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

 
Date: April 26th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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


117/05:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 214 2

121/08:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 214 0

122/14:29:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 213 9

128/00:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 5

Coasting Arc #1 (Orbit 3031)
---------------------------------------

Vector Time (GMT): 2018/115/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         818571
90                 A    =         6786696
53  meter
 Y    =        6276822
11  meter          E    =           
0013755
 Z    =        2434098
05                 I    =           51
27611
 XDOT =      -4831
664500                 Wp   =           93
87183
 YDOT =       2698
739052  meter/sec      RA   =          280
52875  deg
 ZDOT =      -5309
288434                 TA   =           58
73809
                                          MA   =           58
60342
                                          Ha   =            221
337  n
mi
                                          Hp   =            214
359

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2685603
36                 X    =          736498
32
 Y    =       20593248
40  feet           Y    =         6285517
16  meter
 Z    =        7985885
99                 Z    =         2437874
76
 XDOT =     -15851
917652                 XDOT =       -4835
693610
 YDOT =       8854
130749  feet/sec       YDOT =        2644
685269  meter/sec
 ZDOT =     -17418
925309                 ZDOT =       -5332
768993

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13307936
12                 X    =         4056258
93
 Y    =       15935430
86  feet           Y    =         4857119
33  meter
 Z    =        8001849
76                 Z    =         2438963
81
 XDOT =      -7330
990874                 XDOT =       -2234
486018
 YDOT =      14963
047881  feet/sec       YDOT =        4560
736994  meter/sec
 ZDOT =     -17524
005314                 ZDOT =       -5341
316820


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   18115
53706808  
00016717  00000-0  10270-3 0  9000
2 25544  51
6361 281
1814 0002773  10
0177 350
1030 15
54167441 30322


Satellite: ISS
Catalog Number: 25544
Epoch time:      18115
53706808   =   yrday
fracday
Element set:     900
Inclination:       51
6361  deg
RA of node:       281
1814  deg
Eccentricity:     
0002773     
Arg of perigee:    10
0177  deg
Mean anomaly:     350
1030  deg
Mean motion:   15
54167441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3032
Checksum:              266


Coasting Arc #2 (Orbit 3046)
---------------------------------------

Vector Time (GMT): 2018/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          -6224
26                 A    =         6788931
23  meter
 Y    =       -6733250
47  meter          E    =           
0012839
 Z    =        -817059
48                 I    =           51
28032
 XDOT =       4831
921353                 Wp   =           35
02362
 YDOT =       -715
116026  meter/sec      RA   =          275
52992  deg
 ZDOT =       5912
974908                 TA   =          316
09453
                                          MA   =          316
19649
                                          Ha   =            221
433  n
mi
                                          Hp   =            214
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -20420
79                 X    =           73038
12
 Y    =      -22090716
78  feet           Y    =        -6732876
94  meter
 Z    =       -2680641
33                 Z    =         -816896
82
 XDOT =      15852
760345                 XDOT =        4810
836526
 YDOT =      -2346
181188  feet/sec       YDOT =        -661
199711  meter/sec
 ZDOT =      19399
523977                 ZDOT =        5936
395710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12216301
74                 X    =        -3723528
77
 Y    =      -18405732
91  feet           Y    =        -5610067
39  meter
 Z    =       -2678990
58                 Z    =         -816556
33
 XDOT =      10463
636662                 XDOT =        3189
316455
 YDOT =      -9756
746148  feet/sec       YDOT =       -2973
856226  meter/sec
 ZDOT =      19504
058349                 ZDOT =        5944
836985


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   18116
50158000  
00016717  00000-0  10270-3 0  9014
2 25544  51
6378 276
3725 0002747  18
2496 341
8754 15
54167622 30479


Satellite: ISS
Catalog Number: 25544
Epoch time:      18116
50158000   =   yrday
fracday
Element set:     901
Inclination:       51
6378  deg
RA of node:       276
3725  deg
Eccentricity:     
0002747     
Arg of perigee:    18
2496  deg
Mean anomaly:     341
8754  deg
Mean motion:   15
54167622  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3047
Checksum:              307


Coasting Arc #3 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2018/117/05:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2669659
91                 A    =         6785141
20  meter
 Y    =       -5406972
16  meter          E    =           
0014525
 Z    =        3093380
09                 I    =           51
26850
 XDOT =       3733
210901                 Wp   =           72
88843
 YDOT =       4627
142968  meter/sec      RA   =          271
98202  deg
 ZDOT =       4851
308445                 TA   =          322
92214
                                          MA   =          323
02240
                                          Ha   =            221
518  n
mi
                                          Hp   =            214
175

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8758726
72                 X    =         2714897
56
 Y    =      -17739409
96  feet           Y    =        -5376865
06  meter
 Z    =       10148884
80                 Z    =         3106458
69
 XDOT =      12248
067262                 XDOT =        3657
626121
 YDOT =      15180
915250  feet/sec       YDOT =        4668
467963  meter/sec
 ZDOT =      15916
366290                 ZDOT =        4869
259426

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19697027
79                 X    =         6003654
07
 Y    =        1492279
68  feet           Y    =          454846
85  meter
 Z    =       10207939
06                 Z    =         3111379
83
 XDOT =      -9486
762436                 XDOT =       -2891
565191
 YDOT =      15471
236922  feet/sec       YDOT =        4715
633014  meter/sec
 ZDOT =      15995
782556                 ZDOT =        4875
514523


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   18117
27318686  
00016717  00000-0  10270-3 0  9028
2 25544  51
6406 272
5302 0003267  17
3894 342
7370 15
54156579 30596


Satellite: ISS
Catalog Number: 25544
Epoch time:      18117
27318686   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       272
5302  deg
Eccentricity:     
0003267     
Arg of perigee:    17
3894  deg
Mean anomaly:     342
7370  deg
Mean motion:   15
54156579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              318


Coasting Arc #4 (Orbit 3073)
---------------------------------------

Vector Time (GMT): 2018/118/05:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3254296
84                 A    =         6781200
25  meter
 Y    =        4102681
30  meter          E    =           
0010958
 Z    =       -4320073
77                 I    =           51
25545
 XDOT =      -3097
619251                 Wp   =           56
20215
 YDOT =      -6093
337201  meter/sec      RA   =          266
97087  deg
 ZDOT =      -3453
636633                 TA   =          178
47594
                                          MA   =          178
47259
                                          Ha   =            221
553  n
mi
                                          Hp   =            214
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10676826
90                 X    =        -3278947
33
 Y    =       13460240
49  feet           Y    =         4066151
46  meter
 Z    =      -14173470
36                 Z    =        -4335942
32
 XDOT =     -10162
792818                 XDOT =       -3012
475482
 YDOT =     -19991
263782  feet/sec       YDOT =       -6127
501022  meter/sec
 ZDOT =     -11330
828848                 ZDOT =       -3468
476892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16505082
37                 X    =        -5030749
11
 Y    =       -4552849
22  feet           Y    =        -1387708
44  meter
 Z    =      -14244781
11                 Z    =        -4341809
28
 XDOT =      14201
772223                 XDOT =        4328
700174
 YDOT =     -15832
190045  feet/sec       YDOT =       -4825
651526  meter/sec
 ZDOT =     -11396
185968                 ZDOT =       -3473
557483


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   18118
23769211  
00016717  00000-0  10270-3 0  9030
2 25544  51
6405 267
7225 0003228  18
0257 342
1010 15
54181217 30742


Satellite: ISS
Catalog Number: 25544
Epoch time:      18118
23769211   =   yrday
fracday
Element set:     903
Inclination:       51
6405  deg
RA of node:       267
7225  deg
Eccentricity:     
0003228     
Arg of perigee:    18
0257  deg
Mean anomaly:     342
1010  deg
Mean motion:   15
54181217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3074
Checksum:              276


Coasting Arc #5 (Orbit 3089)
---------------------------------------

Vector Time (GMT): 2018/119/05:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3753662
28                 A    =         6778178
46  meter
 Y    =       -2482455
38  meter          E    =           
0005493
 Z    =        5063880
59                 I    =           51
24890
 XDOT =       2385
572269                 Wp   =           90
46415
 YDOT =       7089
980557  meter/sec      RA   =          261
94872  deg
 ZDOT =       1705
720844                 TA   =          342
96391
                                          MA   =          342
98234
                                          Ha   =            221
468  n
mi
                                          Hp   =            214
072

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12315164
96                 X    =         3756544
70
 Y    =       -8144538
64  feet           Y    =        -2440463
04  meter
 Z    =       16613781
46                 Z    =         5082121
99
 XDOT =       7826
680672                 XDOT =        2297
827232
 YDOT =      23261
091065  feet/sec       YDOT =        7116
167119  meter/sec
 ZDOT =       5596
196994                 ZDOT =        1717
095944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12368093
57                 X    =         3769794
92
 Y    =        7893454
51  feet           Y    =         2405924
93  meter
 Z    =       16695453
55                 Z    =         5088774
24
 XDOT =     -17580
953436                 XDOT =       -5358
674607
 YDOT =      15594
018706  feet/sec       YDOT =        4753
056902  meter/sec
 ZDOT =       5645
980335                 ZDOT =        1720
894806


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   18119
26649575  
00016717  00000-0  10270-3 0  9045
2 25544  51
6413 262
5931 0003187  22
5307 337
5985 15
54178592 30907


Satellite: ISS
Catalog Number: 25544
Epoch time:      18119
26649575   =   yrday
fracday
Element set:     904
Inclination:       51
6413  deg
RA of node:       262
5931  deg
Eccentricity:     
0003187     
Arg of perigee:    22
5307  deg
Mean anomaly:     337
5985  deg
Mean motion:   15
54178592  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3090
Checksum:              326


Coasting Arc #6 (Orbit 3104)
---------------------------------------

Vector Time (GMT): 2018/120/05:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4194371
33                 A    =         6777162
33  meter
 Y    =         706945
72  meter          E    =           
0016390
 Z    =       -5290105
80                 I    =           51
25142
 XDOT =      -1550
711614                 Wp   =           81
01999
 YDOT =      -7494
553374  meter/sec      RA   =          256
92115  deg
 ZDOT =        231
103389                 TA   =          191
17972
                                          MA   =          191
21618
                                          Ha   =            221
619  n
mi
                                          Hp   =            213
812

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13761060
79                 X    =        -4176267
81
 Y    =        2319375
71  feet           Y    =          660142
50  meter
 Z    =      -17355990
15                 Z    =        -5310437
03
 XDOT =      -5087
636530                 XDOT =       -1467
912821
 YDOT =     -24588
429706  feet/sec       YDOT =       -7511
431539  meter/sec
 ZDOT =        758
213219                 ZDOT =         223
771658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7813730
83                 X    =        -2381625
16
 Y    =      -11425116
18  feet           Y    =        -3482375
41  meter
 Z    =      -17446748
20                 Z    =        -5317768
85
 XDOT =      19370
331970                 XDOT =        5904
077184
 YDOT =     -14341
351190  feet/sec       YDOT =       -4371
243843  meter/sec
 ZDOT =        726
503047                 ZDOT =         221
438129


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   18120
23099470  
00016717  00000-0  10270-3 0  9058
2 25544  51
6414 257
7845 0003313  23
8991 336
2315 15
54201245 31054


Satellite: ISS
Catalog Number: 25544
Epoch time:      18120
23099470   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:       257
7845  deg
Eccentricity:     
0003313     
Arg of perigee:    23
8991  deg
Mean anomaly:     336
2315  deg
Mean motion:   15
54201245  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3105
Checksum:              286


Coasting Arc #7 (Orbit 3120)
---------------------------------------

Vector Time (GMT): 2018/121/05:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4518071
11                 A    =         6778594
67  meter
 Y    =        1093320
76  meter          E    =           
0009259
 Z    =        4929924
87                 I    =           51
26452
 XDOT =        582
691227                 Wp   =           46
77191
 YDOT =       7339
962671  meter/sec      RA   =          251
89532  deg
 ZDOT =      -2153
015071                 TA   =           64
36350
                                          MA   =           64
26788
                                          Ha   =            221
482  n
mi
                                          Hp   =            213
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14823067
95                 X    =         4481562
06
 Y    =        3587010
38  feet           Y    =         1143640
78  meter
 Z    =       16174294
19                 Z    =         4951783
85
 XDOT =       1911
716625                 XDOT =         511
028873
 YDOT =      24081
242360  feet/sec       YDOT =        7346
078050  meter/sec
 ZDOT =      -7063
697740                 ZDOT =       -2150
358518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3151831
84                 X    =          960678
35
 Y    =       14815452
03  feet           Y    =         4515749
78  meter
 Z    =       16271635
34                 Z    =         4959594
45
 XDOT =     -19766
042145                 XDOT =       -6024
689646
 YDOT =      11982
542380  feet/sec       YDOT =        3652
278917  meter/sec
 ZDOT =      -7052
806431                 ZDOT =       -2149
695400


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   18121
25979021  
00016717  00000-0  10270-3 0  9061
2 25544  51
6409 252
6558 0003300  26
1366 333
9953 15
54227269 31215


Satellite: ISS
Catalog Number: 25544
Epoch time:      18121
25979021   =   yrday
fracday
Element set:     906
Inclination:       51
6409  deg
RA of node:       252
6558  deg
Eccentricity:     
0003300     
Arg of perigee:    26
1366  deg
Mean anomaly:     333
9953  deg
Mean motion:   15
54227269  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3121
Checksum:              300


Coasting Arc #8 (Orbit 3122)
---------------------------------------

Vector Time (GMT): 2018/121/08:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4479489
94                 A    =         6782070
46  meter
 Y    =        3069384
41  meter          E    =           
0012805
 Z    =        4056649
95                 I    =           51
27364
 XDOT =      -1014
415036                 Wp   =           66
64784
 YDOT =       6566
293234  meter/sec      RA   =          251
22248  deg
 ZDOT =      -3833
457477                 TA   =           63
25323
                                          MA   =           63
12225
                                          Ha   =            221
544  n
mi
                                          Hp   =            213
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14696489
30                 X    =         4425128
87
 Y    =       10070158
84  feet           Y    =         3119173
17  meter
 Z    =       13309218
98                 Z    =         4078278
17
 XDOT =      -3328
133320                 XDOT =       -1069
144444
 YDOT =      21542
956806  feet/sec       YDOT =        6554
643370  meter/sec
 ZDOT =     -12576
960226                 ZDOT =       -3838
518122

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11108521
26                 X    =         3385877
28
 Y    =       13835807
33  feet           Y    =         4217154
07  meter
 Z    =       13405274
99                 Z    =         4085927
82
 XDOT =      -8274
458168                 XDOT =       -2522
054850
 YDOT =      18897
936011  feet/sec       YDOT =        5760
090896  meter/sec
 ZDOT =     -12600
383351                 ZDOT =       -3840
596845


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   18121
38839001  
00016717  00000-0  10270-3 0  9079
2 25544  51
6374 252
0110 0003089  27
5379 332
5937 15
54188640 31235


Satellite: ISS
Catalog Number: 25544
Epoch time:      18121
38839001   =   yrday
fracday
Element set:     907
Inclination:       51
6374  deg
RA of node:       252
0110  deg
Eccentricity:     
0003089     
Arg of perigee:    27
5379  deg
Mean anomaly:     332
5937  deg
Mean motion:   15
54188640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3123
Checksum:              298


Coasting Arc #9 (Orbit 3137)
---------------------------------------

Vector Time (GMT): 2018/122/08:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4361211
93                 A    =         6785835
70  meter
 Y    =       -4401060
25  meter          E    =           
0007621
 Z    =       -2765457
56                 I    =           51
29755
 XDOT =       2129
175156                 Wp   =           50
11094
 YDOT =      -5307
872493  meter/sec      RA   =          246
21423  deg
 ZDOT =       5103
562725                 TA   =          278
40459
                                          MA   =          278
49097
                                          Ha   =            221
657  n
mi
                                          Hp   =            213
819

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14308438
09                 X    =        -4298240
56
 Y    =      -14439174
05  feet           Y    =        -4449478
15  meter
 Z    =       -9073023
49                 Z    =        -2786490
38
 XDOT =       6985
482795                 XDOT =        2163
580119
 YDOT =     -17414
279834  feet/sec       YDOT =       -5283
870369  meter/sec
 ZDOT =      16743
972195                 ZDOT =        5113
989121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9818187
18                 X    =        -2992583
45
 Y    =      -17751724
35  feet           Y    =        -5410725
58  meter
 Z    =       -9166263
46                 Z    =        -2793877
10
 XDOT =      10028
045885                 XDOT =        3056
548386
 YDOT =     -14192
842699  feet/sec       YDOT =       -4325
978455  meter/sec
 ZDOT =      16791
158578                 ZDOT =        5117
945135


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   18122
35288469  
00016717  00000-0  10270-3 0  9084
2 25544  51
6371 247
2021 0003071  34
6123 325
5229 15
54190290 31382


Satellite: ISS
Catalog Number: 25544
Epoch time:      18122
35288469   =   yrday
fracday
Element set:     908
Inclination:       51
6371  deg
RA of node:       247
2021  deg
Eccentricity:     
0003071     
Arg of perigee:    34
6123  deg
Mean anomaly:     325
5229  deg
Mean motion:   15
54190290  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3138
Checksum:              290


Coasting Arc #10 (Orbit 3141)
---------------------------------------

Vector Time (GMT): 2018/122/14:29:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4603525
99                 A    =         6784811
71  meter
 Y    =       -3847233
27  meter          E    =           
0006911
 Z    =       -3170219
72                 I    =           51
30128
 XDOT =       1536
241692                 Wp   =           62
56226
 YDOT =      -5779
050026  meter/sec      RA   =          244
93049  deg
 ZDOT =       4793
577804                 TA   =          260
66564
                                          MA   =          260
74379
                                          Ha   =            221
605  n
mi
                                          Hp   =            213
853

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15103431
73                 X    =        -4544763
50
 Y    =      -12622156
38  feet           Y    =        -3898384
40  meter
 Z    =      -10400983
32                 Z    =        -3192439
85
 XDOT =       5040
163032                 XDOT =        1577
465342
 YDOT =     -18960
137879  feet/sec       YDOT =       -5761
640377  meter/sec
 ZDOT =      15726
961299                 ZDOT =        4801
140401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15716059
48                 X    =        -4790254
93
 Y    =       11763372
99  feet           Y    =         3585476
09  meter
 Z    =      -10499593
62                 Z    =        -3200276
13
 XDOT =     -16478
079122                 XDOT =       -5022
518516
 YDOT =      -7979
310654  feet/sec       YDOT =       -2432
093887  meter/sec
 ZDOT =      15761
434703                 ZDOT =        4804
085298


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   18122
61008187  
00016717  00000-0  10270-3 0  9091
2 25544  51
6409 245
9215 0002894  34
3493 325
7846 15
54187851 31424


Satellite: ISS
Catalog Number: 25544
Epoch time:      18122
61008187   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:       245
9215  deg
Eccentricity:     
0002894     
Arg of perigee:    34
3493  deg
Mean anomaly:     325
7846  deg
Mean motion:   15
54187851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3142
Checksum:              319


Coasting Arc #11 (Orbit 3157)
---------------------------------------

Vector Time (GMT): 2018/123/14:29:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4351544
54                 A    =         6787984
61  meter
 Y    =        4947802
28  meter          E    =           
0014942
 Z    =        1607883
62                 I    =           51
32659
 XDOT =      -2778
649092                 Wp   =          105
15018
 YDOT =       4310
129244  meter/sec      RA   =          239
93160  deg
 ZDOT =      -5702
524457                 TA   =           57
17296
                                          MA   =           57
02918
                                          Ha   =            221
732  n
mi
                                          Hp   =            213
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14276720
94                 X    =         4288083
08
 Y    =       16232947
13  feet           Y    =         4996109
34  meter
 Z    =        5275208
73                 Z    =         1628868
33
 XDOT =      -9116
302796                 XDOT =       -2798
939340
 YDOT =      14140
843975  feet/sec       YDOT =        4278
943286  meter/sec
 ZDOT =     -18709
069742                 ZDOT =       -5716
071465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18873162
36                 X    =         5752539
89
 Y    =      -10495118
65  feet           Y    =        -3198912
16  meter
 Z    =        5368182
88                 Z    =         1636222
14
 XDOT =      11157
965650                 XDOT =        3400
947930
 YDOT =      10397
466564  feet/sec       YDOT =        3169
147809  meter/sec
 ZDOT =     -18770
045844                 ZDOT =       -5721
109973


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   18123
63886932  
00016717  00000-0  10270-3 0  9108
2 25544  51
6406 240
7928 0003079  39
9178 320
2201 15
54201537 31582


Satellite: ISS
Catalog Number: 25544
Epoch time:      18123
63886932   =   yrday
fracday
Element set:     910
Inclination:       51
6406  deg
RA of node:       240
7928  deg
Eccentricity:     
0003079     
Arg of perigee:    39
9178  deg
Mean anomaly:     320
2201  deg
Mean motion:   15
54201537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3158
Checksum:              304


Coasting Arc #12 (Orbit 3173)
---------------------------------------

Vector Time (GMT): 2018/124/14:29:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3837428
93                 A    =         6789202
86  meter
 Y    =       -5590881
52  meter          E    =           
0015431
 Z    =          88122
59                 I    =           51
34710
 XDOT =       3999
261671                 Wp   =           45
35059
 YDOT =      -2640
544548  meter/sec      RA   =          234
93983  deg
 ZDOT =       5989
502413                 TA   =          315
60280
                                          MA   =          315
72641
                                          Ha   =            221
821  n
mi
                                          Hp   =            213
778

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12589989
92                 X    =        -3775053
02
 Y    =      -18342787
16  feet           Y    =        -5633445
54  meter
 Z    =         289116
10                 Z    =           69632
68
 XDOT =      13120
937241                 XDOT =        3999
397522
 YDOT =      -8663
203897  feet/sec       YDOT =       -2595
821592  meter/sec
 ZDOT =      19650
598469                 ZDOT =        6008
929880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20438701
55                 X    =        -6229716
23
 Y    =        8790094
76  feet           Y    =         2679220
88  meter
 Z    =         207335
07                 Z    =           63195
73
 XDOT =      -5333
200521                 XDOT =       -1625
559519
 YDOT =     -12934
996831  feet/sec       YDOT =       -3942
587034  meter/sec
 ZDOT =      19737
597872                 ZDOT =        6016
019831


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   18124
66765384  
00016717  00000-0  10270-3 0  9110
2 25544  51
6400 235
6641 0003209  41
2520 318
8875 15
54172627 31748


Satellite: ISS
Catalog Number: 25544
Epoch time:      18124
66765384   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:       235
6641  deg
Eccentricity:     
0003209     
Arg of perigee:    41
2520  deg
Mean anomaly:     318
8875  deg
Mean motion:   15
54172627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3174
Checksum:              302


Coasting Arc #13 (Orbit 3188)
---------------------------------------

Vector Time (GMT): 2018/125/14:29:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2988231
57                 A    =         6787706
84  meter
 Y    =        5815643
95  meter          E    =           
0007738
 Z    =       -1819820
28                 I    =           51
36138
 XDOT =      -5130
829935                 Wp   =          118
07631
 YDOT =        883
312841  meter/sec      RA   =          229
94925  deg
 ZDOT =      -5624
141093                 TA   =           82
00040
                                          MA   =           81
91261
                                          Ha   =            221
821  n
mi
                                          Hp   =            213
672

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9803909
33                 X    =         2931817
17
 Y    =       19080196
68  feet           Y    =         5848745
07  meter
 Z    =       -5970538
99                 Z    =        -1805441
08
 XDOT =     -16833
431546                 XDOT =       -5113
006667
 YDOT =       2898
008010  feet/sec       YDOT =         826
036302  meter/sec
 ZDOT =     -18451
906473                 ZDOT =       -5649
021799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20522512
31                 X    =         6255261
75
 Y    =       -6304795
32  feet           Y    =        -1921701
61  meter
 Z    =       -5907107
91                 Z    =        -1800486
49
 XDOT =       -571
644048                 XDOT =        -174
237106
 YDOT =      15463
349975  feet/sec       YDOT =        4713
229072  meter/sec
 ZDOT =     -18563
023298                 ZDOT =       -5658
009501


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   18125
63213381  
00016717  00000-0  10270-3 0  9124
2 25544  51
6392 230
8559 0003122  46
5131 313
6281 15
54212104 31898


Satellite: ISS
Catalog Number: 25544
Epoch time:      18125
63213381   =   yrday
fracday
Element set:     912
Inclination:       51
6392  deg
RA of node:       230
8559  deg
Eccentricity:     
0003122     
Arg of perigee:    46
5131  deg
Mean anomaly:     313
6281  deg
Mean motion:   15
54212104  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3189
Checksum:              276


Coasting Arc #14 (Orbit 3204)
---------------------------------------

Vector Time (GMT): 2018/126/14:29:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1864109
58                 A    =         6784403
09  meter
 Y    =       -5607226
53  meter          E    =           
0015242
 Z    =        3317840
52                 I    =           51
37282
 XDOT =       6042
895095                 Wp   =           80
89423
 YDOT =        762
454423  meter/sec      RA   =          224
95236  deg
 ZDOT =       4667
737125                 TA   =          317
91288
                                          MA   =          318
02984
                                          Ha   =            221
847  n
mi
                                          Hp   =            213
594

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6115845
08                 X    =        -1817385
94
 Y    =      -18396412
51  feet           Y    =        -5627811
19  meter
 Z    =       10885303
55                 Z    =         3308898
49
 XDOT =      19825
771309                 XDOT =        6011
246420
 YDOT =       2501
490889  feet/sec       YDOT =         829
853072  meter/sec
 ZDOT =      15314
098178                 ZDOT =        4697
014807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19149632
30                 X    =        -5836807
93
 Y    =        3158366
93  feet           Y    =          962670
24  meter
 Z    =       10846090
94                 Z    =         3305888
52
 XDOT =       5862
923542                 XDOT =        1787
019095
 YDOT =     -17671
279598  feet/sec       YDOT =       -5386
206022  meter/sec
 ZDOT =      15444
644445                 ZDOT =        4707
527627


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   18126
66090785  
00016717  00000-0  10270-3 0  9130
2 25544  51
6396 225
7264 0003206  49
1242 311
0188 15
54227947 32051


Satellite: ISS
Catalog Number: 25544
Epoch time:      18126
66090785   =   yrday
fracday
Element set:     913
Inclination:       51
6396  deg
RA of node:       225
7264  deg
Eccentricity:     
0003206     
Arg of perigee:    49
1242  deg
Mean anomaly:     311
0188  deg
Mean motion:   15
54227947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3205
Checksum:              305


Coasting Arc #15 (Orbit 3219)
---------------------------------------

Vector Time (GMT): 2018/127/14:29:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         463018
79                 A    =         6780553
07  meter
 Y    =        5068818
66  meter          E    =           
0012709
 Z    =       -4492711
11                 I    =           51
38321
 XDOT =      -6603
460614                 Wp   =           65
64893
 YDOT =      -2215
314672  meter/sec      RA   =          219
94729  deg
 ZDOT =      -3181
930794                 TA   =          172
23260
                                          MA   =          172
21290
                                          Ha   =            221
931  n
mi
                                          Hp   =            213
514

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1519090
53                 X    =          428126
83
 Y    =       16629982
49  feet           Y    =         5073801
52  meter
 Z    =      -14739865
86                 Z    =        -4490546
48
 XDOT =     -21664
897026                 XDOT =       -6562
741335
 YDOT =      -7268
092757  feet/sec       YDOT =       -2288
931328  meter/sec
 ZDOT =     -10439
405491                 ZDOT =       -3213
909503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16688821
48                 X    =         5086752
79
 Y    =         783459
98  feet           Y    =          238798
60  meter
 Z    =      -14730818
96                 Z    =        -4489953
62
 XDOT =     -10231
868091                 XDOT =       -3118
673394
 YDOT =      19113
677667  feet/sec       YDOT =        5825
848953  meter/sec
 ZDOT =     -10581
846142                 ZDOT =       -3225
346704


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   18127
62538204  
00016717  00000-0  10270-3 0  9141
2 25544  51
6389 220
9183 0003318  53
1615 306
9841 15
54214162 32204


Satellite: ISS
Catalog Number: 25544
Epoch time:      18127
62538204   =   yrday
fracday
Element set:     914
Inclination:       51
6389  deg
RA of node:       220
9183  deg
Eccentricity:     
0003318     
Arg of perigee:    53
1615  deg
Mean anomaly:     306
9841  deg
Mean motion:   15
54214162  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3220
Checksum:              289


Coasting Arc #16 (Orbit 3226)
---------------------------------------

Vector Time (GMT): 2018/128/00:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3232436
56                 A    =         6785939
63  meter
 Y    =       -5287850
13  meter          E    =           
0016729
 Z    =        2743100
95                 I    =           51
41249
 XDOT =       5654
402557                 Wp   =           73
28183
 YDOT =       -785
314072  meter/sec      RA   =          217
88133  deg
 ZDOT =       5127
998518                 TA   =          317
90247
                                          MA   =          318
03087
                                          Ha   =            222
017  n
mi
                                          Hp   =            213
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10605106
82                 X    =        -3186390
75
 Y    =      -17348589
65  feet           Y    =        -5323740
08  meter
 Z    =        8999675
03                 Z    =         2727510
47
 XDOT =      18551
189491                 XDOT =        5637
854637
 YDOT =      -2576
489737  feet/sec       YDOT =        -722
175331  meter/sec
 ZDOT =      16824
142119                 ZDOT =        5155
425603

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20189321
78                 X    =         6153705
28
 Y    =        2658814
05  feet           Y    =          810406
52  meter
 Z    =        8930733
34                 Z    =         2722087
52
 XDOT =      -9432
304957                 XDOT =       -2874
966551
 YDOT =      14464
666259  feet/sec       YDOT =        4408
830276  meter/sec
 ZDOT =      16946
638659                 ZDOT =        5165
335463


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   18128
07546970  
00016717  00000-0  10270-3 0  9151
2 25544  51
6397 218
6757 0003576  50
6257 309
5212 15
54214277 32279


Satellite: ISS
Catalog Number: 25544
Epoch time:      18128
07546970   =   yrday
fracday
Element set:     915
Inclination:       51
6397  deg
RA of node:       218
6757  deg
Eccentricity:     
0003576     
Arg of perigee:    50
6257  deg
Mean anomaly:     309
5212  deg
Mean motion:   15
54214277  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3227
Checksum:              324


Coasting Arc #17 (Orbit 3241)
---------------------------------------

Vector Time (GMT): 2018/129/00:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1872545
05                 A    =         6781983
16  meter
 Y    =        5089324
45  meter          E    =           
0010530
 Z    =       -4084252
17                 I    =           51
42717
 XDOT =      -6604
240050                 Wp   =           65
61941
 YDOT =       -637
023163  meter/sec      RA   =          212
88326  deg
 ZDOT =      -3825
235242                 TA   =          164
68987
                                          MA   =          164
65799
                                          Ha   =            221
911  n
mi
                                          Hp   =            213
492

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6143520
51                 X    =         1835334
94
 Y    =       16697258
68  feet           Y    =         5110056
56  meter
 Z    =      -13399777
47                 Z    =        -4075246
22
 XDOT =     -21667
454233                 XDOT =       -6578
044743
 YDOT =      -2089
971006  feet/sec       YDOT =        -710
729784  meter/sec
 ZDOT =     -12549
984390                 ZDOT =       -3857
252952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16984439
39                 X    =        -5176857
13
 Y    =       -5397184
76  feet           Y    =        -1645061
92  meter
 Z    =      -13360184
99                 Z    =        -4072184
39
 XDOT =      14569
255112                 XDOT =        4440
708958
 YDOT =     -14457
176220  feet/sec       YDOT =       -4406
547312  meter/sec
 ZDOT =     -12692
813862                 ZDOT =       -3868
769665


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   18129
03993749  
00016717  00000-0  10270-3 0  9169
2 25544  51
6407 213
8677 0003408  51
9279 308
2181 15
54241227 32424


Satellite: ISS
Catalog Number: 25544
Epoch time:      18129
03993749   =   yrday
fracday
Element set:     916
Inclination:       51
6407  deg
RA of node:       213
8677  deg
Eccentricity:     
0003408     
Arg of perigee:    51
9279  deg
Mean anomaly:     308
2181  deg
Mean motion:   15
54241227  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3242
Checksum:              317


Coasting Arc #18 (Orbit 3257)
---------------------------------------

Vector Time (GMT): 2018/130/00:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -280799
61                 A    =         6778590
26  meter
 Y    =       -4613356
76  meter          E    =           
0008405
 Z    =        4951910
48                 I    =           51
44454
 XDOT =       7135
534961                 Wp   =          100
55082
 YDOT =       1855
157603  meter/sec      RA   =          207
87552  deg
 ZDOT =       2128
359519                 TA   =          328
65094
                                          MA   =          328
70102
                                          Ha   =            221
979  n
mi
                                          Hp   =            213
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -921258
55                 X    =         -253244
89
 Y    =      -15135684
92  feet           Y    =        -4616342
83  meter
 Z    =       16246425
45                 Z    =         4950613
33
 XDOT =      23410
547772                 XDOT =        7103
921220
 YDOT =       6086
475077  feet/sec       YDOT =        1934
775289  meter/sec
 ZDOT =       6982
806821                 ZDOT =        2162
944990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12689757
99                 X    =         3867838
24
 Y    =        8311332
52  feet           Y    =         2533294
15  meter
 Z    =       16241176
35                 Z    =         4950310
55
 XDOT =     -18345
174201                 XDOT =       -5591
609097
 YDOT =      14033
673133  feet/sec       YDOT =        4277
463571  meter/sec
 ZDOT =       7136
971406                 ZDOT =        2175
348885


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   18130
06870056  
00016717  00000-0  10270-3 0  9170
2 25544  51
6412 208
7380 0003512  56
8107 303
3382 15
54239049 32589


Satellite: ISS
Catalog Number: 25544
Epoch time:      18130
06870056   =   yrday
fracday
Element set:     917
Inclination:       51
6412  deg
RA of node:       208
7380  deg
Eccentricity:     
0003512     
Arg of perigee:    56
8107  deg
Mean anomaly:     303
3382  deg
Mean motion:   15
54239049  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3258
Checksum:              293
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