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

 
Date: August 13th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

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


229/22:24:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 0
000/00:00:00 000 0 0 0 0 212 9

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

237/07:37:09 920 1 4 4 6 4 6
N/A 4 4 -0 5 219 8
000/00:14:15 840 0 4 -0 0 215 9

239/10:03:00 000 0 0 0 0 0 0
N/A 0 0 0 0 219 6
000/00:00:00 000 0 0 0 0 215 9

Coasting Arc #1 (Orbit 1373)
---------------------------------------

Vector Time (GMT): 2016/225/10:49:40
629
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5633400
16                 A    =         6782309
00  meter
 Y    =        1804050
29  meter          E    =           
0014190
 Z    =        3306256
08                 I    =           51
89800
 XDOT =        874
656997                 Wp   =           91
34957
 YDOT =      -5975
400815  meter/sec      RA   =          136
24748  deg
 ZDOT =       4732
941964                 TA   =          306
96777
                                          MA   =          307
09760
                                          Ha   =            220
310  n
mi
                                          Hp   =            212
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18482283
99                 X    =        -5669215
05
 Y    =        5918800
16  feet           Y    =         1740853
56  meter
 Z    =       10847296
85                 Z    =         3278803
70
 XDOT =       2869
609570                 XDOT =         918
420045
 YDOT =     -19604
333381  feet/sec       YDOT =       -5965
375165  meter/sec
 ZDOT =      15528
024817                 ZDOT =        4737
297031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15044411
65                 X    =         4585536
67
 Y    =       12364727
22  feet           Y    =         3768768
86  meter
 Z    =       10727071
58                 Z    =         3269611
42
 XDOT =     -17063
470159                 XDOT =       -5200
945705
 YDOT =       7221
431897  feet/sec       YDOT =        2201
092442  meter/sec
 ZDOT =      15548
032532                 ZDOT =        4739
040316


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   16225
50865708  
00016717  00000-0  10270-3 0  9002
2 25544  51
6412 137
0030 0001691 117
7742 242
3582 15
54983006 13743


Satellite: ISS
Catalog Number: 25544
Epoch time:      16225
50865708   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:       137
0030  deg
Eccentricity:     
0001691     
Arg of perigee:   117
7742  deg
Mean anomaly:     242
3582  deg
Mean motion:   15
54983006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1374
Checksum:              289


Coasting Arc #2 (Orbit 1388)
---------------------------------------

Vector Time (GMT): 2016/226/10:49:40
629
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4957295
94                 A    =         6777810
22  meter
 Y    =        -145425
33  meter          E    =           
0011335
 Z    =       -4630636
07                 I    =           51
90718
 XDOT =      -2610
931598                 Wp   =           76
41420
 YDOT =       6545
182559  meter/sec      RA   =          131
27139  deg
 ZDOT =      -3004
238326                 TA   =          163
71566
                                          MA   =          163
67921
                                          Ha   =            220
184  n
mi
                                          Hp   =            212
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16264094
29                 X    =         4981047
07
 Y    =        -477117
22  feet           Y    =          -89856
65  meter
 Z    =      -15192375
57                 Z    =        -4606497
35
 XDOT =      -8566
048549                 XDOT =       -2669
334300
 YDOT =      21473
696060  feet/sec       YDOT =        6515
658880  meter/sec
 ZDOT =      -9856
424954                 ZDOT =       -3017
063177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9516455
77                 X    =        -2900615
72
 Y    =      -13318392
91  feet           Y    =        -4059446
16  meter
 Z    =      -15086886
99                 Z    =        -4598483
15
 XDOT =      21595
925873                 XDOT =        6582
438206
 YDOT =      -4214
487212  feet/sec       YDOT =       -1284
575702  meter/sec
 ZDOT =      -9913
542480                 ZDOT =       -3021
647748


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   16226
47265341  
00016717  00000-0  10270-3 0  9017
2 25544  51
6425 132
1913 0001649 117
4648 242
6673 15
55009939 13893


Satellite: ISS
Catalog Number: 25544
Epoch time:      16226
47265341   =   yrday
fracday
Element set:     901
Inclination:       51
6425  deg
RA of node:       132
1913  deg
Eccentricity:     
0001649     
Arg of perigee:   117
4648  deg
Mean anomaly:     242
6673  deg
Mean motion:   15
55009939  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1389
Checksum:              314


Coasting Arc #3 (Orbit 1404)
---------------------------------------

Vector Time (GMT): 2016/227/10:49:40
629
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3908491
78                 A    =         6774957
50  meter
 Y    =       -1661216
76  meter          E    =           
0004934
 Z    =        5275380
68                 I    =           51
91857
 XDOT =       3946
660048                 Wp   =          122
19825
 YDOT =      -6523
127706  meter/sec      RA   =          126
28586  deg
 ZDOT =        866
767035                 TA   =          319
53255
                                          MA   =          319
56923
                                          Ha   =            220
192  n
mi
                                          Hp   =            212
768

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12823135
77                 X    =        -3915250
32
 Y    =       -5450186
21  feet           Y    =        -1704962
01  meter
 Z    =       17307679
39                 Z    =         5256378
02
 XDOT =      12948
359737                 XDOT =        4015
099667
 YDOT =     -21401
337619  feet/sec       YDOT =       -6478
610863  meter/sec
 ZDOT =       2843
723868                 ZDOT =         886
104762

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2921721
53                 X    =          890540
72
 Y    =       13728025
31  feet           Y    =         4184302
11  meter
 Z    =       17224922
96                 Z    =         5250156
52
 XDOT =     -23949
949256                 XDOT =       -7299
944533
 YDOT =       1408
716397  feet/sec       YDOT =         429
376758  meter/sec
 ZDOT =       2929
310596                 ZDOT =         892
853870


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   16227
50090779  
00016717  00000-0  10270-3 0  9024
2 25544  51
6425 127
0597 0001537 124
7838 235
3460 15
55039461 14057


Satellite: ISS
Catalog Number: 25544
Epoch time:      16227
50090779   =   yrday
fracday
Element set:     902
Inclination:       51
6425  deg
RA of node:       127
0597  deg
Eccentricity:     
0001537     
Arg of perigee:   124
7838  deg
Mean anomaly:     235
3460  deg
Mean motion:   15
55039461  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1405
Checksum:              305


Coasting Arc #4 (Orbit 1419)
---------------------------------------

Vector Time (GMT): 2016/228/10:49:40
629
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2655674
79                 A    =         6775402
53  meter
 Y    =        3463595
79  meter          E    =           
0015347
 Z    =       -5195958
35                 I    =           51
93877
 XDOT =      -4808
350379                 Wp   =          103
16817
 YDOT =       5792
977358  meter/sec      RA   =          121
29670  deg
 ZDOT =       1404
077973                 TA   =          180
29664
                                          MA   =          180
29756
                                          Ha   =            220
099  n
mi
                                          Hp   =            212
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8712843
80                 X    =         2641985
91
 Y    =       11363503
25  feet           Y    =         3493216
84  meter
 Z    =      -17047107
43                 Z    =        -5183091
17
 XDOT =     -15775
427754                 XDOT =       -4879
591842
 YDOT =      19005
831226  feet/sec       YDOT =        5738
808819  meter/sec
 ZDOT =       4606
555030                 ZDOT =        1380
547640

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4043849
74                 X    =         1232565
40
 Y    =      -13805228
00  feet           Y    =        -4207833
49  meter
 Z    =      -16991459
16                 Z    =        -5178996
75
 XDOT =      23655
042240                 XDOT =        7210
056875
 YDOT =       1387
412351  feet/sec       YDOT =         422
883284  meter/sec
 ZDOT =       4502
753013                 ZDOT =        1372
439118


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   16228
46489348  
00016717  00000-0  10270-3 0  9035
2 25544  51
6431 122
2483 0001572 125
1874 234
9426 15
55014495 14203


Satellite: ISS
Catalog Number: 25544
Epoch time:      16228
46489348   =   yrday
fracday
Element set:     903
Inclination:       51
6431  deg
RA of node:       122
2483  deg
Eccentricity:     
0001572     
Arg of perigee:   125
1874  deg
Mean anomaly:     234
9426  deg
Mean motion:   15
55014495  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1420
Checksum:              302


Coasting Arc #5 (Orbit 1435)
---------------------------------------

Vector Time (GMT): 2016/229/10:49:40
629
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1318721
37                 A    =         6778695
55  meter
 Y    =       -5017954
80  meter          E    =           
0010501
 Z    =        4354922
24                 I    =           51
96595
 XDOT =       5224
037384                 Wp   =           78
79712
 YDOT =      -4407
943076  meter/sec      RA   =          116
31583  deg
 ZDOT =      -3488
064058                 TA   =           46
49266
                                          MA   =           46
40543
                                          Ha   =            220
109  n
mi
                                          Hp   =            212
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4326513
68                 X    =        -1283665
24
 Y    =      -16463106
29  feet           Y    =        -5032505
59  meter
 Z    =       14287802
62                 Z    =         4348601
51
 XDOT =      17139
230264                 XDOT =        5289
883039
 YDOT =     -14461
755498  feet/sec       YDOT =       -4349
156248  meter/sec
 ZDOT =     -11443
779717                 ZDOT =       -3462
527544

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10527775
55                 X    =        -3208865
99
 Y    =       13404587
94  feet           Y    =         4085718
40  meter
 Z    =       14261025
81                 Z    =         4346760
67
 XDOT =     -20916
808828                 XDOT =       -6375
443331
 YDOT =      -4340
591185  feet/sec       YDOT =       -1323
012193  meter/sec
 ZDOT =     -11331
428495                 ZDOT =       -3453
819405


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   16229
49313707  
00016717  00000-0  10270-3 0  9045
2 25544  51
6432 117
1169 0001541 129
6795 230
4494 15
55023651 14362


Satellite: ISS
Catalog Number: 25544
Epoch time:      16229
49313707   =   yrday
fracday
Element set:     904
Inclination:       51
6432  deg
RA of node:       117
1169  deg
Eccentricity:     
0001541     
Arg of perigee:   129
6795  deg
Mean anomaly:     230
4494  deg
Mean motion:   15
55023651  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1436
Checksum:              301


Coasting Arc #6 (Orbit 1442)
---------------------------------------

Vector Time (GMT): 2016/229/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1459375
15                 A    =         6778791
94  meter
 Y    =        5030354
21  meter          E    =           
0010015
 Z    =       -4313756
96                 I    =           51
97411
 XDOT =      -5054
020150                 Wp   =          116
32490
 YDOT =       4520
916262  meter/sec      RA   =          113
91674  deg
 ZDOT =       3564
185082                 TA   =          189
86714
                                          MA   =          189
88682
                                          Ha   =            219
995  n
mi
                                          Hp   =            212
860

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4787976
20                 X    =         1423969
93
 Y    =       16503786
77  feet           Y    =         5046475
89  meter
 Z    =      -14152745
92                 Z    =        -4306753
89
 XDOT =     -16581
430939                 XDOT =       -5121
511477
 YDOT =      14832
402433  feet/sec       YDOT =        4464
021512  meter/sec
 ZDOT =      11693
520610                 ZDOT =        3539
470434

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11657817
62                 X    =        -3553302
81
 Y    =       12658450
04  feet           Y    =         3858295
57  meter
 Z    =      -14122989
83                 Z    =        -4304687
30
 XDOT =     -20357
119667                 XDOT =       -6204
850074
 YDOT =      -5830
460672  feet/sec       YDOT =       -1777
124413  meter/sec
 ZDOT =      11584
736003                 ZDOT =        3531
027534


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   16229
94298935  
00016717  00000-0  10270-3 0  9051
2 25544  51
6439 114
8684 0001801 144
3045 215
8229 15
55052868 14439


Satellite: ISS
Catalog Number: 25544
Epoch time:      16229
94298935   =   yrday
fracday
Element set:     905
Inclination:       51
6439  deg
RA of node:       114
8684  deg
Eccentricity:     
0001801     
Arg of perigee:   144
3045  deg
Mean anomaly:     215
8229  deg
Mean motion:   15
55052868  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1443
Checksum:              324


Coasting Arc #7 (Orbit 1458)
---------------------------------------

Vector Time (GMT): 2016/230/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -214580
88                 A    =         6783315
27  meter
 Y    =       -6157899
29  meter          E    =           
0014692
 Z    =        2819453
88                 I    =           52
00075
 XDOT =       5110
277894                 Wp   =          104
72858
 YDOT =      -2536
410060  meter/sec      RA   =          108
95054  deg
 ZDOT =      -5132
184037                 TA   =           43
39963
                                          MA   =           43
28405
                                          Ha   =            220
028  n
mi
                                          Hp   =            212
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -704005
51                 X    =         -159401
15
 Y    =      -20203081
66  feet           Y    =        -6159990
25  meter
 Z    =        9250176
77                 Z    =         2818545
76
 XDOT =      16766
003589                 XDOT =        5163
190280
 YDOT =      -8321
555315  feet/sec       YDOT =       -2478
967843  meter/sec
 ZDOT =     -16837
874138                 ZDOT =       -5107
231510

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16753358
25                 X    =         5106423
59
 Y    =      -11315439
08  feet           Y    =        -3448945
83  meter
 Z    =        9247255
18                 Z    =         2818563
38
 XDOT =      15152
926562                 XDOT =        4618
612016
 YDOT =       8714
328587  feet/sec       YDOT =        2656
127353  meter/sec
 ZDOT =     -16728
376114                 ZDOT =       -5098
809040


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   16230
97122333  
00016717  00000-0  10270-3 0  9065
2 25544  51
6434 109
7364 0001752 144
3862 215
7408 15
55037908 14597


Satellite: ISS
Catalog Number: 25544
Epoch time:      16230
97122333   =   yrday
fracday
Element set:     906
Inclination:       51
6434  deg
RA of node:       109
7364  deg
Eccentricity:     
0001752     
Arg of perigee:   144
3862  deg
Mean anomaly:     215
7408  deg
Mean motion:   15
55037908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1459
Checksum:              306


Coasting Arc #8 (Orbit 1473)
---------------------------------------

Vector Time (GMT): 2016/231/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -894376
59                 A    =         6786385
06  meter
 Y    =        6656227
32  meter          E    =           
0009462
 Z    =        -950595
95                 I    =           52
01971
 XDOT =      -4834
530275                 Wp   =           47
84651
 YDOT =        193
642219  meter/sec      RA   =          103
99728  deg
 ZDOT =       5948
446884                 TA   =          301
91198
                                          MA   =          302
00398
                                          Ha   =            219
972  n
mi
                                          Hp   =            212
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2934306
41                 X    =         -964124
25
 Y    =       21838016
15  feet           Y    =         6645835
77  meter
 Z    =       -3118753
13                 Z    =         -955110
29
 XDOT =     -15861
319801                 XDOT =       -4865
230738
 YDOT =        635
309118  feet/sec       YDOT =         139
407935  meter/sec
 ZDOT =      19515
901852                 ZDOT =        5924
887841

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19925465
83                 X    =        -6073281
99
 Y    =        9399696
51  feet           Y    =         2865027
49  meter
 Z    =       -3139624
42                 Z    =         -956957
52
 XDOT =      -8523
233801                 XDOT =       -2597
881663
 YDOT =     -11631
188695  feet/sec       YDOT =       -3545
186314  meter/sec
 ZDOT =      19412
887958                 ZDOT =        5917
048250


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   16231
93518756  
00016717  00000-0  10270-3 0  9071
2 25544  51
6428 104
9250 0001555 148
3892 211
7354 15
55006494 14748


Satellite: ISS
Catalog Number: 25544
Epoch time:      16231
93518756   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:       104
9250  deg
Eccentricity:     
0001555     
Arg of perigee:   148
3892  deg
Mean anomaly:     211
7354  deg
Mean motion:   15
55006494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1474
Checksum:              313


Coasting Arc #9 (Orbit 1489)
---------------------------------------

Vector Time (GMT): 2016/232/22:24:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1887824
72                 A    =         6786150
11  meter
 Y    =       -6420386
61  meter          E    =           
0011159
 Z    =       -1094707
97                 I    =           52
02574
 XDOT =       4316
445042                 Wp   =          143
35951
 YDOT =       2271
618658  meter/sec      RA   =           99
04942  deg
 ZDOT =      -5918
826769                 TA   =           48
45779
                                          MA   =           48
36213
                                          Ha   =            219
924  n
mi
                                          Hp   =            212
932

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6193650
64                 X    =         1964796
33
 Y    =      -21064260
54  feet           Y    =        -6398845
40  meter
 Z    =       -3591561
59                 Z    =        -1085350
15
 XDOT =      14161
565098                 XDOT =        4319
473044
 YDOT =       7452
817119  feet/sec       YDOT =        2319
904553  meter/sec
 ZDOT =     -19418
722997                 ZDOT =       -5897
851723

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20957914
93                 X    =         6387972
47
 Y    =       -6567357
59  feet           Y    =        -2001730
59  meter
 Z    =       -3549550
86                 Z    =        -1081903
10
 XDOT =       1288
708283                 XDOT =         392
798285
 YDOT =      14487
573127  feet/sec       YDOT =        4415
812289  meter/sec
 ZDOT =     -19327
425460                 ZDOT =       -5890
999280


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16232
96341100  
00016717  00000-0  10270-3 0  9083
2 25544  51
6424  99
7924 0001664 152
4632 207
6609 15
55051047 14901


Satellite: ISS
Catalog Number: 25544
Epoch time:      16232
96341100   =   yrday
fracday
Element set:     908
Inclination:       51
6424  deg
RA of node:        99
7924  deg
Eccentricity:     
0001664     
Arg of perigee:   152
4632  deg
Mean anomaly:     207
6609  deg
Mean motion:   15
55051047  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1490
Checksum:              298


Coasting Arc #10 (Orbit 1504)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3864061
92                 A    =         6775397
44  meter
 Y    =       -2134265
61  meter          E    =           
0004900
 Z    =        5136352
17                 I    =           51
99531
 XDOT =       1832
594873                 Wp   =           72
99221
 YDOT =      -7268
730974  meter/sec      RA   =           94
31326  deg
 ZDOT =      -1638
978925                 TA   =           32
75118
                                          MA   =           32
72081
                                          Ha   =            219
901  n
mi
                                          Hp   =            212
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12677368
50                 X    =        -3864858
70
 Y    =       -7002183
78  feet           Y    =        -2177480
19  meter
 Z    =       16851549
10                 Z    =         5117580
00
 XDOT =       6012
450370                 XDOT =        1921
700812
 YDOT =     -23847
542565  feet/sec       YDOT =       -7247
739578  meter/sec
 ZDOT =      -5377
227445                 ZDOT =       -1629
859763

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3136478
02                 X    =          955998
50
 Y    =      -14235704
66  feet           Y    =        -4339042
78  meter
 Z    =       16769859
13                 Z    =         5111453
06
 XDOT =      23548
950705                 XDOT =        7177
720175
 YDOT =      -1107
999928  feet/sec       YDOT =        -337
718378  meter/sec
 ZDOT =      -5336
103960                 ZDOT =       -1626
444487


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16233
92736331  
00016717  00000-0  10270-3 0  9095
2 25544  51
6434  94
9792 0001555 157
6063 202
5159 15
55098493 15053


Satellite: ISS
Catalog Number: 25544
Epoch time:      16233
92736331   =   yrday
fracday
Element set:     909
Inclination:       51
6434  deg
RA of node:        94
9792  deg
Eccentricity:     
0001555     
Arg of perigee:   157
6063  deg
Mean anomaly:     202
5159  deg
Mean motion:   15
55098493  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1505
Checksum:              322


Coasting Arc #11 (Orbit 1519)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3357158
50                 A    =         6778995
75  meter
 Y    =        4100660
43  meter          E    =           
0009213
 Z    =       -4237017
77                 I    =           52
00750
 XDOT =      -2806
992484                 Wp   =          117
73803
 YDOT =       6102
577914  meter/sec      RA   =           89
33623  deg
 ZDOT =       3684
026474                 TA   =          189
85505
                                          MA   =          189
87314
                                          Ha   =            219
797  n
mi
                                          Hp   =            212
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11014299
55                 X    =         3331635
80
 Y    =       13453610
33  feet           Y    =         4138059
38  meter
 Z    =      -13900976
94                 Z    =        -4220772
00
 XDOT =      -9209
292928                 XDOT =       -2892
919693
 YDOT =      20021
581082  feet/sec       YDOT =        6070
708088  meter/sec
 ZDOT =      12086
701030                 ZDOT =        3670
181742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9551384
28                 X    =        -2911261
93
 Y    =       14595718
00  feet           Y    =         4448774
85  meter
 Z    =      -13830678
22                 Z    =        -4215590
72
 XDOT =     -20812
382214                 XDOT =       -6343
614099
 YDOT =      -2230
785972  feet/sec       YDOT =        -679
943564  meter/sec
 ZDOT =      12025
111704                 ZDOT =        3665
254048


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16234
89131443  
00016717  00000-0  10270-3 0  9107
2 25544  51
6421  90
1683 0001690 157
8579 202
2648 15
55092883 15204


Satellite: ISS
Catalog Number: 25544
Epoch time:      16234
89131443   =   yrday
fracday
Element set:     910
Inclination:       51
6421  deg
RA of node:        90
1683  deg
Eccentricity:     
0001690     
Arg of perigee:   157
8579  deg
Mean anomaly:     202
2648  deg
Mean motion:   15
55092883  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1520
Checksum:              305


Coasting Arc #12 (Orbit 1535)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2669871
18                 A    =         6783486
81  meter
 Y    =       -5613311
95  meter          E    =           
0014366
 Z    =        2698296
90                 I    =           52
02170
 XDOT =       3672
501913                 Wp   =          107
08716
 YDOT =      -4263
638467  meter/sec      RA   =           84
37188  deg
 ZDOT =      -5217
195763                 TA   =           42
57030
                                          MA   =           42
45902
                                          Ha   =            219
783  n
mi
                                          Hp   =            212
985

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8759419
87                 X    =        -2620010
37
 Y    =      -18416377
79  feet           Y    =        -5642889
26  meter
 Z    =        8852680
13                 Z    =         2685448
91
 XDOT =      12048
890792                 XDOT =        3745
248807
 YDOT =     -13988
315179  feet/sec       YDOT =       -4222
163709  meter/sec
 ZDOT =     -17116
784000                 ZDOT =       -5199
178771

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14728799
39                 X    =         4489338
06
 Y    =      -14139541
50  feet           Y    =        -4309732
25  meter
 Z    =        8797510
30                 Z    =         2681481
14
 XDOT =      16062
655622                 XDOT =        4895
897434
 YDOT =       6093
174416  feet/sec       YDOT =        1857
199562  meter/sec
 ZDOT =     -17037
269042                 ZDOT =       -5192
959604


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16235
91952284  
00016717  00000-0  10270-3 0  9116
2 25544  51
6427  85
0353 0001516 161
8309 198
2898 15
55089167 15369


Satellite: ISS
Catalog Number: 25544
Epoch time:      16235
91952284   =   yrday
fracday
Element set:     911
Inclination:       51
6427  deg
RA of node:        85
0353  deg
Eccentricity:     
0001516     
Arg of perigee:   161
8309  deg
Mean anomaly:     198
2898  deg
Mean motion:   15
55089167  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1536
Checksum:              329


Coasting Arc #13 (Orbit 1550)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1842530
58                 A    =         6786417
40  meter
 Y    =        6478765
99  meter          E    =           
0009696
 Z    =        -796397
42                 I    =           52
02699
 XDOT =      -4378
134794                 Wp   =           45
94860
 YDOT =       1973
643031  meter/sec      RA   =           79
41964  deg
 ZDOT =       5978
123022                 TA   =          305
48528
                                          MA   =          305
57571
                                          Ha   =            219
766  n
mi
                                          Hp   =            213
099

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6045047
83                 X    =         1773814
98
 Y    =       21255793
94  feet           Y    =         6498986
15  meter
 Z    =       -2612852
41                 Z    =         -787614
16
 XDOT =     -14363
959298                 XDOT =       -4428
918223
 YDOT =       6475
206795  feet/sec       YDOT =        1924
400184  meter/sec
 ZDOT =      19613
264509                 ZDOT =        5956
731760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18072293
91                 X    =        -5508435
18
 Y    =       12725437
52  feet           Y    =         3878713
36  meter
 Z    =       -2575618
36                 Z    =         -785048
48
 XDOT =      -9960
911634                 XDOT =       -3036
085866
 YDOT =     -10230
196300  feet/sec       YDOT =       -3118
163832  meter/sec
 ZDOT =      19519
399546                 ZDOT =        5949
512982


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16236
88346333  
00016717  00000-0  10270-3 0  9126
2 25544  51
6428  80
2234 0001273 162
5981 197
5216 15
55039291 15515


Satellite: ISS
Catalog Number: 25544
Epoch time:      16236
88346333   =   yrday
fracday
Element set:     912
Inclination:       51
6428  deg
RA of node:        80
2234  deg
Eccentricity:     
0001273     
Arg of perigee:   162
5981  deg
Mean anomaly:     197
5216  deg
Mean motion:   15
55039291  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1551
Checksum:              305


Coasting Arc #14 (Orbit 1557)
---------------------------------------

Vector Time (GMT): 2016/237/07:44:17
840
Vector Time (MET): N/A
Weight (LBS)     : 929483
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4290425
23                 A    =         6780086
76  meter
 Y    =        2408648
88  meter          E    =           
0007914
 Z    =       -4672548
20                 I    =           51
99533
 XDOT =       -754
443863                 Wp   =          124
43907
 YDOT =       7037
048426  meter/sec      RA   =           77
21797  deg
 ZDOT =       2933
955874                 TA   =          174
64345
                                          MA   =          174
63498
                                          Ha   =            219
796  n
mi
                                          Hp   =            215
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14076198
26                 X    =         4285869
38
 Y    =        7902391
35  feet           Y    =         2456601
59  meter
 Z    =      -15329882
55                 Z    =        -4651717
64
 XDOT =      -2475
209525                 XDOT =        -847
329695
 YDOT =      23087
429218  feet/sec       YDOT =        7028
092515  meter/sec
 ZDOT =       9625
839481                 ZDOT =        2930
065041

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8332181
89                 X    =         2539649
04
 Y    =      -13925956
24  feet           Y    =        -4244631
46  meter
 Z    =      -15239256
32                 Z    =        -4644925
33
 XDOT =      21984
081592                 XDOT =        6700
748069
 YDOT =       2636
938660  feet/sec       YDOT =         803
738903  meter/sec
 ZDOT =       9607
562131                 ZDOT =        2928
384938


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16237
33330380  
00016717  00000-0  10270-3 0  9133
2 25544  51
6435  77
9783 0003436 253
7683 106
3092 15
54165114 15580


Satellite: ISS
Catalog Number: 25544
Epoch time:      16237
33330380   =   yrday
fracday
Element set:     913
Inclination:       51
6435  deg
RA of node:        77
9783  deg
Eccentricity:     
0003436     
Arg of perigee:   253
7683  deg
Mean anomaly:     106
3092  deg
Mean motion:   15
54165114  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1558
Checksum:              307


Coasting Arc #15 (Orbit 1573)
---------------------------------------

Vector Time (GMT): 2016/238/07:44:17
840
Vector Time (MET): N/A
Weight (LBS)     : 929483
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4201207
09                 A    =         6783868
92  meter
 Y    =       -3928946
31  meter          E    =           
0008714
 Z    =        3588696
86                 I    =           51
99945
 XDOT =       1758
470260                 Wp   =           91
44296
 YDOT =      -5975
941199  meter/sec      RA   =           72
25498  deg
 ZDOT =      -4474
795560                 TA   =           46
35666
                                          MA   =           46
28443
                                          Ha   =            219
873  n
mi
                                          Hp   =            215
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13783487
81                 X    =        -4174392
63
 Y    =      -12890243
81  feet           Y    =        -3975776
98  meter
 Z    =       11773939
84                 Z    =         3568353
81
 XDOT =       5769
259384                 XDOT =        1846
900583
 YDOT =     -19606
106295  feet/sec       YDOT =       -5955
782510  meter/sec
 ZDOT =     -14681
087796                 ZDOT =       -4466
038412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13074865
27                 X    =        -3985218
93
 Y    =       13684308
46  feet           Y    =         4170977
22  meter
 Z    =       11685725
54                 Z    =         3561809
14
 XDOT =     -18528
708525                 XDOT =       -5647
550358
 YDOT =      -5174
435656  feet/sec       YDOT =       -1577
167988  meter/sec
 ZDOT =     -14641
715151                 ZDOT =       -4462
794778


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16238
36211485  
00016717  00000-0  10270-3 0  9142
2 25544  51
6431  72
8508 0003456 256
5397 103
5370 15
54155542 15740


Satellite: ISS
Catalog Number: 25544
Epoch time:      16238
36211485   =   yrday
fracday
Element set:     914
Inclination:       51
6431  deg
RA of node:        72
8508  deg
Eccentricity:     
0003456     
Arg of perigee:   256
5397  deg
Mean anomaly:     103
5370  deg
Mean motion:   15
54155542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1574
Checksum:              306


Coasting Arc #16 (Orbit 1588)
---------------------------------------

Vector Time (GMT): 2016/239/07:44:17
840
Vector Time (MET): N/A
Weight (LBS)     : 929483
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3942213
75                 A    =         6787248
83  meter
 Y    =        5090050
57  meter          E    =           
0004325
 Z    =       -2140876
48                 I    =           52
00171
 XDOT =      -2806
121868                 Wp   =            8
56493
 YDOT =       4499
543669  meter/sec      RA   =           67
29974  deg
 ZDOT =       5536
305412                 TA   =          327
83070
                                          MA   =          327
85708
                                          Ha   =            219
633  n
mi
                                          Hp   =            215
918

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12933772
15                 X    =         3895401
90
 Y    =       16699640
97  feet           Y    =         5133873
25  meter
 Z    =       -7023872
98                 Z    =        -2121840
16
 XDOT =      -9206
436574                 XDOT =       -2883
121129
 YDOT =      14762
282380  feet/sec       YDOT =        4467
733339  meter/sec
 ZDOT =      18163
731668                 ZDOT =        5522
486953

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16650614
65                 X    =         5075107
35
 Y    =      -13040958
95  feet           Y    =        -3974884
29  meter
 Z    =       -6941590
84                 Z    =        -2115796
89
 XDOT =      13847
533091                 XDOT =        4220
728086
 YDOT =       8054
524416  feet/sec       YDOT =        2455
019042  meter/sec
 ZDOT =      18102
492528                 ZDOT =        5517
639723


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16239
32661888  
00016717  00000-0  10270-3 0  9156
2 25544  51
6444  68
0420 0003610 261
8515  98
2228 15
54190079 15899


Satellite: ISS
Catalog Number: 25544
Epoch time:      16239
32661888   =   yrday
fracday
Element set:     915
Inclination:       51
6444  deg
RA of node:        68
0420  deg
Eccentricity:     
0003610     
Arg of perigee:   261
8515  deg
Mean anomaly:      98
2228  deg
Mean motion:   15
54190079  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1589
Checksum:              319


Coasting Arc #17 (Orbit 1590)
---------------------------------------

Vector Time (GMT): 2016/239/10:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910045
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4008935
32                 A    =         6787141
92  meter
 Y    =       -5010917
90  meter          E    =           
0010666
 Z    =        2192582
73                 I    =           51
99963
 XDOT =       2717
077009                 Wp   =          117
37162
 YDOT =      -4591
652686  meter/sec      RA   =           66
82142  deg
 ZDOT =      -5510
110731                 TA   =           38
40464
                                          MA   =           38
32876
                                          Ha   =            219
611  n
mi
                                          Hp   =            215
925

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13152674
93                 X    =        -3963254
55
 Y    =      -16440019
35  feet           Y    =        -5055493
03  meter
 Z    =        7193512
89                 Z    =         2173219
55
 XDOT =       8914
294650                 XDOT =        2794
985625
 YDOT =     -15064
477315  feet/sec       YDOT =       -4560
833028  meter/sec
 ZDOT =     -18077
791112                 ZDOT =       -5496
722622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5901498
96                 X    =        -1798776
88
 Y    =       20239489
81  feet           Y    =         6168996
49  meter
 Z    =        7109787
92                 Z    =         2167063
36
 XDOT =     -16045
861715                 XDOT =       -4890
778651
 YDOT =       1669
169131  feet/sec       YDOT =         508
762751  meter/sec
 ZDOT =     -18018
415449                 ZDOT =       -5492
013029


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16239
45521784  
00016717  00000-0  10270-3 0  9161
2 25544  51
6438  67
4008 0003662 265
1739  94
8995 15
54196414 15914


Satellite: ISS
Catalog Number: 25544
Epoch time:      16239
45521784   =   yrday
fracday
Element set:     916
Inclination:       51
6438  deg
RA of node:        67
4008  deg
Eccentricity:     
0003662     
Arg of perigee:   265
1739  deg
Mean anomaly:      94
8995  deg
Mean motion:   15
54196414  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1591
Checksum:              339


Coasting Arc #18 (Orbit 1605)
---------------------------------------

Vector Time (GMT): 2016/240/10:03:00
000
Vector Time (MET): N/A
Weight (LBS)     : 910045
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3543336
90                 A    =         6789083
68  meter
 Y    =        5761161
63  meter          E    =           
0008941
 Z    =        -523124
22                 I    =           51
99080
 XDOT =      -3792
344187                 Wp   =           23
80301
 YDOT =       2874
488608  meter/sec      RA   =           61
87240  deg
 ZDOT =       6013
233233                 TA   =          330
58040
                                          MA   =          330
63069
                                          Ha   =            219
600  n
mi
                                          Hp   =            215
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11625121
05                 X    =         3481191
86
 Y    =       18901448
92  feet           Y    =         5800438
11  meter
 Z    =       -1716286
82                 Z    =         -506062
86
 XDOT =     -12442
074105                 XDOT =       -3853
414946
 YDOT =       9430
736904  feet/sec       YDOT =        2831
738760  meter/sec
 ZDOT =      19728
455490                 ZDOT =        5994
662790

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8462985
57                 X    =         2579518
00
 Y    =      -20519089
44  feet           Y    =        -6254218
46  meter
 Z    =       -1642770
46                 Z    =         -500716
43
 XDOT =      13520
409286                 XDOT =        4121
020750
 YDOT =       4015
464074  feet/sec       YDOT =        1223
913450  meter/sec
 ZDOT =      19646
735171                 ZDOT =        5988
324880


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   16240
41971780  
00016717  00000-0  10270-3 0  9175
2 25544  51
6422  62
5918 0003675 268
5639  91
5093 15
54175725 16065


Satellite: ISS
Catalog Number: 25544
Epoch time:      16240
41971780   =   yrday
fracday
Element set:     917
Inclination:       51
6422  deg
RA of node:        62
5918  deg
Eccentricity:     
0003675     
Arg of perigee:   268
5639  deg
Mean anomaly:      91
5093  deg
Mean motion:   15
54175725  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1606
Checksum:              324
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