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

 
Date: August 4th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 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


217/02:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 212 7

220/05:58:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 212 7

223/08:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 212 8

Coasting Arc #1 (Orbit 1233)
---------------------------------------

Vector Time (GMT): 2016/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3291007
18                 A    =         6777785
57  meter
 Y    =        3657052
29  meter          E    =           
0012568
 Z    =       -4674066
12                 I    =           51
61675
 XDOT =      -6696
909687                 Wp   =          107
16983
 YDOT =      -2364
819754  meter/sec      RA   =          180
79556  deg
 ZDOT =       2867
776684                 TA   =          191
34793
                                          MA   =          191
37629
                                          Ha   =            220
493  n
mi
                                          Hp   =            212
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10797267
64                 X    =        -3308952
61
 Y    =       11998203
06  feet           Y    =         3620149
81  meter
 Z    =      -15334862
61                 Z    =        -4690096
15
 XDOT =     -21971
488474                 XDOT =       -6683
898043
 YDOT =      -7758
594994  feet/sec       YDOT =       -2439
636377  meter/sec
 ZDOT =       9408
716154                 ZDOT =        2835
277100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16073847
13                 X    =         4899308
61
 Y    =          22361
25  feet           Y    =            6815
71  meter
 Z    =      -15405415
11                 Z    =        -4695570
53
 XDOT =       8844
806451                 XDOT =        2695
897006
 YDOT =      20446
904900  feet/sec       YDOT =        6232
216613  meter/sec
 ZDOT =       9267
248584                 ZDOT =        2824
657368


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   16216
51107684  
00016717  00000-0  10270-3 0  9005
2 25544  51
6392 181
9078 0001906  91
5358 268
6014 15
54888267 12340


Satellite: ISS
Catalog Number: 25544
Epoch time:      16216
51107684   =   yrday
fracday
Element set:     900
Inclination:       51
6392  deg
RA of node:       181
9078  deg
Eccentricity:     
0001906     
Arg of perigee:    91
5358  deg
Mean anomaly:     268
6014  deg
Mean motion:   15
54888267  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1234
Checksum:              319


Coasting Arc #2 (Orbit 1243)
---------------------------------------

Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3191517
41                 A    =         6777490
30  meter
 Y    =       -3634940
47  meter          E    =           
0009665
 Z    =        4741529
78                 I    =           51
63908
 XDOT =       6767
221421                 Wp   =          116
04010
 YDOT =      -2399
663145  meter/sec      RA   =          177
83661  deg
 ZDOT =       2706
947439                 TA   =          307
17890
                                          MA   =          307
26710
                                          Ha   =            220
468  n
mi
                                          Hp   =            212
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10470857
65                 X    =        -3173665
17
 Y    =      -11925657
73  feet           Y    =        -3670530
37  meter
 Z    =       15556200
08                 Z    =         4726069
88
 XDOT =      22202
170018                 XDOT =        6780
403231
 YDOT =      -7872
910580  feet/sec       YDOT =       -2323
913870  meter/sec
 ZDOT =       8881
061151                 ZDOT =        2739
852143

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7978462
84                 X    =        -2431835
47
 Y    =      -13794245
56  feet           Y    =        -4204486
05  meter
 Z    =       15489301
25                 Z    =         4721139
02
 XDOT =      22264
068726                 XDOT =        6786
088148
 YDOT =      -2712
031633  feet/sec       YDOT =        -826
627242  meter/sec
 ZDOT =       9025
071671                 ZDOT =        2750
841845


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   16217
15377282  
00016717  00000-0  10270-3 0  9010
2 25544  51
6429 178
6971 0001879 108
7092 251
4266 15
54941575 12443


Satellite: ISS
Catalog Number: 25544
Epoch time:      16217
15377282   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:       178
6971  deg
Eccentricity:     
0001879     
Arg of perigee:   108
7092  deg
Mean anomaly:     251
4266  deg
Mean motion:   15
54941575  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1244
Checksum:              327


Coasting Arc #3 (Orbit 1258)
---------------------------------------

Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1143431
19                 A    =         6775192
59  meter
 Y    =        4080714
03  meter          E    =           
0016398
 Z    =       -5300370
79                 I    =           51
66337
 XDOT =      -7510
777570                 Wp   =           88
36990
 YDOT =       1386
097233  meter/sec      RA   =          172
83310  deg
 ZDOT =       -554
156660                 TA   =          176
34253
                                          MA   =          176
33052
                                          Ha   =            220
410  n
mi
                                          Hp   =            212
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3751414
65                 X    =         1123461
00
 Y    =       13388169
40  feet           Y    =         4093388
93  meter
 Z    =      -17389667
96                 Z    =        -5294864
96
 XDOT =     -24641
658694                 XDOT =       -7523
027249
 YDOT =       4547
563100  feet/sec       YDOT =        1302
038200  meter/sec
 ZDOT =      -1818
099278                 ZDOT =        -590
671130

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1352833
09                 X    =          412343
52
 Y    =       13867183
48  feet           Y    =         4226717
53  meter
 Z    =      -17366283
66                 Z    =        -5293243
26
 XDOT =     -24034
445914                 XDOT =       -7325
699115
 YDOT =       -127
816265  feet/sec       YDOT =         -38
958397  meter/sec
 ZDOT =      -1977
720414                 ZDOT =        -602
809182


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   16218
11781671  
00016717  00000-0  10270-3 0  9029
2 25544  51
6429 173
8870 0001839 108
9723 251
1629 15
54913739 12594


Satellite: ISS
Catalog Number: 25544
Epoch time:      16218
11781671   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:       173
8870  deg
Eccentricity:     
0001839     
Arg of perigee:   108
9723  deg
Mean anomaly:     251
1629  deg
Mean motion:   15
54913739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1259
Checksum:              327


Coasting Arc #4 (Orbit 1274)
---------------------------------------

Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         990610
81                 A    =         6775820
94  meter
 Y    =       -4338472
65  meter          E    =           
0006174
 Z    =        5105140
30                 I    =           51
69809
 XDOT =       7484
620599                 Wp   =           69
75164
 YDOT =       -263
231561  meter/sec      RA   =          167
82801  deg
 ZDOT =      -1672
302933                 TA   =           36
39234
                                          MA   =           36
35038
                                          Ha   =            220
315  n
mi
                                          Hp   =            212
749

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3250035
48                 X    =         1014252
97
 Y    =      -14233834
15  feet           Y    =        -4327262
66  meter
 Z    =       16749147
96                 Z    =         5110009
88
 XDOT =      24555
841859                 XDOT =        7495
131029
 YDOT =       -863
620606  feet/sec       YDOT =        -179
474803  meter/sec
 ZDOT =      -5486
558180                 ZDOT =       -1635
919655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5457545
67                 X    =         1663459
92
 Y    =      -13514591
50  feet           Y    =        -4119247
49  meter
 Z    =       16771098
18                 Z    =         5111830
73
 XDOT =      23408
302580                 XDOT =        7134
850626
 YDOT =       2826
289024  feet/sec       YDOT =         861
452895  meter/sec
 ZDOT =      -5327
672804                 ZDOT =       -1623
874671


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   16219
14612557  
00016717  00000-0  10270-3 0  9030
2 25544  51
6431 168
7549 0001826 112
2404 247
8943 15
54952049 12759


Satellite: ISS
Catalog Number: 25544
Epoch time:      16219
14612557   =   yrday
fracday
Element set:     903
Inclination:       51
6431  deg
RA of node:       168
7549  deg
Eccentricity:     
0001826     
Arg of perigee:   112
2404  deg
Mean anomaly:     247
8943  deg
Mean motion:   15
54952049  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1275
Checksum:              313


Coasting Arc #5 (Orbit 1289)
---------------------------------------

Vector Time (GMT): 2016/220/02:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2963247
47                 A    =         6779295
99  meter
 Y    =        4404295
64  meter          E    =           
0010015
 Z    =       -4227146
54                 I    =           51
74109
 XDOT =      -6657
995367                 Wp   =          111
60480
 YDOT =       -966
813135  meter/sec      RA   =          162
83338  deg
 ZDOT =       3663
329600                 TA   =          195
89756
                                          MA   =          195
92902
                                          Ha   =            220
329  n
mi
                                          Hp   =            212
689

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9721940
50                 X    =        -2991743
83
 Y    =       14449788
85  feet           Y    =         4370999
17  meter
 Z    =      -13868591
01                 Z    =        -4241610
38
 XDOT =     -21843
816820                 XDOT =       -6664
483990
 YDOT =      -3171
959104  feet/sec       YDOT =       -1041
303461  meter/sec
 ZDOT =      12018
797900                 ZDOT =        3630
971488

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11674584
60                 X    =        -3558413
39
 Y    =       12854625
43  feet           Y    =         3918089
83  meter
 Z    =      -13932444
90                 Z    =        -4246609
21
 XDOT =     -20267
909090                 XDOT =       -6177
658690
 YDOT =      -5545
716579  feet/sec       YDOT =       -1690
334413  meter/sec
 ZDOT =      11877
667954                 ZDOT =        3620
313192


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   16220
11016195  
00016717  00000-0  10270-3 0  9046
2 25544  51
6431 163
9448 0001866 115
7683 244
3663 15
54951851 12903


Satellite: ISS
Catalog Number: 25544
Epoch time:      16220
11016195   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       163
9448  deg
Eccentricity:     
0001866     
Arg of perigee:   115
7683  deg
Mean anomaly:     244
3663  deg
Mean motion:   15
54951851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1290
Checksum:              303


Coasting Arc #6 (Orbit 1292)
---------------------------------------

Vector Time (GMT): 2016/220/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4670113
83                 A    =         6778825
04  meter
 Y    =       -2149954
72  meter          E    =           
0011514
 Z    =        4410959
02                 I    =           51
74241
 XDOT =       5247
372798                 Wp   =          109
08578
 YDOT =      -4476
338986  meter/sec      RA   =          162
14554  deg
 ZDOT =       3363
009469                 TA   =          306
93491
                                          MA   =          307
04032
                                          Ha   =            220
576  n
mi
                                          Hp   =            212
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15321895
78                 X    =        -4667151
63
 Y    =       -7053657
21  feet           Y    =        -2202162
36  meter
 Z    =       14471650
32                 Z    =         4388280
37
 XDOT =      17215
790019                 XDOT =        5280
702547
 YDOT =     -14686
151529  feet/sec       YDOT =       -4417
472897  meter/sec
 ZDOT =      11033
495634                 ZDOT =        3388
580602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15903394
51                 X    =        -4847354
65
 Y    =        5868815
48  feet           Y    =         1788814
96  meter
 Z    =       14372970
51                 Z    =         4380881
41
 XDOT =       2229
790161                 XDOT =         679
640041
 YDOT =     -21342
033123  feet/sec       YDOT =       -6505
051696  meter/sec
 ZDOT =      11145
859912                 ZDOT =        3397
258101


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   16220
30296886  
00016717  00000-0  10270-3 0  9055
2 25544  51
6419 162
9834 0002054 105
6299 254
5080 15
54936239 12930


Satellite: ISS
Catalog Number: 25544
Epoch time:      16220
30296886   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:       162
9834  deg
Eccentricity:     
0002054     
Arg of perigee:   105
6299  deg
Mean anomaly:     254
5080  deg
Mean motion:   15
54936239  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1293
Checksum:              319


Coasting Arc #7 (Orbit 1307)
---------------------------------------

Vector Time (GMT): 2016/221/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2935841
10                 A    =         6775620
47  meter
 Y    =        3214298
73  meter          E    =           
0015674
 Z    =       -5205894
98                 I    =           51
76304
 XDOT =      -6496
675345                 Wp   =           83
77390
 YDOT =       3842
868443  meter/sec      RA   =          157
15096  deg
 ZDOT =      -1292
737310                 TA   =          173
82515
                                          MA   =          173
80580
                                          Ha   =            220
425  n
mi
                                          Hp   =            212
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9632024
62                 X    =         2924967
50
 Y    =       10545599
49  feet           Y    =         3247068
32  meter
 Z    =      -17079707
95                 Z    =        -5191660
07
 XDOT =     -21314
551657                 XDOT =       -6532
884940
 YDOT =      12607
836099  feet/sec       YDOT =        3770
015780  meter/sec
 ZDOT =      -4241
264142                 ZDOT =       -1324
384213

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14351226
67                 X    =         4374253
89
 Y    =         360379
94  feet           Y    =          109843
80  meter
 Z    =      -17018061
29                 Z    =        -5187105
08
 XDOT =      -5765
139095                 XDOT =       -1757
214396
 YDOT =      23006
151224  feet/sec       YDOT =        7012
274893  meter/sec
 ZDOT =      -4380
071141                 ZDOT =       -1335
045684


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   16221
26699991  
00016717  00000-0  10270-3 0  9066
2 25544  51
6429 158
1727 0001943 109
6557 250
4806 15
54927831 13082


Satellite: ISS
Catalog Number: 25544
Epoch time:      16221
26699991   =   yrday
fracday
Element set:     906
Inclination:       51
6429  deg
RA of node:       158
1727  deg
Eccentricity:     
0001943     
Arg of perigee:   109
6557  deg
Mean anomaly:     250
4806  deg
Mean motion:   15
54927831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1308
Checksum:              332


Coasting Arc #8 (Orbit 1323)
---------------------------------------

Vector Time (GMT): 2016/222/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -988543
57                 A    =         6775217
72  meter
 Y    =       -4156053
93  meter          E    =           
0004954
 Z    =        5254614
76                 I    =           51
78956
 XDOT =       7049
554063                 Wp   =           78
57775
 YDOT =      -2879
140740  meter/sec      RA   =          152
15237  deg
 ZDOT =       -949
273248                 TA   =           20
49023
                                          MA   =           20
47036
                                          Ha   =            220
464  n
mi
                                          Hp   =            212
668

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3243253
19                 X    =         -967520
47
 Y    =      -13635347
53  feet           Y    =        -4166990
82  meter
 Z    =       17239549
73                 Z    =         5249863
86
 XDOT =      23128
458213                 XDOT =        7085
836523
 YDOT =      -9445
999803  feet/sec       YDOT =       -2800
105068  meter/sec
 ZDOT =      -3114
413544                 ZDOT =        -914
940421

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12236264
04                 X    =        -3729613
28
 Y    =       -6885288
83  feet           Y    =        -2098636
04  meter
 Z    =       17219468
88                 Z    =         5248494
11
 XDOT =       8453
503916                 XDOT =        2576
627993
 YDOT =     -22450
042568  feet/sec       YDOT =       -6842
772975  meter/sec
 ZDOT =      -2964
015023                 ZDOT =        -903
431779


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   16222
29529529  
00016717  00000-0  10270-3 0  9070
2 25544  51
6411 153
0408 0002051 111
1878 248
9494 15
54951816 13241


Satellite: ISS
Catalog Number: 25544
Epoch time:      16222
29529529   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       153
0408  deg
Eccentricity:     
0002051     
Arg of perigee:   111
1878  deg
Mean anomaly:     248
9494  deg
Mean motion:   15
54951816  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1324
Checksum:              305


Coasting Arc #9 (Orbit 1338)
---------------------------------------

Vector Time (GMT): 2016/223/05:58:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -936600
21                 A    =         6778014
13  meter
 Y    =        4904425
95  meter          E    =           
0012007
 Z    =       -4595615
37                 I    =           51
82828
 XDOT =      -6847
239691                 Wp   =          110
86534
 YDOT =       1556
999709  meter/sec      RA   =          147
15990  deg
 ZDOT =       3059
394120                 TA   =          189
65816
                                          MA   =          189
68126
                                          Ha   =            220
360  n
mi
                                          Hp   =            212
753

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3072835
34                 X    =         -969049
80
 Y    =       16090636
32  feet           Y    =         4893770
76  meter
 Z    =      -15077478
26                 Z    =        -4600243
99
 XDOT =     -22464
697148                 XDOT =       -6879
002651
 YDOT =       5108
266763  feet/sec       YDOT =        1480
251744  meter/sec
 ZDOT =      10037
382284                 ZDOT =        3026
055049

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9919567
47                 X    =         3023484
16
 Y    =       13012268
62  feet           Y    =         3966139
47  meter
 Z    =      -15098486
39                 Z    =        -4602018
65
 XDOT =     -10400
802584                 XDOT =       -3170
164628
 YDOT =      19397
509342  feet/sec       YDOT =        5912
360847  meter/sec
 ZDOT =       9891
519622                 ZDOT =        3014
935181


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   16223
25931708  
00016717  00000-0  10270-3 0  9084
2 25544  51
6425 148
2298 0001837 112
9099 247
2248 15
54935972 13394


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
25931708   =   yrday
fracday
Element set:     908
Inclination:       51
6425  deg
RA of node:       148
2298  deg
Eccentricity:     
0001837     
Arg of perigee:   112
9099  deg
Mean anomaly:     247
2248  deg
Mean motion:   15
54935972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1339
Checksum:              332


Coasting Arc #10 (Orbit 1340)
---------------------------------------

Vector Time (GMT): 2016/223/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5578860
56                 A    =         6780733
90  meter
 Y    =         -40676
57  meter          E    =           
0007771
 Z    =       -3861281
41                 I    =           51
83792
 XDOT =      -2832
095581                 Wp   =           84
13999
 YDOT =       5778
648576  meter/sec      RA   =          146
63309  deg
 ZDOT =      -4159
158636                 TA   =          142
22914
                                          MA   =          142
17457
                                          Ha   =            220
389  n
mi
                                          Hp   =            212
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18303348
28                 X    =         5597657
07
 Y    =        -133453
31  feet           Y    =           21815
03  meter
 Z    =      -12668246
11                 Z    =        -3834135
27
 XDOT =      -9291
652168                 XDOT =       -2876
300167
 YDOT =      18958
820789  feet/sec       YDOT =        5746
730973  meter/sec
 ZDOT =     -13645
533584                 ZDOT =       -4173
023578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          54758
19                 X    =           16690
30
 Y    =      -18385251
74  feet           Y    =        -5603824
73  meter
 Z    =      -12549675
19                 Z    =        -3825141
00
 XDOT =      17521
110304                 XDOT =        5340
434421
 YDOT =       9394
030631  feet/sec       YDOT =        2863
300536  meter/sec
 ZDOT =     -13707
024729                 ZDOT =       -4177
901138


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   16223
38785389  
00016717  00000-0  10270-3 0  9091
2 25544  51
6400 147
5876 0001871 110
9901 249
1452 15
54951359 13417


Satellite: ISS
Catalog Number: 25544
Epoch time:      16223
38785389   =   yrday
fracday
Element set:     909
Inclination:       51
6400  deg
RA of node:       147
5876  deg
Eccentricity:     
0001871     
Arg of perigee:   110
9901  deg
Mean anomaly:     249
1452  deg
Mean motion:   15
54951359  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1341
Checksum:              322


Coasting Arc #11 (Orbit 1356)
---------------------------------------

Vector Time (GMT): 2016/224/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4412470
27                 A    =         6776626
43  meter
 Y    =       -1447520
05  meter          E    =           
0008338
 Z    =        4930647
67                 I    =           51
85072
 XDOT =       4461
231449                 Wp   =          120
72251
 YDOT =      -5812
274877  meter/sec      RA   =          141
64998  deg
 ZDOT =       2279
030455                 TA   =          307
04933
                                          MA   =          307
12557
                                          Ha   =            220
355  n
mi
                                          Hp   =            212
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14476608
49                 X    =        -4419906
56
 Y    =       -4749081
53  feet           Y    =        -1496904
81  meter
 Z    =       16176665
60                 Z    =         4909195
11
 XDOT =      14636
586120                 XDOT =        4514
823748
 YDOT =     -19069
143298  feet/sec       YDOT =       -5762
086746  meter/sec
 ZDOT =       7477
134040                 ZDOT =        2300
832015

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4646854
36                 X    =        -1416361
21
 Y    =       14613284
05  feet           Y    =         4454128
98  meter
 Z    =       16083194
72                 Z    =         4902157
75
 XDOT =     -18103
081915                 XDOT =       -5517
819368
 YDOT =     -14117
124677  feet/sec       YDOT =       -4302
899602  meter/sec
 ZDOT =       7573
312148                 ZDOT =        2308
345543


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   16224
41613677  
00016717  00000-0  10270-3 0  9108
2 25544  51
6397 142
4561 0001668 115
8867 244
2458 15
54983465 13578


Satellite: ISS
Catalog Number: 25544
Epoch time:      16224
41613677   =   yrday
fracday
Element set:     910
Inclination:       51
6397  deg
RA of node:       142
4561  deg
Eccentricity:     
0001668     
Arg of perigee:   115
8867  deg
Mean anomaly:     244
2458  deg
Mean motion:   15
54983465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1357
Checksum:              330


Coasting Arc #12 (Orbit 1371)
---------------------------------------

Vector Time (GMT): 2016/225/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2926636
13                 A    =         6774946
14  meter
 Y    =        2999087
89  meter          E    =           
0016399
 Z    =       -5337660
92                 I    =           51
86952
 XDOT =      -5535
195241                 Wp   =           92
43434
 YDOT =       5291
485411  meter/sec      RA   =          136
65745  deg
 ZDOT =        -62
644955                 TA   =          176
97475
                                          MA   =          176
96482
                                          Ha   =            220
264  n
mi
                                          Hp   =            212
893

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9601824
57                 X    =         2918809
89
 Y    =        9839527
19  feet           Y    =         3031771
77  meter
 Z    =      -17512010
91                 Z    =        -5323463
17
 XDOT =     -18160
089373                 XDOT =       -5593
650283
 YDOT =      17360
516440  feet/sec       YDOT =        5229
260317  meter/sec
 ZDOT =       -205
528066                 ZDOT =         -89
675248

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9600926
37                 X    =         2926362
36
 Y    =       -9949111
90  feet           Y    =        -3032489
31  meter
 Z    =      -17450479
70                 Z    =        -5318906
21
 XDOT =      17067
611034                 XDOT =        5202
207843
 YDOT =      17034
558999  feet/sec       YDOT =        5192
133583  meter/sec
 ZDOT =       -324
480916                 ZDOT =         -98
901783


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
38014903  
00016717  00000-0  10270-3 0  9113
2 25544  51
6397 137
6441 0001709 117
8422 242
2905 15
54958617 13729


Satellite: ISS
Catalog Number: 25544
Epoch time:      16225
38014903   =   yrday
fracday
Element set:     911
Inclination:       51
6397  deg
RA of node:       137
6441  deg
Eccentricity:     
0001709     
Arg of perigee:   117
8422  deg
Mean anomaly:     242
2905  deg
Mean motion:   15
54958617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1372
Checksum:              306


Coasting Arc #13 (Orbit 1387)
---------------------------------------

Vector Time (GMT): 2016/226/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1297860
33                 A    =         6776365
27  meter
 Y    =       -4409113
43  meter          E    =           
0007069
 Z    =        4974519
35                 I    =           51
89863
 XDOT =       6030
387027                 Wp   =           69
44572
 YDOT =      -4222
910293  meter/sec      RA   =          131
66711  deg
 ZDOT =      -2164
695288                 TA   =           41
58806
                                          MA   =           41
53432
                                          Ha   =            220
247  n
mi
                                          Hp   =            212
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4258071
95                 X    =        -1272623
86
 Y    =      -14465595
24  feet           Y    =        -4423485
95  meter
 Z    =       16320601
55                 Z    =         4968275
96
 XDOT =      19784
734341                 XDOT =        6087
675532
 YDOT =     -13854
692561  feet/sec       YDOT =       -4155
154118  meter/sec
 ZDOT =      -7102
018663                 ZDOT =       -2135
262418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14271581
76                 X    =        -4349978
12
 Y    =        4957057
39  feet           Y    =         1510911
09  meter
 Z    =       16294053
93                 Z    =         4966427
64
 XDOT =     -14300
934841                 XDOT =       -4358
924940
 YDOT =     -18200
447002  feet/sec       YDOT =       -5547
496246  meter/sec
 ZDOT =      -6972
725474                 ZDOT =       -2125
286724


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
40842146  
00016717  00000-0  10270-3 0  9126
2 25544  51
6409 132
5122 0001631 121
8886 238
2426 15
54979659 13885


Satellite: ISS
Catalog Number: 25544
Epoch time:      16226
40842146   =   yrday
fracday
Element set:     912
Inclination:       51
6409  deg
RA of node:       132
5122  deg
Eccentricity:     
0001631     
Arg of perigee:   121
8886  deg
Mean anomaly:     238
2426  deg
Mean motion:   15
54979659  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1388
Checksum:              315


Coasting Arc #14 (Orbit 1402)
---------------------------------------

Vector Time (GMT): 2016/227/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -271422
72                 A    =         6780299
60  meter
 Y    =        5521734
01  meter          E    =           
0008179
 Z    =       -3934283
91                 I    =           51
93256
 XDOT =      -5933
621473                 Wp   =          109
77460
 YDOT =       2613
621118  meter/sec      RA   =          126
68698  deg
 ZDOT =       4081
740238                 TA   =          202
79351
                                          MA   =          202
82983
                                          Ha   =            220
179  n
mi
                                          Hp   =            212
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -890494
48                 X    =         -314037
17
 Y    =       18115925
21  feet           Y    =         5518460
58  meter
 Z    =      -12907755
62                 Z    =        -3935705
80
 XDOT =     -19467
262052                 XDOT =       -5982
233713
 YDOT =       8574
872435  feet/sec       YDOT =        2546
995512  meter/sec
 ZDOT =      13391
536215                 ZDOT =        4052
798561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18130945
35                 X    =         5526312
14
 Y    =        -253622
80  feet           Y    =          -77304
23  meter
 Z    =      -12914889
79                 Z    =        -3936458
41
 XDOT =       9686
317555                 XDOT =        2952
389591
 YDOT =      17696
334486  feet/sec       YDOT =        5393
842751  meter/sec
 ZDOT =      13264
638172                 ZDOT =        4043
061715


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
37242064  
00016717  00000-0  10270-3 0  9137
2 25544  51
6410 127
7008 0001587 122
0314 238
0994 15
54975366 14032


Satellite: ISS
Catalog Number: 25544
Epoch time:      16227
37242064   =   yrday
fracday
Element set:     913
Inclination:       51
6410  deg
RA of node:       127
7008  deg
Eccentricity:     
0001587     
Arg of perigee:   122
0314  deg
Mean anomaly:     238
0994  deg
Mean motion:   15
54975366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1403
Checksum:              293


Coasting Arc #15 (Orbit 1418)
---------------------------------------

Vector Time (GMT): 2016/228/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1678017
94                 A    =         6784540
62  meter
 Y    =       -6147368
23  meter          E    =           
0015362
 Z    =        2307421
93                 I    =           51
96576
 XDOT =       5372
419665                 Wp   =          109
30670
 YDOT =       -587
295660  meter/sec      RA   =          121
72237  deg
 ZDOT =      -5447
130993                 TA   =           45
08197
                                          MA   =           44
95741
                                          Ha   =            220
147  n
mi
                                          Hp   =            212
817

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5505308
21                 X    =         1735426
38
 Y    =      -20168530
94  feet           Y    =        -6128282
55  meter
 Z    =        7570281
91                 Z    =         2315712
54
 XDOT =      17626
048771                 XDOT =        5405
047037
 YDOT =      -1926
823031  feet/sec       YDOT =        -527
035175  meter/sec
 ZDOT =     -17871
164676                 ZDOT =       -5420
954322

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20522771
81                 X    =        -6255340
85
 Y    =       -3915141
69  feet           Y    =        -1193335
19  meter
 Z    =        7607544
25                 Z    =         2318779
49
 XDOT =      -3550
341907                 XDOT =       -1082
144213
 YDOT =     -16047
973421  feet/sec       YDOT =       -4891
422299  meter/sec
 ZDOT =     -17756
673610                 ZDOT =       -5412
234116


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
40068188  
00016717  00000-0  10270-3 0  9146
2 25544  51
6414 122
5688 0001599 124
9547 235
1757 15
54992086 14195


Satellite: ISS
Catalog Number: 25544
Epoch time:      16228
40068188   =   yrday
fracday
Element set:     914
Inclination:       51
6414  deg
RA of node:       122
5688  deg
Eccentricity:     
0001599     
Arg of perigee:   124
9547  deg
Mean anomaly:     235
1757  deg
Mean motion:   15
54992086  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1419
Checksum:              335


Coasting Arc #16 (Orbit 1433)
---------------------------------------

Vector Time (GMT): 2016/229/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2777451
99                 A    =         6786708
08  meter
 Y    =        6175365
86  meter          E    =           
0011384
 Z    =        -385935
37                 I    =           51
98946
 XDOT =      -4451
903030                 Wp   =           50
27663
 YDOT =      -1633
440760  meter/sec      RA   =          116
76968  deg
 ZDOT =       6026
851270                 TA   =          305
58171
                                          MA   =          305
68775
                                          Ha   =            220
072  n
mi
                                          Hp   =            212
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9112375
29                 X    =        -2844425
40
 Y    =       20260386
69  feet           Y    =         6143932
07  meter
 Z    =       -1266192
17                 Z    =         -399589
96
 XDOT =     -14605
981069                 XDOT =       -4462
581885
 YDOT =      -5359
057613  feet/sec       YDOT =       -1683
284608  meter/sec
 ZDOT =      19773
134089                 ZDOT =        6005
199529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21017547
36                 X    =         6406148
44
 Y    =        7184977
65  feet           Y    =         2189981
19  meter
 Z    =       -1326911
40                 Z    =         -404442
60
 XDOT =      -3443
251015                 XDOT =       -1049
502909
 YDOT =      13634
378621  feet/sec       YDOT =        4155
758604  meter/sec
 ZDOT =      19678
782295                 ZDOT =        5998
092844


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
36467068  
00016717  00000-0  10270-3 0  9153
2 25544  51
6416 117
7579 0001552 131
6712 228
4574 15
55005696 14342


Satellite: ISS
Catalog Number: 25544
Epoch time:      16229
36467068   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       117
7579  deg
Eccentricity:     
0001552     
Arg of perigee:   131
6712  deg
Mean anomaly:     228
4574  deg
Mean motion:   15
55005696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1434
Checksum:              319


Coasting Arc #17 (Orbit 1449)
---------------------------------------

Vector Time (GMT): 2016/230/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3584729
92                 A    =         6785655
76  meter
 Y    =       -5520947
91  meter          E    =           
0009406
 Z    =       -1633065
91                 I    =           52
00057
 XDOT =       3305
440903                 Wp   =          140
67022
 YDOT =       3841
112072  meter/sec      RA   =          111
81955  deg
 ZDOT =      -5755
142165                 TA   =           57
12172
                                          MA   =           57
03124
                                          Ha   =            220
077  n
mi
                                          Hp   =            212
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11760924
93                 X    =         3654132
70
 Y    =      -18113346
18  feet           Y    =        -5480473
05  meter
 Z    =       -5357827
80                 Z    =        -1615483
87
 XDOT =      10844
622385                 XDOT =        3290
198363
 YDOT =      12602
073726  feet/sec       YDOT =        3877
990364  meter/sec
 ZDOT =     -18881
700016                 ZDOT =       -5739
122609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19300345
03                 X    =        -5882745
16
 Y    =       -9733283
39  feet           Y    =        -2966704
78  meter
 Z    =       -5280043
56                 Z    =        -1609357
28
 XDOT =      10609
149851                 XDOT =        3233
668875
 YDOT =     -10877
344337  feet/sec       YDOT =       -3315
414554  meter/sec
 ZDOT =     -18812
333589                 ZDOT =       -5733
999278


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
39291921  
00016717  00000-0  10270-3 0  9162
2 25544  51
6425 112
6253 0001476 131
2323 228
8958 15
55013287 14507


Satellite: ISS
Catalog Number: 25544
Epoch time:      16230
39291921   =   yrday
fracday
Element set:     916
Inclination:       51
6425  deg
RA of node:       112
6253  deg
Eccentricity:     
0001476     
Arg of perigee:   131
2323  deg
Mean anomaly:     228
8958  deg
Mean motion:   15
55013287  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1450
Checksum:              293


Coasting Arc #18 (Orbit 1465)
---------------------------------------

Vector Time (GMT): 2016/231/08:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 930011
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4051036
51                 A    =         6781960
07  meter
 Y    =        4249568
76  meter          E    =           
0013606
 Z    =        3384149
60                 I    =           51
99857
 XDOT =      -2081
365135                 Wp   =           93
81722
 YDOT =      -5718
611934  meter/sec      RA   =          106
86289  deg
 ZDOT =       4672
491221                 TA   =          305
50975
                                          MA   =          305
63659
                                          Ha   =            220
091  n
mi
                                          Hp   =            212
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13290802
21                 X    =        -4114693
59
 Y    =       13942154
71  feet           Y    =         4203911
58  meter
 Z    =       11102853
03                 Z    =         3364316
30
 XDOT =      -6828
625771                 XDOT =       -2039
959954
 YDOT =     -18761
850178  feet/sec       YDOT =       -5741
655437  meter/sec
 ZDOT =      15329
695606                 ZDOT =        4662
481498

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15526964
30                 X    =         4732618
72
 Y    =       11483727
53  feet           Y    =         3500240
15  meter
 Z    =       11015435
91                 Z    =         3357504
87
 XDOT =     -16891
590033                 XDOT =       -5148
556642
 YDOT =       8121
379539  feet/sec       YDOT =        2475
396483  meter/sec
 ZDOT =      15286
917472                 ZDOT =        4659
452446


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
42116328  
00016717  00000-0  10270-3 0  9175
2 25544  51
6417 107
4936 0001496 135
6974 224
4299 15
55017846 14662


Satellite: ISS
Catalog Number: 25544
Epoch time:      16231
42116328   =   yrday
fracday
Element set:     917
Inclination:       51
6417  deg
RA of node:       107
4936  deg
Eccentricity:     
0001496     
Arg of perigee:   135
6974  deg
Mean anomaly:     224
4299  deg
Mean motion:   15
55017846  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1466
Checksum:              321
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