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

 
Date: January 22nd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 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


023/19:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 213 7

029/16:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 0
000/00:00:00 000 0 0 0 0 213 3

030/15:25:14 630 1 4 1 5 1 5
N/A -0 6 -0 1 222 1
000/00:00:29 261 0 0 -0 0 214 1

Coasting Arc #1 (Orbit 1538)
---------------------------------------

Vector Time (GMT): 2018/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5834064
51                 A    =         6787861
92  meter
 Y    =       -2962241
48  meter          E    =           
0014498
 Z    =        1787916
04                 I    =           51
89753
 XDOT =        827
301792                 Wp   =          100
58855
 YDOT =      -5081
653085  meter/sec      RA   =           39
29235  deg
 ZDOT =      -5683
373073                 TA   =           59
84068
                                          MA   =           59
69711
                                          Ha   =            221
777  n
mi
                                          Hp   =            213
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19140631
58                 X    =        -5809190
90
 Y    =       -9718640
03  feet           Y    =        -3027342
96  meter
 Z    =        5865866
28                 Z    =         1759637
11
 XDOT =       2714
244723                 XDOT =         911
670974
 YDOT =     -16672
090173  feet/sec       YDOT =       -5071
929747  meter/sec
 ZDOT =     -18646
237116                 ZDOT =       -5679
149628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -408947
93                 X    =         -124647
33
 Y    =      -21496615
96  feet           Y    =        -6552168
54  meter
 Z    =        5740417
47                 Z    =         1749679
25
 XDOT =      14489
866933                 XDOT =        4416
511441
 YDOT =      -5282
280477  feet/sec       YDOT =       -1610
039090  meter/sec
 ZDOT =     -18626
555157                 ZDOT =       -5677
374012


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   18019
53562654  
00016717  00000-0  10270-3 0  9002
2 25544  51
6396  39
7742 0003526  27
0102 333
1234 15
54187636 15395


Satellite: ISS
Catalog Number: 25544
Epoch time:      18019
53562654   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:        39
7742  deg
Eccentricity:     
0003526     
Arg of perigee:    27
0102  deg
Mean anomaly:     333
1234  deg
Mean motion:   15
54187636  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1539
Checksum:              301


Coasting Arc #2 (Orbit 1553)
---------------------------------------

Vector Time (GMT): 2018/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5642674
94                 A    =         6789083
40  meter
 Y    =        3759920
70  meter          E    =           
0015329
 Z    =         -99707
42                 I    =           51
87693
 XDOT =      -2559
034217                 Wp   =           41
00314
 YDOT =       3986
265017  meter/sec      RA   =           34
33816  deg
 ZDOT =       6033
814550                 TA   =          317
92594
                                          MA   =          318
04355
                                          Ha   =            221
744  n
mi
                                          Hp   =            213
845

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18512713
05                 X    =         5600695
44
 Y    =       12335697
83  feet           Y    =         3822786
24  meter
 Z    =        -327124
08                 Z    =          -72399
73
 XDOT =      -8395
781551                 XDOT =       -2632
728020
 YDOT =      13078
297300  feet/sec       YDOT =        3957
236039  meter/sec
 ZDOT =      19795
979496                 ZDOT =        6021
204949

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1833416
86                 X    =         -558825
46
 Y    =       22171898
49  feet           Y    =         6757994
66  meter
 Z    =        -206144
60                 Z    =          -62832
88
 XDOT =     -13955
653218                 XDOT =       -4253
683101
 YDOT =       -996
393092  feet/sec       YDOT =        -303
700614  meter/sec
 ZDOT =      19739
133791                 ZDOT =        6016
487980


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   18020
50012375  
00016717  00000-0  10270-3 0  9012
2 25544  51
6406  34
9661 0003447  28
7192 331
4150 15
54212866 15542


Satellite: ISS
Catalog Number: 25544
Epoch time:      18020
50012375   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:        34
9661  deg
Eccentricity:     
0003447     
Arg of perigee:    28
7192  deg
Mean anomaly:     331
4150  deg
Mean motion:   15
54212866  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1554
Checksum:              278


Coasting Arc #3 (Orbit 1569)
---------------------------------------

Vector Time (GMT): 2018/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4994953
97                 A    =         6787979
97  meter
 Y    =       -4292482
06  meter          E    =           
0007430
 Z    =       -1641458
17                 I    =           51
84427
 XDOT =       4259
944912                 Wp   =          114
00653
 YDOT =      -2772
791282  meter/sec      RA   =           29
38208  deg
 ZDOT =      -5735
448363                 TA   =           83
90515
                                          MA   =           83
82049
                                          Ha   =            221
865  n
mi
                                          Hp   =            213
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16387644
26                 X    =        -4938609
85
 Y    =      -14082946
38  feet           Y    =        -4348024
02  meter
 Z    =       -5385361
45                 Z    =        -1665584
63
 XDOT =      13976
197217                 XDOT =        4318
493691
 YDOT =      -9097
084259  feet/sec       YDOT =       -2724
826313  meter/sec
 ZDOT =     -18817
087806                 ZDOT =       -5714
613187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4045493
95                 X    =         1233066
56
 Y    =      -21198053
98  feet           Y    =        -6461166
85  meter
 Z    =       -5492073
14                 Z    =        -1673983
89
 XDOT =      13374
839425                 XDOT =        4076
651057
 YDOT =       7384
017226  feet/sec       YDOT =        2250
648450  meter/sec
 ZDOT =     -18723
819284                 ZDOT =       -5707
020118


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   18021
52891847  
00016717  00000-0  10270-3 0  9025
2 25544  51
6395  29
8366 0003636  33
3869 326
7513 15
54182156 15703


Satellite: ISS
Catalog Number: 25544
Epoch time:      18021
52891847   =   yrday
fracday
Element set:     902
Inclination:       51
6395  deg
RA of node:        29
8366  deg
Eccentricity:     
0003636     
Arg of perigee:    33
3869  deg
Mean anomaly:     326
7513  deg
Mean motion:   15
54182156  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1570
Checksum:              322


Coasting Arc #4 (Orbit 1585)
---------------------------------------

Vector Time (GMT): 2018/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3929429
46                 A    =         6784778
77  meter
 Y    =        4521705
16  meter          E    =           
0015232
 Z    =        3168211
28                 I    =           51
80368
 XDOT =      -5737
781549                 Wp   =           75
22702
 YDOT =       1581
018616  meter/sec      RA   =           24
41863  deg
 ZDOT =       4844
315576                 TA   =          321
27710
                                          MA   =          321
38619
                                          Ha   =            221
770  n
mi
                                          Hp   =            213
747

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12891828
94                 X    =         3863185
22
 Y    =       14834990
67  feet           Y    =         4565276
37  meter
 Z    =       10394393
96                 Z    =         3187137
85
 XDOT =     -18824
742614                 XDOT =       -5778
565264
 YDOT =       5187
068950  feet/sec       YDOT =        1516
626829  meter/sec
 ZDOT =      15893
423806                 ZDOT =        4816
344768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6138931
89                 X    =        -1871146
44
 Y    =       18623821
87  feet           Y    =         5676540
91  meter
 Z    =       10477900
62                 Z    =         3193664
11
 XDOT =     -12819
151470                 XDOT =       -3907
277368
 YDOT =     -13125
680640  feet/sec       YDOT =       -4000
707459  meter/sec
 ZDOT =      15768
588836                 ZDOT =        4806
265877


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   18022
55771002  
00016717  00000-0  10270-3 0  9030
2 25544  51
6385  24
7080 0003533  33
7761 326
3616 15
54205273 15863


Satellite: ISS
Catalog Number: 25544
Epoch time:      18022
55771002   =   yrday
fracday
Element set:     903
Inclination:       51
6385  deg
RA of node:        24
7080  deg
Eccentricity:     
0003533     
Arg of perigee:    33
7761  deg
Mean anomaly:     326
3616  deg
Mean motion:   15
54205273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1586
Checksum:              287


Coasting Arc #5 (Orbit 1600)
---------------------------------------

Vector Time (GMT): 2018/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2482014
87                 A    =         6780949
45  meter
 Y    =       -4545113
15  meter          E    =           
0012317
 Z    =       -4390417
85                 I    =           51
76064
 XDOT =       6840
303117                 Wp   =           60
18510
 YDOT =       -438
645469  meter/sec      RA   =           19
44195  deg
 ZDOT =      -3414
109463                 TA   =          175
23447
                                          MA   =          175
22274
                                          Ha   =            221
949  n
mi
                                          Hp   =            213
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8143093
41                 X    =        -2409679
64
 Y    =      -14911788
55  feet           Y    =        -4572464
34  meter
 Z    =      -14404258
05                 Z    =        -4402298
74
 XDOT =      22441
939360                 XDOT =        6861
283536
 YDOT =      -1439
125555  feet/sec       YDOT =        -362
035244  meter/sec
 ZDOT =     -11201
146531                 ZDOT =       -3380
831070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8406764
30                 X    =         2562381
76
 Y    =      -14713718
19  feet           Y    =        -4484741
30  meter
 Z    =      -14456378
14                 Z    =        -4406304
06
 XDOT =      12048
882306                 XDOT =        3672
499327
 YDOT =      17739
869032  feet/sec       YDOT =        5407
112081  meter/sec
 ZDOT =     -11052
882748                 ZDOT =       -3368
918662


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   18023
52220164  
00016717  00000-0  10270-3 0  9047
2 25544  51
6387  19
8991 0003678  38
6972 321
4444 15
54186088 16014


Satellite: ISS
Catalog Number: 25544
Epoch time:      18023
52220164   =   yrday
fracday
Element set:     904
Inclination:       51
6387  deg
RA of node:        19
8991  deg
Eccentricity:     
0003678     
Arg of perigee:    38
6972  deg
Mean anomaly:     321
4444  deg
Mean motion:   15
54186088  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1601
Checksum:              315


Coasting Arc #6 (Orbit 1605)
---------------------------------------

Vector Time (GMT): 2018/023/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1748773
78                 A    =         6779441
46  meter
 Y    =       -4508710
40  meter          E    =           
0014286
 Z    =       -4765030
33                 I    =           51
74939
 XDOT =       7165
748557                 Wp   =           61
87146
 YDOT =         71
581951  meter/sec      RA   =           17
83302  deg
 ZDOT =      -2697
170791                 TA   =          181
47544
                                          MA   =          181
47966
                                          Ha   =            221
839  n
mi
                                          Hp   =            213
680

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5737446
79                 X    =        -1675080
44
 Y    =      -14792356
96  feet           Y    =        -4527854
40  meter
 Z    =      -15633301
60                 Z    =        -4773346
14
 XDOT =      23509
673745                 XDOT =        7177
516831
 YDOT =        234
848922  feet/sec       YDOT =         151
780035  meter/sec
 ZDOT =      -8848
985536                 ZDOT =       -2662
333864

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15556163
16                 X    =        -4741518
53
 Y    =       -2933120
16  feet           Y    =         -894015
02  meter
 Z    =      -15669551
15                 Z    =        -4776079
19
 XDOT =      12309
320739                 XDOT =        3751
880961
 YDOT =     -18831
855750  feet/sec       YDOT =       -5739
949633  meter/sec
 ZDOT =      -8693
873442                 ZDOT =       -2649
892625


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   18023
84369728  
00016717  00000-0  10270-3 0  9053
2 25544  51
6423  18
2979 0003658  33
4763 326
6620 15
54212051 16061


Satellite: ISS
Catalog Number: 25544
Epoch time:      18023
84369728   =   yrday
fracday
Element set:     905
Inclination:       51
6423  deg
RA of node:        18
2979  deg
Eccentricity:     
0003658     
Arg of perigee:    33
4763  deg
Mean anomaly:     326
6620  deg
Mean motion:   15
54212051  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1606
Checksum:              308


Coasting Arc #7 (Orbit 1621)
---------------------------------------

Vector Time (GMT): 2018/024/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -24958
88                 A    =         6777321
61  meter
 Y    =        4259161
34  meter          E    =           
0005281
 Z    =        5267158
59                 I    =           51
71045
 XDOT =      -7555
344720                 Wp   =           74
38701
 YDOT =      -1057
930148  meter/sec      RA   =           12
84081  deg
 ZDOT =        820
373906                 TA   =            7
78800
                                          MA   =            7
77981
                                          Ha   =            221
955  n
mi
                                          Hp   =            213
638

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         -81886
10                 X    =          -98168
98
 Y    =       13973626
44  feet           Y    =         4258472
90  meter
 Z    =       17280704
04                 Z    =         5266859
53
 XDOT =     -24787
876377                 XDOT =       -7546
938044
 YDOT =      -3470
899435  feet/sec       YDOT =       -1142
372185  meter/sec
 ZDOT =       2691
515439                 ZDOT =         783
693391

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11936633
29                 X    =         3638285
83
 Y    =        7270301
63  feet           Y    =         2215987
94  meter
 Z    =       17278633
43                 Z    =         5266527
47
 XDOT =     -15064
168735                 XDOT =       -4591
558631
 YDOT =      18729
426005  feet/sec       YDOT =        5708
729046  meter/sec
 ZDOT =       2528
376661                 ZDOT =         770
649206


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   18024
87248268  
00016717  00000-0  10270-3 0  9063
2 25544  51
6422  13
1685 0003698  38
7959 321
3458 15
54203011 16222


Satellite: ISS
Catalog Number: 25544
Epoch time:      18024
87248268   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:        13
1685  deg
Eccentricity:     
0003698     
Arg of perigee:    38
7959  deg
Mean anomaly:     321
3458  deg
Mean motion:   15
54203011  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1622
Checksum:              309


Coasting Arc #8 (Orbit 1636)
---------------------------------------

Vector Time (GMT): 2018/025/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1841741
47                 A    =         6777558
53  meter
 Y    =       -3918001
74  meter          E    =           
0016399
 Z    =       -5228697
59                 I    =           51
67764
 XDOT =       7322
954221                 Wp   =           87
66418
 YDOT =       1921
208387  meter/sec      RA   =            7
84377  deg
 ZDOT =       1143
557080                 TA   =          193
28877
                                          MA   =          193
33202
                                          Ha   =            221
932  n
mi
                                          Hp   =            213
621

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6042458
88                 X    =         1910814
80
 Y    =      -12854336
42  feet           Y    =        -3897019
84  meter
 Z    =      -17154519
66                 Z    =        -5219583
40
 XDOT =      24025
440358                 XDOT =        7295
371741
 YDOT =       6303
177124  feet/sec       YDOT =        2002
944443  meter/sec
 ZDOT =       3751
827689                 ZDOT =        1179
062217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8146523
66                 X    =        -2483060
41
 Y    =      -11695869
23  feet           Y    =        -3564900
94  meter
 Z    =      -17113258
43                 Z    =        -5216121
17
 XDOT =      16469
146999                 XDOT =        5019
796005
 YDOT =     -17173
635606  feet/sec       YDOT =       -5234
524133  meter/sec
 ZDOT =       3909
572596                 ZDOT =        1191
637727


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   18025
83696618  
00016717  00000-0  10270-3 0  9077
2 25544  51
6408   8
3599 0003688  41
2522 318
8909 15
54220545 16379


Satellite: ISS
Catalog Number: 25544
Epoch time:      18025
83696618   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:         8
3599  deg
Eccentricity:     
0003688     
Arg of perigee:    41
2522  deg
Mean anomaly:     318
8909  deg
Mean motion:   15
54220545  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1637
Checksum:              330


Coasting Arc #9 (Orbit 1652)
---------------------------------------

Vector Time (GMT): 2018/026/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3561741
28                 A    =         6780060
86  meter
 Y    =        3469158
56  meter          E    =           
0011951
 Z    =        4603883
53                 I    =           51
65430
 XDOT =      -6523
938794                 Wp   =           58
41348
 YDOT =      -2700
846543  meter/sec      RA   =            2
84885  deg
 ZDOT =      -3000
145767                 TA   =           61
55549
                                          MA   =           61
43513
                                          Ha   =            221
957  n
mi
                                          Hp   =            213
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11685502
90                 X    =        -3622632
68
 Y    =       11381753
82  feet           Y    =         3428988
13  meter
 Z    =       15104604
77                 Z    =         4586434
19
 XDOT =     -21403
998667                 XDOT =       -6478
679326
 YDOT =      -8861
045089  feet/sec       YDOT =       -2773
548545  meter/sec
 ZDOT =      -9842
997922                 ZDOT =       -3031
726688

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4360860
59                 X    =         1329190
31
 Y    =       15793580
87  feet           Y    =         4813883
45  meter
 Z    =       15026312
96                 Z    =         4580020
19
 XDOT =     -16836
118249                 XDOT =       -5131
648842
 YDOT =      14184
067980  feet/sec       YDOT =        4323
303920  meter/sec
 ZDOT =      -9983
127553                 ZDOT =       -3042
857278


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   18026
86574457  
00016717  00000-0  10270-3 0  9088
2 25544  51
6415   3
2311 0003628  41
7485 318
3944 15
54252492 16538


Satellite: ISS
Catalog Number: 25544
Epoch time:      18026
86574457   =   yrday
fracday
Element set:     908
Inclination:       51
6415  deg
RA of node:         3
2311  deg
Eccentricity:     
0003628     
Arg of perigee:    41
7485  deg
Mean anomaly:     318
3944  deg
Mean motion:   15
54252492  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1653
Checksum:              310


Coasting Arc #10 (Orbit 1667)
---------------------------------------

Vector Time (GMT): 2018/027/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4987174
12                 A    =         6783912
23  meter
 Y    =       -2970891
54  meter          E    =           
0007986
 Z    =       -3514836
85                 I    =           51
63306
 XDOT =       5187
729102                 Wp   =           73
39263
 YDOT =       3381
554412  meter/sec      RA   =          357
85924  deg
 ZDOT =       4513
326063                 TA   =          245
26210
                                          MA   =          245
34523
                                          Ha   =            222
007  n
mi
                                          Hp   =            213
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16362119
81                 X    =         5037097
80
 Y    =       -9747019
48  feet           Y    =        -2914842
24  meter
 Z    =      -11531616
95                 Z    =        -3490490
04
 XDOT =      17020
108604                 XDOT =        5127
606982
 YDOT =      11094
338623  feet/sec       YDOT =        3439
230781  meter/sec
 ZDOT =      14807
500206                 ZDOT =        4538
380097

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1028087
18                 X    =         -313360
97
 Y    =      -19083143
10  feet           Y    =        -5816542
02  meter
 Z    =      -11422706
73                 Z    =        -3481641
01
 XDOT =      16278
767863                 XDOT =        4961
768445
 YDOT =      -9785
545089  feet/sec       YDOT =       -2982
634143  meter/sec
 ZDOT =      14918
448625                 ZDOT =        4547
143141


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   18027
83022243  
00016717  00000-0  10270-3 0  9098
2 25544  51
6405 358
4211 0003630  46
9443 313
2013 15
54223685 16684


Satellite: ISS
Catalog Number: 25544
Epoch time:      18027
83022243   =   yrday
fracday
Element set:     909
Inclination:       51
6405  deg
RA of node:       358
4211  deg
Eccentricity:     
0003630     
Arg of perigee:    46
9443  deg
Mean anomaly:     313
2013  deg
Mean motion:   15
54223685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1668
Checksum:              286


Coasting Arc #11 (Orbit 1683)
---------------------------------------

Vector Time (GMT): 2018/028/19:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6033751
83                 A    =         6787319
09  meter
 Y    =        2356557
19  meter          E    =           
0016021
 Z    =        2007528
79                 I    =           51
61153
 XDOT =      -3430
287299                 Wp   =           99
64884
 YDOT =      -4013
475043  meter/sec      RA   =          352
87978  deg
 ZDOT =      -5563
449791                 TA   =           58
16154
                                          MA   =           58
00567
                                          Ha   =            222
010  n
mi
                                          Hp   =            213
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19795773
71                 X    =        -6069406
41
 Y    =        7731486
85  feet           Y    =         2288884
18  meter
 Z    =        6586380
53                 Z    =         1978132
92
 XDOT =     -11254
223423                 XDOT =       -3358
128728
 YDOT =     -13167
569038  feet/sec       YDOT =       -4051
431101  meter/sec
 ZDOT =     -18252
788027                 ZDOT =       -5579
937628

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1969177
94                 X    =         -600205
44
 Y    =       21201012
83  feet           Y    =         6462068
71  meter
 Z    =        6455102
45                 Z    =         1967515
23
 XDOT =     -15214
351760                 XDOT =       -4637
334416
 YDOT =       4202
370523  feet/sec       YDOT =        1280
882535  meter/sec
 ZDOT =     -18325
489403                 ZDOT =       -5585
609170


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   18028
85899427  
00016717  00000-0  10270-3 0  9109
2 25544  51
6401 353
2922 0003753  49
5891 310
5588 15
54256497 16846


Satellite: ISS
Catalog Number: 25544
Epoch time:      18028
85899427   =   yrday
fracday
Element set:     910
Inclination:       51
6401  deg
RA of node:       353
2922  deg
Eccentricity:     
0003753     
Arg of perigee:    49
5891  deg
Mean anomaly:     310
5588  deg
Mean motion:   15
54256497  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1684
Checksum:              339


Coasting Arc #12 (Orbit 1697)
---------------------------------------

Vector Time (GMT): 2018/029/16:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 905837
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3143463
18                 A    =         6778520
13  meter
 Y    =        3377853
72  meter          E    =           
0008321
 Z    =        4958855
36                 I    =           51
55545
 XDOT =      -6692
570253                 Wp   =           98
24124
 YDOT =       3089
714028  meter/sec      RA   =          348
50301  deg
 ZDOT =       2133
608234                 TA   =          330
94266
                                          MA   =          330
98894
                                          Ha   =            222
001  n
mi
                                          Hp   =            213
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10313199
40                 X    =         3081370
49
 Y    =       11082197
25  feet           Y    =         3412658
65  meter
 Z    =       16269210
48                 Z    =         4973974
25
 XDOT =     -21957
251486                 XDOT =       -6736
986592
 YDOT =      10136
857048  feet/sec       YDOT =        3014
624666  meter/sec
 ZDOT =       7000
027015                 ZDOT =        2100
991016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13686570
67                 X    =         4171666
74
 Y    =        6299170
97  feet           Y    =         1919987
31  meter
 Z    =       16335930
21                 Z    =         4979191
53
 XDOT =     -15943
546524                 XDOT =       -4859
592981
 YDOT =      16830
059719  feet/sec       YDOT =        5129
802202  meter/sec
 ZDOT =       6854
283805                 ZDOT =        2089
185704


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
75916998  
00016717  00000-0  10270-3 0  9113
2 25544  51
6422 348
8055 0003737  56
2343 303
9165 15
54221021 16982


Satellite: ISS
Catalog Number: 25544
Epoch time:      18029
75916998   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:       348
8055  deg
Eccentricity:     
0003737     
Arg of perigee:    56
2343  deg
Mean anomaly:     303
9165  deg
Mean motion:   15
54221021  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1698
Checksum:              319


Coasting Arc #13 (Orbit 1711)
---------------------------------------

Vector Time (GMT): 2018/030/15:25:29
261
Vector Time (MET): N/A
Weight (LBS)     : 905690
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1572859
39                 A    =         6777826
34  meter
 Y    =       -3934156
47  meter          E    =           
0017031
 Z    =       -5305028
97                 I    =           51
52110
 XDOT =       7258
081080                 Wp   =           80
97583
 YDOT =      -2407
851598  meter/sec      RA   =          343
81905  deg
 ZDOT =       -364
660899                 TA   =          185
52640
                                          MA   =          185
54522
                                          Ha   =            222
067  n
mi
                                          Hp   =            214
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5160299
83                 X    =        -1502981
33
 Y    =      -12907337
48  feet           Y    =        -3951354
35  meter
 Z    =      -17404950
69                 Z    =        -5312499
60
 XDOT =      23812
601968                 XDOT =        7286
238181
 YDOT =      -7899
775583  feet/sec       YDOT =       -2326
529311  meter/sec
 ZDOT =      -1196
394025                 ZDOT =        -329
336271

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5116562
74                 X    =        -1559528
32
 Y    =      -12880749
87  feet           Y    =        -3926052
56  meter
 Z    =      -17437529
42                 Z    =        -5314958
97
 XDOT =      22836
757215                 XDOT =        6960
643599
 YDOT =      -7658
019977  feet/sec       YDOT =       -2334
164489  meter/sec
 ZDOT =      -1038
721900                 ZDOT =        -316
602435


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
65934053  
00016717  00000-0  10270-3 0  9127
2 25544  51
6426 344
3167 0002779  47
0274 313
1112 15
53979371 17126


Satellite: ISS
Catalog Number: 25544
Epoch time:      18030
65934053   =   yrday
fracday
Element set:     912
Inclination:       51
6426  deg
RA of node:       344
3167  deg
Eccentricity:     
0002779     
Arg of perigee:    47
0274  deg
Mean anomaly:     313
1112  deg
Mean motion:   15
53979371  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1712
Checksum:              297


Coasting Arc #14 (Orbit 1727)
---------------------------------------

Vector Time (GMT): 2018/031/15:25:29
261
Vector Time (MET): N/A
Weight (LBS)     : 905690
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -114168
04                 A    =         6778490
09  meter
 Y    =        4422981
21  meter          E    =           
0007578
 Z    =        5131244
80                 I    =           51
49214
 XDOT =      -7357
614097                 Wp   =           52
11872
 YDOT =       1565
795967  meter/sec      RA   =          338
81215  deg
 ZDOT =      -1507
289882                 TA   =           52
45659
                                          MA   =           52
38776
                                          Ha   =            222
032  n
mi
                                          Hp   =            214
069

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -374567
07                 X    =         -188542
69
 Y    =       14511093
22  feet           Y    =         4421288
60  meter
 Z    =       16834792
65                 Z    =         5130509
63
 XDOT =     -24139
153860                 XDOT =       -7367
255016
 YDOT =       5137
125876  feet/sec       YDOT =        1483
464191  meter/sec
 ZDOT =      -4945
176777                 ZDOT =       -1543
052983

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -155765
53                 X    =          -47477
33
 Y    =       14519761
13  feet           Y    =         4425623
19  meter
 Z    =       16830764
83                 Z    =         5130017
12
 XDOT =     -22924
320684                 XDOT =       -6987
332945
 YDOT =       5694
331657  feet/sec       YDOT =        1735
632289  meter/sec
 ZDOT =      -5104
648323                 ZDOT =       -1555
896809


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
68828093  
00016717  00000-0  10270-3 0  9138
2 25544  51
6424 339
1889 0002755  48
6794 311
4596 15
54011241 17283


Satellite: ISS
Catalog Number: 25544
Epoch time:      18031
68828093   =   yrday
fracday
Element set:     913
Inclination:       51
6424  deg
RA of node:       339
1889  deg
Eccentricity:     
0002755     
Arg of perigee:    48
6794  deg
Mean anomaly:     311
4596  deg
Mean motion:   15
54011241  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1728
Checksum:              325


Coasting Arc #15 (Orbit 1742)
---------------------------------------

Vector Time (GMT): 2018/032/15:25:29
261
Vector Time (MET): N/A
Weight (LBS)     : 905690
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1695033
54                 A    =         6781324
75  meter
 Y    =       -4809555
50  meter          E    =           
0011034
 Z    =       -4480371
93                 I    =           51
47082
 XDOT =       6928
043687                 Wp   =           97
90880
 YDOT =       -551
666225  meter/sec      RA   =          333
80833  deg
 ZDOT =       3218
572246                 TA   =          204
55670
                                          MA   =          204
60929
                                          Ha   =            222
099  n
mi
                                          Hp   =            214
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5561133
66                 X    =         1770451
96
 Y    =      -15779381
56  feet           Y    =        -4790178
87  meter
 Z    =      -14699382
97                 Z    =        -4471955
01
 XDOT =      22729
802124                 XDOT =        6918
063997
 YDOT =      -1809
928559  feet/sec       YDOT =        -474
247823  meter/sec
 ZDOT =      10559
620230                 ZDOT =        3252
201069

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5023631
56                 X    =         1531202
90
 Y    =      -15993814
32  feet           Y    =        -4874914
60  meter
 Z    =      -14661104
30                 Z    =        -4468704
59
 XDOT =      21403
143366                 XDOT =        6523
678098
 YDOT =      -3078
276865  feet/sec       YDOT =        -938
258788  meter/sec
 ZDOT =      10709
409929                 ZDOT =        3264
228146


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
65291172  
00016717  00000-0  10270-3 0  9149
2 25544  51
6422 334
3822 0002722  51
8033 308
3365 15
53974990 17435


Satellite: ISS
Catalog Number: 25544
Epoch time:      18032
65291172   =   yrday
fracday
Element set:     914
Inclination:       51
6422  deg
RA of node:       334
3822  deg
Eccentricity:     
0002722     
Arg of perigee:    51
8033  deg
Mean anomaly:     308
3365  deg
Mean motion:   15
53974990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1743
Checksum:              298


Coasting Arc #16 (Orbit 1758)
---------------------------------------

Vector Time (GMT): 2018/033/15:25:29
261
Vector Time (MET): N/A
Weight (LBS)     : 905690
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3102649
33                 A    =         6785006
09  meter
 Y    =        5005676
63  meter          E    =           
0014946
 Z    =        3358021
58                 I    =           51
45459
 XDOT =      -6076
133350                 Wp   =           84
55619
 YDOT =       -641
662174  meter/sec      RA   =          328
81112  deg
 ZDOT =      -4638
344254                 TA   =           56
14810
                                          MA   =           56
00595
                                          Ha   =            222
168  n
mi
                                          Hp   =            214
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10179295
71                 X    =        -3174704
63
 Y    =       16422823
58  feet           Y    =         4970577
95  meter
 Z    =       11017131
16                 Z    =         3342775
15
 XDOT =     -19934
820701                 XDOT =       -6045
976498
 YDOT =      -2105
190860  feet/sec       YDOT =        -709
441265  meter/sec
 ZDOT =     -15217
664875                 ZDOT =       -4667
785934

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9297347
81                 X    =        -2833831
61
 Y    =       16982211
94  feet           Y    =         5176178
20  meter
 Z    =       10948432
58                 Z    =         3337082
25
 XDOT =     -18683
592270                 XDOT =       -5694
758924
 YDOT =       -292
683086  feet/sec       YDOT =         -89
209805  meter/sec
 ZDOT =     -15348
608260                 ZDOT =       -4678
255798


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
68184592  
00016717  00000-0  10270-3 0  9151
2 25544  51
6426 329
2546 0002817  55
8007 304
3412 15
53991485 17599


Satellite: ISS
Catalog Number: 25544
Epoch time:      18033
68184592   =   yrday
fracday
Element set:     915
Inclination:       51
6426  deg
RA of node:       329
2546  deg
Eccentricity:     
0002817     
Arg of perigee:    55
8007  deg
Mean anomaly:     304
3412  deg
Mean motion:   15
53991485  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1759
Checksum:              324
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