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

 
Date: May 30th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13813 3257 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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


160/13:47:39 077 -0 2 1 9 2 0
N/A 1 9 -0 2 220 2
000/00:05:18 153 0 2 -0 0 214 9

161/01:18:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 214 8

Coasting Arc #1 (Orbit 175)
---------------------------------------

Vector Time (GMT): 2016/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4534160
59                 A    =         6783916
95  meter
 Y    =        4104747
54  meter          E    =           
0005594
 Z    =       -2938749
84                 I    =           51
76823
 XDOT =      -5317
486063                 Wp   =           82
21237
 YDOT =      -2283
418774  meter/sec      RA   =          160
08885  deg
 ZDOT =       5023
804118                 TA   =          244
32833
                                          MA   =          244
38612
                                          Ha   =            220
583  n
mi
                                          Hp   =            213
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14875854
94                 X    =        -4565448
68
 Y    =       13467019
50  feet           Y    =         4053868
84  meter
 Z    =       -9641567
70                 Z    =        -2960851
39
 XDOT =     -17445
820418                 XDOT =       -5315
960655
 YDOT =      -7491
531410  feet/sec       YDOT =       -2342
874325  meter/sec
 ZDOT =      16482
296976                 ZDOT =        4997
976526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5818140
50                 X    =         1773369
23
 Y    =       19155238
93  feet           Y    =         5838516
83  meter
 Z    =       -9738458
03                 Z    =        -2968282
01
 XDOT =     -12892
566322                 XDOT =       -3929
654215
 YDOT =      12223
793173  feet/sec       YDOT =        3725
812159  meter/sec
 ZDOT =      16370
271755                 ZDOT =        4989
658831


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   16148
50606296  
00016717  00000-0  10270-3 0  9001
2 25544  51
6409 161
2087 0001609 124
5472 235
5834 15
54704009  1762


Satellite: ISS
Catalog Number: 25544
Epoch time:      16148
50606296   =   yrday
fracday
Element set:     900
Inclination:       51
6409  deg
RA of node:       161
2087  deg
Eccentricity:     
0001609     
Arg of perigee:   124
5472  deg
Mean anomaly:     235
5834  deg
Mean motion:   15
54704009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             176
Checksum:              297


Coasting Arc #2 (Orbit 191)
---------------------------------------

Vector Time (GMT): 2016/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5613646
66                 A    =         6787057
59  meter
 Y    =       -3617200
68  meter          E    =           
0015310
 Z    =        1169261
02                 I    =           51
80753
 XDOT =       3481
091814                 Wp   =          122
33618
 YDOT =       3485
773462  meter/sec      RA   =          155
12127  deg
 ZDOT =      -5881
187280                 TA   =           44
98778
                                          MA   =           44
86385
                                          Ha   =            220
602  n
mi
                                          Hp   =            213
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18417475
90                 X    =         5647998
10
 Y    =      -11867456
30  feet           Y    =        -3554233
16  meter
 Z    =        3836158
20                 Z    =         1196613
99
 XDOT =      11420
904900                 XDOT =        3470
422669
 YDOT =      11436
264638  feet/sec       YDOT =        3524
642097  meter/sec
 ZDOT =     -19295
233858                 ZDOT =       -5864
302623

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3212491
55                 X    =         -979167
43
 Y    =      -21651496
27  feet           Y    =        -6599376
06  meter
 Z    =        3955838
08                 Z    =         1205739
45
 XDOT =      13602
725058                 XDOT =        4146
110598
 YDOT =      -5558
246545  feet/sec       YDOT =       -1694
153547  meter/sec
 ZDOT =     -19222
327342                 ZDOT =       -5858
965374


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   16149
53452301  
00016717  00000-0  10270-3 0  9012
2 25544  51
6399 156
0773 0001584 123
1384 236
9921 15
54699194  1921


Satellite: ISS
Catalog Number: 25544
Epoch time:      16149
53452301   =   yrday
fracday
Element set:     901
Inclination:       51
6399  deg
RA of node:       156
0773  deg
Eccentricity:     
0001584     
Arg of perigee:   123
1384  deg
Mean anomaly:     236
9921  deg
Mean motion:   15
54699194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             192
Checksum:              317


Coasting Arc #3 (Orbit 207)
---------------------------------------

Vector Time (GMT): 2016/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6108789
65                 A    =         6787371
00  meter
 Y    =        2857365
28  meter          E    =           
0013478
 Z    =         713623
96                 I    =           51
83669
 XDOT =      -1439
060440                 Wp   =           59
23670
 YDOT =      -4588
097841  meter/sec      RA   =          150
16214  deg
 ZDOT =       5975
276953                 TA   =          308
45457
                                          MA   =          308
57544
                                          Ha   =            220
484  n
mi
                                          Hp   =            213
332

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20041960
79                 X    =        -6143753
90
 Y    =        9374558
01  feet           Y    =         2788857
19  meter
 Z    =        2341285
95                 Z    =          683864
07
 XDOT =      -4721
326902                 XDOT =       -1416
673693
 YDOT =     -15052
814439  feet/sec       YDOT =       -4604
065540  meter/sec
 ZDOT =      19603
927010                 ZDOT =        5968
340436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         636105
61                 X    =          193884
99
 Y    =       22130294
34  feet           Y    =         6745313
72  meter
 Z    =        2211242
19                 Z    =          673986
62
 XDOT =     -14124
378593                 XDOT =       -4305
110595
 YDOT =      -1576
563799  feet/sec       YDOT =        -480
536646  meter/sec
 ZDOT =      19574
510124                 ZDOT =        5966
310686


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   16150
56297941  
00016717  00000-0  10270-3 0  9025
2 25544  51
6390 150
9470 0001562 135
4428 224
6851 15
54736909  2080


Satellite: ISS
Catalog Number: 25544
Epoch time:      16150
56297941   =   yrday
fracday
Element set:     902
Inclination:       51
6390  deg
RA of node:       150
9470  deg
Eccentricity:     
0001562     
Arg of perigee:   135
4428  deg
Mean anomaly:     224
6851  deg
Mean motion:   15
54736909  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             208
Checksum:              309


Coasting Arc #4 (Orbit 222)
---------------------------------------

Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6036673
71                 A    =         6785024
65  meter
 Y    =       -1760526
89  meter          E    =           
0006796
 Z    =       -2546020
75                 I    =           51
85532
 XDOT =       -624
669885                 Wp   =          130
88222
 YDOT =       5503
123801  meter/sec      RA   =          145
20013  deg
 ZDOT =      -5299
972172                 TA   =           77
62050
                                          MA   =           77
54445
                                          Ha   =            220
606  n
mi
                                          Hp   =            213
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19805359
94                 X    =         6068279
27
 Y    =       -5776006
87  feet           Y    =        -1692843
94  meter
 Z    =       -8353086
44                 Z    =        -2516619
18
 XDOT =      -2049
441881                 XDOT =        -660
415582
 YDOT =      18054
868115  feet/sec       YDOT =        5495
938726  meter/sec
 ZDOT =     -17388
360145                 ZDOT =       -5303
093233

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2233881
24                 X    =          680887
00
 Y    =      -20560920
10  feet           Y    =        -6266968
45  meter
 Z    =       -8224775
40                 Z    =        -2506911
54
 XDOT =      14450
419586                 XDOT =        4404
487890
 YDOT =       8513
426440  feet/sec       YDOT =        2594
892379  meter/sec
 ZDOT =     -17402
889650                 ZDOT =       -5304
400765


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   16151
52715967  
00016717  00000-0  10270-3 0  9036
2 25544  51
6386 146
1358 0001493 130
6539 229
4744 15
54691068  2237


Satellite: ISS
Catalog Number: 25544
Epoch time:      16151
52715967   =   yrday
fracday
Element set:     903
Inclination:       51
6386  deg
RA of node:       146
1358  deg
Eccentricity:     
0001493     
Arg of perigee:   130
6539  deg
Mean anomaly:     229
4744  deg
Mean motion:   15
54691068  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             223
Checksum:              317


Coasting Arc #5 (Orbit 238)
---------------------------------------

Vector Time (GMT): 2016/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5439723
66                 A    =         6780863
13  meter
 Y    =         423033
47  meter          E    =           
0012000
 Z    =        4018581
46                 I    =           51
86758
 XDOT =       2461
164552                 Wp   =          105
07194
 YDOT =      -6092
837906  meter/sec      RA   =          140
23047  deg
 ZDOT =       3960
043353                 TA   =          303
86026
                                          MA   =          303
97440
                                          Ha   =            220
528  n
mi
                                          Hp   =            213
431

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17846862
40                 X    =        -5463570
59
 Y    =        1387905
07  feet           Y    =          362069
31  meter
 Z    =       13184322
37                 Z    =         3992098
44
 XDOT =       8074
686849                 XDOT =        2509
876868
 YDOT =     -19989
625676  feet/sec       YDOT =       -6065
043363  meter/sec
 ZDOT =      12992
268219                 ZDOT =        3972
117215

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5259743
34                 X    =        -1603169
77
 Y    =       17198870
37  feet           Y    =         5242215
69  meter
 Z    =       13068936
17                 Z    =         3983411
75
 XDOT =     -14431
644599                 XDOT =       -4398
765274
 YDOT =     -14359
078159  feet/sec       YDOT =       -4376
647023  meter/sec
 ZDOT =      13045
889850                 ZDOT =        3976
387226


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   16152
55561201  
00016717  00000-0  10270-3 0  9041
2 25544  51
6386 141
0051 0001323 138
8136 221
3117 15
54723209  2391


Satellite: ISS
Catalog Number: 25544
Epoch time:      16152
55561201   =   yrday
fracday
Element set:     904
Inclination:       51
6386  deg
RA of node:       141
0051  deg
Eccentricity:     
0001323     
Arg of perigee:   138
8136  deg
Mean anomaly:     221
3117  deg
Mean motion:   15
54723209  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             239
Checksum:              266


Coasting Arc #6 (Orbit 253)
---------------------------------------

Vector Time (GMT): 2016/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4438668
84                 A    =         6777193
61  meter
 Y    =        1131939
37  meter          E    =           
0013272
 Z    =       -5006735
63                 I    =           51
87840
 XDOT =      -3944
601527                 Wp   =           79
75818
 YDOT =       6222
752570  meter/sec      RA   =          135
24863  deg
 ZDOT =      -2092
595997                 TA   =          169
93318
                                          MA   =          169
90657
                                          Ha   =            220
496  n
mi
                                          Hp   =            213
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14562561
82                 X    =         4450002
24
 Y    =        3713711
84  feet           Y    =         1181639
20  meter
 Z    =      -16426297
99                 Z    =        -4985145
77
 XDOT =     -12941
606060                 XDOT =       -4003
727655
 YDOT =      20415
854889  feet/sec       YDOT =        6178
310947  meter/sec
 ZDOT =      -6865
472432                 ZDOT =       -2111
901388

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8602855
92                 X    =         2622150
48
 Y    =      -12446851
73  feet           Y    =        -3793800
41  meter
 Z    =      -16332479
30                 Z    =        -4978139
69
 XDOT =      13715
230014                 XDOT =        4180
402108
 YDOT =      18589
526316  feet/sec       YDOT =        5666
087621  meter/sec
 ZDOT =      -6950
621984                 ZDOT =       -2118
549581


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   16153
51978629  
00016717  00000-0  10270-3 0  9055
2 25544  51
6379 136
1938 0001343 134
2772 225
8491 15
54694839  2547


Satellite: ISS
Catalog Number: 25544
Epoch time:      16153
51978629   =   yrday
fracday
Element set:     905
Inclination:       51
6379  deg
RA of node:       136
1938  deg
Eccentricity:     
0001343     
Arg of perigee:   134
2772  deg
Mean anomaly:     225
8491  deg
Mean motion:   15
54694839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             254
Checksum:              336


Coasting Arc #7 (Orbit 269)
---------------------------------------

Vector Time (GMT): 2016/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3169257
39                 A    =         6775694
56  meter
 Y    =       -2725479
99  meter          E    =           
0003346
 Z    =        5329940
87                 I    =           51
89549
 XDOT =       4975
618300                 Wp   =          107
54234
 YDOT =      -5840
206345  meter/sec      RA   =          130
26097  deg
 ZDOT =        -28
801929                 TA   =          342
72531
                                          MA   =          342
73669
                                          Ha   =            220
545  n
mi
                                          Hp   =            213
479

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10397826
07                 X    =        -3164435
82
 Y    =       -8941863
50  feet           Y    =        -2760894
21  meter
 Z    =       17486682
64                 Z    =         5314556
64
 XDOT =      16324
207020                 XDOT =        5040
695059
 YDOT =     -19160
781973  feet/sec       YDOT =       -5784
201801  meter/sec
 ZDOT =        -94
494517                 ZDOT =          -4
473628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11931385
37                 X    =        -3636686
26
 Y    =        6930780
67  feet           Y    =         2112501
95  meter
 Z    =       17420163
66                 Z    =         5309665
88
 XDOT =     -12121
114629                 XDOT =       -3694
515739
 YDOT =     -20905
972912  feet/sec       YDOT =       -6372
140544  meter/sec
 ZDOT =         12
483190                 ZDOT =           3
804876


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   16154
54823663  
00016717  00000-0  10270-3 0  9067
2 25544  51
6377 131
0626 0001261 141
3673 218
7571 15
54695616  2703


Satellite: ISS
Catalog Number: 25544
Epoch time:      16154
54823663   =   yrday
fracday
Element set:     906
Inclination:       51
6377  deg
RA of node:       131
0626  deg
Eccentricity:     
0001261     
Arg of perigee:   141
3673  deg
Mean anomaly:     218
7571  deg
Mean motion:   15
54695616  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             270
Checksum:              304


Coasting Arc #8 (Orbit 284)
---------------------------------------

Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1793657
42                 A    =         6777196
25  meter
 Y    =        4234809
02  meter          E    =           
0013527
 Z    =       -4990374
77                 I    =           51
92166
 XDOT =      -5507
770374                 Wp   =          108
85474
 YDOT =       4867
460399  meter/sec      RA   =          125
27445  deg
 ZDOT =       2151
387550                 TA   =          182
04978
                                          MA   =          182
05533
                                          Ha   =            220
405  n
mi
                                          Hp   =            213
560

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5884702
82                 X    =         1770410
90
 Y    =       13893730
39  feet           Y    =         4254737
43  meter
 Z    =      -16372620
65                 Z    =        -4981717
52
 XDOT =     -18070
112776                 XDOT =       -5572
240867
 YDOT =      15969
358265  feet/sec       YDOT =        4805
508146  meter/sec
 ZDOT =       7058
358105                 ZDOT =        2124
475654

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15074477
05                 X    =         4594700
60
 Y    =       -1278370
99  feet           Y    =         -389647
48  meter
 Z    =      -16335669
18                 Z    =        -4979111
97
 XDOT =       9312
178757                 XDOT =        2838
352085
 YDOT =      21143
521970  feet/sec       YDOT =        6444
545496  meter/sec
 ZDOT =       6940
276742                 ZDOT =        2115
396351


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   16155
51240519  
00016717  00000-0  10270-3 0  9079
2 25544  51
6388 126
2519 0001191 142
0853 218
0384 15
54693003  2851


Satellite: ISS
Catalog Number: 25544
Epoch time:      16155
51240519   =   yrday
fracday
Element set:     907
Inclination:       51
6388  deg
RA of node:       126
2519  deg
Eccentricity:     
0001191     
Arg of perigee:   142
0853  deg
Mean anomaly:     218
0384  deg
Mean motion:   15
54693003  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             285
Checksum:              294


Coasting Arc #9 (Orbit 300)
---------------------------------------

Vector Time (GMT): 2016/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -422155
92                 A    =         6780862
63  meter
 Y    =       -5462278
76  meter          E    =           
0011419
 Z    =        3986763
22                 I    =           51
95201
 XDOT =       5605
613431                 Wp   =           84
24949
 YDOT =      -3369
575168  meter/sec      RA   =          120
29776  deg
 ZDOT =      -4012
138563                 TA   =           47
40402
                                          MA   =           47
30775
                                          Ha   =            220
351  n
mi
                                          Hp   =            213
502

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1385025
99                 X    =         -380410
21
 Y    =      -17920862
08  feet           Y    =        -5466766
67  meter
 Z    =       13079931
83                 Z    =         3984813
18
 XDOT =      18391
120180                 XDOT =        5662
365744
 YDOT =     -11055
036642  feet/sec       YDOT =       -3306
571648  meter/sec
 ZDOT =     -13163
184262                 ZDOT =       -3984
770096

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17532635
43                 X    =        -5343947
28
 Y    =       -3984800
80  feet           Y    =        -1214567
28  meter
 Z    =       13072423
98                 Z    =         3984474
83
 XDOT =      -5282
351276                 XDOT =       -1610
060669
 YDOT =     -19665
938428  feet/sec       YDOT =       -5994
178033  meter/sec
 ZDOT =     -13043
359967                 ZDOT =       -3975
616118


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   16156
54084961  
00016717  00000-0  10270-3 0  9081
2 25544  51
6387 121
1205 0001071 144
0155 216
1070 15
54721197  3016


Satellite: ISS
Catalog Number: 25544
Epoch time:      16156
54084961   =   yrday
fracday
Element set:     908
Inclination:       51
6387  deg
RA of node:       121
1205  deg
Eccentricity:     
0001071     
Arg of perigee:   144
0155  deg
Mean anomaly:     216
1070  deg
Mean motion:   15
54721197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             301
Checksum:              271


Coasting Arc #10 (Orbit 315)
---------------------------------------

Vector Time (GMT): 2016/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -803566
21                 A    =         6785001
39  meter
 Y    =        6257729
56  meter          E    =           
0005261
 Z    =       -2496103
50                 I    =           51
98139
 XDOT =      -5304
131732                 Wp   =           61
22996
 YDOT =       1444
963889  meter/sec      RA   =          115
33510  deg
 ZDOT =       5341
031973                 TA   =          270
93186
                                          MA   =          270
99213
                                          Ha   =            220
328  n
mi
                                          Hp   =            213
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2636372
07                 X    =         -861356
88
 Y    =       20530608
81  feet           Y    =         6248420
77  meter
 Z    =       -8189315
94                 Z    =        -2500146
56
 XDOT =     -17402
006994                 XDOT =       -5345
840129
 YDOT =       4740
695175  feet/sec       YDOT =        1385
415610  meter/sec
 ZDOT =      17523
070779                 ZDOT =        5315
164486

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18949722
17                 X    =         5775875
32
 Y    =        8310043
10  feet           Y    =         2532901
14  meter
 Z    =       -8208073
14                 Z    =        -2501820
69
 XDOT =        176
605713                 XDOT =          53
829421
 YDOT =      16758
328712  feet/sec       YDOT =        5107
938591  meter/sec
 ZDOT =      17410
115662                 ZDOT =        5306
603254


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   16157
50501532  
00016717  00000-0  10270-3 0  9097
2 25544  51
6390 116
3104 0001075 148
1513 211
9705 15
54702660  3169


Satellite: ISS
Catalog Number: 25544
Epoch time:      16157
50501532   =   yrday
fracday
Element set:     909
Inclination:       51
6390  deg
RA of node:       116
3104  deg
Eccentricity:     
0001075     
Arg of perigee:   148
1513  deg
Mean anomaly:     211
9705  deg
Mean motion:   15
54702660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             316
Checksum:              270


Coasting Arc #11 (Orbit 331)
---------------------------------------

Vector Time (GMT): 2016/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1868526
65                 A    =         6787430
88  meter
 Y    =       -6485436
25  meter          E    =           
0014114
 Z    =         649512
74                 I    =           52
00445
 XDOT =       4720
690321                 Wp   =          129
97376
 YDOT =        751
485067  meter/sec      RA   =          110
38355  deg
 ZDOT =      -5999
835757                 TA   =           43
04440
                                          MA   =           42
93409
                                          Ha   =            220
276  n
mi
                                          Hp   =            213
570

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6130336
76                 X    =         1937754
48
 Y    =      -21277677
98  feet           Y    =        -6464154
16  meter
 Z    =        2130947
30                 Z    =          658756
82
 XDOT =      15487
829137                 XDOT =        4741
080905
 YDOT =       2465
502188  feet/sec       YDOT =         804
389841  meter/sec
 ZDOT =     -19684
500516                 ZDOT =       -5976
854094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18864869
34                 X    =        -5750012
17
 Y    =      -11587011
50  feet           Y    =        -3531721
11  meter
 Z    =        2172421
36                 Z    =          662154
03
 XDOT =       5707
080803                 XDOT =        1739
518229
 YDOT =     -13010
080464  feet/sec       YDOT =       -3965
472525  meter/sec
 ZDOT =     -19584
508583                 ZDOT =       -5969
358216


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   16158
53345608  
00016717  00000-0  10270-3 0  9103
2 25544  51
6410 111
1789 0001035 154
7855 205
3349 15
54718635  3320


Satellite: ISS
Catalog Number: 25544
Epoch time:      16158
53345608   =   yrday
fracday
Element set:     910
Inclination:       51
6410  deg
RA of node:       111
1789  deg
Eccentricity:     
0001035     
Arg of perigee:   154
7855  deg
Mean anomaly:     205
3349  deg
Mean motion:   15
54718635  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             332
Checksum:              297


Coasting Arc #12 (Orbit 347)
---------------------------------------

Vector Time (GMT): 2016/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2693776
94                 A    =         6786940
20  meter
 Y    =        6096629
61  meter          E    =           
0013659
 Z    =        1247088
45                 I    =           52
01302
 XDOT =      -3945
511931                 Wp   =           62
86363
 YDOT =      -2954
327431  meter/sec      RA   =          105
43636  deg
 ZDOT =       5877
083806                 TA   =          310
63053
                                          MA   =          310
74924
                                          Ha   =            220
249  n
mi
                                          Hp   =            213
583

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8837850
85                 X    =        -2767808
59
 Y    =       20002065
63  feet           Y    =         6066091
89  meter
 Z    =        4091497
55                 Z    =         1233823
79
 XDOT =     -12944
592949                 XDOT =       -3940
730990
 YDOT =      -9692
675298  feet/sec       YDOT =       -2998
422851  meter/sec
 ZDOT =      19281
771017                 ZDOT =        5857
928704

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17137606
72                 X    =         5223542
53
 Y    =       13600421
75  feet           Y    =         4145408
55  meter
 Z    =        4032561
65                 Z    =         1229124
79
 XDOT =     -11668
811882                 XDOT =       -3556
653862
 YDOT =       8968
480635  feet/sec       YDOT =        2733
592897  meter/sec
 ZDOT =      19198
854164                 ZDOT =        5851
810749


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   16159
56189338  
00016717  00000-0  10270-3 0  9114
2 25544  51
6408 106
0482 0001015 155
6402 204
4799 15
54731231  3489


Satellite: ISS
Catalog Number: 25544
Epoch time:      16159
56189338   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:       106
0482  deg
Eccentricity:     
0001015     
Arg of perigee:   155
6402  deg
Mean anomaly:     204
4799  deg
Mean motion:   15
54731231  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             348
Checksum:              297


Coasting Arc #13 (Orbit 362)
---------------------------------------

Vector Time (GMT): 2016/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 924109
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3337260
72                 A    =         6783743
07  meter
 Y    =       -5076702
00  meter          E    =           
0005193
 Z    =       -3018963
91                 I    =           52
01054
 XDOT =       3043
296080                 Wp   =          118
11908
 YDOT =       4961
245354  meter/sec      RA   =          100
48408  deg
 ZDOT =      -4987
583506                 TA   =           96
25803
                                          MA   =           96
19887
                                          Ha   =            220
220  n
mi
                                          Hp   =            213
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10949018
11                 X    =         3408446
42
 Y    =      -16655846
45  feet           Y    =        -5038984
13  meter
 Z    =       -9904737
23                 Z    =        -3002580
11
 XDOT =       9984
567191                 XDOT =        3011
819457
 YDOT =      16277
051685  feet/sec       YDOT =        4995
102139  meter/sec
 ZDOT =     -16363
462947                 ZDOT =       -4972
875818

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13613076
23                 X    =        -4149265
64
 Y    =      -14608571
86  feet           Y    =        -4452692
70  meter
 Z    =       -9832386
38                 Z    =        -2996911
37
 XDOT =      17121
160700                 XDOT =        5218
529781
 YDOT =      -5003
209420  feet/sec       YDOT =       -1524
978231  meter/sec
 ZDOT =     -16300
300799                 ZDOT =       -4968
331683


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   16160
52605253  
00016717  00000-0  10270-3 0  9122
2 25544  51
6412 101
2381 0000908 157
7699 202
3493 15
54738844  3632


Satellite: ISS
Catalog Number: 25544
Epoch time:      16160
52605253   =   yrday
fracday
Element set:     912
Inclination:       51
6412  deg
RA of node:       101
2381  deg
Eccentricity:     
0000908     
Arg of perigee:   157
7699  deg
Mean anomaly:     202
3493  deg
Mean motion:   15
54738844  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             363
Checksum:              298


Coasting Arc #14 (Orbit 363)
---------------------------------------

Vector Time (GMT): 2016/160/13:50:18
153
Vector Time (MET): N/A
Weight (LBS)     : 923904
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3731545
55                 A    =         6777282
89  meter
 Y    =        2247720
82  meter          E    =           
0012884
 Z    =       -5203197
38                 I    =           51
98723
 XDOT =      -2371
124978                 Wp   =          105
04620
 YDOT =       7149
490631  meter/sec      RA   =          100
06905  deg
 ZDOT =       1387
618037                 TA   =          178
25012
                                          MA   =          178
24561
                                          Ha   =            220
201  n
mi
                                          Hp   =            214
854

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12242603
50                 X    =         3731408
44
 Y    =        7374412
14  feet           Y    =         2289449
32  meter
 Z    =      -17070857
55                 Z    =        -5185070
58
 XDOT =      -7779
281423                 XDOT =       -2457
636574
 YDOT =      23456
334092  feet/sec       YDOT =        7122
491248  meter/sec
 ZDOT =       4552
552614                 ZDOT =        1375
890496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4141068
05                 X    =         1262197
54
 Y    =      -13776474
39  feet           Y    =        -4199069
39  meter
 Z    =      -16992285
94                 Z    =        -5179248
76
 XDOT =      23647
768797                 XDOT =        7207
839929
 YDOT =       1556
127373  feet/sec       YDOT =         474
307623  meter/sec
 ZDOT =       4500
102659                 ZDOT =        1371
631291


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   16160
59033051  
00016717  00000-0  10270-3 0  9131
2 25544  51
6426 100
9178 0001462 236
7783 123
3230 15
54367558  3647


Satellite: ISS
Catalog Number: 25544
Epoch time:      16160
59033051   =   yrday
fracday
Element set:     913
Inclination:       51
6426  deg
RA of node:       100
9178  deg
Eccentricity:     
0001462     
Arg of perigee:   236
7783  deg
Mean anomaly:     123
3230  deg
Mean motion:   15
54367558  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             364
Checksum:              292


Coasting Arc #15 (Orbit 371)
---------------------------------------

Vector Time (GMT): 2016/161/01:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 923904
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4232008
88                 A    =         6776977
95  meter
 Y    =         695583
89  meter          E    =           
0003880
 Z    =        5246259
31                 I    =           51
98990
 XDOT =        145
062017                 Wp   =          152
26473
 YDOT =      -7586
603895  meter/sec      RA   =           97
71525  deg
 ZDOT =       1119
224770                 TA   =          287
04113
                                          MA   =          287
08364
                                          Ha   =            220
278  n
mi
                                          Hp   =            214
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13884543
55                 X    =        -4264956
50
 Y    =        2282099
38  feet           Y    =          648073
93  meter
 Z    =       17212136
86                 Z    =         5225621
41
 XDOT =        475
925251                 XDOT =         224
449853
 YDOT =     -24890
432725  feet/sec       YDOT =       -7584
537959  meter/sec
 ZDOT =       3671
997276                 ZDOT =        1120
121397

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3882387
55                 X    =        -1183351
72
 Y    =      -13638479
11  feet           Y    =        -4157008
43  meter
 Z    =       17122065
79                 Z    =         5218805
65
 XDOT =      23781
651700                 XDOT =        7248
647438
 YDOT =      -2137
957882  feet/sec       YDOT =        -651
649563  meter/sec
 ZDOT =       3677
334794                 ZDOT =        1120
851645


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   16161
10466597  
00016717  00000-0  10270-3 0  9145
2 25544  51
6434  98
3498 0001920 227
4374 132
6617 15
54398239  3724


Satellite: ISS
Catalog Number: 25544
Epoch time:      16161
10466597   =   yrday
fracday
Element set:     914
Inclination:       51
6434  deg
RA of node:        98
3498  deg
Eccentricity:     
0001920     
Arg of perigee:   227
4374  deg
Mean anomaly:     132
6617  deg
Mean motion:   15
54398239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             372
Checksum:              323


Coasting Arc #16 (Orbit 386)
---------------------------------------

Vector Time (GMT): 2016/162/01:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 923904
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4075718
27                 A    =         6776885
80  meter
 Y    =        1228831
20  meter          E    =           
0013200
 Z    =       -5284483
75                 I    =           51
99284
 XDOT =      -1078
128246                 Wp   =          102
31427
 YDOT =       7527
137852  meter/sec      RA   =           92
73745  deg
 ZDOT =        918
002472                 TA   =          176
43995
                                          MA   =          176
43055
                                          Ha   =            220
115  n
mi
                                          Hp   =            214
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13371779
11                 X    =         4087343
89
 Y    =        4031598
44  feet           Y    =         1274474
11  meter
 Z    =      -17337545
12                 Z    =        -5264656
66
 XDOT =      -3537
166160                 XDOT =       -1166
677700
 YDOT =      24695
334160  feet/sec       YDOT =        7514
586306  meter/sec
 ZDOT =       3011
819135                 ZDOT =         912
550869

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2209476
11                 X    =         -673448
32
 Y    =       13898103
50  feet           Y    =         4236141
95  meter
 Z    =      -17251367
13                 Z    =        -5258216
70
 XDOT =     -23935
617146                 XDOT =       -7295
576106
 YDOT =        -94
674385  feet/sec       YDOT =         -28
856753  meter/sec
 ZDOT =       2986
630767                 ZDOT =         910
325058


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   16162
06904674  
00016717  00000-0  10270-3 0  9155
2 25544  51
6434  93
5415 0001780 234
2112 125
8875 15
54384173  3878


Satellite: ISS
Catalog Number: 25544
Epoch time:      16162
06904674   =   yrday
fracday
Element set:     915
Inclination:       51
6434  deg
RA of node:        93
5415  deg
Eccentricity:     
0001780     
Arg of perigee:   234
2112  deg
Mean anomaly:     125
8875  deg
Mean motion:   15
54384173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             387
Checksum:              307


Coasting Arc #17 (Orbit 402)
---------------------------------------

Vector Time (GMT): 2016/163/01:18:30
000
Vector Time (MET): N/A
Weight (LBS)     : 923904
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3798577
74                 A    =         6779229
52  meter
 Y    =       -3057900
87  meter          E    =           
0006317
 Z    =        4705683
32                 I    =           52
00144
 XDOT =       1964
900383                 Wp   =           64
70222
 YDOT =      -6843
156614  meter/sec      RA   =           87
76244  deg
 ZDOT =      -2855
159143                 TA   =           53
51266
                                          MA   =           53
45447
                                          Ha   =            220
182  n
mi
                                          Hp   =            214
788

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12462525
40                 X    =        -3786959
32
 Y    =      -10032483
16  feet           Y    =        -3100314
52  meter
 Z    =       15438593
58                 Z    =         4687258
81
 XDOT =       6446
523566                 XDOT =        2055
145327
 YDOT =     -22451
301227  feet/sec       YDOT =       -6820
678965  meter/sec
 ZDOT =      -9367
320022                 ZDOT =       -2845
395549

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8041465
21                 X    =         2451038
60
 Y    =      -13919596
39  feet           Y    =        -4242692
98  meter
 Z    =       15358877
01                 Z    =         4681385
71
 XDOT =      22157
330851                 XDOT =        6753
554443
 YDOT =       2492
563529  feet/sec       YDOT =         759
733364  meter/sec
 ZDOT =      -9323
457420                 ZDOT =       -2841
789822


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   16163
09771581  
00016717  00000-0  10270-3 0  9169
2 25544  51
6434  88
4118 0001720 240
3326 119
7655 15
54401192  4038


Satellite: ISS
Catalog Number: 25544
Epoch time:      16163
09771581   =   yrday
fracday
Element set:     916
Inclination:       51
6434  deg
RA of node:        88
4118  deg
Eccentricity:     
0001720     
Arg of perigee:   240
3326  deg
Mean anomaly:     119
7655  deg
Mean motion:   15
54401192  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             403
Checksum:              291
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