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

 
Date: June 14th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 77 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 664 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


167/11:42:30 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 216 6

167/16:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 4

Coasting Arc #1 (Orbit 2132)
---------------------------------------

Vector Time (GMT): 2017/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2601731
78                 A    =         6787713
10  meter
 Y    =       -5888767
88  meter          E    =           
0004209
 Z    =       -2142187
67                 I    =           51
95030
 XDOT =       5298
402323                 Wp   =          188
79850
 YDOT =       -329
884163  meter/sec      RA   =           51
06768  deg
 ZDOT =      -5530
801589                 TA   =           14
83811
                                          MA   =           14
82576
                                          Ha   =            219
432  n
mi
                                          Hp   =            216
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8535865
42                 X    =        -2525283
00
 Y    =      -19320104
58  feet           Y    =        -5917434
50  meter
 Z    =       -7028174
77                 Z    =        -2154641
06
 XDOT =      17383
209720                 XDOT =        5328
563231
 YDOT =      -1082
297123  feet/sec       YDOT =        -270
464545  meter/sec
 ZDOT =     -18145
674503                 ZDOT =       -5504
990442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20302976
80                 X    =        -6188347
33
 Y    =        5758136
16  feet           Y    =         1755079
90  meter
 Z    =       -7082067
59                 Z    =        -2158614
20
 XDOT =       1747
880753                 XDOT =         532
754054
 YDOT =     -16004
059936  feet/sec       YDOT =       -4878
037468  meter/sec
 ZDOT =     -18031
607790                 ZDOT =       -5496
034054


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   17165
52789449  
00016717  00000-0  10270-3 0  9005
2 25544  51
6427  51
5915 0004883 275
8672  84
1924 15
54004308 21330


Satellite: ISS
Catalog Number: 25544
Epoch time:      17165
52789449   =   yrday
fracday
Element set:     900
Inclination:       51
6427  deg
RA of node:        51
5915  deg
Eccentricity:     
0004883     
Arg of perigee:   275
8672  deg
Mean anomaly:      84
1924  deg
Mean motion:   15
54004308  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2133
Checksum:              319


Coasting Arc #2 (Orbit 2148)
---------------------------------------

Vector Time (GMT): 2017/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1498076
80                 A    =         6784259
10  meter
 Y    =        5576010
58  meter          E    =           
0007384
 Z    =        3555504
60                 I    =           51
91689
 XDOT =      -6085
275684                 Wp   =           86
34923
 YDOT =      -1239
272710  meter/sec      RA   =           46
10902  deg
 ZDOT =       4499
915696                 TA   =          315
42328
                                          MA   =          315
48265
                                          Ha   =            219
564  n
mi
                                          Hp   =            216
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4914950
12                 X    =         1418342
19
 Y    =       18293997
98  feet           Y    =         5592316
90  meter
 Z    =       11665041
35                 Z    =         3562588
70
 XDOT =     -19964
815236                 XDOT =       -6092
823869
 YDOT =      -4065
855347  feet/sec       YDOT =       -1307
365059  meter/sec
 ZDOT =      14763
502938                 ZDOT =        4470
336919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18743915
64                 X    =         5713145
49
 Y    =       -2605096
08  feet           Y    =         -794033
28  meter
 Z    =       11695272
01                 Z    =         3564718
91
 XDOT =      -6635
717193                 XDOT =       -2022
566600
 YDOT =      18060
237494  feet/sec       YDOT =        5504
760388  meter/sec
 ZDOT =      14633
095203                 ZDOT =        4460
167418


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   17166
55679086  
00016717  00000-0  10270-3 0  9015
2 25544  51
6419  46
4628 0004799 282
3693  77
6923 15
54018947 21494


Satellite: ISS
Catalog Number: 25544
Epoch time:      17166
55679086   =   yrday
fracday
Element set:     901
Inclination:       51
6419  deg
RA of node:        46
4628  deg
Eccentricity:     
0004799     
Arg of perigee:   282
3693  deg
Mean anomaly:      77
6923  deg
Mean motion:   15
54018947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2149
Checksum:              353


Coasting Arc #3 (Orbit 2163)
---------------------------------------

Vector Time (GMT): 2017/167/11:42:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5438733
88                 A    =         6789461
47  meter
 Y    =       -3987620
80  meter          E    =           
0009054
 Z    =         738441
11                 I    =           51
91178
 XDOT =       2282
843104                 Wp   =          139
74399
 YDOT =      -4226
695347  meter/sec      RA   =           41
17165  deg
 ZDOT =      -5976
817809                 TA   =           32
30685
                                          MA   =           32
25143
                                          Ha   =            219
594  n
mi
                                          Hp   =            216
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17843615
09                 X    =        -5397326
02
 Y    =      -13082745
40  feet           Y    =        -4048208
95  meter
 Z    =        2422707
04                 Z    =          712121
64
 XDOT =       7489
642730                 XDOT =        2358
969881
 YDOT =     -13867
110718  feet/sec       YDOT =       -4200
740842  meter/sec
 ZDOT =     -19608
982314                 ZDOT =       -5965
543965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16065783
93                 X    =        -4896850
94
 Y    =       15231206
11  feet           Y    =         4642471
62  meter
 Z    =        2307224
15                 Z    =          703241
92
 XDOT =     -11172
094428                 XDOT =       -3405
254382
 YDOT =      -8803
775664  feet/sec       YDOT =       -2683
390822  meter/sec
 ZDOT =     -19558
384061                 ZDOT =       -5961
395462


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   17167
52137711  
00016717  00000-0  10270-3 0  9028
2 25544  51
6426  41
6557 0004816 283
3226  76
7390 15
54010920 21641


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
52137711   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:        41
6557  deg
Eccentricity:     
0004816     
Arg of perigee:   283
3226  deg
Mean anomaly:      76
7390  deg
Mean motion:   15
54010920  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2164
Checksum:              293


Coasting Arc #4 (Orbit 2166)
---------------------------------------

Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3159564
92                 A    =         6786486
06  meter
 Y    =       -5389382
15  meter          E    =           
0001844
 Z    =       -2647943
87                 I    =           51
89420
 XDOT =       5554
767342                 Wp   =          195
95271
 YDOT =       -683
560784  meter/sec      RA   =           40
20328  deg
 ZDOT =      -5237
634343                 TA   =           13
77965
                                          MA   =           13
77462
                                          Ha   =            219
536  n
mi
                                          Hp   =            216
435

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10366026
63                 X    =        -3086202
20
 Y    =      -17681699
98  feet           Y    =        -5424304
11  meter
 Z    =       -8687479
90                 Z    =        -2663114
36
 XDOT =      18224
302303                 XDOT =        5587
440106
 YDOT =      -2242
653491  feet/sec       YDOT =        -621
260449  meter/sec
 ZDOT =     -17183
839707                 ZDOT =       -5210
571714

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         718331
56                 X    =          218947
46
 Y    =       20455571
03  feet           Y    =         6234858
05  meter
 Z    =       -8753453
20                 Z    =        -2668052
54
 XDOT =     -15724
941928                 XDOT =       -4792
962300
 YDOT =      -6748
784264  feet/sec       YDOT =       -2057
029444  meter/sec
 ZDOT =     -17064
184809                 ZDOT =       -5201
163530


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   17167
71429259  
00016717  00000-0  10270-3 0  9031
2 25544  51
6392  40
6887 0004684 283
4394  76
6236 15
54067991 21679


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
71429259   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:        40
6887  deg
Eccentricity:     
0004684     
Arg of perigee:   283
4394  deg
Mean anomaly:      76
6236  deg
Mean motion:   15
54067991  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2167
Checksum:              344


Coasting Arc #5 (Orbit 2182)
---------------------------------------

Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1916228
40                 A    =         6782809
59  meter
 Y    =        5159973
44  meter          E    =           
0006298
 Z    =        3958699
89                 I    =           51
85623
 XDOT =      -6482
290616                 Wp   =           97
04830
 YDOT =       -695
907608  meter/sec      RA   =           35
23742  deg
 ZDOT =       4038
616234                 TA   =          310
88879
                                          MA   =          310
94332
                                          Ha   =            219
555  n
mi
                                          Hp   =            216
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6286838
59                 X    =         1839156
34
 Y    =       16929046
72  feet           Y    =         5180970
73  meter
 Z    =       12987860
52                 Z    =         3967821
60
 XDOT =     -21267
357663                 XDOT =       -6493
644684
 YDOT =      -2283
161443  feet/sec       YDOT =        -768
460807  meter/sec
 ZDOT =      13250
053261                 ZDOT =        4007
099551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2237030
85                 X    =          681847
00
 Y    =      -17891070
05  feet           Y    =        -5453198
15  meter
 Z    =       13027155
82                 Z    =         3970677
09
 XDOT =      16634
996714                 XDOT =        5070
346998
 YDOT =      11641
470098  feet/sec       YDOT =        3548
320086  meter/sec
 ZDOT =      13110
997555                 ZDOT =        3996
232055


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   17168
74317828  
00016717  00000-0  10270-3 0  9044
2 25544  51
6389  35
5594 0004694 284
9031  75
1601 15
54070690 21836


Satellite: ISS
Catalog Number: 25544
Epoch time:      17168
74317828   =   yrday
fracday
Element set:     904
Inclination:       51
6389  deg
RA of node:        35
5594  deg
Eccentricity:     
0004694     
Arg of perigee:   284
9031  deg
Mean anomaly:      75
1601  deg
Mean motion:   15
54070690  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2183
Checksum:              324


Coasting Arc #6 (Orbit 2197)
---------------------------------------

Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -425990
99                 A    =         6779406
06  meter
 Y    =       -4693229
17  meter          E    =           
0008716
 Z    =       -4881684
95                 I    =           51
81819
 XDOT =       7018
175677                 Wp   =           54
13702
 YDOT =       1887
151470  meter/sec      RA   =           30
26209  deg
 ZDOT =      -2424
777672                 TA   =          192
10918
                                          MA   =          192
13014
                                          Ha   =            219
726  n
mi
                                          Hp   =            216
357

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1397608
23                 X    =         -349765
44
 Y    =      -15397733
48  feet           Y    =        -4697566
25  meter
 Z    =      -16016026
73                 Z    =        -4883569
57
 XDOT =      23025
510752                 XDOT =        7008
329897
 YDOT =       6191
441830  feet/sec       YDOT =        1965
578630  meter/sec
 ZDOT =      -7955
307324                 ZDOT =       -2390
709094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5653833
38                 X    =        -1723288
42
 Y    =       14381933
64  feet           Y    =         4383613
37  meter
 Z    =      -16023444
39                 Z    =        -4883945
85
 XDOT =     -16907
512190                 XDOT =       -5153
409715
 YDOT =     -15349
895191  feet/sec       YDOT =       -4678
648054  meter/sec
 ZDOT =      -7805
220556                 ZDOT =       -2379
031226


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   17169
70775696  
00016717  00000-0  10270-3 0  9053
2 25544  51
6395  30
7532 0004565 289
7186  70
3474 15
54068174 21988


Satellite: ISS
Catalog Number: 25544
Epoch time:      17169
70775696   =   yrday
fracday
Element set:     905
Inclination:       51
6395  deg
RA of node:        30
7532  deg
Eccentricity:     
0004565     
Arg of perigee:   289
7186  deg
Mean anomaly:      70
3474  deg
Mean motion:   15
54068174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2198
Checksum:              345


Coasting Arc #7 (Orbit 2213)
---------------------------------------

Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1202072
14                 A    =         6777679
53  meter
 Y    =        4049100
57  meter          E    =           
0001889
 Z    =        5302044
97                 I    =           51
78386
 XDOT =      -7094
286112                 Wp   =          295
20145
 YDOT =      -2852
504445  meter/sec      RA   =           25
27493  deg
 ZDOT =        570
956642                 TA   =          149
36565
                                          MA   =          149
35461
                                          Ha   =            219
924  n
mi
                                          Hp   =            216
398

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3943806
22                 X    =        -1273015
86
 Y    =       13284450
70  feet           Y    =         4035260
99  meter
 Z    =       17395160
65                 Z    =         5296033
71
 XDOT =     -23275
216903                 XDOT =       -7064
634846
 YDOT =      -9358
610385  feet/sec       YDOT =       -2931
671827  meter/sec
 ZDOT =       1873
217331                 ZDOT =         536
566234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9341527
23                 X    =         2847297
50
 Y    =      -10281838
44  feet           Y    =        -3133904
36  meter
 Z    =       17367830
02                 Z    =         5293714
59
 XDOT =      16312
354994                 XDOT =        4972
005802
 YDOT =      17723
896771  feet/sec       YDOT =        5402
243736  meter/sec
 ZDOT =       1721
907582                 ZDOT =         524
837431


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   17170
73663741  
00016717  00000-0  10270-3 0  9066
2 25544  51
6398  25
6237 0004677 293
6331  66
4330 15
54046066 22148


Satellite: ISS
Catalog Number: 25544
Epoch time:      17170
73663741   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:        25
6237  deg
Eccentricity:     
0004677     
Arg of perigee:   293
6331  deg
Mean anomaly:      66
4330  deg
Mean motion:   15
54046066  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              308


Coasting Arc #8 (Orbit 2228)
---------------------------------------

Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2835084
01                 A    =         6778128
11  meter
 Y    =       -3317218
83  meter          E    =           
0009554
 Z    =       -5194964
48                 I    =           51
75663
 XDOT =       6639
815563                 Wp   =           92
06420
 YDOT =       3579
832781  meter/sec      RA   =           20
28598  deg
 ZDOT =       1339
499175                 TA   =          190
78812
                                          MA   =          190
80863
                                          Ha   =            219
953  n
mi
                                          Hp   =            216
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9301456
73                 X    =         2897202
16
 Y    =      -10883263
87  feet           Y    =        -3285167
07  meter
 Z    =      -17043846
70                 Z    =        -5181041
88
 XDOT =      21784
171793                 XDOT =        6592
784751
 YDOT =      11744
858205  feet/sec       YDOT =        3653
820577  meter/sec
 ZDOT =       4394
682333                 ZDOT =        1371
639860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13056786
93                 X    =        -3979708
66
 Y    =        6049520
22  feet           Y    =         1843893
76  meter
 Z    =      -16981721
36                 Z    =        -5176028
67
 XDOT =     -14556
894841                 XDOT =       -4436
941548
 YDOT =     -18702
136697  feet/sec       YDOT =       -5700
411265  meter/sec
 ZDOT =       4535
904829                 ZDOT =        1382
543792


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   17171
70120745  
00016717  00000-0  10270-3 0  9077
2 25544  51
6407  20
8169 0004621 297
3432  62
7250 15
54079356 22296


Satellite: ISS
Catalog Number: 25544
Epoch time:      17171
70120745   =   yrday
fracday
Element set:     907
Inclination:       51
6407  deg
RA of node:        20
8169  deg
Eccentricity:     
0004621     
Arg of perigee:   297
3432  deg
Mean anomaly:      62
7250  deg
Mean motion:   15
54079356  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2229
Checksum:              297


Coasting Arc #9 (Orbit 2244)
---------------------------------------

Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4344089
91                 A    =         6780914
34  meter
 Y    =        2531814
10  meter          E    =           
0007131
 Z    =        4549045
38                 I    =           51
73402
 XDOT =      -5672
360259                 Wp   =           36
31662
 YDOT =      -4105
856885  meter/sec      RA   =           15
29784  deg
 ZDOT =      -3123
522528                 TA   =           84
97932
                                          MA   =           84
89792
                                          Ha   =            220
193  n
mi
                                          Hp   =            216
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14252263
48                 X    =        -4394175
70
 Y    =        8306476
72  feet           Y    =         2482954
87  meter
 Z    =       14924689
56                 Z    =         4527821
63
 XDOT =     -18610
105835                 XDOT =       -5610
853222
 YDOT =     -13470
659073  feet/sec       YDOT =       -4168
944721  meter/sec
 ZDOT =     -10247
777322                 ZDOT =       -3150
928541

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16465474
97                 X    =         5018676
77
 Y    =       -1953451
70  feet           Y    =         -595412
08  meter
 Z    =       14830478
38                 Z    =         4520329
81
 XDOT =      11558
304655                 XDOT =        3522
971259
 YDOT =      18507
413245  feet/sec       YDOT =        5641
059557  meter/sec
 ZDOT =     -10367
980966                 ZDOT =       -3160
160599


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   17172
73008056  
00016717  00000-0  10270-3 0  9082
2 25544  51
6401  15
6880 0004563 300
9612  59
1092 15
54042537 22451


Satellite: ISS
Catalog Number: 25544
Epoch time:      17172
73008056   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:        15
6880  deg
Eccentricity:     
0004563     
Arg of perigee:   300
9612  deg
Mean anomaly:      59
1092  deg
Mean motion:   15
54042537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              287


Coasting Arc #10 (Orbit 2259)
---------------------------------------

Vector Time (GMT): 2017/173/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5567408
75                 A    =         6784566
06  meter
 Y    =       -1757745
63  meter          E    =           
0002861
 Z    =       -3454165
41                 I    =           51
71524
 XDOT =       4243
649807                 Wp   =           19
06732
 YDOT =       4447
378216  meter/sec      RA   =           10
31730  deg
 ZDOT =       4580
438605                 TA   =          300
48867
                                          MA   =          300
51692
                                          Ha   =            220
285  n
mi
                                          Hp   =            216
303

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18265776
73                 X    =         5603429
29
 Y    =       -5766881
98  feet           Y    =        -1695285
14  meter
 Z    =      -11332563
67                 Z    =        -3427033
27
 XDOT =      13922
735586                 XDOT =        4171
352996
 YDOT =      14591
135880  feet/sec       YDOT =        4494
428620  meter/sec
 ZDOT =      15027
685713                 ZDOT =        4600
878184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19156003
98                 X    =        -5838750
01
 Y    =       -1628419
29  feet           Y    =         -496342
20  meter
 Z    =      -11212416
74                 Z    =        -3417544
62
 XDOT =      -7366
053857                 XDOT =       -2245
173216
 YDOT =     -17352
157023  feet/sec       YDOT =       -5288
937461  meter/sec
 ZDOT =      15117
055695                 ZDOT =        4607
678576


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   17173
69464420  
00016717  00000-0  10270-3 0  9090
2 25544  51
6406  10
8804 0004776 304
7293  55
3410 15
54062800 22606


Satellite: ISS
Catalog Number: 25544
Epoch time:      17173
69464420   =   yrday
fracday
Element set:     909
Inclination:       51
6406  deg
RA of node:        10
8804  deg
Eccentricity:     
0004776     
Arg of perigee:   304
7293  deg
Mean anomaly:      55
3410  deg
Mean motion:   15
54062800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2260
Checksum:              290


Coasting Arc #11 (Orbit 2275)
---------------------------------------

Vector Time (GMT): 2017/174/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6412370
31                 A    =         6787878
33  meter
 Y    =         977047
99  meter          E    =           
0009494
 Z    =        1987590
38                 I    =           51
69474
 XDOT =      -2445
138927                 Wp   =          104
23770
 YDOT =      -4655
543726  meter/sec      RA   =            5
34383  deg
 ZDOT =      -5579
921563                 TA   =           53
83962
                                          MA   =           53
75182
                                          Ha   =            220
306  n
mi
                                          Hp   =            216
145

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21037960
33                 X    =        -6432474
08
 Y    =        3205538
02  feet           Y    =          905227
77  meter
 Z    =        6520965
81                 Z    =         1956392
37
 XDOT =      -8022
109339                 XDOT =       -2365
793140
 YDOT =     -15274
093589  feet/sec       YDOT =       -4682
442326  meter/sec
 ZDOT =     -18306
829274                 ZDOT =       -5591
607379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20802185
96                 X    =         6340506
28
 Y    =        4681916
84  feet           Y    =         1427048
25  meter
 Z    =        6383021
06                 Z    =         1945544
82
 XDOT =       2145
389306                 XDOT =         653
914660
 YDOT =      15586
878234  feet/sec       YDOT =        4750
880486  meter/sec
 ZDOT =     -18357
503665                 ZDOT =       -5595
367117


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   17174
72350924  
00016717  00000-0  10270-3 0  9100
2 25544  51
6410   5
7514 0004716 308
2900  51
7828 15
54075942 22761


Satellite: ISS
Catalog Number: 25544
Epoch time:      17174
72350924   =   yrday
fracday
Element set:     910
Inclination:       51
6410  deg
RA of node:         5
7514  deg
Eccentricity:     
0004716     
Arg of perigee:   308
2900  deg
Mean anomaly:      51
7828  deg
Mean motion:   15
54075942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2276
Checksum:              295


Coasting Arc #12 (Orbit 2290)
---------------------------------------

Vector Time (GMT): 2017/175/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6769614
12                 A    =         6789428
52  meter
 Y    =        -222174
75  meter          E    =           
0012549
 Z    =        -337105
47                 I    =           51
66806
 XDOT =        451
071560                 Wp   =           20
35517
 YDOT =       4751
312389  meter/sec      RA   =             
37549  deg
 ZDOT =       6005
446047                 TA   =          336
01163
                                          MA   =          336
07004
                                          Ha   =            220
515  n
mi
                                          Hp   =            215
930

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22210020
09                 X    =         6773232
89
 Y    =        -728919
78  feet           Y    =         -146452
05  meter
 Z    =       -1105989
08                 Z    =         -304212
19
 XDOT =       1479
893570                 XDOT =         368
736251
 YDOT =      15588
295241  feet/sec       YDOT =        4755
895194  meter/sec
 ZDOT =      19702
906979                 ZDOT =        6007
438030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21084086
17                 X    =        -6426429
47
 Y    =       -7041155
91  feet           Y    =        -2146144
32  meter
 Z    =        -960709
13                 Z    =         -292824
14
 XDOT =       3640
385116                 XDOT =        1109
589383
 YDOT =     -13549
643199  feet/sec       YDOT =       -4129
931247  meter/sec
 ZDOT =      19710
760424                 ZDOT =        6007
839777


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   17175
68806647  
00016717  00000-0  10270-3 0  9115
2 25544  51
6415    
9436 0004754 314
3940  45
6823 15
54082173 22918


Satellite: ISS
Catalog Number: 25544
Epoch time:      17175
68806647   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:          
9436  deg
Eccentricity:     
0004754     
Arg of perigee:   314
3940  deg
Mean anomaly:      45
6823  deg
Mean motion:   15
54082173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2291
Checksum:              307


Coasting Arc #13 (Orbit 2306)
---------------------------------------

Vector Time (GMT): 2017/176/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6623958
07                 A    =         6788567
48  meter
 Y    =        -555266
95  meter          E    =           
0003866
 Z    =       -1369227
51                 I    =           51
63253
 XDOT =       1595
682370                 Wp   =          148
83358
 YDOT =      -4740
671546  meter/sec      RA   =          355
40648  deg
 ZDOT =      -5807
564128                 TA   =           46
07748
                                          MA   =           46
04558
                                          Ha   =            220
536  n
mi
                                          Hp   =            215
832

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21732145
90                 X    =        -6610605
66
 Y    =       -1821741
95  feet           Y    =         -629265
66  meter
 Z    =       -4492216
23                 Z    =        -1401371
98
 XDOT =       5235
178378                 XDOT =        1676
785223
 YDOT =     -15553
384338  feet/sec       YDOT =       -4722
373163  meter/sec
 ZDOT =     -19053
688085                 ZDOT =       -5799
616631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19870962
31                 X    =         6056669
31
 Y    =        8913781
11  feet           Y    =         2716920
48  meter
 Z    =       -4634034
87                 Z    =        -1412453
83
 XDOT =      -9563
304303                 XDOT =       -2914
895152
 YDOT =      11449
623542  feet/sec       YDOT =        3489
845255  meter/sec
 ZDOT =     -19017
660228                 ZDOT =       -5796
582838


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   17176
71692483  
00016717  00000-0  10270-3 0  9122
2 25544  51
6412 355
8152 0004735 316
8492  43
2289 15
54098327 23076


Satellite: ISS
Catalog Number: 25544
Epoch time:      17176
71692483   =   yrday
fracday
Element set:     912
Inclination:       51
6412  deg
RA of node:       355
8152  deg
Eccentricity:     
0004735     
Arg of perigee:   316
8492  deg
Mean anomaly:      43
2289  deg
Mean motion:   15
54098327  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2307
Checksum:              322


Coasting Arc #14 (Orbit 2322)
---------------------------------------

Vector Time (GMT): 2017/177/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5971663
30                 A    =         6785650
91  meter
 Y    =        1337496
29  meter          E    =           
0011474
 Z    =        2915825
03                 I    =           51
59197
 XDOT =      -3494
028262                 Wp   =           61
18651
 YDOT =       4627
972587  meter/sec      RA   =          350
42966  deg
 ZDOT =       5023
407352                 TA   =          332
10676
                                          MA   =          332
16822
                                          Ha   =            220
542  n
mi
                                          Hp   =            215
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19592071
21                 X    =         5942099
78
 Y    =        4388111
18  feet           Y    =         1404109
78  meter
 Z    =        9566355
10                 Z    =         2944761
54
 XDOT =     -11463
347315                 XDOT =       -3569
920721
 YDOT =      15183
637097  feet/sec       YDOT =        4588
474977  meter/sec
 ZDOT =      16480
995250                 ZDOT =        5006
250954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17149790
47                 X    =        -5227256
13
 Y    =      -10321522
04  feet           Y    =        -3145999
92  meter
 Z    =        9693853
38                 Z    =         2954686
51
 XDOT =      15015
160462                 XDOT =        4576
620909
 YDOT =      -9512
691391  feet/sec       YDOT =       -2899
468336  meter/sec
 ZDOT =      16404
335747                 ZDOT =        5000
041536


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   17177
74577855  
00016717  00000-0  10270-3 0  9132
2 25544  51
6425 350
6866 0004752 321
2039  38
8772 15
54120157 23233


Satellite: ISS
Catalog Number: 25544
Epoch time:      17177
74577855   =   yrday
fracday
Element set:     913
Inclination:       51
6425  deg
RA of node:       350
6866  deg
Eccentricity:     
0004752     
Arg of perigee:   321
2039  deg
Mean anomaly:      38
8772  deg
Mean motion:   15
54120157  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2323
Checksum:              319


Coasting Arc #15 (Orbit 2337)
---------------------------------------

Vector Time (GMT): 2017/178/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4894716
47                 A    =         6781924
05  meter
 Y    =       -2156695
76  meter          E    =           
0008156
 Z    =       -4178107
95                 I    =           51
54729
 XDOT =       5089
445699                 Wp   =           34
57939
 YDOT =      -4363
164420  meter/sec      RA   =          345
44197  deg
 ZDOT =      -3707
132004                 TA   =          197
24004
                                          MA   =          197
26775
                                          Ha   =            220
813  n
mi
                                          Hp   =            215
522

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16058781
07                 X    =        -4849941
02
 Y    =       -7075773
49  feet           Y    =        -2211180
98  meter
 Z    =      -13707703
24                 Z    =        -4201776
15
 XDOT =      16697
656493                 XDOT =        5155
864686
 YDOT =     -14314
843898  feet/sec       YDOT =       -4305
879003  meter/sec
 ZDOT =     -12162
506574                 ZDOT =       -3682
248541

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13123861
47                 X    =         4000152
98
 Y    =       11526108
78  feet           Y    =         3513157
96  meter
 Z    =      -13811778
47                 Z    =        -4209830
08
 XDOT =     -19448
099443                 XDOT =       -5927
780710
 YDOT =       7690
548144  feet/sec       YDOT =        2344
079074  meter/sec
 ZDOT =     -12051
792073                 ZDOT =       -3673
386224


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   17178
71032659  
00016717  00000-0  10270-3 0  9149
2 25544  51
6424 345
8794 0004861 324
9430  35
1402 15
54095351 23387


Satellite: ISS
Catalog Number: 25544
Epoch time:      17178
71032659   =   yrday
fracday
Element set:     914
Inclination:       51
6424  deg
RA of node:       345
8794  deg
Eccentricity:     
0004861     
Arg of perigee:   324
9430  deg
Mean anomaly:      35
1402  deg
Mean motion:   15
54095351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2338
Checksum:              310


Coasting Arc #16 (Orbit 2353)
---------------------------------------

Vector Time (GMT): 2017/179/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922015
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3477156
85                 A    =         6778612
00  meter
 Y    =        2980561
25  meter          E    =           
0002506
 Z    =        4995219
58                 I    =           51
50531
 XDOT =      -6269
334956                 Wp   =           67
28171
 YDOT =       3930
979174  meter/sec      RA   =          340
44169  deg
 ZDOT =       2018
656865                 TA   =            3
06972
                                          MA   =            3
06818
                                          Ha   =            220
795  n
mi
                                          Hp   =            215
453

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11407994
93                 X    =         3419304
96
 Y    =        9778744
26  feet           Y    =         3019121
24  meter
 Z    =       16388515
68                 Z    =         5011970
10
 XDOT =     -20568
684239                 XDOT =       -6322
631782
 YDOT =      12896
913302  feet/sec       YDOT =        3860
573033  meter/sec
 ZDOT =       6622
889977                 ZDOT =        1988
073643

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8078580
85                 X    =        -2462351
44
 Y    =      -12573480
10  feet           Y    =        -3832396
73  meter
 Z    =       16461888
20                 Z    =         5017583
52
 XDOT =      22498
027667                 XDOT =        6857
398833
 YDOT =      -5962
518567  feet/sec       YDOT =       -1817
375659  meter/sec
 ZDOT =       6487
107271                 ZDOT =        1977
270296


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   17179
73917321  
00016717  00000-0  10270-3 0  9151
2 25544  51
6424 340
7512 0004909 329
1072  30
9791 15
54137672 23546


Satellite: ISS
Catalog Number: 25544
Epoch time:      17179
73917321   =   yrday
fracday
Element set:     915
Inclination:       51
6424  deg
RA of node:       340
7512  deg
Eccentricity:     
0004909     
Arg of perigee:   329
1072  deg
Mean anomaly:      30
9791  deg
Mean motion:   15
54137672  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2354
Checksum:              311
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