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

 
Date: October 31st 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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


306/03:16:43 186 0 6 1 4 1 4
N/A 1 2 -0 1 222 6
000/00:03:26 372 -0 0 0 0 213 4

307/05:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 213 4

310/13:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 6
000/00:00:00 000 0 0 0 0 213 3

315/12:37:22 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 213 3

317/10:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 2

317/21:54:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 5
000/00:00:00 000 0 0 0 0 213 3

Coasting Arc #1 (Orbit 278)
---------------------------------------

Vector Time (GMT): 2017/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3940267
01                 A    =         6777183
45  meter
 Y    =       -1681498
24  meter          E    =           
0019554
 Z    =       -5268479
57                 I    =           51
99392
 XDOT =       1742
245835                 Wp   =           79
69696
 YDOT =       7378
596169  meter/sec      RA   =           82
93881  deg
 ZDOT =      -1051
863934                 TA   =          180
25828
                                          MA   =          180
25929
                                          Ha   =            222
605  n
mi
                                          Hp   =            212
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12927385
20                 X    =         3984369
24
 Y    =       -5516726
51  feet           Y    =        -1637189
23  meter
 Z    =      -17285037
95                 Z    =        -5249231
43
 XDOT =       5716
029641                 XDOT =        1664
716437
 YDOT =      24207
992680  feet/sec       YDOT =        7397
645591  meter/sec
 ZDOT =      -3450
997160                 ZDOT =       -1043
589286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6851325
14                 X    =        -2088283
90
 Y    =       12392184
51  feet           Y    =         3777137
84  meter
 Z    =      -17199337
29                 Z    =        -5242358
01
 XDOT =     -18556
590305                 XDOT =       -5656
048725
 YDOT =     -15000
174983  feet/sec       YDOT =       -4572
053335  meter/sec
 ZDOT =      -3415
408406                 ZDOT =       -1041
016482


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   17303
51789025  
00016717  00000-0  10270-3 0  9008
2 25544  51
6388  83
6772 0005285  73
7590 286
4144 15
54313213  2792


Satellite: ISS
Catalog Number: 25544
Epoch time:      17303
51789025   =   yrday
fracday
Element set:     900
Inclination:       51
6388  deg
RA of node:        83
6772  deg
Eccentricity:     
0005285     
Arg of perigee:    73
7590  deg
Mean anomaly:     286
4144  deg
Mean motion:   15
54313213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             279
Checksum:              314


Coasting Arc #2 (Orbit 294)
---------------------------------------

Vector Time (GMT): 2017/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4251385
02                 A    =         6777211
49  meter
 Y    =        -194694
87  meter          E    =           
0008784
 Z    =        5267656
80                 I    =           51
98844
 XDOT =       -847
340218                 Wp   =           69
63327
 YDOT =      -7567
470862  meter/sec      RA   =           77
96028  deg
 ZDOT =       -959
295489                 TA   =           29
51948
                                          MA   =           29
46991
                                          Ha   =            222
861  n
mi
                                          Hp   =            212
504

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13948113
57                 X    =        -4274480
10
 Y    =        -638762
71  feet           Y    =         -242365
51  meter
 Z    =       17282338
58                 Z    =         5246948
41
 XDOT =      -2779
987593                 XDOT =        -757
995883
 YDOT =     -24827
660309  feet/sec       YDOT =       -7576
446915  meter/sec
 ZDOT =      -3147
294913                 ZDOT =        -963
194121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11312290
86                 X    =         3447986
25
 Y    =       -8376021
00  feet           Y    =        -2553011
20  meter
 Z    =       17190446
90                 Z    =         5239648
22
 XDOT =      17192
797227                 XDOT =        5240
364595
 YDOT =      16698
554039  feet/sec       YDOT =        5089
719271  meter/sec
 ZDOT =      -3163
415936                 ZDOT =        -964
209177


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   17304
54660930  
00016717  00000-0  10270-3 0  9016
2 25544  51
6385  78
5467 0005362  77
4171 282
7581 15
54279564  2957


Satellite: ISS
Catalog Number: 25544
Epoch time:      17304
54660930   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:        78
5467  deg
Eccentricity:     
0005362     
Arg of perigee:    77
4171  deg
Mean anomaly:     282
7581  deg
Mean motion:   15
54279564  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             295
Checksum:              327


Coasting Arc #3 (Orbit 309)
---------------------------------------

Vector Time (GMT): 2017/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 920041
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4462228
90                 A    =         6779521
68  meter
 Y    =        1991362
57  meter          E    =           
0015436
 Z    =       -4713793
57                 I    =           51
98905
 XDOT =       -159
848429                 Wp   =          100
10593
 YDOT =       7102
712960  meter/sec      RA   =           72
98638  deg
 ZDOT =       2854
553136                 TA   =          198
10831
                                          MA   =          198
16335
                                          Ha   =            222
623  n
mi
                                          Hp   =            212
614

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14639858
60                 X    =         4462527
14
 Y    =        6533341
75  feet           Y    =         2041263
58  meter
 Z    =      -15465201
99                 Z    =        -4692116
36
 XDOT =       -524
437104                 XDOT =        -253
127325
 YDOT =      23302
864043  feet/sec       YDOT =        7100
404083  meter/sec
 ZDOT =       9365
331812                 ZDOT =        2853
549534

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15483351
20                 X    =        -4719325
45
 Y    =        4498115
29  feet           Y    =         1371025
54  meter
 Z    =      -15369296
71                 Z    =        -4684561
64
 XDOT =     -14233
719897                 XDOT =       -4338
437825
 YDOT =     -17074
207883  feet/sec       YDOT =       -5204
218563  meter/sec
 ZDOT =       9359
750797                 ZDOT =        2852
852043


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   17305
51102865  
00016717  00000-0  10270-3 0  9023
2 25544  51
6389  73
7386 0005209  81
1143 279
0599 15
54309724  3107


Satellite: ISS
Catalog Number: 25544
Epoch time:      17305
51102865   =   yrday
fracday
Element set:     902
Inclination:       51
6389  deg
RA of node:        73
7386  deg
Eccentricity:     
0005209     
Arg of perigee:    81
1143  deg
Mean anomaly:     279
0599  deg
Mean motion:   15
54309724  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             310
Checksum:              304


Coasting Arc #4 (Orbit 319)
---------------------------------------

Vector Time (GMT): 2017/306/03:18:26
372
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3904947
01                 A    =         6777514
31  meter
 Y    =       -1499864
22  meter          E    =           
0018964
 Z    =       -5348890
92                 I    =           51
97603
 XDOT =       2677
437595                 Wp   =           86
42428
 YDOT =       7170
647744  meter/sec      RA   =           69
84722  deg
 ZDOT =        -55
057621                 TA   =          183
04676
                                          MA   =          183
05833
                                          Ha   =            222
588  n
mi
                                          Hp   =            213
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12811505
94                 X    =         3947411
63
 Y    =       -4920814
38  feet           Y    =        -1455959
37  meter
 Z    =      -17548854
72                 Z    =        -5329818
16
 XDOT =       8784
244077                 XDOT =        2597
321951
 YDOT =      23525
747192  feet/sec       YDOT =        7200
140723  meter/sec
 ZDOT =       -180
635240                 ZDOT =         -42
246209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4998181
30                 X    =        -1523445
66
 Y    =      -12897280
17  feet           Y    =        -3931091
00  meter
 Z    =      -17463955
69                 Z    =        -5323013
69
 XDOT =      22533
193564                 XDOT =        6868
117398
 YDOT =      -8558
933570  feet/sec       YDOT =       -2608
762952  meter/sec
 ZDOT =       -124
915806                 ZDOT =         -38
074338


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   17306
15397416  
00016717  00000-0  10270-3 0  9033
2 25544  51
6413  70
5366 0004191  75
5231 284
6387 15
54075871  3203


Satellite: ISS
Catalog Number: 25544
Epoch time:      17306
15397416   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:        70
5366  deg
Eccentricity:     
0004191     
Arg of perigee:    75
5231  deg
Mean anomaly:     284
6387  deg
Mean motion:   15
54075871  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             320
Checksum:              300


Coasting Arc #5 (Orbit 335)
---------------------------------------

Vector Time (GMT): 2017/307/03:18:26
372
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4478006
26                 A    =         6778542
38  meter
 Y    =        -192091
76  meter          E    =           
0009523
 Z    =        5078905
15                 I    =           51
96821
 XDOT =      -1793
732123                 Wp   =           64
74432
 YDOT =      -7228
532479  meter/sec      RA   =           64
87121  deg
 ZDOT =      -1848
249950                 TA   =           43
09824
                                          MA   =           43
02371
                                          Ha   =            222
676  n
mi
                                          Hp   =            213
214

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14691621
59                 X    =        -4500196
99
 Y    =        -630222
32  feet           Y    =         -242291
70  meter
 Z    =       16663074
64                 Z    =         5057097
85
 XDOT =      -5884
947911                 XDOT =       -1703
789265
 YDOT =     -23715
657740  feet/sec       YDOT =       -7248
088413  meter/sec
 ZDOT =      -6063
812171                 ZDOT =       -1856
744761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -287080
74                 X    =          -87502
21
 Y    =       14811275
95  feet           Y    =         4514476
91  meter
 Z    =       16566311
33                 Z    =         5049411
69
 XDOT =     -22494
892946                 XDOT =       -6856
443370
 YDOT =       6411
746368  feet/sec       YDOT =        1954
300293  meter/sec
 ZDOT =      -6100
343260                 ZDOT =       -1859
384626


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   17307
18284978  
00016717  00000-0  10270-3 0  9046
2 25544  51
6419  65
4081 0004138  77
6845 282
4771 15
54110921  3367


Satellite: ISS
Catalog Number: 25544
Epoch time:      17307
18284978   =   yrday
fracday
Element set:     904
Inclination:       51
6419  deg
RA of node:        65
4081  deg
Eccentricity:     
0004138     
Arg of perigee:    77
6845  deg
Mean anomaly:     282
4771  deg
Mean motion:   15
54110921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             336
Checksum:              317


Coasting Arc #6 (Orbit 336)
---------------------------------------

Vector Time (GMT): 2017/307/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4779320
44                 A    =         6782035
25  meter
 Y    =        2318329
37  meter          E    =           
0011581
 Z    =       -4227609
15                 I    =           51
97629
 XDOT =         11
449021                 Wp   =           98
80246
 YDOT =       6706
782360  meter/sec      RA   =           64
36359  deg
 ZDOT =       3697
702235                 TA   =          208
96502
                                          MA   =          209
02934
                                          Ha   =            222
596  n
mi
                                          Hp   =            213
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15680185
18                 X    =         4773577
33
 Y    =        7606067
48  feet           Y    =         2371742
67  meter
 Z    =      -13870108
76                 Z    =        -4204406
06
 XDOT =         37
562405                 XDOT =         -81
511030
 YDOT =      22003
879133  feet/sec       YDOT =        6706
390805  meter/sec
 ZDOT =      12131
569013                 ZDOT =        3697
531722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3548243
25                 X    =        -1081504
54
 Y    =      -17145448
44  feet           Y    =        -5225932
68  meter
 Z    =      -13767496
31                 Z    =        -4196332
88
 XDOT =      16247
876544                 XDOT =        4952
352771
 YDOT =     -13084
119704  feet/sec       YDOT =       -3988
039686  meter/sec
 ZDOT =      12129
720919                 ZDOT =        3697
138936


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   17307
24715457  
00016717  00000-0  10270-3 0  9055
2 25544  51
6400  65
0860 0004112  78
0905 282
0709 15
54073793  3375


Satellite: ISS
Catalog Number: 25544
Epoch time:      17307
24715457   =   yrday
fracday
Element set:     905
Inclination:       51
6400  deg
RA of node:        65
0860  deg
Eccentricity:     
0004112     
Arg of perigee:    78
0905  deg
Mean anomaly:     282
0709  deg
Mean motion:   15
54073793  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             337
Checksum:              294


Coasting Arc #7 (Orbit 352)
---------------------------------------

Vector Time (GMT): 2017/308/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4864674
12                 A    =         6785750
28  meter
 Y    =       -3675698
44  meter          E    =           
0017171
 Z    =        2962237
70                 I    =           51
97405
 XDOT =       1210
997787                 Wp   =           93
51240
 YDOT =      -5670
761946  meter/sec      RA   =           59
40374  deg
 ZDOT =      -5023
853651                 TA   =           52
79425
                                          MA   =           52
63766
                                          Ha   =            222
585  n
mi
                                          Hp   =            213
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15960216
94                 X    =        -4837599
49
 Y    =      -12059378
09  feet           Y    =        -3729947
09  meter
 Z    =        9718627
64                 Z    =         2938671
72
 XDOT =       3973
089851                 XDOT =        1298
723967
 YDOT =     -18604
862028  feet/sec       YDOT =       -5656
729368  meter/sec
 ZDOT =     -16482
459484                 ZDOT =       -5017
757577

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         510480
05                 X    =          155594
32
 Y    =       20047618
51  feet           Y    =         6110514
12  meter
 Z    =        9614637
28                 Z    =         2930541
44
 XDOT =     -15651
548902                 XDOT =       -4770
592105
 YDOT =       8328
086953  feet/sec       YDOT =        2538
400903  meter/sec
 ZDOT =     -16454
464055                 ZDOT =       -5015
320644


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   17308
27602749  
00016717  00000-0  10270-3 0  9069
2 25544  51
6401  59
9582 0004088  79
9245 280
2368 15
54107503  3534


Satellite: ISS
Catalog Number: 25544
Epoch time:      17308
27602749   =   yrday
fracday
Element set:     906
Inclination:       51
6401  deg
RA of node:        59
9582  deg
Eccentricity:     
0004088     
Arg of perigee:    79
9245  deg
Mean anomaly:     280
2368  deg
Mean motion:   15
54107503  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             353
Checksum:              317


Coasting Arc #8 (Orbit 367)
---------------------------------------

Vector Time (GMT): 2017/309/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4715733
48                 A    =         6788642
73  meter
 Y    =        4661954
44  meter          E    =           
0011619
 Z    =       -1439858
40                 I    =           51
96537
 XDOT =      -2505
884335                 Wp   =           52
19721
 YDOT =       4319
246275  meter/sec      RA   =           54
45091  deg
 ZDOT =       5816
538254                 TA   =          292
17410
                                          MA   =          292
29736
                                          Ha   =            222
580  n
mi
                                          Hp   =            213
317

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15471566
53                 X    =         4670246
12
 Y    =       15295126
11  feet           Y    =         4714434
65  meter
 Z    =       -4723944
88                 Z    =        -1417060
58
 XDOT =      -8221
405297                 XDOT =       -2582
251853
 YDOT =      14170
755495  feet/sec       YDOT =        4290
796773  meter/sec
 ZDOT =      19083
130753                 ZDOT =        5804
179559

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1976196
81                 X    =          602344
79
 Y    =      -21687402
48  feet           Y    =        -6610320
28  meter
 Z    =       -4623540
73                 Z    =        -1409255
21
 XDOT =      14667
444839                 XDOT =        4470
637187
 YDOT =      -2692
194915  feet/sec       YDOT =        -820
581010  meter/sec
 ZDOT =      19027
550977                 ZDOT =        5799
597538


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   17309
24059465  
00016717  00000-0  10270-3 0  9079
2 25544  51
6395  55
1499 0003997  85
7496 274
4113 15
54073146  3686


Satellite: ISS
Catalog Number: 25544
Epoch time:      17309
24059465   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:        55
1499  deg
Eccentricity:     
0003997     
Arg of perigee:    85
7496  deg
Mean anomaly:     274
4113  deg
Mean motion:   15
54073146  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             368
Checksum:              339


Coasting Arc #9 (Orbit 383)
---------------------------------------

Vector Time (GMT): 2017/310/05:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4232533
87                 A    =         6789409
33  meter
 Y    =       -5294639
00  meter          E    =           
0014507
 Z    =        -280895
92                 I    =           51
94843
 XDOT =       3844
979647                 Wp   =          124
33106
 YDOT =      -2765
922533  meter/sec      RA   =           49
50238  deg
 ZDOT =      -6030
237715                 TA   =           58
68290
                                          MA   =           58
54096
                                          Ha   =            222
563  n
mi
                                          Hp   =            213
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13886265
99                 X    =        -4171648
74
 Y    =      -17370862
85  feet           Y    =        -5341629
65  meter
 Z    =        -921574
54                 Z    =         -301309
08
 XDOT =      12614
762621                 XDOT =        3904
915950
 YDOT =      -9074
548993  feet/sec       YDOT =       -2722
590093  meter/sec
 ZDOT =     -19784
244473                 ZDOT =       -6011
413931

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4235445
76                 X    =        -1290963
87
 Y    =       21828029
71  feet           Y    =         6653183
46  meter
 Z    =       -1011274
99                 Z    =         -308236
62
 XDOT =     -13579
586384                 XDOT =       -4139
057930
 YDOT =      -3515
868967  feet/sec       YDOT =       -1071
636861  meter/sec
 ZDOT =     -19700
223635                 ZDOT =       -6004
628164


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   17310
26946079  
00016717  00000-0  10270-3 0  9080
2 25544  51
6397  50
0211 0004118  88
0464 272
1161 15
54086673  3846


Satellite: ISS
Catalog Number: 25544
Epoch time:      17310
26946079   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:        50
0211  deg
Eccentricity:     
0004118     
Arg of perigee:    88
0464  deg
Mean anomaly:     272
1161  deg
Mean motion:   15
54086673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             384
Checksum:              300


Coasting Arc #10 (Orbit 388)
---------------------------------------

Vector Time (GMT): 2017/310/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5025156
26                 A    =         6780724
30  meter
 Y    =         218606
98  meter          E    =           
0013828
 Z    =       -4560729
99                 I    =           51
91374
 XDOT =       2566
227300                 Wp   =          104
97228
 YDOT =       6493
310800  meter/sec      RA   =           47
77550  deg
 ZDOT =       3143
257980                 TA   =          196
44223
                                          MA   =          196
48712
                                          Ha   =            222
597  n
mi
                                          Hp   =            213
279

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16486733
15                 X    =         5044492
66
 Y    =         717214
51  feet           Y    =          274909
95  meter
 Z    =      -14963024
89                 Z    =        -4536271
69
 XDOT =       8419
380906                 XDOT =        2478
157809
 YDOT =      21303
513123  feet/sec       YDOT =        6521
515594  meter/sec
 ZDOT =      10312
526180                 ZDOT =        3155
510522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5230486
71                 X    =        -1594252
35
 Y    =       15754510
03  feet           Y    =         4801974
66  meter
 Z    =      -14854504
46                 Z    =        -4527652
96
 XDOT =     -21628
213311                 XDOT =       -6592
279417
 YDOT =       2579
158395  feet/sec       YDOT =         786
127479  meter/sec
 ZDOT =      10365
796480                 ZDOT =        3159
494767


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   17310
59098098  
00016717  00000-0  10270-3 0  9096
2 25544  51
6413  48
4186 0004244  93
6282 266
5356 15
54106201  3895


Satellite: ISS
Catalog Number: 25544
Epoch time:      17310
59098098   =   yrday
fracday
Element set:     909
Inclination:       51
6413  deg
RA of node:        48
4186  deg
Eccentricity:     
0004244     
Arg of perigee:    93
6282  deg
Mean anomaly:     266
5356  deg
Mean motion:   15
54106201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             389
Checksum:              315


Coasting Arc #11 (Orbit 404)
---------------------------------------

Vector Time (GMT): 2017/311/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5634953
01                 A    =         6784467
35  meter
 Y    =       -1555148
25  meter          E    =           
0016559
 Z    =        3428864
87                 I    =           51
90354
 XDOT =      -1163
026187                 Wp   =           91
29443
 YDOT =      -6014
905693  meter/sec      RA   =           42
80740  deg
 ZDOT =      -4620
494610                 TA   =           48
69640
                                          MA   =           48
55398
                                          Ha   =            222
615  n
mi
                                          Hp   =            213
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18487378
65                 X    =        -5633800
24
 Y    =       -5102192
44  feet           Y    =        -1618155
83  meter
 Z    =       11249556
66                 Z    =         3401494
14
 XDOT =      -3815
702713                 XDOT =       -1073
234864
 YDOT =     -19733
942563  feet/sec       YDOT =       -6027
409224  meter/sec
 ZDOT =     -15159
103050                 ZDOT =       -4625
926482

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9704822
33                 X    =         2958029
85
 Y    =      -16623613
40  feet           Y    =        -5066877
36  meter
 Z    =       11128340
53                 Z    =         3391918
19
 XDOT =      18814
735475                 XDOT =        5734
731373
 YDOT =        778
758431  feet/sec       YDOT =         237
365570  meter/sec
 ZDOT =     -15182
170319                 ZDOT =       -4627
525513


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   17311
61984147  
00016717  00000-0  10270-3 0  9101
2 25544  51
6411  43
2904 0004119  95
8524 264
3096 15
54121842  4052


Satellite: ISS
Catalog Number: 25544
Epoch time:      17311
61984147   =   yrday
fracday
Element set:     910
Inclination:       51
6411  deg
RA of node:        43
2904  deg
Eccentricity:     
0004119     
Arg of perigee:    95
8524  deg
Mean anomaly:     264
3096  deg
Mean motion:   15
54121842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             405
Checksum:              287


Coasting Arc #12 (Orbit 419)
---------------------------------------

Vector Time (GMT): 2017/312/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5930790
83                 A    =         6787856
07  meter
 Y    =        2635144
62  meter          E    =           
0009660
 Z    =       -1986312
82                 I    =           51
88913
 XDOT =       -449
362993                 Wp   =           60
93535
 YDOT =       5213
340019  meter/sec      RA   =           37
84752  deg
 ZDOT =       5599
656747                 TA   =          277
22823
                                          MA   =          277
33804
                                          Ha   =            222
610  n
mi
                                          Hp   =            213
292

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19457975
15                 X    =         5910531
85
 Y    =        8645487
58  feet           Y    =         2701353
56  meter
 Z    =       -6516774
35                 Z    =        -1957551
49
 XDOT =      -1474
288034                 XDOT =        -534
827418
 YDOT =      17104
133921  feet/sec       YDOT =        5207
836883  meter/sec
 ZDOT =      18371
577254                 ZDOT =        5597
266438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13083078
64                 X    =        -3987722
37
 Y    =       16847313
29  feet           Y    =         5135061
09  meter
 Z    =       -6389576
55                 Z    =        -1947542
93
 XDOT =     -14990
831725                 XDOT =       -4569
205510
 YDOT =      -4709
934772  feet/sec       YDOT =       -1435
588118  meter/sec
 ZDOT =      18360
056976                 ZDOT =        5596
145366


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   17312
58439565  
00016717  00000-0  10270-3 0  9118
2 25544  51
6404  38
4827 0004129  99
5363 260
6257 15
54080015  4208


Satellite: ISS
Catalog Number: 25544
Epoch time:      17312
58439565   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:        38
4827  deg
Eccentricity:     
0004129     
Arg of perigee:    99
5363  deg
Mean anomaly:     260
6257  deg
Mean motion:   15
54080015  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             420
Checksum:              300


Coasting Arc #13 (Orbit 435)
---------------------------------------

Vector Time (GMT): 2017/313/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5810438
02                 A    =         6789320
92  meter
 Y    =       -3486946
41  meter          E    =           
0016392
 Z    =         289776
20                 I    =           51
86875
 XDOT =       2209
659701                 Wp   =          123
82329
 YDOT =      -4202
161268  meter/sec      RA   =           32
89236  deg
 ZDOT =      -6023
716898                 TA   =           53
06321
                                          MA   =           52
91318
                                          Ha   =            222
562  n
mi
                                          Hp   =            213
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19063116
85                 X    =        -5772421
81
 Y    =      -11440112
89  feet           Y    =        -3551710
14  meter
 Z    =         950709
31                 Z    =          261642
76
 XDOT =       7249
539702                 XDOT =        2285
745829
 YDOT =     -13786
618333  feet/sec       YDOT =       -4177
025786  meter/sec
 ZDOT =     -19762
850716                 ZDOT =       -6012
798199

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15418903
94                 X    =         4699681
92
 Y    =      -16023633
60  feet           Y    =        -4884003
52  meter
 Z    =         826451
88                 Z    =          251902
53
 XDOT =      10617
717238                 XDOT =        3236
280214
 YDOT =       9154
494007  feet/sec       YDOT =        2790
289773  meter/sec
 ZDOT =     -19713
649994                 ZDOT =       -6008
720518


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   17313
61324716  
00016717  00000-0  10270-3 0  9125
2 25544  51
6411  33
3536 0004300 100
7943 259
3693 15
54122695  4364


Satellite: ISS
Catalog Number: 25544
Epoch time:      17313
61324716   =   yrday
fracday
Element set:     912
Inclination:       51
6411  deg
RA of node:        33
3536  deg
Eccentricity:     
0004300     
Arg of perigee:   100
7943  deg
Mean anomaly:     259
3693  deg
Mean motion:   15
54122695  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             436
Checksum:              283


Coasting Arc #14 (Orbit 451)
---------------------------------------

Vector Time (GMT): 2017/314/13:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5275376
43                 A    =         6788634
28  meter
 Y    =        4030316
97  meter          E    =           
0017354
 Z    =        1385868
81                 I    =           51
83717
 XDOT =      -3913
796795                 Wp   =           70
07096
 YDOT =       3102
799145  meter/sec      RA   =           27
93704  deg
 ZDOT =       5821
334748                 TA   =          304
99323
                                          MA   =          305
15602
                                          Ha   =            222
655  n
mi
                                          Hp   =            213
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17307665
47                 X    =         5223184
32
 Y    =       13222824
71  feet           Y    =         4089018
00  meter
 Z    =        4546813
69                 Z    =         1411368
52
 XDOT =     -12840
540665                 XDOT =       -3976
479767
 YDOT =      10179
787220  feet/sec       YDOT =        3058
681881  meter/sec
 ZDOT =      19098
867285                 ZDOT =        5802
170279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16514511
51                 X    =        -5033623
11
 Y    =       14164529
97  feet           Y    =         4317348
74  meter
 Z    =        4659280
23                 Z    =         1420148
61
 XDOT =      -6242
747548                 XDOT =       -1902
789453
 YDOT =     -13588
822827  feet/sec       YDOT =       -4141
873198  meter/sec
 ZDOT =      19013
261422                 ZDOT =        5795
242081


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   17314
64209613  
00016717  00000-0  10270-3 0  9138
2 25544  51
6402  28
2254 0004371 102
8945 257
2696 15
54075108  4521


Satellite: ISS
Catalog Number: 25544
Epoch time:      17314
64209613   =   yrday
fracday
Element set:     913
Inclination:       51
6402  deg
RA of node:        28
2254  deg
Eccentricity:     
0004371     
Arg of perigee:   102
8945  deg
Mean anomaly:     257
2696  deg
Mean motion:   15
54075108  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             452
Checksum:              293


Coasting Arc #15 (Orbit 465)
---------------------------------------

Vector Time (GMT): 2017/315/12:37:22
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1439896
52                 A    =         6777482
04  meter
 Y    =       -3951554
11  meter          E    =           
0018773
 Z    =       -5330869
91                 I    =           51
77232
 XDOT =       7095
049161                 Wp   =           92
92293
 YDOT =       2865
219875  meter/sec      RA   =           23
22351  deg
 ZDOT =       -209
026828                 TA   =          175
09419
                                          MA   =          175
07576
                                          Ha   =            222
524  n
mi
                                          Hp   =            213
322

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4724069
96                 X    =         1509871
91
 Y    =      -12964416
36  feet           Y    =        -3935061
00  meter
 Z    =      -17489730
67                 Z    =        -5323705
25
 XDOT =      23277
720346                 XDOT =        7063
497548
 YDOT =       9400
327674  feet/sec       YDOT =        2944
385143  meter/sec
 ZDOT =       -685
783558                 ZDOT =        -174
637528

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8682392
59                 X    =         2646393
26
 Y    =       10777041
53  feet           Y    =         3284842
26  meter
 Z    =      -17457234
67                 Z    =        -5320965
13
 XDOT =     -19177
527514                 XDOT =       -5845
310386
 YDOT =      14594
033665  feet/sec       YDOT =        4448
261461  meter/sec
 ZDOT =       -533
664312                 ZDOT =        -162
660882


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   17315
54233287  
00016717  00000-0  10270-3 0  9143
2 25544  51
6403  23
7376 0004138 110
2510 249
9088 15
54089788  4666


Satellite: ISS
Catalog Number: 25544
Epoch time:      17315
54233287   =   yrday
fracday
Element set:     914
Inclination:       51
6403  deg
RA of node:        23
7376  deg
Eccentricity:     
0004138     
Arg of perigee:   110
2510  deg
Mean anomaly:     249
9088  deg
Mean motion:   15
54089788  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             466
Checksum:              313


Coasting Arc #16 (Orbit 481)
---------------------------------------

Vector Time (GMT): 2017/316/12:37:22
000
Vector Time (MET): N/A
Weight (LBS)     : 919897
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3091005
18                 A    =         6778310
23  meter
 Y    =        3214069
81  meter          E    =           
0008268
 Z    =        5098365
13                 I    =           51
74599
 XDOT =      -6564
271776                 Wp   =           79
43092
 YDOT =      -3586
158849  meter/sec      RA   =           18
23264  deg
 ZDOT =      -1715
148410                 TA   =           27
12630
                                          MA   =           27
08313
                                          Ha   =            222
506  n
mi
                                          Hp   =            213
232

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10141093
11                 X    =        -3151481
74
 Y    =       10544848
46  feet           Y    =         3179166
05  meter
 Z    =       16726919
73                 Z    =         5083202
82
 XDOT =     -21536
324723                 XDOT =       -6515
351049
 YDOT =     -11765
613022  feet/sec       YDOT =       -3659
291528  meter/sec
 ZDOT =      -5627
127330                 ZDOT =       -1746
917148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4083791
10                 X    =        -1244739
53
 Y    =      -14128826
69  feet           Y    =        -4306466
38  meter
 Z    =       16659062
06                 Z    =         5077682
12
 XDOT =      19840
283967                 XDOT =        6047
318553
 YDOT =     -12549
882693  feet/sec       YDOT =       -3825
204245  meter/sec
 ZDOT =      -5767
478474                 ZDOT =       -1757
927439


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   17316
57117043  
00016717  00000-0  10270-3 0  9159
2 25544  51
6411  18
6090 0004094 112
8136 247
3450 15
54147940  4822


Satellite: ISS
Catalog Number: 25544
Epoch time:      17316
57117043   =   yrday
fracday
Element set:     915
Inclination:       51
6411  deg
RA of node:        18
6090  deg
Eccentricity:     
0004094     
Arg of perigee:   112
8136  deg
Mean anomaly:     247
3450  deg
Mean motion:   15
54147940  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             482
Checksum:              285


Coasting Arc #17 (Orbit 495)
---------------------------------------

Vector Time (GMT): 2017/317/10:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934611
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5291565
12                 A    =         6786458
62  meter
 Y    =       -3379336
78  meter          E    =           
0009257
 Z    =       -2574997
96                 I    =           51
74464
 XDOT =       4576
380022                 Wp   =          122
08866
 YDOT =      -3163
153059  meter/sec      RA   =           13
69607  deg
 ZDOT =      -5271
818473                 TA   =           86
80716
                                          MA   =           86
70125
                                          Ha   =            222
427  n
mi
                                          Hp   =            213
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17360777
94                 X    =        -5240874
90
 Y    =      -11087062
94  feet           Y    =        -3438227
33  meter
 Z    =       -8448156
02                 Z    =        -2600579
95
 XDOT =      15014
370150                 XDOT =        4637
019458
 YDOT =     -10377
798750  feet/sec       YDOT =       -3111
637947  meter/sec
 ZDOT =     -17295
992367                 ZDOT =       -5249
440087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20550449
51                 X    =         6263777
01
 Y    =         279054
64  feet           Y    =           85055
86  meter
 Z    =       -8561078
72                 Z    =        -2609416
79
 XDOT =      -7346
334023                 XDOT =       -2239
162610
 YDOT =      15303
420677  feet/sec       YDOT =        4664
482623  meter/sec
 ZDOT =     -17196
124987                 ZDOT =       -5241
378896


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   17317
47140193  
00016717  00000-0  10270-3 0  9162
2 25544  51
6414  14
1208 0004227 117
0062 243
1522 15
54121514  4968


Satellite: ISS
Catalog Number: 25544
Epoch time:      17317
47140193   =   yrday
fracday
Element set:     916
Inclination:       51
6414  deg
RA of node:        14
1208  deg
Eccentricity:     
0004227     
Arg of perigee:   117
0062  deg
Mean anomaly:     243
1522  deg
Mean motion:   15
54121514  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             496
Checksum:              264


Coasting Arc #18 (Orbit 502)
---------------------------------------

Vector Time (GMT): 2017/317/21:54:30
000
Vector Time (MET): N/A
Weight (LBS)     : 934611
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4997084
73                 A    =         6782572
04  meter
 Y    =       -2233344
53  meter          E    =           
0011021
 Z    =       -4017262
09                 I    =           51
71710
 XDOT =       5046
049108                 Wp   =          108
70781
 YDOT =       4191
241057  meter/sec      RA   =           11
31908  deg
 ZDOT =       3952
165121                 TA   =          202
37322
                                          MA   =          202
42133
                                          Ha   =            222
462  n
mi
                                          Hp   =            213
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16394634
94                 X    =         5041201
44
 Y    =       -7327245
85  feet           Y    =        -2177217
17  meter
 Z    =      -13179993
75                 Z    =        -3992880
14
 XDOT =      16555
279225                 XDOT =        4979
608460
 YDOT =      13750
790870  feet/sec       YDOT =        4247
298051  meter/sec
 ZDOT =      12966
421001                 ZDOT =        3976
516213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12769388
67                 X    =         3892109
67
 Y    =      -12738364
63  feet           Y    =        -3882653
54  meter
 Z    =      -13071403
94                 Z    =        -3984163
92
 XDOT =      19370
039315                 XDOT =        5903
987983
 YDOT =       6020
124247  feet/sec       YDOT =        1834
933870  meter/sec
 ZDOT =      13073
732346                 ZDOT =        3984
873619


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   17317
92151709  
00016717  00000-0  10270-3 0  9178
2 25544  51
6419  11
8792 0004189 112
2905 247
8692 15
54141743  5039


Satellite: ISS
Catalog Number: 25544
Epoch time:      17317
92151709   =   yrday
fracday
Element set:     917
Inclination:       51
6419  deg
RA of node:        11
8792  deg
Eccentricity:     
0004189     
Arg of perigee:   112
2905  deg
Mean anomaly:     247
8692  deg
Mean motion:   15
54141743  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             503
Checksum:              311
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