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

 
Date: June 13th 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


165/09:20:13 000 0 0 0 0 0 0
N/A 0 0 0 0 219 5
000/00:00:00 000 0 0 0 0 216 7

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 6
000/00:00:00 000 0 0 0 0 216 4

Coasting Arc #1 (Orbit 2102)
---------------------------------------

Vector Time (GMT): 2017/163/12:53:26
982
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2250601
09                 A    =         6788840
51  meter
 Y    =        6247052
36  meter          E    =           
0009980
 Z    =        1385281
35                 I    =           51
98885
 XDOT =      -4952
805126                 Wp   =           46
45748
 YDOT =        486
080271  meter/sec      RA   =           60
80307  deg
 ZDOT =       5835
036828                 TA   =          328
56552
                                          MA   =          328
62512
                                          Ha   =            219
435  n
mi
                                          Hp   =            216
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7383861
85                 X    =         2173848
62
 Y    =       20495578
62  feet           Y    =         6271790
76  meter
 Z    =        4544886
32                 Z    =         1396028
54
 XDOT =     -16249
360651                 XDOT =       -4986
216261
 YDOT =       1594
751544  feet/sec       YDOT =         430
507011  meter/sec
 ZDOT =      19143
821613                 ZDOT =        5810
896535

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20002744
26                 X    =         6096836
45
 Y    =       -8605658
10  feet           Y    =        -2623004
59  meter
 Z    =        4591189
50                 Z    =         1399394
56
 XDOT =       1977
023872                 XDOT =         602
596876
 YDOT =      14785
627579  feet/sec       YDOT =        4506
659286  meter/sec
 ZDOT =      19037
107295                 ZDOT =        5802
510303


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   17163
59870279  
00016717  00000-0  10270-3 0  9002
2 25544  51
6425  61
2068 0004789 270
7591  89
3013 15
54011823 21037


Satellite: ISS
Catalog Number: 25544
Epoch time:      17163
59870279   =   yrday
fracday
Element set:     900
Inclination:       51
6425  deg
RA of node:        61
2068  deg
Eccentricity:     
0004789     
Arg of perigee:   270
7591  deg
Mean anomaly:      89
3013  deg
Mean motion:   15
54011823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2103
Checksum:              303


Coasting Arc #2 (Orbit 2117)
---------------------------------------

Vector Time (GMT): 2017/164/12:53:26
982
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1289123
20                 A    =         6786034
67  meter
 Y    =       -5982751
79  meter          E    =           
0001734
 Z    =       -2929039
40                 I    =           51
96319
 XDOT =       5627
798936                 Wp   =          205
82448
 YDOT =       1259
439335  meter/sec      RA   =           55
85199  deg
 ZDOT =      -5049
779323                 TA   =            7
41315
                                          MA   =            7
41059
                                          Ha   =            219
387  n
mi
                                          Hp   =            216
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4229406
83                 X    =        -1207898
88
 Y    =      -19628450
76  feet           Y    =        -5996713
10  meter
 Z    =       -9609709
33                 Z    =        -2935105
06
 XDOT =      18463
907269                 XDOT =        5637
826593
 YDOT =       4132
018814  feet/sec       YDOT =        1322
429924  meter/sec
 ZDOT =     -16567
517464                 ZDOT =       -5022
416740

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19239313
52                 X    =        -5864142
76
 Y    =        5702525
93  feet           Y    =         1738129
90  meter
 Z    =       -9635376
90                 Z    =        -2936862
88
 XDOT =       3067
961717                 XDOT =         935
114731
 YDOT =     -17436
842679  feet/sec       YDOT =       -5314
749649  meter/sec
 ZDOT =     -16446
896709                 ZDOT =       -5013
014117


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   17164
56330185  
00016717  00000-0  10270-3 0  9018
2 25544  51
6429  56
3997 0004952 273
2695  86
7891 15
54003745 21187


Satellite: ISS
Catalog Number: 25544
Epoch time:      17164
56330185   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:        56
3997  deg
Eccentricity:     
0004952     
Arg of perigee:   273
2695  deg
Mean anomaly:      86
7891  deg
Mean motion:   15
54003745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2118
Checksum:              329


Coasting Arc #3 (Orbit 2130)
---------------------------------------

Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5026295
23                 A    =         6781121
91  meter
 Y    =         651743
13  meter          E    =           
0004963
 Z    =       -4510084
02                 I    =           51
92886
 XDOT =       2038
407548                 Wp   =          122
13725
 YDOT =       6642
585632  meter/sec      RA   =           51
57548  deg
 ZDOT =       3231
649712                 TA   =          180
25316
                                          MA   =          180
25341
                                          Ha   =            219
532  n
mi
                                          Hp   =            216
671

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16490469
90                 X    =         5040541
41
 Y    =        2138264
85  feet           Y    =          708030
76  meter
 Z    =      -14796863
59                 Z    =        -4485633
22
 XDOT =       6687
688806                 XDOT =        1948
279188
 YDOT =      21793
259948  feet/sec       YDOT =        6664
876161  meter/sec
 ZDOT =      10602
525301                 ZDOT =        3241
333527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13746751
45                 X    =         4190009
84
 Y    =       -9524459
25  feet           Y    =        -2903055
18  meter
 Z    =      -14688990
66                 Z    =        -4477204
35
 XDOT =      18818
760763                 XDOT =        5735
958281
 YDOT =      10745
785600  feet/sec       YDOT =        3275
315451  meter/sec
 ZDOT =      10644
043642                 ZDOT =        3244
304502


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
39928538  
00016717  00000-0  10270-3 0  9026
2 25544  51
6410  52
2313 0004696 277
8922  82
1698 15
54030515 21317


Satellite: ISS
Catalog Number: 25544
Epoch time:      17165
39928538   =   yrday
fracday
Element set:     902
Inclination:       51
6410  deg
RA of node:        52
2313  deg
Eccentricity:     
0004696     
Arg of perigee:   277
8922  deg
Mean anomaly:      82
1698  deg
Mean motion:   15
54030515  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2131
Checksum:              307


Coasting Arc #4 (Orbit 2146)
---------------------------------------

Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5529926
90                 A    =         6784861
73  meter
 Y    =       -1989182
23  meter          E    =           
0007941
 Z    =        3384778
72                 I    =           51
92030
 XDOT =       -686
445705                 Wp   =           84
43246
 YDOT =      -6047
004401  meter/sec      RA   =           46
60991  deg
 ZDOT =      -4665
084502                 TA   =           56
21816
                                          MA   =           56
14255
                                          Ha   =            219
623  n
mi
                                          Hp   =            216
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18142804
79                 X    =        -5523713
90
 Y    =       -6526188
43  feet           Y    =        -2050987
24  meter
 Z    =       11104917
06                 Z    =         3357930
99
 XDOT =      -2252
118456                 XDOT =        -596
114865
 YDOT =     -19839
253283  feet/sec       YDOT =       -6054
175138  meter/sec
 ZDOT =     -15305
395347                 ZDOT =       -4668
200274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17766019
32                 X    =        -5415082
69
 Y    =        7663704
36  feet           Y    =         2335897
09  meter
 Z    =       10986713
64                 Z    =         3348750
32
 XDOT =     -14556
140005                 XDOT =       -4436
711473
 YDOT =     -11735
939486  feet/sec       YDOT =       -3577
114355  meter/sec
 ZDOT =     -15318
009964                 ZDOT =       -4668
929437


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
42818437  
00016717  00000-0  10270-3 0  9038
2 25544  51
6410  47
1038 0004734 281
8972  78
1649 15
54029940 21475


Satellite: ISS
Catalog Number: 25544
Epoch time:      17166
42818437   =   yrday
fracday
Element set:     903
Inclination:       51
6410  deg
RA of node:        47
1038  deg
Eccentricity:     
0004734     
Arg of perigee:   281
8972  deg
Mean anomaly:      78
1649  deg
Mean motion:   15
54029940  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2147
Checksum:              317


Coasting Arc #5 (Orbit 2161)
---------------------------------------

Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 907581
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5732081
62                 A    =         6788067
66  meter
 Y    =        3069617
02  meter          E    =           
0006743
 Z    =       -1933873
21                 I    =           51
90852
 XDOT =       -856
470274                 Wp   =          357
91154
 YDOT =       5139
666759  meter/sec      RA   =           41
65129  deg
 ZDOT =       5625
471476                 TA   =          340
85203
                                          MA   =          340
87736
                                          Ha   =            219
679  n
mi
                                          Hp   =            216
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18806042
06                 X    =         5706724
13
 Y    =       10070921
98  feet           Y    =         3133575
44  meter
 Z    =       -6344728
39                 Z    =        -1906089
86
 XDOT =      -2809
941845                 XDOT =        -941
205475
 YDOT =      16862
423751  feet/sec       YDOT =        5129
614817  meter/sec
 ZDOT =      18456
271246                 ZDOT =        5621
105686

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20550005
21                 X    =         6263641
59
 Y    =       -5858561
89  feet           Y    =        -1785689
67  meter
 Z    =       -6222604
29                 Z    =        -1896649
79
 XDOT =       9186
626488                 XDOT =        2800
083754
 YDOT =      12663
344678  feet/sec       YDOT =        3859
787458  meter/sec
 ZDOT =      18436
009585                 ZDOT =        5619
295721


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
39277370  
00016717  00000-0  10270-3 0  9041
2 25544  51
6414  42
2958 0004833 285
2180  74
8438 15
54036957 21627


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
39277370   =   yrday
fracday
Element set:     904
Inclination:       51
6414  deg
RA of node:        42
2958  deg
Eccentricity:     
0004833     
Arg of perigee:   285
2180  deg
Mean anomaly:      74
8438  deg
Mean motion:   15
54036957  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2162
Checksum:              322


Coasting Arc #6 (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    =       -5440320
12                 A    =         6789473
78  meter
 Y    =       -3984780
81  meter          E    =           
0009034
 Z    =         742569
04                 I    =           51
91196
 XDOT =       2278
018987                 Wp   =          139
18014
 YDOT =      -4230
169911  meter/sec      RA   =           41
17207  deg
 ZDOT =      -5976
131321                 TA   =           32
82606
                                          MA   =           32
76997
                                          Ha   =            219
631  n
mi
                                          Hp   =            216
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17848819
30                 X    =        -5398963
95
 Y    =      -13073427
84  feet           Y    =        -4045386
99  meter
 Z    =        2436250
14                 Z    =          716241
75
 XDOT =       7473
815574                 XDOT =        2354
181641
 YDOT =     -13878
510207  feet/sec       YDOT =       -4204
269152  meter/sec
 ZDOT =     -19606
730056                 ZDOT =       -5964
880824

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16057562
04                 X    =        -4894344
91
 Y    =       15238080
07  feet           Y    =         4644566
81  meter
 Z    =        2320732
13                 Z    =          707359
15
 XDOT =     -11185
642008                 XDOT =       -3409
383684
 YDOT =      -8790
827947  feet/sec       YDOT =       -2679
444358  meter/sec
 ZDOT =     -19556
234256                 ZDOT =       -5960
740201


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
52138541  
00016717  00000-0  10270-3 0  9053
2 25544  51
6428  41
6561 0004788 284
2332  75
8289 15
54005823 21647


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
52138541   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:        41
6561  deg
Eccentricity:     
0004788     
Arg of perigee:   284
2332  deg
Mean anomaly:      75
8289  deg
Mean motion:   15
54005823  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2164
Checksum:              314


Coasting Arc #7 (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    =       -3163762
92                 A    =         6786510
41  meter
 Y    =       -5388936
20  meter          E    =           
0001781
 Z    =       -2644015
89                 I    =           51
89442
 XDOT =       5551
655926                 Wp   =          195
04340
 YDOT =       -688
705615  meter/sec      RA   =           40
20373  deg
 ZDOT =      -5240
162804                 TA   =           14
63999
                                          MA   =           14
63483
                                          Ha   =            219
574  n
mi
                                          Hp   =            216
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10379799
59                 X    =        -3090423
95
 Y    =      -17680236
88  feet           Y    =        -5423905
24  meter
 Z    =       -8674592
81                 Z    =        -2659206
83
 XDOT =      18214
094244                 XDOT =        5584
398734
 YDOT =      -2259
532858  feet/sec       YDOT =        -626
439682  meter/sec
 ZDOT =     -17192
135184                 ZDOT =       -5213
115120

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         731232
72                 X    =          222879
73
 Y    =       20460835
72  feet           Y    =         6236462
73  meter
 Z    =       -8740656
52                 Z    =        -2664152
11
 XDOT =     -15723
597059                 XDOT =       -4792
552384
 YDOT =      -6730
049894  feet/sec       YDOT =       -2051
319208  meter/sec
 ZDOT =     -17072
545307                 ZDOT =       -5203
711809


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
71430155  
00016717  00000-0  10270-3 0  9061
2 25544  51
6394  40
6890 0004656 284
3718  75
6917 15
54062657 21673


Satellite: ISS
Catalog Number: 25544
Epoch time:      17167
71430155   =   yrday
fracday
Element set:     906
Inclination:       51
6394  deg
RA of node:        40
6890  deg
Eccentricity:     
0004656     
Arg of perigee:   284
3718  deg
Mean anomaly:      75
6917  deg
Mean motion:   15
54062657  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2167
Checksum:              328


Coasting Arc #8 (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    =        1923185
94                 A    =         6782842
49  meter
 Y    =        5160699
12  meter          E    =           
0006355
 Z    =        3954322
05                 I    =           51
85646
 XDOT =      -6479
667336                 Wp   =           96
27505
 YDOT =       -688
844924  meter/sec      RA   =           35
23796  deg
 ZDOT =       4044
137866                 TA   =          311
59197
                                          MA   =          311
64641
                                          Ha   =            219
596  n
mi
                                          Hp   =            216
432

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6309665
15                 X    =         1846126
50
 Y    =       16931427
57  feet           Y    =         5181774
29  meter
 Z    =       12973497
55                 Z    =         3963477
60
 XDOT =     -21258
751104                 XDOT =       -6491
127398
 YDOT =      -2259
989907  feet/sec       YDOT =        -761
369381  meter/sec
 ZDOT =      13268
168852                 ZDOT =        4012
633669

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2217743
25                 X    =          675968
14
 Y    =      -17903678
54  feet           Y    =        -5457041
22  meter
 Z    =       13012942
11                 Z    =         3966344
75
 XDOT =      16637
139873                 XDOT =        5071
000233
 YDOT =      11618
388579  feet/sec       YDOT =        3541
284839  meter/sec
 ZDOT =      13129
166934                 ZDOT =        4001
770081


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
74319115  
00016717  00000-0  10270-3 0  9078
2 25544  51
6391  35
5599 0004661 285
8219  74
2419 15
54064372 21833


Satellite: ISS
Catalog Number: 25544
Epoch time:      17168
74319115   =   yrday
fracday
Element set:     907
Inclination:       51
6391  deg
RA of node:        35
5599  deg
Eccentricity:     
0004661     
Arg of perigee:   285
8219  deg
Mean anomaly:      74
2419  deg
Mean motion:   15
54064372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2183
Checksum:              325


Coasting Arc #9 (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    =        -436244
30                 A    =         6779441
53  meter
 Y    =       -4696028
08  meter          E    =           
0008779
 Z    =       -4878189
86                 I    =           51
81843
 XDOT =       7017
287758                 Wp   =           53
91404
 YDOT =       1878
465205  meter/sec      RA   =           30
26275  deg
 ZDOT =      -2433
873160                 TA   =          192
23727
                                          MA   =          192
25861
                                          Ha   =            219
770  n
mi
                                          Hp   =            216
347

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1431247
69                 X    =         -360003
66
 Y    =      -15406916
28  feet           Y    =        -4700479
74  meter
 Z    =      -16004559
91                 Z    =        -4880124
25
 XDOT =      23022
597631                 XDOT =        7007
583357
 YDOT =       6162
943586  feet/sec       YDOT =        1956
883227  meter/sec
 ZDOT =      -7985
148162                 ZDOT =       -2399
808552

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5627661
59                 X    =        -1715311
25
 Y    =       14405084
34  feet           Y    =         4390669
71  meter
 Z    =      -16012196
83                 Z    =        -4880517
59
 XDOT =     -16915
996620                 XDOT =       -5155
995770
 YDOT =     -15325
041612  feet/sec       YDOT =       -4671
072683  meter/sec
 ZDOT =      -7835
077252                 ZDOT =       -2388
131546


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
70777407  
00016717  00000-0  10270-3 0  9088
2 25544  51
6397  30
7536 0004533 290
6780  69
3886 15
54060942 21980


Satellite: ISS
Catalog Number: 25544
Epoch time:      17169
70777407   =   yrday
fracday
Element set:     908
Inclination:       51
6397  deg
RA of node:        30
7536  deg
Eccentricity:     
0004533     
Arg of perigee:   290
6780  deg
Mean anomaly:      69
3886  deg
Mean motion:   15
54060942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2198
Checksum:              342


Coasting Arc #10 (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    =       -1188778
85                 A    =         6777706
56  meter
 Y    =        4054406
76  meter          E    =           
0001842
 Z    =        5300958
35                 I    =           51
78406
 XDOT =      -7097
160890                 Wp   =          297
02216
 YDOT =      -2842
861577  meter/sec      RA   =           25
27572  deg
 ZDOT =        583
728192                 TA   =          147
42312
                                          MA   =          147
41175
                                          Ha   =            219
969  n
mi
                                          Hp   =            216
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3900193
08                 X    =        -1259777
62
 Y    =       13301859
46  feet           Y    =         4040715
53  meter
 Z    =       17391595
64                 Z    =         5295011
53
 XDOT =     -23284
648589                 XDOT =       -7067
679278
 YDOT =      -9326
973677  feet/sec       YDOT =       -2922
062056  meter/sec
 ZDOT =       1915
118739                 ZDOT =         549
323407

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9309501
47                 X    =         2837536
05
 Y    =      -10316210
85  feet           Y    =        -3144381
07  meter
 Z    =       17364548
53                 Z    =         5292714
39
 XDOT =      16332
133827                 XDOT =        4978
034390
 YDOT =      17701
764275  feet/sec       YDOT =        5395
497751  meter/sec
 ZDOT =       1763
743634                 ZDOT =         537
589060


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
73665962  
00016717  00000-0  10270-3 0  9096
2 25544  51
6400  25
6242 0004645 294
5687  65
4982 15
54038277 22144


Satellite: ISS
Catalog Number: 25544
Epoch time:      17170
73665962   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:        25
6242  deg
Eccentricity:     
0004645     
Arg of perigee:   294
5687  deg
Mean anomaly:      65
4982  deg
Mean motion:   15
54038277  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2214
Checksum:              324


Coasting Arc #11 (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    =        2819356
14                 A    =         6778139
88  meter
 Y    =       -3325693
95  meter          E    =           
0009644
 Z    =       -5198188
87                 I    =           51
75677
 XDOT =       6648
257998                 Wp   =           91
59086
 YDOT =       3569
857658  meter/sec      RA   =           20
28687  deg
 ZDOT =       1323
772559                 TA   =          191
10759
                                          MA   =          191
12890
                                          Ha   =            220
000  n
mi
                                          Hp   =            216
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9249856
10                 X    =         2881585
89
 Y    =      -10911069
39  feet           Y    =        -3293817
44  meter
 Z    =      -17054425
44                 Z    =        -5184342
41
 XDOT =      21811
870071                 XDOT =        6601
414496
 YDOT =      11712
131423  feet/sec       YDOT =        3643
940912  meter/sec
 ZDOT =       4343
085825                 ZDOT =        1355
954709

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13021255
71                 X    =        -3968878
74
 Y    =        6096061
76  feet           Y    =         1858079
62  meter
 Z    =      -16992634
61                 Z    =        -5179355
03
 XDOT =     -14592
517950                 XDOT =       -4447
799471
 YDOT =     -18686
425380  feet/sec       YDOT =       -5695
622456  meter/sec
 ZDOT =       4484
493367                 ZDOT =        1366
873578


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
70123503  
00016717  00000-0  10270-3 0  9106
2 25544  51
6409  20
8175 0004587 298
3033  61
7657 15
54070396 22299


Satellite: ISS
Catalog Number: 25544
Epoch time:      17171
70123503   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:        20
8175  deg
Eccentricity:     
0004587     
Arg of perigee:   298
3033  deg
Mean anomaly:      61
7657  deg
Mean motion:   15
54070396  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2229
Checksum:              299


Coasting Arc #12 (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    =       -4327773
78                 A    =         6780908
37  meter
 Y    =        2543550
60  meter          E    =           
0007192
 Z    =        4558025
43                 I    =           51
73410
 XDOT =      -5688
285245                 Wp   =           36
14029
 YDOT =      -4096
577597  meter/sec      RA   =           15
29877  deg
 ZDOT =      -3106
721401                 TA   =           84
96905
                                          MA   =           84
88695
                                          Ha   =            220
242  n
mi
                                          Hp   =            216
251

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14198732
87                 X    =        -4378035
64
 Y    =        8344982
27  feet           Y    =         2494872
83  meter
 Z    =       14954151
67                 Z    =         4536880
51
 XDOT =     -18662
353166                 XDOT =       -5626
962401
 YDOT =     -13440
215213  feet/sec       YDOT =       -4159
844549  meter/sec
 ZDOT =     -10192
655516                 ZDOT =       -3134
205220

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16431722
86                 X    =         5008389
13
 Y    =       -2009918
54  feet           Y    =         -612623
17  meter
 Z    =       14860286
26                 Z    =         4529415
25
 XDOT =      11614
547535                 XDOT =        3540
114089
 YDOT =      18502
720632  feet/sec       YDOT =        5639
629249  meter/sec
 ZDOT =     -10313
204537                 ZDOT =       -3143
464743


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
73011445  
00016717  00000-0  10270-3 0  9112
2 25544  51
6403  15
6886 0004528 301
9429  58
1283 15
54032602 22450


Satellite: ISS
Catalog Number: 25544
Epoch time:      17172
73011445   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:        15
6886  deg
Eccentricity:     
0004528     
Arg of perigee:   301
9429  deg
Mean anomaly:      58
1283  deg
Mean motion:   15
54032602  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2245
Checksum:              286


Coasting Arc #13 (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    =        5552637
54                 A    =         6784551
06  meter
 Y    =       -1773151
27  meter          E    =           
0002881
 Z    =       -3470126
43                 I    =           51
71528
 XDOT =       4268
248032                 Wp   =           21
21069
 YDOT =       4439
569341  meter/sec      RA   =           10
31823  deg
 ZDOT =       4565
026537                 TA   =          298
11963
                                          MA   =          298
14875
                                          Ha   =            220
333  n
mi
                                          Hp   =            216
289

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18217314
75                 X    =         5588908
97
 Y    =       -5817425
42  feet           Y    =        -1710854
56  meter
 Z    =      -11384929
23                 Z    =        -3443065
44
 XDOT =      14003
438424                 XDOT =        4196
111578
 YDOT =      14565
516211  feet/sec       YDOT =        4486
895718  meter/sec
 ZDOT =      14977
121184                 ZDOT =        4585
585995

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19130684
97                 X    =        -5831032
78
 Y    =       -1563384
90  feet           Y    =         -476519
72  meter
 Z    =      -11265093
39                 Z    =        -3433600
47
 XDOT =      -7446
003779                 XDOT =       -2269
541952
 YDOT =     -17361
069645  feet/sec       YDOT =       -5291
654028  meter/sec
 ZDOT =      15067
022029                 ZDOT =        4592
428314


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
69468456  
00016717  00000-0  10270-3 0  9127
2 25544  51
6408  10
8811 0004740 305
6554  54
4157 15
54051946 22604


Satellite: ISS
Catalog Number: 25544
Epoch time:      17173
69468456   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:        10
8811  deg
Eccentricity:     
0004740     
Arg of perigee:   305
6554  deg
Mean anomaly:      54
4157  deg
Mean motion:   15
54051946  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2260
Checksum:              305


Coasting Arc #14 (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    =       -6402372
23                 A    =         6787875
10  meter
 Y    =         995944
19  meter          E    =           
0009568
 Z    =        2010358
98                 I    =           51
69481
 XDOT =      -2478
540407                 Wp   =          103
46296
 YDOT =      -4650
392619  meter/sec      RA   =            5
34473  deg
 ZDOT =      -5569
446617                 TA   =           54
35003
                                          MA   =           54
26097
                                          Ha   =            220
355  n
mi
                                          Hp   =            216
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21005158
24                 X    =        -6422798
65
 Y    =        3267533
43  feet           Y    =          924233
97  meter
 Z    =        6595665
95                 Z    =         1979208
76
 XDOT =      -8131
694248                 XDOT =       -2399
300621
 YDOT =     -15257
193631  feet/sec       YDOT =       -4677
665331  meter/sec
 ZDOT =     -18272
462654                 ZDOT =       -5581
294945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20794641
37                 X    =         6338206
69
 Y    =        4612407
99  feet           Y    =         1405861
96  meter
 Z    =        6457928
45                 Z    =         1968376
59
 XDOT =       2248
753563                 XDOT =         685
420086
 YDOT =      15611
628300  feet/sec       YDOT =        4758
424306  meter/sec
 ZDOT =     -18323
855614                 ZDOT =       -5585
111191


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
72355710  
00016717  00000-0  10270-3 0  9131
2 25544  51
6413   5
7522 0004678 309
2307  50
8430 15
54064046 22764


Satellite: ISS
Catalog Number: 25544
Epoch time:      17174
72355710   =   yrday
fracday
Element set:     913
Inclination:       51
6413  deg
RA of node:         5
7522  deg
Eccentricity:     
0004678     
Arg of perigee:   309
2307  deg
Mean anomaly:      50
8430  deg
Mean motion:   15
54064046  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2276
Checksum:              289


Coasting Arc #15 (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    =        6767377
43                 A    =         6789457
70  meter
 Y    =        -244814
69  meter          E    =           
0012565
 Z    =        -365858
09                 I    =           51
66823
 XDOT =        492
412168                 Wp   =           20
34568
 YDOT =       4749
870405  meter/sec      RA   =             
37640  deg
 ZDOT =       6003
306047                 TA   =          335
71079
                                          MA   =          335
76997
                                          Ha   =            220
564  n
mi
                                          Hp   =            215
916

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22202681
86                 X    =         6771389
20
 Y    =        -803197
81  feet           Y    =         -169114
80  meter
 Z    =       -1200321
82                 Z    =         -332974
72
 XDOT =       1615
525487                 XDOT =         410
100307
 YDOT =      15583
564322  feet/sec       YDOT =        4754
915640  meter/sec
 ZDOT =      19695
885982                 ZDOT =        6005
498906

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21103613
23                 X    =        -6432381
31
 Y    =       -6969167
32  feet           Y    =        -2124202
20  meter
 Z    =       -1055081
16                 Z    =         -321588
74
 XDOT =       3516
779685                 XDOT =        1071
914448
 YDOT =     -13590
956587  feet/sec       YDOT =       -4142
523568  meter/sec
 ZDOT =      19704
626652                 ZDOT =        6005
970204


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
68812190  
00016717  00000-0  10270-3 0  9148
2 25544  51
6417    
9444 0004719 315
3504  44
7268 15
54069545 22918


Satellite: ISS
Catalog Number: 25544
Epoch time:      17175
68812190   =   yrday
fracday
Element set:     914
Inclination:       51
6417  deg
RA of node:          
9444  deg
Eccentricity:     
0004719     
Arg of perigee:   315
3504  deg
Mean anomaly:      44
7268  deg
Mean motion:   15
54069545  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2291
Checksum:              310


Coasting Arc #16 (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    =       -6632647
00                 A    =         6788644
39  meter
 Y    =        -529355
13  meter          E    =           
0003983
 Z    =       -1337348
31                 I    =           51
63285
 XDOT =       1549
262781                 Wp   =          147
40447
 YDOT =      -4744
393468  meter/sec      RA   =          355
40750  deg
 ZDOT =      -5817
055405                 TA   =           47
15146
                                          MA   =           47
11801
                                          Ha   =            220
584  n
mi
                                          Hp   =            215
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21760652
89                 X    =        -6619738
55
 Y    =       -1736729
44  feet           Y    =         -603453
50  meter
 Z    =       -4387625
69                 Z    =        -1369536
07
 XDOT =       5082
883141                 XDOT =        1630
456808
 YDOT =     -15565
595366  feet/sec       YDOT =       -4726
613668  meter/sec
 ZDOT =     -19084
827444                 ZDOT =       -5809
333176

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19926687
88                 X    =         6073654
47
 Y    =        8843244
27  feet           Y    =         2695420
85  meter
 Z    =       -4529640
56                 Z    =        -1380634
44
 XDOT =      -9429
009306                 XDOT =       -2873
962036
 YDOT =      11507
502940  feet/sec       YDOT =        3507
486896  meter/sec
 ZDOT =     -19049
793485                 ZDOT =       -5806
377054


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
71698894  
00016717  00000-0  10270-3 0  9157
2 25544  51
6414 355
8162 0004697 317
8052  42
2739 15
54084815 23075


Satellite: ISS
Catalog Number: 25544
Epoch time:      17176
71698894   =   yrday
fracday
Element set:     915
Inclination:       51
6414  deg
RA of node:       355
8162  deg
Eccentricity:     
0004697     
Arg of perigee:   317
8052  deg
Mean anomaly:      42
2739  deg
Mean motion:   15
54084815  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2307
Checksum:              336


Coasting Arc #17 (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    =        5993461
04                 A    =         6785773
04  meter
 Y    =        1308456
40  meter          E    =           
0011642
 Z    =        2884164
14                 I    =           51
59243
 XDOT =      -3446
016676                 Wp   =           60
84058
 YDOT =       4638
546053  meter/sec      RA   =          350
43094  deg
 ZDOT =       5046
827210                 TA   =          332
04471
                                          MA   =          332
10719
                                          Ha   =            220
593  n
mi
                                          Hp   =            215
664

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19663586
07                 X    =         5964374
41
 Y    =        4292835
97  feet           Y    =         1375316
33  meter
 Z    =        9462480
78                 Z    =         2913207
68
 XDOT =     -11305
828990                 XDOT =       -3522
144700
 YDOT =      15218
326947  feet/sec       YDOT =        4599
584021  meter/sec
 ZDOT =      16557
832054                 ZDOT =        5029
903464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17248339
36                 X    =        -5257293
84
 Y    =      -10253853
76  feet           Y    =        -3125374
62  meter
 Z    =        9590457
38                 Z    =         2923171
41
 XDOT =      14882
025779                 XDOT =        4536
041457
 YDOT =      -9587
929221  feet/sec       YDOT =       -2922
400827  meter/sec
 ZDOT =      16482
197679                 ZDOT =        5023
773853


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
74585196  
00016717  00000-0  10270-3 0  9162
2 25544  51
6427 350
6877 0004713 322
1857  37
8964 15
54105249 23239


Satellite: ISS
Catalog Number: 25544
Epoch time:      17177
74585196   =   yrday
fracday
Element set:     916
Inclination:       51
6427  deg
RA of node:       350
6877  deg
Eccentricity:     
0004713     
Arg of perigee:   322
1857  deg
Mean anomaly:      37
8964  deg
Mean motion:   15
54105249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2323
Checksum:              335
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