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

 
Date: June 10th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


159/13:01:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 214 3

164/10:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 1
000/00:00:00 000 0 0 0 0 214 7

172/07:16:17 060 0 9 1 0 1 0
N/A 0 1 -0 1 220 4
000/00:02:34 120 0 3 -0 0 215 9

Coasting Arc #1 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2018/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907993
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2426941
58                 A    =         6778437
92  meter
 Y    =       -3814477
21  meter          E    =           
0013333
 Z    =       -5061977
21                 I    =           51
96105
 XDOT =       4813
523706                 Wp   =           89
11773
 YDOT =       5632
039883  meter/sec      RA   =           61
30499  deg
 ZDOT =      -1940
433145                 TA   =          162
14027
                                          MA   =          162
09337
                                          Ha   =            221
500  n
mi
                                          Hp   =            214
329

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7962406
74                 X    =         2494004
32
 Y    =      -12514689
02  feet           Y    =        -3786962
08  meter
 Z    =      -16607536
77                 Z    =        -5050025
32
 XDOT =      15792
400609                 XDOT =        4759
612609
 YDOT =      18477
821139  feet/sec       YDOT =        5685
566752  meter/sec
 ZDOT =      -6366
250475                 ZDOT =       -1917
181010

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10181433
59                 X    =        -3103300
96
 Y    =      -10869647
36  feet           Y    =        -3313068
52  meter
 Z    =      -16553453
30                 Z    =        -5045492
57
 XDOT =      20976
459670                 XDOT =        6393
624908
 YDOT =     -10131
387058  feet/sec       YDOT =       -3088
046775  meter/sec
 ZDOT =      -6263
037406                 ZDOT =       -1908
973801


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   18159
51941492  
00016717  00000-0  10270-3 0  9006
2 25544  51
6421  61
9290 0003129 166
3168 193
8070 15
54170133 37169


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
51941492   =   yrday
fracday
Element set:     900
Inclination:       51
6421  deg
RA of node:        61
9290  deg
Eccentricity:     
0003129     
Arg of perigee:   166
3168  deg
Mean anomaly:     193
8070  deg
Mean motion:   15
54170133  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              299


Coasting Arc #2 (Orbit 3716)
---------------------------------------

Vector Time (GMT): 2018/159/13:01:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4899799
60                 A    =         6781871
74  meter
 Y    =       -2101188
46  meter          E    =           
0010710
 Z    =        4182283
63                 I    =           51
97199
 XDOT =       -343
191798                 Wp   =           91
96842
 YDOT =      -6684
176500  meter/sec      RA   =           61
05533  deg
 ZDOT =      -3752
312252                 TA   =           36
44389
                                          MA   =           36
37103
                                          Ha   =            221
572  n
mi
                                          Hp   =            214
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16075458
02                 X    =        -4896254
85
 Y    =       -6893662
92  feet           Y    =        -2155961
93  meter
 Z    =       13721402
98                 Z    =         4158490
36
 XDOT =      -1125
957344                 XDOT =        -250
195114
 YDOT =     -21929
712926  feet/sec       YDOT =       -6687
494011  meter/sec
 ZDOT =     -12310
735736                 ZDOT =       -3753
754067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6541347
65                 X    =        -1993802
76
 Y    =       16311230
46  feet           Y    =         4971663
04  meter
 Z    =       13615225
68                 Z    =         4149920
79
 XDOT =     -20713
550548                 XDOT =       -6313
490207
 YDOT =       1995
468810  feet/sec       YDOT =         608
218893  meter/sec
 ZDOT =     -12316
161919                 ZDOT =       -3753
966153


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   18159
58371548  
00016717  00000-0  10270-3 0  9013
2 25544  51
6423  61
6091 0003038 167
5854 192
5374 15
54177604 37175


Satellite: ISS
Catalog Number: 25544
Epoch time:      18159
58371548   =   yrday
fracday
Element set:     901
Inclination:       51
6423  deg
RA of node:        61
6091  deg
Eccentricity:     
0003038     
Arg of perigee:   167
5854  deg
Mean anomaly:     192
5374  deg
Mean motion:   15
54177604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3717
Checksum:              322


Coasting Arc #3 (Orbit 3731)
---------------------------------------

Vector Time (GMT): 2018/160/13:01:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5067194
88                 A    =         6785725
05  meter
 Y    =        3447613
91  meter          E    =           
0004678
 Z    =       -2917837
98                 I    =           51
96752
 XDOT =       -952
352199                 Wp   =          101
47699
 YDOT =       5675
523303  meter/sec      RA   =           56
09381  deg
 ZDOT =       5058
061088                 TA   =          225
44802
                                          MA   =          225
48623
                                          Ha   =            221
406  n
mi
                                          Hp   =            214
474

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16624655
13                 X    =         5042439
58
 Y    =       11311069
26  feet           Y    =         3504140
64  meter
 Z    =       -9572959
24                 Z    =        -2893282
84
 XDOT =      -3124
515088                 XDOT =       -1040
316319
 YDOT =      18620
483276  feet/sec       YDOT =        5664
381129  meter/sec
 ZDOT =      16594
688609                 ZDOT =        5053
221727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10653960
06                 X    =         3247327
03
 Y    =      -17114164
07  feet           Y    =        -5216397
21  meter
 Z    =       -9463589
06                 Z    =        -2884501
95
 XDOT =      17485
349381                 XDOT =        5329
534491
 YDOT =       1732
070680  feet/sec       YDOT =         527
935143  meter/sec
 ZDOT =      16572
143881                 ZDOT =        5051
189455


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   18160
54823249  
00016717  00000-0  10270-3 0  9022
2 25544  51
6420  56
8007 0003022 171
6684 188
4520 15
54154455 37328


Satellite: ISS
Catalog Number: 25544
Epoch time:      18160
54823249   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:        56
8007  deg
Eccentricity:     
0003022     
Arg of perigee:   171
6684  deg
Mean anomaly:     188
4520  deg
Mean motion:   15
54154455  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3732
Checksum:              294


Coasting Arc #4 (Orbit 3747)
---------------------------------------

Vector Time (GMT): 2018/161/13:01:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4925192
48                 A    =         6788640
86  meter
 Y    =       -4468989
64  meter          E    =           
0015892
 Z    =        1318155
27                 I    =           51
95772
 XDOT =       2374
316463                 Wp   =          129
84992
 YDOT =      -4354
221691  meter/sec      RA   =           51
14174  deg
 ZDOT =      -5854
122501                 TA   =           35
85791
                                          MA   =           35
75134
                                          Ha   =            221
477  n
mi
                                          Hp   =            214
497

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16158767
97                 X    =        -4881255
94
 Y    =      -14662039
51  feet           Y    =        -4523821
02  meter
 Z    =        4324656
39                 Z    =         1294336
30
 XDOT =       7789
752174                 XDOT =        2451
266696
 YDOT =     -14285
504235  feet/sec       YDOT =       -4327
239541  meter/sec
 ZDOT =     -19206
438650                 ZDOT =       -5842
402330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13732164
77                 X    =        -4185563
82
 Y    =       16982744
45  feet           Y    =         5176340
51  meter
 Z    =        4218753
30                 Z    =         1285876
00
 XDOT =     -13469
583062                 XDOT =       -4105
528917
 YDOT =      -6102
837617  feet/sec       YDOT =       -1860
144906  meter/sec
 ZDOT =     -19153
293549                 ZDOT =       -5837
923874


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   18161
57705007  
00016717  00000-0  10270-3 0  9038
2 25544  51
6420  51
6727 0003205 174
4355 185
6834 15
54125669 37488


Satellite: ISS
Catalog Number: 25544
Epoch time:      18161
57705007   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:        51
6727  deg
Eccentricity:     
0003205     
Arg of perigee:   174
4355  deg
Mean anomaly:     185
6834  deg
Mean motion:   15
54125669  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3748
Checksum:              310


Coasting Arc #5 (Orbit 3763)
---------------------------------------

Vector Time (GMT): 2018/162/13:01:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4465518
35                 A    =         6789092
09  meter
 Y    =        5093640
75  meter          E    =           
0011009
 Z    =         387563
25                 I    =           51
93880
 XDOT =      -3791
792315                 Wp   =           61
02580
 YDOT =       2856
726159  meter/sec      RA   =           46
19179  deg
 ZDOT =       6020
311779                 TA   =          303
13452
                                          MA   =          303
24012
                                          Ha   =            221
192  n
mi
                                          Hp   =            214
534

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14650650
74                 X    =         4406345
37
 Y    =       16711419
78  feet           Y    =         5143246
34  meter
 Z    =        1271532
97                 Z    =          409112
44
 XDOT =     -12440
263500                 XDOT =       -3852
699088
 YDOT =       9372
461151  feet/sec       YDOT =        2813
982369  meter/sec
 ZDOT =      19751
679064                 ZDOT =        6001
744762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15595398
69                 X    =         4753477
52
 Y    =      -15825432
54  feet           Y    =        -4823591
84  meter
 Z    =        1367164
57                 Z    =          416711
76
 XDOT =       9114
703441                 XDOT =        2778
161609
 YDOT =      10713
950675  feet/sec       YDOT =        3265
612166  meter/sec
 ZDOT =      19668
120680                 ZDOT =        5994
843183


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   18162
60586087  
00016717  00000-0  10270-3 0  9049
2 25544  51
6424  46
5434 0003050 182
1638 177
9502 15
54184764 37643


Satellite: ISS
Catalog Number: 25544
Epoch time:      18162
60586087   =   yrday
fracday
Element set:     904
Inclination:       51
6424  deg
RA of node:        46
5434  deg
Eccentricity:     
0003050     
Arg of perigee:   182
1638  deg
Mean anomaly:     177
9502  deg
Mean motion:   15
54184764  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3764
Checksum:              316


Coasting Arc #6 (Orbit 3778)
---------------------------------------

Vector Time (GMT): 2018/163/13:01:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3615699
14                 A    =         6787411
67  meter
 Y    =       -5346355
23  meter          E    =           
0008754
 Z    =       -2088080
09                 I    =           51
90836
 XDOT =       5122
206194                 Wp   =          153
22174
 YDOT =      -1300
841199  meter/sec      RA   =           41
23930  deg
 ZDOT =      -5555
512905                 TA   =           49
80191
                                          MA   =           49
72532
                                          Ha   =            221
160  n
mi
                                          Hp   =            214
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11862529
98                 X    =        -3545503
09
 Y    =      -17540535
54  feet           Y    =        -5386395
65  meter
 Z    =       -6850656
46                 Z    =        -2105474
46
 XDOT =      16805
138432                 XDOT =        5163
357938
 YDOT =      -4267
851703  feet/sec       YDOT =       -1243
330194  meter/sec
 ZDOT =     -18226
748377                 ZDOT =       -5530
530951

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16402183
91                 X    =        -4999385
66
 Y    =       13352815
28  feet           Y    =         4069938
10  meter
 Z    =       -6927639
25                 Z    =        -2111544
44
 XDOT =      -4806
764002                 XDOT =       -1465
101668
 YDOT =     -15274
649915  feet/sec       YDOT =       -4655
713294  meter/sec
 ZDOT =     -18114
726332                 ZDOT =       -5521
368586


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   18163
57037175  
00016717  00000-0  10270-3 0  9056
2 25544  51
6416  41
7351 0003058 186
4750 173
6364 15
54136723 37796


Satellite: ISS
Catalog Number: 25544
Epoch time:      18163
57037175   =   yrday
fracday
Element set:     905
Inclination:       51
6416  deg
RA of node:        41
7351  deg
Eccentricity:     
0003058     
Arg of perigee:   186
4750  deg
Mean anomaly:     173
6364  deg
Mean motion:   15
54136723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3779
Checksum:              316


Coasting Arc #7 (Orbit 3792)
---------------------------------------

Vector Time (GMT): 2018/164/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3026566
66                 A    =         6777329
69  meter
 Y    =       -2948016
94  meter          E    =           
0014837
 Z    =       -5311820
32                 I    =           51
85222
 XDOT =       5835
387236                 Wp   =          106
04251
 YDOT =       4923
719508  meter/sec      RA   =           36
67908  deg
 ZDOT =        589
633583                 TA   =          169
59164
                                          MA   =          169
56089
                                          Ha   =            221
085  n
mi
                                          Hp   =            214
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9929680
64                 X    =         3085109
49
 Y    =       -9671971
60  feet           Y    =        -2913843
53  meter
 Z    =      -17427232
02                 Z    =        -5296976
50
 XDOT =      19144
971246                 XDOT =        5777
031004
 YDOT =      16153
935393  feet/sec       YDOT =        4988
648434  meter/sec
 ZDOT =       1934
493384                 ZDOT =         617
839241

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4483143
19                 X    =        -1366462
04
 Y    =      -13205112
44  feet           Y    =        -4024918
27  meter
 Z    =      -17360312
23                 Z    =        -5291423
17
 XDOT =      21793
859430                 XDOT =        6642
768354
 YDOT =     -10118
512447  feet/sec       YDOT =       -3084
122594  meter/sec
 ZDOT =       2059
923852                 ZDOT =         627
864790


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   18164
47057994  
00016717  00000-0  10270-3 0  9068
2 25544  51
6420  37
2480 0002976 187
5366 172
5742 15
54182980 37937


Satellite: ISS
Catalog Number: 25544
Epoch time:      18164
47057994   =   yrday
fracday
Element set:     906
Inclination:       51
6420  deg
RA of node:        37
2480  deg
Eccentricity:     
0002976     
Arg of perigee:   187
5366  deg
Mean anomaly:     172
5742  deg
Mean motion:   15
54182980  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3793
Checksum:              339


Coasting Arc #8 (Orbit 3808)
---------------------------------------

Vector Time (GMT): 2018/165/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4378926
42                 A    =         6779178
07  meter
 Y    =        1780786
22  meter          E    =           
0005540
 Z    =        4854687
07                 I    =           51
83200
 XDOT =      -4924
117615                 Wp   =           82
08566
 YDOT =      -5333
456117  meter/sec      RA   =           31
69504  deg
 ZDOT =      -2481
983134                 TA   =           32
23099
                                          MA   =           32
19715
                                          Ha   =            221
020  n
mi
                                          Hp   =            214
744

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14366556
51                 X    =        -4422095
78
 Y    =        5842474
47  feet           Y    =         1731575
77  meter
 Z    =       15927451
02                 Z    =         4833311
18
 XDOT =     -16155
241518                 XDOT =       -4852
055280
 YDOT =     -17498
215608  feet/sec       YDOT =       -5388
117607  meter/sec
 ZDOT =      -8142
989285                 ZDOT =       -2505
728822

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -597371
75                 X    =         -182078
91
 Y    =       15595621
24  feet           Y    =         4753545
35  meter
 Z    =       15831484
30                 Z    =         4825436
41
 XDOT =     -21421
715475                 XDOT =       -6529
338877
 YDOT =       7563
192540  feet/sec       YDOT =        2305
261086  meter/sec
 ZDOT =      -8248
384176                 ZDOT =       -2514
107497


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   18165
49938532  
00016717  00000-0  10270-3 0  9078
2 25544  51
6424  32
1195 0002937 195
0575 165
0491 15
54217941 38093


Satellite: ISS
Catalog Number: 25544
Epoch time:      18165
49938532   =   yrday
fracday
Element set:     907
Inclination:       51
6424  deg
RA of node:        32
1195  deg
Eccentricity:     
0002937     
Arg of perigee:   195
0575  deg
Mean anomaly:     165
0491  deg
Mean motion:   15
54217941  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3809
Checksum:              325


Coasting Arc #9 (Orbit 3823)
---------------------------------------

Vector Time (GMT): 2018/166/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5513774
86                 A    =         6782861
52  meter
 Y    =        -661236
60  meter          E    =           
0006811
 Z    =       -3902671
79                 I    =           51
81489
 XDOT =       3553
731744                 Wp   =          129
68224
 YDOT =       5403
681687  meter/sec      RA   =           26
71589  deg
 ZDOT =       4105
753223                 TA   =          183
30444
                                          MA   =          183
30894
                                          Ha   =            220
886  n
mi
                                          Hp   =            214
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18089812
53                 X    =         5539716
25
 Y    =       -2169411
41  feet           Y    =         -599432
01  meter
 Z    =      -12804041
30                 Z    =        -3875824
98
 XDOT =      11659
224883                 XDOT =        3473
098660
 YDOT =      17728
614460  feet/sec       YDOT =        5442
970367  meter/sec
 ZDOT =      13470
318973                 ZDOT =        4122
821109

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5163763
23                 X    =         1573915
03
 Y    =      -17559857
52  feet           Y    =        -5352244
57  meter
 Z    =      -12683772
71                 Z    =        -3866013
92
 XDOT =      19573
142455                 XDOT =        5965
893820
 YDOT =      -4027
305878  feet/sec       YDOT =       -1227
522832  meter/sec
 ZDOT =      13545
810171                 ZDOT =        4128
762940


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   18166
46388993  
00016717  00000-0  10270-3 0  9087
2 25544  51
6420  27
3105 0002885 198
2187 161
8863 15
54176032 38241


Satellite: ISS
Catalog Number: 25544
Epoch time:      18166
46388993   =   yrday
fracday
Element set:     908
Inclination:       51
6420  deg
RA of node:        27
3105  deg
Eccentricity:     
0002885     
Arg of perigee:   198
2187  deg
Mean anomaly:     161
8863  deg
Mean motion:   15
54176032  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3824
Checksum:              332


Coasting Arc #10 (Orbit 3839)
---------------------------------------

Vector Time (GMT): 2018/167/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6283400
48                 A    =         6786585
22  meter
 Y    =        -373983
82  meter          E    =           
0013832
 Z    =        2516577
16                 I    =           51
79673
 XDOT =      -1822
887838                 Wp   =          116
20141
 YDOT =      -5227
747540  meter/sec      RA   =           21
74600  deg
 ZDOT =      -5311
654247                 TA   =           35
60740
                                          MA   =           35
51519
                                          Ha   =            220
948  n
mi
                                          Hp   =            214
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20614830
97                 X    =        -6290975
60
 Y    =       -1226981
03  feet           Y    =         -444291
90  meter
 Z    =        8256486
76                 Z    =         2486036
36
 XDOT =      -5980
603144                 XDOT =       -1738
493248
 YDOT =     -17151
402691  feet/sec       YDOT =       -5247
659561  meter/sec
 ZDOT =     -17426
687162                 ZDOT =       -5320
305030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8948769
73                 X    =        -2727585
01
 Y    =       18671736
21  feet           Y    =         5691145
20  meter
 Z    =        8119858
30                 Z    =         2474932
81
 XDOT =     -16735
562636                 XDOT =       -5100
999491
 YDOT =       -401
826793  feet/sec       YDOT =        -122
476807  meter/sec
 ZDOT =     -17464
533284                 ZDOT =       -5323
189745


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   18167
49269290  
00016717  00000-0  10270-3 0  9090
2 25544  51
6413  22
1816 0002799 198
6894 161
4156 15
54179400 38409


Satellite: ISS
Catalog Number: 25544
Epoch time:      18167
49269290   =   yrday
fracday
Element set:     909
Inclination:       51
6413  deg
RA of node:        22
1816  deg
Eccentricity:     
0002799     
Arg of perigee:   198
6894  deg
Mean anomaly:     161
4156  deg
Mean motion:   15
54179400  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3840
Checksum:              333


Coasting Arc #11 (Orbit 3854)
---------------------------------------

Vector Time (GMT): 2018/168/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6608078
95                 A    =         6788847
28  meter
 Y    =        1261110
73  meter          E    =           
0007383
 Z    =        -889418
46                 I    =           51
77335
 XDOT =       -130
289164                 Wp   =           44
13718
 YDOT =       4846
196972  meter/sec      RA   =           16
78214  deg
 ZDOT =       5938
247141                 TA   =          306
25833
                                          MA   =          306
32653
                                          Ha   =            220
736  n
mi
                                          Hp   =            214
996

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21680049
05                 X    =         6597806
02
 Y    =        4137502
38  feet           Y    =         1334949
51  meter
 Z    =       -2918039
58                 Z    =         -857343
80
 XDOT =       -427
457887                 XDOT =        -213
315554
 YDOT =      15899
596366  feet/sec       YDOT =        4844
274905  meter/sec
 ZDOT =      19482
438128                 ZDOT =        5937
413292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11712590
20                 X    =         3569997
49
 Y    =      -18728980
01  feet           Y    =        -5708593
11  meter
 Z    =       -2774697
54                 Z    =         -845727
81
 XDOT =      13255
221569                 XDOT =        4040
191534
 YDOT =       5421
593556  feet/sec       YDOT =        1652
501716  meter/sec
 ZDOT =      19477
898361                 ZDOT =        5936
863420


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   18168
45719316  
00016717  00000-0  10270-3 0  9108
2 25544  51
6412  17
3728 0002890 205
9370 154
1638 15
54188349 38551


Satellite: ISS
Catalog Number: 25544
Epoch time:      18168
45719316   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:        17
3728  deg
Eccentricity:     
0002890     
Arg of perigee:   205
9370  deg
Mean anomaly:     154
1638  deg
Mean motion:   15
54188349  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3855
Checksum:              323


Coasting Arc #12 (Orbit 3870)
---------------------------------------

Vector Time (GMT): 2018/169/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6412316
62                 A    =         6788907
16  meter
 Y    =       -2035609
42  meter          E    =           
0011387
 Z    =        -861047
48                 I    =           51
74182
 XDOT =       2168
972901                 Wp   =          154
65866
 YDOT =      -4334
750853  meter/sec      RA   =           11
81972  deg
 ZDOT =      -5943
834270                 TA   =           34
64538
                                          MA   =           34
57125
                                          Ha   =            220
645  n
mi
                                          Hp   =            215
136

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21037784
18                 X    =        -6384894
83
 Y    =       -6678508
60  feet           Y    =        -2107162
94  meter
 Z    =       -2824958
91                 Z    =         -892129
61
 XDOT =       7116
052826                 XDOT =        2246
155786
 YDOT =     -14221
623534  feet/sec       YDOT =       -4310
063634  meter/sec
 ZDOT =     -19500
768604                 ZDOT =       -5933
111317

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13537874
25                 X    =        -4126344
07
 Y    =       17410156
04  feet           Y    =         5306615
56  meter
 Z    =       -2963724
08                 Z    =         -903343
10
 XDOT =      -9568
853442                 XDOT =       -2916
586529
 YDOT =     -10731
112709  feet/sec       YDOT =       -3270
843154  meter/sec
 ZDOT =     -19452
058392                 ZDOT =       -5928
987398


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   18169
48599189  
00016717  00000-0  10270-3 0  9117
2 25544  51
6416  12
2434 0002979 210
7960 149
3019 15
54154608 38718


Satellite: ISS
Catalog Number: 25544
Epoch time:      18169
48599189   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:        12
2434  deg
Eccentricity:     
0002979     
Arg of perigee:   210
7960  deg
Mean anomaly:     149
3019  deg
Mean motion:   15
54154608  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3871
Checksum:              329


Coasting Arc #13 (Orbit 3886)
---------------------------------------

Vector Time (GMT): 2018/170/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5716611
40                 A    =         6786419
78  meter
 Y    =        2667578
04  meter          E    =           
0011632
 Z    =        2490152
02                 I    =           51
70012
 XDOT =      -4069
679724                 Wp   =           84
51435
 YDOT =       3739
732915  meter/sec      RA   =            6
85113  deg
 ZDOT =       5316
247136                 TA   =          303
38119
                                          MA   =          303
49244
                                          Ha   =            220
491  n
mi
                                          Hp   =            215
096

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18755286
74                 X    =         5674261
19
 Y    =        8751896
45  feet           Y    =         2731268
08  meter
 Z    =        8169790
08                 Z    =         2517818
52
 XDOT =     -13351
967600                 XDOT =       -4137
019291
 YDOT =      12269
464945  feet/sec       YDOT =        3693
845893  meter/sec
 ZDOT =      17441
755694                 ZDOT =        5296
315025

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14429851
73                 X    =         4398218
81
 Y    =      -14768373
87  feet           Y    =        -4501400
35  meter
 Z    =        8293157
09                 Z    =         2527754
28
 XDOT =       6066
484335                 XDOT =        1849
064425
 YDOT =      15708
176390  feet/sec       YDOT =        4787
852164  meter/sec
 ZDOT =      17351
937150                 ZDOT =        5288
870443


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   18170
51478726  
00016717  00000-0  10270-3 0  9127
2 25544  51
6403   7
1136 0002884 215
7162 144
3798 15
54198346 38873


Satellite: ISS
Catalog Number: 25544
Epoch time:      18170
51478726   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:         7
1136  deg
Eccentricity:     
0002884     
Arg of perigee:   215
7162  deg
Mean anomaly:     144
3798  deg
Mean motion:   15
54198346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3887
Checksum:              324


Coasting Arc #14 (Orbit 3901)
---------------------------------------

Vector Time (GMT): 2018/171/10:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923033
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4539602
97                 A    =         6782692
04  meter
 Y    =       -3219690
42  meter          E    =           
0004420
 Z    =       -3880391
55                 I    =           51
65384
 XDOT =       5690
419137                 Wp   =           95
35255
 YDOT =      -3070
205248  meter/sec      RA   =            1
87262  deg
 ZDOT =      -4114
110670                 TA   =          131
47109
                                          MA   =          131
43313
                                          Ha   =            220
422  n
mi
                                          Hp   =            215
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14893710
54                 X    =        -4484413
31
 Y    =      -10563288
77  feet           Y    =        -3270146
45  meter
 Z    =      -12730943
42                 Z    =        -3902309
52
 XDOT =      18669
354123                 XDOT =        5744
312175
 YDOT =     -10072
851864  feet/sec       YDOT =       -3006
269346  meter/sec
 ZDOT =     -13497
738417                 ZDOT =       -4086
338101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14674145
36                 X    =        -4472679
51
 Y    =       10750905
83  feet           Y    =         3276876
10  meter
 Z    =      -12828487
25                 Z    =        -3910122
92
 XDOT =      -2901
827845                 XDOT =        -884
477127
 YDOT =     -19900
759105  feet/sec       YDOT =       -6065
751375  meter/sec
 ZDOT =     -13372
954341                 ZDOT =       -4076
076483


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   18171
47928338  
00016717  00000-0  10270-3 0  9133
2 25544  51
6394   2
3056 0002927 219
8389 140
2549 15
54182358 39027


Satellite: ISS
Catalog Number: 25544
Epoch time:      18171
47928338   =   yrday
fracday
Element set:     913
Inclination:       51
6394  deg
RA of node:         2
3056  deg
Eccentricity:     
0002927     
Arg of perigee:   219
8389  deg
Mean anomaly:     140
2549  deg
Mean motion:   15
54182358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3902
Checksum:              324


Coasting Arc #15 (Orbit 3914)
---------------------------------------

Vector Time (GMT): 2018/172/07:17:34
120
Vector Time (MET): N/A
Weight (LBS)     : 922932
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2842858
39                 A    =         6780113
22  meter
 Y    =       -3901050
93  meter          E    =           
0009544
 Z    =       -4770417
84                 I    =           51
61824
 XDOT =       6951
572465                 Wp   =          123
97007
 YDOT =       1814
947944  meter/sec      RA   =          357
59869  deg
 ZDOT =       2657
100256                 TA   =          172
30070
                                          MA   =          172
28604
                                          Ha   =            220
411  n
mi
                                          Hp   =            215
864

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9326963
22                 X    =         2909441
86
 Y    =      -12798723
52  feet           Y    =        -3868887
40  meter
 Z    =      -15650977
16                 Z    =        -4756446
88
 XDOT =      22806
996277                 XDOT =        6917
853797
 YDOT =       5954
553622  feet/sec       YDOT =        1892
496445  meter/sec
 ZDOT =       8717
520524                 ZDOT =        2690
786799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5024204
80                 X    =         1531377
62
 Y    =      -15084095
12  feet           Y    =        -4597632
19  meter
 Z    =      -15587818
74                 Z    =        -4751167
15
 XDOT =      22376
632790                 XDOT =        6820
397674
 YDOT =      -1715
635478  feet/sec       YDOT =        -522
925694  meter/sec
 ZDOT =       8867
948857                 ZDOT =        2702
950811


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   18172
31517934  
00016717  00000-0  10270-3 0  9144
2 25544  51
6424 358
1392 0003189 235
2016 124
8837 15
54012376 39150


Satellite: ISS
Catalog Number: 25544
Epoch time:      18172
31517934   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       358
1392  deg
Eccentricity:     
0003189     
Arg of perigee:   235
2016  deg
Mean anomaly:     124
8837  deg
Mean motion:   15
54012376  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3915
Checksum:              308


Coasting Arc #16 (Orbit 3930)
---------------------------------------

Vector Time (GMT): 2018/173/07:17:34
120
Vector Time (MET): N/A
Weight (LBS)     : 922932
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4323328
98                 A    =         6783643
51  meter
 Y    =        3591046
10  meter          E    =           
0008934
 Z    =        3790926
98                 I    =           51
59683
 XDOT =      -5860
381816                 Wp   =           91
22660
 YDOT =      -2603
737831  meter/sec      RA   =          352
60823  deg
 ZDOT =      -4208
576992                 TA   =           43
24707
                                          MA   =           43
17697
                                          Ha   =            220
451  n
mi
                                          Hp   =            215
788

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14184150
21                 X    =        -4381578
08
 Y    =       11781647
30  feet           Y    =         3542373
59  meter
 Z    =       12437424
47                 Z    =         3769784
59
 XDOT =     -19226
974462                 XDOT =       -5810
387475
 YDOT =      -8542
446953  feet/sec       YDOT =       -2668
992711  meter/sec
 ZDOT =     -13807
667295                 ZDOT =       -4236
923567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9668125
86                 X    =        -2946844
76
 Y    =       15776038
93  feet           Y    =         4808536
67  meter
 Z    =       12342236
26                 Z    =         3761913
61
 XDOT =     -19721
885286                 XDOT =       -6011
230635
 YDOT =      -1163
397409  feet/sec       YDOT =        -354
603530  meter/sec
 ZDOT =     -13934
062272                 ZDOT =       -4247
102181


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   18173
34409082  
00016717  00000-0  10270-3 0  9153
2 25544  51
6421 353
0115 0003013 238
8134 121
2723 15
54018920 39314


Satellite: ISS
Catalog Number: 25544
Epoch time:      18173
34409082   =   yrday
fracday
Element set:     915
Inclination:       51
6421  deg
RA of node:       353
0115  deg
Eccentricity:     
0003013     
Arg of perigee:   238
8134  deg
Mean anomaly:     121
2723  deg
Mean motion:   15
54018920  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3931
Checksum:              271


Coasting Arc #17 (Orbit 3945)
---------------------------------------

Vector Time (GMT): 2018/174/07:17:34
120
Vector Time (MET): N/A
Weight (LBS)     : 922932
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5465350
20                 A    =         6787154
63  meter
 Y    =       -3189689
71  meter          E    =           
0002683
 Z    =       -2450911
82                 I    =           51
57574
 XDOT =       4355
931736                 Wp   =           27
13052
 YDOT =       3372
339643  meter/sec      RA   =          347
62456  deg
 ZDOT =       5329
177564                 TA   =          305
41740
                                          MA   =          305
44245
                                          Ha   =            220
264  n
mi
                                          Hp   =            215
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17930938
98                 X    =         5512517
27
 Y    =      -10464861
25  feet           Y    =        -3128308
39  meter
 Z    =       -8041049
28                 Z    =        -2424248
75
 XDOT =      14291
114620                 XDOT =        4292
011150
 YDOT =      11064
106441  feet/sec       YDOT =        3420
692674  meter/sec
 ZDOT =      17484
178361                 ZDOT =        5350
182370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13339236
72                 X    =         4065799
35
 Y    =      -15969006
44  feet           Y    =        -4867353
16  meter
 Z    =       -7921235
04                 Z    =        -2414392
44
 XDOT =      15933
511559                 XDOT =        4856
534323
 YDOT =       4598
095666  feet/sec       YDOT =        1401
499559  meter/sec
 ZDOT =      17577
591964                 ZDOT =        5357
650031


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   18174
30869337  
00016717  00000-0  10270-3 0  9164
2 25544  51
6417 348
2037 0003138 243
6039 116
4792 15
54025443 39460


Satellite: ISS
Catalog Number: 25544
Epoch time:      18174
30869337   =   yrday
fracday
Element set:     916
Inclination:       51
6417  deg
RA of node:       348
2037  deg
Eccentricity:     
0003138     
Arg of perigee:   243
6039  deg
Mean anomaly:     116
4792  deg
Mean motion:   15
54025443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3946
Checksum:              318
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