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

 
Date: January 31st 2018

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 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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


030/15:25:11 379 1 1 1 1 1 1
N/A -0 5 -0 1 222 1
000/00:00:22 759 0 0 -0 0 213 8

037/00:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 6

040/08:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 2
000/00:00:00 000 0 0 0 0 213 5

043/19:08:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 6

Coasting Arc #1 (Orbit 1697)
---------------------------------------

Vector Time (GMT): 2018/029/16:59:17
652
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2801840
72                 A    =         6778075
74  meter
 Y    =        3527647
01  meter          E    =           
0007566
 Z    =        5058061
41                 I    =           51
55432
 XDOT =      -6883
973219                 Wp   =           95
98805
 YDOT =       2867
558363  meter/sec      RA   =          348
49681  deg
 ZDOT =       1810
253016                 TA   =          336
46514
                                          MA   =          336
49974
                                          Ha   =            222
019  n
mi
                                          Hp   =            213
316

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9192390
83                 X    =         2737616
51
 Y    =       11573645
05  feet           Y    =         3558619
76  meter
 Z    =       16594689
66                 Z    =         5071515
68
 XDOT =     -22585
213974                 XDOT =       -6924
320473
 YDOT =       9407
999879  feet/sec       YDOT =        2790
351370  meter/sec
 ZDOT =       5939
150315                 ZDOT =        1776
715920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12864360
03                 X    =         3921056
94
 Y    =        7140480
79  feet           Y    =         2176418
55  meter
 Z    =       16653972
76                 Z    =         5076130
90
 XDOT =     -16675
409747                 XDOT =       -5082
664891
 YDOT =      16516
238158  feet/sec       YDOT =        5034
149391  meter/sec
 ZDOT =       5789
350587                 ZDOT =        1764
594059


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   18029
75913906  
00016717  00000-0  10270-3 0  9007
2 25544  51
6426 348
8048 0003829  55
3745 304
7768 15
54230964 16980


Satellite: ISS
Catalog Number: 25544
Epoch time:      18029
75913906   =   yrday
fracday
Element set:     900
Inclination:       51
6426  deg
RA of node:       348
8048  deg
Eccentricity:     
0003829     
Arg of perigee:    55
3745  deg
Mean anomaly:     304
7768  deg
Mean motion:   15
54230964  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1698
Checksum:              341


Coasting Arc #2 (Orbit 1711)
---------------------------------------

Vector Time (GMT): 2018/030/15:25:22
759
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1598995
86                 A    =         6777641
09  meter
 Y    =       -3925437
88  meter          E    =           
0017368
 Z    =       -5303723
03                 I    =           51
52142
 XDOT =       7250
685679                 Wp   =           80
56063
 YDOT =      -2425
805135  meter/sec      RA   =          343
81858  deg
 ZDOT =       -388
872719                 TA   =          185
70911
                                          MA   =          185
72894
                                          Ha   =            222
091  n
mi
                                          Hp   =            213
833

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5246049
41                 X    =        -1529219
69
 Y    =      -12878733
22  feet           Y    =        -3942928
62  meter
 Z    =      -17400666
10                 Z    =        -5311320
87
 XDOT =      23788
338843                 XDOT =        7279
161697
 YDOT =      -7958
678264  feet/sec       YDOT =       -2344
563765  meter/sec
 ZDOT =      -1275
829129                 ZDOT =        -353
583240

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5196085
63                 X    =        -1583766
90
 Y    =      -12854137
70  feet           Y    =        -3917941
17  meter
 Z    =      -17433812
63                 Z    =        -5313826
09
 XDOT =      22818
467372                 XDOT =        6955
068855
 YDOT =      -7699
735982  feet/sec       YDOT =       -2346
879527  meter/sec
 ZDOT =      -1118
310385                 ZDOT =        -340
861005


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   18030
65930659  
00016717  00000-0  10270-3 0  9013
2 25544  51
6430 344
3160 0003105  49
4097 310
7326 15
54044848 17120


Satellite: ISS
Catalog Number: 25544
Epoch time:      18030
65930659   =   yrday
fracday
Element set:     901
Inclination:       51
6430  deg
RA of node:       344
3160  deg
Eccentricity:     
0003105     
Arg of perigee:    49
4097  deg
Mean anomaly:     310
7326  deg
Mean motion:   15
54044848  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1712
Checksum:              287


Coasting Arc #3 (Orbit 1727)
---------------------------------------

Vector Time (GMT): 2018/031/15:25:22
759
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -114722
35                 A    =         6778301
10  meter
 Y    =        4422841
59  meter          E    =           
0007908
 Z    =        5130840
85                 I    =           51
49243
 XDOT =      -7357
888655                 Wp   =           52
96968
 YDOT =       1565
619384  meter/sec      RA   =          338
81101  deg
 ZDOT =      -1507
822729                 TA   =           51
61126
                                          MA   =           51
54026
                                          Ha   =            222
058  n
mi
                                          Hp   =            213
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -376385
66                 X    =         -189093
43
 Y    =       14510635
13  feet           Y    =         4421142
80  meter
 Z    =       16833467
35                 Z    =         5130103
00
 XDOT =     -24140
054642                 XDOT =       -7367
524992
 YDOT =       5136
546536  feet/sec       YDOT =        1483
284564  meter/sec
 ZDOT =      -4946
924964                 ZDOT =       -1543
587153

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -164469
36                 X    =          -50130
26
 Y    =       14519267
81  feet           Y    =         4425472
83  meter
 Z    =       16829427
59                 Z    =         5129609
53
 XDOT =     -22927
950352                 XDOT =       -6988
439267
 YDOT =       5683
034960  feet/sec       YDOT =        1732
189056  meter/sec
 ZDOT =      -5106
402363                 ZDOT =       -1556
431440


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   18031
68820380  
00016717  00000-0  10270-3 0  9027
2 25544  51
6428 339
1881 0003077  51
2986 308
8442 15
54076250 17281


Satellite: ISS
Catalog Number: 25544
Epoch time:      18031
68820380   =   yrday
fracday
Element set:     902
Inclination:       51
6428  deg
RA of node:       339
1881  deg
Eccentricity:     
0003077     
Arg of perigee:    51
2986  deg
Mean anomaly:     308
8442  deg
Mean motion:   15
54076250  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1728
Checksum:              312


Coasting Arc #4 (Orbit 1742)
---------------------------------------

Vector Time (GMT): 2018/032/15:25:22
759
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1719875
00                 A    =         6781182
24  meter
 Y    =       -4811504
96  meter          E    =           
0011290
 Z    =       -4468736
65                 I    =           51
47126
 XDOT =       6920
077440                 Wp   =           97
17383
 YDOT =       -529
647039  meter/sec      RA   =          333
80666  deg
 ZDOT =       3239
256891                 TA   =          205
52483
                                          MA   =          205
58062
                                          Ha   =            222
127  n
mi
                                          Hp   =            213
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5642634
51                 X    =         1795256
86
 Y    =      -15785777
42  feet           Y    =        -4791850
74  meter
 Z    =      -14661209
47                 Z    =        -4460199
15
 XDOT =      22703
666141                 XDOT =        6909
751645
 YDOT =      -1737
687137  feet/sec       YDOT =        -452
319656  meter/sec
 ZDOT =      10627
483238                 ZDOT =        3272
846177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5112146
27                 X    =         1558182
18
 Y    =      -16001022
42  feet           Y    =        -4877111
64  meter
 Z    =      -14622393
72                 Z    =        -4456905
60
 XDOT =      21380
187946                 XDOT =        6516
681286
 YDOT =      -3000
791165  feet/sec       YDOT =        -914
641147  meter/sec
 ZDOT =      10777
093220                 ZDOT =        3284
858013


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   18032
65279447  
00016717  00000-0  10270-3 0  9038
2 25544  51
6427 334
3811 0003043  54
4738 305
6699 15
54039170 17439


Satellite: ISS
Catalog Number: 25544
Epoch time:      18032
65279447   =   yrday
fracday
Element set:     903
Inclination:       51
6427  deg
RA of node:       334
3811  deg
Eccentricity:     
0003043     
Arg of perigee:    54
4738  deg
Mean anomaly:     305
6699  deg
Mean motion:   15
54039170  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1743
Checksum:              311


Coasting Arc #5 (Orbit 1758)
---------------------------------------

Vector Time (GMT): 2018/033/15:25:22
759
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3146428
02                 A    =         6784920
25  meter
 Y    =        5000699
95  meter          E    =           
0015349
 Z    =        3324070
66                 I    =           51
45520
 XDOT =      -6047
394500                 Wp   =           84
95569
 YDOT =       -687
815943  meter/sec      RA   =          328
80918  deg
 ZDOT =      -4669
528581                 TA   =           56
21992
                                          MA   =           56
07382
                                          Ha   =            222
198  n
mi
                                          Hp   =            213
801

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10322926
58                 X    =        -3218259
50
 Y    =       16406495
90  feet           Y    =         4965112
95  meter
 Z    =       10905743
63                 Z    =         3308612
12
 XDOT =     -19840
533138                 XDOT =       -6016
572207
 YDOT =      -2256
613986  feet/sec       YDOT =        -755
269937  meter/sec
 ZDOT =     -15319
975661                 ZDOT =       -4698
829044

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9448987
62                 X    =        -2880051
43
 Y    =       16969581
53  feet           Y    =         5172328
45  meter
 Z    =       10836101
73                 Z    =         3302843
81
 XDOT =     -18597
816754                 XDOT =       -5668
614547
 YDOT =       -447
635834  feet/sec       YDOT =        -136
439402  meter/sec
 ZDOT =     -15450
282764                 ZDOT =       -4709
246187


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   18033
68168631  
00016717  00000-0  10270-3 0  9045
2 25544  51
6431 329
2533 0003140  58
4666 301
6793 15
54054109 17597


Satellite: ISS
Catalog Number: 25544
Epoch time:      18033
68168631   =   yrday
fracday
Element set:     904
Inclination:       51
6431  deg
RA of node:       329
2533  deg
Eccentricity:     
0003140     
Arg of perigee:    58
4666  deg
Mean anomaly:     301
6793  deg
Mean motion:   15
54054109  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1759
Checksum:              306


Coasting Arc #6 (Orbit 1773)
---------------------------------------

Vector Time (GMT): 2018/034/15:25:22
759
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4236078
70                 A    =         6788068
14  meter
 Y    =       -4955642
54  meter          E    =           
0010145
 Z    =       -1880566
07                 I    =           51
43804
 XDOT =       4826
788784                 Wp   =           44
91327
 YDOT =       2007
811843  meter/sec      RA   =          323
81840  deg
 ZDOT =       5607
208011                 TA   =          294
32704
                                          MA   =          294
43294
                                          Ha   =            222
172  n
mi
                                          Hp   =            213
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13897896
00                 X    =         4300313
79
 Y    =      -16258669
76  feet           Y    =        -4907912
76  meter
 Z    =       -6169836
19                 Z    =        -1859832
82
 XDOT =      15835
921207                 XDOT =        4776
741923
 YDOT =       6587
309196  feet/sec       YDOT =        2061
508830  meter/sec
 ZDOT =      18396
351742                 ZDOT =        5630
532655

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12700631
95                 X    =         3871152
62
 Y    =      -17243257
47  feet           Y    =        -5255744
88  meter
 Z    =       -6076738
79                 Z    =        -1852189
98
 XDOT =      14900
186636                 XDOT =        4541
576887
 YDOT =       4485
259648  feet/sec       YDOT =        1367
107141  meter/sec
 ZDOT =      18499
836644                 ZDOT =        5638
750209


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   18034
64626725  
00016717  00000-0  10270-3 0  9056
2 25544  51
6428 324
4452 0003098  60
4200 299
7261 15
54060220 17744


Satellite: ISS
Catalog Number: 25544
Epoch time:      18034
64626725   =   yrday
fracday
Element set:     905
Inclination:       51
6428  deg
RA of node:       324
4452  deg
Eccentricity:     
0003098     
Arg of perigee:    60
4200  deg
Mean anomaly:     299
7261  deg
Mean motion:   15
54060220  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1774
Checksum:              294


Coasting Arc #7 (Orbit 1789)
---------------------------------------

Vector Time (GMT): 2018/035/15:25:22
759
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4997564
47                 A    =         6789641
80  meter
 Y    =        4583887
01  meter          E    =           
0013980
 Z    =         201939
26                 I    =           51
41592
 XDOT =      -3371
996588                 Wp   =          121
07702
 YDOT =      -3399
192676  meter/sec      RA   =          318
83357  deg
 ZDOT =      -5989
369323                 TA   =           56
74076
                                          MA   =           56
60688
                                          Ha   =            222
224  n
mi
                                          Hp   =            213
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16396208
90                 X    =        -5049432
21
 Y    =       15038999
38  feet           Y    =         4527710
82  meter
 Z    =         662530
40                 Z    =          177537
02
 XDOT =     -11062
980931                 XDOT =       -3304
642641
 YDOT =     -11152
206942  feet/sec       YDOT =       -3436
524456  meter/sec
 ZDOT =     -19650
161821                 ZDOT =       -6005
585184

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14964832
99                 X    =        -4561281
09
 Y    =       16467965
32  feet           Y    =         5019435
83  meter
 Z    =         553178
93                 Z    =          168608
94
 XDOT =     -10701
194364                 XDOT =       -3261
724042
 YDOT =      -9022
233622  feet/sec       YDOT =       -2749
976808  meter/sec
 ZDOT =     -19721
778529                 ZDOT =       -6011
198096


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   18035
67515227  
00016717  00000-0  10270-3 0  9065
2 25544  51
6417 319
3173 0003052  67
7960 292
3516 15
54016756 17903


Satellite: ISS
Catalog Number: 25544
Epoch time:      18035
67515227   =   yrday
fracday
Element set:     906
Inclination:       51
6417  deg
RA of node:       319
3173  deg
Eccentricity:     
0003052     
Arg of perigee:    67
7960  deg
Mean anomaly:     292
3516  deg
Mean motion:   15
54016756  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1790
Checksum:              312


Coasting Arc #8 (Orbit 1805)
---------------------------------------

Vector Time (GMT): 2018/036/15:25:22
759
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5353643
51                 A    =         6788539
04  meter
 Y    =       -3899651
83  meter          E    =           
0016811
 Z    =        1452053
15                 I    =           51
38856
 XDOT =       1856
646979                 Wp   =           62
25733
 YDOT =       4711
002042  meter/sec      RA   =          313
84654  deg
 ZDOT =       5763
039209                 TA   =          313
64846
                                          MA   =          313
78773
                                          Ha   =            222
065  n
mi
                                          Hp   =            213
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17564447
21                 X    =         5389799
38
 Y    =      -12794133
31  feet           Y    =        -3839581
47  meter
 Z    =        4763953
89                 Z    =         1478146
92
 XDOT =       6091
361480                 XDOT =        1775
835929
 YDOT =      15456
043444  feet/sec       YDOT =        4731
312848  meter/sec
 ZDOT =      18907
608954                 ZDOT =        5771
861455

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16047739
73                 X    =         4891351
07
 Y    =      -14613132
25  feet           Y    =        -4454082
71  meter
 Z    =        4880709
47                 Z    =         1487640
25
 XDOT =       6536
106392                 XDOT =        1992
205228
 YDOT =      13552
228291  feet/sec       YDOT =        4130
719183  meter/sec
 ZDOT =      18946
111171                 ZDOT =        5774
774685


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   18036
70403054  
00016717  00000-0  10270-3 0  9075
2 25544  51
6414 314
1886 0002941  67
2741 292
8723 15
54079394 18062


Satellite: ISS
Catalog Number: 25544
Epoch time:      18036
70403054   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       314
1886  deg
Eccentricity:     
0002941     
Arg of perigee:    67
2741  deg
Mean anomaly:     292
8723  deg
Mean motion:   15
54079394  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1806
Checksum:              311


Coasting Arc #9 (Orbit 1810)
---------------------------------------

Vector Time (GMT): 2018/037/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4178787
22                 A    =         6778294
17  meter
 Y    =       -1499848
61  meter          E    =           
0016544
 Z    =       -5136676
67                 I    =           51
34603
 XDOT =       4083
742779                 Wp   =           78
35066
 YDOT =      -6303
728845  meter/sec      RA   =          312
01894  deg
 ZDOT =      -1482
381421                 TA   =          177
29787
                                          MA   =          177
28892
                                          Ha   =            222
121  n
mi
                                          Hp   =            213
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13709931
81                 X    =        -4136754
03
 Y    =       -4920763
16  feet           Y    =        -1546343
94  meter
 Z    =      -16852613
74                 Z    =        -5156873
29
 XDOT =      13398
106231                 XDOT =        4161
129789
 YDOT =     -20681
525083  feet/sec       YDOT =       -6257
629018  meter/sec
 ZDOT =      -4863
456106                 ZDOT =       -1462
356001

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6748965
19                 X    =         2057084
59
 Y    =       12790553
29  feet           Y    =         3898560
64  meter
 Z    =      -16942253
26                 Z    =        -5163998
79
 XDOT =     -22917
809936                 XDOT =       -6985
348468
 YDOT =       5773
350350  feet/sec       YDOT =        1759
717187  meter/sec
 ZDOT =      -4773
324184                 ZDOT =       -1454
909211


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   18037
02555552  
00016717  00000-0  10270-3 0  9083
2 25544  51
6417 312
5828 0002772  77
4962 282
6500 15
54047954 18116


Satellite: ISS
Catalog Number: 25544
Epoch time:      18037
02555552   =   yrday
fracday
Element set:     908
Inclination:       51
6417  deg
RA of node:       312
5828  deg
Eccentricity:     
0002772     
Arg of perigee:    77
4962  deg
Mean anomaly:     282
6500  deg
Mean motion:   15
54047954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1811
Checksum:              313


Coasting Arc #10 (Orbit 1826)
---------------------------------------

Vector Time (GMT): 2018/038/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3086091
49                 A    =         6777479
87  meter
 Y    =        2921391
85  meter          E    =           
0005523
 Z    =        5275217
76                 I    =           51
32289
 XDOT =      -4874
549741                 Wp   =           74
54552
 YDOT =       5910
695048  meter/sec      RA   =          306
99842  deg
 ZDOT =       -419
808433                 TA   =           19
48382
                                          MA   =           19
46272
                                          Ha   =            221
954  n
mi
                                          Hp   =            213
678

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10124972
09                 X    =         3027570
45
 Y    =        9584618
92  feet           Y    =         2955575
66  meter
 Z    =       17307144
89                 Z    =         5290066
46
 XDOT =     -15992
617261                 XDOT =       -4938
243266
 YDOT =      19392
044120  feet/sec       YDOT =        5855
828337  meter/sec
 ZDOT =      -1377
324256                 ZDOT =        -443
641942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1194406
15                 X    =         -364054
99
 Y    =      -13808617
51  feet           Y    =        -4208866
62  meter
 Z    =       17372757
99                 Z    =         5295216
63
 XDOT =      23799
188627                 XDOT =        7253
992693
 YDOT =      -3933
467817  feet/sec       YDOT =       -1198
920990  meter/sec
 ZDOT =      -1484
327152                 ZDOT =        -452
422916


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   18038
05442888  
00016717  00000-0  10270-3 0  9095
2 25544  51
6420 307
4541 0002844  79
2164 280
9309 15
54104680 18274


Satellite: ISS
Catalog Number: 25544
Epoch time:      18038
05442888   =   yrday
fracday
Element set:     909
Inclination:       51
6420  deg
RA of node:       307
4541  deg
Eccentricity:     
0002844     
Arg of perigee:    79
2164  deg
Mean anomaly:     280
9309  deg
Mean motion:   15
54104680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1827
Checksum:              313


Coasting Arc #11 (Orbit 1841)
---------------------------------------

Vector Time (GMT): 2018/039/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1961453
58                 A    =         6779243
49  meter
 Y    =       -4269564
68  meter          E    =           
0014890
 Z    =       -4900641
19                 I    =           51
30831
 XDOT =       5295
347149                 Wp   =          101
76917
 YDOT =      -5040
706549  meter/sec      RA   =          301
97904  deg
 ZDOT =       2275
068161                 TA   =          190
59131
                                          MA   =          190
62271
                                          Ha   =            222
150  n
mi
                                          Hp   =            213
556

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6435215
16                 X    =        -1889759
96
 Y    =      -14007758
15  feet           Y    =        -4291098
29  meter
 Z    =      -16078219
13                 Z    =        -4909994
86
 XDOT =      17373
186186                 XDOT =        5340
269200
 YDOT =     -16537
751146  feet/sec       YDOT =       -4981
239099  meter/sec
 ZDOT =       7464
134387                 ZDOT =        2300
900041

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4237048
81                 X    =        -1291452
48
 Y    =       14776948
20  feet           Y    =         4504013
81  meter
 Z    =      -16119169
71                 Z    =        -4913122
93
 XDOT =     -22830
943150                 XDOT =       -6958
871472
 YDOT =       1711
599213  feet/sec       YDOT =         521
695440  meter/sec
 ZDOT =       7579
881394                 ZDOT =        2310
347849


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   18039
01899811  
00016717  00000-0  10270-3 0  9106
2 25544  51
6407 302
6472 0003002  82
6302 277
5192 15
54087227 18424


Satellite: ISS
Catalog Number: 25544
Epoch time:      18039
01899811   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:       302
6472  deg
Eccentricity:     
0003002     
Arg of perigee:    82
6302  deg
Mean anomaly:     277
5192  deg
Mean motion:   15
54087227  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1842
Checksum:              294


Coasting Arc #12 (Orbit 1857)
---------------------------------------

Vector Time (GMT): 2018/040/00:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         840643
19                 A    =         6782600
09  meter
 Y    =        5407907
94  meter          E    =           
0013727
 Z    =        3996536
02                 I    =           51
30378
 XDOT =      -5428
245345                 Wp   =           79
72405
 YDOT =       3749
204161  meter/sec      RA   =          296
96434  deg
 ZDOT =      -3917
532786                 TA   =           51
19620
                                          MA   =           51
07370
                                          Ha   =            222
053  n
mi
                                          Hp   =            213
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2758015
72                 X    =          760695
24
 Y    =       17742480
11  feet           Y    =         5416861
65  meter
 Z    =       13111994
82                 Z    =         4000425
22
 XDOT =     -17809
203887                 XDOT =       -5450
737489
 YDOT =      12300
538587  feet/sec       YDOT =        3688
375953  meter/sec
 ZDOT =     -12852
797855                 ZDOT =       -3943
955648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9178218
72                 X    =         2797521
07
 Y    =      -15418513
40  feet           Y    =        -4699562
88  meter
 Z    =       13128457
82                 Z    =         4001553
94
 XDOT =      20380
721482                 XDOT =        6212
043908
 YDOT =       1048
855138  feet/sec       YDOT =         319
691046  meter/sec
 ZDOT =     -12970
964065                 ZDOT =       -3953
549847


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   18040
04786703  
00016717  00000-0  10270-3 0  9117
2 25544  51
6413 297
5184 0002872  84
4053 275
7427 15
54105009 18587


Satellite: ISS
Catalog Number: 25544
Epoch time:      18040
04786703   =   yrday
fracday
Element set:     911
Inclination:       51
6413  deg
RA of node:       297
5184  deg
Eccentricity:     
0002872     
Arg of perigee:    84
4053  deg
Mean anomaly:     275
7427  deg
Mean motion:   15
54105009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1858
Checksum:              308


Coasting Arc #13 (Orbit 1862)
---------------------------------------

Vector Time (GMT): 2018/040/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4450229
33                 A    =         6778259
46  meter
 Y    =        -196057
67  meter          E    =           
0016771
 Z    =       -5124039
49                 I    =           51
28240
 XDOT =       2062
964483                 Wp   =           78
72132
 YDOT =      -7214
786521  meter/sec      RA   =          295
28162  deg
 ZDOT =      -1516
648446                 TA   =          176
57560
                                          MA   =          176
56410
                                          Ha   =            222
192  n
mi
                                          Hp   =            213
467

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14600489
94                 X    =        -4422816
71
 Y    =        -643233
82  feet           Y    =         -245670
01  meter
 Z    =      -16811153
19                 Z    =        -5145590
26
 XDOT =       6768
256177                 XDOT =        2150
855822
 YDOT =     -23670
559452  feet/sec       YDOT =       -7191
225635  meter/sec
 ZDOT =      -4975
880729                 ZDOT =       -1506
413825

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1964580
17                 X    =          598804
04
 Y    =      -14369965
66  feet           Y    =        -4379965
53  meter
 Z    =      -16907023
38                 Z    =        -5153260
73
 XDOT =      21903
426491                 XDOT =        6676
164394
 YDOT =       8790
087465  feet/sec       YDOT =        2679
218659  meter/sec
 ZDOT =      -4929
215342                 ZDOT =       -1502
424836


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   18040
36938985  
00016717  00000-0  10270-3 0  9124
2 25544  51
6397 295
9167 0003073  80
5428 279
6072 15
54076097 18637


Satellite: ISS
Catalog Number: 25544
Epoch time:      18040
36938985   =   yrday
fracday
Element set:     912
Inclination:       51
6397  deg
RA of node:       295
9167  deg
Eccentricity:     
0003073     
Arg of perigee:    80
5428  deg
Mean anomaly:     279
6072  deg
Mean motion:   15
54076097  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1863
Checksum:              345


Coasting Arc #14 (Orbit 1878)
---------------------------------------

Vector Time (GMT): 2018/041/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3815129
65                 A    =         6777504
22  meter
 Y    =        1877843
71  meter          E    =           
0005707
 Z    =        5272841
88                 I    =           51
26697
 XDOT =      -2943
491117                 Wp   =           76
98440
 YDOT =       7075
421633  meter/sec      RA   =          290
25797  deg
 ZDOT =       -388
442243                 TA   =           16
74592
                                          MA   =           16
72709
                                          Ha   =            222
038  n
mi
                                          Hp   =            213
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12516829
55                 X    =         3768235
30
 Y    =        6160904
57  feet           Y    =         1920244
98  meter
 Z    =       17299349
99                 Z    =         5291260
21
 XDOT =      -9657
123088                 XDOT =       -3020
504815
 YDOT =      23213
325567  feet/sec       YDOT =        7042
074880  meter/sec
 ZDOT =      -1274
416809                 ZDOT =        -402
927609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7064905
43                 X    =        -2153383
18
 Y    =       11911439
24  feet           Y    =         3630606
68  meter
 Z    =       17381024
25                 Z    =         5297736
19
 XDOT =     -21565
364595                 XDOT =       -6573
123129
 YDOT =     -10827
859326  feet/sec       YDOT =       -3300
331523  meter/sec
 ZDOT =      -1339
963346                 ZDOT =        -408
420828


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   18041
39825469  
00016717  00000-0  10270-3 0  9131
2 25544  51
6397 290
7890 0003083  81
7533 278
3969 15
54092171 18793


Satellite: ISS
Catalog Number: 25544
Epoch time:      18041
39825469   =   yrday
fracday
Element set:     913
Inclination:       51
6397  deg
RA of node:       290
7890  deg
Eccentricity:     
0003083     
Arg of perigee:    81
7533  deg
Mean anomaly:     278
3969  deg
Mean motion:   15
54092171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1879
Checksum:              348


Coasting Arc #15 (Orbit 1893)
---------------------------------------

Vector Time (GMT): 2018/042/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3125777
52                 A    =         6779203
71  meter
 Y    =       -3500816
75  meter          E    =           
0015132
 Z    =       -4905970
51                 I    =           51
26165
 XDOT =       3605
369355                 Wp   =          102
29548
 YDOT =      -6368
698264  meter/sec      RA   =          285
23392  deg
 ZDOT =       2250
218383                 TA   =          189
82426
                                          MA   =          189
85388
                                          Ha   =            222
198  n
mi
                                          Hp   =            213
484

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10255175
58                 X    =        -3062567
98
 Y    =      -11485619
25  feet           Y    =        -3535417
98  meter
 Z    =      -16095703
76                 Z    =        -4921000
58
 XDOT =      11828
639616                 XDOT =        3665
387745
 YDOT =     -20894
679343  feet/sec       YDOT =       -6328
044934  meter/sec
 ZDOT =       7382
606244                 ZDOT =        2267
877538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12046523
12                 X    =         3671780
25
 Y    =       -9477807
91  feet           Y    =        -2888835
85  meter
 Z    =      -16162060
30                 Z    =        -4926195
98
 XDOT =      19497
819241                 XDOT =        5942
935305
 YDOT =      12072
602596  feet/sec       YDOT =        3679
729271  meter/sec
 ZDOT =       7462
155680                 ZDOT =        2274
465051


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   18042
36281459  
00016717  00000-0  10270-3 0  9145
2 25544  51
6393 285
9811 0003106  86
0746 274
0762 15
54082477 18947


Satellite: ISS
Catalog Number: 25544
Epoch time:      18042
36281459   =   yrday
fracday
Element set:     914
Inclination:       51
6393  deg
RA of node:       285
9811  deg
Eccentricity:     
0003106     
Arg of perigee:    86
0746  deg
Mean anomaly:     274
0762  deg
Mean motion:   15
54082477  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1894
Checksum:              326


Coasting Arc #16 (Orbit 1909)
---------------------------------------

Vector Time (GMT): 2018/043/08:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2378073
46                 A    =         6782573
06  meter
 Y    =        4921293
24  meter          E    =           
0013764
 Z    =        4005945
68                 I    =           51
26589
 XDOT =      -4111
294913                 Wp   =           80
64960
 YDOT =       5172
706179  meter/sec      RA   =          280
21697  deg
 ZDOT =      -3900
353821                 TA   =           50
07773
                                          MA   =           49
95684
                                          Ha   =            222
093  n
mi
                                          Hp   =            213
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7802078
29                 X    =         2303407
15
 Y    =       16145975
19  feet           Y    =         4947469
08  meter
 Z    =       13142866
41                 Z    =         4017315
84
 XDOT =     -13488
500372                 XDOT =       -4149
886513
 YDOT =      16970
820796  feet/sec       YDOT =        5126
515001  meter/sec
 ZDOT =     -12796
436419                 ZDOT =       -3920
418456

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16441285
69                 X    =        -5011303
88
 Y    =        7066523
65  feet           Y    =         2153876
41  meter
 Z    =       13192734
60                 Z    =         4021145
51
 XDOT =     -15907
620168                 XDOT =       -4848
642627
 YDOT =     -12869
594647  feet/sec       YDOT =       -3922
652449  meter/sec
 ZDOT =     -12886
499791                 ZDOT =       -3927
805136


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   18043
39167553  
00016717  00000-0  10270-3 0  9158
2 25544  51
6398 280
8532 0003004  89
2968 270
8528 15
54091202 19103


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
39167553   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:       280
8532  deg
Eccentricity:     
0003004     
Arg of perigee:    89
2968  deg
Mean anomaly:     270
8528  deg
Mean motion:   15
54091202  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1910
Checksum:              315


Coasting Arc #17 (Orbit 1916)
---------------------------------------

Vector Time (GMT): 2018/043/19:08:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905723
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3601305
93                 A    =         6779013
90  meter
 Y    =        2906934
97  meter          E    =           
0008798
 Z    =        4946986
50                 I    =           51
25165
 XDOT =      -2665
571784                 Wp   =           71
36027
 YDOT =       6882
745845  meter/sec      RA   =          277
98353  deg
 ZDOT =      -2098
099758                 TA   =           39
19518
                                          MA   =           39
13150
                                          Ha   =            222
133  n
mi
                                          Hp   =            213
606

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11815308
17                 X    =         3544502
85
 Y    =        9537188
22  feet           Y    =         2946889
76  meter
 Z    =       16230270
68                 Z    =         4964341
96
 XDOT =      -8745
314251                 XDOT =       -2732
147175
 YDOT =      22581
187156  feet/sec       YDOT =        6852
565296  meter/sec
 ZDOT =      -6883
529389                 ZDOT =       -2111
209743

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13112600
70                 X    =         3996720
69
 Y    =       -7491328
72  feet           Y    =        -2283356
99  meter
 Z    =       16307079
74                 Z    =         4970397
90
 XDOT =      17391
182545                 XDOT =        5300
832440
 YDOT =      15286
269599  feet/sec       YDOT =        4659
254974  meter/sec
 ZDOT =      -6942
889827                 ZDOT =       -2116
192819


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   18043
84180186  
00016717  00000-0  10270-3 0  9166
2 25544  51
6402 278
6049 0003196 100
3519 259
7994 15
54065196 19179


Satellite: ISS
Catalog Number: 25544
Epoch time:      18043
84180186   =   yrday
fracday
Element set:     916
Inclination:       51
6402  deg
RA of node:       278
6049  deg
Eccentricity:     
0003196     
Arg of perigee:   100
3519  deg
Mean anomaly:     259
7994  deg
Mean motion:   15
54065196  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1917
Checksum:              329
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