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

 
Date: March 1st 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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


060/14:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 214 1

063/17:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 214 1

069/22:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 0
000/00:00:00 000 0 0 0 0 214 4

072/21:25:54 349 -0 6 0 7 0 7
N/A 0 4 -0 0 220 8
000/00:01:48 697 0 2 -0 0 215 0

073/06:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 9
000/00:00:00 000 0 0 0 0 215 0

Coasting Arc #1 (Orbit 2160)
---------------------------------------

Vector Time (GMT): 2018/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6290521
56                 A    =         6789136
77  meter
 Y    =        2510599
34  meter          E    =           
0014479
 Z    =        -351438
50                 I    =           51
52673
 XDOT =      -2052
798548                 Wp   =          139
20444
 YDOT =       4325
693803  meter/sec      RA   =          199
39414  deg
 ZDOT =      -5992
265712                 TA   =           44
59061
                                          MA   =           44
47422
                                          Ha   =            221
734  n
mi
                                          Hp   =            213
888

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20638194
11                 X    =         6263686
90
 Y    =        8236874
47  feet           Y    =         2580794
20  meter
 Z    =       -1153013
46                 Z    =         -320947
49
 XDOT =      -6734
903373                 XDOT =       -2071
910525
 YDOT =      14191
908801  feet/sec       YDOT =        4302
630625  meter/sec
 ZDOT =     -19659
664411                 ZDOT =       -6002
284032

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15890902
22                 X    =         4843547
00
 Y    =       15542028
20  feet           Y    =         4737210
20  meter
 Z    =       -1017439
39                 Z    =         -310115
53
 XDOT =     -10420
301870                 XDOT =       -3176
108010
 YDOT =       9400
841379  feet/sec       YDOT =        2865
376452  meter/sec
 ZDOT =     -19704
802424                 ZDOT =       -6006
023779


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   18059
53159838  
00016717  00000-0  10270-3 0  9002
2 25544  51
6375 200
3882 0003034 145
3158 214
8193 15
54181080 21610


Satellite: ISS
Catalog Number: 25544
Epoch time:      18059
53159838   =   yrday
fracday
Element set:     900
Inclination:       51
6375  deg
RA of node:       200
3882  deg
Eccentricity:     
0003034     
Arg of perigee:   145
3158  deg
Mean anomaly:     214
8193  deg
Mean motion:   15
54181080  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2161
Checksum:              296


Coasting Arc #2 (Orbit 2176)
---------------------------------------

Vector Time (GMT): 2018/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5680787
15                 A    =         6787479
42  meter
 Y    =       -3110357
67  meter          E    =           
0014759
 Z    =        2013103
23                 I    =           51
55470
 XDOT =       3921
653662                 Wp   =           80
54660
 YDOT =      -3545
819207  meter/sec      RA   =          194
41576  deg
 ZDOT =       5555
634726                 TA   =          301
72420
                                          MA   =          301
86797
                                          Ha   =            221
702  n
mi
                                          Hp   =            213
951

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18637753
11                 X    =        -5655362
44
 Y    =      -10204585
54  feet           Y    =        -3173741
76  meter
 Z    =        6604669
39                 Z    =         1985570
70
 XDOT =      12866
317788                 XDOT =        3934
026809
 YDOT =     -11633
265114  feet/sec       YDOT =       -3501
894779  meter/sec
 ZDOT =      18227
148050                 ZDOT =        5574
714747

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13604676
07                 X    =        -4146705
27
 Y    =      -16371111
22  feet           Y    =        -4989914
70  meter
 Z    =        6482327
60                 Z    =         1975813
45
 XDOT =      14941
864337                 XDOT =        4554
280250
 YDOT =      -5122
974109  feet/sec       YDOT =       -1561
482509  meter/sec
 ZDOT =      18312
577539                 ZDOT =        5581
673634


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   18060
56040556  
00016717  00000-0  10270-3 0  9014
2 25544  51
6396 195
2593 0003133 149
3167 210
8169 15
54196812 21773


Satellite: ISS
Catalog Number: 25544
Epoch time:      18060
56040556   =   yrday
fracday
Element set:     901
Inclination:       51
6396  deg
RA of node:       195
2593  deg
Eccentricity:     
0003133     
Arg of perigee:   149
3167  deg
Mean anomaly:     210
8169  deg
Mean motion:   15
54196812  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2177
Checksum:              311


Coasting Arc #3 (Orbit 2177)
---------------------------------------

Vector Time (GMT): 2018/060/14:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2846232
98                 A    =         6781106
79  meter
 Y    =        4308902
12  meter          E    =           
0009786
 Z    =       -4403687
47                 I    =           51
53737
 XDOT =      -6801
441232                 Wp   =           87
47501
 YDOT =       1064
982842  meter/sec      RA   =          193
91227  deg
 ZDOT =      -3359
955513                 TA   =          148
48787
                                          MA   =          148
42922
                                          Ha   =            221
684  n
mi
                                          Hp   =            214
100

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9338034
72                 X    =         2819228
42
 Y    =       14136817
97  feet           Y    =         4340579
16  meter
 Z    =      -14447793
55                 Z    =        -4389927
87
 XDOT =     -22314
439737                 XDOT =       -6796
524158
 YDOT =       3494
038196  feet/sec       YDOT =         988
951562  meter/sec
 ZDOT =     -11023
476094                 ZDOT =       -3392
981950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12838162
24                 X    =         3913071
85
 Y    =       11134815
96  feet           Y    =         3393891
90  meter
 Z    =      -14386963
44                 Z    =        -4385146
46
 XDOT =     -19711
491542                 XDOT =       -6008
062622
 YDOT =       8319
155003  feet/sec       YDOT =        2535
678445  meter/sec
 ZDOT =     -11170
775750                 ZDOT =       -3404
852449


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   18060
62470634  
00016717  00000-0  10270-3 0  9026
2 25544  51
6408 194
9406 0002983 151
3421 208
7896 15
54156065 21784


Satellite: ISS
Catalog Number: 25544
Epoch time:      18060
62470634   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:       194
9406  deg
Eccentricity:     
0002983     
Arg of perigee:   151
3421  deg
Mean anomaly:     208
7896  deg
Mean motion:   15
54156065  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2178
Checksum:              314


Coasting Arc #4 (Orbit 2193)
---------------------------------------

Vector Time (GMT): 2018/061/14:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1153228
23                 A    =         6778030
32  meter
 Y    =       -4290673
90  meter          E    =           
0007726
 Z    =        5115431
17                 I    =           51
56019
 XDOT =       7502
897325                 Wp   =          135
75162
 YDOT =       -105
712046  meter/sec      RA   =          188
91162  deg
 ZDOT =       1595
916939                 TA   =          298
80713
                                          MA   =          298
88468
                                          Ha   =            221
588  n
mi
                                          Hp   =            214
022

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3783557
19                 X    =        -1130010
61
 Y    =      -14077014
12  feet           Y    =        -4303439
59  meter
 Z    =       16782910
66                 Z    =         5109886
27
 XDOT =      24615
804872                 XDOT =        7495
769831
 YDOT =       -346
824299  feet/sec       YDOT =         -21
849128  meter/sec
 ZDOT =       5235
947962                 ZDOT =        1632
345379

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7695525
37                 X    =        -2345596
13
 Y    =      -12412465
69  feet           Y    =        -3783319
54  meter
 Z    =       16758678
55                 Z    =         5108045
22
 XDOT =      22586
124922                 XDOT =        6884
250876
 YDOT =      -6683
994242  feet/sec       YDOT =       -2037
281445  meter/sec
 ZDOT =       5398
315851                 ZDOT =        1645
406671


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   18061
65350919  
00016717  00000-0  10270-3 0  9034
2 25544  51
6412 189
8122 0002901 153
4933 206
6368 15
54202527 21942


Satellite: ISS
Catalog Number: 25544
Epoch time:      18061
65350919   =   yrday
fracday
Element set:     903
Inclination:       51
6412  deg
RA of node:       189
8122  deg
Eccentricity:     
0002901     
Arg of perigee:   153
4933  deg
Mean anomaly:     206
6368  deg
Mean motion:   15
54202527  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2194
Checksum:              300


Coasting Arc #5 (Orbit 2208)
---------------------------------------

Vector Time (GMT): 2018/062/14:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -689006
92                 A    =         6777262
73  meter
 Y    =        4172739
52  meter          E    =           
0016248
 Z    =       -5309665
97                 I    =           51
58936
 XDOT =      -7606
399653                 Wp   =          101
87159
 YDOT =       -801
550596  meter/sec      RA   =          183
90782  deg
 ZDOT =        354
776428                 TA   =          171
53218
                                          MA   =          171
50473
                                          Ha   =            221
527  n
mi
                                          Hp   =            214
101

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2260521
39                 X    =         -709825
25
 Y    =       13690090
30  feet           Y    =         4164917
40  meter
 Z    =      -17420163
95                 Z    =        -5313064
05
 XDOT =     -24955
379438                 XDOT =       -7598
594468
 YDOT =      -2629
759173  feet/sec       YDOT =        -886
566894  meter/sec
 ZDOT =       1163
964659                 ZDOT =         317
846827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2026787
06                 X    =          617764
69
 Y    =       13706806
66  feet           Y    =         4177834
67  meter
 Z    =      -17435774
34                 Z    =        -5314424
02
 XDOT =     -23614
086838                 XDOT =       -7197
573668
 YDOT =       4772
881279  feet/sec       YDOT =        1454
774214  meter/sec
 ZDOT =        999
448714                 ZDOT =         304
631968


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   18062
61801092  
00016717  00000-0  10270-3 0  9045
2 25544  51
6405 185
0046 0002824 156
8346 203
2934 15
54172113 22092


Satellite: ISS
Catalog Number: 25544
Epoch time:      18062
61801092   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       185
0046  deg
Eccentricity:     
0002824     
Arg of perigee:   156
8346  deg
Mean anomaly:     203
2934  deg
Mean motion:   15
54172113  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2209
Checksum:              281


Coasting Arc #6 (Orbit 2224)
---------------------------------------

Vector Time (GMT): 2018/063/14:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2482165
70                 A    =         6778704
65  meter
 Y    =       -3942636
71  meter          E    =           
0006410
 Z    =        4918751
75                 I    =           51
62865
 XDOT =       7138
989079                 Wp   =           82
51202
 YDOT =       1660
200636  meter/sec      RA   =          178
90656  deg
 ZDOT =      -2268
483084                 TA   =           29
66155
                                          MA   =           29
62522
                                          Ha   =            221
308  n
mi
                                          Hp   =            214
142

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8143588
24                 X    =         2502176
41
 Y    =      -12935159
79  feet           Y    =        -3914766
83  meter
 Z    =       16137636
98                 Z    =         4930858
28
 XDOT =      23421
880179                 XDOT =        7130
912658
 YDOT =       5446
852479  feet/sec       YDOT =        1739
988237  meter/sec
 ZDOT =      -7442
529804                 ZDOT =       -2233
824595

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3568105
49                 X    =         1087558
55
 Y    =      -14803584
71  feet           Y    =        -4512132
62  meter
 Z    =       16192041
83                 Z    =         4935334
35
 XDOT =      22913
899121                 XDOT =        6984
156452
 YDOT =      -2460
843725  feet/sec       YDOT =        -750
065167  meter/sec
 ZDOT =      -7288
217408                 ZDOT =       -2221
448666


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   18063
64680620  
00016717  00000-0  10270-3 0  9052
2 25544  51
6415 179
8755 0002701 160
9368 199
1887 15
54222760 22257


Satellite: ISS
Catalog Number: 25544
Epoch time:      18063
64680620   =   yrday
fracday
Element set:     905
Inclination:       51
6415  deg
RA of node:       179
8755  deg
Eccentricity:     
0002701     
Arg of perigee:   160
9368  deg
Mean anomaly:     199
1887  deg
Mean motion:   15
54222760  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2225
Checksum:              323


Coasting Arc #7 (Orbit 2226)
---------------------------------------

Vector Time (GMT): 2018/063/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3208786
40                 A    =         6779739
85  meter
 Y    =       -3648532
73  meter          E    =           
0010280
 Z    =        4723795
13                 I    =           51
63409
 XDOT =       6757
817418                 Wp   =          126
05375
 YDOT =      -2371
551190  meter/sec      RA   =          178
34913  deg
 ZDOT =       2748
635601                 TA   =          296
70087
                                          MA   =          296
80607
                                          Ha   =            221
615  n
mi
                                          Hp   =            214
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10527514
43                 X    =        -3190694
50
 Y    =      -11970251
73  feet           Y    =        -3684313
75  meter
 Z    =       15498015
52                 Z    =         4708252
59
 XDOT =      22171
316989                 XDOT =        6770
483212
 YDOT =      -7780
679758  feet/sec       YDOT =       -2295
909419  meter/sec
 ZDOT =       9017
833336                 ZDOT =        2781
493481

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15587565
41                 X    =        -4751089
94
 Y    =        3643286
56  feet           Y    =         1110473
74  meter
 Z    =       15429136
05                 Z    =         4702800
67
 XDOT =       3959
851517                 XDOT =        1206
962742
 YDOT =     -22010
503382  feet/sec       YDOT =       -6708
801431  meter/sec
 ZDOT =       9164
568376                 ZDOT =        2793
360441


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   18063
77540677  
00016717  00000-0  10270-3 0  9064
2 25544  51
6400 179
2355 0002741 152
0229 208
1071 15
54196933 22273


Satellite: ISS
Catalog Number: 25544
Epoch time:      18063
77540677   =   yrday
fracday
Element set:     906
Inclination:       51
6400  deg
RA of node:       179
2355  deg
Eccentricity:     
0002741     
Arg of perigee:   152
0229  deg
Mean anomaly:     208
1071  deg
Mean motion:   15
54196933  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2227
Checksum:              301


Coasting Arc #8 (Orbit 2241)
---------------------------------------

Vector Time (GMT): 2018/064/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1457772
63                 A    =         6777474
19  meter
 Y    =        4024575
38  meter          E    =           
0015394
 Z    =       -5267886
31                 I    =           51
66018
 XDOT =      -7445
800273                 Wp   =           92
97148
 YDOT =       1561
119473  meter/sec      RA   =          173
35238  deg
 ZDOT =       -870
772226                 TA   =          168
70951
                                          MA   =          168
67494
                                          Ha   =            221
470  n
mi
                                          Hp   =            214
183

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4782718
60                 X    =         1438248
82
 Y    =       13203987
46  feet           Y    =         4040767
35  meter
 Z    =      -17283091
56                 Z    =        -5260852
95
 XDOT =     -24428
478587                 XDOT =       -7458
474029
 YDOT =       5121
783049  feet/sec       YDOT =        1477
784439  meter/sec
 ZDOT =      -2856
864257                 ZDOT =        -906
972050

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13972933
50                 X    =         4258950
13
 Y    =        1744771
60  feet           Y    =          531806
38  meter
 Z    =      -17252183
55                 Z    =        -5258465
55
 XDOT =      -6586
804945                 XDOT =       -2007
658147
 YDOT =      23000
980706  feet/sec       YDOT =        7010
698919  meter/sec
 ZDOT =      -3018
423505                 ZDOT =        -920
015484


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   18064
73989883  
00016717  00000-0  10270-3 0  9078
2 25544  51
6409 174
4275 0002667 156
8506 203
2767 15
54184350 22422


Satellite: ISS
Catalog Number: 25544
Epoch time:      18064
73989883   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       174
4275  deg
Eccentricity:     
0002667     
Arg of perigee:   156
8506  deg
Mean anomaly:     203
2767  deg
Mean motion:   15
54184350  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2242
Checksum:              334


Coasting Arc #9 (Orbit 2257)
---------------------------------------

Vector Time (GMT): 2018/065/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         370133
97                 A    =         6777467
38  meter
 Y    =       -4292998
73  meter          E    =           
0004165
 Z    =        5227718
51                 I    =           51
69112
 XDOT =       7563
684287                 Wp   =           97
05089
 YDOT =       -677
988220  meter/sec      RA   =          168
35467  deg
 ZDOT =      -1092
043329                 TA   =            3
40170
                                          MA   =            3
39887
                                          Ha   =            221
430  n
mi
                                          Hp   =            214
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1214350
28                 X    =          392718
58
 Y    =      -14084641
50  feet           Y    =        -4288732
77  meter
 Z    =       17151307
44                 Z    =         5229571
82
 XDOT =      24815
237162                 XDOT =        7576
008129
 YDOT =      -2224
370800  feet/sec       YDOT =        -593
337118  meter/sec
 ZDOT =      -3582
819320                 ZDOT =       -1055
271786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12114705
43                 X    =        -3692562
21
 Y    =       -7265374
86  feet           Y    =        -2214486
26  meter
 Z    =       17160051
29                 Z    =         5230383
63
 XDOT =       8554
441826                 XDOT =        2607
393869
 YDOT =     -22340
897469  feet/sec       YDOT =       -6809
505548  meter/sec
 ZDOT =      -3418
791184                 ZDOT =       -1042
047553


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   18065
76868579  
00016717  00000-0  10270-3 0  9081
2 25544  51
6390 169
2987 0002675 157
5534 202
5736 15
54209675 22584


Satellite: ISS
Catalog Number: 25544
Epoch time:      18065
76868579   =   yrday
fracday
Element set:     908
Inclination:       51
6390  deg
RA of node:       169
2987  deg
Eccentricity:     
0002675     
Arg of perigee:   157
5534  deg
Mean anomaly:     202
5736  deg
Mean motion:   15
54209675  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2258
Checksum:              359


Coasting Arc #10 (Orbit 2272)
---------------------------------------

Vector Time (GMT): 2018/066/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2131374
13                 A    =         6779947
46  meter
 Y    =        4464040
29  meter          E    =           
0012150
 Z    =       -4648552
98                 I    =           51
73252
 XDOT =      -7064
220146                 Wp   =          119
59398
 YDOT =       -310
300548  meter/sec      RA   =          163
36274  deg
 ZDOT =       2940
906265                 TA   =          179
68894
                                          MA   =          179
68819
                                          Ha   =            221
325  n
mi
                                          Hp   =            214
213

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6992697
27                 X    =        -2158553
74
 Y    =       14645801
49  feet           Y    =         4440053
39  meter
 Z    =      -15251158
06                 Z    =        -4658972
83
 XDOT =     -23176
575281                 XDOT =       -7074
510546
 YDOT =      -1018
046416  feet/sec       YDOT =        -389
354768  meter/sec
 ZDOT =       9648
642601                 ZDOT =        2906
565972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10251958
44                 X    =         3124796
93
 Y    =       12524369
73  feet           Y    =         3817427
89  meter
 Z    =      -15298125
69                 Z    =        -4662868
71
 XDOT =     -10008
257558                 XDOT =       -3050
516904
 YDOT =      19791
176585  feet/sec       YDOT =        6032
350623  meter/sec
 ZDOT =       9495
547361                 ZDOT =        2894
242836


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   18066
73316853  
00016717  00000-0  10270-3 0  9093
2 25544  51
6402 164
4905 0002479 163
6756 196
4477 15
54191845 22730


Satellite: ISS
Catalog Number: 25544
Epoch time:      18066
73316853   =   yrday
fracday
Element set:     909
Inclination:       51
6402  deg
RA of node:       164
4905  deg
Eccentricity:     
0002479     
Arg of perigee:   163
6756  deg
Mean anomaly:     196
4477  deg
Mean motion:   15
54191845  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2273
Checksum:              337


Coasting Arc #11 (Orbit 2288)
---------------------------------------

Vector Time (GMT): 2018/067/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3670858
37                 A    =         6783584
87  meter
 Y    =       -4458713
95  meter          E    =           
0012836
 Z    =        3545633
32                 I    =           51
77503
 XDOT =       6058
913132                 Wp   =           97
98937
 YDOT =       1405
585581  meter/sec      RA   =          158
38149  deg
 ZDOT =      -4493
195315                 TA   =           40
25251
                                          MA   =           40
15754
                                          Ha   =            221
174  n
mi
                                          Hp   =            214
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12043498
58                 X    =         3703221
39
 Y    =      -14628326
62  feet           Y    =        -4417482
64  meter
 Z    =       11632655
25                 Z    =         3563543
93
 XDOT =      19878
323923                 XDOT =        6064
570609
 YDOT =       4611
501250  feet/sec       YDOT =        1473
371767  meter/sec
 ZDOT =     -14741
454447                 ZDOT =       -4463
749799

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8345047
51                 X    =        -2543570
48
 Y    =      -16956336
90  feet           Y    =        -5168291
49  meter
 Z    =       11713039
19                 Z    =         3570134
34
 XDOT =      11245
142271                 XDOT =        3427
519364
 YDOT =     -15654
086147  feet/sec       YDOT =       -4771
365458  meter/sec
 ZDOT =     -14610
294339                 ZDOT =       -4453
217715


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   18067
76194451  
00016717  00000-0  10270-3 0  9107
2 25544  51
6388 159
3612 0002391 163
6274 196
4956 15
54243369 22897


Satellite: ISS
Catalog Number: 25544
Epoch time:      18067
76194451   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       159
3612  deg
Eccentricity:     
0002391     
Arg of perigee:   163
6274  deg
Mean anomaly:     196
4956  deg
Mean motion:   15
54243369  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2289
Checksum:              338


Coasting Arc #12 (Orbit 2303)
---------------------------------------

Vector Time (GMT): 2018/068/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4851662
78                 A    =         6787081
34  meter
 Y    =        4262800
69  meter          E    =           
0005339
 Z    =       -2086219
97                 I    =           51
81634
 XDOT =      -4628
575284                 Wp   =           64
61207
 YDOT =      -2560
528037  meter/sec      RA   =          153
41380  deg
 ZDOT =       5545
441927                 TA   =          272
36732
                                          MA   =          272
42845
                                          Ha   =            221
198  n
mi
                                          Hp   =            214
203

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15917528
80                 X    =        -4888836
32
 Y    =       13985566
56  feet           Y    =         4208338
05  meter
 Z    =       -6844553
70                 Z    =        -2109878
08
 XDOT =     -15185
614448                 XDOT =       -4626
535363
 YDOT =      -8400
682536  feet/sec       YDOT =       -2612
276109  meter/sec
 ZDOT =      18193
707108                 ZDOT =        5522
963263

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6487637
23                 X    =         1977431
83
 Y    =       20134843
27  feet           Y    =         6137100
23  meter
 Z    =       -6950565
45                 Z    =        -2118532
35
 XDOT =     -12341
895267                 XDOT =       -3761
809677
 YDOT =      10207
817063  feet/sec       YDOT =        3111
342641  meter/sec
 ZDOT =      18093
738281                 ZDOT =        5514
971428


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   18068
72641922  
00016717  00000-0  10270-3 0  9115
2 25544  51
6383 154
5534 0002523 166
7810 193
3409 15
54245499 23042


Satellite: ISS
Catalog Number: 25544
Epoch time:      18068
72641922   =   yrday
fracday
Element set:     911
Inclination:       51
6383  deg
RA of node:       154
5534  deg
Eccentricity:     
0002523     
Arg of perigee:   166
7810  deg
Mean anomaly:     193
3409  deg
Mean motion:   15
54245499  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2304
Checksum:              311


Coasting Arc #13 (Orbit 2319)
---------------------------------------

Vector Time (GMT): 2018/069/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5615118
01                 A    =         6788959
02  meter
 Y    =       -3784389
93  meter          E    =           
0014665
 Z    =         365954
37                 I    =           51
85079
 XDOT =       2927
765833                 Wp   =          136
93526
 YDOT =       3749
437217  meter/sec      RA   =          148
45444  deg
 ZDOT =      -6018
041103                 TA   =           39
12981
                                          MA   =           39
02385
                                          Ha   =            221
154  n
mi
                                          Hp   =            214
315

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18422303
17                 X    =         5655241
16
 Y    =      -12415977
45  feet           Y    =        -3721373
45  meter
 Z    =        1200637
69                 Z    =          393328
11
 XDOT =       9605
530948                 XDOT =        2914
853173
 YDOT =      12301
303204  feet/sec       YDOT =        3782
104846  meter/sec
 ZDOT =     -19744
229341                 ZDOT =       -6003
850835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4409371
77                 X    =        -1343976
52
 Y    =      -21766623
50  feet           Y    =        -6634466
84  meter
 Z    =        1323186
75                 Z    =          403307
32
 XDOT =      13504
806750                 XDOT =        4116
265098
 YDOT =      -3955
940354  feet/sec       YDOT =       -1205
770620  meter/sec
 ZDOT =     -19681
361124                 ZDOT =       -5998
878871


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   18069
75518747  
00016717  00000-0  10270-3 0  9128
2 25544  51
6377 149
4234 0002333 171
1804 188
9390 15
54233187 23205


Satellite: ISS
Catalog Number: 25544
Epoch time:      18069
75518747   =   yrday
fracday
Element set:     912
Inclination:       51
6377  deg
RA of node:       149
4234  deg
Eccentricity:     
0002333     
Arg of perigee:   171
1804  deg
Mean anomaly:     188
9390  deg
Mean motion:   15
54233187  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2320
Checksum:              317


Coasting Arc #14 (Orbit 2322)
---------------------------------------

Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =           3253
09                 A    =         6778603
47  meter
 Y    =        4630582
23  meter          E    =           
0013327
 Z    =       -4962809
08                 I    =           51
82455
 XDOT =      -6936
452235                 Wp   =          115
17988
 YDOT =       2375
552196  meter/sec      RA   =          147
37943  deg
 ZDOT =       2211
093807                 TA   =          176
37286
                                          MA   =          176
36319
                                          Ha   =            221
039  n
mi
                                          Hp   =            214
418

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          10672
88                 X    =          -24421
13
 Y    =       15192198
91  feet           Y    =         4630463
49  meter
 Z    =      -16282182
03                 Z    =        -4962860
85
 XDOT =     -22757
389224                 XDOT =       -6973
240986
 YDOT =       7793
806417  feet/sec       YDOT =        2297
778491  meter/sec
 ZDOT =       7254
244772                 ZDOT =        2177
309769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8715058
32                 X    =         2656349
78
 Y    =      -12442901
64  feet           Y    =        -3792596
42  meter
 Z    =      -16282949
07                 Z    =        -4963042
88
 XDOT =      22190
212837                 XDOT =        6763
576873
 YDOT =       6242
898353  feet/sec       YDOT =        1902
835418  meter/sec
 ZDOT =       7103
258247                 ZDOT =        2165
073114


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   18069
94808195  
00016717  00000-0  10270-3 0  9139
2 25544  51
6400 148
4620 0002184 176
3508 183
7661 15
54234074 23235


Satellite: ISS
Catalog Number: 25544
Epoch time:      18069
94808195   =   yrday
fracday
Element set:     913
Inclination:       51
6400  deg
RA of node:       148
4620  deg
Eccentricity:     
0002184     
Arg of perigee:   176
3508  deg
Mean anomaly:     183
7661  deg
Mean motion:   15
54234074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2323
Checksum:              308


Coasting Arc #15 (Orbit 2338)
---------------------------------------

Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1550769
70                 A    =         6782038
14  meter
 Y    =       -5207387
59  meter          E    =           
0010510
 Z    =        4049833
79                 I    =           51
86325
 XDOT =       6499
458371                 Wp   =           89
67496
 YDOT =      -1120
168561  meter/sec      RA   =          142
40139  deg
 ZDOT =      -3920
304527                 TA   =           40
87804
                                          MA   =           40
79927
                                          Ha   =            221
017  n
mi
                                          Hp   =            214
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5087827
10                 X    =         1589213
16
 Y    =      -17084604
96  feet           Y    =        -5189830
54  meter
 Z    =       13286856
26                 Z    =         4057460
58
 XDOT =      21323
682321                 XDOT =        6530
543875
 YDOT =      -3675
093704  feet/sec       YDOT =       -1047
313659  meter/sec
 ZDOT =     -12861
891492                 ZDOT =       -3888
657237

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13790501
90                 X    =        -4203344
98
 Y    =       11254785
31  feet           Y    =         3430458
56  meter
 Z    =       13321491
12                 Z    =         4060390
49
 XDOT =     -18909
589411                 XDOT =       -5763
642852
 YDOT =      -8079
338331  feet/sec       YDOT =       -2462
582323  meter/sec
 ZDOT =     -12720
564040                 ZDOT =       -3877
227919


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   18070
97684418  
00016717  00000-0  10270-3 0  9145
2 25544  51
6401 143
3337 0002162 177
8891 182
2271 15
54228333 23391


Satellite: ISS
Catalog Number: 25544
Epoch time:      18070
97684418   =   yrday
fracday
Element set:     914
Inclination:       51
6401  deg
RA of node:       143
3337  deg
Eccentricity:     
0002162     
Arg of perigee:   177
8891  deg
Mean anomaly:     182
2271  deg
Mean motion:   15
54228333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2339
Checksum:              310


Coasting Arc #16 (Orbit 2353)
---------------------------------------

Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904792
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2859379
01                 A    =         6785785
85  meter
 Y    =        5521613
18  meter          E    =           
0003978
 Z    =       -2719896
89                 I    =           51
90188
 XDOT =      -5625
423768                 Wp   =           83
93833
 YDOT =       -359
505398  meter/sec      RA   =          137
43461  deg
 ZDOT =       5191
001133                 TA   =          245
44783
                                          MA   =          245
48929
                                          Ha   =            220
914  n
mi
                                          Hp   =            214
464

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9381164
74                 X    =        -2907699
04
 Y    =       18115528
81  feet           Y    =         5489367
22  meter
 Z    =       -8923546
21                 Z    =        -2733904
41
 XDOT =     -18456
114723                 XDOT =       -5646
200370
 YDOT =      -1179
479652  feet/sec       YDOT =        -422
528453  meter/sec
 ZDOT =      17030
843612                 ZDOT =        5163
624748

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17768629
67                 X    =         5415878
32
 Y    =       -9966111
70  feet           Y    =        -3037670
85  meter
 Z    =       -8986697
40                 Z    =        -2739145
37
 XDOT =      14110
238401                 XDOT =        4300
800664
 YDOT =       9930
505299  feet/sec       YDOT =        3026
818015  meter/sec
 ZDOT =      16908
730078                 ZDOT =        5153
780928


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   18071
94130519  
00016717  00000-0  10270-3 0  9152
2 25544  51
6405 138
5249 0002146 182
9591 177
1549 15
54252249 23540


Satellite: ISS
Catalog Number: 25544
Epoch time:      18071
94130519   =   yrday
fracday
Element set:     915
Inclination:       51
6405  deg
RA of node:       138
5249  deg
Eccentricity:     
0002146     
Arg of perigee:   182
9591  deg
Mean anomaly:     177
1549  deg
Mean motion:   15
54252249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2354
Checksum:              316


Coasting Arc #17 (Orbit 2368)
---------------------------------------

Vector Time (GMT): 2018/072/21:26:48
697
Vector Time (MET): N/A
Weight (LBS)     : 904718
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1089239
79                 A    =         6779080
92  meter
 Y    =        4528725
42  meter          E    =           
0012120
 Z    =       -4936732
76                 I    =           51
90052
 XDOT =      -6124
826688                 Wp   =          116
46689
 YDOT =       3981
502506  meter/sec      RA   =          132
68061  deg
 ZDOT =       2300
164506                 TA   =          175
97354
                                          MA   =          175
96378
                                          Ha   =            220
845  n
mi
                                          Hp   =            215
008

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3573621
35                 X    =         1062497
07
 Y    =       14858023
04  feet           Y    =         4540756
01  meter
 Z    =      -16196629
80                 Z    =        -4931507
12
 XDOT =     -20094
575747                 XDOT =       -6180
066540
 YDOT =      13062
672265  feet/sec       YDOT =        3912
701855  meter/sec
 ZDOT =       7546
471475                 ZDOT =        2270
278105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8513733
82                 X    =         2594986
07
 Y    =      -12719492
45  feet           Y    =        -3876901
30  meter
 Z    =      -16173845
66                 Z    =        -4929788
16
 XDOT =      22290
538981                 XDOT =        6794
156281
 YDOT =       5490
570410  feet/sec       YDOT =        1673
525861  meter/sec
 ZDOT =       7412
632316                 ZDOT =        2259
370330


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   18072
90576356  
00016717  00000-0  10270-3 0  9163
2 25544  51
6404 133
7161 0002054 204
0936 156
0120 15
54117192 23690


Satellite: ISS
Catalog Number: 25544
Epoch time:      18072
90576356   =   yrday
fracday
Element set:     916
Inclination:       51
6404  deg
RA of node:       133
7161  deg
Eccentricity:     
0002054     
Arg of perigee:   204
0936  deg
Mean anomaly:     156
0120  deg
Mean motion:   15
54117192  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2369
Checksum:              287


Coasting Arc #18 (Orbit 2374)
---------------------------------------

Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904718
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -634020
64                 A    =         6782758
81  meter
 Y    =        5481560
17  meter          E    =           
0006985
 Z    =       -3952273
30                 I    =           51
92078
 XDOT =      -6106
943109                 Wp   =          128
20094
 YDOT =       2218
954507  meter/sec      RA   =          130
73537  deg
 ZDOT =       4057
880595                 TA   =          184
09027
                                          MA   =          184
09598
                                          Ha   =            220
905  n
mi
                                          Hp   =            215
003

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2080120
21                 X    =         -676072
05
 Y    =       17984121
31  feet           Y    =         5474234
56  meter
 Z    =      -12966775
93                 Z    =        -3955455
84
 XDOT =     -20035
902590                 XDOT =       -6151
012928
 YDOT =       7280
034472  feet/sec       YDOT =        2150
416503  meter/sec
 ZDOT =      13313
256545                 ZDOT =        4028
108364

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18059955
22                 X    =        -5504674
35
 Y    =       -1099154
49  feet           Y    =         -335022
29  meter
 Z    =      -12981628
33                 Z    =        -3956800
32
 XDOT =      -8351
356656                 XDOT =       -2545
493509
 YDOT =     -18420
079496  feet/sec       YDOT =       -5614
440230  meter/sec
 ZDOT =      13180
129755                 ZDOT =        4017
303549


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   18073
29157857  
00016717  00000-0  10270-3 0  9178
2 25544  51
6397 131
7886 0002516 201
4803 158
6244 15
54108190 23750


Satellite: ISS
Catalog Number: 25544
Epoch time:      18073
29157857   =   yrday
fracday
Element set:     917
Inclination:       51
6397  deg
RA of node:       131
7886  deg
Eccentricity:     
0002516     
Arg of perigee:   201
4803  deg
Mean anomaly:     158
6244  deg
Mean motion:   15
54108190  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2375
Checksum:              322


Coasting Arc #19 (Orbit 2390)
---------------------------------------

Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 904718
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1814722
55                 A    =         6786506
26  meter
 Y    =       -5993783
34  meter          E    =           
0013421
 Z    =        2595986
85                 I    =           51
95382
 XDOT =       5534
631043                 Wp   =          114
00049
 YDOT =       -616
866452  meter/sec      RA   =          125
77413  deg
 ZDOT =      -5277
111536                 TA   =           36
90475
                                          MA   =           36
81247
                                          Ha   =            220
894  n
mi
                                          Hp   =            215
014

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5953814
14                 X    =         1869002
04
 Y    =      -19664643
52  feet           Y    =        -5973186
05  meter
 Z    =        8517017
21                 Z    =         2604934
59
 XDOT =      18158
238331                 XDOT =        5566
750728
 YDOT =      -2023
840066  feet/sec       YDOT =        -554
795464  meter/sec
 ZDOT =     -17313
358058                 ZDOT =       -5250
148522

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20014109
89                 X    =         6100300
69
 Y    =        4570276
63  feet           Y    =         1393020
32  meter
 Z    =        8557667
13                 Z    =         2608376
94
 XDOT =       3574
914131                 XDOT =        1089
633827
 YDOT =      16636
520232  feet/sec       YDOT =        5070
811367  meter/sec
 ZDOT =     -17192
947641                 ZDOT =       -5240
410441


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   18074
32041737  
00016717  00000-0  10270-3 0  9183
2 25544  51
6396 126
6598 0002526 202
7237 157
3804 15
54107559 23912


Satellite: ISS
Catalog Number: 25544
Epoch time:      18074
32041737   =   yrday
fracday
Element set:     918
Inclination:       51
6396  deg
RA of node:       126
6598  deg
Eccentricity:     
0002526     
Arg of perigee:   202
7237  deg
Mean anomaly:     157
3804  deg
Mean motion:   15
54107559  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2391
Checksum:              319
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