp   =            214
068

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18027449
98                 X    =        -5445780
57
 Y    =      -12026915
68  feet           Y    =        -3726976
27  meter
 Z    =       -5123677
81                 Z    =        -1588269
27
 XDOT =      12567
180767                 XDOT =        3895
049403
 YDOT =     -10818
916580  feet/sec       YDOT =       -3254
409780  meter/sec
 ZDOT =     -18900
356066                 ZDOT =       -5742
064789

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21284591
92                 X    =        -6487543
62
 Y    =        3921968
21  feet           Y    =         1195415
91  meter
 Z    =       -5241377
67                 Z    =        -1597571
91
 XDOT =       1840
823131                 XDOT =         561
082890
 YDOT =     -15053
278748  feet/sec       YDOT =       -4588
239362  meter/sec
 ZDOT =     -18816
228460                 ZDOT =       -5735
186435


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   18022
81518450  
00016717  00000-0  10270-3 0  9158
2 25544  51
6421  23
4293 0003299  28
7880 331
3454 15
54091841 15906


Satellite: ISS
Catalog Number: 25544
Epoch time:      18022
81518450   =   yrday
fracday
Element set:     915
Inclination:       51
6421  deg
RA of node:        23
4293  deg
Eccentricity:     
0003299     
Arg of perigee:    28
7880  deg
Mean anomaly:     331
3454  deg
Mean motion:   15
54091841  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1590
Checksum:              298
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