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

 
Date: January 31st 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 ET - UTC (sec) : 67 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


There are no maneuvers



Coasting Arc #1 (Orbit 2325)
---------------------------------------

Vector Time (GMT): 2016/029/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1965126
28                 A    =         6776852
16  meter
 Y    =        3711110
42  meter          E    =           
0008425
 Z    =        5312074
09                 I    =           51
82883
 XDOT =      -6526
671002                 Wp   =           68
13986
 YDOT =      -4019
669508  meter/sec      RA   =           33
95768  deg
 ZDOT =        396
324483                 TA   =           18
10924
                                          MA   =           18
07925
                                          Ha   =            223
020  n
mi
                                          Hp   =            212
309

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6447264
69                 X    =        -2032282
18
 Y    =       12175559
11  feet           Y    =         3688759
83  meter
 Z    =       17428064
61                 Z    =         5302364
85
 XDOT =     -21412
962604                 XDOT =       -6483
162138
 YDOT =     -13187
892086  feet/sec       YDOT =       -4092
411776  meter/sec
 ZDOT =       1300
277176                 ZDOT =         364
725870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13364114
42                 X    =        -4073382
07
 Y    =        3564283
52  feet           Y    =         1086393
62  meter
 Z    =       17385201
37                 Z    =         5299009
38
 XDOT =      -4808
141733                 XDOT =       -1465
521600
 YDOT =     -23664
589079  feet/sec       YDOT =       -7212
966751  meter/sec
 ZDOT =       1164
044116                 ZDOT =         354
800647


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   16029
56522138  
00016717  00000-0  10270-3 0  9007
2 25544  51
6395  34
3188 0006563  54
8698 305
3069 15
54310511 23263


Satellite: ISS
Catalog Number: 25544
Epoch time:      16029
56522138   =   yrday
fracday
Element set:     900
Inclination:       51
6395  deg
RA of node:        34
3188  deg
Eccentricity:     
0006563     
Arg of perigee:    54
8698  deg
Mean anomaly:     305
3069  deg
Mean motion:   15
54310511  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2326
Checksum:              304


Coasting Arc #2 (Orbit 2340)
---------------------------------------

Vector Time (GMT): 2016/030/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3537433
77                 A    =         6777734
00  meter
 Y    =       -2668396
36  meter          E    =           
0018755
 Z    =       -5144723
32                 I    =           51
80467
 XDOT =       5846
172556                 Wp   =           87
70399
 YDOT =       4675
628268  meter/sec      RA   =           28
96836  deg
 ZDOT =       1600
415334                 TA   =          197
69073
                                          MA   =          197
75612
                                          Ha   =            222
989  n
mi
                                          Hp   =            212
356

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11605753
84                 X    =         3592000
08
 Y    =       -8754581
22  feet           Y    =        -2628533
56  meter
 Z    =      -16879013
52                 Z    =        -5127406
91
 XDOT =      19180
356154                 XDOT =        5785
679992
 YDOT =      15339
987756  feet/sec       YDOT =        4740
665880  meter/sec
 ZDOT =       5250
706476                 ZDOT =        1628
667105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14444942
36                 X    =         4402818
43
 Y    =        2286417
17  feet           Y    =          696899
95  meter
 Z    =      -16803370
17                 Z    =        -5121667
23
 XDOT =       2528
727080                 XDOT =         770
756014
 YDOT =      23366
543043  feet/sec       YDOT =        7122
122319  meter/sec
 ZDOT =       5372
279687                 ZDOT =        1637
470849


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   16030
52963178  
00016717  00000-0  10270-3 0  9019
2 25544  51
6396  29
5098 0006583  57
8809 302
2982 15
54303723 23413


Satellite: ISS
Catalog Number: 25544
Epoch time:      16030
52963178   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:        29
5098  deg
Eccentricity:     
0006583     
Arg of perigee:    57
8809  deg
Mean anomaly:     302
2982  deg
Mean motion:   15
54303723  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2341
Checksum:              316


Coasting Arc #3 (Orbit 2356)
---------------------------------------

Vector Time (GMT): 2016/031/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4940098
39                 A    =         6780704
70  meter
 Y    =        1563449
33  meter          E    =           
0016155
 Z    =        4364667
33                 I    =           51
78618
 XDOT =      -4652
101032                 Wp   =           66
84324
 YDOT =      -5037
662657  meter/sec      RA   =           23
98166  deg
 ZDOT =      -3444
588879                 TA   =           58
07699
                                          MA   =           57
91997
                                          Ha   =            223
038  n
mi
                                          Hp   =            212
165

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16207671
88                 X    =        -4978415
56
 Y    =        5129426
93  feet           Y    =         1507991
79  meter
 Z    =       14319774
72                 Z    =         4340576
69
 XDOT =     -15262
798662                 XDOT =       -4578
690734
 YDOT =     -16527
764624  feet/sec       YDOT =       -5089
275201  meter/sec
 ZDOT =     -11301
144616                 ZDOT =       -3467
008898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15182535
24                 X    =        -4627636
74
 Y    =       -7840951
56  feet           Y    =        -2389922
04  meter
 Z    =       14214981
48                 Z    =         4332726
36
 XDOT =        291
587113                 XDOT =          88
875752
 YDOT =     -21324
793315  feet/sec       YDOT =       -6499
797002  meter/sec
 ZDOT =     -11397
342531                 ZDOT =       -3473
910004


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   16031
55832576  
00016717  00000-0  10270-3 0  9021
2 25544  51
6392  24
3791 0006567  60
7941 299
3868 15
54352216 23571


Satellite: ISS
Catalog Number: 25544
Epoch time:      16031
55832576   =   yrday
fracday
Element set:     902
Inclination:       51
6392  deg
RA of node:        24
3791  deg
Eccentricity:     
0006567     
Arg of perigee:    60
7941  deg
Mean anomaly:     299
3868  deg
Mean motion:   15
54352216  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2357
Checksum:              326


Coasting Arc #4 (Orbit 2371)
---------------------------------------

Vector Time (GMT): 2016/032/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5995459
79                 A    =         6784641
47  meter
 Y    =        -545179
30  meter          E    =           
0011183
 Z    =       -3132638
61                 I    =           51
76966
 XDOT =       3000
681148                 Wp   =           68
02323
 YDOT =       5094
704536  meter/sec      RA   =           19
00441  deg
 ZDOT =       4874
286020                 TA   =          255
98777
                                          MA   =          256
11213
                                          Ha   =            223
070  n
mi
                                          Hp   =            212
126

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19670143
65                 X    =         6016327
38
 Y    =       -1788645
99  feet           Y    =         -478017
51  meter
 Z    =      -10277685
72                 Z    =        -3103463
75
 XDOT =       9844
754423                 XDOT =        2919
810932
 YDOT =      16714
909895  feet/sec       YDOT =        5127
808106  meter/sec
 ZDOT =      15991
752033                 ZDOT =        4888
665873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15482784
33                 X    =         4719152
66
 Y    =       12368671
81  feet           Y    =         3769971
17  meter
 Z    =      -10151057
90                 Z    =        -3094042
45
 XDOT =      -3637
351468                 XDOT =       -1108
664728
 YDOT =      17678
889298  feet/sec       YDOT =        5388
525458  meter/sec
 ZDOT =      16053
063378                 ZDOT =        4892
973718


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   16032
52271758  
00016717  00000-0  10270-3 0  9039
2 25544  51
6392  19
5700 0006705  64
6189 295
5658 15
54343396 23729


Satellite: ISS
Catalog Number: 25544
Epoch time:      16032
52271758   =   yrday
fracday
Element set:     903
Inclination:       51
6392  deg
RA of node:        19
5700  deg
Eccentricity:     
0006705     
Arg of perigee:    64
6189  deg
Mean anomaly:     295
5658  deg
Mean motion:   15
54343396  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2372
Checksum:              322


Coasting Arc #5 (Orbit 2387)
---------------------------------------

Vector Time (GMT): 2016/033/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6601462
73                 A    =         6787689
97  meter
 Y    =        -440110
95  meter          E    =           
0018714
 Z    =        1489113
23                 I    =           51
74992
 XDOT =       -987
250144                 Wp   =          102
17777
 YDOT =      -4943
869815  meter/sec      RA   =           14
03454  deg
 ZDOT =      -5780
357955                 TA   =           61
58543
                                          MA   =           61
39694
                                          Ha   =            222
964  n
mi
                                          Hp   =            212
012

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21658342
28                 X    =        -6603284
06
 Y    =       -1443933
56  feet           Y    =         -513943
04  meter
 Z    =        4885542
09                 Z    =         1457040
88
 XDOT =      -3239
009660                 XDOT =        -903
814992
 YDOT =     -16220
045325  feet/sec       YDOT =       -4954
443483  meter/sec
 ZDOT =     -18964
428986                 ZDOT =       -5784
950987

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14928919
32                 X    =        -4550334
61
 Y    =      -15799835
81  feet           Y    =        -4815789
96  meter
 Z    =        4746557
92                 Z    =         1446750
86
 XDOT =       7586
298845                 XDOT =        2312
303888
 YDOT =     -12929
339143  feet/sec       YDOT =       -3940
862571  meter/sec
 ZDOT =     -18983
326836                 ZDOT =       -5786
118020


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   16033
55139111  
00016717  00000-0  10270-3 0  9040
2 25544  51
6394  14
4388 0006647  67
1013 293
0841 15
54388390 23883


Satellite: ISS
Catalog Number: 25544
Epoch time:      16033
55139111   =   yrday
fracday
Element set:     904
Inclination:       51
6394  deg
RA of node:        14
4388  deg
Eccentricity:     
0006647     
Arg of perigee:    67
1013  deg
Mean anomaly:     293
0841  deg
Mean motion:   15
54388390  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2388
Checksum:              307


Coasting Arc #6 (Orbit 2403)
---------------------------------------

Vector Time (GMT): 2016/034/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6653791
44                 A    =         6788452
33  meter
 Y    =        1277890
92  meter          E    =           
0018923
 Z    =         269994
43                 I    =           51
72136
 XDOT =      -1143
819537                 Wp   =           56
26458
 YDOT =       4623
344017  meter/sec      RA   =            9
06947  deg
 ZDOT =       6013
889673                 TA   =          306
64287
                                          MA   =          306
81671
                                          Ha   =            222
940  n
mi
                                          Hp   =            211
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21830024
42                 X    =         6637695
73
 Y    =        4192555
50  feet           Y    =         1352208
03  meter
 Z    =         885808
51                 Z    =          302277
40
 XDOT =      -3752
688769                 XDOT =       -1224
646438
 YDOT =      15168
451499  feet/sec       YDOT =        4610
101173  meter/sec
 ZDOT =      19730
609162                 ZDOT =        6008
137008

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13465325
27                 X    =         4104231
14
 Y    =       17678955
07  feet           Y    =         5388545
50  meter
 Z    =        1025527
98                 Z    =          312580
93
 XDOT =     -11718
806997                 XDOT =       -3571
892373
 YDOT =       7734
656540  feet/sec       YDOT =        2357
523313  meter/sec
 ZDOT =      19704
709896                 ZDOT =        6005
995576


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   16034
58005338  
00016717  00000-0  10270-3 0  9058
2 25544  51
6392   9
3088 0006632  72
8054 287
3824 15
54417444 24042


Satellite: ISS
Catalog Number: 25544
Epoch time:      16034
58005338   =   yrday
fracday
Element set:     905
Inclination:       51
6392  deg
RA of node:         9
3088  deg
Eccentricity:     
0006632     
Arg of perigee:    72
8054  deg
Mean anomaly:     287
3824  deg
Mean motion:   15
54417444  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2404
Checksum:              304


Coasting Arc #7 (Orbit 2418)
---------------------------------------

Vector Time (GMT): 2016/035/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6125998
96                 A    =         6786625
09  meter
 Y    =       -2072201
39  meter          E    =           
0011046
 Z    =       -2061403
15                 I    =           51
68447
 XDOT =       3264
054132                 Wp   =          105
37874
 YDOT =      -4159
754033  meter/sec      RA   =            4
09999  deg
 ZDOT =      -5546
089252                 TA   =           97
39387
                                          MA   =           97
26833
                                          Ha   =            222
915  n
mi
                                          Hp   =            211
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20098421
79                 X    =        -6092358
54
 Y    =       -6798560
99  feet           Y    =        -2140518
27  meter
 Z    =       -6763133
69                 Z    =        -2091079
57
 XDOT =      10708
839016                 XDOT =        3337
267052
 YDOT =     -13647
486985  feet/sec       YDOT =       -4122
843854  meter/sec
 ZDOT =     -18195
830879                 ZDOT =       -5530
055711

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10724278
90                 X    =        -3268760
21
 Y    =      -18259398
94  feet           Y    =        -5565464
80  meter
 Z    =       -6891383
00                 Z    =        -2100493
54
 XDOT =      15784
472615                 XDOT =        4811
107253
 YDOT =      -2463
444671  feet/sec       YDOT =        -750
857936  meter/sec
 ZDOT =     -18125
449385                 ZDOT =       -5524
636973


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   16035
54441582  
00016717  00000-0  10270-3 0  9061
2 25544  51
6400   4
4983 0006636  74
1503 286
0381 15
54413077 24198


Satellite: ISS
Catalog Number: 25544
Epoch time:      16035
54441582   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:         4
4983  deg
Eccentricity:     
0006636     
Arg of perigee:    74
1503  deg
Mean anomaly:     286
0381  deg
Mean motion:   15
54413077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2419
Checksum:              293


Coasting Arc #8 (Orbit 2434)
---------------------------------------

Vector Time (GMT): 2016/036/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5067572
33                 A    =         6782897
71  meter
 Y    =        2742000
52  meter          E    =           
0018372
 Z    =        3562398
85                 I    =           51
64077
 XDOT =      -5100
449808                 Wp   =           87
81416
 YDOT =       3607
882067  meter/sec      RA   =          359
12124  deg
 ZDOT =       4459
299735                 TA   =          314
30295
                                          MA   =          314
45347
                                          Ha   =            222
769  n
mi
                                          Hp   =            211
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16625893
48                 X    =         5019229
69
 Y    =        8996064
69  feet           Y    =         2798399
17  meter
 Z    =       11687660
27                 Z    =         3586897
98
 XDOT =     -16733
759213                 XDOT =       -5162
075922
 YDOT =      11836
883421  feet/sec       YDOT =        3550
500888  meter/sec
 ZDOT =      14630
248473                 ZDOT =        4434
373800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6938296
14                 X    =         2114792
66
 Y    =       17513667
61  feet           Y    =         5338165
89  meter
 Z    =       11793320
56                 Z    =         3594604
11
 XDOT =     -19227
074861                 XDOT =       -5860
412418
 YDOT =      -2203
288265  feet/sec       YDOT =        -671
562263  meter/sec
 ZDOT =      14521
426884                 ZDOT =        4426
130914


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   16036
57305633  
00016717  00000-0  10270-3 0  9072
2 25544  51
6404 359
3684 0006506  79
0870 281
1014 15
54453419 24350


Satellite: ISS
Catalog Number: 25544
Epoch time:      16036
57305633   =   yrday
fracday
Element set:     907
Inclination:       51
6404  deg
RA of node:       359
3684  deg
Eccentricity:     
0006506     
Arg of perigee:    79
0870  deg
Mean anomaly:     281
1014  deg
Mean motion:   15
54453419  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2435
Checksum:              306


Coasting Arc #9 (Orbit 2449)
---------------------------------------

Vector Time (GMT): 2016/037/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3554046
33                 A    =         6778994
59  meter
 Y    =       -3378008
97  meter          E    =           
0017396
 Z    =       -4697758
18                 I    =           51
59600
 XDOT =       6492
418951                 Wp   =           74
25524
 YDOT =      -2914
917536  meter/sec      RA   =          354
12718  deg
 ZDOT =      -2819
854465                 TA   =          167
72758
                                          MA   =          167
68515
                                          Ha   =            222
898  n
mi
                                          Hp   =            211
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11660256
98                 X    =        -3493189
27
 Y    =      -11082706
58  feet           Y    =        -3417412
45  meter
 Z    =      -15412592
46                 Z    =        -4714874
62
 XDOT =      21300
587110                 XDOT =        6538
229091
 YDOT =      -9563
377744  feet/sec       YDOT =       -2842
058898  meter/sec
 ZDOT =      -9251
491028                 ZDOT =       -2788
205313

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2044273
05                 X    =         -623094
43
 Y    =      -15885127
86  feet           Y    =        -4841786
97  meter
 Z    =      -15486111
36                 Z    =        -4720166
74
 XDOT =      21473
303588                 XDOT =        6545
062934
 YDOT =       6108
273509  feet/sec       YDOT =        1861
801766  meter/sec
 ZDOT =      -9113
666378                 ZDOT =       -2777
845512


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   16037
53739887  
00016717  00000-0  10270-3 0  9082
2 25544  51
6407 354
5576 0006593  81
2503 278
9397 15
54443910 24504


Satellite: ISS
Catalog Number: 25544
Epoch time:      16037
53739887   =   yrday
fracday
Element set:     908
Inclination:       51
6407  deg
RA of node:       354
5576  deg
Eccentricity:     
0006593     
Arg of perigee:    81
2503  deg
Mean anomaly:     278
9397  deg
Mean motion:   15
54443910  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2450
Checksum:              340


Coasting Arc #10 (Orbit 2465)
---------------------------------------

Vector Time (GMT): 2016/038/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1752518
49                 A    =         6776526
45  meter
 Y    =        3904117
04  meter          E    =           
0009316
 Z    =        5246422
53                 I    =           51
55699
 XDOT =      -7327
912322                 Wp   =           95
85065
 YDOT =       2113
559416  meter/sec      RA   =          349
12302  deg
 ZDOT =        872
755400                 TA   =          345
78971
                                          MA   =          345
81589
                                          Ha   =            222
743  n
mi
                                          Hp   =            211
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5749732
60                 X    =         1683247
21
 Y    =       12808782
95  feet           Y    =         3923327
70  meter
 Z    =       17212672
36                 Z    =         5254767
26
 XDOT =     -24041
707092                 XDOT =       -7355
241409
 YDOT =       6934
250051  feet/sec       YDOT =        2031
461063  meter/sec
 ZDOT =       2863
370734                 ZDOT =         837
092673

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3416598
78                 X    =        -1041379
31
 Y    =       13573206
37  feet           Y    =         4137113
30  meter
 Z    =       17248053
71                 Z    =         5257206
77
 XDOT =     -22257
016772                 XDOT =       -6783
938712
 YDOT =      -9053
445954  feet/sec       YDOT =       -2759
490327  meter/sec
 ZDOT =       2708
315608                 ZDOT =         825
494597


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   16038
56601793  
00016717  00000-0  10270-3 0  9091
2 25544  51
6414 349
4278 0006440  84
9499 275
2389 15
54485567 24661


Satellite: ISS
Catalog Number: 25544
Epoch time:      16038
56601793   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       349
4278  deg
Eccentricity:     
0006440     
Arg of perigee:    84
9499  deg
Mean anomaly:     275
2389  deg
Mean motion:   15
54485567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2466
Checksum:              356


Coasting Arc #11 (Orbit 2480)
---------------------------------------

Vector Time (GMT): 2016/039/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         160496
17                 A    =         6776883
77  meter
 Y    =       -4351217
66  meter          E    =           
0020498
 Z    =       -5211019
19                 I    =           51
52681
 XDOT =       7473
565659                 Wp   =           95
38436
 YDOT =      -1145
197952  meter/sec      RA   =          344
11172  deg
 ZDOT =       1188
582315                 TA   =          186
04433
                                          MA   =          186
06910
                                          Ha   =            222
847  n
mi
                                          Hp   =            211
736

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         526562
24                 X    =          234452
87
 Y    =      -14275648
47  feet           Y    =        -4349009
63  meter
 Z    =      -17096519
66                 Z    =        -5210059
72
 XDOT =      24519
572371                 XDOT =        7480
042625
 YDOT =      -3757
211128  feet/sec       YDOT =       -1061
587312  meter/sec
 ZDOT =       3899
548278                 ZDOT =        1224
901884

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9081603
34                 X    =         2768072
70
 Y    =      -11034868
99  feet           Y    =        -3363428
07  meter
 Z    =      -17091475
62                 Z    =        -5209481
77
 XDOT =      21038
065263                 XDOT =        6412
402292
 YDOT =      11041
005771  feet/sec       YDOT =        3365
298559  meter/sec
 ZDOT =       4057
245313                 ZDOT =        1236
648372


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   16039
53034008  
00016717  00000-0  10270-3 0  9100
2 25544  51
6416 344
6172 0006506  88
0094 272
1804 15
54466251 24816


Satellite: ISS
Catalog Number: 25544
Epoch time:      16039
53034008   =   yrday
fracday
Element set:     910
Inclination:       51
6416  deg
RA of node:       344
6172  deg
Eccentricity:     
0006506     
Arg of perigee:    88
0094  deg
Mean anomaly:     272
1804  deg
Mean motion:   15
54466251  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2481
Checksum:              290


Coasting Arc #12 (Orbit 2496)
---------------------------------------

Vector Time (GMT): 2016/040/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2015795
14                 A    =         6779640
90  meter
 Y    =        4619800
67  meter          E    =           
0015092
 Z    =        4523007
53                 I    =           51
50606
 XDOT =      -7010
221630                 Wp   =           77
48648
 YDOT =         14
470725  meter/sec      RA   =          339
10412  deg
 ZDOT =      -3127
044132                 TA   =           43
93879
                                          MA   =           43
81889
                                          Ha   =            222
878  n
mi
                                          Hp   =            211
713

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6613501
12                 X    =        -2089275
36
 Y    =       15156826
35  feet           Y    =         4596848
18  meter
 Z    =       14839263
55                 Z    =         4513036
75
 XDOT =     -22999
414795                 XDOT =       -6994
672974
 YDOT =         47
476131  feet/sec       YDOT =         -63
835506  meter/sec
 ZDOT =     -10259
331142                 ZDOT =       -3161
059430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14325029
92                 X    =        -4366269
12
 Y    =        8340856
87  feet           Y    =         2542293
18  meter
 Z    =       14795105
59                 Z    =         4509548
18
 XDOT =     -17991
921161                 XDOT =       -5483
937570
 YDOT =     -12370
404411  feet/sec       YDOT =       -3770
499264  meter/sec
 ZDOT =     -10406
800486                 ZDOT =       -3171
992788


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   16040
55893884  
00016717  00000-0  10270-3 0  9110
2 25544  51
6420 339
4872 0006543  92
0076 268
1826 15
54486296 24973


Satellite: ISS
Catalog Number: 25544
Epoch time:      16040
55893884   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:       339
4872  deg
Eccentricity:     
0006543     
Arg of perigee:    92
0076  deg
Mean anomaly:     268
1826  deg
Mean motion:   15
54486296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2497
Checksum:              337


Coasting Arc #13 (Orbit 2511)
---------------------------------------

Vector Time (GMT): 2016/041/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3596120
21                 A    =         6783589
18  meter
 Y    =       -4694463
65  meter          E    =           
0011132
 Z    =       -3333479
13                 I    =           51
48985
 XDOT =       5942
705179                 Wp   =           90
59216
 YDOT =       1245
730451  meter/sec      RA   =          334
10416  deg
 ZDOT =       4670
006295                 TA   =          230
53826
                                          MA   =          230
63680
                                          Ha   =            222
793  n
mi
                                          Hp   =            211
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11798294
65                 X    =         3664539
85
 Y    =      -15401783
62  feet           Y    =        -4653867
18  meter
 Z    =      -10936611
31                 Z    =        -3315843
87
 XDOT =      19497
064237                 XDOT =        5905
649054
 YDOT =       4087
042161  feet/sec       YDOT =        1311
978936  meter/sec
 ZDOT =      15321
542962                 ZDOT =        4698
783728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18549574
11                 X    =         5653910
19
 Y    =       -5832216
60  feet           Y    =        -1777659
62  meter
 Z    =      -10859222
44                 Z    =        -3309891
00
 XDOT =      13137
250400                 XDOT =        4004
233922
 YDOT =      13106
467447  feet/sec       YDOT =        3994
851278  meter/sec
 ZDOT =      15446
044529                 ZDOT =        4707
954373


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   16041
52323958  
00016717  00000-0  10270-3 0  9129
2 25544  51
6420 334
6772 0006489  95
2884 264
9010 15
54505077 25126


Satellite: ISS
Catalog Number: 25544
Epoch time:      16041
52323958   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:       334
6772  deg
Eccentricity:     
0006489     
Arg of perigee:    95
2884  deg
Mean anomaly:     264
9010  deg
Mean motion:   15
54505077  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2512
Checksum:              309


Coasting Arc #14 (Orbit 2527)
---------------------------------------

Vector Time (GMT): 2016/042/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4822366
69                 A    =         6787042
30  meter
 Y    =        4453317
24  meter          E    =           
0020270
 Z    =        1690912
98                 I    =           51
47346
 XDOT =      -4433
811999                 Wp   =          110
33791
 YDOT =      -2623
664724  meter/sec      RA   =          329
11375  deg
 ZDOT =      -5686
602199                 TA   =           51
06760
                                          MA   =           50
88709
                                          Ha   =            222
780  n
mi
                                          Hp   =            211
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15821413
03                 X    =        -4880019
96
 Y    =       14610620
88  feet           Y    =         4399068
15  meter
 Z    =        5547614
76                 Z    =         1667347
09
 XDOT =     -14546
627294                 XDOT =       -4376
521427
 YDOT =      -8607
823897  feet/sec       YDOT =       -2672
926766  meter/sec
 ZDOT =     -18656
831362                 ZDOT =       -5708
000763

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21313132
61                 X    =        -6496242
82
 Y    =        3266547
79  feet           Y    =          995643
77  meter
 Z    =        5444577
67                 Z    =         1659507
27
 XDOT =      -6922
052637                 XDOT =       -2109
841644
 YDOT =     -13643
835581  feet/sec       YDOT =       -4158
641085  meter/sec
 ZDOT =     -18749
066867                 ZDOT =       -5714
715581


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   16042
55181671  
00016717  00000-0  10270-3 0  9138
2 25544  51
6423 329
5462 0006528  99
2165 260
9727 15
54515343 25283


Satellite: ISS
Catalog Number: 25544
Epoch time:      16042
55181671   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:       329
5462  deg
Eccentricity:     
0006528     
Arg of perigee:    99
2165  deg
Mean anomaly:     260
9727  deg
Mean motion:   15
54515343  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2528
Checksum:              315


Coasting Arc #15 (Orbit 2543)
---------------------------------------

Vector Time (GMT): 2016/043/12:23:33
678
Vector Time (MET): N/A
Weight (LBS)     : 922504
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5543663
81                 A    =         6788161
04  meter
 Y    =       -3907272
36  meter          E    =           
0016918
 Z    =         103200
09                 I    =           51
45006
 XDOT =       2669
494093                 Wp   =           64
72033
 YDOT =       3966
025492  meter/sec      RA   =          324
12840  deg
 ZDOT =       5996
088394                 TA   =          296
39438
                                          MA   =          296
56794
                                          Ha   =            222
721  n
mi
                                          Hp   =            211
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18187873
40                 X    =         5586442
59
 Y    =      -12819135
04  feet           Y    =        -3845040
24  meter
 Z    =         338582
96                 Z    =          130233
72
 XDOT =       8758
182720                 XDOT =        2595
820599
 YDOT =      13011
894658  feet/sec       YDOT =        3995
466182  meter/sec
 ZDOT =      19672
206018                 ZDOT =        6008
876630

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22232674
19                 X    =         6776519
09
 Y    =        -862193
69  feet           Y    =         -262796
64  meter
 Z    =         456531
27                 Z    =          139150
73
 XDOT =         99
483308                 XDOT =          30
322512
 YDOT =      13994
010286  feet/sec       YDOT =        4265
374335  meter/sec
 ZDOT =      19726
852246                 ZDOT =        6012
744564


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   16043
58038268  
00016717  00000-0  10270-3 0  9146
2 25544  51
6419 324
4155 0006458 102
2299 257
9577 15
54527973 25445


Satellite: ISS
Catalog Number: 25544
Epoch time:      16043
58038268   =   yrday
fracday
Element set:     914
Inclination:       51
6419  deg
RA of node:       324
4155  deg
Eccentricity:     
0006458     
Arg of perigee:   102
2299  deg
Mean anomaly:     257
9577  deg
Mean motion:   15
54527973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2544
Checksum:              335
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