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

 
Date: November 13th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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


319/09:49:38 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 5

320/05:28:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 5

320/18:14:08 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 3

322/09:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 213 1

322/19:30:01 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 2

325/21:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 9
000/00:00:00 000 0 0 0 0 213 1

Coasting Arc #1 (Orbit 2156)
---------------------------------------

Vector Time (GMT): 2018/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6261652
13                 A    =         6788193
18  meter
 Y    =       -1683840
07  meter          E    =           
0011825
 Z    =       -1995691
52                 I    =           51
65232
 XDOT =       2941
989032                 Wp   =           38
81451
 YDOT =       4362
938606  meter/sec      RA   =          359
04097  deg
 ZDOT =       5576
467184                 TA   =          299
15593
                                          MA   =          299
27421
                                          Ha   =            222
781  n
mi
                                          Hp   =            213
709

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20543478
13                 X    =         6289710
10
 Y    =       -5524409
67  feet           Y    =        -1613660
94  meter
 Z    =       -6547544
35                 Z    =        -1965206
00
 XDOT =       9652
194988                 XDOT =        2865
894780
 YDOT =      14314
103039  feet/sec       YDOT =        4395
412204  meter/sec
 ZDOT =      18295
496012                 ZDOT =        5590
574002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8767666
41                 X    =        -2672384
72
 Y    =       19428361
93  feet           Y    =         5921764
72  meter
 Z    =       -6410203
68                 Z    =        -1953830
08
 XDOT =     -15697
027908                 XDOT =       -4784
454106
 YDOT =      -1056
381499  feet/sec       YDOT =        -321
985081  meter/sec
 ZDOT =      18358
297501                 ZDOT =        5595
609078


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   18316
50385145  
00016717  00000-0  10270-3 0  9007
2 25544  51
6409 359
6196 0004941  38
8013 321
3494 15
53960916 21573


Satellite: ISS
Catalog Number: 25544
Epoch time:      18316
50385145   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       359
6196  deg
Eccentricity:     
0004941     
Arg of perigee:    38
8013  deg
Mean anomaly:     321
3494  deg
Mean motion:   15
53960916  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2157
Checksum:              314


Coasting Arc #2 (Orbit 2172)
---------------------------------------

Vector Time (GMT): 2018/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6706136
32                 A    =         6789729
91  meter
 Y    =         976708
17  meter          E    =           
0013692
 Z    =         351939
50                 I    =           51
62465
 XDOT =      -1004
533178                 Wp   =          109
64653
 YDOT =      -4669
641272  meter/sec      RA   =          354
07042  deg
 ZDOT =      -5996
326951                 TA   =           66
56033
                                          MA   =           66
41644
                                          Ha   =            222
762  n
mi
                                          Hp   =            213
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22001759
59                 X    =        -6718269
29
 Y    =        3204423
12  feet           Y    =          901647
64  meter
 Z    =        1154657
16                 Z    =          319333
52
 XDOT =      -3295
712525                 XDOT =        -923
113870
 YDOT =     -15320
345380  feet/sec       YDOT =       -4680
419129  meter/sec
 ZDOT =     -19672
988686                 ZDOT =       -6001
009164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11134552
59                 X    =         3393811
63
 Y    =      -19253178
49  feet           Y    =        -5868368
80  meter
 Z    =        1007890
12                 Z    =          307204
91
 XDOT =      12578
444449                 XDOT =        3833
909868
 YDOT =       6206
952129  feet/sec       YDOT =        1891
879009  meter/sec
 ZDOT =     -19693
362702                 ZDOT =       -6002
536952


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   18317
53279802  
00016717  00000-0  10270-3 0  9014
2 25544  51
6410 354
4915 0004999  42
6889 317
4652 15
53976336 21737


Satellite: ISS
Catalog Number: 25544
Epoch time:      18317
53279802   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:       354
4915  deg
Eccentricity:     
0004999     
Arg of perigee:    42
6889  deg
Mean anomaly:     317
4652  deg
Mean motion:   15
53976336  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2173
Checksum:              335


Coasting Arc #3 (Orbit 2188)
---------------------------------------

Vector Time (GMT): 2018/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6653314
33                 A    =         6789159
67  meter
 Y    =        -249461
47  meter          E    =           
0018915
 Z    =        1277971
70                 I    =           51
58926
 XDOT =       -946
943576                 Wp   =           55
41713
 YDOT =       4893
262217  meter/sec      RA   =          349
09872  deg
 ZDOT =       5834
157853                 TA   =          318
50300
                                          MA   =          318
64647
                                          Ha   =            222
925  n
mi
                                          Hp   =            213
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21828459
09                 X    =         6649401
60
 Y    =        -818443
15  feet           Y    =         -175081
42  meter
 Z    =        4192820
54                 Z    =         1310282
10
 XDOT =      -3106
770262                 XDOT =       -1029
930648
 YDOT =      16054
009897  feet/sec       YDOT =        4882
208600  meter/sec
 ZDOT =      19140
937837                 ZDOT =        5829
356496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12572297
57                 X    =        -3832036
30
 Y    =       17828321
52  feet           Y    =         5434072
40  meter
 Z    =        4338145
37                 Z    =         1322266
71
 XDOT =      -9503
104551                 XDOT =       -2896
546267
 YDOT =     -11392
887906  feet/sec       YDOT =       -3472
552234  meter/sec
 ZDOT =      19118
636793                 ZDOT =        5827
360495


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   18318
56174252  
00016717  00000-0  10270-3 0  9022
2 25544  51
6407 349
3636 0005225  46
2312 313
9272 15
53934233 21896


Satellite: ISS
Catalog Number: 25544
Epoch time:      18318
56174252   =   yrday
fracday
Element set:     902
Inclination:       51
6407  deg
RA of node:       349
3636  deg
Eccentricity:     
0005225     
Arg of perigee:    46
2312  deg
Mean anomaly:     313
9272  deg
Mean motion:   15
53934233  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2189
Checksum:              302


Coasting Arc #4 (Orbit 2202)
---------------------------------------

Vector Time (GMT): 2018/319/09:49:38
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3753682
94                 A    =         6779783
95  meter
 Y    =        2933367
89  meter          E    =           
0009742
 Z    =        4815641
95                 I    =           51
52963
 XDOT =      -6186
794373                 Wp   =           91
52448
 YDOT =       3780
857045  meter/sec      RA   =          344
56749  deg
 ZDOT =       2514
764714                 TA   =          333
70856
                                          MA   =          333
75798
                                          Ha   =            222
660  n
mi
                                          Hp   =            213
486

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12315232
76                 X    =         3697210
09
 Y    =        9623910
39  feet           Y    =         2975028
28  meter
 Z    =       15799350
22                 Z    =         4833739
18
 XDOT =     -20297
881801                 XDOT =       -6240
828707
 YDOT =      12404
386631  feet/sec       YDOT =        3711
369817  meter/sec
 ZDOT =       8250
540401                 ZDOT =        2484
579905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14845244
47                 X    =        -4524830
51
 Y    =       -4619403
36  feet           Y    =        -1407994
14  meter
 Z    =       15880299
30                 Z    =         4840315
23
 XDOT =      14229
863199                 XDOT =        4337
262303
 YDOT =     -17783
141621  feet/sec       YDOT =       -5420
301566  meter/sec
 ZDOT =       8114
270089                 ZDOT =        2473
229523


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   18319
46206084  
00016717  00000-0  10270-3 0  9032
2 25544  51
6413 344
8760 0004828  48
4835 311
6731 15
53986178 22030


Satellite: ISS
Catalog Number: 25544
Epoch time:      18319
46206084   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:       344
8760  deg
Eccentricity:     
0004828     
Arg of perigee:    48
4835  deg
Mean anomaly:     311
6731  deg
Mean motion:   15
53986178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2203
Checksum:              316


Coasting Arc #5 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2018/320/05:28:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4516014
50                 A    =         6786175
23  meter
 Y    =       -4106524
58  meter          E    =           
0009335
 Z    =       -2966242
97                 I    =           51
52417
 XDOT =       5351
463439                 Wp   =           59
01769
 YDOT =       2299
258645  meter/sec      RA   =          340
43801  deg
 ZDOT =       4980
647800                 TA   =          267
04369
                                          MA   =          267
15052
                                          Ha   =            222
895  n
mi
                                          Hp   =            213
506

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14816320
54                 X    =         4576007
79
 Y    =      -13472849
69  feet           Y    =        -4055687
88  meter
 Z    =       -9731768
28                 Z    =        -2944159
82
 XDOT =      17557
294749                 XDOT =        5301
161085
 YDOT =       7543
499491  feet/sec       YDOT =        2358
821081  meter/sec
 ZDOT =      16340
708006                 ZDOT =        5006
521550

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20067555
57                 X    =        -6116590
94
 Y    =        -517974
43  feet           Y    =         -157878
61  meter
 Z    =       -9631887
81                 Z    =        -2935799
40
 XDOT =      -7458
814282                 XDOT =       -2273
446593
 YDOT =     -16037
693447  feet/sec       YDOT =       -4888
288963  meter/sec
 ZDOT =      16456
711298                 ZDOT =        5016
005604


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   18320
23376399  
00016717  00000-0  10270-3 0  9047
2 25544  51
6410 341
0279 0004828  53
0675 307
0920 15
53955283 22150


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
23376399   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:       341
0279  deg
Eccentricity:     
0004828     
Arg of perigee:    53
0675  deg
Mean anomaly:     307
0920  deg
Mean motion:   15
53955283  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              301


Coasting Arc #6 (Orbit 2223)
---------------------------------------

Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4135638
12                 A    =         6779843
05  meter
 Y    =        2426372
63  meter          E    =           
0010270
 Z    =        4784532
06                 I    =           51
48648
 XDOT =      -5642
098994                 Wp   =           92
00490
 YDOT =       4517
133296  meter/sec      RA   =          337
82925  deg
 ZDOT =       2580
986461                 TA   =          332
51300
                                          MA   =          332
56728
                                          Ha   =            222
717  n
mi
                                          Hp   =            213
338

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13568366
53                 X    =         4084957
33
 Y    =        7960540
13  feet           Y    =         2472336
79  meter
 Z    =       15697283
65                 Z    =         4804498
75
 XDOT =     -18510
823472                 XDOT =       -5704
728746
 YDOT =      14819
991128  feet/sec       YDOT =        4453
689212  meter/sec
 ZDOT =       8467
803351                 ZDOT =        2553
426662

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7300362
07                 X    =         2225150
36
 Y    =       13833295
11  feet           Y    =         4216388
35  meter
 Z    =       15786707
81                 Z    =         4811788
54
 XDOT =     -22569
863744                 XDOT =       -6879
294469
 YDOT =       2370
425028  feet/sec       YDOT =         722
505548  meter/sec
 ZDOT =       8343
246565                 ZDOT =        2543
021553


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   18320
81253819  
00016717  00000-0  10270-3 0  9053
2 25544  51
6403 338
1476 0005024  51
7031 308
4573 15
54005893 22241


Satellite: ISS
Catalog Number: 25544
Epoch time:      18320
81253819   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       338
1476  deg
Eccentricity:     
0005024     
Arg of perigee:    51
7031  deg
Mean anomaly:     308
4573  deg
Mean motion:   15
54005893  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2224
Checksum:              288


Coasting Arc #7 (Orbit 2238)
---------------------------------------

Vector Time (GMT): 2018/321/18:14:08
000
Vector Time (MET): N/A
Weight (LBS)     : 902349
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2695167
69                 A    =         6777926
96  meter
 Y    =       -3333816
68  meter          E    =           
0019248
 Z    =       -5266685
99                 I    =           51
45023
 XDOT =       6472
144369                 Wp   =           76
30853
 YDOT =      -4012
821286  meter/sec      RA   =          332
82105  deg
 ZDOT =       -769
843006                 TA   =          186
29020
                                          MA   =          186
31440
                                          Ha   =            222
926  n
mi
                                          Hp   =            213
157

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8842413
68                 X    =        -2632104
53
 Y    =      -10937718
77  feet           Y    =        -3363603
31  meter
 Z    =      -17279153
50                 Z    =        -5279625
21
 XDOT =      21234
069452                 XDOT =        6520
275382
 YDOT =     -13165
424168  feet/sec       YDOT =       -3940
176153  meter/sec
 ZDOT =      -2525
731646                 ZDOT =        -738
286180

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1944878
08                 X    =         -592798
84
 Y    =      -13857926
93  feet           Y    =        -4223896
13  meter
 Z    =      -17336851
72                 Z    =        -5284272
40
 XDOT =      23982
374224                 XDOT =        7309
827663
 YDOT =       -375
656998  feet/sec       YDOT =        -114
500253  meter/sec
 ZDOT =      -2383
290412                 ZDOT =        -726
426917


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   18321
77716187  
00016717  00000-0  10270-3 0  9062
2 25544  51
6410 333
3398 0005157  54
7475 305
4160 15
53994446 22396


Satellite: ISS
Catalog Number: 25544
Epoch time:      18321
77716187   =   yrday
fracday
Element set:     906
Inclination:       51
6410  deg
RA of node:       333
3398  deg
Eccentricity:     
0005157     
Arg of perigee:    54
7475  deg
Mean anomaly:     305
4160  deg
Mean motion:   15
53994446  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2239
Checksum:              322


Coasting Arc #8 (Orbit 2248)
---------------------------------------

Vector Time (GMT): 2018/322/09:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917504
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4597715
84                 A    =         6780253
07  meter
 Y    =       -1661593
96  meter          E    =           
0016008
 Z    =       -4713682
14                 I    =           51
43917
 XDOT =       4751
904446                 Wp   =           67
05682
 YDOT =      -5330
877696  meter/sec      RA   =          329
63916  deg
 ZDOT =      -2757
219916                 TA   =          175
52333
                                          MA   =          175
50900
                                          Ha   =            222
960  n
mi
                                          Hp   =            213
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15084369
55                 X    =        -4555896
74
 Y    =       -5451423
75  feet           Y    =        -1712775
00  meter
 Z    =      -15464836
42                 Z    =        -4735915
06
 XDOT =      15590
237685                 XDOT =        4824
555992
 YDOT =     -17489
756221  feet/sec       YDOT =       -5277
332387  meter/sec
 ZDOT =      -9045
997099                 ZDOT =       -2733
959930

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15942307
88                 X    =         4859215
44
 Y    =         -70474
19  feet           Y    =          -21480
53  meter
 Z    =      -15564550
88                 Z    =        -4744075
11
 XDOT =      -8633
086213                 XDOT =       -2631
364678
 YDOT =      20664
056885  feet/sec       YDOT =        6298
404539  meter/sec
 ZDOT =      -8940
677653                 ZDOT =       -2725
118549


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   18322
42024052  
00016717  00000-0  10270-3 0  9079
2 25544  51
6409 330
1335 0005063  59
7757 300
3896 15
53979389 22494


Satellite: ISS
Catalog Number: 25544
Epoch time:      18322
42024052   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       330
1335  deg
Eccentricity:     
0005063     
Arg of perigee:    59
7757  deg
Mean anomaly:     300
3896  deg
Mean motion:   15
53979389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2249
Checksum:              317


Coasting Arc #9 (Orbit 2255)
---------------------------------------

Vector Time (GMT): 2018/322/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5969318
43                 A    =         6785616
27  meter
 Y    =        -878678
23  meter          E    =           
0017739
 Z    =        3084983
14                 I    =           51
44646
 XDOT =      -1694
082044                 Wp   =           76
97534
 YDOT =       5679
338601  meter/sec      RA   =          327
57932  deg
 ZDOT =       4875
854143                 TA   =          318
62529
                                          MA   =          318
75951
                                          Ha   =            222
897  n
mi
                                          Hp   =            213
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19584378
05                 X    =         5963714
90
 Y    =       -2882802
60  feet           Y    =         -811956
49  meter
 Z    =       10121335
76                 Z    =         3113966
96
 XDOT =      -5558
011957                 XDOT =       -1781
148862
 YDOT =      18633
000661  feet/sec       YDOT =        5659
907395  meter/sec
 ZDOT =      15996
896794                 ZDOT =        4867
413231

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19713840
19                 X    =         6008778
49
 Y    =         752262
56  feet           Y    =          229289
63  meter
 Z    =       10251753
90                 Z    =         3124734
59
 XDOT =      -8936
339925                 XDOT =       -2723
796409
 YDOT =      15838
922786  feet/sec       YDOT =        4827
703665  meter/sec
 ZDOT =      15958
151503                 ZDOT =        4864
044578


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   18322
87039581  
00016717  00000-0  10270-3 0  9082
2 25544  51
6420 327
8915 0005213  58
0031 302
1628 15
53981322 22569


Satellite: ISS
Catalog Number: 25544
Epoch time:      18322
87039581   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:       327
8915  deg
Eccentricity:     
0005213     
Arg of perigee:    58
0031  deg
Mean anomaly:     302
1628  deg
Mean motion:   15
53981322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2256
Checksum:              295


Coasting Arc #10 (Orbit 2270)
---------------------------------------

Vector Time (GMT): 2018/323/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5258470
21                 A    =         6781793
73  meter
 Y    =        -285415
36  meter          E    =           
0013614
 Z    =       -4287461
52                 I    =           51
40586
 XDOT =       3199
669691                 Wp   =           65
86662
 YDOT =      -5994
078459  meter/sec      RA   =          322
58123  deg
 ZDOT =      -3528
727635                 TA   =          168
01457
                                          MA   =          167
98214
                                          Ha   =            222
943  n
mi
                                          Hp   =            213
042

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17252198
86                 X    =        -5234061
10
 Y    =        -936402
11  feet           Y    =         -344082
74  meter
 Z    =      -14066474
80                 Z    =        -4312946
63
 XDOT =      10497
603974                 XDOT =        3283
600424
 YDOT =     -19665
611743  feet/sec       YDOT =       -5957
828231  meter/sec
 ZDOT =     -11577
190402                 ZDOT =       -3512
980565

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16761517
07                 X    =        -5108910
40
 Y    =       -3785748
80  feet           Y    =        -1153896
23  meter
 Z    =      -14180993
59                 Z    =        -4322366
85
 XDOT =      13430
067273                 XDOT =        4093
484505
 YDOT =     -16405
302468  feet/sec       YDOT =       -5000
336192  meter/sec
 ZDOT =     -11505
567135                 ZDOT =       -3506
896863


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   18323
83500996  
00016717  00000-0  10270-3 0  9093
2 25544  51
6414 323
0846 0005111  60
7787 299
3876 15
54003360 22715


Satellite: ISS
Catalog Number: 25544
Epoch time:      18323
83500996   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       323
0846  deg
Eccentricity:     
0005111     
Arg of perigee:    60
7787  deg
Mean anomaly:     299
3876  deg
Mean motion:   15
54003360  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2271
Checksum:              312


Coasting Arc #11 (Orbit 2286)
---------------------------------------

Vector Time (GMT): 2018/324/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4262762
51                 A    =         6778825
85  meter
 Y    =        1549639
98  meter          E    =           
0009215
 Z    =        5030154
89                 I    =           51
37027
 XDOT =      -4384
488774                 Wp   =           95
68949
 YDOT =       6018
793261  meter/sec      RA   =          317
57100  deg
 ZDOT =       1857
554819                 TA   =          336
24029
                                          MA   =          336
28280
                                          Ha   =            222
857  n
mi
                                          Hp   =            213
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13985441
31                 X    =         4220682
73
 Y    =        5084120
67  feet           Y    =         1597073
77  meter
 Z    =       16503132
86                 Z    =         5050760
27
 XDOT =     -14384
805690                 XDOT =       -4460
489986
 YDOT =      19746
697051  feet/sec       YDOT =        5969
337875  meter/sec
 ZDOT =       6094
339958                 ZDOT =        1836
071474

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12956991
95                 X    =         3949291
15
 Y    =        7106250
18  feet           Y    =         2165985
05  meter
 Z    =       16595535
96                 Z    =         5058319
36
 XDOT =     -16701
932860                 XDOT =       -5090
749136
 YDOT =      16418
903640  feet/sec       YDOT =        5004
481830  meter/sec
 ZDOT =       5996
938555                 ZDOT =        1827
866872


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   18324
86393006  
00016717  00000-0  10270-3 0  9101
2 25544  51
6415 317
9562 0005117  65
5407 294
6279 15
53999140 22872


Satellite: ISS
Catalog Number: 25544
Epoch time:      18324
86393006   =   yrday
fracday
Element set:     910
Inclination:       51
6415  deg
RA of node:       317
9562  deg
Eccentricity:     
0005117     
Arg of perigee:    65
5407  deg
Mean anomaly:     294
6279  deg
Mean motion:   15
53999140  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2287
Checksum:              327


Coasting Arc #12 (Orbit 2301)
---------------------------------------

Vector Time (GMT): 2018/325/19:30:01
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3117306
42                 A    =         6777660
48  meter
 Y    =       -2876986
30  meter          E    =           
0019632
 Z    =       -5302980
77                 I    =           51
34276
 XDOT =       5182
587172                 Wp   =           84
16856
 YDOT =      -5632
263066  meter/sec      RA   =          312
55266  deg
 ZDOT =         11
085685                 TA   =          185
92608
                                          MA   =          185
94934
                                          Ha   =            222
941  n
mi
                                          Hp   =            212
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10227383
27                 X    =        -3059143
68
 Y    =       -9438931
42  feet           Y    =        -2911520
75  meter
 Z    =      -17398230
87                 Z    =        -5317982
83
 XDOT =      17003
238753                 XDOT =        5245
129678
 YDOT =     -18478
553367  feet/sec       YDOT =       -5573
958080  meter/sec
 ZDOT =         36
370359                 ZDOT =          36
413252

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8768561
28                 X    =        -2672657
48
 Y    =      -10698979
45  feet           Y    =        -3261048
93  meter
 Z    =      -17465262
78                 Z    =        -5323412
10
 XDOT =      18525
038653                 XDOT =        5646
431782
 YDOT =     -15418
420866  feet/sec       YDOT =       -4699
534680  meter/sec
 ZDOT =        150
988442                 ZDOT =          46
021277


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   18325
82853767  
00016717  00000-0  10270-3 0  9114
2 25544  51
6415 313
1479 0005068  67
1628 293
0059 15
54025864 23026


Satellite: ISS
Catalog Number: 25544
Epoch time:      18325
82853767   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:       313
1479  deg
Eccentricity:     
0005068     
Arg of perigee:    67
1628  deg
Mean anomaly:     293
0059  deg
Mean motion:   15
54025864  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2302
Checksum:              314


Coasting Arc #13 (Orbit 2303)
---------------------------------------

Vector Time (GMT): 2018/325/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4216289
33                 A    =         6778559
82  meter
 Y    =        1425434
00  meter          E    =           
0008679
 Z    =        5105408
86                 I    =           51
34112
 XDOT =      -4038
664689                 Wp   =           95
30296
 YDOT =       6335
958417  meter/sec      RA   =          312
09491  deg
 ZDOT =       1563
233345                 TA   =          339
55933
                                          MA   =          339
59404
                                          Ha   =            222
894  n
mi
                                          Hp   =            213
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13832970
24                 X    =         4175236
30
 Y    =        4676620
74  feet           Y    =         1472353
71  meter
 Z    =       16750029
06                 Z    =         5125791
04
 XDOT =     -13250
212235                 XDOT =       -4116
808553
 YDOT =      20787
265149  feet/sec       YDOT =        6290
358263  meter/sec
 ZDOT =       5128
718325                 ZDOT =        1543
424858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14376372
08                 X    =         4381918
21
 Y    =       -1863069
73  feet           Y    =         -567863
65  meter
 Z    =       16841443
46                 Z    =         5133271
97
 XDOT =      -2873
181081                 XDOT =        -875
745593
 YDOT =      23468
993453  feet/sec       YDOT =        7153
349204  meter/sec
 ZDOT =       5038
810162                 ZDOT =        1535
829337


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   18325
95715235  
00016717  00000-0  10270-3 0  9126
2 25544  51
6393 312
5051 0005094  68
2831 291
8864 15
53978826 23043


Satellite: ISS
Catalog Number: 25544
Epoch time:      18325
95715235   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:       312
5051  deg
Eccentricity:     
0005094     
Arg of perigee:    68
2831  deg
Mean anomaly:     291
8864  deg
Mean motion:   15
53978826  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2304
Checksum:              323


Coasting Arc #14 (Orbit 2318)
---------------------------------------

Vector Time (GMT): 2018/326/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3164536
99                 A    =         6777727
39  meter
 Y    =       -2842801
73  meter          E    =           
0019673
 Z    =       -5293561
30                 I    =           51
31532
 XDOT =       4810
810665                 Wp   =           87
32381
 YDOT =      -5944
356628  meter/sec      RA   =          307
07368  deg
 ZDOT =        318
282527                 TA   =          185
71871
                                          MA   =          185
74121
                                          Ha   =            222
995  n
mi
                                          Hp   =            212
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10382339
21                 X    =        -3106798
76
 Y    =       -9326777
34  feet           Y    =        -2877866
58  meter
 Z    =      -17367327
09                 Z    =        -5308793
90
 XDOT =      15783
499557                 XDOT =        4875
378479
 YDOT =     -19502
482374  feet/sec       YDOT =       -5890
197802  meter/sec
 ZDOT =       1044
234013                 ZDOT =         341
808827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13394667
29                 X    =        -4082694
59
 Y    =       -3604923
66  feet           Y    =        -1098780
73  meter
 Z    =      -17435400
97                 Z    =        -5314310
22
 XDOT =       4856
323408                 XDOT =        1480
207375
 YDOT =     -23579
824701  feet/sec       YDOT =       -7187
130569  meter/sec
 ZDOT =       1150
792054                 ZDOT =         350
761418


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   18326
92175607  
00016717  00000-0  10270-3 0  9138
2 25544  51
6375 307
6961 0005096  72
7229 287
4481 15
54017006 23198


Satellite: ISS
Catalog Number: 25544
Epoch time:      18326
92175607   =   yrday
fracday
Element set:     913
Inclination:       51
6375  deg
RA of node:       307
6961  deg
Eccentricity:     
0005096     
Arg of perigee:    72
7229  deg
Mean anomaly:     287
4481  deg
Mean motion:   15
54017006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2319
Checksum:              320


Coasting Arc #15 (Orbit 2334)
---------------------------------------

Vector Time (GMT): 2018/327/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2034803
27                 A    =         6779320
14  meter
 Y    =        4183261
41  meter          E    =           
0011210
 Z    =        4924140
22                 I    =           51
30200
 XDOT =      -5271
512274                 Wp   =           65
58855
 YDOT =       5134
890733  meter/sec      RA   =          302
05331  deg
 ZDOT =      -2175
483519                 TA   =           45
75673
                                          MA   =           45
66476
                                          Ha   =            222
901  n
mi
                                          Hp   =            213
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6675863
76                 X    =         1963954
18
 Y    =       13724610
92  feet           Y    =         4205619
40  meter
 Z    =       16155315
68                 Z    =         4933853
14
 XDOT =     -17294
987777                 XDOT =       -5317
972652
 YDOT =      16846
754372  feet/sec       YDOT =        5075
681445  meter/sec
 ZDOT =      -7137
413119                 ZDOT =       -2201
203710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12271612
05                 X    =         3740387
35
 Y    =        8996981
52  feet           Y    =         2742279
97  meter
 Z    =       16198400
78                 Z    =         4937272
56
 XDOT =      -6590
872962                 XDOT =       -2008
898079
 YDOT =      22099
439465  feet/sec       YDOT =        6735
909149  meter/sec
 ZDOT =      -7253
716535                 ZDOT =       -2210
932800


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   18327
95066457  
00016717  00000-0  10270-3 0  9145
2 25544  51
6381 302
5678 0004928  76
6055 283
5647 15
54007565 23355


Satellite: ISS
Catalog Number: 25544
Epoch time:      18327
95066457   =   yrday
fracday
Element set:     914
Inclination:       51
6381  deg
RA of node:       302
5678  deg
Eccentricity:     
0004928     
Arg of perigee:    76
6055  deg
Mean anomaly:     283
5647  deg
Mean motion:   15
54007565  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2335
Checksum:              334


Coasting Arc #16 (Orbit 2349)
---------------------------------------

Vector Time (GMT): 2018/328/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -963411
41                 A    =         6782508
71  meter
 Y    =       -5329543
02  meter          E    =           
0012101
 Z    =       -4094466
24                 I    =           51
29595
 XDOT =       5397
992044                 Wp   =           97
38772
 YDOT =      -3885
878675  meter/sec      RA   =          297
03713  deg
 ZDOT =       3796
063847                 TA   =          212
00870
                                          MA   =          212
08225
                                          Ha   =            222
990  n
mi
                                          Hp   =            212
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3160798
59                 X    =         -883854
21
 Y    =      -17485377
35  feet           Y    =        -5339871
28  meter
 Z    =      -13433288
19                 Z    =        -4098953
59
 XDOT =      17709
947650                 XDOT =        5422
604183
 YDOT =     -12748
945783  feet/sec       YDOT =       -3825
377372  meter/sec
 ZDOT =      12454
277714                 ZDOT =        3822
345320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11203764
28                 X    =        -3414907
35
 Y    =      -13772502
66  feet           Y    =        -4197858
81  meter
 Z    =      -13452737
16                 Z    =        -4100394
29
 XDOT =       8174
686874                 XDOT =        2491
644559
 YDOT =     -18904
934467  feet/sec       YDOT =       -5762
224026  meter/sec
 ZDOT =      12572
931803                 ZDOT =        3832
229614


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   18328
91526267  
00016717  00000-0  10270-3 0  9153
2 25544  51
6379 297
7587 0005060  81
0848 279
0877 15
54026885 23502


Satellite: ISS
Catalog Number: 25544
Epoch time:      18328
91526267   =   yrday
fracday
Element set:     915
Inclination:       51
6379  deg
RA of node:       297
7587  deg
Eccentricity:     
0005060     
Arg of perigee:    81
0848  deg
Mean anomaly:     279
0877  deg
Mean motion:   15
54026885  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2350
Checksum:              349


Coasting Arc #17 (Orbit 2365)
---------------------------------------

Vector Time (GMT): 2018/329/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -65188
74                 A    =         6786214
02  meter
 Y    =        6167701
33  meter          E    =           
0018176
 Z    =        2811779
29                 I    =           51
29438
 XDOT =      -5296
984006                 Wp   =           95
28651
 YDOT =       2266
118575  meter/sec      RA   =          292
03086  deg
 ZDOT =      -5066
907683                 TA   =           52
60407
                                          MA   =           52
43873
                                          Ha   =            222
911  n
mi
                                          Hp   =            212
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -213873
80                 X    =         -147811
19
 Y    =       20235240
58  feet           Y    =         6166510
05  meter
 Z    =        9224997
68                 Z    =         2811262
65
 XDOT =     -17378
556449                 XDOT =       -5297
317966
 YDOT =       7434
772229  feet/sec       YDOT =        2206
882729  meter/sec
 ZDOT =     -16623
712870                 ZDOT =       -5092
639532

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9926329
54                 X    =         3025545
24
 Y    =       17636232
98  feet           Y    =         5375523
81  meter
 Z    =        9221851
97                 Z    =         2810820
48
 XDOT =      -9911
205969                 XDOT =       -3020
935579
 YDOT =      14377
233797  feet/sec       YDOT =        4382
180861  meter/sec
 ZDOT =     -16739
678632                 ZDOT =       -5102
254047


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   18329
94416140  
00016717  00000-0  10270-3 0  9166
2 25544  51
6379 292
6302 0004933  83
4783 276
6931 15
54048553 23660


Satellite: ISS
Catalog Number: 25544
Epoch time:      18329
94416140   =   yrday
fracday
Element set:     916
Inclination:       51
6379  deg
RA of node:       292
6302  deg
Eccentricity:     
0004933     
Arg of perigee:    83
4783  deg
Mean anomaly:     276
6931  deg
Mean motion:   15
54048553  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2366
Checksum:              330


Coasting Arc #18 (Orbit 2380)
---------------------------------------

Vector Time (GMT): 2018/330/21:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932630
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         936344
82                 A    =         6788904
92  meter
 Y    =       -6595411
43  meter          E    =           
0012776
 Z    =       -1293529
42                 I    =           51
29110
 XDOT =       4992
012114                 Wp   =           56
16345
 YDOT =       -419
805447  meter/sec      RA   =          287
03275  deg
 ZDOT =       5802
402600                 TA   =          289
69738
                                          MA   =          289
83517
                                          Ha   =            223
038  n
mi
                                          Hp   =            212
917

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3071997
44                 X    =         1016310
30
 Y    =      -21638488
94  feet           Y    =        -6584493
32  meter
 Z    =       -4243862
92                 Z    =        -1288787
42
 XDOT =      16377
992499                 XDOT =        4968
150204
 YDOT =      -1377
314460  feet/sec       YDOT =        -364
115348  meter/sec
 ZDOT =      19036
753937                 ZDOT =        5826
594293

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8535752
92                 X    =        -2601697
49
 Y    =      -20124365
30  feet           Y    =        -6133906
54  meter
 Z    =       -4221680
65                 Z    =        -1286768
26
 XDOT =      11730
563550                 XDOT =        3575
475770
 YDOT =      -8958
413742  feet/sec       YDOT =       -2730
524509  meter/sec
 ZDOT =      19145
554754                 ZDOT =        5835
565089


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   18330
90875396  
00016717  00000-0  10270-3 0  9177
2 25544  51
6371 287
8225 0005163  89
6763 270
4981 15
54031044 23815


Satellite: ISS
Catalog Number: 25544
Epoch time:      18330
90875396   =   yrday
fracday
Element set:     917
Inclination:       51
6371  deg
RA of node:       287
8225  deg
Eccentricity:     
0005163     
Arg of perigee:    89
6763  deg
Mean anomaly:     270
4981  deg
Mean motion:   15
54031044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2381
Checksum:              326
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