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

 
Date: December 18th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


353/08:43:02 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 6

361/06:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 8
000/00:00:00 000 0 0 0 0 215 4

362/01:04:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 215 4

364/11:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 215 2

Coasting Arc #1 (Orbit 1042)
---------------------------------------

Vector Time (GMT): 2017/352/14:05:06
902
Vector Time (MET): N/A
Weight (LBS)     : 923966
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4146903
97                 A    =         6784370
09  meter
 Y    =       -4166124
15  meter          E    =           
0009535
 Z    =        3379724
64                 I    =           51
51812
 XDOT =       5782
897362                 Wp   =           93
46411
 YDOT =      -1993
566619  meter/sec      RA   =          197
93586  deg
 ZDOT =       4626
302036                 TA   =          306
08508
                                          MA   =          306
17334
                                          Ha   =            219
876  n
mi
                                          Hp   =            215
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13605327
97                 X    =        -4116426
11
 Y    =      -13668386
32  feet           Y    =        -4212327
65  meter
 Z    =       11088335
44                 Z    =         3359653
77
 XDOT =      18972
760374                 XDOT =        5782
287818
 YDOT =      -6540
572898  feet/sec       YDOT =       -1928
902257  meter/sec
 ZDOT =      15178
156286                 ZDOT =        4654
391901

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5715072
85                 X    =         1741954
20
 Y    =      -18472253
88  feet           Y    =        -5630342
98  meter
 Z    =       10999758
89                 Z    =         3352726
51
 XDOT =      13236
154201                 XDOT =        4034
379800
 YDOT =      13231
103689  feet/sec       YDOT =        4032
840405  meter/sec
 ZDOT =      15303
213527                 ZDOT =        4664
419483


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   17352
64420480  
00016717  00000-0  10270-3 0  9003
2 25544  51
6357 198
7788 0003099 256
7529 103
3278 15
54194944 10432


Satellite: ISS
Catalog Number: 25544
Epoch time:      17352
64420480   =   yrday
fracday
Element set:     900
Inclination:       51
6357  deg
RA of node:       198
7788  deg
Eccentricity:     
0003099     
Arg of perigee:   256
7529  deg
Mean anomaly:     103
3278  deg
Mean motion:   15
54194944  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1043
Checksum:              329


Coasting Arc #2 (Orbit 1054)
---------------------------------------

Vector Time (GMT): 2017/353/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1718507
64                 A    =         6779197
37  meter
 Y    =       -4407003
59  meter          E    =           
0004988
 Z    =        4854811
91                 I    =           51
52944
 XDOT =       7274
662156                 Wp   =          139
25302
 YDOT =       -162
681221  meter/sec      RA   =          194
05720  deg
 ZDOT =       2422
302415                 TA   =          286
92713
                                          MA   =          286
98181
                                          Ha   =            219
905  n
mi
                                          Hp   =            215
616

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5638148
43                 X    =        -1692681
89
 Y    =      -14458673
18  feet           Y    =        -4426077
28  meter
 Z    =       15927860
59                 Z    =         4846526
15
 XDOT =      23867
001824                 XDOT =        7264
174289
 YDOT =       -533
731040  feet/sec       YDOT =         -81
389902  meter/sec
 ZDOT =       7947
186401                 ZDOT =        2457
614950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13430499
16                 X    =         4093616
14
 Y    =        7849551
66  feet           Y    =         2392543
34  meter
 Z    =       15891662
02                 Z    =         4843778
58
 XDOT =     -17857
043645                 XDOT =       -5442
826903
 YDOT =      14112
212188  feet/sec       YDOT =        4301
402275  meter/sec
 ZDOT =       8104
092062                 ZDOT =        2470
127260


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   17353
41578779  
00016717  00000-0  10270-3 0  9015
2 25544  51
6399 194
9356 0002853 266
1535  93
9291 15
54188586 10553


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
41578779   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:       194
9356  deg
Eccentricity:     
0002853     
Arg of perigee:   266
1535  deg
Mean anomaly:      93
9291  deg
Mean motion:   15
54188586  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1055
Checksum:              352


Coasting Arc #3 (Orbit 1069)
---------------------------------------

Vector Time (GMT): 2017/354/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -82774
31                 A    =         6777199
52  meter
 Y    =        4242891
66  meter          E    =           
0011786
 Z    =       -5294315
64                 I    =           51
55450
 XDOT =      -7601
104901                 Wp   =           84
60621
 YDOT =       -794
644613  meter/sec      RA   =          189
05211  deg
 ZDOT =       -517
903154                 TA   =          180
44096
                                          MA   =          180
44200
                                          Ha   =            219
777  n
mi
                                          Hp   =            215
580

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -271569
27                 X    =         -104496
24
 Y    =       13920248
22  feet           Y    =         4241845
16  meter
 Z    =      -17369801
98                 Z    =        -5294770
01
 XDOT =     -24938
008205                 XDOT =       -7589
138334
 YDOT =      -2607
101749  feet/sec       YDOT =        -879
578396  meter/sec
 ZDOT =      -1699
157329                 ZDOT =        -554
797841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8640349
32                 X    =        -2633578
47
 Y    =      -10913335
45  feet           Y    =        -3326384
65  meter
 Z    =      -17372407
84                 Z    =        -5295109
91
 XDOT =      20212
329283                 XDOT =        6160
717966
 YDOT =     -13036
523113  feet/sec       YDOT =       -3973
532245  meter/sec
 ZDOT =      -1862
986147                 ZDOT =        -567
838178


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   17354
38027658  
00016717  00000-0  10270-3 0  9028
2 25544  51
6392 190
1275 0002943 271
5377  88
5439 15
54218820 10704


Satellite: ISS
Catalog Number: 25544
Epoch time:      17354
38027658   =   yrday
fracday
Element set:     902
Inclination:       51
6392  deg
RA of node:       190
1275  deg
Eccentricity:     
0002943     
Arg of perigee:   271
5377  deg
Mean anomaly:      88
5439  deg
Mean motion:   15
54218820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1070
Checksum:              316


Coasting Arc #4 (Orbit 1085)
---------------------------------------

Vector Time (GMT): 2017/355/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1914239
38                 A    =         6777651
46  meter
 Y    =       -3962171
33  meter          E    =           
0002858
 Z    =        5155058
48                 I    =           51
58946
 XDOT =       7344
907938                 Wp   =           11
31604
 YDOT =       1666
934887  meter/sec      RA   =          184
04716  deg
 ZDOT =      -1443
318341                 TA   =           92
59809
                                          MA   =           92
56537
                                          Ha   =            219
609  n
mi
                                          Hp   =            215
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6280312
92                 X    =         1933362
60
 Y    =      -12999249
79  feet           Y    =        -3940658
61  meter
 Z    =       16912921
52                 Z    =         5164403
24
 XDOT =      24097
466989                 XDOT =        7332
732821
 YDOT =       5468
946481  feet/sec       YDOT =        1749
002744  meter/sec
 ZDOT =      -4735
296394                 ZDOT =       -1407
668694

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3629787
43                 X    =         1106359
21
 Y    =       13922014
60  feet           Y    =         4243430
05  meter
 Z    =       16954996
09                 Z    =         5167882
81
 XDOT =     -20982
618298                 XDOT =       -6395
502057
 YDOT =      11056
359024  feet/sec       YDOT =        3369
978231  meter/sec
 ZDOT =      -4577
094079                 ZDOT =       -1395
098275


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   17355
40905929  
00016717  00000-0  10270-3 0  9039
2 25544  51
6398 184
9985 0003131 274
7712  85
3083 15
54246071 10863


Satellite: ISS
Catalog Number: 25544
Epoch time:      17355
40905929   =   yrday
fracday
Element set:     903
Inclination:       51
6398  deg
RA of node:       184
9985  deg
Eccentricity:     
0003131     
Arg of perigee:   274
7712  deg
Mean anomaly:      85
3083  deg
Mean motion:   15
54246071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1086
Checksum:              326


Coasting Arc #5 (Orbit 1100)
---------------------------------------

Vector Time (GMT): 2017/356/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3610253
43                 A    =         6780472
28  meter
 Y    =        3602779
41  meter          E    =           
0006506
 Z    =       -4474400
36                 I    =           51
63176
 XDOT =      -6486
407987                 Wp   =          115
83022
 YDOT =      -2465
264760  meter/sec      RA   =          179
04848  deg
 ZDOT =       3249
562591                 TA   =          186
91128
                                          MA   =          186
92025
                                          Ha   =            219
720  n
mi
                                          Hp   =            215
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11844663
50                 X    =        -3628538
11
 Y    =       11820142
42  feet           Y    =         3562305
26  meter
 Z    =      -14679791
21                 Z    =        -4491981
79
 XDOT =     -21280
866099                 XDOT =       -6474
143295
 YDOT =      -8088
138975  feet/sec       YDOT =       -2537
731928  meter/sec
 ZDOT =      10661
294591                 ZDOT =        3218
083467

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1115750
49                 X    =          340080
75
 Y    =      -16626843
29  feet           Y    =        -5067861
83  meter
 Z    =      -14758430
59                 Z    =        -4498369
64
 XDOT =      20208
373194                 XDOT =        6159
512150
 YDOT =      -7980
627379  feet/sec       YDOT =       -2432
495225  meter/sec
 ZDOT =      10521
713516                 ZDOT =        3207
018280


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   17356
37353931  
00016717  00000-0  10270-3 0  9047
2 25544  51
6400 180
1893 0003128 280
2317  79
8483 15
54226522 11011


Satellite: ISS
Catalog Number: 25544
Epoch time:      17356
37353931   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       180
1893  deg
Eccentricity:     
0003128     
Arg of perigee:   280
2317  deg
Mean anomaly:      79
8483  deg
Mean motion:   15
54226522  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1101
Checksum:              292


Coasting Arc #6 (Orbit 1116)
---------------------------------------

Vector Time (GMT): 2017/357/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5026316
63                 A    =         6784270
19  meter
 Y    =       -3140283
03  meter          E    =           
0009653
 Z    =        3293890
87                 I    =           51
67723
 XDOT =       5114
259214                 Wp   =           87
02324
 YDOT =       3220
204095  meter/sec      RA   =          174
06237  deg
 ZDOT =      -4721
643464                 TA   =           54
71819
                                          MA   =           54
62792
                                          Ha   =            219
710  n
mi
                                          Hp   =            215
519

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16490540
12                 X    =         5045058
60
 Y    =      -10302765
83  feet           Y    =        -3083970
77  meter
 Z    =       10806728
57                 Z    =         3318352
21
 XDOT =      16779
065664                 XDOT =        5100
805138
 YDOT =      10564
974066  feet/sec       YDOT =        3277
320372  meter/sec
 ZDOT =     -15490
956248                 ZDOT =       -4696
832641

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5317022
37                 X    =        -1620628
42
 Y    =       18639815
41  feet           Y    =         5681415
74  meter
 Z    =       10915898
24                 Z    =         3327165
78
 XDOT =     -18255
576423                 XDOT =       -5564
299694
 YDOT =       3823
753507  feet/sec       YDOT =        1165
480069  meter/sec
 ZDOT =     -15381
100293                 ZDOT =       -4688
159369


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   17357
40231149  
00016717  00000-0  10270-3 0  9059
2 25544  51
6397 175
0601 0003082 287
1415  72
9400 15
54253917 11178


Satellite: ISS
Catalog Number: 25544
Epoch time:      17357
40231149   =   yrday
fracday
Element set:     905
Inclination:       51
6397  deg
RA of node:       175
0601  deg
Eccentricity:     
0003082     
Arg of perigee:   287
1415  deg
Mean anomaly:      72
9400  deg
Mean motion:   15
54253917  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1117
Checksum:              291


Coasting Arc #7 (Orbit 1131)
---------------------------------------

Vector Time (GMT): 2017/358/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6015594
11                 A    =         6787666
83  meter
 Y    =        2585386
49  meter          E    =           
0006959
 Z    =       -1773952
69                 I    =           51
72018
 XDOT =      -3353
349144                 Wp   =           13
30616
 YDOT =      -3915
451519  meter/sec      RA   =          169
08879  deg
 ZDOT =       5676
030462                 TA   =          327
23519
                                          MA   =          327
27832
                                          Ha   =            219
774  n
mi
                                          Hp   =            215
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19736201
14                 X    =        -6035440
59
 Y    =        8482239
15  feet           Y    =         2518005
15  meter
 Z    =       -5820054
74                 Z    =        -1803222
37
 XDOT =     -11001
801655                 XDOT =       -3336
887417
 YDOT =     -12845
969552  feet/sec       YDOT =       -3952
859271  meter/sec
 ZDOT =      18622
147185                 ZDOT =        5659
780812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8635228
42                 X    =         2632017
62
 Y    =      -19630663
66  feet           Y    =        -5983426
28  meter
 Z    =       -5950540
17                 Z    =        -1813724
64
 XDOT =      15462
740591                 XDOT =        4713
043332
 YDOT =       1189
462083  feet/sec       YDOT =         362
548043  meter/sec
 ZDOT =      18550
433270                 ZDOT =        5654
172061


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   17358
36678173  
00016717  00000-0  10270-3 0  9068
2 25544  51
6392 170
2515 0003203 289
4637  70
6169 15
54219452 11320


Satellite: ISS
Catalog Number: 25544
Epoch time:      17358
36678173   =   yrday
fracday
Element set:     906
Inclination:       51
6392  deg
RA of node:       170
2515  deg
Eccentricity:     
0003203     
Arg of perigee:   289
4637  deg
Mean anomaly:      70
6169  deg
Mean motion:   15
54219452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1132
Checksum:              312


Coasting Arc #8 (Orbit 1147)
---------------------------------------

Vector Time (GMT): 2017/359/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6517440
45                 A    =         6789083
32  meter
 Y    =       -1882752
08  meter          E    =           
0009425
 Z    =          35630
67                 I    =           51
75750
 XDOT =       1351
957978                 Wp   =          141
75361
 YDOT =       4550
070607  meter/sec      RA   =          164
12427  deg
 ZDOT =      -6022
336910                 TA   =           37
86323
                                          MA   =           37
79698
                                          Ha   =            219
874  n
mi
                                          Hp   =            215
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21382678
64                 X    =         6537836
43
 Y    =       -6177008
14  feet           Y    =        -1809755
57  meter
 Z    =         116898
52                 Z    =           67339
61
 XDOT =       4435
557672                 XDOT =        1330
230745
 YDOT =      14928
053171  feet/sec       YDOT =        4565
067947  meter/sec
 ZDOT =     -19758
323194                 ZDOT =       -6015
822101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11108168
52                 X    =        -3385769
76
 Y    =       19285486
54  feet           Y    =         5878216
30  meter
 Z    =         258150
48                 Z    =           78684
27
 XDOT =     -12239
279792                 XDOT =       -3730
532481
 YDOT =      -6768
768873  feet/sec       YDOT =       -2063
120753  meter/sec
 ZDOT =     -19729
973157                 ZDOT =       -6013
695818


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   17359
39554448  
00016717  00000-0  10270-3 0  9071
2 25544  51
6399 165
1221 0003169 290
7934  69
2879 15
54212005 11486


Satellite: ISS
Catalog Number: 25544
Epoch time:      17359
39554448   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       165
1221  deg
Eccentricity:     
0003169     
Arg of perigee:   290
7934  deg
Mean anomaly:      69
2879  deg
Mean motion:   15
54212005  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1148
Checksum:              331


Coasting Arc #9 (Orbit 1163)
---------------------------------------

Vector Time (GMT): 2017/360/08:43:02
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6483609
86                 A    =         6787760
80  meter
 Y    =        1045919
06  meter          E    =           
0012208
 Z    =        1687865
44                 I    =           51
78351
 XDOT =        675
031500                 Wp   =           52
09801
 YDOT =      -5071
950910  meter/sec      RA   =          159
16096  deg
 ZDOT =       5715
124174                 TA   =          326
37251
                                          MA   =          326
44993
                                          Ha   =            219
869  n
mi
                                          Hp   =            215
536

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21271685
90                 X    =        -6503022
52
 Y    =        3431492
99  feet           Y    =          973306
28  meter
 Z    =        5537616
27                 Z    =         1656323
10
 XDOT =       2214
670274                 XDOT =         703
936093
 YDOT =     -16640
258891  feet/sec       YDOT =       -5064
240892  meter/sec
 ZDOT =      18750
407394                 ZDOT =        5718
473227

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12661237
55                 X    =         3859145
20
 Y    =      -17478221
56  feet           Y    =        -5327361
93  meter
 Z    =        5397202
41                 Z    =         1645067
29
 XDOT =       8996
007195                 XDOT =        2741
982993
 YDOT =      12333
210322  feet/sec       YDOT =        3759
162506  meter/sec
 ZDOT =      18765
992047                 ZDOT =        5719
874376


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   17360
42429860  
00016717  00000-0  10270-3 0  9087
2 25544  51
6386 159
9917 0003222 295
7368  64
3452 15
54274463 11648


Satellite: ISS
Catalog Number: 25544
Epoch time:      17360
42429860   =   yrday
fracday
Element set:     908
Inclination:       51
6386  deg
RA of node:       159
9917  deg
Eccentricity:     
0003222     
Arg of perigee:   295
7368  deg
Mean anomaly:      64
3452  deg
Mean motion:   15
54274463  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1164
Checksum:              329


Coasting Arc #10 (Orbit 1177)
---------------------------------------

Vector Time (GMT): 2017/361/06:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939197
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         928537
92                 A    =         6778879
30  meter
 Y    =       -4658055
01  meter          E    =           
0006195
 Z    =        4835854
11                 I    =           51
78346
 XDOT =       7142
768138                 Wp   =           32
86755
 YDOT =      -1199
617469  meter/sec      RA   =          154
56366  deg
 ZDOT =      -2520
410845                 TA   =           81
89553
                                          MA   =           81
82526
                                          Ha   =            219
835  n
mi
                                          Hp   =            215
420

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3046384
27                 X    =          957066
36
 Y    =      -15282332
71  feet           Y    =        -4647512
18  meter
 Z    =       15865663
08                 Z    =         4840433
72
 XDOT =      23434
278669                 XDOT =        7167
894620
 YDOT =      -3935
752850  feet/sec       YDOT =       -1119
601537  meter/sec
 ZDOT =      -8269
064453                 ZDOT =       -2485
652569

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1404734
91                 X    =          428163
20
 Y    =       15498060
48  feet           Y    =         4723808
84  meter
 Z    =       15886669
13                 Z    =         4842256
75
 XDOT =     -20349
446315                 XDOT =       -6202
511237
 YDOT =      10184
375631  feet/sec       YDOT =        3104
197692  meter/sec
 ZDOT =      -8114
311384                 ZDOT =       -2473
242110


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   17361
32445664  
00016717  00000-0  10270-3 0  9098
2 25544  51
6399 155
5054 0003282 300
8902  59
1928 15
54300205 11783


Satellite: ISS
Catalog Number: 25544
Epoch time:      17361
32445664   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       155
5054  deg
Eccentricity:     
0003282     
Arg of perigee:   300
8902  deg
Mean anomaly:      59
1928  deg
Mean motion:   15
54300205  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1178
Checksum:              305


Coasting Arc #11 (Orbit 1189)
---------------------------------------

Vector Time (GMT): 2017/362/01:04:30
000
Vector Time (MET): N/A
Weight (LBS)     : 924764
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3625183
24                 A    =         6777871
47  meter
 Y    =       -2581317
67  meter          E    =           
0002048
 Z    =        5111136
66                 I    =           51
79996
 XDOT =       5774
940712                 Wp   =          129
13635
 YDOT =      -4754
633183  meter/sec      RA   =          150
79385  deg
 ZDOT =       1693
015445                 TA   =          304
54032
                                          MA   =          304
55965
                                          Ha   =            220
034  n
mi
                                          Hp   =            215
396

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11893645
79                 X    =        -3620876
22
 Y    =       -8468889
98  feet           Y    =        -2621833
14  meter
 Z    =       16768821
05                 Z    =         5093536
95
 XDOT =      18946
655878                 XDOT =        5819
455251
 YDOT =     -15599
190233  feet/sec       YDOT =       -4689
805042  meter/sec
 ZDOT =       5554
512614                 ZDOT =        1721
176190

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3365546
30                 X    =        -1025818
51
 Y    =       14298999
86  feet           Y    =         4358335
16  meter
 Z    =       16690894
77                 Z    =         5087384
72
 XDOT =     -20494
593346                 XDOT =       -6246
752052
 YDOT =     -11461
027690  feet/sec       YDOT =       -3493
321240  meter/sec
 ZDOT =       5680
424679                 ZDOT =        1731
393442


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   17362
09601784  
00016717  00000-0  10270-3 0  9102
2 25544  51
6377 151
6570 0003209 302
5635  57
5207 15
54289820 11905


Satellite: ISS
Catalog Number: 25544
Epoch time:      17362
09601784   =   yrday
fracday
Element set:     910
Inclination:       51
6377  deg
RA of node:       151
6570  deg
Eccentricity:     
0003209     
Arg of perigee:   302
5635  deg
Mean anomaly:      57
5207  deg
Mean motion:   15
54289820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1190
Checksum:              301


Coasting Arc #12 (Orbit 1204)
---------------------------------------

Vector Time (GMT): 2017/363/01:04:30
000
Vector Time (MET): N/A
Weight (LBS)     : 924764
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2088363
71                 A    =         6776976
26  meter
 Y    =        3645563
36  meter          E    =           
0012447
 Z    =       -5328124
43                 I    =           51
82517
 XDOT =      -6455
025056                 Wp   =           83
42125
 YDOT =       4113
767540  meter/sec      RA   =          145
80389  deg
 ZDOT =        286
596599                 TA   =          189
29523
                                          MA   =          189
31829
                                          Ha   =            220
100  n
mi
                                          Hp   =            215
407

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6851586
98                 X    =         2073324
29
 Y    =       11960509
71  feet           Y    =         3668833
16  meter
 Z    =      -17480723
19                 Z    =        -5318016
05
 XDOT =     -21177
903727                 XDOT =       -6501
938708
 YDOT =      13496
612663  feet/sec       YDOT =        4041
320703  meter/sec
 ZDOT =        940
277556                 ZDOT =         255
126370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8297875
58                 X    =         2529192
48
 Y    =      -11076807
44  feet           Y    =        -3376210
91  meter
 Z    =      -17436264
45                 Z    =        -5314573
40
 XDOT =      19878
275276                 XDOT =        6058
898304
 YDOT =      13642
568217  feet/sec       YDOT =        4158
254792  meter/sec
 ZDOT =        799
710752                 ZDOT =         243
751837


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   17363
06046335  
00016717  00000-0  10270-3 0  9116
2 25544  51
6379 146
8472 0003189 308
9219  51
1649 15
54265738 12058


Satellite: ISS
Catalog Number: 25544
Epoch time:      17363
06046335   =   yrday
fracday
Element set:     911
Inclination:       51
6379  deg
RA of node:       146
8472  deg
Eccentricity:     
0003189     
Arg of perigee:   308
9219  deg
Mean anomaly:      51
1649  deg
Mean motion:   15
54265738  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1205
Checksum:              318


Coasting Arc #13 (Orbit 1220)
---------------------------------------

Vector Time (GMT): 2017/364/01:04:30
000
Vector Time (MET): N/A
Weight (LBS)     : 924764
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -496013
31                 A    =         6778536
67  meter
 Y    =       -4607183
01  meter          E    =           
0006462
 Z    =        4946581
35                 I    =           51
85701
 XDOT =       6631
227869                 Wp   =           29
32433
 YDOT =      -3130
914404  meter/sec      RA   =          140
81829  deg
 ZDOT =      -2244
421857                 TA   =           82
55885
                                          MA   =           82
48543
                                          Ha   =            220
197  n
mi
                                          Hp   =            215
254

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1627340
26                 X    =         -468485
79
 Y    =      -15115429
82  feet           Y    =        -4612576
31  meter
 Z    =       16228941
44                 Z    =         4944238
30
 XDOT =      21755
996946                 XDOT =        6676
648067
 YDOT =     -10272
028884  feet/sec       YDOT =       -3056
505309  meter/sec
 ZDOT =      -7363
588770                 ZDOT =       -2212
099325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13112031
90                 X    =        -3996547
32
 Y    =        7714676
68  feet           Y    =         2351433
45  meter
 Z    =       16219167
00                 Z    =         4943602
10
 XDOT =     -17670
055379                 XDOT =       -5385
832880
 YDOT =     -14808
154652  feet/sec       YDOT =       -4513
525538  meter/sec
 ZDOT =      -7219
343225                 ZDOT =       -2200
455815


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   17364
08919903  
00016717  00000-0  10270-3 0  9120
2 25544  51
6378 141
7182 0003194 314
4127  45
6764 15
54272991 12218


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
08919903   =   yrday
fracday
Element set:     912
Inclination:       51
6378  deg
RA of node:       141
7182  deg
Eccentricity:     
0003194     
Arg of perigee:   314
4127  deg
Mean anomaly:      45
6764  deg
Mean motion:   15
54272991  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1221
Checksum:              312


Coasting Arc #14 (Orbit 1227)
---------------------------------------

Vector Time (GMT): 2017/364/11:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924764
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3425368
13                 A    =         6777123
54  meter
 Y    =       -2508985
62  meter          E    =           
0000615
 Z    =        5281632
77                 I    =           51
86318
 XDOT =       5281
718715                 Wp   =           74
96444
 YDOT =      -5501
526573  meter/sec      RA   =          138
62778  deg
 ZDOT =        812
056832                 TA   =            7
29964
                                          MA   =            7
29875
                                          Ha   =            220
197  n
mi
                                          Hp   =            215
236

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11238084
42                 X    =        -3422712
99
 Y    =       -8231580
12  feet           Y    =        -2547276
13  meter
 Z    =       17328191
51                 Z    =         5264999
57
 XDOT =      17328
473473                 XDOT =        5338
901140
 YDOT =     -18049
627863  feet/sec       YDOT =       -5442
143139  meter/sec
 ZDOT =       2664
228452                 ZDOT =         837
852123

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7316328
03                 X    =         2230016
78
 Y    =      -11961263
40  feet           Y    =        -3645793
08  meter
 Z    =       17254541
30                 Z    =         5259184
19
 XDOT =      18476
709915                 XDOT =        5631
701182
 YDOT =      15311
186066  feet/sec       YDOT =        4666
849513  meter/sec
 ZDOT =       2779
780064                 ZDOT =         847
276963


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   17364
53926899  
00016717  00000-0  10270-3 0  9133
2 25544  51
6374 139
4696 0002915 308
6679  51
4213 15
54287091 12283


Satellite: ISS
Catalog Number: 25544
Epoch time:      17364
53926899   =   yrday
fracday
Element set:     913
Inclination:       51
6374  deg
RA of node:       139
4696  deg
Eccentricity:     
0002915     
Arg of perigee:   308
6679  deg
Mean anomaly:      51
4213  deg
Mean motion:   15
54287091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1228
Checksum:              340


Coasting Arc #15 (Orbit 1242)
---------------------------------------

Vector Time (GMT): 2017/365/11:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924764
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2049665
61                 A    =         6777273
97  meter
 Y    =        3799964
48  meter          E    =           
0011916
 Z    =       -5234355
86                 I    =           51
88921
 XDOT =      -5857
054341                 Wp   =           91
45698
 YDOT =       4791
841183  meter/sec      RA   =          133
64337  deg
 ZDOT =       1187
247485                 TA   =          189
89203
                                          MA   =          189
91551
                                          Ha   =            220
147  n
mi
                                          Hp   =            215
206

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6724624
70                 X    =         2032446
89
 Y    =       12467075
06  feet           Y    =         3822789
61  meter
 Z    =      -17173083
53                 Z    =        -5224440
61
 XDOT =     -19216
057548                 XDOT =       -5915
969735
 YDOT =      15721
263725  feet/sec       YDOT =        4726
014035  meter/sec
 ZDOT =       3895
168915                 ZDOT =        1158
653316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11756387
66                 X    =        -3583346
96
 Y    =        7995666
04  feet           Y    =         2437079
01  meter
 Z    =      -17129506
99                 Z    =        -5221073
73
 XDOT =     -16902
594332                 XDOT =       -5151
910752
 YDOT =     -16796
248424  feet/sec       YDOT =       -5119
496520  meter/sec
 ZDOT =       3767
237434                 ZDOT =        1148
253970


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   17365
50370081  
00016717  00000-0  10270-3 0  9148
2 25544  51
6387 134
6615 0002867 312
6031  47
4880 15
54306179 12439


Satellite: ISS
Catalog Number: 25544
Epoch time:      17365
50370081   =   yrday
fracday
Element set:     914
Inclination:       51
6387  deg
RA of node:       134
6615  deg
Eccentricity:     
0002867     
Arg of perigee:   312
6031  deg
Mean anomaly:      47
4880  deg
Mean motion:   15
54306179  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1243
Checksum:              301
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