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

 
Date: December 11th 2015

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


There are no maneuvers



Coasting Arc #1 (Orbit 1563)
---------------------------------------

Vector Time (GMT): 2015/345/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3890752
37                 A    =         6780416
80  meter
 Y    =       -3698474
38  meter          E    =           
0003505
 Z    =        4142472
60                 I    =           51
27587
 XDOT =       2091
786466                 Wp   =          146
35836
 YDOT =       6370
319127  meter/sec      RA   =          278
22518  deg
 ZDOT =       3718
475479                 TA   =          265
18456
                                          MA   =          265
22458
                                          Ha   =            217
663  n
mi
                                          Hp   =            217
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12764935
58                 X    =         3911697
70
 Y    =      -12134102
30  feet           Y    =        -3654848
71  meter
 Z    =       13590789
38                 Z    =         4161423
79
 XDOT =       6862
816491                 XDOT =        2002
333427
 YDOT =      20899
997136  feet/sec       YDOT =        6393
210338  meter/sec
 ZDOT =      12199
722700                 ZDOT =        3728
420404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12518413
67                 X    =         3815612
49
 Y    =       12297039
54  feet           Y    =         3748137
65  meter
 Z    =       13673394
33                 Z    =         4167650
59
 XDOT =     -19785
025126                 XDOT =       -6030
475658
 YDOT =       6513
750802  feet/sec       YDOT =        1985
391245  meter/sec
 ZDOT =      12241
426139                 ZDOT =        3731
186687


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   15345
59032597  
00016717  00000-0  10270-3 0  9005
2 25544  51
6429 278
7244 0008049 267
9201  92
1030 15
54659985 15649


Satellite: ISS
Catalog Number: 25544
Epoch time:      15345
59032597   =   yrday
fracday
Element set:     900
Inclination:       51
6429  deg
RA of node:       278
7244  deg
Eccentricity:     
0008049     
Arg of perigee:   267
9201  deg
Mean anomaly:      92
1030  deg
Mean motion:   15
54659985  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1564
Checksum:              328


Coasting Arc #2 (Orbit 1578)
---------------------------------------

Vector Time (GMT): 2015/346/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4148250
71                 A    =         6776798
73  meter
 Y    =        1851981
25  meter          E    =           
0005840
 Z    =       -5033716
52                 I    =           51
26109
 XDOT =      -1061
456055                 Wp   =           54
46628
 YDOT =      -7366
414233  meter/sec      RA   =          273
20054  deg
 ZDOT =      -1833
647342                 TA   =          197
66355
                                          MA   =          197
68386
                                          Ha   =            217
340  n
mi
                                          Hp   =            216
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13609746
43                 X    =        -4144199
71
 Y    =        6076053
96  feet           Y    =         1805615
92  meter
 Z    =      -16514817
96                 Z    =        -5053857
97
 XDOT =      -3482
467371                 XDOT =        -970
096909
 YDOT =     -24168
025700  feet/sec       YDOT =       -7377
773132  meter/sec
 ZDOT =      -6015
903352                 ZDOT =       -1838
582547

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6716462
06                 X    =        -2047177
64
 Y    =      -13196167
87  feet           Y    =        -4022191
97  meter
 Z    =      -16602202
66                 Z    =        -5060351
37
 XDOT =      23012
873309                 XDOT =        7014
323785
 YDOT =      -4111
699069  feet/sec       YDOT =       -1253
245876  meter/sec
 ZDOT =      -6035
779695                 ZDOT =       -1839
705651


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   15346
55451882  
00016717  00000-0  10270-3 0  9015
2 25544  51
6435 273
9138 0007998 271
9945  88
0292 15
54703313 15792


Satellite: ISS
Catalog Number: 25544
Epoch time:      15346
55451882   =   yrday
fracday
Element set:     901
Inclination:       51
6435  deg
RA of node:       273
9138  deg
Eccentricity:     
0007998     
Arg of perigee:   271
9945  deg
Mean anomaly:      88
0292  deg
Mean motion:   15
54703313  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1579
Checksum:              341


Coasting Arc #3 (Orbit 1594)
---------------------------------------

Vector Time (GMT): 2015/347/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4246217
42                 A    =         6775574
14  meter
 Y    =         198856
38  meter          E    =           
0005849
 Z    =        5281221
54                 I    =           51
25618
 XDOT =          8
655024                 Wp   =          283
42259
 YDOT =       7659
944599  meter/sec      RA   =          268
16847  deg
 ZDOT =       -294
323574                 TA   =          169
40527
                                          MA   =          169
39294
                                          Ha   =            218
026  n
mi
                                          Hp   =            217
423

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13931159
53                 X    =         4218023
98
 Y    =         652415
94  feet           Y    =          246182
24  meter
 Z    =       17326842
32                 Z    =         5301780
38
 XDOT =         28
395749                 XDOT =         -75
571283
 YDOT =      25131
051833  feet/sec       YDOT =        7659
570476  meter/sec
 ZDOT =       -965
628524                 ZDOT =        -294
485370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         248872
99                 X    =           75856
49
 Y    =       13833150
25  feet           Y    =         4216344
20  meter
 Z    =       17415634
75                 Z    =         5308285
47
 XDOT =     -24066
442996                 XDOT =       -7335
451825
 YDOT =       1655
792747  feet/sec       YDOT =         504
685629  meter/sec
 ZDOT =       -967
817200                 ZDOT =        -294
990683


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   15347
58297109  
00016717  00000-0  10270-3 0  9020
2 25544  51
6431 268
7827 0008189 275
5297  84
4922 15
54748776 15958


Satellite: ISS
Catalog Number: 25544
Epoch time:      15347
58297109   =   yrday
fracday
Element set:     902
Inclination:       51
6431  deg
RA of node:       268
7827  deg
Eccentricity:     
0008189     
Arg of perigee:   275
5297  deg
Mean anomaly:      84
4922  deg
Mean motion:   15
54748776  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1595
Checksum:              362


Coasting Arc #4 (Orbit 1609)
---------------------------------------

Vector Time (GMT): 2015/348/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4184296
66                 A    =         6777459
08  meter
 Y    =       -2229608
86  meter          E    =           
0004029
 Z    =       -4846744
77                 I    =           51
26475
 XDOT =       1066
234623                 Wp   =          123
38249
 YDOT =      -7204
375959  meter/sec      RA   =          263
13673  deg
 ZDOT =       2392
933284                 TA   =          170
21041
                                          MA   =          170
20256
                                          Ha   =            218
058  n
mi
                                          Hp   =            216
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13728007
41                 X    =        -4135510
05
 Y    =       -7314989
71  feet           Y    =        -2276127
23  meter
 Z    =      -15901393
59                 Z    =        -4866952
90
 XDOT =       3498
145089                 XDOT =        1135
092543
 YDOT =     -23636
404064  feet/sec       YDOT =       -7192
067819  meter/sec
 ZDOT =       7850
830985                 ZDOT =        2398
279452

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6168986
35                 X    =         1880307
04
 Y    =      -14182378
53  feet           Y    =        -4322788
98  meter
 Z    =      -15988287
16                 Z    =        -4873229
93
 XDOT =      22805
168099                 XDOT =        6951
015237
 YDOT =       1038
865294  feet/sec       YDOT =         316
646142  meter/sec
 ZDOT =       7875
318441                 ZDOT =        2400
397061


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   15348
54712973  
00016717  00000-0  10270-3 0  9039
2 25544  51
6434 263
9717 0008098 279
4059  80
6178 15
54746168 16106


Satellite: ISS
Catalog Number: 25544
Epoch time:      15348
54712973   =   yrday
fracday
Element set:     903
Inclination:       51
6434  deg
RA of node:       263
9717  deg
Eccentricity:     
0008098     
Arg of perigee:   279
4059  deg
Mean anomaly:      80
6178  deg
Mean motion:   15
54746168  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1610
Checksum:              339


Coasting Arc #5 (Orbit 1625)
---------------------------------------

Vector Time (GMT): 2015/349/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3938723
42                 A    =         6781354
43  meter
 Y    =        4029623
02  meter          E    =           
0004814
 Z    =        3772651
76                 I    =           51
28207
 XDOT =      -2162
165899                 Wp   =           47
67783
 YDOT =       6044
318171  meter/sec      RA   =          258
11508  deg
 ZDOT =      -4192
054040                 TA   =           86
83901
                                          MA   =           86
78393
                                          Ha   =            218
475  n
mi
                                          Hp   =            216
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12922320
93                 X    =         3875044
43
 Y    =       13220547
95  feet           Y    =         4073312
10  meter
 Z    =       12377466
42                 Z    =         3791630
83
 XDOT =      -7093
720141                 XDOT =       -2209
230939
 YDOT =      19830
440194  feet/sec       YDOT =        6019
876553  meter/sec
 ZDOT =     -13753
458138                 ZDOT =       -4202
671240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11877958
07                 X    =        -3620401
62
 Y    =       14094871
39  feet           Y    =         4296116
80  meter
 Z    =       12458717
99                 Z    =         3797417
24
 XDOT =     -19400
069421                 XDOT =       -5913
141159
 YDOT =      -4131
135071  feet/sec       YDOT =       -1259
169970  meter/sec
 ZDOT =     -13800
489169                 ZDOT =       -4206
389099


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   15349
57554648  
00016717  00000-0  10270-3 0  9047
2 25544  51
6428 258
8402 0008055 283
2361  76
7893 15
54767847 16269


Satellite: ISS
Catalog Number: 25544
Epoch time:      15349
57554648   =   yrday
fracday
Element set:     904
Inclination:       51
6428  deg
RA of node:       258
8402  deg
Eccentricity:     
0008055     
Arg of perigee:   283
2361  deg
Mean anomaly:      76
7893  deg
Mean motion:   15
54767847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1626
Checksum:              350


Coasting Arc #6 (Orbit 1640)
---------------------------------------

Vector Time (GMT): 2015/350/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3477035
92                 A    =         6785253
50  meter
 Y    =       -5389616
10  meter          E    =           
0007709
 Z    =       -2197980
14                 I    =           51
30345
 XDOT =       3247
886834                 Wp   =          331
76423
 YDOT =      -4316
592556  meter/sec      RA   =          253
10553  deg
 ZDOT =       5445
534757                 TA   =            3
69305
                                          MA   =            3
68736
                                          Ha   =            218
529  n
mi
                                          Hp   =            216
781

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11407598
16                 X    =        -3405832
59
 Y    =      -17682467
51  feet           Y    =        -5428100
37  meter
 Z    =       -7211220
94                 Z    =        -2214698
16
 XDOT =      10655
796700                 XDOT =        3269
462441
 YDOT =     -14162
049068  feet/sec       YDOT =       -4280
152210  meter/sec
 ZDOT =      17865
927681                 ZDOT =        5461
364424

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16237522
90                 X    =         4949196
98
 Y    =      -13345908
92  feet           Y    =        -4067833
04  meter
 Z    =       -7282460
15                 Z    =        -2219693
85
 XDOT =      14319
861229                 XDOT =        4364
693703
 YDOT =       7633
746098  feet/sec       YDOT =        2326
765811  meter/sec
 ZDOT =      17935
150740                 ZDOT =        5466
633946


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   15350
53966905  
00016717  00000-0  10270-3 0  9059
2 25544  51
6432 254
0284 0008154 286
7014  73
3244 15
54810953 16410


Satellite: ISS
Catalog Number: 25544
Epoch time:      15350
53966905   =   yrday
fracday
Element set:     905
Inclination:       51
6432  deg
RA of node:       254
0284  deg
Eccentricity:     
0008154     
Arg of perigee:   286
7014  deg
Mean anomaly:      73
3244  deg
Mean motion:   15
54810953  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1641
Checksum:              303


Coasting Arc #7 (Orbit 1656)
---------------------------------------

Vector Time (GMT): 2015/351/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2760673
01                 A    =         6787350
68  meter
 Y    =        6188106
52  meter          E    =           
0005984
 Z    =         317565
79                 I    =           51
32020
 XDOT =      -4266
597618                 Wp   =          161
81978
 YDOT =       2211
349105  meter/sec      RA   =          248
10736  deg
 ZDOT =      -5975
037590                 TA   =           14
74218
                                          MA   =           14
72474
                                          Ha   =            218
795  n
mi
                                          Hp   =            216
643

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9057326
14                 X    =         2689728
29
 Y    =       20302186
75  feet           Y    =         6218581
50  meter
 Z    =        1041882
50                 Z    =          330804
47
 XDOT =     -13998
023680                 XDOT =       -4261
984016
 YDOT =       7255
082367  feet/sec       YDOT =        2163
663235  meter/sec
 ZDOT =     -19603
141698                 ZDOT =       -5995
752492

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18910092
36                 X    =        -5763796
15
 Y    =       11683422
94  feet           Y    =         3561107
31  meter
 Z    =        1097951
72                 Z    =          334655
68
 XDOT =      -8190
701940                 XDOT =       -2496
525951
 YDOT =     -11399
028799  feet/sec       YDOT =       -3474
423978  meter/sec
 ZDOT =     -19693
083241                 ZDOT =       -6002
451772


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   15351
56805019  
00016717  00000-0  10270-3 0  9062
2 25544  51
6430 248
8964 0008126 289
5604  70
4671 15
54792415 16570


Satellite: ISS
Catalog Number: 25544
Epoch time:      15351
56805019   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:       248
8964  deg
Eccentricity:     
0008126     
Arg of perigee:   289
5604  deg
Mean anomaly:      70
4671  deg
Mean motion:   15
54792415  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1657
Checksum:              326


Coasting Arc #8 (Orbit 1672)
---------------------------------------

Vector Time (GMT): 2015/352/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1770937
06                 A    =         6786156
48  meter
 Y    =       -6342138
46  meter          E    =           
0010914
 Z    =        1610512
52                 I    =           51
32941
 XDOT =       5129
123632                 Wp   =           26
73428
 YDOT =         18
093749  meter/sec      RA   =          243
11046  deg
 ZDOT =       5705
773600                 TA   =          350
98153
                                          MA   =          351
00112
                                          Ha   =            218
979  n
mi
                                          Hp   =            216
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5810160
97                 X    =        -1707709
34
 Y    =      -20807540
89  feet           Y    =        -6361588
78  meter
 Z    =        5283833
74                 Z    =         1602063
04
 XDOT =      16827
833437                 XDOT =        5100
823650
 YDOT =         59
362694  feet/sec       YDOT =          75
292579  meter/sec
 ZDOT =      18719
729660                 ZDOT =        5730
621093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19688596
70                 X    =         6001084
28
 Y    =       -8913095
02  feet           Y    =        -2716711
36  meter
 Z    =        5248478
27                 Z    =         1599736
18
 XDOT =       1807
709741                 XDOT =         550
989929
 YDOT =      15090
235062  feet/sec       YDOT =        4599
503647  meter/sec
 ZDOT =      18827
125208                 ZDOT =        5738
507763


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   15352
59641162  
00016717  00000-0  10270-3 0  9074
2 25544  51
6430 243
7633 0008291 294
8634  65
1657 15
54847537 16731


Satellite: ISS
Catalog Number: 25544
Epoch time:      15352
59641162   =   yrday
fracday
Element set:     907
Inclination:       51
6430  deg
RA of node:       243
7633  deg
Eccentricity:     
0008291     
Arg of perigee:   294
8634  deg
Mean anomaly:      65
1657  deg
Mean motion:   15
54847537  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1673
Checksum:              329


Coasting Arc #9 (Orbit 1687)
---------------------------------------

Vector Time (GMT): 2015/353/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         523925
37                 A    =         6782509
53  meter
 Y    =        5886124
73  meter          E    =           
0004487
 Z    =       -3330267
74                 I    =           51
33252
 XDOT =      -5708
586671                 Wp   =          321
87595
 YDOT =      -2127
796391  meter/sec      RA   =          238
10772  deg
 ZDOT =      -4652
059662                 TA   =          257
08582
                                          MA   =          257
13594
                                          Ha   =            219
141  n
mi
                                          Hp   =            216
174

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1718915
24                 X    =          474243
54
 Y    =       19311432
85  feet           Y    =         5891705
94  meter
 Z    =      -10926075
25                 Z    =        -3327843
08
 XDOT =     -18728
958893                 XDOT =       -5661
770872
 YDOT =      -6980
959289  feet/sec       YDOT =       -2191
371661  meter/sec
 ZDOT =     -15262
662932                 ZDOT =       -4679
677253

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18736940
14                 X    =        -5711019
35
 Y    =        5001866
52  feet           Y    =         1524568
91  meter
 Z    =      -10916667
73                 Z    =        -3327400
33
 XDOT =       4123
904779                 XDOT =        1256
966177
 YDOT =     -18171
591545  feet/sec       YDOT =       -5538
701103  meter/sec
 ZDOT =     -15381
654968                 ZDOT =       -4688
328434


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   15353
56048475  
00016717  00000-0  10270-3 0  9081
2 25544  51
6429 238
9520 0008416 297
2410  62
7885 15
54859477 16886


Satellite: ISS
Catalog Number: 25544
Epoch time:      15353
56048475   =   yrday
fracday
Element set:     908
Inclination:       51
6429  deg
RA of node:       238
9520  deg
Eccentricity:     
0008416     
Arg of perigee:   297
2410  deg
Mean anomaly:      62
7885  deg
Mean motion:   15
54859477  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1688
Checksum:              351


Coasting Arc #10 (Orbit 1703)
---------------------------------------

Vector Time (GMT): 2015/354/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         930982
94                 A    =         6778122
90  meter
 Y    =       -4889370
80  meter          E    =           
0001146
 Z    =        4600085
22                 I    =           51
33581
 XDOT =       5897
611737                 Wp   =           34
66727
 YDOT =       3907
914875  meter/sec      RA   =          233
09187  deg
 ZDOT =       2960
652326                 TA   =           25
70551
                                          MA   =           25
69982
                                          Ha   =            219
266  n
mi
                                          Hp   =            215
866

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3054405
97                 X    =          963242
32
 Y    =      -16041242
78  feet           Y    =        -4878779
76  meter
 Z    =       15092143
11                 Z    =         4604685
91
 XDOT =      19349
119873                 XDOT =        5839
092361
 YDOT =      12821
243029  feet/sec       YDOT =        3973
538534  meter/sec
 ZDOT =       9713
426265                 ZDOT =        2989
159914

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16310131
23                 X    =         4971328
00
 Y    =         -54640
34  feet           Y    =          -16654
37  meter
 Z    =       15112917
76                 Z    =         4606417
33
 XDOT =      -9044
813033                 XDOT =       -2756
859013
 YDOT =      20132
953489  feet/sec       YDOT =        6136
524224  meter/sec
 ZDOT =       9835
954619                 ZDOT =        2997
998968


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   15354
58881386  
00016717  00000-0  10270-3 0  9091
2 25544  51
6429 233
8189 0008312 302
4936  57
5413 15
54883842 17049


Satellite: ISS
Catalog Number: 25544
Epoch time:      15354
58881386   =   yrday
fracday
Element set:     909
Inclination:       51
6429  deg
RA of node:       233
8189  deg
Eccentricity:     
0008312     
Arg of perigee:   302
4936  deg
Mean anomaly:      57
5413  deg
Mean motion:   15
54883842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1704
Checksum:              334


Coasting Arc #11 (Orbit 1718)
---------------------------------------

Vector Time (GMT): 2015/355/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2467026
35                 A    =         6775233
57  meter
 Y    =        3525903
90  meter          E    =           
0010008
 Z    =       -5240469
97                 I    =           51
34580
 XDOT =      -5578
533050                 Wp   =           48
61330
 YDOT =      -5184
552351  meter/sec      RA   =          228
06564  deg
 ZDOT =       -856
678831                 TA   =          213
12572
                                          MA   =          213
18843
                                          Ha   =            219
373  n
mi
                                          Hp   =            215
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8093918
48                 X    =        -2480814
17
 Y    =       11567926
20  feet           Y    =         3498239
22  meter
 Z    =      -17193142
93                 Z    =        -5252487
63
 XDOT =     -18302
273787                 XDOT =       -5515
982061
 YDOT =     -17009
686192  feet/sec       YDOT =       -5246
585397  meter/sec
 ZDOT =      -2810
626085                 ZDOT =        -883
626773

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12937804
28                 X    =        -3943442
74
 Y    =       -5489118
30  feet           Y    =        -1673083
26  meter
 Z    =      -17245735
63                 Z    =        -5256500
22
 XDOT =      12576
364736                 XDOT =        3833
275972
 YDOT =     -20393
067262  feet/sec       YDOT =       -6215
806901  meter/sec
 ZDOT =      -2926
195865                 ZDOT =        -891
904500


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   15355
55285472  
00016717  00000-0  10270-3 0  9105
2 25544  51
6420 229
0068 0008468 305
5839  54
4524 15
54947745 17199


Satellite: ISS
Catalog Number: 25544
Epoch time:      15355
55285472   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:       229
0068  deg
Eccentricity:     
0008468     
Arg of perigee:   305
5839  deg
Mean anomaly:      54
4524  deg
Mean motion:   15
54947745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1719
Checksum:              328


Coasting Arc #12 (Orbit 1734)
---------------------------------------

Vector Time (GMT): 2015/356/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3957691
94                 A    =         6775527
16  meter
 Y    =       -1936963
30  meter          E    =           
0008379
 Z    =        5151303
91                 I    =           51
36921
 XDOT =       4697
140036                 Wp   =          339
10002
 YDOT =       5898
826287  meter/sec      RA   =          223
03724  deg
 ZDOT =      -1383
734164                 TA   =          124
29856
                                          MA   =          124
21922
                                          Ha   =            219
464  n
mi
                                          Hp   =            215
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12984553
60                 X    =         3954034
20
 Y    =       -6354866
46  feet           Y    =        -1892726
64  meter
 Z    =       16900603
40                 Z    =         5170520
64
 XDOT =      15410
564423                 XDOT =        4637
550496
 YDOT =      19353
104616  feet/sec       YDOT =        5951
019736  meter/sec
 ZDOT =      -4539
810248                 ZDOT =       -1361
060551

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9011188
13                 X    =         2746610
14
 Y    =       11178290
27  feet           Y    =         3407142
87  meter
 Z    =       16984041
63                 Z    =         5176735
89
 XDOT =     -14699
818758                 XDOT =       -4480
504757
 YDOT =      18635
003706  feet/sec       YDOT =        5679
949130  meter/sec
 ZDOT =      -4442
833916                 ZDOT =       -1354
175778


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   15356
58114992  
00016717  00000-0  10270-3 0  9118
2 25544  51
6421 223
8743 0008492 308
8713  51
1682 15
54965182 17358


Satellite: ISS
Catalog Number: 25544
Epoch time:      15356
58114992   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:       223
8743  deg
Eccentricity:     
0008492     
Arg of perigee:   308
8713  deg
Mean anomaly:      51
1682  deg
Mean motion:   15
54965182  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1735
Checksum:              320


Coasting Arc #13 (Orbit 1749)
---------------------------------------

Vector Time (GMT): 2015/357/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5191265
77                 A    =         6778692
26  meter
 Y    =         344752
54  meter          E    =           
0003319
 Z    =       -4345616
16                 I    =           51
40247
 XDOT =      -3268
131423                 Wp   =           38
30396
 YDOT =      -6029
596436  meter/sec      RA   =          218
01510  deg
 ZDOT =       3429
718644                 TA   =          266
58709
                                          MA   =          266
62505
                                          Ha   =            219
552  n
mi
                                          Hp   =            215
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17031711
84                 X    =        -5173625
67
 Y    =        1131077
88  feet           Y    =          286799
43  meter
 Z    =      -14257270
87                 Z    =        -4370791
46
 XDOT =     -10722
215956                 XDOT =       -3217
124397
 YDOT =     -19782
140538  feet/sec       YDOT =       -6065
857973  meter/sec
 ZDOT =      11252
357756                 ZDOT =        3413
965996

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5080359
94                 X    =        -1548493
71
 Y    =      -16199707
77  feet           Y    =        -4937670
93  meter
 Z    =      -14366200
92                 Z    =        -4378818
04
 XDOT =      15507
911374                 XDOT =        4726
811387
 YDOT =     -14771
311273  feet/sec       YDOT =       -4502
295676  meter/sec
 ZDOT =      11185
317313                 ZDOT =        3409
284717


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   15357
54516177  
00016717  00000-0  10270-3 0  9127
2 25544  51
6405 219
0612 0008522 312
3924  47
6508 15
54986902 17507


Satellite: ISS
Catalog Number: 25544
Epoch time:      15357
54516177   =   yrday
fracday
Element set:     912
Inclination:       51
6405  deg
RA of node:       219
0612  deg
Eccentricity:     
0008522     
Arg of perigee:   312
3924  deg
Mean anomaly:      47
6508  deg
Mean motion:   15
54986902  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1750
Checksum:              308


Coasting Arc #14 (Orbit 1765)
---------------------------------------

Vector Time (GMT): 2015/358/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6019218
37                 A    =         6782975
79  meter
 Y    =        1144710
14  meter          E    =           
0008406
 Z    =        2909633
30                 I    =           51
44308
 XDOT =       1355
784863                 Wp   =           57
75293
 YDOT =       5642
150963  meter/sec      RA   =          213
00893  deg
 ZDOT =      -5009
459679                 TA   =           88
97880
                                          MA   =           88
88249
                                          Ha   =            219
798  n
mi
                                          Hp   =            214
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19748091
77                 X    =         5991836
73
 Y    =        3755610
70  feet           Y    =         1211867
61  meter
 Z    =        9546041
00                 Z    =         2938807
00
 XDOT =       4448
113067                 XDOT =        1316
926165
 YDOT =      18510
993974  feet/sec       YDOT =        5657
095508  meter/sec
 ZDOT =     -16435
235167                 ZDOT =       -5002
967345

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1320898
66                 X    =          402609
91
 Y    =       19998150
05  feet           Y    =         6095436
13  meter
 Z    =        9672014
31                 Z    =         2948029
96
 XDOT =     -15308
534092                 XDOT =       -4666
041191
 YDOT =       8970
400124  feet/sec       YDOT =        2734
177958  meter/sec
 ZDOT =     -16408
162458                 ZDOT =       -5001
207917


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   15358
57342354  
00016717  00000-0  10270-3 0  9136
2 25544  51
6405 213
9285 0008734 316
5125  43
5339 15
55046759 17662


Satellite: ISS
Catalog Number: 25544
Epoch time:      15358
57342354   =   yrday
fracday
Element set:     913
Inclination:       51
6405  deg
RA of node:       213
9285  deg
Eccentricity:     
0008734     
Arg of perigee:   316
5125  deg
Mean anomaly:      43
5339  deg
Mean motion:   15
55046759  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1766
Checksum:              322


Coasting Arc #15 (Orbit 1780)
---------------------------------------

Vector Time (GMT): 2015/359/12:50:46
594
Vector Time (MET): N/A
Weight (LBS)     : 906357
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6259280
47                 A    =         6786243
82  meter
 Y    =       -2369113
45  meter          E    =           
0013997
 Z    =       -1065983
92                 I    =           51
47902
 XDOT =        839
346180                 Wp   =            1
50042
 YDOT =      -4857
286101  meter/sec      RA   =          208
01561  deg
 ZDOT =       5882
109802                 TA   =          346
90144
                                          MA   =          346
93775
                                          Ha   =            219
906  n
mi
                                          Hp   =            214
666

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20535697
09                 X    =        -6227145
16
 Y    =       -7772681
92  feet           Y    =        -2438929
06  meter
 Z    =       -3497322
58                 Z    =        -1096312
24
 XDOT =       2753
760433                 XDOT =         865
026325
 YDOT =     -15935
978022  feet/sec       YDOT =       -4847
757036  meter/sec
 ZDOT =      19298
260505                 ZDOT =        5886
248990

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1982676
11                 X    =          604319
68
 Y    =      -21846433
04  feet           Y    =        -6658792
79  meter
 Z    =       -3628093
63                 Z    =        -1105842
94
 XDOT =      14462
353606                 XDOT =        4408
125379
 YDOT =      -1887
378094  feet/sec       YDOT =        -575
272843  meter/sec
 ZDOT =      19317
027966                 ZDOT =        5887
830124


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   15359
53740620  
00016717  00000-0  10270-3 0  9142
2 25544  51
6386 209
1149 0008617 319
6675  40
3838 15
55012382 17811


Satellite: ISS
Catalog Number: 25544
Epoch time:      15359
53740620   =   yrday
fracday
Element set:     914
Inclination:       51
6386  deg
RA of node:       209
1149  deg
Eccentricity:     
0008617     
Arg of perigee:   319
6675  deg
Mean anomaly:      40
3838  deg
Mean motion:   15
55012382  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1781
Checksum:              317
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