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

 
Date: August 21st 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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


233/21:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 212 9

237/07:36:05 457 1 3 4 0 4 0
N/A 3 8 -0 4 219 8
000/00:12:06 914 0 1 -0 0 215 5

239/10:11:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 215 6

Coasting Arc #1 (Orbit 1482)
---------------------------------------

Vector Time (GMT): 2016/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3646581
17                 A    =         6775339
41  meter
 Y    =        2431179
51  meter          E    =           
0014704
 Z    =       -5179974
03                 I    =           51
98794
 XDOT =      -2583
166708                 Wp   =          104
73106
 YDOT =       7054
012006  meter/sec      RA   =          101
18100  deg
 ZDOT =       1492
148309                 TA   =          179
58607
                                          MA   =          179
58486
                                          Ha   =            219
822  n
mi
                                          Hp   =            213
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11963848
98                 X    =         3644285
70
 Y    =        7976310
71  feet           Y    =         2471944
85  meter
 Z    =      -16994665
47                 Z    =        -5162265
92
 XDOT =      -8474
956392                 XDOT =       -2669
102552
 YDOT =      23143
084009  feet/sec       YDOT =        7024
644906  meter/sec
 ZDOT =       4895
499701                 ZDOT =        1479
390991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5878105
47                 X    =        -1791646
55
 Y    =      -13221724
07  feet           Y    =        -4029981
50  meter
 Z    =      -16917675
90                 Z    =        -5156507
62
 XDOT =      18667
380067                 XDOT =        5689
817444
 YDOT =     -14490
648528  feet/sec       YDOT =       -4416
749671  meter/sec
 ZDOT =       4838
523757                 ZDOT =        1474
782041


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   16232
51354799  
00016717  00000-0  10270-3 0  9004
2 25544  51
6431 102
0399 0001275 144
7815 215
3422 15
55069242 14835


Satellite: ISS
Catalog Number: 25544
Epoch time:      16232
51354799   =   yrday
fracday
Element set:     900
Inclination:       51
6431  deg
RA of node:       102
0399  deg
Eccentricity:     
0001275     
Arg of perigee:   144
7815  deg
Mean anomaly:     215
3422  deg
Mean motion:   15
55069242  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1483
Checksum:              293


Coasting Arc #2 (Orbit 1498)
---------------------------------------

Vector Time (GMT): 2016/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2909015
46                 A    =         6778673
93  meter
 Y    =       -4347929
94  meter          E    =           
0010183
 Z    =        4303542
81                 I    =           52
00500
 XDOT =       3444
512072                 Wp   =           78
63080
 YDOT =      -5851
591689  meter/sec      RA   =           96
20168  deg
 ZDOT =      -3574
516044                 TA   =           47
64737
                                          MA   =           47
56118
                                          Ha   =            219
782  n
mi
                                          Hp   =            212
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9544013
96                 X    =        -2881084
05
 Y    =      -14264862
02  feet           Y    =        -4380304
00  meter
 Z    =       14119234
95                 Z    =         4289479
92
 XDOT =      11300
892625                 XDOT =        3527
053254
 YDOT =     -19198
135463  feet/sec       YDOT =       -5812
611605  meter/sec
 ZDOT =     -11727
414844                 ZDOT =       -3557
582794

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         732602
25                 X    =          223297
16
 Y    =       17197348
75  feet           Y    =         5241751
90  meter
 Z    =       14058512
60                 Z    =         4285034
64
 XDOT =     -18495
671985                 XDOT =       -5637
480821
 YDOT =      10337
982240  feet/sec       YDOT =        3151
016987  meter/sec
 ZDOT =     -11652
382370                 ZDOT =       -3551
646146


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   16233
54176398  
00016717  00000-0  10270-3 0  9016
2 25544  51
6433  96
9068 0001062 147
9082 212
2136 15
55109240 14994


Satellite: ISS
Catalog Number: 25544
Epoch time:      16233
54176398   =   yrday
fracday
Element set:     901
Inclination:       51
6433  deg
RA of node:        96
9068  deg
Eccentricity:     
0001062     
Arg of perigee:   147
9082  deg
Mean anomaly:     212
2136  deg
Mean motion:   15
55109240  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1499
Checksum:              304


Coasting Arc #3 (Orbit 1504)
---------------------------------------

Vector Time (GMT): 2016/233/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3861104
79                 A    =         6775399
50  meter
 Y    =       -2146003
72  meter          E    =           
0004917
 Z    =        5133685
90                 I    =           51
99536
 XDOT =       1840
528552                 Wp   =           72
80868
 YDOT =      -7264
308837  meter/sec      RA   =           94
31249  deg
 ZDOT =      -1649
659347                 TA   =           33
04005
                                          MA   =           33
00933
                                          Ha   =            219
892  n
mi
                                          Hp   =            212
909

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12667666
62                 X    =        -3861757
57
 Y    =       -7040694
62  feet           Y    =        -2189184
43  meter
 Z    =       16842801
51                 Z    =         5114928
45
 XDOT =       6038
479500                 XDOT =        1929
636332
 YDOT =     -23833
034242  feet/sec       YDOT =       -7243
228712  meter/sec
 ZDOT =      -5412
268200                 ZDOT =       -1640
501642

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3176181
08                 X    =          968099
99
 Y    =      -14237131
38  feet           Y    =        -4339477
65  meter
 Z    =       16761177
90                 Z    =         5108807
02
 XDOT =      23542
281505                 XDOT =        7175
687403
 YDOT =      -1081
626847  feet/sec       YDOT =        -329
679863  meter/sec
 ZDOT =      -5370
976992                 ZDOT =       -1637
073787


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   16233
92734445  
00016717  00000-0  10270-3 0  9022
2 25544  51
6434  94
9789 0001546 157
8245 202
2975 15
55101750 15057


Satellite: ISS
Catalog Number: 25544
Epoch time:      16233
92734445   =   yrday
fracday
Element set:     902
Inclination:       51
6434  deg
RA of node:        94
9789  deg
Eccentricity:     
0001546     
Arg of perigee:   157
8245  deg
Mean anomaly:     202
2975  deg
Mean motion:   15
55101750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1505
Checksum:              313


Coasting Arc #4 (Orbit 1519)
---------------------------------------

Vector Time (GMT): 2016/234/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3352117
55                 A    =         6779009
80  meter
 Y    =        4111624
30  meter          E    =           
0009166
 Z    =       -4230346
81                 I    =           52
00759
 XDOT =      -2814
650054                 Wp   =          117
72076
 YDOT =       6093
171815  meter/sec      RA   =           89
33549  deg
 ZDOT =       3693
803108                 TA   =          189
98921
                                          MA   =          190
00745
                                          Ha   =            219
788  n
mi
                                          Hp   =            212
987

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10997761
00                 X    =         3326440
22
 Y    =       13489581
02  feet           Y    =         4148966
01  meter
 Z    =      -13879090
60                 Z    =        -4214125
90
 XDOT =      -9234
416189                 XDOT =       -2900
519003
 YDOT =      19990
721178  feet/sec       YDOT =        6061
216684  meter/sec
 ZDOT =      12118
776600                 ZDOT =        3679
921320

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9590686
22                 X    =        -2923241
16
 Y    =       14590464
32  feet           Y    =         4447173
52  meter
 Z    =      -13808902
48                 Z    =        -4208953
48
 XDOT =     -20790
814780                 XDOT =       -6337
040345
 YDOT =      -2261
265885  feet/sec       YDOT =        -689
233842  meter/sec
 ZDOT =      12057
026933                 ZDOT =        3674
981809


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   16234
89129349  
00016717  00000-0  10270-3 0  9031
2 25544  51
6421  90
1679 0001680 158
0827 202
0398 15
55096170 15200


Satellite: ISS
Catalog Number: 25544
Epoch time:      16234
89129349   =   yrday
fracday
Element set:     903
Inclination:       51
6421  deg
RA of node:        90
1679  deg
Eccentricity:     
0001680     
Arg of perigee:   158
0827  deg
Mean anomaly:     202
0398  deg
Mean motion:   15
55096170  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1520
Checksum:              305


Coasting Arc #5 (Orbit 1535)
---------------------------------------

Vector Time (GMT): 2016/235/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2662615
07                 A    =         6783500
84  meter
 Y    =       -5621752
68  meter          E    =           
0014370
 Z    =        2687905
96                 I    =           52
02179
 XDOT =       3679
254011                 Wp   =          107
21278
 YDOT =      -4249
347677  meter/sec      RA   =           84
37119  deg
 ZDOT =      -5224
083779                 TA   =           42
57385
                                          MA   =           42
46254
                                          Ha   =            219
774  n
mi
                                          Hp   =            212
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8735613
75                 X    =        -2612609
94
 Y    =      -18444070
46  feet           Y    =        -5651248
03  meter
 Z    =        8818589
09                 Z    =         2675093
56
 XDOT =      12071
043342                 XDOT =        3751
874058
 YDOT =     -13941
429387  feet/sec       YDOT =       -4207
798123  meter/sec
 ZDOT =     -17139
382477                 ZDOT =       -5206
034296

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14762625
54                 X    =         4499648
27
 Y    =      -14125396
01  feet           Y    =        -4305420
70  meter
 Z    =        8763576
38                 Z    =         2671138
08
 XDOT =      16026
143286                 XDOT =        4884
768474
 YDOT =       6126
565249  feet/sec       YDOT =        1867
377088  meter/sec
 ZDOT =     -17059
728018                 ZDOT =       -5199
805100


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   16235
91949970  
00016717  00000-0  10270-3 0  9046
2 25544  51
6427  85
0350 0001506 162
0483 198
0723 15
55092441 15365


Satellite: ISS
Catalog Number: 25544
Epoch time:      16235
91949970   =   yrday
fracday
Element set:     904
Inclination:       51
6427  deg
RA of node:        85
0350  deg
Eccentricity:     
0001506     
Arg of perigee:   162
0483  deg
Mean anomaly:     198
0723  deg
Mean motion:   15
55092441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1536
Checksum:              305


Coasting Arc #6 (Orbit 1550)
---------------------------------------

Vector Time (GMT): 2016/236/21:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1833059
36                 A    =         6786416
50  meter
 Y    =        6483008
29  meter          E    =           
0009731
 Z    =        -783375
84                 I    =           52
02703
 XDOT =      -4383
236646                 Wp   =           45
93852
 YDOT =       1955
646979  meter/sec      RA   =           79
41900  deg
 ZDOT =       5980
339881                 TA   =          305
63642
                                          MA   =          305
72701
                                          Ha   =            219
758  n
mi
                                          Hp   =            213
096

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6013974
28                 X    =         1764233
77
 Y    =       21269712
24  feet           Y    =         6503121
92  meter
 Z    =       -2570130
70                 Z    =         -774638
85
 XDOT =     -14380
697658                 XDOT =       -4433
829228
 YDOT =       6416
164628  feet/sec       YDOT =        1906
348147  meter/sec
 ZDOT =      19620
537666                 ZDOT =        5958
924300

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18095765
92                 X    =        -5515589
45
 Y    =       12700424
36  feet           Y    =         3871089
35  meter
 Z    =       -2533099
70                 Z    =         -772088
79
 XDOT =      -9912
518846                 XDOT =       -3021
335744
 YDOT =     -10263
782207  feet/sec       YDOT =       -3128
400817  meter/sec
 ZDOT =      19526
569620                 ZDOT =        5951
698420


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   16236
88343812  
00016717  00000-0  10270-3 0  9057
2 25544  51
6427  80
2230 0001263 162
7959 197
3237 15
55042564 15514


Satellite: ISS
Catalog Number: 25544
Epoch time:      16236
88343812   =   yrday
fracday
Element set:     905
Inclination:       51
6427  deg
RA of node:        80
2230  deg
Eccentricity:     
0001263     
Arg of perigee:   162
7959  deg
Mean anomaly:     197
3237  deg
Mean motion:   15
55042564  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1551
Checksum:              305


Coasting Arc #7 (Orbit 1557)
---------------------------------------

Vector Time (GMT): 2016/237/07:42:08
914
Vector Time (MET): N/A
Weight (LBS)     : 929563
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4341920
36                 A    =         6778372
21  meter
 Y    =        1495699
79  meter          E    =           
0010305
 Z    =       -4995122
11                 I    =           51
99089
 XDOT =        -57
156357                 Wp   =          116
36578
 YDOT =       7352
219412  meter/sec      RA   =           77
22949  deg
 ZDOT =       2150
782200                 TA   =          174
51510
                                          MA   =          174
50380
                                          Ha   =            219
787  n
mi
                                          Hp   =            215
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14245145
53                 X    =         4349136
43
 Y    =        4907151
54  feet           Y    =         1544294
15  meter
 Z    =      -16388195
90                 Z    =        -4974012
77
 XDOT =       -187
520855                 XDOT =        -149
814027
 YDOT =      24121
454764  feet/sec       YDOT =        7351
062275  meter/sec
 ZDOT =       7056
372046                 ZDOT =        2150
279142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5476851
77                 X    =         1669344
42
 Y    =      -14142689
85  feet           Y    =        -4310691
87  meter
 Z    =      -16296186
39                 Z    =        -4967077
61
 XDOT =      23062
065892                 XDOT =        7029
317684
 YDOT =        800
260362  feet/sec       YDOT =         243
919358  meter/sec
 ZDOT =       7052
847525                 ZDOT =        2149
707926


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   16237
33327771  
00016717  00000-0  10270-3 0  9065
2 25544  51
6433  77
9781 0003027 246
7440 113
3394 15
54304663 15582


Satellite: ISS
Catalog Number: 25544
Epoch time:      16237
33327771   =   yrday
fracday
Element set:     906
Inclination:       51
6433  deg
RA of node:        77
9781  deg
Eccentricity:     
0003027     
Arg of perigee:   246
7440  deg
Mean anomaly:     113
3394  deg
Mean motion:   15
54304663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1558
Checksum:              311


Coasting Arc #8 (Orbit 1573)
---------------------------------------

Vector Time (GMT): 2016/238/07:42:08
914
Vector Time (MET): N/A
Weight (LBS)     : 929563
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4371113
60                 A    =         6781823
47  meter
 Y    =       -3185776
40  meter          E    =           
0007685
 Z    =        4085513
64                 I    =           51
99405
 XDOT =       1106
954516                 Wp   =           80
57287
 YDOT =      -6517
246525  meter/sec      RA   =           72
26096  deg
 ZDOT =      -3890
205634                 TA   =           49
52662
                                          MA   =           49
45966
                                          Ha   =            219
861  n
mi
                                          Hp   =            215
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14340923
88                 X    =        -4355010
14
 Y    =      -10452022
30  feet           Y    =        -3234566
94  meter
 Z    =       13403916
15                 Z    =         4064319
18
 XDOT =       3631
740538                 XDOT =        1198
646602
 YDOT =     -21382
042405  feet/sec       YDOT =       -6504
355265  meter/sec
 ZDOT =     -12763
141844                 ZDOT =       -3884
605432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10778204
16                 X    =        -3285196
63
 Y    =       14184391
13  feet           Y    =         4323402
42  meter
 Z    =       13311844
33                 Z    =         4057450
15
 XDOT =     -20258
260947                 XDOT =       -6174
717937
 YDOT =      -3416
533765  feet/sec       YDOT =       -1041
359491  meter/sec
 ZDOT =     -12737
471279                 ZDOT =       -3882
381246


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   16238
36199413  
00016717  00000-0  10270-3 0  9070
2 25544  51
6430  72
8499 0003040 250
1612 109
9214 15
54306850 15744


Satellite: ISS
Catalog Number: 25544
Epoch time:      16238
36199413   =   yrday
fracday
Element set:     907
Inclination:       51
6430  deg
RA of node:        72
8499  deg
Eccentricity:     
0003040     
Arg of perigee:   250
1612  deg
Mean anomaly:     109
9214  deg
Mean motion:   15
54306850  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1574
Checksum:              298


Coasting Arc #9 (Orbit 1588)
---------------------------------------

Vector Time (GMT): 2016/239/07:42:08
914
Vector Time (MET): N/A
Weight (LBS)     : 929563
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4221701
80                 A    =         6785621
46  meter
 Y    =        4552443
99  meter          E    =           
0002131
 Z    =       -2736201
36                 I    =           51
99761
 XDOT =      -2227
478472                 Wp   =           27
40221
 YDOT =       5182
765835  meter/sec      RA   =           67
30072  deg
 ZDOT =       5189
646682                 TA   =          301
81485
                                          MA   =          301
83560
                                          Ha   =            219
613  n
mi
                                          Hp   =            215
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13850727
71                 X    =         4183772
64
 Y    =       14935839
86  feet           Y    =         4599441
75  meter
 Z    =       -8977038
58                 Z    =        -2715785
78
 XDOT =      -7308
000235                 XDOT =       -2310
476797
 YDOT =      17003
824917  feet/sec       YDOT =        5157
392731  meter/sec
 ZDOT =      17026
399875                 ZDOT =        5178
624519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15013813
95                 X    =         4576210
49
 Y    =      -13823417
84  feet           Y    =        -4213377
76  meter
 Z    =       -8888627
69                 Z    =        -2709253
72
 XDOT =      15954
915250                 XDOT =        4863
058168
 YDOT =       6419
610332  feet/sec       YDOT =        1956
697229  meter/sec
 ZDOT =      16977
259281                 ZDOT =        5174
668629


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   16239
32640980  
00016717  00000-0  10270-3 0  9088
2 25544  51
6443  68
0406 0003171 255
2644 104
8157 15
54332393 15896


Satellite: ISS
Catalog Number: 25544
Epoch time:      16239
32640980   =   yrday
fracday
Element set:     908
Inclination:       51
6443  deg
RA of node:        68
0406  deg
Eccentricity:     
0003171     
Arg of perigee:   255
2644  deg
Mean anomaly:     104
8157  deg
Mean motion:   15
54332393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1589
Checksum:              308


Coasting Arc #10 (Orbit 1590)
---------------------------------------

Vector Time (GMT): 2016/239/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2102175
23                 A    =         6788607
44  meter
 Y    =       -6404840
06  meter          E    =           
0009428
 Z    =        -753937
54                 I    =           52
00499
 XDOT =       4721
067323                 Wp   =          158
64518
 YDOT =       -848
944872  meter/sec      RA   =           66
81721  deg
 ZDOT =      -5983
597122                 TA   =           29
46299
                                          MA   =           29
40988
                                          Ha   =            219
609  n
mi
                                          Hp   =            215
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6896900
36                 X    =        -2026736
17
 Y    =      -21013254
77  feet           Y    =        -6427926
20  meter
 Z    =       -2473548
36                 Z    =         -763965
92
 XDOT =      15489
066019                 XDOT =        4759
275064
 YDOT =      -2785
252205  feet/sec       YDOT =        -795
937245  meter/sec
 ZDOT =     -19631
224153                 ZDOT =       -5960
570723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12644572
46                 X    =        -3854065
69
 Y    =       18139074
94  feet           Y    =         5528790
04  meter
 Z    =       -2516207
43                 Z    =         -766940
03
 XDOT =     -10298
808921                 XDOT =       -3139
076959
 YDOT =      -9874
105011  feet/sec       YDOT =       -3009
627207  meter/sec
 ZDOT =     -19530
403527                 ZDOT =       -5952
866995


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   16239
45499759  
00016717  00000-0  10270-3 0  9099
2 25544  51
6433  67
3994 0003336 255
7799 104
2983 15
54290792 15918


Satellite: ISS
Catalog Number: 25544
Epoch time:      16239
45499759   =   yrday
fracday
Element set:     909
Inclination:       51
6433  deg
RA of node:        67
3994  deg
Eccentricity:     
0003336     
Arg of perigee:   255
7799  deg
Mean anomaly:     104
2983  deg
Mean motion:   15
54290792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1591
Checksum:              361


Coasting Arc #11 (Orbit 1606)
---------------------------------------

Vector Time (GMT): 2016/240/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1159114
00                 A    =         6786163
67  meter
 Y    =        6218600
82  meter          E    =           
0010459
 Z    =        2443249
79                 I    =           51
98249
 XDOT =      -5359
416546                 Wp   =           72
33005
 YDOT =      -1117
607672  meter/sec      RA   =           61
86647  deg
 ZDOT =       5371
377820                 TA   =          314
88533
                                          MA   =          314
97020
                                          Ha   =            219
484  n
mi
                                          Hp   =            215
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3802867
47                 X    =         1077621
77
 Y    =       20402233
66  feet           Y    =         6231107
22  meter
 Z    =        8015911
39                 Z    =         2448682
32
 XDOT =     -17583
387619                 XDOT =       -5372
612384
 YDOT =      -3666
691837  feet/sec       YDOT =       -1177
613903  meter/sec
 ZDOT =      17622
630642                 ZDOT =        5345
311401

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13775241
25                 X    =         4198693
53
 Y    =      -15511059
06  feet           Y    =        -4727770
80  meter
 Z    =        8038504
22                 Z    =         2450136
09
 XDOT =       6869
001401                 XDOT =        2093
671627
 YDOT =      15200
891596  feet/sec       YDOT =        4633
231758  meter/sec
 ZDOT =      17508
882402                 ZDOT =        5336
707356


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   16240
48370155  
00016717  00000-0  10270-3 0  9104
2 25544  51
6420  62
2689 0003311 261
4567  98
6210 15
54342417 16078


Satellite: ISS
Catalog Number: 25544
Epoch time:      16240
48370155   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:        62
2689  deg
Eccentricity:     
0003311     
Arg of perigee:   261
4567  deg
Mean anomaly:      98
6210  deg
Mean motion:   15
54342417  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1607
Checksum:              286


Coasting Arc #12 (Orbit 1621)
---------------------------------------

Vector Time (GMT): 2016/241/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          -2468
53                 A    =         6782371
73  meter
 Y    =       -5565409
71  meter          E    =           
0003194
 Z    =       -3880060
77                 I    =           51
95230
 XDOT =       5759
219282                 Wp   =           63
63060
 YDOT =       2889
386119  meter/sec      RA   =           56
90703  deg
 ZDOT =      -4149
344257                 TA   =          162
94076
                                          MA   =          162
93002
                                          Ha   =            219
488  n
mi
                                          Hp   =            215
575

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          -8098
85                 X    =           78612
86
 Y    =      -18259218
21  feet           Y    =        -5564984
10  meter
 Z    =      -12729858
18                 Z    =        -3879875
64
 XDOT =      18895
076384                 XDOT =        5746
636821
 YDOT =       9479
613252  feet/sec       YDOT =        2953
719066  meter/sec
 ZDOT =     -13613
334177                 ZDOT =       -4121
398497

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14245563
34                 X    =        -4342047
71
 Y    =       11424104
71  feet           Y    =         3482067
12  meter
 Z    =      -12728006
95                 Z    =        -3879496
52
 XDOT =      -3732
756193                 XDOT =       -1137
744088
 YDOT =     -19681
649929  feet/sec       YDOT =       -5998
966898  meter/sec
 ZDOT =     -13491
701690                 ZDOT =       -4112
270675


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   16241
44810972  
00016717  00000-0  10270-3 0  9118
2 25544  51
6406  57
4604 0003307 265
0031  95
0744 15
54327340 16224


Satellite: ISS
Catalog Number: 25544
Epoch time:      16241
44810972   =   yrday
fracday
Element set:     911
Inclination:       51
6406  deg
RA of node:        57
4604  deg
Eccentricity:     
0003307     
Arg of perigee:   265
0031  deg
Mean anomaly:      95
0744  deg
Mean motion:   15
54327340  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1622
Checksum:              276


Coasting Arc #13 (Orbit 1637)
---------------------------------------

Vector Time (GMT): 2016/242/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1287728
16                 A    =         6778806
72  meter
 Y    =        4539175
23  meter          E    =           
0004508
 Z    =        4866189
18                 I    =           51
92218
 XDOT =      -5839
027789                 Wp   =          141
74696
 YDOT =      -4313
026524  meter/sec      RA   =           51
93409  deg
 ZDOT =       2473
347067                 TA   =          284
04149
                                          MA   =          284
09160
                                          Ha   =            219
581  n
mi
                                          Hp   =            215
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4224829
91                 X    =        -1362028
11
 Y    =       14892307
17  feet           Y    =         4524359
80  meter
 Z    =       15965187
58                 Z    =         4859753
13
 XDOT =     -19156
915317                 XDOT =       -5802
378715
 YDOT =     -14150
349488  feet/sec       YDOT =       -4378
117399  meter/sec
 ZDOT =       8114
655730                 ZDOT =        2445
072251

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14197126
84                 X    =         4327284
26
 Y    =       -6244712
06  feet           Y    =        -1903388
24  meter
 Z    =       15936197
04                 Z    =         4857352
86
 XDOT =       1030
276185                 XDOT =         314
028181
 YDOT =      22776
292111  feet/sec       YDOT =        6942
213835  meter/sec
 ZDOT =       7991
855441                 ZDOT =        2435
917538


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   16242
47680757  
00016717  00000-0  10270-3 0  9129
2 25544  51
6411  52
3299 0003264 269
9882  90
0896 15
54303431 16388


Satellite: ISS
Catalog Number: 25544
Epoch time:      16242
47680757   =   yrday
fracday
Element set:     912
Inclination:       51
6411  deg
RA of node:        52
3299  deg
Eccentricity:     
0003264     
Arg of perigee:   269
9882  deg
Mean anomaly:      90
0896  deg
Mean motion:   15
54303431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1638
Checksum:              321


Coasting Arc #14 (Orbit 1652)
---------------------------------------

Vector Time (GMT): 2016/243/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2656415
99                 A    =         6776780
42  meter
 Y    =       -3267786
73  meter          E    =           
0011608
 Z    =       -5319440
03                 I    =           51
89384
 XDOT =       5502
959844                 Wp   =           84
29933
 YDOT =       5304
627736  meter/sec      RA   =           46
95103  deg
 ZDOT =       -510
458664                 TA   =          180
84180
                                          MA   =          180
84375
                                          Ha   =            219
484  n
mi
                                          Hp   =            215
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8715275
55                 X    =         2718598
87
 Y    =      -10721085
07  feet           Y    =        -3237733
59  meter
 Z    =      -17452231
06                 Z    =        -5306384
79
 XDOT =      18054
330197                 XDOT =        5445
712707
 YDOT =      17403
634304  feet/sec       YDOT =        5365
845394  meter/sec
 ZDOT =      -1674
733149                 ZDOT =        -483
866543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13884580
00                 X    =        -4232019
99
 Y    =         355577
64  feet           Y    =          108380
06  meter
 Z    =      -17394541
23                 Z    =        -5301856
17
 XDOT =       1338
814115                 XDOT =         408
070542
 YDOT =     -24037
358901  feet/sec       YDOT =       -7326
586993  meter/sec
 ZDOT =      -1559
481640                 ZDOT =        -475
330004


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   16243
44120412  
00016717  00000-0  10270-3 0  9135
2 25544  51
6398  47
5197 0003178 272
5717  87
5072 15
54351654 16530


Satellite: ISS
Catalog Number: 25544
Epoch time:      16243
44120412   =   yrday
fracday
Element set:     913
Inclination:       51
6398  deg
RA of node:        47
5197  deg
Eccentricity:     
0003178     
Arg of perigee:   272
5717  deg
Mean anomaly:      87
5072  deg
Mean motion:   15
54351654  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1653
Checksum:              309


Coasting Arc #15 (Orbit 1668)
---------------------------------------

Vector Time (GMT): 2016/244/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3971426
21                 A    =         6777555
57  meter
 Y    =        1876734
46  meter          E    =           
0003122
 Z    =        5161591
84                 I    =           51
87335
 XDOT =      -4728
450312                 Wp   =           12
23419
 YDOT =      -5845
816937  meter/sec      RA   =           41
96607  deg
 ZDOT =      -1509
501499                 TA   =           92
27435
                                          MA   =           92
23860
                                          Ha   =            219
635  n
mi
                                          Hp   =            215
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13029613
57                 X    =        -4017189
55
 Y    =        6157265
29  feet           Y    =         1832067
89  meter
 Z    =       16934356
44                 Z    =         5142188
65
 XDOT =     -15513
288426                 XDOT =       -4655
397090
 YDOT =     -19179
189427  feet/sec       YDOT =       -5898
285302  meter/sec
 ZDOT =      -4952
432738                 ZDOT =       -1532
292802

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13360316
10                 X    =         4072224
35
 Y    =        5662353
67  feet           Y    =         1725885
40  meter
 Z    =       16849180
34                 Z    =         5135630
17
 XDOT =      -3516
702219                 XDOT =       -1071
890836
 YDOT =      23358
362455  feet/sec       YDOT =        7119
628876  meter/sec
 ZDOT =      -5050
959135                 ZDOT =       -1539
532344


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   16244
46989122  
00016717  00000-0  10270-3 0  9140
2 25544  51
6397  42
3902 0003256 275
2501  84
8280 15
54327329 16694


Satellite: ISS
Catalog Number: 25544
Epoch time:      16244
46989122   =   yrday
fracday
Element set:     914
Inclination:       51
6397  deg
RA of node:        42
3902  deg
Eccentricity:     
0003256     
Arg of perigee:   275
2501  deg
Mean anomaly:      84
8280  deg
Mean motion:   15
54327329  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1669
Checksum:              318


Coasting Arc #16 (Orbit 1683)
---------------------------------------

Vector Time (GMT): 2016/245/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5110774
89                 A    =         6780444
97  meter
 Y    =        -508713
77  meter          E    =           
0005935
 Z    =       -4432812
93                 I    =           51
85872
 XDOT =       3499
922503                 Wp   =          117
06659
 YDOT =       5933
952628  meter/sec      RA   =           36
98349  deg
 ZDOT =       3355
040080                 TA   =          186
75723
                                          MA   =          186
76523
                                          Ha   =            219
510  n
mi
                                          Hp   =            215
581

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16767634
17                 X    =         5137616
01
 Y    =       -1669008
45  feet           Y    =         -451412
05  meter
 Z    =      -14543349
52                 Z    =        -4407921
18
 XDOT =      11482
685378                 XDOT =        3417
010307
 YDOT =      19468
348518  feet/sec       YDOT =        5972
627864  meter/sec
 ZDOT =      11007
349345                 ZDOT =        3371
839591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12702002
65                 X    =        -3871570
41
 Y    =      -11214013
02  feet           Y    =        -3418031
17  meter
 Z    =      -14434444
93                 Z    =        -4399618
82
 XDOT =       5675
406364                 XDOT =        1729
863860
 YDOT =     -20686
497514  feet/sec       YDOT =       -6305
244442  meter/sec
 ZDOT =      11079
658815                 ZDOT =        3377
080007


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   16245
43428037  
00016717  00000-0  10270-3 0  9152
2 25544  51
6397  37
5799 0003185 277
6642  82
4149 15
54363221 16843


Satellite: ISS
Catalog Number: 25544
Epoch time:      16245
43428037   =   yrday
fracday
Element set:     915
Inclination:       51
6397  deg
RA of node:        37
5799  deg
Eccentricity:     
0003185     
Arg of perigee:   277
6642  deg
Mean anomaly:      82
4149  deg
Mean motion:   15
54363221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1684
Checksum:              329


Coasting Arc #17 (Orbit 1699)
---------------------------------------

Vector Time (GMT): 2016/246/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5937486
40                 A    =         6784405
90  meter
 Y    =        -761399
74  meter          E    =           
0009614
 Z    =        3184391
47                 I    =           51
84639
 XDOT =      -1874
806866                 Wp   =           91
17737
 YDOT =      -5651
077741  meter/sec      RA   =           32
01066  deg
 ZDOT =      -4834
492586                 TA   =           52
14992
                                          MA   =           52
06298
                                          Ha   =            219
525  n
mi
                                          Hp   =            215
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19479942
25                 X    =        -5943999
18
 Y    =       -2498030
64  feet           Y    =         -827832
74  meter
 Z    =       10447478
57                 Z    =         3155533
23
 XDOT =      -6150
941162                 XDOT =       -1787
992111
 YDOT =     -18540
281301  feet/sec       YDOT =       -5671
558233  meter/sec
 ZDOT =     -15861
196148                 ZDOT =       -4843
388318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11751535
17                 X    =         3581867
92
 Y    =       15818548
32  feet           Y    =         4821493
53  meter
 Z    =       10321485
64                 Z    =         3145988
82
 XDOT =      -8016
327440                 XDOT =       -2443
376604
 YDOT =      16356
125308  feet/sec       YDOT =        4985
346994  meter/sec
 ZDOT =     -15899
004069                 ZDOT =       -4846
016440


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   16246
46295549  
00016717  00000-0  10270-3 0  9167
2 25544  51
6403  32
4500 0003352 283
1529  76
9250 15
54378217 17008


Satellite: ISS
Catalog Number: 25544
Epoch time:      16246
46295549   =   yrday
fracday
Element set:     916
Inclination:       51
6403  deg
RA of node:        32
4500  deg
Eccentricity:     
0003352     
Arg of perigee:   283
1529  deg
Mean anomaly:      76
9250  deg
Mean motion:   15
54378217  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1700
Checksum:              299


Coasting Arc #18 (Orbit 1714)
---------------------------------------

Vector Time (GMT): 2016/247/10:11:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910124
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6335021
85                 A    =         6787593
14  meter
 Y    =        1829573
53  meter          E    =           
0007526
 Z    =       -1591593
18                 I    =           51
82910
 XDOT =        -21
296890                 Wp   =           15
24733
 YDOT =       5068
119048  meter/sec      RA   =           27
04667  deg
 ZDOT =       5754
400639                 TA   =          327
38801
                                          MA   =          327
43447
                                          Ha   =            219
630  n
mi
                                          Hp   =            215
387

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20784192
41                 X    =         6321823
48
 Y    =        6002537
83  feet           Y    =         1900342
00  meter
 Z    =       -5221762
41                 Z    =        -1560851
74
 XDOT =        -69
871686                 XDOT =        -105
920502
 YDOT =      16627
687164  feet/sec       YDOT =        5067
408425  meter/sec
 ZDOT =      18879
267189                 ZDOT =        5754
091036

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10434418
41                 X    =        -3180410
73
 Y    =      -18987301
04  feet           Y    =        -5787329
36  meter
 Z    =       -5087752
85                 Z    =        -1550747
07
 XDOT =      10535
411524                 XDOT =        3211
193432
 YDOT =     -10835
936012  feet/sec       YDOT =       -3302
793296  meter/sec
 ZDOT =      18876
946891                 ZDOT =        5753
693412


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   16247
42733615  
00016717  00000-0  10270-3 0  9176
2 25544  51
6402  27
6408 0003048 285
4450  74
6366 15
54373842 17158


Satellite: ISS
Catalog Number: 25544
Epoch time:      16247
42733615   =   yrday
fracday
Element set:     917
Inclination:       51
6402  deg
RA of node:        27
6408  deg
Eccentricity:     
0003048     
Arg of perigee:   285
4450  deg
Mean anomaly:      74
6366  deg
Mean motion:   15
54373842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1715
Checksum:              308
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