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

 
Date: November 5th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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


311/14:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 215 3

314/21:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 8
000/00:00:00 000 0 0 0 0 215 7

322/07:16:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 216 7

322/20:20:13 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 217 0

Coasting Arc #1 (Orbit 2680)
---------------------------------------

Vector Time (GMT): 2016/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4324630
33                 A    =         6781039
44  meter
 Y    =       -1767269
68  meter          E    =           
0007830
 Z    =        4907684
63                 I    =           51
99115
 XDOT =        278
493946                 Wp   =          120
08394
 YDOT =      -7288
989514  meter/sec      RA   =           77
41209  deg
 ZDOT =      -2380
371959                 TA   =          353
09793
                                          MA   =          353
10870
                                          Ha   =            223
811  n
mi
                                          Hp   =            214
789

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14188419
73                 X    =        -4328386
78
 Y    =       -5798128
88  feet           Y    =        -1815651
60  meter
 Z    =       16101327
51                 Z    =         4886667
08
 XDOT =        913
694050                 XDOT =         371
543661
 YDOT =     -23914
007593  feet/sec       YDOT =       -7285
354937  meter/sec
 ZDOT =      -7809
619289                 ZDOT =       -2378
793063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14376460
94                 X    =         4381945
29
 Y    =       -5585032
68  feet           Y    =        -1702317
96  meter
 Z    =       16009593
42                 Z    =         4879724
07
 XDOT =      15294
228233                 XDOT =        4661
680765
 YDOT =      17015
605145  feet/sec       YDOT =        5186
356448  meter/sec
 ZDOT =      -7801
371040                 ZDOT =       -2377
857893


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   16309
54410407  
00016717  00000-0  10270-3 0  9001
2 25544  51
6414  78
0075 0007508 173
2436 186
8819 15
53500653 26817


Satellite: ISS
Catalog Number: 25544
Epoch time:      16309
54410407   =   yrday
fracday
Element set:     900
Inclination:       51
6414  deg
RA of node:        78
0075  deg
Eccentricity:     
0007508     
Arg of perigee:   173
2436  deg
Mean anomaly:     186
8819  deg
Mean motion:   15
53500653  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2681
Checksum:              302


Coasting Arc #2 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2016/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4377620
13                 A    =         6783985
44  meter
 Y    =        3157909
93  meter          E    =           
0012164
 Z    =       -4122532
67                 I    =           51
99314
 XDOT =      -1086
400181                 Wp   =          143
44595
 YDOT =       6530
744895  meter/sec      RA   =           72
45052  deg
 ZDOT =       3845
335210                 TA   =          166
17080
                                          MA   =          166
13745
                                          Ha   =            223
456  n
mi
                                          Hp   =            215
095

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14362270
76                 X    =         4362008
07
 Y    =       10360596
87  feet           Y    =         3206776
13  meter
 Z    =      -13525369
66                 Z    =        -4101304
81
 XDOT =      -3564
305055                 XDOT =       -1178
027221
 YDOT =      21426
328397  feet/sec       YDOT =        6518
083718  meter/sec
 ZDOT =      12615
929168                 ZDOT =        3839
835105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17576981
49                 X    =        -5357463
96
 Y    =        2675332
11  feet           Y    =          815441
23  meter
 Z    =      -13432971
86                 Z    =        -4094369
82
 XDOT =     -12158
393857                 XDOT =       -3705
878448
 YDOT =     -16601
805728  feet/sec       YDOT =       -5060
230386  meter/sec
 ZDOT =      12590
630761                 ZDOT =        3837
624256


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   16310
50900158  
00016717  00000-0  10270-3 0  9017
2 25544  51
6413  73
2028 0007427 178
0373 182
0809 15
53529892 26963


Satellite: ISS
Catalog Number: 25544
Epoch time:      16310
50900158   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:        73
2028  deg
Eccentricity:     
0007427     
Arg of perigee:   178
0373  deg
Mean anomaly:     182
0809  deg
Mean motion:   15
53529892  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2696
Checksum:              304


Coasting Arc #3 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2016/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4303904
22                 A    =         6787364
27  meter
 Y    =       -4304443
22  meter          E    =           
0015886
 Z    =        2979853
84                 I    =           51
99432
 XDOT =       1980
963652                 Wp   =          125
50595
 YDOT =      -5460
169450  meter/sec      RA   =           67
49535  deg
 ZDOT =      -5016
391725                 TA   =           20
57577
                                          MA   =           20
51186
                                          Ha   =            223
484  n
mi
                                          Hp   =            215
106

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14120420
67                 X    =        -4269926
03
 Y    =      -14122189
05  feet           Y    =        -4352382
37  meter
 Z    =        9776423
37                 Z    =         2959028
77
 XDOT =       6499
224580                 XDOT =        2066
241287
 YDOT =     -17913
941765  feet/sec       YDOT =       -5437
540187  meter/sec
 ZDOT =     -16457
978100                 ZDOT =       -5006
561396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20014053
35                 X    =         6100283
46
 Y    =        -141037
61  feet           Y    =          -42988
26  meter
 Z    =        9686007
15                 Z    =         2952294
98
 XDOT =       8070
898968                 XDOT =        2460
010005
 YDOT =      15840
628220  feet/sec       YDOT =        4828
223481  meter/sec
 ZDOT =     -16413
900017                 ZDOT =       -5002
956725


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   16311
53822078  
00016717  00000-0  10270-3 0  9026
2 25544  51
6418  68
0767 0007507 181
5222 178
5909 15
53532977 27129


Satellite: ISS
Catalog Number: 25544
Epoch time:      16311
53822078   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:        68
0767  deg
Eccentricity:     
0007507     
Arg of perigee:   181
5222  deg
Mean anomaly:     178
5909  deg
Mean motion:   15
53532977  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              319


Coasting Arc #4 (Orbit 2712)
---------------------------------------

Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3939554
07                 A    =         6779067
19  meter
 Y    =       -1417298
17  meter          E    =           
0016383
 Z    =       -5344375
41                 I    =           51
96650
 XDOT =       2836
276076                 Wp   =          117
90584
 YDOT =       7109
292618  meter/sec      RA   =           67
08852  deg
 ZDOT =        198
398264                 TA   =          154
02056
                                          MA   =          153
93823
                                          Ha   =            223
278  n
mi
                                          Hp   =            215
310

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12925046
16                 X    =         3981070
94
 Y    =       -4649928
38  feet           Y    =        -1373011
32  meter
 Z    =      -17534040
05                 Z    =        -5325136
90
 XDOT =       9305
367705                 XDOT =        2755
603601
 YDOT =      23324
450847  feet/sec       YDOT =        7140
558695  meter/sec
 ZDOT =        650
912940                 ZDOT =         211
980421

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1506497
41                 X    =          459180
41
 Y    =       13761047
54  feet           Y    =         4194367
29  meter
 Z    =      -17449505
69                 Z    =        -5318609
33
 XDOT =     -23840
672850                 XDOT =       -7266
637085
 YDOT =       3538
330968  feet/sec       YDOT =        1078
483279  meter/sec
 ZDOT =        709
079175                 ZDOT =         216
127332


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   16311
60254524  
00016717  00000-0  10270-3 0  9030
2 25544  51
6425  67
7581 0007283 183
1004 177
0104 15
53546897 27132


Satellite: ISS
Catalog Number: 25544
Epoch time:      16311
60254524   =   yrday
fracday
Element set:     903
Inclination:       51
6425  deg
RA of node:        67
7581  deg
Eccentricity:     
0007283     
Arg of perigee:   183
1004  deg
Mean anomaly:     177
0104  deg
Mean motion:   15
53546897  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2713
Checksum:              296


Coasting Arc #5 (Orbit 2728)
---------------------------------------

Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4499236
32                 A    =         6780086
05  meter
 Y    =         -24836
19  meter          E    =           
0005474
 Z    =        5067638
39                 I    =           51
95775
 XDOT =      -2094
217509                 Wp   =          135
21609
 YDOT =      -7131
876227  meter/sec      RA   =           62
11738  deg
 ZDOT =      -1896
818636                 TA   =          333
06803
                                          MA   =          333
09643
                                          Ha   =            223
148  n
mi
                                          Hp   =            215
291

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14761274
00                 X    =        -4523240
95
 Y    =         -81483
57  feet           Y    =          -75283
82  meter
 Z    =       16626110
21                 Z    =         5045723
62
 XDOT =      -6870
792354                 XDOT =       -2005
097341
 YDOT =     -23398
544051  feet/sec       YDOT =       -7154
796900  meter/sec
 ZDOT =      -6223
158254                 ZDOT =       -1906
775394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3271182
84                 X    =          997056
53
 Y    =      -14504614
10  feet           Y    =        -4421006
38  meter
 Z    =       16530121
69                 Z    =         5038381
09
 XDOT =      23262
307898                 XDOT =        7090
351447
 YDOT =      -1884
530210  feet/sec       YDOT =        -574
404808  meter/sec
 ZDOT =      -6265
429707                 ZDOT =       -1909
702975


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   16312
63175443  
00016717  00000-0  10270-3 0  9047
2 25544  51
6433  62
6318 0007138 187
0035 173
1018 15
53600047 27295


Satellite: ISS
Catalog Number: 25544
Epoch time:      16312
63175443   =   yrday
fracday
Element set:     904
Inclination:       51
6433  deg
RA of node:        62
6318  deg
Eccentricity:     
0007138     
Arg of perigee:   187
0035  deg
Mean anomaly:     173
1018  deg
Mean motion:   15
53600047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2729
Checksum:              286


Coasting Arc #6 (Orbit 2743)
---------------------------------------

Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4990881
20                 A    =         6782848
04  meter
 Y    =        1399445
04  meter          E    =           
0012314
 Z    =       -4387059
46                 I    =           51
94972
 XDOT =       1142
747556                 Wp   =          144
75056
 YDOT =       6741
783739  meter/sec      RA   =           57
15089  deg
 ZDOT =       3445
651823                 TA   =          160
12475
                                          MA   =          160
07674
                                          Ha   =            222
941  n
mi
                                          Hp   =            215
528

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16374282
17                 X    =         4996172
06
 Y    =        4591355
13  feet           Y    =         1455285
89  meter
 Z    =      -14393239
71                 Z    =        -4362801
86
 XDOT =       3749
171772                 XDOT =        1050
536548
 YDOT =      22118
713055  feet/sec       YDOT =        6754
047223  meter/sec
 ZDOT =      11304
631966                 ZDOT =        3450
978923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7758434
52                 X    =        -2364770
84
 Y    =       15232996
28  feet           Y    =         4643017
26  meter
 Z    =      -14287250
47                 Z    =        -4354753
94
 XDOT =     -21298
884467                 XDOT =       -6491
899986
 YDOT =       -209
031946  feet/sec       YDOT =         -63
712937  meter/sec
 ZDOT =      11326
688264                 ZDOT =        3452
374583


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   16313
59663339  
00016717  00000-0  10270-3 0  9050
2 25544  51
6420  57
8269 0007123 188
9530 171
1496 15
53600964 27449


Satellite: ISS
Catalog Number: 25544
Epoch time:      16313
59663339   =   yrday
fracday
Element set:     905
Inclination:       51
6420  deg
RA of node:        57
8269  deg
Eccentricity:     
0007123     
Arg of perigee:   188
9530  deg
Mean anomaly:     171
1496  deg
Mean motion:   15
53600964  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2744
Checksum:              323


Coasting Arc #7 (Orbit 2759)
---------------------------------------

Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5306624
40                 A    =         6786236
59  meter
 Y    =       -2589961
66  meter          E    =           
0013158
 Z    =        3327132
63                 I    =           51
94318
 XDOT =        -13
194860                 Wp   =          123
17257
 YDOT =      -6048
115843  meter/sec      RA   =           52
19036  deg
 ZDOT =      -4722
683013                 TA   =           18
26026
                                          MA   =           18
21306
                                          Ha   =            222
867  n
mi
                                          Hp   =            215
605

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17410185
04                 X    =        -5293430
41
 Y    =       -8497249
54  feet           Y    =        -2649229
99  meter
 Z    =       10915789
47                 Z    =         3301386
13
 XDOT =        -43
290224                 XDOT =          77
378814
 YDOT =     -19842
899748  feet/sec       YDOT =       -6047
757161  meter/sec
 ZDOT =     -15494
366841                 ZDOT =       -4722
526871

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11520375
15                 X    =         3511410
35
 Y    =      -15653669
55  feet           Y    =        -4771238
48  meter
 Z    =       10803510
47                 Z    =         3292909
99
 XDOT =      18364
606511                 XDOT =        5597
532064
 YDOT =       2808
475315  feet/sec       YDOT =         856
023276  meter/sec
 ZDOT =     -15492
528773                 ZDOT =       -4722
122770


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   16314
62582924  
00016717  00000-0  10270-3 0  9066
2 25544  51
6424  52
7008 0007008 193
8421 166
2540 15
53609727 27603


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
62582924   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:        52
7008  deg
Eccentricity:     
0007008     
Arg of perigee:   193
8421  deg
Mean anomaly:     166
2540  deg
Mean motion:   15
53609727  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2760
Checksum:              303


Coasting Arc #8 (Orbit 2764)
---------------------------------------

Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5354536
73                 A    =         6787724
43  meter
 Y    =       -3094679
63  meter          E    =           
0014687
 Z    =        2774664
59                 I    =           51
94009
 XDOT =        586
508643                 Wp   =          127
73047
 YDOT =      -5649
707295  meter/sec      RA   =           50
59148  deg
 ZDOT =      -5159
643386                 TA   =           20
94513
                                          MA   =           20
88503
                                          Ha   =            222
776  n
mi
                                          Hp   =            215
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17567377
73                 X    =        -5333011
61
 Y    =      -10153148
39  feet           Y    =        -3154437
18  meter
 Z    =        9103230
30                 Z    =         2748705
59
 XDOT =       1924
240954                 XDOT =         674
705258
 YDOT =     -18535
785089  feet/sec       YDOT =       -5642
655651  meter/sec
 ZDOT =     -16927
963865                 ZDOT =       -5156
579758

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19753356
68                 X    =        -6020823
12
 Y    =       -4852899
65  feet           Y    =        -1479163
81  meter
 Z    =        8990119
51                 Z    =         2740188
43
 XDOT =      -3552
801604                 XDOT =       -1082
893929
 YDOT =     -16931
704716  feet/sec       YDOT =       -5160
783597  meter/sec
 ZDOT =     -16913
464369                 ZDOT =       -5155
223940


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   16314
94745319  
00016717  00000-0  10270-3 0  9071
2 25544  51
6409  51
0997 0006683 194
4433 165
6529 15
53585690 27650


Satellite: ISS
Catalog Number: 25544
Epoch time:      16314
94745319   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:        51
0997  deg
Eccentricity:     
0006683     
Arg of perigee:   194
4433  deg
Mean anomaly:     165
6529  deg
Mean motion:   15
53585690  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2765
Checksum:              345


Coasting Arc #9 (Orbit 2779)
---------------------------------------

Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5354308
03                 A    =         6790117
33  meter
 Y    =        3946838
20  meter          E    =           
0003392
 Z    =       -1364182
61                 I    =           51
92736
 XDOT =      -1901
045520                 Wp   =           77
88578
 YDOT =       4590
376791  meter/sec      RA   =           45
63975  deg
 ZDOT =       5832
296351                 TA   =          267
32856
                                          MA   =          267
36738
                                          Ha   =            222
503  n
mi
                                          Hp   =            215
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17566627
39                 X    =         5316402
27
 Y    =       12948944
21  feet           Y    =         4006501
65  meter
 Z    =       -4475664
73                 Z    =        -1338264
48
 XDOT =      -6237
025984                 XDOT =       -1980
566337
 YDOT =      15060
291310  feet/sec       YDOT =        4568
673684  meter/sec
 ZDOT =      19134
830549                 ZDOT =        5822
867991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20627865
29                 X    =         6287373
34
 Y    =        7193701
90  feet           Y    =         2192640
34  meter
 Z    =       -4362906
78                 Z    =        -1329813
99
 XDOT =      -1119
408885                 XDOT =        -341
195828
 YDOT =      14763
017369  feet/sec       YDOT =        4499
767694  meter/sec
 ZDOT =      19092
650942                 ZDOT =        5819
440007


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   16315
91231333  
00016717  00000-0  10270-3 0  9086
2 25544  51
6412  46
2938 0006597 198
2010 161
8908 15
53597528 27801


Satellite: ISS
Catalog Number: 25544
Epoch time:      16315
91231333   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:        46
2938  deg
Eccentricity:     
0006597     
Arg of perigee:   198
2010  deg
Mean anomaly:     161
8908  deg
Mean motion:   15
53597528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2780
Checksum:              321


Coasting Arc #10 (Orbit 2795)
---------------------------------------

Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5042727
30                 A    =         6790838
70  meter
 Y    =       -4529875
81  meter          E    =           
0015552
 Z    =        -187465
19                 I    =           51
90716
 XDOT =       3284
954830                 Wp   =          158
50724
 YDOT =      -3414
238380  meter/sec      RA   =           40
69109  deg
 ZDOT =      -6034
614289                 TA   =           23
50578
                                          MA   =           23
43478
                                          Ha   =            222
360  n
mi
                                          Hp   =            216
011

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16544380
90                 X    =        -4990787
63
 Y    =      -14861797
29  feet           Y    =        -4585976
57  meter
 Z    =        -615043
28                 Z    =         -211835
71
 XDOT =      10777
410858                 XDOT =        3352
203821
 YDOT =     -11201
569488  feet/sec       YDOT =       -3377
128066  meter/sec
 ZDOT =     -19798
603311                 ZDOT =       -6018
492929

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20340346
53                 X    =        -6199737
62
 Y    =       -8984344
52  feet           Y    =        -2738428
21  meter
 Z    =        -720897
41                 Z    =         -219729
53
 XDOT =       6227
661156                 XDOT =        1898
191120
 YDOT =     -12554
979857  feet/sec       YDOT =       -3826
757861  meter/sec
 ZDOT =     -19727
333984                 ZDOT =       -6012
891398


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   16316
94148967  
00016717  00000-0  10270-3 0  9091
2 25544  51
6417  41
1677 0006546 202
0491 158
0381 15
53603854 27961


Satellite: ISS
Catalog Number: 25544
Epoch time:      16316
94148967   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:        41
1677  deg
Eccentricity:     
0006546     
Arg of perigee:   202
0491  deg
Mean anomaly:     158
0381  deg
Mean motion:   15
53603854  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2796
Checksum:              326


Coasting Arc #11 (Orbit 2811)
---------------------------------------

Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4442717
42                 A    =         6789516
65  meter
 Y    =        4841298
57  meter          E    =           
0009696
 Z    =        1700600
72                 I    =           51
87805
 XDOT =      -4605
844265                 Wp   =           89
29573
 YDOT =       2209
670905  meter/sec      RA   =           35
74040  deg
 ZDOT =       5713
973905                 TA   =          289
27584
                                          MA   =          289
38070
                                          Ha   =            222
177  n
mi
                                          Hp   =            216
132

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14575844
54                 X    =         4379989
57
 Y    =       15883525
50  feet           Y    =         4890629
34  meter
 Z    =        5579398
70                 Z    =         1722030
42
 XDOT =     -15111
037616                 XDOT =       -4657
967832
 YDOT =       7249
576461  feet/sec       YDOT =        2157
873983  meter/sec
 ZDOT =      18746
633547                 ZDOT =        5691
472590

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18935698
15                 X    =         5771600
80
 Y    =       10253569
17  feet           Y    =         3125287
88  meter
 Z    =        5672298
56                 Z    =         1728916
60
 XDOT =     -11274
152843                 XDOT =       -3436
361787
 YDOT =      10454
556171  feet/sec       YDOT =        3186
548721  meter/sec
 ZDOT =      18647
657470                 ZDOT =        5683
805997


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   16317
97065708  
00016717  00000-0  10270-3 0  9108
2 25544  51
6418  36
0421 0006580 206
4533 153
6284 15
53628851 28121


Satellite: ISS
Catalog Number: 25544
Epoch time:      16317
97065708   =   yrday
fracday
Element set:     910
Inclination:       51
6418  deg
RA of node:        36
0421  deg
Eccentricity:     
0006580     
Arg of perigee:   206
4533  deg
Mean anomaly:     153
6284  deg
Mean motion:   15
53628851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2812
Checksum:              303


Coasting Arc #12 (Orbit 2826)
---------------------------------------

Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3497381
22                 A    =         6786581
87  meter
 Y    =       -4917336
92  meter          E    =           
0006765
 Z    =       -3098746
67                 I    =           51
84309
 XDOT =       5798
189234                 Wp   =          169
88633
 YDOT =      -1035
513262  meter/sec      RA   =           30
78220  deg
 ZDOT =      -4908
968429                 TA   =           45
63120
                                          MA   =           45
57580
                                          Ha   =            221
929  n
mi
                                          Hp   =            216
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11474347
82                 X    =        -3427081
55
 Y    =      -16132995
15  feet           Y    =        -4956053
93  meter
 Z    =      -10166491
70                 Z    =        -3115565
79
 XDOT =      19022
930558                 XDOT =        5833
184014
 YDOT =      -3397
353223  feet/sec       YDOT =        -970
478365  meter/sec
 ZDOT =     -16105
539466                 ZDOT =       -4880
716459

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16254259
76                 X    =        -4954298
38
 Y    =      -11236108
72  feet           Y    =        -3424765
94  meter
 Z    =      -10239172
06                 Z    =        -3120899
64
 XDOT =      15977
812750                 XDOT =        4870
037326
 YDOT =      -8574
110017  feet/sec       YDOT =       -2613
388733  meter/sec
 ZDOT =     -15981
612587                 ZDOT =       -4871
195516


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   16318
93549267  
00016717  00000-0  10270-3 0  9113
2 25544  51
6431  31
2362 0006426 210
3776 149
7004 15
53652460 28274


Satellite: ISS
Catalog Number: 25544
Epoch time:      16318
93549267   =   yrday
fracday
Element set:     911
Inclination:       51
6431  deg
RA of node:        31
2362  deg
Eccentricity:     
0006426     
Arg of perigee:   210
3776  deg
Mean anomaly:     149
7004  deg
Mean motion:   15
53652460  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2827
Checksum:              301


Coasting Arc #13 (Orbit 2842)
---------------------------------------

Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2301665
49                 A    =         6783139
05  meter
 Y    =        4793951
44  meter          E    =           
0010187
 Z    =        4210847
12                 I    =           51
80289
 XDOT =      -6719
443699                 Wp   =          142
16992
 YDOT =        -25
605293  meter/sec      RA   =           25
81463  deg
 ZDOT =       3689
445246                 TA   =          270
00734
                                          MA   =          270
12408
                                          Ha   =            221
811  n
mi
                                          Hp   =            216
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7551395
95                 X    =         2227432
18
 Y    =       15728187
14  feet           Y    =         4819275
04  meter
 Z    =       13815115
22                 Z    =         4221848
15
 XDOT =     -22045
418959                 XDOT =       -6736
580198
 YDOT =        -84
006866  feet/sec       YDOT =        -100
842529  meter/sec
 ZDOT =      12104
479154                 ZDOT =        3656
761339

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12616995
83                 X    =         3845660
33
 Y    =       11996001
97  feet           Y    =         3656381
40  meter
 Z    =       13862330
72                 Z    =         4225238
40
 XDOT =     -19799
781263                 XDOT =       -6034
973329
 YDOT =       6954
922435  feet/sec       YDOT =        2119
860358  meter/sec
 ZDOT =      11961
358349                 ZDOT =        3645
822025


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   16319
96464192  
00016717  00000-0  10270-3 0  9121
2 25544  51
6425  26
1104 0006407 213
6692 146
4054 15
53656832 28430


Satellite: ISS
Catalog Number: 25544
Epoch time:      16319
96464192   =   yrday
fracday
Element set:     912
Inclination:       51
6425  deg
RA of node:        26
1104  deg
Eccentricity:     
0006407     
Arg of perigee:   213
6692  deg
Mean anomaly:     146
4054  deg
Mean motion:   15
53656832  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2843
Checksum:              305


Coasting Arc #14 (Orbit 2857)
---------------------------------------

Vector Time (GMT): 2016/320/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -854122
08                 A    =         6780086
69  meter
 Y    =       -4525658
39  meter          E    =           
0008457
 Z    =       -4982427
71                 I    =           51
76383
 XDOT =       7292
904971                 Wp   =          100
97070
 YDOT =        972
731208  meter/sec      RA   =           20
83613  deg
 ZDOT =      -2138
402897                 TA   =          148
24161
                                          MA   =          148
19057
                                          Ha   =            221
632  n
mi
                                          Hp   =            216
521

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2802237
80                 X    =         -779248
47
 Y    =      -14847960
60  feet           Y    =        -4534790
88  meter
 Z    =      -16346547
61                 Z    =        -4986395
27
 XDOT =      23926
853578                 XDOT =        7291
873300
 YDOT =       3191
375354  feet/sec       YDOT =        1054
279696  meter/sec
 ZDOT =      -7015
757536                 ZDOT =       -2102
977404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8074242
91                 X    =        -2461029
24
 Y    =      -12750789
40  feet           Y    =        -3886440
61  meter
 Z    =      -16363008
90                 Z    =        -4987445
11
 XDOT =      22486
256432                 XDOT =        6853
810960
 YDOT =      -5454
174409  feet/sec       YDOT =       -1662
432360  meter/sec
 ZDOT =      -6860
824536                 ZDOT =       -2091
179319


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   16320
92946213  
00016717  00000-0  10270-3 0  9139
2 25544  51
6429  21
3046 0006338 217
6506 142
4204 15
53684975 28585


Satellite: ISS
Catalog Number: 25544
Epoch time:      16320
92946213   =   yrday
fracday
Element set:     913
Inclination:       51
6429  deg
RA of node:        21
3046  deg
Eccentricity:     
0006338     
Arg of perigee:   217
6506  deg
Mean anomaly:     142
4204  deg
Mean motion:   15
53684975  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2858
Checksum:              308


Coasting Arc #15 (Orbit 2873)
---------------------------------------

Vector Time (GMT): 2016/321/21:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -690761
34                 A    =         6778597
14  meter
 Y    =        4158821
83  meter          E    =           
0005845
 Z    =        5310084
57                 I    =           51
72852
 XDOT =      -7446
993524                 Wp   =          198
55671
 YDOT =      -1773
808660  meter/sec      RA   =           15
85017  deg
 ZDOT =        415
208281                 TA   =          247
45673
                                          MA   =          247
51860
                                          Ha   =            221
419  n
mi
                                          Hp   =            216
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2266277
35                 X    =         -763009
59
 Y    =       13644428
56  feet           Y    =         4150693
01  meter
 Z    =       17421537
32                 Z    =         5306553
71
 XDOT =     -24432
393453                 XDOT =       -7428
621802
 YDOT =      -5819
582217  feet/sec       YDOT =       -1856
983241  meter/sec
 ZDOT =       1362
231894                 ZDOT =         379
076500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3150823
88                 X    =          960371
12
 Y    =       13488758
62  feet           Y    =         4111373
63  meter
 Z    =       17405232
15                 Z    =         5305114
76
 XDOT =     -23785
247406                 XDOT =       -7249
743409
 YDOT =       3979
510010  feet/sec       YDOT =        1212
954651  meter/sec
 ZDOT =       1204
370918                 ZDOT =         367
092256


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   16321
95859380  
00016717  00000-0  10270-3 0  9142
2 25544  51
6428  16
1785 0006502 222
7791 137
2856 15
53715306 28748


Satellite: ISS
Catalog Number: 25544
Epoch time:      16321
95859380   =   yrday
fracday
Element set:     914
Inclination:       51
6428  deg
RA of node:        16
1785  deg
Eccentricity:     
0006502     
Arg of perigee:   222
7791  deg
Mean anomaly:     137
2856  deg
Mean motion:   15
53715306  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2874
Checksum:              324


Coasting Arc #16 (Orbit 2879)
---------------------------------------

Vector Time (GMT): 2016/322/07:16:00
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4681313
42                 A    =         6782926
72  meter
 Y    =        2344252
96  meter          E    =           
0005643
 Z    =        4306637
36                 I    =           51
72965
 XDOT =      -5357
453441                 Wp   =          113
86538
 YDOT =      -4196
738288  meter/sec      RA   =           13
86220  deg
 ZDOT =      -3537
689449                 TA   =           12
12011
                                          MA   =           12
10654
                                          Ha   =            221
784  n
mi
                                          Hp   =            216
721

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15358639
82                 X    =        -4728099
66
 Y    =        7691118
62  feet           Y    =         2291641
53  meter
 Z    =       14129387
67                 Z    =         4283782
83
 XDOT =     -17576
946986                 XDOT =       -5292
941407
 YDOT =     -13768
826404  feet/sec       YDOT =       -4256
288020  meter/sec
 ZDOT =     -11606
592681                 ZDOT =       -3563
558591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16918861
87                 X    =         5156869
10
 Y    =       -3409502
36  feet           Y    =        -1039216
32  meter
 Z    =       14028831
94                 Z    =         4275987
98
 XDOT =      13069
200110                 XDOT =        3983
492194
 YDOT =      16614
022738  feet/sec       YDOT =        5063
954131  meter/sec
 ZDOT =     -11719
020451                 ZDOT =       -3571
957433


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   16322
34451780  
00016717  00000-0  10270-3 0  9159
2 25544  51
6424  14
2509 0006769 219
8683 140
1973 15
53662085 28804


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
34451780   =   yrday
fracday
Element set:     915
Inclination:       51
6424  deg
RA of node:        14
2509  deg
Eccentricity:     
0006769     
Arg of perigee:   219
8683  deg
Mean anomaly:     140
1973  deg
Mean motion:   15
53662085  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2880
Checksum:              317


Coasting Arc #17 (Orbit 2887)
---------------------------------------

Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3463775
23                 A    =         6780679
12  meter
 Y    =       -3229431
34  meter          E    =           
0010320
 Z    =       -4861698
89                 I    =           51
70504
 XDOT =       6485
469234                 Wp   =          139
90282
 YDOT =       3254
619285  meter/sec      RA   =           11
16139  deg
 ZDOT =       2453
931545                 TA   =          154
21382
                                          MA   =          154
16234
                                          Ha   =            221
309  n
mi
                                          Hp   =            216
956

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11364091
95                 X    =         3523246
48
 Y    =      -10595247
18  feet           Y    =        -3190364
29  meter
 Z    =      -15950455
69                 Z    =        -4844728
23
 XDOT =      21277
786201                 XDOT =        6436
672926
 YDOT =      10677
884793  feet/sec       YDOT =        3326
871186  meter/sec
 ZDOT =       8050
956511                 ZDOT =        2485
318422

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11182846
44                 X    =         3408531
59
 Y    =      -10896412
67  feet           Y    =        -3321226
58  meter
 Z    =      -15875484
93                 Z    =        -4838847
81
 XDOT =      20705
694896                 XDOT =        6311
095804
 YDOT =       9297
817914  feet/sec       YDOT =        2833
974900  meter/sec
 ZDOT =       8187
736066                 ZDOT =        2495
621953


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   16322
85907865  
00016717  00000-0  10270-3 0  9166
2 25544  51
6421  11
6914 0006280 225
6836 134
3802 15
53696732 28885


Satellite: ISS
Catalog Number: 25544
Epoch time:      16322
85907865   =   yrday
fracday
Element set:     916
Inclination:       51
6421  deg
RA of node:        11
6914  deg
Eccentricity:     
0006280     
Arg of perigee:   225
6836  deg
Mean anomaly:     134
3802  deg
Mean motion:   15
53696732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2888
Checksum:              325


Coasting Arc #18 (Orbit 2903)
---------------------------------------

Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS)     : 893835
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4771938
83                 A    =         6783877
89  meter
 Y    =        2669573
81  meter          E    =           
0006327
 Z    =        4008641
23                 I    =           51
68363
 XDOT =      -5411
014729                 Wp   =          108
54674
 YDOT =      -3729
177648  meter/sec      RA   =            6
17903  deg
 ZDOT =      -3954
732963                 TA   =           22
55245
                                          MA   =           22
52466
                                          Ha   =            221
240  n
mi
                                          Hp   =            217
017

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15655967
30                 X    =        -4820908
47
 Y    =        8758444
27  feet           Y    =         2615936
81  meter
 Z    =       13151710
06                 Z    =         3985341
28
 XDOT =     -17752
672997                 XDOT =       -5349
701371
 YDOT =     -12234
834803  feet/sec       YDOT =       -3789
344255  meter/sec
 ZDOT =     -12974
845678                 ZDOT =       -3980
869817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15343524
26                 X    =        -4676706
20
 Y    =        9438398
90  feet           Y    =         2876823
99  meter
 Z    =       13049138
85                 Z    =         3977377
52
 XDOT =     -17497
205886                 XDOT =       -5333
148354
 YDOT =     -10334
266854  feet/sec       YDOT =       -3149
884537  meter/sec
 ZDOT =     -13088
536434                 ZDOT =       -3989
385905


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   16323
88819752  
00016717  00000-0  10270-3 0  9178
2 25544  51
6418   6
5657 0006286 229
5801 130
4804 15
53695207 29043


Satellite: ISS
Catalog Number: 25544
Epoch time:      16323
88819752   =   yrday
fracday
Element set:     917
Inclination:       51
6418  deg
RA of node:         6
5657  deg
Eccentricity:     
0006286     
Arg of perigee:   229
5801  deg
Mean anomaly:     130
4804  deg
Mean motion:   15
53695207  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2904
Checksum:              325
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