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

 
Date: July 18th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15476 3504 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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


199/15:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 215 4

201/19:34:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 2
000/00:00:00 000 0 0 0 0 215 3

203/18:49:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 215 1

206/03:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 5
000/00:00:00 000 0 0 0 0 214 8

207/15:56:37 527 -1 2 1 2 1 2
N/A 0 2 0 0 221 8
000/00:03:15 055 -0 3 0 0 215 4

209/20:18:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 9
000/00:00:00 000 0 0 0 0 215 3

212/23:22:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 214 9

Coasting Arc #1 (Orbit 337)
---------------------------------------

Vector Time (GMT): 2018/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2336008
30                 A    =         6777903
41  meter
 Y    =        3568154
52  meter          E    =           
0013347
 Z    =       -5279218
57                 I    =           51
36408
 XDOT =      -5996
108872                 Wp   =           70
35235
 YDOT =      -4733
796712  meter/sec      RA   =          221
54731  deg
 ZDOT =       -543
008083                 TA   =          194
42090
                                          MA   =          194
45903
                                          Ha   =            220
987  n
mi
                                          Hp   =            215
480

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7664069
22                 X    =        -2350091
47
 Y    =       11706543
71  feet           Y    =         3541953
20  meter
 Z    =      -17320270
90                 Z    =        -5290599
95
 XDOT =     -19672
273201                 XDOT =       -5940
091003
 YDOT =     -15530
829109  feet/sec       YDOT =       -4800
536099  meter/sec
 ZDOT =      -1781
522581                 ZDOT =        -571
998888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13810858
53                 X    =         4209549
68
 Y    =        1805281
71  feet           Y    =          550249
87  meter
 Z    =      -17371645
04                 Z    =        -5294877
41
 XDOT =      -5477
123435                 XDOT =       -1669
427223
 YDOT =      23411
526786  feet/sec       YDOT =        7135
833364  meter/sec
 ZDOT =      -1910
766832                 ZDOT =        -582
401731


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   18199
51708513  
00016717  00000-0  10270-3 0  9005
2 25544  51
6398 222
5590 0004007 328
2925  31
7985 15
53979603  3386


Satellite: ISS
Catalog Number: 25544
Epoch time:      18199
51708513   =   yrday
fracday
Element set:     900
Inclination:       51
6398  deg
RA of node:       222
5590  deg
Eccentricity:     
0004007     
Arg of perigee:   328
2925  deg
Mean anomaly:      31
7985  deg
Mean motion:   15
53979603  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             338
Checksum:              325


Coasting Arc #2 (Orbit 339)
---------------------------------------

Vector Time (GMT): 2018/199/15:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5109573
65                 A    =         6781261
86  meter
 Y    =         288034
61  meter          E    =           
0006843
 Z    =       -4454930
60                 I    =           51
37551
 XDOT =      -3174
274364                 Wp   =           87
88767
 YDOT =      -6172
508933  meter/sec      RA   =          220
84209  deg
 ZDOT =       3246
217596                 TA   =          214
92815
                                          MA   =          214
97307
                                          Ha   =            221
011  n
mi
                                          Hp   =            215
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16763693
07                 X    =        -5090775
36
 Y    =         944995
44  feet           Y    =          231001
17  meter
 Z    =      -14615914
04                 Z    =        -4479705
13
 XDOT =     -10414
285972                 XDOT =       -3120
783953
 YDOT =     -20251
013560  feet/sec       YDOT =       -6207
706948  meter/sec
 ZDOT =      10650
320197                 ZDOT =        3230
927872

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16297172
01                 X    =         4967378
03
 Y    =        3613980
58  feet           Y    =         1101541
28  meter
 Z    =      -14726869
78                 Z    =        -4488749
91
 XDOT =       4859
984578                 XDOT =        1481
323299
 YDOT =      21147
029316  feet/sec       YDOT =        6445
614535  meter/sec
 ZDOT =      10582
584525                 ZDOT =        3225
571763


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   18199
64570141  
00016717  00000-0  10270-3 0  9014
2 25544  51
6366 221
9182 0004166 330
3167  29
7748 15
53967485  3401


Satellite: ISS
Catalog Number: 25544
Epoch time:      18199
64570141   =   yrday
fracday
Element set:     901
Inclination:       51
6366  deg
RA of node:       221
9182  deg
Eccentricity:     
0004166     
Arg of perigee:   330
3167  deg
Mean anomaly:      29
7748  deg
Mean motion:   15
53967485  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             340
Checksum:              319


Coasting Arc #3 (Orbit 355)
---------------------------------------

Vector Time (GMT): 2018/200/15:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5833704
70                 A    =         6784905
49  meter
 Y    =         935468
50  meter          E    =           
0011216
 Z    =        3330438
21                 I    =           51
41320
 XDOT =       1733
207754                 Wp   =           71
37645
 YDOT =       5837
889424  meter/sec      RA   =          215
83965  deg
 ZDOT =      -4659
296470                 TA   =           69
70515
                                          MA   =           69
58464
                                          Ha   =            221
086  n
mi
                                          Hp   =            215
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19139451
11                 X    =         5806633
11
 Y    =        3069122
39  feet           Y    =         1000553
46  meter
 Z    =       10926634
55                 Z    =         3358710
34
 XDOT =       5686
377145                 XDOT =        1690
430227
 YDOT =      19153
180525  feet/sec       YDOT =        5857
032434  meter/sec
 ZDOT =     -15286
405740                 ZDOT =       -4650
980794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17655374
58                 X    =        -5381358
17
 Y    =       -7825964
61  feet           Y    =        -2385354
01  meter
 Z    =       11053120
37                 Z    =         3368991
09
 XDOT =      -1288
341795                 XDOT =        -392
686579
 YDOT =     -18707
064755  feet/sec       YDOT =       -5701
913337  meter/sec
 ZDOT =     -15249
843896                 ZDOT =       -4648
152420


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   18200
67462652  
00016717  00000-0  10270-3 0  9028
2 25544  51
6362 216
7898 0004263 333
6751  26
4184 15
53995791  3562


Satellite: ISS
Catalog Number: 25544
Epoch time:      18200
67462652   =   yrday
fracday
Element set:     902
Inclination:       51
6362  deg
RA of node:       216
7898  deg
Eccentricity:     
0004263     
Arg of perigee:   333
6751  deg
Mean anomaly:      26
4184  deg
Mean motion:   15
53995791  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             356
Checksum:              324


Coasting Arc #4 (Orbit 370)
---------------------------------------

Vector Time (GMT): 2018/201/15:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6213343
71                 A    =         6788131
43  meter
 Y    =       -1947655
96  meter          E    =           
0009629
 Z    =       -1899998
12                 I    =           51
45157
 XDOT =        -65
905772                 Wp   =           17
22341
 YDOT =      -5237
760005  meter/sec      RA   =          210
84895  deg
 ZDOT =       5600
957051                 TA   =          321
78922
                                          MA   =          321
85743
                                          Ha   =            221
153  n
mi
                                          Hp   =            215
319

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20384985
94                 X    =        -6181873
59
 Y    =       -6389947
37  feet           Y    =        -2016961
77  meter
 Z    =       -6233589
65                 Z    =        -1930103
85
 XDOT =       -216
226285                 XDOT =         -34
537077
 YDOT =     -17184
251984  feet/sec       YDOT =       -5238
321997  meter/sec
 ZDOT =      18375
843344                 ZDOT =        5600
712738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18236766
69                 X    =         5558566
49
 Y    =       11050035
02  feet           Y    =         3368050
67  meter
 Z    =       -6368185
44                 Z    =        -1941022
92
 XDOT =      -2956
735878                 XDOT =        -901
213095
 YDOT =      15439
380276  feet/sec       YDOT =        4705
923108  meter/sec
 ZDOT =      18375
347685                 ZDOT =        5600
805974


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   18201
63924192  
00016717  00000-0  10270-3 0  9038
2 25544  51
6364 211
9824 0004205 337
3242  22
7724 15
53990000  3716


Satellite: ISS
Catalog Number: 25544
Epoch time:      18201
63924192   =   yrday
fracday
Element set:     903
Inclination:       51
6364  deg
RA of node:       211
9824  deg
Eccentricity:     
0004205     
Arg of perigee:   337
3242  deg
Mean anomaly:      22
7724  deg
Mean motion:   15
53990000  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             371
Checksum:              278


Coasting Arc #5 (Orbit 373)
---------------------------------------

Vector Time (GMT): 2018/201/19:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1692289
86                 A    =         6777756
19  meter
 Y    =        3896832
62  meter          E    =           
0013898
 Z    =       -5292593
31                 I    =           51
42573
 XDOT =      -6785
940555                 Wp   =           69
78595
 YDOT =      -3525
104218  meter/sec      RA   =          209
97249  deg
 ZDOT =       -421
880428                 TA   =          196
15142
                                          MA   =          196
19577
                                          Ha   =            221
188  n
mi
                                          Hp   =            215
259

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5552132
07                 X    =        -1710031
11
 Y    =       12784883
93  feet           Y    =         3877809
44  meter
 Z    =      -17364151
27                 Z    =        -5300856
62
 XDOT =     -22263
584497                 XDOT =       -6743
968269
 YDOT =     -11565
302554  feet/sec       YDOT =       -3600
754581  meter/sec
 ZDOT =      -1384
122138                 ZDOT =        -454
742229

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6546099
95                 X    =        -1995251
27
 Y    =      -12252592
72  feet           Y    =        -3734590
26  meter
 Z    =      -17401601
19                 Z    =        -5304008
04
 XDOT =      22072
401021                 XDOT =        6727
667831
 YDOT =      -9600
558902  feet/sec       YDOT =       -2926
250353  meter/sec
 ZDOT =      -1530
883386                 ZDOT =        -466
613256


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   18201
83216446  
00016717  00000-0  10270-3 0  9047
2 25544  51
6401 211
0221 0004321 336
5314  23
5640 15
54016393  3744


Satellite: ISS
Catalog Number: 25544
Epoch time:      18201
83216446   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       211
0221  deg
Eccentricity:     
0004321     
Arg of perigee:   336
5314  deg
Mean anomaly:      23
5640  deg
Mean motion:   15
54016393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             374
Checksum:              255


Coasting Arc #6 (Orbit 389)
---------------------------------------

Vector Time (GMT): 2018/202/19:34:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3233321
31                 A    =         6778266
12  meter
 Y    =       -3011459
44  meter          E    =           
0007072
 Z    =        5139748
01                 I    =           51
45717
 XDOT =       6249
295854                 Wp   =           18
22458
 YDOT =       4196
491347  meter/sec      RA   =          204
96017  deg
 ZDOT =      -1465
393571                 TA   =           85
95675
                                          MA   =           85
87592
                                          Ha   =            221
139  n
mi
                                          Hp   =            215
220

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10608009
53                 X    =         3241789
97
 Y    =       -9880116
28  feet           Y    =        -2975255
29  meter
 Z    =       16862690
32                 Z    =         5155474
57
 XDOT =      20502
939153                 XDOT =        6209
023130
 YDOT =      13768
016230  feet/sec       YDOT =        4266
150233  meter/sec
 ZDOT =      -4807
721691                 ZDOT =       -1435
134341

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1357615
21                 X    =          413801
12
 Y    =       14349614
35  feet           Y    =         4373762
45  meter
 Z    =       16933467
98                 Z    =         5161321
04
 XDOT =     -22426
063403                 XDOT =       -6835
464125
 YDOT =       7663
283109  feet/sec       YDOT =        2335
768692  meter/sec
 ZDOT =      -4672
672002                 ZDOT =       -1424
230426


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   18202
86108194  
00016717  00000-0  10270-3 0  9052
2 25544  51
6402 205
8937 0004416 339
5755  20
5220 15
54045154  3903


Satellite: ISS
Catalog Number: 25544
Epoch time:      18202
86108194   =   yrday
fracday
Element set:     905
Inclination:       51
6402  deg
RA of node:       205
8937  deg
Eccentricity:     
0004416     
Arg of perigee:   339
5755  deg
Mean anomaly:      20
5220  deg
Mean motion:   15
54045154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             390
Checksum:              289


Coasting Arc #7 (Orbit 404)
---------------------------------------

Vector Time (GMT): 2018/203/18:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5020633
00                 A    =         6781999
18  meter
 Y    =       -1732292
92  meter          E    =           
0011074
 Z    =        4214779
74                 I    =           51
49772
 XDOT =       4728
822847                 Wp   =           50
71432
 YDOT =       4815
432547  meter/sec      RA   =          200
10954  deg
 ZDOT =      -3640
504449                 TA   =           76
69422
                                          MA   =           76
57075
                                          Ha   =            221
359  n
mi
                                          Hp   =            215
053

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16471893
04                 X    =         5019157
83
 Y    =       -5683375
73  feet           Y    =        -1676157
39  meter
 Z    =       13828017
53                 Z    =         4239164
29
 XDOT =      15514
510653                 XDOT =        4692
307400
 YDOT =      15798
663213  feet/sec       YDOT =        4868
109689  meter/sec
 ZDOT =     -11943
912235                 ZDOT =       -3617
621884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8411585
03                 X    =        -2563851
12
 Y    =       15160180
05  feet           Y    =         4620822
88  meter
 Z    =       13937441
19                 Z    =         4248132
07
 XDOT =     -21049
783913                 XDOT =       -6415
974137
 YDOT =       -752
794917  feet/sec       YDOT =        -229
451891  meter/sec
 ZDOT =     -11841
954729                 ZDOT =       -3609
427801


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   18203
82569314  
00016717  00000-0  10270-3 0  9065
2 25544  51
6391 201
0863 0004407 345
8281  14
2747 15
54017696  4051


Satellite: ISS
Catalog Number: 25544
Epoch time:      18203
82569314   =   yrday
fracday
Element set:     906
Inclination:       51
6391  deg
RA of node:       201
0863  deg
Eccentricity:     
0004407     
Arg of perigee:   345
8281  deg
Mean anomaly:      14
2747  deg
Mean motion:   15
54017696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             405
Checksum:              300


Coasting Arc #8 (Orbit 419)
---------------------------------------

Vector Time (GMT): 2018/204/18:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6013936
23                 A    =         6785682
01  meter
 Y    =         859157
78  meter          E    =           
0006570
 Z    =       -3019047
68                 I    =           51
54183
 XDOT =      -3179
021100                 Wp   =           30
73144
 YDOT =      -4924
296267  meter/sec      RA   =          195
11757  deg
 ZDOT =       4941
536531                 TA   =          294
63483
                                          MA   =          294
70326
                                          Ha   =            221
396  n
mi
                                          Hp   =            214
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19730761
91                 X    =        -6008431
82
 Y    =        2818759
14  feet           Y    =          791936
89  meter
 Z    =       -9905012
07                 Z    =        -3048247
53
 XDOT =     -10429
859251                 XDOT =       -3147
723113
 YDOT =     -16155
827648  feet/sec       YDOT =       -4959
671801  meter/sec
 ZDOT =      16212
390195                 ZDOT =        4926
169608

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12505799
15                 X    =         3811767
58
 Y    =      -15435116
13  feet           Y    =        -4704623
40  meter
 Z    =      -10035925
98                 Z    =        -3058950
24
 XDOT =      17584
437675                 XDOT =        5359
736603
 YDOT =       3771
964934  feet/sec       YDOT =        1149
694912  meter/sec
 ZDOT =      16144
097413                 ZDOT =        4920
720891


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   18204
79030034  
00016717  00000-0  10270-3 0  9075
2 25544  51
6395 196
2783 0004428 347
0480  13
0558 15
54017125  4200


Satellite: ISS
Catalog Number: 25544
Epoch time:      18204
79030034   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:       196
2783  deg
Eccentricity:     
0004428     
Arg of perigee:   347
0480  deg
Mean anomaly:      13
0558  deg
Mean motion:   15
54017125  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             420
Checksum:              289


Coasting Arc #9 (Orbit 435)
---------------------------------------

Vector Time (GMT): 2018/205/18:49:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6619475
98                 A    =         6788735
95  meter
 Y    =         -16396
15  meter          E    =           
0011897
 Z    =        1489531
08                 I    =           51
58406
 XDOT =       1317
568092                 Wp   =          101
09888
 YDOT =       4879
737663  meter/sec      RA   =          190
13769  deg
 ZDOT =      -5764
682861                 TA   =           62
62974
                                          MA   =           62
50872
                                          Ha   =            221
614  n
mi
                                          Hp   =            214
896

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21717440
88                 X    =         6611932
10
 Y    =         -53793
13  feet           Y    =           57585
06  meter
 Z    =        4886912
99                 Z    =         1521667
44
 XDOT =       4322
729961                 XDOT =        1290
905005
 YDOT =      16009
638001  feet/sec       YDOT =        4894
323168  meter/sec
 ZDOT =     -18913
001513                 ZDOT =       -5758
346883

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15609990
86                 X    =        -4757925
21
 Y    =       15051583
76  feet           Y    =         4587722
73  meter
 Z    =        5030910
69                 Z    =         1533421
58
 XDOT =     -13195
141703                 XDOT =       -4021
879191
 YDOT =      -7333
133891  feet/sec       YDOT =       -2235
139210  meter/sec
 ZDOT =     -18885
155616                 ZDOT =       -5756
195432


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   18205
81921217  
00016717  00000-0  10270-3 0  9082
2 25544  51
6397 191
1502 0004327 352
1536   7
9548 15
53990083  4362


Satellite: ISS
Catalog Number: 25544
Epoch time:      18205
81921217   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:       191
1502  deg
Eccentricity:     
0004327     
Arg of perigee:   352
1536  deg
Mean anomaly:       7
9548  deg
Mean motion:   15
53990083  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             436
Checksum:              308


Coasting Arc #10 (Orbit 440)
---------------------------------------

Vector Time (GMT): 2018/206/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -899757
93                 A    =         6777646
21  meter
 Y    =        4128802
38  meter          E    =           
0014790
 Z    =       -5311385
47                 I    =           51
55752
 XDOT =      -7538
662378                 Wp   =           76
70767
 YDOT =      -1322
245492  meter/sec      RA   =          188
44382  deg
 ZDOT =        253
135077                 TA   =          195
68819
                                          MA   =          195
73407
                                          Ha   =            221
497  n
mi
                                          Hp   =            214
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2951961
71                 X    =         -920060
93
 Y    =       13545939
58  feet           Y    =         4118627
73  meter
 Z    =      -17425805
36                 Z    =        -5315804
98
 XDOT =     -24733
144284                 XDOT =       -7524
545958
 YDOT =      -4338
075760  feet/sec       YDOT =       -1406
469118  meter/sec
 ZDOT =        830
495659                 ZDOT =         216
549540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5831998
98                 X    =        -1777593
29
 Y    =       12549410
95  feet           Y    =         3825060
46  meter
 Z    =      -17446068
97                 Z    =        -5317561
82
 XDOT =     -22196
266855                 XDOT =       -6765
422137
 YDOT =      -9406
126254  feet/sec       YDOT =       -2866
987282  meter/sec
 ZDOT =        666
702329                 ZDOT =         203
210870


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   18206
14074523  
00016717  00000-0  10270-3 0  9099
2 25544  51
6387 189
5428 0003956 353
0502   7
0595 15
54033988  4411


Satellite: ISS
Catalog Number: 25544
Epoch time:      18206
14074523   =   yrday
fracday
Element set:     909
Inclination:       51
6387  deg
RA of node:       189
5428  deg
Eccentricity:     
0003956     
Arg of perigee:   353
0502  deg
Mean anomaly:       7
0595  deg
Mean motion:   15
54033988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             441
Checksum:              314


Coasting Arc #11 (Orbit 456)
---------------------------------------

Vector Time (GMT): 2018/207/03:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944469
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2628780
43                 A    =         6779123
69  meter
 Y    =       -3787415
88  meter          E    =           
0008813
 Z    =        4968098
78                 I    =           51
59494
 XDOT =       7062
574174                 Wp   =           34
59611
 YDOT =       2108
731468  meter/sec      RA   =          183
44130  deg
 ZDOT =      -2120
499442                 TA   =           76
11253
                                          MA   =           76
01451
                                          Ha   =            221
562  n
mi
                                          Hp   =            214
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8624607
70                 X    =         2646805
00
 Y    =      -12425905
11  feet           Y    =        -3757918
78  meter
 Z    =       16299536
69                 Z    =         4980911
65
 XDOT =      23171
175112                 XDOT =        7048
768942
 YDOT =       6918
410329  feet/sec       YDOT =        2187
633081  meter/sec
 ZDOT =      -6957
019167                 ZDOT =       -2086
225815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10933795
27                 X    =         3332620
80
 Y    =      -10360990
48  feet           Y    =        -3158029
90  meter
 Z    =       16357379
66                 Z    =         4985729
32
 XDOT =      20492
784020                 XDOT =        6246
200569
 YDOT =      10838
294843  feet/sec       YDOT =        3303
512268  meter/sec
 ZDOT =      -6803
647152                 ZDOT =       -2073
751652


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   18207
16965271  
00016717  00000-0  10270-3 0  9103
2 25544  51
6385 184
4138 0003965 357
8953   2
2182 15
54009978  4571


Satellite: ISS
Catalog Number: 25544
Epoch time:      18207
16965271   =   yrday
fracday
Element set:     910
Inclination:       51
6385  deg
RA of node:       184
4138  deg
Eccentricity:     
0003965     
Arg of perigee:   357
8953  deg
Mean anomaly:       2
2182  deg
Mean motion:   15
54009978  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             457
Checksum:              328


Coasting Arc #12 (Orbit 464)
---------------------------------------

Vector Time (GMT): 2018/207/15:58:15
055
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1569778
47                 A    =         6779030
85  meter
 Y    =        4114708
52  meter          E    =           
0014255
 Z    =       -5165969
30                 I    =           51
61045
 XDOT =      -7450
099655                 Wp   =           61
80595
 YDOT =       1035
839056  meter/sec      RA   =          180
77982  deg
 ZDOT =      -1435
249381                 TA   =          194
33864
                                          MA   =          194
37913
                                          Ha   =            221
790  n
mi
                                          Hp   =            215
403

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5150191
84                 X    =         1548743
07
 Y    =       13499699
88  feet           Y    =         4132145
77  meter
 Z    =      -16948718
17                 Z    =        -5158394
69
 XDOT =     -24442
584169                 XDOT =       -7454
157439
 YDOT =       3398
422099  feet/sec       YDOT =         952
504350  meter/sec
 ZDOT =      -4708
823428                 ZDOT =       -1471
448448

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5957787
09                 X    =        -1815933
51
 Y    =      -13206266
35  feet           Y    =        -4025269
98  meter
 Z    =      -16915221
63                 Z    =        -5155759
55
 XDOT =      23237
902451                 XDOT =        7082
912667
 YDOT =      -4229
165489  feet/sec       YDOT =       -1289
049641  meter/sec
 ZDOT =      -4871
186036                 ZDOT =       -1484
737504


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   18207
68410615  
00016717  00000-0  10270-3 0  9118
2 25544  51
6387 181
8539 0004261 347
1927  12
9117 15
53805718  4652


Satellite: ISS
Catalog Number: 25544
Epoch time:      18207
68410615   =   yrday
fracday
Element set:     911
Inclination:       51
6387  deg
RA of node:       181
8539  deg
Eccentricity:     
0004261     
Arg of perigee:   347
1927  deg
Mean anomaly:      12
9117  deg
Mean motion:   15
53805718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             465
Checksum:              314


Coasting Arc #13 (Orbit 480)
---------------------------------------

Vector Time (GMT): 2018/208/15:58:15
055
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         115234
12                 A    =         6778241
11  meter
 Y    =       -4217492
20  meter          E    =           
0005096
 Z    =        5303976
77                 I    =           51
64168
 XDOT =       7655
684321                 Wp   =           18
24322
 YDOT =       -267
512108  meter/sec      RA   =          175
78310  deg
 ZDOT =       -374
209773                 TA   =           75
35245
                                          MA   =           75
29596
                                          Ha   =            221
737  n
mi
                                          Hp   =            215
318

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         378064
69                 X    =          136623
34
 Y    =      -13836916
67  feet           Y    =        -4216084
44  meter
 Z    =       17401498
58                 Z    =         5304588
11
 XDOT =      25117
074543                 XDOT =        7659
924409
 YDOT =       -877
664396  feet/sec       YDOT =        -181
877218  meter/sec
 ZDOT =      -1227
722352                 ZDOT =        -337
011623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         695527
40                 X    =          211996
75
 Y    =       13820563
22  feet           Y    =         4212507
67  meter
 Z    =       17404701
17                 Z    =         5304952
92
 XDOT =     -23995
879269                 XDOT =       -7313
944001
 YDOT =       2563
643261  feet/sec       YDOT =         781
398466  meter/sec
 ZDOT =      -1060
941113                 ZDOT =        -323
374851


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   18208
71316027  
00016717  00000-0  10270-3 0  9126
2 25544  51
6391 176
7267 0004302 347
7946  12
3102 15
53833501  4818


Satellite: ISS
Catalog Number: 25544
Epoch time:      18208
71316027   =   yrday
fracday
Element set:     912
Inclination:       51
6391  deg
RA of node:       176
7267  deg
Eccentricity:     
0004302     
Arg of perigee:   347
7946  deg
Mean anomaly:      12
3102  deg
Mean motion:   15
53833501  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             481
Checksum:              288


Coasting Arc #14 (Orbit 495)
---------------------------------------

Vector Time (GMT): 2018/209/15:58:15
055
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1755714
60                 A    =         6779745
35  meter
 Y    =        4268514
95  meter          E    =           
0011686
 Z    =       -4975883
70                 I    =           51
68062
 XDOT =      -7335
037302                 Wp   =           85
64930
 YDOT =       -525
765344  meter/sec      RA   =          170
78930  deg
 ZDOT =       2142
311753                 TA   =          205
20705
                                          MA   =          205
26413
                                          Ha   =            221
944  n
mi
                                          Hp   =            215
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5760218
52                 X    =        -1779146
15
 Y    =       14004314
15  feet           Y    =         4248750
68  meter
 Z    =      -16325077
76                 Z    =        -4984468
77
 XDOT =     -24065
083012                 XDOT =       -7339
018887
 YDOT =      -1724
951917  feet/sec       YDOT =        -607
813211  meter/sec
 ZDOT =       7028
581868                 ZDOT =        2106
671768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4421423
63                 X    =         1347649
92
 Y    =      -14438785
40  feet           Y    =        -4400941
79  meter
 Z    =      -16364033
28                 Z    =        -4987757
34
 XDOT =      23117
150159                 XDOT =        7046
107368
 YDOT =       -686
524750  feet/sec       YDOT =        -209
252744  meter/sec
 ZDOT =       6868
849065                 ZDOT =        2093
625195


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   18209
67789730  
00016717  00000-0  10270-3 0  9138
2 25544  51
6403 171
9197 0004364 353
4347   6
6748 15
53804391  4961


Satellite: ISS
Catalog Number: 25544
Epoch time:      18209
67789730   =   yrday
fracday
Element set:     913
Inclination:       51
6403  deg
RA of node:       171
9197  deg
Eccentricity:     
0004364     
Arg of perigee:   353
4347  deg
Mean anomaly:       6
6748  deg
Mean motion:   15
53804391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             496
Checksum:              333


Coasting Arc #15 (Orbit 498)
---------------------------------------

Vector Time (GMT): 2018/209/20:18:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5552587
13                 A    =         6785278
08  meter
 Y    =        1796816
75  meter          E    =           
0006196
 Z    =       -3469453
07                 I    =           51
70122
 XDOT =      -4280
543799                 Wp   =           45
26231
 YDOT =       4419
553161  meter/sec      RA   =          169
93138  deg
 ZDOT =      -4562
555036                 TA   =          175
36504
                                          MA   =          175
35930
                                          Ha   =            221
941  n
mi
                                          Hp   =            215
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18217149
39                 X    =         5548934
35
 Y    =        5895068
09  feet           Y    =         1858889
43  meter
 Z    =      -11382720
03                 Z    =        -3442489
87
 XDOT =     -14043
778868                 XDOT =       -4307
484334
 YDOT =      14499
846330  feet/sec       YDOT =        4371
534835  meter/sec
 ZDOT =     -14969
012586                 ZDOT =       -4583
413108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11776803
95                 X    =        -3589569
84
 Y    =       15187375
32  feet           Y    =         4629112
00  meter
 Z    =      -11262024
44                 Z    =        -3432665
05
 XDOT =      -7769
368555                 XDOT =       -2368
103535
 YDOT =     -17192
588355  feet/sec       YDOT =       -5240
300931  meter/sec
 ZDOT =     -15063
011620                 ZDOT =       -4591
205942


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   18209
87084268  
00016717  00000-0  10270-3 0  9145
2 25544  51
6368 170
9564 0004362 352
9728   7
1362 15
53806160  4990


Satellite: ISS
Catalog Number: 25544
Epoch time:      18209
87084268   =   yrday
fracday
Element set:     914
Inclination:       51
6368  deg
RA of node:       170
9564  deg
Eccentricity:     
0004362     
Arg of perigee:   352
9728  deg
Mean anomaly:       7
1362  deg
Mean motion:   15
53806160  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             499
Checksum:              329


Coasting Arc #16 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2018/210/20:18:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4394676
33                 A    =         6781800
33  meter
 Y    =       -2504059
70  meter          E    =           
0008100
 Z    =        4510213
39                 I    =           51
72165
 XDOT =       5628
716894                 Wp   =           83
36083
 YDOT =      -4121
770634  meter/sec      RA   =          164
95181  deg
 ZDOT =       3192
130020                 TA   =          334
61260
                                          MA   =          334
65237
                                          Ha   =            222
137  n
mi
                                          Hp   =            215
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14418229
44                 X    =        -4388256
39
 Y    =       -8215418
97  feet           Y    =        -2553168
33  meter
 Z    =       14797288
02                 Z    =         4488881
51
 XDOT =      18466
918943                 XDOT =        5658
883991
 YDOT =     -13522
869535  feet/sec       YDOT =       -4058
657915  meter/sec
 ZDOT =      10472
867519                 ZDOT =        3219
544844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12482220
27                 X    =         3804580
74
 Y    =      -11062837
81  feet           Y    =        -3371952
96  meter
 Z    =       14701903
90                 Z    =         4481140
31
 XDOT =       6009
898857                 XDOT =        1831
817172
 YDOT =      20880
362734  feet/sec       YDOT =        6364
334561  meter/sec
 ZDOT =      10596
245739                 ZDOT =        3229
735701


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   18210
89989259  
00016717  00000-0  10270-3 0  9154
2 25544  51
6367 165
8287 0004334 355
4857   4
6256 15
53785371  5157


Satellite: ISS
Catalog Number: 25544
Epoch time:      18210
89989259   =   yrday
fracday
Element set:     915
Inclination:       51
6367  deg
RA of node:       165
8287  deg
Eccentricity:     
0004334     
Arg of perigee:   355
4857  deg
Mean anomaly:       4
6256  deg
Mean motion:   15
53785371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              345


Coasting Arc #17 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2018/211/20:18:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3004057
26                 A    =         6779089
19  meter
 Y    =        3233894
47  meter          E    =           
0015067
 Z    =       -5158380
09                 I    =           51
74453
 XDOT =      -6551
275248                 Wp   =           62
83440
 YDOT =       3661
578789  meter/sec      RA   =          159
96586  deg
 ZDOT =      -1516
409856                 TA   =          192
53860
                                          MA   =          192
57612
                                          Ha   =            222
069  n
mi
                                          Hp   =            215
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9855830
90                 X    =         2992727
87
 Y    =       10609890
00  feet           Y    =         3267424
74  meter
 Z    =      -16923819
20                 Z    =        -5143815
13
 XDOT =     -21493
685197                 XDOT =       -6584
367361
 YDOT =      12013
053771  feet/sec       YDOT =        3588
132921  meter/sec
 ZDOT =      -4975
097953                 ZDOT =       -1548
313292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13165284
17                 X    =        -4012778
62
 Y    =        6211064
20  feet           Y    =         1893132
37  meter
 Z    =      -16858849
28                 Z    =        -5138577
26
 XDOT =      -4357
135940                 XDOT =       -1328
055035
 YDOT =     -23158
578984  feet/sec       YDOT =       -7058
734874  meter/sec
 ZDOT =      -5118
569916                 ZDOT =       -1560
140110


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   18211
86462300  
00016717  00000-0  10270-3 0  9166
2 25544  51
6367 161
0213 0004197    
5965 359
5191 15
53812272  5307


Satellite: ISS
Catalog Number: 25544
Epoch time:      18211
86462300   =   yrday
fracday
Element set:     916
Inclination:       51
6367  deg
RA of node:       161
0213  deg
Eccentricity:     
0004197     
Arg of perigee:      
5965  deg
Mean anomaly:     359
5191  deg
Mean motion:   15
53812272  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             530
Checksum:              287


Coasting Arc #18 (Orbit 545)
---------------------------------------

Vector Time (GMT): 2018/212/20:18:00
000
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1462820
38                 A    =         6778384
85  meter
 Y    =       -3938894
93  meter          E    =           
0005501
 Z    =        5316743
06                 I    =           51
77294
 XDOT =       7041
787722                 Wp   =           31
21090
 YDOT =      -3026
334418  meter/sec      RA   =          154
97746  deg
 ZDOT =       -299
879052                 TA   =           61
66948
                                          MA   =           61
61400
                                          Ha   =            222
250  n
mi
                                          Hp   =            214
929

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4799279
47                 X    =        -1444491
33
 Y    =      -12922883
62  feet           Y    =        -3955150
81  meter
 Z    =       17443382
75                 Z    =         5309681
76
 XDOT =      23102
978092                 XDOT =        7076
562301
 YDOT =      -9928
918695  feet/sec       YDOT =       -2947
393838  meter/sec
 ZDOT =       -983
855158                 ZDOT =        -265
588687

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13793512
28                 X    =         4204262
54
 Y    =        -928496
12  feet           Y    =         -283005
62  meter
 Z    =       17412137
15                 Z    =         5307219
40
 XDOT =       2682
247491                 XDOT =         817
549035
 YDOT =      23995
127017  feet/sec       YDOT =        7313
714715  meter/sec
 ZDOT =       -829
730493                 ZDOT =        -252
901854


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   18212
89366603  
00016717  00000-0  10270-3 0  9170
2 25544  51
6369 155
8933 0004231   5
1067 355
0127 15
53779352  5460


Satellite: ISS
Catalog Number: 25544
Epoch time:      18212
89366603   =   yrday
fracday
Element set:     917
Inclination:       51
6369  deg
RA of node:       155
8933  deg
Eccentricity:     
0004231     
Arg of perigee:     5
1067  deg
Mean anomaly:     355
0127  deg
Mean motion:   15
53779352  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             546
Checksum:              314


Coasting Arc #19 (Orbit 547)
---------------------------------------

Vector Time (GMT): 2018/212/23:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1811499
66                 A    =         6778242
21  meter
 Y    =       -3780904
94  meter          E    =           
0004793
 Z    =        5323697
32                 I    =           51
77922
 XDOT =       6914
785825                 Wp   =           36
26966
 YDOT =      -3320
388659  meter/sec      RA   =          154
34162  deg
 ZDOT =         -1
475073                 TA   =           53
76651
                                          MA   =           53
72222
                                          Ha   =            222
154  n
mi
                                          Hp   =            214
870

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5943240
36                 X    =        -1794945
18
 Y    =      -12404543
78  feet           Y    =        -3801069
92  meter
 Z    =       17466198
54                 Z    =         5314937
97
 XDOT =      22686
305199                 XDOT =        6951
408574
 YDOT =     -10893
663578  feet/sec       YDOT =       -3242
857973  meter/sec
 ZDOT =         -4
839479                 ZDOT =          32
202873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7855817
52                 X    =         2394453
18
 Y    =      -11350663
87  feet           Y    =        -3459682
35  meter
 Z    =       17427319
49                 Z    =         5311846
98
 XDOT =      19768
573082                 XDOT =        6025
461075
 YDOT =      13887
859852  feet/sec       YDOT =        4233
019683  meter/sec
 ZDOT =        146
572229                 ZDOT =          44
675215


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   18213
02229595  
00016717  00000-0  10270-3 0  9185
2 25544  51
6395 155
2510 0003993   5
8977 354
2222 15
53820684  5489


Satellite: ISS
Catalog Number: 25544
Epoch time:      18213
02229595   =   yrday
fracday
Element set:     918
Inclination:       51
6395  deg
RA of node:       155
2510  deg
Eccentricity:     
0003993     
Arg of perigee:     5
8977  deg
Mean anomaly:     354
2222  deg
Mean motion:   15
53820684  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             548
Checksum:              318


Coasting Arc #20 (Orbit 562)
---------------------------------------

Vector Time (GMT): 2018/213/23:22:30
000
Vector Time (MET): N/A
Weight (LBS)     : 944337
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         298275
93                 A    =         6779226
04  meter
 Y    =        4478658
98  meter          E    =           
0013648
 Z    =       -5091974
34                 I    =           51
81160
 XDOT =      -7008
901465                 Wp   =           86
98697
 YDOT =       2506
974625  meter/sec      RA   =          149
35795  deg
 ZDOT =       1799
309051                 TA   =          200
37912
                                          MA   =          200
43363
                                          Ha   =            222
152  n
mi
                                          Hp   =            214
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         978595
57                 X    =          272905
95
 Y    =       14693763
06  feet           Y    =         4481852
72  meter
 Z    =      -16705952
55                 Z    =        -5090587
00
 XDOT =     -22995
083548                 XDOT =       -7045
154209
 YDOT =       8224
982366  feet/sec       YDOT =        2428
393521  meter/sec
 ZDOT =       5903
244918                 ZDOT =        1765
174682

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12141205
95                 X    =        -3700639
57
 Y    =        8345483
47  feet           Y    =         2543703
36  meter
 Z    =      -16700215
46                 Z    =        -5090225
67
 XDOT =     -18104
136314                 XDOT =       -5518
140749
 YDOT =     -14864
142963  feet/sec       YDOT =       -4530
590775  meter/sec
 ZDOT =       5749
857699                 ZDOT =        1752
556627


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   18213
98701957  
00016717  00000-0  10270-3 0  9198
2 25544  51
6390 150
4456 0003902  10
2739 349
8492 15
53834562  5632


Satellite: ISS
Catalog Number: 25544
Epoch time:      18213
98701957   =   yrday
fracday
Element set:     919
Inclination:       51
6390  deg
RA of node:       150
4456  deg
Eccentricity:     
0003902     
Arg of perigee:    10
2739  deg
Mean anomaly:     349
8492  deg
Mean motion:   15
53834562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             563
Checksum:              324
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