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


012/22:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 214 2

017/20:15:08 782 0 8 0 9 0 9
N/A 0 4 -0 1 221 6
000/00:00:17 563 -0 2 -0 0 214 2

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 1

Coasting Arc #1 (Orbit 1397)
---------------------------------------

Vector Time (GMT): 2018/010/11:02:00
930
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3861278
16                 A    =         6780369
56  meter
 Y    =        3317717
04  meter          E    =           
0008513
 Z    =       -4485814
89                 I    =           52
00944
 XDOT =      -1901
646008                 Wp   =           90
23094
 YDOT =       6653
385995  meter/sec      RA   =           84
15775  deg
 ZDOT =       3289
308092                 TA   =          212
74919
                                          MA   =          212
80200
                                          Ha   =            221
029  n
mi
                                          Hp   =            214
485

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12668235
43                 X    =         3845681
22
 Y    =       10884898
42  feet           Y    =         3360809
47  meter
 Z    =      -14717240
45                 Z    =        -4467095
95
 XDOT =      -6238
996089                 XDOT =       -1991
882297
 YDOT =      21828
694210  feet/sec       YDOT =        6631
615808  meter/sec
 ZDOT =      10791
693216                 ZDOT =        3279
851698

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9835457
75                 X    =        -2997847
52
 Y    =       13588986
40  feet           Y    =         4141923
06  meter
 Z    =      -14634397
44                 Z    =        -4460564
34
 XDOT =     -21270
869761                 XDOT =       -6483
361103
 YDOT =      -3839
021435  feet/sec       YDOT =       -1170
133733  meter/sec
 ZDOT =      10748
527755                 ZDOT =        3276
151260


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
46991590  
00016717  00000-0  10270-3 0  9000
2 25544  51
6415  84
9753 0003243 355
9001   4
2125 15
54310966 13980


Satellite: ISS
Catalog Number: 25544
Epoch time:      18010
46991590   =   yrday
fracday
Element set:     900
Inclination:       51
6415  deg
RA of node:        84
9753  deg
Eccentricity:     
0003243     
Arg of perigee:   355
9001  deg
Mean anomaly:       4
2125  deg
Mean motion:   15
54310966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1398
Checksum:              294


Coasting Arc #2 (Orbit 1413)
---------------------------------------

Vector Time (GMT): 2018/011/11:02:00
930
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3513189
26                 A    =         6784363
43  meter
 Y    =       -4789648
85  meter          E    =           
0013062
 Z    =        3270003
25                 I    =           52
01875
 XDOT =       2782
744336                 Wp   =           77
54085
 YDOT =      -5315
421493  meter/sec      RA   =           79
19587  deg
 ZDOT =      -4777
151521                 TA   =           64
73640
                                          MA   =           64
60109
                                          Ha   =            221
167  n
mi
                                          Hp   =            214
325

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11526211
50                 X    =        -3475252
91
 Y    =      -15714071
03  feet           Y    =        -4828723
80  meter
 Z    =       10728357
11                 Z    =         3253029
33
 XDOT =       9129
738634                 XDOT =        2865
180791
 YDOT =     -17439
046892  feet/sec       YDOT =       -5283
841750  meter/sec
 ZDOT =     -15673
069293                 ZDOT =       -4763
434027

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14520000
44                 X    =         4425696
13
 Y    =      -13059677
41  feet           Y    =        -3980589
67  meter
 Z    =       10653527
07                 Z    =         3247195
05
 XDOT =      17298
043651                 XDOT =        5272
443705
 YDOT =       6446
807905  feet/sec       YDOT =        1964
987050  meter/sec
 ZDOT =     -15611
123891                 ZDOT =       -4758
270562


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
49864366  
00016717  00000-0  10270-3 0  9015
2 25544  51
6420  79
8460 0003427    
7087 359
4070 15
54299086 14149


Satellite: ISS
Catalog Number: 25544
Epoch time:      18011
49864366   =   yrday
fracday
Element set:     901
Inclination:       51
6420  deg
RA of node:        79
8460  deg
Eccentricity:     
0003427     
Arg of perigee:      
7087  deg
Mean anomaly:     359
4070  deg
Mean motion:   15
54299086  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1414
Checksum:              308


Coasting Arc #3 (Orbit 1428)
---------------------------------------

Vector Time (GMT): 2018/012/11:02:00
930
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3038466
48                 A    =         6787715
34  meter
 Y    =        5813792
18  meter          E    =           
0010749
 Z    =       -1723752
27                 I    =           52
02178
 XDOT =      -3630
568274                 Wp   =           26
81266
 YDOT =       3587
607469  meter/sec      RA   =           74
24463  deg
 ZDOT =       5723
661774                 TA   =          314
37823
                                          MA   =          314
46621
                                          Ha   =            221
297  n
mi
                                          Hp   =            214
328

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9968722
05                 X    =         2981602
30
 Y    =       19074121
31  feet           Y    =         5847452
56  meter
 Z    =       -5655355
22                 Z    =        -1709130
25
 XDOT =     -11911
313234                 XDOT =       -3698
218429
 YDOT =      11770
365712  feet/sec       YDOT =        3546
629336  meter/sec
 ZDOT =      18778
417893                 ZDOT =        5705
861744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17812732
07                 X    =        -5429320
74
 Y    =       12108918
30  feet           Y    =         3690798
30  meter
 Z    =       -5591175
15                 Z    =        -1704190
19
 XDOT =     -12180
583212                 XDOT =       -3712
641763
 YDOT =      -9319
773214  feet/sec       YDOT =       -2840
666876  meter/sec
 ZDOT =      18698
556399                 ZDOT =        5699
319990


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
46307280  
00016717  00000-0  10270-3 0  9021
2 25544  51
6413  75
0379 0003558   2
3521 357
7648 15
54258837 14291


Satellite: ISS
Catalog Number: 25544
Epoch time:      18012
46307280   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:        75
0379  deg
Eccentricity:     
0003558     
Arg of perigee:     2
3521  deg
Mean anomaly:     357
7648  deg
Mean motion:   15
54258837  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1429
Checksum:              306


Coasting Arc #4 (Orbit 1436)
---------------------------------------

Vector Time (GMT): 2018/012/22:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 926807
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3351142
80                 A    =         6787490
21  meter
 Y    =       -5601690
70  meter          E    =           
0013373
 Z    =        1844297
03                 I    =           52
01718
 XDOT =       3381
062818                 Wp   =           98
63384
 YDOT =      -3900
542419  meter/sec      RA   =           71
85529  deg
 ZDOT =      -5670
614856                 TA   =           61
18682
                                          MA   =           61
05261
                                          Ha   =            221
358  n
mi
                                          Hp   =            214
187

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10994562
99                 X    =        -3297212
69
 Y    =      -18378250
34  feet           Y    =        -5638864
07  meter
 Z    =        6050843
27                 Z    =         1828149
02
 XDOT =      11092
725782                 XDOT =        3451
973140
 YDOT =     -12797
055180  feet/sec       YDOT =       -3862
336175  meter/sec
 ZDOT =     -18604
379450                 ZDOT =       -5654
018969

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18281195
12                 X    =        -5572108
27
 Y    =       11193420
35  feet           Y    =         3411754
52  meter
 Z    =        5979837
02                 Z    =         1822654
32
 XDOT =     -12079
326437                 XDOT =       -3681
778698
 YDOT =      -9770
343502  feet/sec       YDOT =       -2978
000699  meter/sec
 ZDOT =     -18529
825150                 ZDOT =       -5647
890706


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
97743593  
00016717  00000-0  10270-3 0  9039
2 25544  51
6417  72
4758 0003682   7
5464 352
5744 15
54277308 14371


Satellite: ISS
Catalog Number: 25544
Epoch time:      18012
97743593   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:        72
4758  deg
Eccentricity:     
0003682     
Arg of perigee:     7
5464  deg
Mean anomaly:     352
5744  deg
Mean motion:   15
54277308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1437
Checksum:              324


Coasting Arc #5 (Orbit 1451)
---------------------------------------

Vector Time (GMT): 2018/013/22:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906172
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2742235
87                 A    =         6788809
58  meter
 Y    =        6200235
48  meter          E    =           
0015193
 Z    =        -116238
14                 I    =           52
01176
 XDOT =      -4280
038565                 Wp   =           35
89345
 YDOT =       1998
616238  meter/sec      RA   =           66
90838  deg
 ZDOT =       6045
135245                 TA   =          322
86021
                                          MA   =          322
96523
                                          Ha   =            221
387  n
mi
                                          Hp   =            214
061

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8996836
86                 X    =         2673263
98
 Y    =       20341979
94  feet           Y    =         6230515
41  meter
 Z    =        -381358
74                 Z    =         -103084
46
 XDOT =     -14042
121275                 XDOT =       -4331
433357
 YDOT =       6557
139890  feet/sec       YDOT =        1950
466083  meter/sec
 ZDOT =      19833
120884                 ZDOT =        6024
219805

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20102177
19                 X    =         6127143
61
 Y    =       -9522724
57  feet           Y    =        -2902526
45  meter
 Z    =        -323797
50                 Z    =          -98693
48
 XDOT =       6229
077523                 XDOT =        1898
622829
 YDOT =      12532
062212  feet/sec       YDOT =        3819
772562  meter/sec
 ZDOT =      19739
631949                 ZDOT =        6016
639818


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
94185937  
00016717  00000-0  10270-3 0  9040
2 25544  51
6427  67
6668 0003850   8
4104 351
7112 15
54306425 14526


Satellite: ISS
Catalog Number: 25544
Epoch time:      18013
94185937   =   yrday
fracday
Element set:     904
Inclination:       51
6427  deg
RA of node:        67
6668  deg
Eccentricity:     
0003850     
Arg of perigee:     8
4104  deg
Mean anomaly:     351
7112  deg
Mean motion:   15
54306425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1452
Checksum:              300


Coasting Arc #6 (Orbit 1467)
---------------------------------------

Vector Time (GMT): 2018/014/22:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906172
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1884756
89                 A    =         6787694
10  meter
 Y    =       -6304605
78  meter          E    =           
0006092
 Z    =       -1663483
51                 I    =           51
99400
 XDOT =       5077
587223                 Wp   =          113
45528
 YDOT =         -8
407401  meter/sec      RA   =           61
96230  deg
 ZDOT =      -5740
099699                 TA   =           84
66698
                                          MA   =           84
59748
                                          Ha   =            221
442  n
mi
                                          Hp   =            214
036

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6183585
58                 X    =        -1806036
78
 Y    =      -20684402
18  feet           Y    =        -6325242
14  meter
 Z    =       -5457623
06                 Z    =        -1672448
20
 XDOT =      16658
750733                 XDOT =        5105
185913
 YDOT =        -27
583337  feet/sec       YDOT =          48
528422  meter/sec
 ZDOT =     -18832
348095                 ZDOT =       -5715
367796

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20400839
03                 X    =        -6218175
74
 Y    =        7032861
19  feet           Y    =         2143616
09  meter
 Z    =       -5496499
24                 Z    =        -1675332
97
 XDOT =       -239
252549                 XDOT =         -72
924177
 YDOT =     -15277
970891  feet/sec       YDOT =       -4656
725528  meter/sec
 ZDOT =     -18722
187062                 ZDOT =       -5706
522616


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
97057554  
00016717  00000-0  10270-3 0  9058
2 25544  51
6427  62
5379 0003750  12
6007 347
5239 15
54279884 14685


Satellite: ISS
Catalog Number: 25544
Epoch time:      18014
97057554   =   yrday
fracday
Element set:     905
Inclination:       51
6427  deg
RA of node:        62
5379  deg
Eccentricity:     
0003750     
Arg of perigee:    12
6007  deg
Mean anomaly:     347
5239  deg
Mean motion:   15
54279884  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1468
Checksum:              327


Coasting Arc #7 (Orbit 1483)
---------------------------------------

Vector Time (GMT): 2018/015/22:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906172
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         825430
20                 A    =         6784419
99  meter
 Y    =        5902760
54  meter          E    =           
0014615
 Z    =        3223916
73                 I    =           51
96594
 XDOT =      -5685
556462                 Wp   =           71
71846
 YDOT =      -1841
634373  meter/sec      RA   =           57
00767  deg
 ZDOT =       4814
235891                 TA   =          325
44117
                                          MA   =          325
53609
                                          Ha   =            221
580  n
mi
                                          Hp   =            213
863

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2708104
32                 X    =          743702
74
 Y    =       19366012
26  feet           Y    =         5911533
85  meter
 Z    =       10577154
63                 Z    =         3227728
27
 XDOT =     -18653
400465                 XDOT =       -5687
924920
 YDOT =      -6042
107522  feet/sec       YDOT =       -1905
227760  meter/sec
 ZDOT =      15794
737176                 ZDOT =        4786
611948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19172731
28                 X    =         5843848
49
 Y    =       -3800563
45  feet           Y    =        -1158411
74  meter
 Z    =       10593137
05                 Z    =         3228788
17
 XDOT =      -5176
700156                 XDOT =       -1577
858207
 YDOT =      17688
880669  feet/sec       YDOT =        5391
570828  meter/sec
 ZDOT =      15672
004283                 ZDOT =        4776
826906


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
99928915  
00016717  00000-0  10270-3 0  9060
2 25544  51
6417  57
4082 0004000  16
8901 343
2384 15
54295317 14847


Satellite: ISS
Catalog Number: 25544
Epoch time:      18015
99928915   =   yrday
fracday
Element set:     906
Inclination:       51
6417  deg
RA of node:        57
4082  deg
Eccentricity:     
0004000     
Arg of perigee:    16
8901  deg
Mean anomaly:     343
2384  deg
Mean motion:   15
54295317  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1484
Checksum:              311


Coasting Arc #8 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2018/016/22:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906172
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         443562
34                 A    =         6780391
15  meter
 Y    =       -5103254
98  meter          E    =           
0012076
 Z    =       -4454747
78                 I    =           51
93408
 XDOT =       5983
036145                 Wp   =           54
36427
 YDOT =       3428
241701  meter/sec      RA   =           52
04153  deg
 ZDOT =      -3331
062647                 TA   =          182
09523
                                          MA   =          182
10029
                                          Ha   =            221
508  n
mi
                                          Hp   =            213
855

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1455257
01                 X    =          522233
77
 Y    =      -16742962
52  feet           Y    =        -5097854
59  meter
 Z    =      -14615314
22                 Z    =        -4452402
40
 XDOT =      19629
383678                 XDOT =        5960
436212
 YDOT =      11247
512144  feet/sec       YDOT =        3495
021962  meter/sec
 ZDOT =     -10928
683224                 ZDOT =       -3302
054312

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16814051
84                 X    =        -5124923
00
 Y    =        -250556
43  feet           Y    =          -76369
60  meter
 Z    =      -14604001
47                 Z    =        -4451299
65
 XDOT =       9669
357835                 XDOT =        2947
220268
 YDOT =     -19286
433455  feet/sec       YDOT =       -5878
504917  meter/sec
 ZDOT =     -10800
054195                 ZDOT =       -3291
856519


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
96370404  
00016717  00000-0  10270-3 0  9073
2 25544  51
6418  52
5995 0003911  17
4609 342
6677 15
54319699 14993


Satellite: ISS
Catalog Number: 25544
Epoch time:      18016
96370404   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:        52
5995  deg
Eccentricity:     
0003911     
Arg of perigee:    17
4609  deg
Mean anomaly:     342
6677  deg
Mean motion:   15
54319699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1499
Checksum:              340


Coasting Arc #9 (Orbit 1512)
---------------------------------------

Vector Time (GMT): 2018/017/20:15:17
563
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1200711
80                 A    =         6778760
99  meter
 Y    =       -4462690
79  meter          E    =           
0014635
 Z    =       -4972722
21                 I    =           51
90864
 XDOT =       6084
338491                 Wp   =           61
87844
 YDOT =       4093
722710  meter/sec      RA   =           47
55327  deg
 ZDOT =      -2202
944807                 TA   =          186
67016
                                          MA   =          186
68966
                                          Ha   =            221
610  n
mi
                                          Hp   =            214
180

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3939343
16                 X    =         1274679
95
 Y    =      -14641373
99  feet           Y    =        -4448849
77  meter
 Z    =      -16314705
43                 Z    =        -4966710
27
 XDOT =      19961
740455                 XDOT =        6048
809717
 YDOT =      13430
848787  feet/sec       YDOT =        4161
563413  meter/sec
 ZDOT =      -7227
509210                 ZDOT =       -2173
475854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10686416
54                 X    =        -3257219
76
 Y    =      -10797526
75  feet           Y    =        -3291086
15  meter
 Z    =      -16287166
35                 Z    =        -4964328
30
 XDOT =      20819
679051                 XDOT =        6345
838175
 YDOT =      -9891
467862  feet/sec       YDOT =       -3014
919404  meter/sec
 ZDOT =      -7096
944959                 ZDOT =       -2163
148824


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
86382426  
00016717  00000-0  10270-3 0  9081
2 25544  51
6421  48
1102 0003559  16
0943 344
0323 15
54179564 15138


Satellite: ISS
Catalog Number: 25544
Epoch time:      18017
86382426   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:        48
1102  deg
Eccentricity:     
0003559     
Arg of perigee:    16
0943  deg
Mean anomaly:     344
0323  deg
Mean motion:   15
54179564  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1513
Checksum:              293


Coasting Arc #10 (Orbit 1527)
---------------------------------------

Vector Time (GMT): 2018/018/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5113833
37                 A    =         6780987
32  meter
 Y    =          16587
37  meter          E    =           
0011936
 Z    =        4448306
54                 I    =           51
89223
 XDOT =      -2922
795035                 Wp   =           56
36675
 YDOT =      -6264
657575  meter/sec      RA   =           42
83327  deg
 ZDOT =      -3323
878885                 TA   =           67
11238
                                          MA   =           66
98642
                                          Ha   =            221
835  n
mi
                                          Hp   =            214
119

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16777668
54                 X    =        -5135245
87
 Y    =          54420
52  feet           Y    =          -40718
91  meter
 Z    =       14594181
57                 Z    =         4423413
82
 XDOT =      -9589
222555                 XDOT =       -2836
379403
 YDOT =     -20553
338501  feet/sec       YDOT =       -6296
858966  meter/sec
 ZDOT =     -10905
114452                 ZDOT =       -3337
866869

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12840888
96                 X    =        -3913902
95
 Y    =       10946633
17  feet           Y    =         3336533
79  meter
 Z    =       14483302
51                 Z    =         4414510
61
 XDOT =     -19747
507262                 XDOT =       -6019
040214
 YDOT =      -8599
133182  feet/sec       YDOT =       -2621
015794  meter/sec
 ZDOT =     -10966
348139                 ZDOT =       -3342
542913


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
82833669  
00016717  00000-0  10270-3 0  9099
2 25544  51
6402  43
3019 0003571  20
0504 340
0788 15
54153060 15283


Satellite: ISS
Catalog Number: 25544
Epoch time:      18018
82833669   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:        43
3019  deg
Eccentricity:     
0003571     
Arg of perigee:    20
0504  deg
Mean anomaly:     340
0788  deg
Mean motion:   15
54153060  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1528
Checksum:              286


Coasting Arc #11 (Orbit 1542)
---------------------------------------

Vector Time (GMT): 2018/019/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5802596
80                 A    =         6784718
45  meter
 Y    =        1240876
83  meter          E    =           
0007062
 Z    =       -3290507
89                 I    =           51
88075
 XDOT =       1438
732799                 Wp   =           56
34439
 YDOT =       5840
011312  meter/sec      RA   =           37
86333  deg
 ZDOT =       4750
555419                 TA   =          265
59975
                                          MA   =          265
68044
                                          Ha   =            221
780  n
mi
                                          Hp   =            214
113

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19037391
09                 X    =         5804272
95
 Y    =        4071118
22  feet           Y    =         1305774
89  meter
 Z    =      -10795629
56                 Z    =        -3262317
37
 XDOT =       4720
251965                 XDOT =        1350
246074
 YDOT =      19160
142100  feet/sec       YDOT =        5855
605350  meter/sec
 ZDOT =      15585
811742                 ZDOT =        4757
329346

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17050978
06                 X    =         5197138
11
 Y    =       -9536829
92  feet           Y    =        -2906825
76  meter
 Z    =      -10670281
30                 Z    =        -3252301
74
 XDOT =      15408
912419                 XDOT =        4696
636505
 YDOT =      10120
233055  feet/sec       YDOT =        3084
647035  meter/sec
 ZDOT =      15614
981947                 ZDOT =        4759
446497


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
79284620  
00016717  00000-0  10270-3 0  9105
2 25544  51
6408  38
4931 0003522  22
2208 337
9096 15
54170837 15433


Satellite: ISS
Catalog Number: 25544
Epoch time:      18019
79284620   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:        38
4931  deg
Eccentricity:     
0003522     
Arg of perigee:    22
2208  deg
Mean anomaly:     337
9096  deg
Mean motion:   15
54170837  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1543
Checksum:              302


Coasting Arc #12 (Orbit 1558)
---------------------------------------

Vector Time (GMT): 2018/020/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6126194
76                 A    =         6788014
44  meter
 Y    =       -2328761
36  meter          E    =           
0014423
 Z    =        1748371
51                 I    =           51
86578
 XDOT =        311
767208                 Wp   =          101
05420
 YDOT =      -5124
611680  meter/sec      RA   =           32
90239  deg
 ZDOT =      -5696
297705                 TA   =           59
81680
                                          MA   =           59
67401
                                          Ha   =            221
816  n
mi
                                          Hp   =            214
023

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20099064
18                 X    =        -6108191
12
 Y    =       -7640293
19  feet           Y    =        -2397168
02  meter
 Z    =        5736127
00                 Z    =         1718656
87
 XDOT =       1022
858293                 XDOT =         396
717898
 YDOT =     -16813
030445  feet/sec       YDOT =       -5120
650267  meter/sec
 ZDOT =     -18688
640766                 ZDOT =       -5694
576978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20044958
51                 X    =        -6109703
35
 Y    =        7876698
20  feet           Y    =         2400817
61  meter
 Z    =        5604183
95                 Z    =         1708155
27
 XDOT =      -9878
135534                 XDOT =       -3010
855711
 YDOT =     -11759
057488  feet/sec       YDOT =       -3584
160722  meter/sec
 ZDOT =     -18680
096931                 ZDOT =       -5693
693544


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
82165360  
00016717  00000-0  10270-3 0  9111
2 25544  51
6415  33
3641 0003516  26
4278 333
7054 15
54156088 15596


Satellite: ISS
Catalog Number: 25544
Epoch time:      18020
82165360   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:        33
3641  deg
Eccentricity:     
0003516     
Arg of perigee:    26
4278  deg
Mean anomaly:     333
7054  deg
Mean motion:   15
54156088  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1559
Checksum:              291


Coasting Arc #13 (Orbit 1573)
---------------------------------------

Vector Time (GMT): 2018/021/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6012892
51                 A    =         6789216
49  meter
 Y    =        3134848
37  meter          E    =           
0015615
 Z    =         -61771
92                 I    =           51
84223
 XDOT =      -2149
496644                 Wp   =           41
04898
 YDOT =       4224
539796  meter/sec      RA   =           27
94559  deg
 ZDOT =       6031
660801                 TA   =          318
28726
                                          MA   =          318
40621
                                          Ha   =            221
877  n
mi
                                          Hp   =            213
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19727337
64                 X    =         5977690
96
 Y    =       10284935
61  feet           Y    =         3201891
83  meter
 Z    =        -202663
77                 Z    =          -32649
39
 XDOT =      -7052
154345                 XDOT =       -2225
874960
 YDOT =      13860
038700  feet/sec       YDOT =        4200
075633  meter/sec
 ZDOT =      19788
913389                 ZDOT =        6021
033937

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21420222
46                 X    =         6528883
81
 Y    =       -6013109
86  feet           Y    =        -1832795
89  meter
 Z    =         -73505
24                 Z    =          -22404
40
 XDOT =       3818
650917                 XDOT =        1163
924799
 YDOT =      13458
329767  feet/sec       YDOT =        4102
098913  meter/sec
 ZDOT =      19740
859508                 ZDOT =        6017
013978


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
78615712  
00016717  00000-0  10270-3 0  9129
2 25544  51
6418  28
5557 0003667  28
5307 331
6046 15
54167676 15744


Satellite: ISS
Catalog Number: 25544
Epoch time:      18021
78615712   =   yrday
fracday
Element set:     912
Inclination:       51
6418  deg
RA of node:        28
5557  deg
Eccentricity:     
0003667     
Arg of perigee:    28
5307  deg
Mean anomaly:     331
6046  deg
Mean motion:   15
54167676  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1574
Checksum:              317


Coasting Arc #14 (Orbit 1589)
---------------------------------------

Vector Time (GMT): 2018/022/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5419220
17                 A    =         6788023
69  meter
 Y    =       -3728632
21  meter          E    =           
0007251
 Z    =       -1672972
66                 I    =           51
80902
 XDOT =       3965
251071                 Wp   =          114
92403
 YDOT =      -3206
364849  meter/sec      RA   =           22
98838  deg
 ZDOT =      -5720
759575                 TA   =           83
35267
                                          MA   =           83
27014
                                          Ha   =            221
841  n
mi
                                          Hp   =            213
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17779593
74                 X    =        -5368996
53
 Y    =      -12233045
31  feet           Y    =        -3788952
85  meter
 Z    =       -5488755
43                 Z    =        -1699174
95
 XDOT =      13009
353909                 XDOT =        4028
598849
 YDOT =     -10519
569713  feet/sec       YDOT =       -3161
668564  meter/sec
 ZDOT =     -18768
896243                 ZDOT =       -5701
344133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21248910
64                 X    =        -6476667
96
 Y    =        3599699
45  feet           Y    =         1097188
39  meter
 Z    =       -5604796
85                 Z    =        -1708342
08
 XDOT =       2342
394585                 XDOT =         713
961869
 YDOT =     -15148
929862  feet/sec       YDOT =       -4617
393822  meter/sec
 ZDOT =     -18681
882208                 ZDOT =       -5694
237697


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
81496000  
00016717  00000-0  10270-3 0  9132
2 25544  51
6421  23
4276 0003441  32
3203 327
8160 15
54150230 15908


Satellite: ISS
Catalog Number: 25544
Epoch time:      18022
81496000   =   yrday
fracday
Element set:     913
Inclination:       51
6421  deg
RA of node:        23
4276  deg
Eccentricity:     
0003441     
Arg of perigee:    32
3203  deg
Mean anomaly:     327
8160  deg
Mean motion:   15
54150230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1590
Checksum:              254


Coasting Arc #15 (Orbit 1605)
---------------------------------------

Vector Time (GMT): 2018/023/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4379622
79                 A    =         6784807
83  meter
 Y    =        4068914
05  meter          E    =           
0015314
 Z    =        3191573
71                 I    =           51
76844
 XDOT =      -5555
864401                 Wp   =           75
36456
 YDOT =       2186
471580  meter/sec      RA   =           18
02135  deg
 ZDOT =       4820
969837                 TA   =          321
47389
                                          MA   =          321
58309
                                          Ha   =            221
870  n
mi
                                          Hp   =            213
748

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14368841
16                 X    =         4318294
78
 Y    =       13349455
54  feet           Y    =         4117547
12  meter
 Z    =       10471042
35                 Z    =         3212699
17
 XDOT =     -18227
901579                 XDOT =       -5603
318670
 YDOT =       7173
463188  feet/sec       YDOT =        2124
076816  meter/sec
 ZDOT =      15816
830173                 ZDOT =        4793
866387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19549112
02                 X    =         5958569
34
 Y    =        -734704
04  feet           Y    =         -223937
79  meter
 Z    =       10564408
02                 Z    =         3220031
56
 XDOT =      -7884
109592                 XDOT =       -2403
076604
 YDOT =      16635
819200  feet/sec       YDOT =        5070
597692  meter/sec
 ZDOT =      15695
763446                 ZDOT =        4784
068698


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   18023
84375942  
00016717  00000-0  10270-3 0  9148
2 25544  51
6426  18
2983 0003674  34
7604 325
3789 15
54170574 16060


Satellite: ISS
Catalog Number: 25544
Epoch time:      18023
84375942   =   yrday
fracday
Element set:     914
Inclination:       51
6426  deg
RA of node:        18
2983  deg
Eccentricity:     
0003674     
Arg of perigee:    34
7604  deg
Mean anomaly:     325
3789  deg
Mean motion:   15
54170574  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1606
Checksum:              322


Coasting Arc #16 (Orbit 1620)
---------------------------------------

Vector Time (GMT): 2018/024/18:52:00
000
Vector Time (MET): N/A
Weight (LBS)     : 906084
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2940370
19                 A    =         6780859
03  meter
 Y    =       -4248510
71  meter          E    =           
0012341
 Z    =       -4404283
04                 I    =           51
72380
 XDOT =       6767
224509                 Wp   =           59
72311
 YDOT =      -1174
711198  meter/sec      RA   =           13
04285  deg
 ZDOT =      -3385
760956                 TA   =          176
00323
                                          MA   =          175
99337
                                          Ha   =            221
903  n
mi
                                          Hp   =            213
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9646883
84                 X    =        -2871250
17
 Y    =      -13938683
43  feet           Y    =        -4281005
48  meter
 Z    =      -14449747
50                 Z    =        -4418398
33
 XDOT =      22202
180148                 XDOT =        6796
303597
 YDOT =      -3854
039363  feet/sec       YDOT =       -1098
872872  meter/sec
 ZDOT =     -11108
139621                 ZDOT =       -3352
817776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16670860
13                 X    =        -5081278
17
 Y    =       -2762754
83  feet           Y    =         -842087
67  meter
 Z    =      -14511859
80                 Z    =        -4423214
87
 XDOT =      12442
845335                 XDOT =        3792
579258
 YDOT =     -17523
433564  feet/sec       YDOT =       -5341
142550  meter/sec
 ZDOT =     -10961
253767                 ZDOT =       -3340
990148


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   18024
80825447  
00016717  00000-0  10270-3 0  9156
2 25544  51
6425  13
4904 0003655  36
6731 323
4671 15
54195478 16216


Satellite: ISS
Catalog Number: 25544
Epoch time:      18024
80825447   =   yrday
fracday
Element set:     915
Inclination:       51
6425  deg
RA of node:        13
4904  deg
Eccentricity:     
0003655     
Arg of perigee:    36
6731  deg
Mean anomaly:     323
4671  deg
Mean motion:   15
54195478  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1621
Checksum:              306
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