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

 
Date: August 6th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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


219/05:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 0
000/00:00:00 000 0 0 0 0 212 3

221/12:26:03 547 -0 5 0 8 0 8
N/A 0 6 -0 1 222 8
000/00:02:03 094 0 0 -0 0 213 0

225/16:27:14 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 213 2

225/21:12:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 7
000/00:00:00 000 0 0 0 0 213 3

Coasting Arc #1 (Orbit 2925)
---------------------------------------

Vector Time (GMT): 2017/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3249128
92                 A    =         6777860
83  meter
 Y    =        3006534
65  meter          E    =           
0019242
 Z    =       -5149497
59                 I    =           51
76689
 XDOT =      -6272
675962                 Wp   =           85
33510
 YDOT =       4095
817239  meter/sec      RA   =          156
36077  deg
 ZDOT =      -1569
996891                 TA   =          169
54798
                                          MA   =          169
50792
                                          Ha   =            223
007  n
mi
                                          Hp   =            212
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10659871
80                 X    =         3240280
95
 Y    =        9863958
84  feet           Y    =         3042819
46  meter
 Z    =      -16894677
14                 Z    =        -5133735
87
 XDOT =     -20579
645544                 XDOT =       -6310
384112
 YDOT =      13437
720599  feet/sec       YDOT =        4025
461169  meter/sec
 ZDOT =      -5150
908435                 ZDOT =       -1600
558511

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          25976
91                 X    =            7917
76
 Y    =      -14603674
37  feet           Y    =        -4451199
95  meter
 Z    =      -16825358
43                 Z    =        -5128369
25
 XDOT =      22709
506416                 XDOT =        6921
857556
 YDOT =       6118
011510  feet/sec       YDOT =        1864
769908  meter/sec
 ZDOT =      -5286
734311                 ZDOT =       -1611
396618


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   17216
51889490  
00016717  00000-0  10270-3 0  9008
2 25544  51
6388 157
3927 0006055 100
9477 259
2357 15
54251671 29260


Satellite: ISS
Catalog Number: 25544
Epoch time:      17216
51889490   =   yrday
fracday
Element set:     900
Inclination:       51
6388  deg
RA of node:       157
3927  deg
Eccentricity:     
0006055     
Arg of perigee:   100
9477  deg
Mean anomaly:     259
2357  deg
Mean motion:   15
54251671  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2926
Checksum:              332


Coasting Arc #2 (Orbit 2941)
---------------------------------------

Vector Time (GMT): 2017/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1604873
28                 A    =         6776950
87  meter
 Y    =       -3884581
01  meter          E    =           
0008222
 Z    =        5309050
35                 I    =           51
79471
 XDOT =       6874
117978                 Wp   =           95
38734
 YDOT =      -3390
830634  meter/sec      RA   =          151
37070  deg
 ZDOT =       -403
278620                 TA   =          358
44520
                                          MA   =          358
44775
                                          Ha   =            222
959  n
mi
                                          Hp   =            212
329

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5265332
27                 X    =        -1587103
91
 Y    =      -12744688
34  feet           Y    =        -3902428
72  meter
 Z    =       17418144
19                 Z    =         5301297
46
 XDOT =      22552
880504                 XDOT =        6913
483143
 YDOT =     -11124
772421  feet/sec       YDOT =       -3313
739450  meter/sec
 ZDOT =      -1323
092584                 ZDOT =        -369
791427

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5570681
23                 X    =        -1697943
64
 Y    =       12660691
80  feet           Y    =         3858978
86  meter
 Z    =       17384387
98                 Z    =         5298761
46
 XDOT =     -22655
814512                 XDOT =       -6905
492263
 YDOT =      -8356
935111  feet/sec       YDOT =       -2547
193822  meter/sec
 ZDOT =      -1174
399149                 ZDOT =        -357
956861


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   17217
54764439  
00016717  00000-0  10270-3 0  9018
2 25544  51
6398 152
2643 0005880 104
2268 255
9538 15
54276939 29426


Satellite: ISS
Catalog Number: 25544
Epoch time:      17217
54764439   =   yrday
fracday
Element set:     901
Inclination:       51
6398  deg
RA of node:       152
2643  deg
Eccentricity:     
0005880     
Arg of perigee:   104
2268  deg
Mean anomaly:     255
9538  deg
Mean motion:   15
54276939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2942
Checksum:              338


Coasting Arc #3 (Orbit 2956)
---------------------------------------

Vector Time (GMT): 2017/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -51681
49                 A    =         6778717
38  meter
 Y    =        4679658
44  meter          E    =           
0018183
 Z    =       -4920931
76                 I    =           51
82883
 XDOT =      -6891
015469                 Wp   =          107
14498
 YDOT =       2377
237600  meter/sec      RA   =          146
38254  deg
 ZDOT =       2334
956778                 TA   =          185
67605
                                          MA   =          185
69669
                                          Ha   =            222
960  n
mi
                                          Hp   =            212
321

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -169558
69                 X    =          -80103
82
 Y    =       15353210
11  feet           Y    =         4678921
79  meter
 Z    =      -16144789
25                 Z    =        -4921251
65
 XDOT =     -22608
318467                 XDOT =       -6928
428071
 YDOT =       7799
335959  feet/sec       YDOT =        2299
968300  meter/sec
 ZDOT =       7660
619352                 ZDOT =        2301
392240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11022416
01                 X    =         3359632
40
 Y    =      -10685913
05  feet           Y    =        -3257066
30  meter
 Z    =      -16146877
06                 Z    =        -4921568
13
 XDOT =      20637
266607                 XDOT =        6290
238862
 YDOT =       9946
058089  feet/sec       YDOT =        3031
558505  meter/sec
 ZDOT =       7511
708282                 ZDOT =        2289
568684


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   17218
51209605  
00016717  00000-0  10270-3 0  9026
2 25544  51
6400 147
4553 0006036 106
9706 253
2108 15
54258585 29573


Satellite: ISS
Catalog Number: 25544
Epoch time:      17218
51209605   =   yrday
fracday
Element set:     902
Inclination:       51
6400  deg
RA of node:       147
4553  deg
Eccentricity:     
0006036     
Arg of perigee:   106
9706  deg
Mean anomaly:     253
2108  deg
Mean motion:   15
54258585  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2957
Checksum:              303


Coasting Arc #4 (Orbit 2968)
---------------------------------------

Vector Time (GMT): 2017/219/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -139006
51                 A    =         6778791
63  meter
 Y    =       -4703162
72  meter          E    =           
0011785
 Z    =        4870215
48                 I    =           51
84904
 XDOT =       6746
719976                 Wp   =           84
04158
 YDOT =      -2730
864611  meter/sec      RA   =          142
70543  deg
 ZDOT =      -2438
379364                 TA   =           29
81736
                                          MA   =           29
75026
                                          Ha   =            222
991  n
mi
                                          Hp   =            212
263

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -456058
09                 X    =         -110060
80
 Y    =      -15430323
88  feet           Y    =        -4704555
48  meter
 Z    =       15978397
23                 Z    =         4869610
41
 XDOT =      22134
908059                 XDOT =        6788
600008
 YDOT =      -8959
529563  feet/sec       YDOT =       -2655
183968  meter/sec
 ZDOT =      -7999
932298                 ZDOT =       -2405
504920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10610052
50                 X    =        -3233944
00
 Y    =      -11215776
97  feet           Y    =        -3418568
82  meter
 Z    =       15976394
93                 Z    =         4869605
17
 XDOT =       9925
721215                 XDOT =        3025
359826
 YDOT =     -20606
575260  feet/sec       YDOT =       -6280
884139  meter/sec
 ZDOT =      -7854
011294                 ZDOT =       -2393
902642


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   17219
28365416  
00016717  00000-0  10270-3 0  9035
2 25544  51
6398 143
6084 0006209 111
1372 249
0445 15
54283249 29690


Satellite: ISS
Catalog Number: 25544
Epoch time:      17219
28365416   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       143
6084  deg
Eccentricity:     
0006209     
Arg of perigee:   111
1372  deg
Mean anomaly:     249
0445  deg
Mean motion:   15
54283249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2969
Checksum:              319


Coasting Arc #5 (Orbit 2983)
---------------------------------------

Vector Time (GMT): 2017/220/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1342141
57                 A    =         6782408
80  meter
 Y    =        5378038
25  meter          E    =           
0012682
 Z    =       -3922311
45                 I    =           51
88734
 XDOT =      -6317
495912                 Wp   =          110
59766
 YDOT =       1403
713888  meter/sec      RA   =          137
72981  deg
 ZDOT =       4092
767808                 TA   =          202
16689
                                          MA   =          202
22177
                                          Ha   =            222
940  n
mi
                                          Hp   =            212
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4403351
62                 X    =        -1383128
20
 Y    =       17644482
44  feet           Y    =         5362800
38  meter
 Z    =      -12868475
89                 Z    =        -3928930
52
 XDOT =     -20726
692626                 XDOT =       -6352
603331
 YDOT =       4605
360525  feet/sec       YDOT =        1332
871016  meter/sec
 ZDOT =      13427
715907                 ZDOT =        4061
994756

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8683846
94                 X    =         2646836
55
 Y    =       15954090
74  feet           Y    =         4862806
86  meter
 Z    =      -12898555
30                 Z    =        -3931479
66
 XDOT =     -11126
755140                 XDOT =       -3391
434967
 YDOT =      16785
233230  feet/sec       YDOT =        5116
139088  meter/sec
 ZDOT =      13291
272658                 ZDOT =        4051
179906


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   17220
24810192  
00016717  00000-0  10270-3 0  9040
2 25544  51
6408 138
8005 0006112 114
4462 245
7329 15
54258952 29844


Satellite: ISS
Catalog Number: 25544
Epoch time:      17220
24810192   =   yrday
fracday
Element set:     904
Inclination:       51
6408  deg
RA of node:       138
8005  deg
Eccentricity:     
0006112     
Arg of perigee:   114
4462  deg
Mean anomaly:     245
7329  deg
Mean motion:   15
54258952  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2984
Checksum:              298


Coasting Arc #6 (Orbit 2999)
---------------------------------------

Vector Time (GMT): 2017/221/05:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902274
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2624615
69                 A    =         6786166
25  meter
 Y    =       -5724665
78  meter          E    =           
0019715
 Z    =        2502004
92                 I    =           51
92276
 XDOT =       5517
327853                 Wp   =          108
44756
 YDOT =        186
862524  meter/sec      RA   =          132
76556  deg
 ZDOT =      -5331
945586                 TA   =           43
58036
                                          MA   =           43
42478
                                          Ha   =            222
871  n
mi
                                          Hp   =            212
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8610943
88                 X    =         2676282
08
 Y    =      -18781711
87  feet           Y    =        -5695026
63  meter
 Z    =        8208677
56                 Z    =         2514879
77
 XDOT =      18101
469334                 XDOT =        5540
727715
 YDOT =        613
066024  feet/sec       YDOT =         248
691829  meter/sec
 ZDOT =     -17493
259795                 ZDOT =       -5305
087816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6652899
96                 X    =        -2027803
91
 Y    =      -19536815
53  feet           Y    =        -5954821
37  meter
 Z    =        8266510
96                 Z    =         2519632
54
 XDOT =      12251
597295                 XDOT =        3734
286856
 YDOT =     -11562
469752  feet/sec       YDOT =       -3524
240781  meter/sec
 ZDOT =     -17374
368721                 ZDOT =       -5295
707586


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   17221
27684191  
00016717  00000-0  10270-3 0  9053
2 25544  51
6400 133
6708 0006125 116
7522 243
4258 15
54291347 30006


Satellite: ISS
Catalog Number: 25544
Epoch time:      17221
27684191   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:       133
6708  deg
Eccentricity:     
0006125     
Arg of perigee:   116
7522  deg
Mean anomaly:     243
4258  deg
Mean motion:   15
54291347  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3000
Checksum:              283


Coasting Arc #7 (Orbit 3003)
---------------------------------------

Vector Time (GMT): 2017/221/12:27:05
094
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2714693
14                 A    =         6777438
54  meter
 Y    =        3229724
20  meter          E    =           
0019680
 Z    =       -5320989
12                 I    =           51
90038
 XDOT =      -5366
408602                 Wp   =          101
43860
 YDOT =       5429
204817  meter/sec      RA   =          131
39590  deg
 ZDOT =        555
484813                 TA   =          173
86505
                                          MA   =          173
84091
                                          Ha   =            222
827  n
mi
                                          Hp   =            212
996

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8906473
57                 X    =         2704222
01
 Y    =       10596208
02  feet           Y    =         3260023
13  meter
 Z    =      -17457313
38                 Z    =        -5307827
71
 XDOT =     -17606
327435                 XDOT =       -5429
418788
 YDOT =      17812
351763  feet/sec       YDOT =        5368
841682  meter/sec
 ZDOT =       1822
456734                 ZDOT =         529
263856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1093833
89                 X    =         -333400
57
 Y    =      -13871677
92  feet           Y    =        -4228087
43  meter
 Z    =      -17399504
75                 Z    =        -5303369
05
 XDOT =      23704
676628                 XDOT =        7225
185436
 YDOT =      -4017
030136  feet/sec       YDOT =       -1224
390786  meter/sec
 ZDOT =       1705
569997                 ZDOT =         519
857735


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   17221
53402815  
00016717  00000-0  10270-3 0  9064
2 25544  51
6422 132
3892 0005374 120
9216 239
2465 15
54132756 30047


Satellite: ISS
Catalog Number: 25544
Epoch time:      17221
53402815   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       132
3892  deg
Eccentricity:     
0005374     
Arg of perigee:   120
9216  deg
Mean anomaly:     239
2465  deg
Mean motion:   15
54132756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3004
Checksum:              285


Coasting Arc #8 (Orbit 3019)
---------------------------------------

Vector Time (GMT): 2017/222/12:27:05
094
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1449279
62                 A    =         6779161
56  meter
 Y    =       -4470752
65  meter          E    =           
0010259
 Z    =        4876958
55                 I    =           51
92649
 XDOT =       5706
218301                 Wp   =           87
20037
 YDOT =      -4516
056059  meter/sec      RA   =          126
41755  deg
 ZDOT =      -2439
302317                 TA   =           26
63747
                                          MA   =           26
58480
                                          Ha   =            222
774  n
mi
                                          Hp   =            212
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4754854
40                 X    =        -1422868
25
 Y    =      -14667823
67  feet           Y    =        -4486811
68  meter
 Z    =       16000520
18                 Z    =         4869982
78
 XDOT =      18721
188653                 XDOT =        5768
142679
 YDOT =     -14816
456887  feet/sec       YDOT =       -4451
899070  meter/sec
 ZDOT =      -8002
960356                 ZDOT =       -2411
433212

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4410352
40                 X    =        -1344275
41
 Y    =       14807742
93  feet           Y    =         4513400
05  meter
 Z    =       15970281
10                 Z    =         4867741
68
 XDOT =     -22795
078809                 XDOT =       -6947
940021
 YDOT =       1725
514031  feet/sec       YDOT =         525
936677  meter/sec
 ZDOT =      -7878
895535                 ZDOT =       -2401
487359


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   17222
56286437  
00016717  00000-0  10270-3 0  9079
2 25544  51
6413 127
2614 0005236 124
7823 235
3824 15
54159986 30203


Satellite: ISS
Catalog Number: 25544
Epoch time:      17222
56286437   =   yrday
fracday
Element set:     907
Inclination:       51
6413  deg
RA of node:       127
2614  deg
Eccentricity:     
0005236     
Arg of perigee:   124
7823  deg
Mean anomaly:     235
3824  deg
Mean motion:   15
54159986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3020
Checksum:              306


Coasting Arc #9 (Orbit 3034)
---------------------------------------

Vector Time (GMT): 2017/223/12:27:05
094
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         258208
49                 A    =         6782696
51  meter
 Y    =        5512337
39  meter          E    =           
0011661
 Z    =       -3956751
34                 I    =           51
95718
 XDOT =      -5664
134733                 Wp   =          116
79131
 YDOT =       3175
413636  meter/sec      RA   =          121
44693  deg
 ZDOT =       4058
286539                 TA   =          195
48619
                                          MA   =          195
52190
                                          Ha   =            222
677  n
mi
                                          Hp   =            213
129

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         847140
72                 X    =          215768
60
 Y    =       18085096
41  feet           Y    =         5514987
41  meter
 Z    =      -12981467
66                 Z    =        -3955600
34
 XDOT =     -18583
119204                 XDOT =       -5718
934995
 YDOT =      10418
023740  feet/sec       YDOT =        3111
767164  meter/sec
 ZDOT =      13314
588382                 ZDOT =        4030
639069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9321252
69                 X    =         2841117
82
 Y    =      -15524623
78  feet           Y    =        -4731905
33  meter
 Z    =      -12977178
70                 Z    =        -3955444
07
 XDOT =      20174
439334                 XDOT =        6149
169109
 YDOT =       1097
262844  feet/sec       YDOT =         334
445715  meter/sec
 ZDOT =      13191
689035                 ZDOT =        4020
826818


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   17223
52739701  
00016717  00000-0  10270-3 0  9084
2 25544  51
6419 122
4532 0005175 129
2285 230
9327 15
54132818 30359


Satellite: ISS
Catalog Number: 25544
Epoch time:      17223
52739701   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:       122
4532  deg
Eccentricity:     
0005175     
Arg of perigee:   129
2285  deg
Mean anomaly:     230
9327  deg
Mean motion:   15
54132818  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3035
Checksum:              297


Coasting Arc #10 (Orbit 3050)
---------------------------------------

Vector Time (GMT): 2017/224/12:27:05
094
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         832762
19                 A    =         6786500
00  meter
 Y    =       -6207465
55  meter          E    =           
0018462
 Z    =        2588332
81                 I    =           51
98587
 XDOT =       5360
562813                 Wp   =          111
36438
 YDOT =      -1494
458132  meter/sec      RA   =          116
48807  deg
 ZDOT =      -5285
141122                 TA   =           39
63759
                                          MA   =           39
50277
                                          Ha   =            222
730  n
mi
                                          Hp   =            213
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2732159
40                 X    =          889541
07
 Y    =      -20365700
62  feet           Y    =        -6197835
47  meter
 Z    =        8491905
55                 Z    =         2592516
21
 XDOT =      17587
148337                 XDOT =        5402
548233
 YDOT =      -4903
077862  feet/sec       YDOT =       -1434
278107  meter/sec
 ZDOT =     -17339
701845                 ZDOT =       -5258
999370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13321642
64                 X    =        -4060436
68
 Y    =       15634246
01  feet           Y    =         4765318
18  meter
 Z    =        8511351
58                 Z    =         2594259
96
 XDOT =     -16381
059860                 XDOT =       -4992
947045
 YDOT =      -4539
214065  feet/sec       YDOT =       -1383
552447  meter/sec
 ZDOT =     -17223
708436                 ZDOT =       -5249
786331


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   17224
55622825  
00016717  00000-0  10270-3 0  9097
2 25544  51
6418 117
3246 0005314 131
9913 228
1693 15
54120679 30511


Satellite: ISS
Catalog Number: 25544
Epoch time:      17224
55622825   =   yrday
fracday
Element set:     909
Inclination:       51
6418  deg
RA of node:       117
3246  deg
Eccentricity:     
0005314     
Arg of perigee:   131
9913  deg
Mean anomaly:     228
1693  deg
Mean motion:   15
54120679  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3051
Checksum:              302


Coasting Arc #11 (Orbit 3065)
---------------------------------------

Vector Time (GMT): 2017/225/12:27:05
094
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1728992
50                 A    =         6788816
00  meter
 Y    =        6488358
84  meter          E    =           
0010412
 Z    =        -990608
75                 I    =           52
00723
 XDOT =      -4831
442772                 Wp   =           68
26982
 YDOT =       -389
281916  meter/sec      RA   =          111
53814  deg
 ZDOT =       5936
624165                 TA   =          281
05790
                                          MA   =          281
17498
                                          Ha   =            222
555  n
mi
                                          Hp   =            213
219

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5672547
58                 X    =        -1796606
68
 Y    =       21287266
55  feet           Y    =         6468645
99  meter
 Z    =       -3250028
71                 Z    =         -999172
02
 XDOT =     -15851
190197                 XDOT =       -4855
567690
 YDOT =      -1277
171639  feet/sec       YDOT =        -443
445122  meter/sec
 ZDOT =      19477
113402                 ZDOT =        5913
096057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16062530
68                 X    =         4895859
35
 Y    =      -15068718
13  feet           Y    =        -4592945
29  meter
 Z    =       -3288927
16                 Z    =        -1002465
00
 XDOT =      11782
249124                 XDOT =        3591
229533
 YDOT =       8368
893273  feet/sec       YDOT =        2550
838670  meter/sec
 ZDOT =      19372
969198                 ZDOT =        5904
881012


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   17225
52075311  
00016717  00000-0  10270-3 0  9109
2 25544  51
6414 112
5160 0005163 136
1416 224
0148 15
54156142 30666


Satellite: ISS
Catalog Number: 25544
Epoch time:      17225
52075311   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       112
5160  deg
Eccentricity:     
0005163     
Arg of perigee:   136
1416  deg
Mean anomaly:     224
0148  deg
Mean motion:   15
54156142  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3066
Checksum:              259


Coasting Arc #12 (Orbit 3068)
---------------------------------------

Vector Time (GMT): 2017/225/16:27:14
000
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3749394
85                 A    =         6787397
50  meter
 Y    =       -5244650
01  meter          E    =           
0011775
 Z    =       -2111601
15                 I    =           52
00021
 XDOT =       2987
957427                 Wp   =          138
06003
 YDOT =       4361
257933  meter/sec      RA   =          110
73444  deg
 ZDOT =      -5553
042293                 TA   =           65
20555
                                          MA   =           65
08311
                                          Ha   =            222
647  n
mi
                                          Hp   =            213
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12301164
20                 X    =         3818020
32
 Y    =      -17206856
97  feet           Y    =        -5202338
07  meter
 Z    =       -6927825
30                 Z    =        -2093221
03
 XDOT =       9803
009932                 XDOT =        2965
940438
 YDOT =      14308
589020  feet/sec       YDOT =        4394
548060  meter/sec
 ZDOT =     -18218
642692                 ZDOT =       -5538
581381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2734545
87                 X    =         -833489
58
 Y    =       21001164
06  feet           Y    =         6401154
81  meter
 Z    =       -6845633
51                 Z    =        -2086549
09
 XDOT =     -13979
405699                 XDOT =       -4260
922857
 YDOT =      -7709
732923  feet/sec       YDOT =       -2349
926595  meter/sec
 ZDOT =     -18155
252345                 ZDOT =       -5533
720915


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   17225
71365766  
00016717  00000-0  10270-3 0  9117
2 25544  51
6372 111
5503 0005300 136
7328 223
4241 15
54156474 30698


Satellite: ISS
Catalog Number: 25544
Epoch time:      17225
71365766   =   yrday
fracday
Element set:     911
Inclination:       51
6372  deg
RA of node:       111
5503  deg
Eccentricity:     
0005300     
Arg of perigee:   136
7328  deg
Mean anomaly:     223
4241  deg
Mean motion:   15
54156474  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3069
Checksum:              289


Coasting Arc #13 (Orbit 3071)
---------------------------------------

Vector Time (GMT): 2017/225/21:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4492995
73                 A    =         6782249
68  meter
 Y    =       -2984356
27  meter          E    =           
0010614
 Z    =       -4119111
62                 I    =           51
98878
 XDOT =        840
209454                 Wp   =          101
26693
 YDOT =       6568
317244  meter/sec      RA   =          109
75971  deg
 ZDOT =      -3852
769511                 TA   =          129
11611
                                          MA   =          129
02169
                                          Ha   =            222
728  n
mi
                                          Hp   =            213
343

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14740799
65                 X    =         4546042
20
 Y    =       -9791195
10  feet           Y    =        -2933816
02  meter
 Z    =      -13514145
73                 Z    =        -4097157
23
 XDOT =       2756
592698                 XDOT =         785
413126
 YDOT =      21549
597257  feet/sec       YDOT =        6577
406566  meter/sec
 ZDOT =     -12640
319917                 ZDOT =       -3848
821292

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12134382
34                 X    =         3698559
74
 Y    =       12982532
10  feet           Y    =         3957075
78  meter
 Z    =      -13416461
38                 Z    =        -4089337
43
 XDOT =     -19823
509181                 XDOT =       -6042
205598
 YDOT =       5518
199015  feet/sec       YDOT =        1681
947060  meter/sec
 ZDOT =     -12623
823399                 ZDOT =       -3847
741372


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   17225
90656350  
00016717  00000-0  10270-3 0  9121
2 25544  51
6410 110
5884 0005602 141
9695 218
1854 15
54126904 30722


Satellite: ISS
Catalog Number: 25544
Epoch time:      17225
90656350   =   yrday
fracday
Element set:     912
Inclination:       51
6410  deg
RA of node:       110
5884  deg
Eccentricity:     
0005602     
Arg of perigee:   141
9695  deg
Mean anomaly:     218
1854  deg
Mean motion:   15
54126904  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3072
Checksum:              297


Coasting Arc #14 (Orbit 3087)
---------------------------------------

Vector Time (GMT): 2017/226/21:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4386799
33                 A    =         6778812
71  meter
 Y    =        1382500
31  meter          E    =           
0011671
 Z    =        4974985
74                 I    =           51
98860
 XDOT =        174
322115                 Wp   =          133
10059
 YDOT =      -7352
037853  meter/sec      RA   =          104
79130  deg
 ZDOT =       2185
784569                 TA   =          295
64055
                                          MA   =          295
76107
                                          Ha   =            222
661  n
mi
                                          Hp   =            213
290

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14392386
26                 X    =        -4426098
73
 Y    =        4535762
18  feet           Y    =         1333224
43  meter
 Z    =       16322131
68                 Z    =         4953580
64
 XDOT =        571
922950                 XDOT =         245
904161
 YDOT =     -24120
859099  feet/sec       YDOT =       -7349
688213  meter/sec
 ZDOT =       7171
209216                 ZDOT =        2186
805270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7129827
10                 X    =        -2173171
30
 Y    =      -13415374
36  feet           Y    =        -4089006
10  meter
 Z    =       16227113
10                 Z    =         4946024
07
 XDOT =      22826
065722                 XDOT =        6957
384832
 YDOT =      -3406
381317  feet/sec       YDOT =       -1038
265025  meter/sec
 ZDOT =       7176
854276                 ZDOT =        2187
505183


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   17226
93538674  
00016717  00000-0  10270-3 0  9134
2 25544  51
6417 105
4596 0005526 145
3696 214
7817 15
54171566 30888


Satellite: ISS
Catalog Number: 25544
Epoch time:      17226
93538674   =   yrday
fracday
Element set:     913
Inclination:       51
6417  deg
RA of node:       105
4596  deg
Eccentricity:     
0005526     
Arg of perigee:   145
3696  deg
Mean anomaly:     214
7817  deg
Mean motion:   15
54171566  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3088
Checksum:              336


Coasting Arc #15 (Orbit 3102)
---------------------------------------

Vector Time (GMT): 2017/227/21:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 902191
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4166034
50                 A    =         6777340
66  meter
 Y    =         420377
73  meter          E    =           
0018137
 Z    =       -5344209
79                 I    =           51
99098
 XDOT =      -1099
183039                 Wp   =          102
85035
 YDOT =       7571
620958  meter/sec      RA   =           99
81672  deg
 ZDOT =       -265
949780                 TA   =          164
65021
                                          MA   =          164
59512
                                          Ha   =            222
497  n
mi
                                          Hp   =            213
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13668092
20                 X    =         4186983
52
 Y    =        1379192
03  feet           Y    =          467082
36  meter
 Z    =      -17533496
70                 Z    =        -5323921
70
 XDOT =      -3606
243565                 XDOT =       -1182
477368
 YDOT =      24841
276108  feet/sec       YDOT =        7558
863422  meter/sec
 ZDOT =       -872
538649                 ZDOT =        -271
491463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1421441
01                 X    =          433255
22
 Y    =       13778221
35  feet           Y    =         4199601
87  meter
 Z    =      -17443696
38                 Z    =        -5316838
66
 XDOT =     -24053
112229                 XDOT =       -7331
388608
 YDOT =       1363
759171  feet/sec       YDOT =         415
673795  meter/sec
 ZDOT =       -898
260219                 ZDOT =        -273
789715


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   17227
89990745  
00016717  00000-0  10270-3 0  9142
2 25544  51
6420 100
6520 0005379 147
9261 212
2220 15
54143170 31037


Satellite: ISS
Catalog Number: 25544
Epoch time:      17227
89990745   =   yrday
fracday
Element set:     914
Inclination:       51
6420  deg
RA of node:       100
6520  deg
Eccentricity:     
0005379     
Arg of perigee:   147
9261  deg
Mean anomaly:     212
2220  deg
Mean motion:   15
54143170  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3103
Checksum:              283


Coasting Arc #16 (Orbit 3118)
---------------------------------------

Vector Time (GMT): 2017/228/21:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924696
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3835748
41                 A    =         6778089
79  meter
 Y    =       -2202707
75  meter          E    =           
0006936
 Z    =        5129709
50                 I    =           51
99862
 XDOT =       1922
909224                 Wp   =          104
81658
 YDOT =      -7238
861067  meter/sec      RA   =           94
84140  deg
 ZDOT =      -1670
373825                 TA   =            1
21968
                                          MA   =            1
21799
                                          Ha   =            222
499  n
mi
                                          Hp   =            213
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12584476
40                 X    =        -3835749
48
 Y    =       -7226731
45  feet           Y    =        -2245601
82  meter
 Z    =       16829755
58                 Z    =         5111076
72
 XDOT =       6308
757298                 XDOT =        2011
826962
 YDOT =     -23749
544182  feet/sec       YDOT =       -7216
860580  meter/sec
 ZDOT =      -5480
229085                 ZDOT =       -1660
817204

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4285976
83                 X    =         1306365
74
 Y    =      -13963699
63  feet           Y    =        -4256135
65  meter
 Z    =       16747562
86                 Z    =         5104657
16
 XDOT =      23543
513874                 XDOT =        7176
063029
 YDOT =        705
133724  feet/sec       YDOT =         214
924759  meter/sec
 ZDOT =      -5436
756721                 ZDOT =       -1657
123449


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   17228
92872631  
00016717  00000-0  10270-3 0  9151
2 25544  51
6420  95
5233 0005331 151
4632 208
6813 15
54183450 31199


Satellite: ISS
Catalog Number: 25544
Epoch time:      17228
92872631   =   yrday
fracday
Element set:     915
Inclination:       51
6420  deg
RA of node:        95
5233  deg
Eccentricity:     
0005331     
Arg of perigee:   151
4632  deg
Mean anomaly:     208
6813  deg
Mean motion:   15
54183450  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3119
Checksum:              294


Coasting Arc #17 (Orbit 3133)
---------------------------------------

Vector Time (GMT): 2017/229/21:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924696
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3446973
76                 A    =         6781071
12  meter
 Y    =        3852515
07  meter          E    =           
0013326
 Z    =       -4402493
95                 I    =           52
00971
 XDOT =      -2665
067479                 Wp   =          127
01756
 YDOT =       6305
221763  meter/sec      RA   =           89
87268  deg
 ZDOT =       3430
254147                 TA   =          177
62807
                                          MA   =          177
62174
                                          Ha   =            222
336  n
mi
                                          Hp   =            213
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11308969
04                 X    =         3425022
63
 Y    =       12639485
14  feet           Y    =         3890938
85  meter
 Z    =      -14443877
78                 Z    =        -4385803
04
 XDOT =      -8743
659707                 XDOT =       -2752
038353
 YDOT =      20686
423106  feet/sec       YDOT =        6274
932799  meter/sec
 ZDOT =      11254
114655                 ZDOT =        3417
097149

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9609933
40                 X    =        -2929107
70
 Y    =       14050319
75  feet           Y    =         4282537
46  meter
 Z    =      -14370548
55                 Z    =        -4380143
20
 XDOT =     -21154
087692                 XDOT =       -6447
765928
 YDOT =      -3016
493703  feet/sec       YDOT =        -919
427281  meter/sec
 ZDOT =      11194
824488                 ZDOT =        3412
182504


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   17229
89324397  
00016717  00000-0  10270-3 0  9160
2 25544  51
6415  90
7163 0005442 154
5656 205
5765 15
54178440 31347


Satellite: ISS
Catalog Number: 25544
Epoch time:      17229
89324397   =   yrday
fracday
Element set:     916
Inclination:       51
6415  deg
RA of node:        90
7163  deg
Eccentricity:     
0005442     
Arg of perigee:   154
5656  deg
Mean anomaly:     205
5765  deg
Mean motion:   15
54178440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3134
Checksum:              321


Coasting Arc #18 (Orbit 3149)
---------------------------------------

Vector Time (GMT): 2017/230/21:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924696
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2960458
73                 A    =         6784954
60  meter
 Y    =       -5195085
33  meter          E    =           
0015939
 Z    =        3187180
17                 I    =           52
02205
 XDOT =       3365
934664                 Wp   =          111
23590
 YDOT =      -4903
005565  meter/sec      RA   =           84
91262  deg
 ZDOT =      -4851
560970                 TA   =           32
12745
                                          MA   =           32
03041
                                          Ha   =            222
324  n
mi
                                          Hp   =            213
677

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9712791
11                 X    =        -2917627
39
 Y    =      -17044243
20  feet           Y    =        -5227951
75  meter
 Z    =       10456627
86                 Z    =         3172903
37
 XDOT =      11043
092731                 XDOT =        3444
077324
 YDOT =     -16085
976262  feet/sec       YDOT =       -4864
928402  meter/sec
 ZDOT =     -15917
194782                 ZDOT =       -4835
020849

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14038243
79                 X    =         4278856
71
 Y    =      -13750407
18  feet           Y    =        -4191124
11  meter
 Z    =       10394210
75                 Z    =         3168155
44
 XDOT =      17369
745948                 XDOT =        5294
298565
 YDOT =       5722
743848  feet/sec       YDOT =        1744
292325  meter/sec
 ZDOT =     -15843
128244                 ZDOT =       -4828
985489


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   17230
92205911  
00016717  00000-0  10270-3 0  9177
2 25544  51
6420  85
5875 0005258 157
6275 202
5107 15
54167870 31501


Satellite: ISS
Catalog Number: 25544
Epoch time:      17230
92205911   =   yrday
fracday
Element set:     917
Inclination:       51
6420  deg
RA of node:        85
5875  deg
Eccentricity:     
0005258     
Arg of perigee:   157
6275  deg
Mean anomaly:     202
5107  deg
Mean motion:   15
54167870  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3150
Checksum:              302
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