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

 
Date: December 7th 2017

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 582 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


341/18:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 7
000/00:00:00 000 0 0 0 0 215 1

342/18:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 5
000/00:00:00 000 0 0 0 0 215 4

344/22:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 3
000/00:00:00 000 0 0 0 0 215 4

348/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 215 4

348/05:14:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

349/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 1
000/00:00:00 000 0 0 0 0 215 6

351/07:21:01 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 6

353/08:42:47 000 0 0 0 0 0 0
N/A 0 0 0 0 219 9
000/00:00:00 000 0 0 0 0 215 6

Coasting Arc #1 (Orbit 823)
---------------------------------------

Vector Time (GMT): 2017/340/14:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2968459
32                 A    =         6787524
26  meter
 Y    =        5708699
46  meter          E    =           
0013900
 Z    =        2136198
31                 I    =           51
28550
 XDOT =      -3644
338262                 Wp   =          122
15769
 YDOT =       3950
707808  meter/sec      RA   =          257
95953  deg
 ZDOT =      -5474
643521                 TA   =           34
02528
                                          MA   =           33
93623
                                          Ha   =            220
855  n
mi
                                          Hp   =            215
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9739039
75                 X    =         2894025
86
 Y    =       18729328
94  feet           Y    =         5741478
39  meter
 Z    =        7008524
64                 Z    =         2150438
02
 XDOT =     -11956
490360                 XDOT =       -3661
652092
 YDOT =      12961
639789  feet/sec       YDOT =        3909
858106  meter/sec
 ZDOT =     -17961
428876                 ZDOT =       -5492
388258

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15662941
60                 X    =        -4774064
60
 Y    =       14122041
30  feet           Y    =         4304398
19  meter
 Z    =        7070805
16                 Z    =         2155181
41
 XDOT =     -14506
813153                 XDOT =       -4421
676649
 YDOT =      -7026
010892  feet/sec       YDOT =       -2141
528120  meter/sec
 ZDOT =     -18040
772565                 ZDOT =       -5498
827478


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   17340
61978750  
00016717  00000-0  10270-3 0  9005
2 25544  51
6417 258
7256 0003025 205
9108 154
1894 15
54072761  8240


Satellite: ISS
Catalog Number: 25544
Epoch time:      17340
61978750   =   yrday
fracday
Element set:     900
Inclination:       51
6417  deg
RA of node:       258
7256  deg
Eccentricity:     
0003025     
Arg of perigee:   205
9108  deg
Mean anomaly:     154
1894  deg
Mean motion:   15
54072761  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             824
Checksum:              309


Coasting Arc #2 (Orbit 838)
---------------------------------------

Vector Time (GMT): 2017/341/14:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2364285
01                 A    =         6789240
48  meter
 Y    =       -6340634
54  meter          E    =           
0007978
 Z    =        -502801
72                 I    =           51
29910
 XDOT =       4350
676506                 Wp   =           44
36086
 YDOT =      -2089
592316  meter/sec      RA   =          252
96334  deg
 ZDOT =       5956
205797                 TA   =          310
19100
                                          MA   =          310
26082
                                          Ha   =            220
674  n
mi
                                          Hp   =            215
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7756840
57                 X    =        -2290764
25
 Y    =      -20802606
76  feet           Y    =        -6366662
47  meter
 Z    =       -1649611
95                 Z    =         -514108
65
 XDOT =      14273
873052                 XDOT =        4344
787240
 YDOT =      -6855
617834  feet/sec       YDOT =       -2040
973523  meter/sec
 ZDOT =      19541
357602                 ZDOT =        5977
325532

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17939167
70                 X    =         5467858
31
 Y    =      -13074347
94  feet           Y    =        -3985061
25  meter
 Z    =       -1698803
02                 Z    =         -517795
16
 XDOT =       9464
796884                 XDOT =        2884
870090
 YDOT =      10461
326084  feet/sec       YDOT =        3188
612190  meter/sec
 ZDOT =      19635
386606                 ZDOT =        5984
865837


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   17341
58433441  
00016717  00000-0  10270-3 0  9016
2 25544  51
6413 253
9176 0003047 214
0132 146
0826 15
54118523  8394


Satellite: ISS
Catalog Number: 25544
Epoch time:      17341
58433441   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:       253
9176  deg
Eccentricity:     
0003047     
Arg of perigee:   214
0132  deg
Mean anomaly:     146
0826  deg
Mean motion:   15
54118523  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             839
Checksum:              284


Coasting Arc #3 (Orbit 841)
---------------------------------------

Vector Time (GMT): 2017/341/18:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2249977
11                 A    =         6780976
86  meter
 Y    =        4615146
59  meter          E    =           
0007137
 Z    =       -4435904
96                 I    =           51
26857
 XDOT =      -4460
917997                 Wp   =           85
62720
 YDOT =      -5306
929997  meter/sec      RA   =          252
12684  deg
 ZDOT =      -3262
721110                 TA   =          151
30861
                                          MA   =          151
26932
                                          Ha   =            220
722  n
mi
                                          Hp   =            215
144

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7381814
67                 X    =        -2279870
27
 Y    =       15141557
06  feet           Y    =         4589819
03  meter
 Z    =      -14553493
96                 Z    =        -4446906
86
 XDOT =     -14635
557734                 XDOT =       -4385
394261
 YDOT =     -17411
187653  feet/sec       YDOT =       -5356
392480  meter/sec
 ZDOT =     -10704
465585                 ZDOT =       -3284
207847

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10342448
73                 X    =        -3152378
37
 Y    =       13241892
67  feet           Y    =         4036128
89  meter
 Z    =      -14603018
76                 Z    =        -4451000
12
 XDOT =      -9558
032334                 XDOT =       -2913
288255
 YDOT =     -19359
725738  feet/sec       YDOT =       -5900
844405  meter/sec
 ZDOT =     -10798
986993                 ZDOT =       -3291
531235


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   17341
77724329  
00016717  00000-0  10270-3 0  9026
2 25544  51
6368 252
9521 0003123 210
4451 149
6529 15
54114866  8424


Satellite: ISS
Catalog Number: 25544
Epoch time:      17341
77724329   =   yrday
fracday
Element set:     902
Inclination:       51
6368  deg
RA of node:       252
9521  deg
Eccentricity:     
0003123     
Arg of perigee:   210
4451  deg
Mean anomaly:     149
6529  deg
Mean motion:   15
54114866  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             842
Checksum:              304


Coasting Arc #4 (Orbit 857)
---------------------------------------

Vector Time (GMT): 2017/342/18:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3114094
59                 A    =         6778274
92  meter
 Y    =       -3172798
73  meter          E    =           
0005681
 Z    =        5116091
11                 I    =           51
27041
 XDOT =       4000
902240                 Wp   =          158
38061
 YDOT =       6366
671731  meter/sec      RA   =          247
10567  deg
 ZDOT =       1507
336584                 TA   =          276
99408
                                          MA   =          277
05870
                                          Ha   =            220
618  n
mi
                                          Hp   =            215
366

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10216845
78                 X    =         3124490
82
 Y    =      -10409444
66  feet           Y    =        -3137916
99  meter
 Z    =       16785075
81                 Z    =         5131243
44
 XDOT =      13126
319686                 XDOT =        3922
089165
 YDOT =      20888
030614  feet/sec       YDOT =        6410
971790  meter/sec
 ZDOT =       4945
330000                 ZDOT =        1526
580668

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11950805
33                 X    =         3642605
47
 Y    =       -8224408
68  feet           Y    =        -2506799
77  meter
 Z    =       16852792
04                 Z    =         5136731
01
 XDOT =       8143
946558                 XDOT =        2482
274911
 YDOT =      22178
825063  feet/sec       YDOT =        6760
105879  meter/sec
 ZDOT =       5029
761566                 ZDOT =        1533
071325


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   17342
80608852  
00016717  00000-0  10270-3 0  9034
2 25544  51
6370 247
8226 0003103 215
7581 144
3364 15
54078843  8582


Satellite: ISS
Catalog Number: 25544
Epoch time:      17342
80608852   =   yrday
fracday
Element set:     903
Inclination:       51
6370  deg
RA of node:       247
8226  deg
Eccentricity:     
0003103     
Arg of perigee:   215
7581  deg
Mean anomaly:     144
3364  deg
Mean motion:   15
54078843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             858
Checksum:              310


Coasting Arc #5 (Orbit 857)
---------------------------------------

Vector Time (GMT): 2017/342/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4715106
94                 A    =         6781165
94  meter
 Y    =        2123550
42  meter          E    =           
0006907
 Z    =        4380927
49                 I    =           51
28049
 XDOT =          8
891851                 Wp   =           85
95231
 YDOT =       6901
042485  meter/sec      RA   =          247
02554  deg
 ZDOT =      -3349
631055                 TA   =           38
10475
                                          MA   =           38
05593
                                          Ha   =            220
547  n
mi
                                          Hp   =            215
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15469510
96                 X    =         4669730
03
 Y    =        6967028
94  feet           Y    =         2176023
98  meter
 Z    =       14373121
67                 Z    =         4403721
90
 XDOT =         29
172738                 XDOT =         -52
007281
 YDOT =      22641
215502  feet/sec       YDOT =        6900
801619  meter/sec
 ZDOT =     -10989
603198                 ZDOT =       -3349
735348

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14227730
00                 X    =         4336612
10
 Y    =        9083413
29  feet           Y    =         2768624
37  meter
 Z    =       14473948
67                 Z    =         4411659
56
 XDOT =      -2456
162812                 XDOT =        -748
638425
 YDOT =      21387
196860  feet/sec       YDOT =        6518
817603  meter/sec
 ZDOT =     -10991
108416                 ZDOT =       -3350
089845


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   17342
80608749  
00016717  00000-0  10270-3 0  9040
2 25544  51
6371 247
8224 0003277 215
3253 144
7683 15
54094135  8585


Satellite: ISS
Catalog Number: 25544
Epoch time:      17342
80608749   =   yrday
fracday
Element set:     904
Inclination:       51
6371  deg
RA of node:       247
8224  deg
Eccentricity:     
0003277     
Arg of perigee:   215
3253  deg
Mean anomaly:     144
7683  deg
Mean motion:   15
54094135  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             858
Checksum:              319


Coasting Arc #6 (Orbit 872)
---------------------------------------

Vector Time (GMT): 2017/343/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4806153
23                 A    =         6784856
88  meter
 Y    =       -3549839
77  meter          E    =           
0003389
 Z    =       -3219276
21                 I    =           51
30732
 XDOT =       1174
757493                 Wp   =          126
09927
 YDOT =      -5896
592771  meter/sec      RA   =          242
01509  deg
 ZDOT =       4749
793032                 TA   =          196
47648
                                          MA   =          196
48750
                                          Ha   =            220
647  n
mi
                                          Hp   =            215
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15768219
25                 X    =        -4750463
10
 Y    =      -11646455
92  feet           Y    =        -3603273
92  meter
 Z    =      -10561929
82                 Z    =        -3242487
91
 XDOT =       3854
191250                 XDOT =        1217
535304
 YDOT =     -19345
776808  feet/sec       YDOT =       -5883
216865  meter/sec
 ZDOT =      15583
310472                 ZDOT =        4755
603266

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14117592
49                 X    =        -4303042
19
 Y    =      -13520169
65  feet           Y    =        -4120947
71  meter
 Z    =      -10664409
52                 Z    =        -3250512
02
 XDOT =       5156
806983                 XDOT =        1571
794769
 YDOT =     -17693
490882  feet/sec       YDOT =       -5392
976021  meter/sec
 ZDOT =      15609
971281                 ZDOT =        4757
919246


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   17343
77062386  
00016717  00000-0  10270-3 0  9059
2 25544  51
6375 243
0136 0003184 214
8996 145
1949 15
54126468  8736


Satellite: ISS
Catalog Number: 25544
Epoch time:      17343
77062386   =   yrday
fracday
Element set:     905
Inclination:       51
6375  deg
RA of node:       243
0136  deg
Eccentricity:     
0003184     
Arg of perigee:   214
8996  deg
Mean anomaly:     145
1949  deg
Mean motion:   15
54126468  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             873
Checksum:              329


Coasting Arc #7 (Orbit 888)
---------------------------------------

Vector Time (GMT): 2017/344/18:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4636343
42                 A    =         6788033
35  meter
 Y    =        4646620
96  meter          E    =           
0013386
 Z    =        1698946
26                 I    =           51
33317
 XDOT =      -2463
957358                 Wp   =          128
93810
 YDOT =       4540
283563  meter/sec      RA   =          237
01664  deg
 ZDOT =      -5671
759081                 TA   =           32
34355
                                          MA   =           32
26155
                                          Ha   =            220
421  n
mi
                                          Hp   =            215
382

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15211100
47                 X    =         4575786
41
 Y    =       15244819
43  feet           Y    =         4698129
06  meter
 Z    =        5573970
67                 Z    =         1721321
33
 XDOT =      -8083
849599                 XDOT =       -2486
994208
 YDOT =      14895
943449  feet/sec       YDOT =        4512
601320  meter/sec
 ZDOT =     -18608
133468                 ZDOT =       -5683
784030

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13438092
33                 X    =         4095930
54
 Y    =       16795553
71  feet           Y    =         5119284
77  meter
 Z    =        5672591
65                 Z    =         1729005
94
 XDOT =      -8299
206455                 XDOT =       -2529
598127
 YDOT =      12967
055744  feet/sec       YDOT =        3952
358591  meter/sec
 ZDOT =     -18662
166380                 ZDOT =       -5688
228313


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   17344
79945727  
00016717  00000-0  10270-3 0  9062
2 25544  51
6364 237
8849 0003234 221
9918 138
0987 15
54139244  8891


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
79945727   =   yrday
fracday
Element set:     906
Inclination:       51
6364  deg
RA of node:       237
8849  deg
Eccentricity:     
0003234     
Arg of perigee:   221
9918  deg
Mean anomaly:     138
0987  deg
Mean motion:   15
54139244  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             889
Checksum:              357


Coasting Arc #8 (Orbit 891)
---------------------------------------

Vector Time (GMT): 2017/344/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3260816
10                 A    =         6777303
08  meter
 Y    =       -2727924
73  meter          E    =           
0003372
 Z    =        5278015
13                 I    =           51
30519
 XDOT =       4525
850002                 Wp   =          176
41411
 YDOT =       6178
624125  meter/sec      RA   =          236
13856  deg
 ZDOT =        393
960917                 TA   =          269
79272
                                          MA   =          269
83136
                                          Ha   =            220
321  n
mi
                                          Hp   =            215
424

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10698215
56                 X    =         3265440
05
 Y    =       -8949884
29  feet           Y    =        -2691434
40  meter
 Z    =       17316322
61                 Z    =         5293866
34
 XDOT =      14848
589245                 XDOT =        4454
508923
 YDOT =      20271
076527  feet/sec       YDOT =        6228
836367  meter/sec
 ZDOT =       1292
522695                 ZDOT =         415
773121

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2123322
51                 X    =         -647188
70
 Y    =      -13696296
18  feet           Y    =        -4174631
08  meter
 Z    =       17387071
23                 Z    =         5299579
31
 XDOT =      24035
433852                 XDOT =        7326
000238
 YDOT =      -1949
848507  feet/sec       YDOT =        -594
313825  meter/sec
 ZDOT =       1388
424419                 ZDOT =         423
191763


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   17344
99236219  
00016717  00000-0  10270-3 0  9074
2 25544  51
6410 236
9248 0003407 222
6026 137
4863 15
54164183  8926


Satellite: ISS
Catalog Number: 25544
Epoch time:      17344
99236219   =   yrday
fracday
Element set:     907
Inclination:       51
6410  deg
RA of node:       236
9248  deg
Eccentricity:     
0003407     
Arg of perigee:   222
6026  deg
Mean anomaly:     137
4863  deg
Mean motion:   15
54164183  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             892
Checksum:              314


Coasting Arc #9 (Orbit 906)
---------------------------------------

Vector Time (GMT): 2017/345/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4284633
30                 A    =         6778039
11  meter
 Y    =        1215260
46  meter          E    =           
0012084
 Z    =       -5120194
03                 I    =           51
32668
 XDOT =      -3690
396396                 Wp   =          114
55961
 YDOT =      -6533
876167  meter/sec      RA   =          231
11678  deg
 ZDOT =       1535
307048                 TA   =          170
32895
                                          MA   =          170
30567
                                          Ha   =            220
340  n
mi
                                          Hp   =            215
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14057195
88                 X    =        -4273032
69
 Y    =        3987075
01  feet           Y    =         1167411
83  meter
 Z    =      -16798536
83                 Z    =        -5140979
35
 XDOT =     -12107
599724                 XDOT =       -3624
516374
 YDOT =     -21436
601599  feet/sec       YDOT =       -6574
776406  meter/sec
 ZDOT =       5037
096613                 ZDOT =        1517
539892

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3623396
41                 X    =        -1104411
23
 Y    =       14044877
12  feet           Y    =         4280878
54  meter
 Z    =      -16890967
65                 Z    =        -5148366
94
 XDOT =     -23608
214905                 XDOT =       -7195
783903
 YDOT =       -118
393652  feet/sec       YDOT =         -36
086385  meter/sec
 ZDOT =       4959
182275                 ZDOT =        1511
558758


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   17345
95688967  
00016717  00000-0  10270-3 0  9083
2 25544  51
6410 232
1172 0003282 226
9496 133
1382 15
54154111  9075


Satellite: ISS
Catalog Number: 25544
Epoch time:      17345
95688967   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:       232
1172  deg
Eccentricity:     
0003282     
Arg of perigee:   226
9496  deg
Mean anomaly:     133
1382  deg
Mean motion:   15
54154111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             907
Checksum:              312


Coasting Arc #10 (Orbit 922)
---------------------------------------

Vector Time (GMT): 2017/346/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5139474
20                 A    =         6780825
03  meter
 Y    =         254451
77  meter          E    =           
0006208
 Z    =        4411413
26                 I    =           51
35800
 XDOT =       2526
493576                 Wp   =           78
14134
 YDOT =       6441
791799  meter/sec      RA   =          226
10100  deg
 ZDOT =      -3309
822574                 TA   =           45
41999
                                          MA   =           45
36934
                                          Ha   =            220
068  n
mi
                                          Hp   =            215
507

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16861791
99                 X    =         5114818
21
 Y    =         834815
50  feet           Y    =          311786
81  meter
 Z    =       14473140
60                 Z    =         4436319
57
 XDOT =       8289
020920                 XDOT =        2470
349588
 YDOT =      21134
487530  feet/sec       YDOT =        6469
731013  meter/sec
 ZDOT =     -10858
997946                 ZDOT =       -3297
685609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8966306
04                 X    =         2732930
08
 Y    =      -14191933
26  feet           Y    =        -4325701
26  meter
 Z    =       14583659
74                 Z    =         4445099
49
 XDOT =      21479
451946                 XDOT =        6546
936953
 YDOT =       2448
735528  feet/sec       YDOT =         746
374589  meter/sec
 ZDOT =     -10806
046695                 ZDOT =       -3293
683032


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   17346
98571320  
00016717  00000-0  10270-3 0  9092
2 25544  51
6414 226
9884 0003189 232
6453 127
4409 15
54168542  9230


Satellite: ISS
Catalog Number: 25544
Epoch time:      17346
98571320   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       226
9884  deg
Eccentricity:     
0003189     
Arg of perigee:   232
6453  deg
Mean anomaly:     127
4409  deg
Mean motion:   15
54168542  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             923
Checksum:              326


Coasting Arc #11 (Orbit 937)
---------------------------------------

Vector Time (GMT): 2017/347/22:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5746470
47                 A    =         6784663
52  meter
 Y    =       -1566485
91  meter          E    =           
0002403
 Z    =       -3252239
60                 I    =           51
39287
 XDOT =      -1058
490487                 Wp   =          125
59801
 YDOT =      -5935
318136  meter/sec      RA   =          221
09733  deg
 ZDOT =       4730
199483                 TA   =          196
57513
                                          MA   =          196
58299
                                          Ha   =            220
171  n
mi
                                          Hp   =            215
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18853249
57                 X    =        -5712728
57
 Y    =       -5139389
48  feet           Y    =        -1630558
02  meter
 Z    =      -10670077
44                 Z    =        -3280072
60
 XDOT =      -3472
737817                 XDOT =       -1015
018713
 YDOT =     -19472
828529  feet/sec       YDOT =       -5946
912117  meter/sec
 ZDOT =      15519
027176                 ZDOT =        4725
162845

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13465938
40                 X    =        -4104418
03
 Y    =       14066969
27  feet           Y    =         4287612
23  meter
 Z    =      -10793413
50                 Z    =        -3289832
43
 XDOT =     -17797
841520                 XDOT =       -5424
782095
 YDOT =      -5149
080324  feet/sec       YDOT =       -1569
439683  meter/sec
 ZDOT =      15497
512617                 ZDOT =        4723
641846


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   17347
95023301  
00016717  00000-0  10270-3 0  9103
2 25544  51
6401 222
1812 0003255 235
2004 124
8843 15
54155278  9381


Satellite: ISS
Catalog Number: 25544
Epoch time:      17347
95023301   =   yrday
fracday
Element set:     910
Inclination:       51
6401  deg
RA of node:       222
1812  deg
Eccentricity:     
0003255     
Arg of perigee:   235
2004  deg
Mean anomaly:     124
8843  deg
Mean motion:   15
54155278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             938
Checksum:              278


Coasting Arc #12 (Orbit 939)
---------------------------------------

Vector Time (GMT): 2017/348/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905672
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2663173
64                 A    =         6777344
25  meter
 Y    =        3295561
59  meter          E    =           
0012453
 Z    =       -5300245
91                 I    =           51
37116
 XDOT =      -5875
261749                 Wp   =           96
71174
 YDOT =      -4913
157238  meter/sec      RA   =          220
52814  deg
 ZDOT =       -104
420653                 TA   =          172
29792
                                          MA   =          172
27878
                                          Ha   =            220
220  n
mi
                                          Hp   =            215
447

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8737446
34                 X    =        -2674081
31
 Y    =       10812209
94  feet           Y    =         3265719
50  meter
 Z    =      -17389258
23                 Z    =        -5313209
20
 XDOT =     -19275
793141                 XDOT =       -5819
377614
 YDOT =     -16119
282277  feet/sec       YDOT =       -4978
545958  meter/sec
 ZDOT =       -342
587445                 ZDOT =        -132
825710

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12630138
52                 X    =         3849666
22
 Y    =        5630748
54  feet           Y    =         1716252
16  meter
 Z    =      -17447275
61                 Z    =        -5317929
61
 XDOT =     -10350
471830                 XDOT =       -3154
823814
 YDOT =      21783
293447  feet/sec       YDOT =        6639
547843  meter/sec
 ZDOT =       -467
988866                 ZDOT =        -142
643006


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   17348
07883599  
00016717  00000-0  10270-3 0  9111
2 25544  51
6403 221
5408 0002993 236
2792 123
8076 15
54134703  9400


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
07883599   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       221
5408  deg
Eccentricity:     
0002993     
Arg of perigee:   236
2792  deg
Mean anomaly:     123
8076  deg
Mean motion:   15
54134703  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             940
Checksum:              315


Coasting Arc #13 (Orbit 942)
---------------------------------------

Vector Time (GMT): 2017/348/05:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 890441
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -78955
55                 A    =         6779966
81  meter
 Y    =       -4915969
08  meter          E    =           
0006868
 Z    =        4666842
94                 I    =           51
38099
 XDOT =       6641
709653                 Wp   =          137
56809
 YDOT =       2586
708550  meter/sec      RA   =          219
76945  deg
 ZDOT =       2829
744796                 TA   =          284
21181
                                          MA   =          284
28809
                                          Ha   =            220
094  n
mi
                                          Hp   =            215
564

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -259040
53                 X    =          -46647
46
 Y    =      -16128507
48  feet           Y    =        -4916671
67  meter
 Z    =       15311164
50                 Z    =         4666537
55
 XDOT =      21790
386000                 XDOT =        6598
545106
 YDOT =       8486
576609  feet/sec       YDOT =        2660
739160  meter/sec
 ZDOT =       9283
939618                 ZDOT =        2861
903817

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4956693
74                 X    =        -1510800
25
 Y    =       15350803
48  feet           Y    =         4678924
90  meter
 Z    =       15310507
30                 Z    =         4666642
62
 XDOT =     -16616
776344                 XDOT =       -5064
793430
 YDOT =     -14791
329749  feet/sec       YDOT =       -4508
397307  meter/sec
 ZDOT =       9426
339783                 ZDOT =        2873
148366


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   17348
27173863  
00016717  00000-0  10270-3 0  9120
2 25544  51
6373 220
5798 0003035 240
6394 119
4456 15
54170632  9439


Satellite: ISS
Catalog Number: 25544
Epoch time:      17348
27173863   =   yrday
fracday
Element set:     912
Inclination:       51
6373  deg
RA of node:       220
5798  deg
Eccentricity:     
0003035     
Arg of perigee:   240
6394  deg
Mean anomaly:     119
4456  deg
Mean motion:   15
54170632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             943
Checksum:              313


Coasting Arc #14 (Orbit 957)
---------------------------------------

Vector Time (GMT): 2017/349/05:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 890441
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1465981
03                 A    =         6777642
03  meter
 Y    =        4065613
35  meter          E    =           
0011619
 Z    =       -5231086
99                 I    =           51
39938
 XDOT =      -6655
342244                 Wp   =           86
90724
 YDOT =      -3662
763083  meter/sec      RA   =          214
75458  deg
 ZDOT =       -982
866429                 TA   =          173
65032
                                          MA   =          173
63558
                                          Ha   =            220
096  n
mi
                                          Hp   =            215
510

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4809649
05                 X    =        -1485924
55
 Y    =       13338626
47  feet           Y    =         4049108
65  meter
 Z    =      -17162358
89                 Z    =        -5238256
46
 XDOT =     -21835
112349                 XDOT =       -6609
115274
 YDOT =     -12016
939248  feet/sec       YDOT =       -3736
929120  meter/sec
 ZDOT =      -3224
627392                 ZDOT =       -1015
084358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8624856
57                 X    =         2628856
28
 Y    =      -11204914
90  feet           Y    =        -3415258
06  meter
 Z    =      -17194765
89                 Z    =        -5240964
64
 XDOT =      16155
729441                 XDOT =        4924
266334
 YDOT =      17596
414468  feet/sec       YDOT =        5363
387130  meter/sec
 ZDOT =      -3367
155676                 ZDOT =       -1026
309050


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   17349
23625378  
00016717  00000-0  10270-3 0  9131
2 25544  51
6377 215
7709 0002886 244
1368 115
9487 15
54149881  9587


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
23625378   =   yrday
fracday
Element set:     913
Inclination:       51
6377  deg
RA of node:       215
7709  deg
Eccentricity:     
0002886     
Arg of perigee:   244
1368  deg
Mean anomaly:     115
9487  deg
Mean motion:   15
54149881  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             958
Checksum:              352


Coasting Arc #15 (Orbit 961)
---------------------------------------

Vector Time (GMT): 2017/349/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 911610
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6078439
12                 A    =         6788347
94  meter
 Y    =        2622666
03  meter          E    =           
0012337
 Z    =        1470390
42                 I    =           51
44511
 XDOT =       -760
016372                 Wp   =          129
50656
 YDOT =       5005
801551  meter/sec      RA   =          213
53510  deg
 ZDOT =      -5762
153630                 TA   =           34
39629
                                          MA   =           34
31649
                                          Ha   =            220
057  n
mi
                                          Hp   =            215
599

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19942385
56                 X    =         6041517
50
 Y    =        8604547
35  feet           Y    =         2690432
73  meter
 Z    =        4824115
55                 Z    =         1499828
43
 XDOT =      -2493
492035                 XDOT =        -787
946117
 YDOT =      16423
233434  feet/sec       YDOT =        4997
146848  meter/sec
 ZDOT =     -18904
703511                 ZDOT =       -5765
913007

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15323651
37                 X    =        -4670648
94
 Y    =       15350836
34  feet           Y    =         4678934
92  meter
 Z    =        4954452
56                 Z    =         1510117
14
 XDOT =     -13280
397412                 XDOT =       -4047
865131
 YDOT =      -7124
412170  feet/sec       YDOT =       -2171
520829  meter/sec
 ZDOT =     -18922
102412                 ZDOT =       -5767
456815


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   17349
49345760  
00016717  00000-0  10270-3 0  9144
2 25544  51
6413 214
4911 0002956 245
1892 114
8953 15
54134322  9625


Satellite: ISS
Catalog Number: 25544
Epoch time:      17349
49345760   =   yrday
fracday
Element set:     914
Inclination:       51
6413  deg
RA of node:       214
4911  deg
Eccentricity:     
0002956     
Arg of perigee:   245
1892  deg
Mean anomaly:     114
8953  deg
Mean motion:   15
54134322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             962
Checksum:              313


Coasting Arc #16 (Orbit 977)
---------------------------------------

Vector Time (GMT): 2017/350/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 911610
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5865244
17                 A    =         6789153
05  meter
 Y    =       -3400927
46  meter          E    =           
0009833
 Z    =         231200
34                 I    =           51
47545
 XDOT =       2578
009682                 Wp   =           40
17648
 YDOT =      -4029
413094  meter/sec      RA   =          208
55135  deg
 ZDOT =       5993
378718                 TA   =          322
32027
                                          MA   =          322
38910
                                          Ha   =            219
894  n
mi
                                          Hp   =            215
649

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19242927
08                 X    =        -5827901
24
 Y    =      -11157898
51  feet           Y    =        -3466307
86  meter
 Z    =         758531
31                 Z    =          202798
93
 XDOT =       8458
037015                 XDOT =        2593
762930
 YDOT =     -13219
859233  feet/sec       YDOT =       -4000
496540  meter/sec
 ZDOT =      19663
316004                 ZDOT =        6005
939856

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17214058
06                 X    =         5246844
90
 Y    =      -14093969
26  feet           Y    =        -4295841
83  meter
 Z    =         632887
75                 Z    =          192904
19
 XDOT =       8417
067027                 XDOT =        2565
522030
 YDOT =      11189
787039  feet/sec       YDOT =        3410
647090  meter/sec
 ZDOT =      19719
662944                 ZDOT =        6010
553265


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   17350
52226472  
00016717  00000-0  10270-3 0  9159
2 25544  51
6406 209
3615 0003012 253
1280 106
9542 15
54184051  9782


Satellite: ISS
Catalog Number: 25544
Epoch time:      17350
52226472   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:       209
3615  deg
Eccentricity:     
0003012     
Arg of perigee:   253
1280  deg
Mean anomaly:     106
9542  deg
Mean motion:   15
54184051  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             978
Checksum:              285


Coasting Arc #17 (Orbit 990)
---------------------------------------

Vector Time (GMT): 2017/351/07:21:01
000
Vector Time (MET): N/A
Weight (LBS)     : 911610
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -494411
05                 A    =         6778620
36  meter
 Y    =       -4574357
13  meter          E    =           
0004748
 Z    =        4977392
68                 I    =           51
46289
 XDOT =       7238
393707                 Wp   =          151
87815
 YDOT =       1468
615632  meter/sec      RA   =          204
32858  deg
 ZDOT =       2063
786480                 TA   =          277
97131
                                          MA   =          278
02519
                                          Ha   =            219
867  n
mi
                                          Hp   =            215
625

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1622083
48                 X    =         -467400
48
 Y    =      -15007733
35  feet           Y    =        -4579735
49  meter
 Z    =       16330028
48                 Z    =         4975056
08
 XDOT =      23748
010849                 XDOT =        7211
408358
 YDOT =       4818
292757  feet/sec       YDOT =        1549
409189  meter/sec
 ZDOT =       6770
953019                 ZDOT =        2098
883184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5676779
70                 X    =         1730282
45
 Y    =       13998402
40  feet           Y    =         4266713
05  meter
 Z    =       16320292
52                 Z    =         4974425
16
 XDOT =     -23107
908003                 XDOT =       -7043
290359
 YDOT =       1276
644245  feet/sec       YDOT =         389
121166  meter/sec
 ZDOT =       6926
620320                 ZDOT =        2111
233874


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   17351
35817035  
00016717  00000-0  10270-3 0  9163
2 25544  51
6385 205
1940 0003027 254
7729 105
3089 15
54199862  9914


Satellite: ISS
Catalog Number: 25544
Epoch time:      17351
35817035   =   yrday
fracday
Element set:     916
Inclination:       51
6385  deg
RA of node:       205
1940  deg
Eccentricity:     
0003027     
Arg of perigee:   254
7729  deg
Mean anomaly:     105
3089  deg
Mean motion:   15
54199862  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             991
Checksum:              321


Coasting Arc #18 (Orbit 1005)
---------------------------------------

Vector Time (GMT): 2017/352/07:21:01
000
Vector Time (MET): N/A
Weight (LBS)     : 911610
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1246517
14                 A    =         6777200
92  meter
 Y    =        4038852
58  meter          E    =           
0011980
 Z    =       -5307950
39                 I    =           51
48888
 XDOT =      -7263
872591                 Wp   =           91
07543
 YDOT =      -2427
028768  meter/sec      RA   =          199
31744  deg
 ZDOT =       -141
392945                 TA   =          177
57575
                                          MA   =          177
56994
                                          Ha   =            219
868  n
mi
                                          Hp   =            215
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4089623
16                 X    =        -1265804
54
 Y    =       13250828
68  feet           Y    =         4024805
95  meter
 Z    =      -17414535
39                 Z    =        -5314051
98
 XDOT =     -23831
602989                 XDOT =       -7235
506218
 YDOT =      -7962
692809  feet/sec       YDOT =       -2508
099733  meter/sec
 ZDOT =       -463
887614                 ZDOT =        -176
610073

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =          51798
54                 X    =           15788
20
 Y    =      -13832657
47  feet           Y    =        -4216194
00  meter
 Z    =      -17442202
42                 Z    =        -5316383
30
 XDOT =      24099
416688                 XDOT =        7345
502206
 YDOT =        869
953401  feet/sec       YDOT =         265
161797  meter/sec
 ZDOT =       -619
981177                 ZDOT =        -188
970263


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   17352
32267407  
00016717  00000-0  10270-3 0  9174
2 25544  51
6390 200
3851 0002919 259
9728 100
1096 15
54185753 10066


Satellite: ISS
Catalog Number: 25544
Epoch time:      17352
32267407   =   yrday
fracday
Element set:     917
Inclination:       51
6390  deg
RA of node:       200
3851  deg
Eccentricity:     
0002919     
Arg of perigee:   259
9728  deg
Mean anomaly:     100
1096  deg
Mean motion:   15
54185753  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1006
Checksum:              304


Coasting Arc #19 (Orbit 1021)
---------------------------------------

Vector Time (GMT): 2017/353/07:21:01
000
Vector Time (MET): N/A
Weight (LBS)     : 911610
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2963389
54                 A    =         6778142
05  meter
 Y    =       -3396045
28  meter          E    =           
0003147
 Z    =        5061978
73                 I    =           51
52347
 XDOT =       6736
642654                 Wp   =           26
94499
 YDOT =       3193
239099  meter/sec      RA   =          194
30902  deg
 ZDOT =      -1798
265388                 TA   =           80
50181
                                          MA   =           80
46625
                                          Ha   =            219
700  n
mi
                                          Hp   =            215
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9722406
64                 X    =         2976556
20
 Y    =      -11141880
82  feet           Y    =        -3362833
60  meter
 Z    =       16607541
77                 Z    =         5076405
53
 XDOT =      22101
845978                 XDOT =        6709
169400
 YDOT =      10476
506230  feet/sec       YDOT =        3268
419440  meter/sec
 ZDOT =      -5899
820828                 ZDOT =       -1765
607239

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5824864
05                 X    =        -1775418
56
 Y    =       13512547
39  feet           Y    =         4118624
44  meter
 Z    =       16672107
38                 Z    =         5081658
33
 XDOT =     -23278
624200                 XDOT =       -7095
324656
 YDOT =      -2921
009927  feet/sec       YDOT =        -890
323826  meter/sec
 ZDOT =      -5755
175669                 ZDOT =       -1754
177544


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   17353
35147120  
00016717  00000-0  10270-3 0  9188
2 25544  51
6389 195
2567 0002962 266
1338  93
9476 15
54206334 10223


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
35147120   =   yrday
fracday
Element set:     918
Inclination:       51
6389  deg
RA of node:       195
2567  deg
Eccentricity:     
0002962     
Arg of perigee:   266
1338  deg
Mean anomaly:      93
9476  deg
Mean motion:   15
54206334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1022
Checksum:              315


Coasting Arc #20 (Orbit 1022)
---------------------------------------

Vector Time (GMT): 2017/353/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 926842
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1817028
87                 A    =         6779360
78  meter
 Y    =       -4404316
92  meter          E    =           
0005198
 Z    =        4821423
04                 I    =           51
53023
 XDOT =       7243
966401                 Wp   =          138
27370
 YDOT =       -238
923714  meter/sec      RA   =          194
05930  deg
 ZDOT =       2506
390385                 TA   =          287
02553
                                          MA   =          287
08247
                                          Ha   =            219
911  n
mi
                                          Hp   =            215
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5961380
82                 X    =        -1791063
66
 Y    =      -14449858
65  feet           Y    =        -4424491
56  meter
 Z    =       15818317
08                 Z    =         4812659
04
 XDOT =      23766
293968                 XDOT =        7233
924922
 YDOT =       -783
870452  feet/sec       YDOT =        -157
973169  meter/sec
 ZDOT =       8223
065569                 ZDOT =        2541
554885

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13670734
03                 X    =         4166839
73
 Y    =        7658881
75  feet           Y    =         2334427
16  meter
 Z    =       15779993
43                 Z    =         4809742
00
 XDOT =     -17652
743245                 XDOT =       -5380
556141
 YDOT =      14208
630989  feet/sec       YDOT =        4330
790725  meter/sec
 ZDOT =       8379
324143                 ZDOT =        2554
017999


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   17353
41577135  
00016717  00000-0  10270-3 0  9199
2 25544  51
6402 194
9358 0002891 264
6116  95
4707 15
54180471 10239


Satellite: ISS
Catalog Number: 25544
Epoch time:      17353
41577135   =   yrday
fracday
Element set:     919
Inclination:       51
6402  deg
RA of node:       194
9358  deg
Eccentricity:     
0002891     
Arg of perigee:   264
6116  deg
Mean anomaly:      95
4707  deg
Mean motion:   15
54180471  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1023
Checksum:              312


Coasting Arc #21 (Orbit 1037)
---------------------------------------

Vector Time (GMT): 2017/354/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 926842
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          23604
82                 A    =         6777263
85  meter
 Y    =        4253454
89  meter          E    =           
0011684
 Z    =       -5286422
25                 I    =           51
55496
 XDOT =      -7601
642279                 Wp   =           84
06923
 YDOT =       -719
047312  meter/sec      RA   =          189
05459  deg
 ZDOT =       -612
473793                 TA   =          180
07123
                                          MA   =          180
07139
                                          Ha   =            219
777  n
mi
                                          Hp   =            215
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          77443
62                 X    =            1718
52
 Y    =       13954904
51  feet           Y    =         4253597
08  meter
 Z    =      -17343905
03                 Z    =        -5286360
27
 XDOT =     -24939
771258                 XDOT =       -7590
061646
 YDOT =      -2359
079109  feet/sec       YDOT =        -803
989252  meter/sec
 ZDOT =      -2009
428456                 ZDOT =        -649
372020

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8921467
88                 X    =        -2719263
41
 Y    =      -10730419
98  feet           Y    =        -3270632
01  meter
 Z    =      -17344217
97                 Z    =        -5286517
64
 XDOT =      20084
472412                 XDOT =        6121
747191
 YDOT =     -13185
715038  feet/sec       YDOT =       -4019
005943  meter/sec
 ZDOT =      -2173
283447                 ZDOT =        -662
416795


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   17354
38026498  
00016717  00000-0  10270-3 0  9209
2 25544  51
6396 190
1278 0002980 269
9399  90
1402 15
54209893 10380


Satellite: ISS
Catalog Number: 25544
Epoch time:      17354
38026498   =   yrday
fracday
Element set:     920
Inclination:       51
6396  deg
RA of node:       190
1278  deg
Eccentricity:     
0002980     
Arg of perigee:   269
9399  deg
Mean anomaly:      90
1402  deg
Mean motion:   15
54209893  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1038
Checksum:              333


Coasting Arc #22 (Orbit 1053)
---------------------------------------

Vector Time (GMT): 2017/355/08:42:47
000
Vector Time (MET): N/A
Weight (LBS)     : 926842
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1806755
61                 A    =         6777601
08  meter
 Y    =       -3985952
18  meter          E    =           
0002596
 Z    =        5175501
85                 I    =           51
58950
 XDOT =       7379
531844                 Wp   =            7
84370
 YDOT =       1592
958225  meter/sec      RA   =          184
04971  deg
 ZDOT =      -1346
751198                 TA   =           95
12234
                                          MA   =           95
09270
                                          Ha   =            219
615  n
mi
                                          Hp   =            215
656

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5927675
89                 X    =         1826053
44
 Y    =      -13077270
93  feet           Y    =        -3965640
44  meter
 Z    =       16979992
95                 Z    =         5184324
91
 XDOT =      24211
062479                 XDOT =        7367
712307
 YDOT =       5226
240896  feet/sec       YDOT =        1675
415248  meter/sec
 ZDOT =      -4418
475060                 ZDOT =       -1310
932504

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3935347
88                 X    =         1199494
04
 Y    =       13759127
37  feet           Y    =         4193782
02  meter
 Z    =       17019752
30                 Z    =         5187620
50
 XDOT =     -20936
566440                 XDOT =       -6381
465451
 YDOT =      11267
661346  feet/sec       YDOT =        3434
383178  meter/sec
 ZDOT =      -4259
511307                 ZDOT =       -1298
299046


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   17355
40905481  
00016717  00000-0  10270-3 0  9212
2 25544  51
6401 184
9989 0003165 273
1467  86
9324 15
54233615 10549


Satellite: ISS
Catalog Number: 25544
Epoch time:      17355
40905481   =   yrday
fracday
Element set:     921
Inclination:       51
6401  deg
RA of node:       184
9989  deg
Eccentricity:     
0003165     
Arg of perigee:   273
1467  deg
Mean anomaly:      86
9324  deg
Mean motion:   15
54233615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1054
Checksum:              315
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