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

 
Date: September 21st 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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


265/17:52:27 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 215 4

267/01:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 7
000/00:00:00 000 0 0 0 0 215 7

270/11:54:38 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 216 0

271/01:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 3
000/00:00:00 000 0 0 0 0 216 1

274/09:07:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 216 3

277/07:57:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 216 4

Coasting Arc #1 (Orbit 1348)
---------------------------------------

Vector Time (GMT): 2018/264/12:03:24
619
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2611787
56                 A    =         6789418
99  meter
 Y    =        6053002
01  meter          E    =           
0015531
 Z    =        1585388
86                 I    =           51
27943
 XDOT =      -3985
690604                 Wp   =          131
38446
 YDOT =       3222
079650  meter/sec      RA   =          257
77713  deg
 ZDOT =      -5709
455164                 TA   =           31
17658
                                          MA   =           31
08453
                                          Ha   =            221
866  n
mi
                                          Hp   =            215
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8568856
82                 X    =         2536206
15
 Y    =       19858930
48  feet           Y    =         6081786
37  meter
 Z    =        5201407
01                 Z    =         1597891
86
 XDOT =     -13076
412742                 XDOT =       -3993
691162
 YDOT =      10571
127462  feet/sec       YDOT =        3177
463659  meter/sec
 ZDOT =     -18731
808280                 ZDOT =       -5728
835897

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8635066
37                 X    =        -2631968
23
 Y    =      -19815612
68  feet           Y    =        -6039798
75  meter
 Z    =        5256822
70                 Z    =         1602279
56
 XDOT =      11452
645850                 XDOT =        3490
766455
 YDOT =     -10005
877893  feet/sec       YDOT =       -3049
791582  meter/sec
 ZDOT =     -18819
091228                 ZDOT =       -5736
059006


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   18264
53769407  
00016717  00000-0  10270-3 0  9009
2 25544  51
6363 258
5570 0004017 190
7069 169
3998 15
53724827 13498


Satellite: ISS
Catalog Number: 25544
Epoch time:      18264
53769407   =   yrday
fracday
Element set:     900
Inclination:       51
6363  deg
RA of node:       258
5570  deg
Eccentricity:     
0004017     
Arg of perigee:   190
7069  deg
Mean anomaly:     169
3998  deg
Mean motion:   15
53724827  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1349
Checksum:              341


Coasting Arc #2 (Orbit 1363)
---------------------------------------

Vector Time (GMT): 2018/265/12:03:24
619
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2043523
60                 A    =         6790383
79  meter
 Y    =       -6472449
76  meter          E    =           
0008689
 Z    =         -45284
96                 I    =           51
29136
 XDOT =       4560
729810                 Wp   =           60
69593
 YDOT =      -1475
672249  meter/sec      RA   =          252
78407  deg
 ZDOT =       5980
981892                 TA   =          298
81420
                                          MA   =          298
90141
                                          Ha   =            221
871  n
mi
                                          Hp   =            215
422

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6704473
77                 X    =        -1970775
02
 Y    =      -21235071
40  feet           Y    =        -6494895
10  meter
 Z    =        -148572
69                 Z    =          -55034
28
 XDOT =      14963
024310                 XDOT =        4547
839854
 YDOT =      -4841
444386  feet/sec       YDOT =       -1424
742452  meter/sec
 ZDOT =      19622
644004                 ZDOT =        6003
105112

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7175015
08                 X    =         2186944
60
 Y    =       21080387
65  feet           Y    =         6425302
16  meter
 Z    =        -191610
75                 Z    =          -58402
96
 XDOT =     -13183
460285                 XDOT =       -4018
318695
 YDOT =       4646
228827  feet/sec       YDOT =        1416
170547  meter/sec
 ZDOT =      19722
036314                 ZDOT =        6011
276669


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   18265
50248361  
00016717  00000-0  10270-3 0  9019
2 25544  51
6365 253
7509 0004301 192
3770 167
7277 15
53763701 13645


Satellite: ISS
Catalog Number: 25544
Epoch time:      18265
50248361   =   yrday
fracday
Element set:     901
Inclination:       51
6365  deg
RA of node:       253
7509  deg
Eccentricity:     
0004301     
Arg of perigee:   192
3770  deg
Mean anomaly:     167
7277  deg
Mean motion:   15
53763701  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1364
Checksum:              308


Coasting Arc #3 (Orbit 1367)
---------------------------------------

Vector Time (GMT): 2018/265/17:52:27
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4241523
68                 A    =         6778654
20  meter
 Y    =         627631
02  meter          E    =           
0014322
 Z    =       -5262428
74                 I    =           51
25795
 XDOT =      -1909
028233                 Wp   =          110
90184
 YDOT =      -7386
971378  meter/sec      RA   =          251
56571  deg
 ZDOT =        654
091967                 TA   =          165
40609
                                          MA   =          165
36470
                                          Ha   =            221
722  n
mi
                                          Hp   =            215
449

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13915760
11                 X    =        -4222664
74
 Y    =        2059156
87  feet           Y    =          580304
23  meter
 Z    =      -17265186
17                 Z    =        -5282986
80
 XDOT =      -6263
215988                 XDOT =       -1829
460411
 YDOT =     -24235
470401  feet/sec       YDOT =       -7407
874494  meter/sec
 ZDOT =       2145
971019                 ZDOT =         645
012649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1762658
05                 X    =         -537258
17
 Y    =      -13841477
85  feet           Y    =        -4218882
45  meter
 Z    =      -17357467
76                 Z    =        -5290556
17
 XDOT =      23354
535348                 XDOT =        7118
462374
 YDOT =      -5629
717593  feet/sec       YDOT =       -1715
937922  meter/sec
 ZDOT =       2106
030997                 ZDOT =         641
918248


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   18265
75976082  
00016717  00000-0  10270-3 0  9025
2 25544  51
6403 252
4695 0003990 197
6950 162
4064 15
53730364 13680


Satellite: ISS
Catalog Number: 25544
Epoch time:      18265
75976082   =   yrday
fracday
Element set:     902
Inclination:       51
6403  deg
RA of node:       252
4695  deg
Eccentricity:     
0003990     
Arg of perigee:   197
6950  deg
Mean anomaly:     162
4064  deg
Mean motion:   15
53730364  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1368
Checksum:              329


Coasting Arc #4 (Orbit 1383)
---------------------------------------

Vector Time (GMT): 2018/266/17:52:27
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4641142
07                 A    =         6780281
76  meter
 Y    =         921211
45  meter          E    =           
0004350
 Z    =        4852455
04                 I    =           51
27492
 XDOT =       1053
885512                 Wp   =           91
37056
 YDOT =       7216
533103  meter/sec      RA   =          246
54604  deg
 ZDOT =      -2376
261908                 TA   =           22
03536
                                          MA   =           22
01666
                                          Ha   =            221
406  n
mi
                                          Hp   =            215
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15226844
08                 X    =         4606925
22
 Y    =        3022347
28  feet           Y    =          972921
19  meter
 Z    =       15920128
09                 Z    =         4874916
89
 XDOT =       3457
629632                 XDOT =         984
652539
 YDOT =      23676
289709  feet/sec       YDOT =        7227
930989  meter/sec
 ZDOT =      -7796
134868                 ZDOT =       -2371
311526

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3086362
40                 X    =         -940723
26
 Y    =       15107960
45  feet           Y    =         4604906
35  meter
 Z    =       16020790
87                 Z    =         4883137
06
 XDOT =     -22588
432095                 XDOT =       -6884
954103
 YDOT =       3635
943690  feet/sec       YDOT =        1108
235637  meter/sec
 ZDOT =      -7774
677938                 ZDOT =       -2369
721836


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   18266
78886499  
00016717  00000-0  10270-3 0  9032
2 25544  51
6400 247
3426 0003904 202
7723 157
3257 15
53758719 13842


Satellite: ISS
Catalog Number: 25544
Epoch time:      18266
78886499   =   yrday
fracday
Element set:     903
Inclination:       51
6400  deg
RA of node:       247
3426  deg
Eccentricity:     
0003904     
Arg of perigee:   202
7723  deg
Mean anomaly:     157
3257  deg
Mean motion:   15
53758719  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1384
Checksum:              338


Coasting Arc #5 (Orbit 1388)
---------------------------------------

Vector Time (GMT): 2018/267/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3930788
96                 A    =         6778592
38  meter
 Y    =       -1599581
99  meter          E    =           
0003906
 Z    =        5284816
99                 I    =           51
27058
 XDOT =       3104
625626                 Wp   =          165
22205
 YDOT =       7010
048129  meter/sec      RA   =          244
96685  deg
 ZDOT =       -191
101846                 TA   =          286
58695
                                          MA   =          286
62985
                                          Ha   =            221
685  n
mi
                                          Hp   =            215
717

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12896289
24                 X    =         3922712
89
 Y    =       -5247972
39  feet           Y    =        -1555669
68  meter
 Z    =       17338638
41                 Z    =         5303892
00
 XDOT =      10185
779614                 XDOT =        3026
934852
 YDOT =      22998
845567  feet/sec       YDOT =        7044
331787  meter/sec
 ZDOT =       -626
974562                 ZDOT =        -176
210201

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9460806
77                 X    =         2883653
90
 Y    =      -10068183
83  feet           Y    =        -3068782
43  meter
 Z    =       17424370
34                 Z    =         5310948
08
 XDOT =      18064
544706                 XDOT =        5506
073226
 YDOT =      16024
870380  feet/sec       YDOT =        4884
380492  meter/sec
 ZDOT =       -560
895898                 ZDOT =        -170
961070


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   18267
11046221  
00016717  00000-0  10270-3 0  9042
2 25544  51
6376 245
7349 0004351 199
1875 160
9114 15
53704150 13891


Satellite: ISS
Catalog Number: 25544
Epoch time:      18267
11046221   =   yrday
fracday
Element set:     904
Inclination:       51
6376  deg
RA of node:       245
7349  deg
Eccentricity:     
0004351     
Arg of perigee:   199
1875  deg
Mean anomaly:     160
9114  deg
Mean motion:   15
53704150  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1389
Checksum:              307


Coasting Arc #6 (Orbit 1403)
---------------------------------------

Vector Time (GMT): 2018/268/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4581836
91                 A    =         6779749
15  meter
 Y    =          94841
55  meter          E    =           
0013011
 Z    =       -5007812
60                 I    =           51
29042
 XDOT =      -2276
387671                 Wp   =          124
35773
 YDOT =      -7048
250068  meter/sec      RA   =          239
94769  deg
 ZDOT =       1945
691549                 TA   =          164
66377
                                          MA   =          164
62430
                                          Ha   =            221
660  n
mi
                                          Hp   =            215
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15032273
34                 X    =        -4558231
48
 Y    =         311159
93  feet           Y    =           43735
61  meter
 Z    =      -16429831
35                 Z    =        -5030012
37
 XDOT =      -7468
463488                 XDOT =       -2206
854191
 YDOT =     -23124
180012  feet/sec       YDOT =       -7073
317178  meter/sec
 ZDOT =       6383
502458                 ZDOT =        1934
803383

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13341653
71                 X    =        -4066536
05
 Y    =        6692059
93  feet           Y    =         2039739
87  meter
 Z    =      -16529429
23                 Z    =        -5038170
03
 XDOT =     -16230
088783                 XDOT =       -4946
931061
 YDOT =     -16679
975099  feet/sec       YDOT =       -5084
056410  meter/sec
 ZDOT =       6335
369020                 ZDOT =        1931
020477


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   18268
07524550  
00016717  00000-0  10270-3 0  9055
2 25544  51
6383 240
9290 0004445 203
2275 156
8677 15
53732375 14042


Satellite: ISS
Catalog Number: 25544
Epoch time:      18268
07524550   =   yrday
fracday
Element set:     905
Inclination:       51
6383  deg
RA of node:       240
9290  deg
Eccentricity:     
0004445     
Arg of perigee:   203
2275  deg
Mean anomaly:     156
8677  deg
Mean motion:   15
53732375  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1404
Checksum:              311


Coasting Arc #7 (Orbit 1419)
---------------------------------------

Vector Time (GMT): 2018/269/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5097450
12                 A    =         6782703
45  meter
 Y    =        1309641
07  meter          E    =           
0007456
 Z    =        4271466
65                 I    =           51
31879
 XDOT =       1243
754618                 Wp   =           98
02542
 YDOT =       6694
661835  meter/sec      RA   =          234
93384  deg
 ZDOT =      -3532
581904                 TA   =           28
14583
                                          MA   =           28
10555
                                          Ha   =            221
484  n
mi
                                          Hp   =            215
922

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16723917
73                 X    =         5061677
76
 Y    =        4296722
67  feet           Y    =         1366444
82  meter
 Z    =       14013998
20                 Z    =         4296141
48
 XDOT =       4080
559771                 XDOT =        1185
960200
 YDOT =      21964
113632  feet/sec       YDOT =        6708
246768  meter/sec
 ZDOT =     -11589
835643                 ZDOT =       -3526
681336

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16804869
77                 X    =         5122124
31
 Y    =       -3554772
10  feet           Y    =        -1083494
54  meter
 Z    =       14124565
22                 Z    =         4305167
48
 XDOT =      13240
820104                 XDOT =        4035
801968
 YDOT =      16590
848270  feet/sec       YDOT =        5056
890553  meter/sec
 ZDOT =     -11564
027306                 ZDOT =       -3524
715523


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   18269
10434642  
00016717  00000-0  10270-3 0  9063
2 25544  51
6396 235
8012 0004407 206
1875 153
9055 15
53701778 14206


Satellite: ISS
Catalog Number: 25544
Epoch time:      18269
10434642   =   yrday
fracday
Element set:     906
Inclination:       51
6396  deg
RA of node:       235
8012  deg
Eccentricity:     
0004407     
Arg of perigee:   206
1875  deg
Mean anomaly:     153
9055  deg
Mean motion:   15
53701778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1420
Checksum:              303


Coasting Arc #8 (Orbit 1434)
---------------------------------------

Vector Time (GMT): 2018/270/01:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 909660
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5442755
13                 A    =         6786196
99  meter
 Y    =       -2534128
95  meter          E    =           
0003595
 Z    =       -3168624
50                 I    =           51
35084
 XDOT =        -11
533151                 Wp   =          141
97722
 YDOT =      -5973
393265  meter/sec      RA   =          229
93101  deg
 ZDOT =       4797
208412                 TA   =          181
32114
                                          MA   =          181
32209
                                          Ha   =            221
444  n
mi
                                          Hp   =            215
969

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17856808
16                 X    =        -5398621
56
 Y    =       -8314071
37  feet           Y    =        -2594747
22  meter
 Z    =      -10395749
68                 Z    =        -3194956
39
 XDOT =        -37
838423                 XDOT =          31
961218
 YDOT =     -19597
746933  feet/sec       YDOT =       -5973
278484  meter/sec
 ZDOT =      15738
872744                 ZDOT =        4797
258727

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19618049
13                 X    =        -5979581
37
 Y    =         810256
42  feet           Y    =          246966
16  meter
 Z    =      -10513639
94                 Z    =        -3204557
46
 XDOT =      -9091
573993                 XDOT =       -2771
111753
 YDOT =     -15898
973708  feet/sec       YDOT =       -4846
007186  meter/sec
 ZDOT =      15739
681205                 ZDOT =        4797
454831


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   18270
06912444  
00016717  00000-0  10270-3 0  9072
2 25544  51
6399 230
9951 0004274 212
0098 148
0796 15
53709750 14353


Satellite: ISS
Catalog Number: 25544
Epoch time:      18270
06912444   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       230
9951  deg
Eccentricity:     
0004274     
Arg of perigee:   212
0098  deg
Mean anomaly:     148
0796  deg
Mean motion:   15
53709750  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1435
Checksum:              319


Coasting Arc #9 (Orbit 1441)
---------------------------------------

Vector Time (GMT): 2018/270/11:54:38
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         399521
86                 A    =         6783242
58  meter
 Y    =        5365315
99  meter          E    =           
0004946
 Z    =       -4134933
71                 I    =           51
34820
 XDOT =      -6233
260003                 Wp   =           97
43171
 YDOT =      -2418
183460  meter/sec      RA   =          227
81385  deg
 ZDOT =      -3744
484351                 TA   =          133
85539
                                          MA   =          133
81451
                                          Ha   =            221
251  n
mi
                                          Hp   =            216
043

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1310767
27                 X    =          359581
35
 Y    =       17602742
75  feet           Y    =         5369559
94  meter
 Z    =      -13566055
47                 Z    =        -4133090
54
 XDOT =     -20450
328095                 XDOT =       -6187
566925
 YDOT =      -7933
672770  feet/sec       YDOT =       -2487
633029  meter/sec
 ZDOT =     -12285
053646                 ZDOT =       -3774
652571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2626899
90                 X    =         -800679
09
 Y    =      -17460934
74  feet           Y    =        -5322092
91  meter
 Z    =      -13558306
65                 Z    =        -4132571
87
 XDOT =      19599
375869                 XDOT =        5973
889765
 YDOT =       6684
132719  feet/sec       YDOT =        2037
323653  meter/sec
 ZDOT =     -12420
172060                 ZDOT =       -3785
668444


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   18270
51935405  
00016717  00000-0  10270-3 0  9085
2 25544  51
6378 228
7550 0003823 215
8494 144
2402 15
53733689 14428


Satellite: ISS
Catalog Number: 25544
Epoch time:      18270
51935405   =   yrday
fracday
Element set:     908
Inclination:       51
6378  deg
RA of node:       228
7550  deg
Eccentricity:     
0003823     
Arg of perigee:   215
8494  deg
Mean anomaly:     144
2402  deg
Mean motion:   15
53733689  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1442
Checksum:              317


Coasting Arc #10 (Orbit 1450)
---------------------------------------

Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -436902
57                 A    =         6782721
60  meter
 Y    =       -5259159
87  meter          E    =           
0009562
 Z    =        4259007
05                 I    =           51
36109
 XDOT =       6369
470199                 Wp   =          132
74452
 YDOT =       2360
170503  meter/sec      RA   =          225
07382  deg
 ZDOT =       3556
349800                 TA   =          280
77312
                                          MA   =          280
88075
                                          Ha   =            221
309  n
mi
                                          Hp   =            216
080

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1433407
37                 X    =         -398749
06
 Y    =      -17254461
52  feet           Y    =        -5263831
85  meter
 Z    =       13973120
24                 Z    =         4256977
90
 XDOT =      20897
211939                 XDOT =        6325
329561
 YDOT =       7743
341546  feet/sec       YDOT =        2431
151896  meter/sec
 ZDOT =      11667
814305                 ZDOT =        3587
183537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7746458
47                 X    =        -2361120
54
 Y    =      -15492051
49  feet           Y    =        -4721977
30  meter
 Z    =       13964523
26                 Z    =         4256386
69
 XDOT =      21079
004522                 XDOT =        6424
880578
 YDOT =        135
695764  feet/sec       YDOT =          41
360069  meter/sec
 ZDOT =      11805
931476                 ZDOT =        3598
447914


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   18271
09821932  
00016717  00000-0  10270-3 0  9099
2 25544  51
6399 225
8678 0004404 214
9521 145
1342 15
53760303 14513


Satellite: ISS
Catalog Number: 25544
Epoch time:      18271
09821932   =   yrday
fracday
Element set:     909
Inclination:       51
6399  deg
RA of node:       225
8678  deg
Eccentricity:     
0004404     
Arg of perigee:   214
9521  deg
Mean anomaly:     145
1342  deg
Mean motion:   15
53760303  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1451
Checksum:              306


Coasting Arc #11 (Orbit 1465)
---------------------------------------

Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -871412
36                 A    =         6779838
44  meter
 Y    =        4495456
96  meter          E    =           
0009618
 Z    =       -5008073
91                 I    =           51
37626
 XDOT =      -6548
419710                 Wp   =           90
90100
 YDOT =      -3455
433130  meter/sec      RA   =          220
06596  deg
 ZDOT =      -1965
733758                 TA   =          159
94357
                                          MA   =          159
90574
                                          Ha   =            221
184  n
mi
                                          Hp   =            216
181

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2858964
44                 X    =         -897290
02
 Y    =       14748874
55  feet           Y    =         4485567
12  meter
 Z    =      -16430688
69                 Z    =        -5012370
23
 XDOT =     -21484
316635                 XDOT =       -6499
744731
 YDOT =     -11336
722866  feet/sec       YDOT =       -3528
390106  meter/sec
 ZDOT =      -6449
257736                 ZDOT =       -1997
425771

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3102470
84                 X    =          945633
11
 Y    =       14677520
83  feet           Y    =         4473708
35  meter
 Z    =      -16450397
13                 Z    =        -5014081
05
 XDOT =     -23076
989492                 XDOT =       -7033
866397
 YDOT =      -2496
769183  feet/sec       YDOT =        -761
015247  meter/sec
 ZDOT =      -6591
136247                 ZDOT =       -2008
978328


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   18272
06299481  
00016717  00000-0  10270-3 0  9107
2 25544  51
6407 221
0621 0004340 219
0970 140
9869 15
53733140 14664


Satellite: ISS
Catalog Number: 25544
Epoch time:      18272
06299481   =   yrday
fracday
Element set:     910
Inclination:       51
6407  deg
RA of node:       221
0621  deg
Eccentricity:     
0004340     
Arg of perigee:   219
0970  deg
Mean anomaly:     140
9869  deg
Mean motion:   15
53733140  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1466
Checksum:              295


Coasting Arc #12 (Orbit 1481)
---------------------------------------

Vector Time (GMT): 2018/273/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2229978
93                 A    =         6778385
27  meter
 Y    =       -3598617
49  meter          E    =           
0003627
 Z    =        5294265
18                 I    =           51
39803
 XDOT =       6370
055903                 Wp   =          187
63633
 YDOT =       4263
248687  meter/sec      RA   =          215
05340  deg
 ZDOT =        211
195379                 TA   =          260
32347
                                          MA   =          260
36444
                                          Ha   =            220
951  n
mi
                                          Hp   =            216
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7316203
83                 X    =         2244336
73
 Y    =      -11806487
84  feet           Y    =        -3573599
71  meter
 Z    =       17369636
42                 Z    =         5305132
93
 XDOT =      20899
133541                 XDOT =        6320
883740
 YDOT =      13987
036374  feet/sec       YDOT =        4334
208146  meter/sec
 ZDOT =        692
898225                 ZDOT =         242
019742

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1900268
79                 X    =          579201
93
 Y    =      -13696729
86  feet           Y    =        -4174763
26  meter
 Z    =       17418749
45                 Z    =         5309234
83
 XDOT =      23738
276686                 XDOT =        7235
426734
 YDOT =       4364
625636  feet/sec       YDOT =        1330
337894  meter/sec
 ZDOT =        830
824760                 ZDOT =         253
235387


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   18273
09208285  
00016717  00000-0  10270-3 0  9114
2 25544  51
6408 215
9348 0004240 223
4724 136
6094 15
53779625 14826


Satellite: ISS
Catalog Number: 25544
Epoch time:      18273
09208285   =   yrday
fracday
Element set:     911
Inclination:       51
6408  deg
RA of node:       215
9348  deg
Eccentricity:     
0004240     
Arg of perigee:   223
4724  deg
Mean anomaly:     136
6094  deg
Mean motion:   15
53779625  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1482
Checksum:              314


Coasting Arc #13 (Orbit 1496)
---------------------------------------

Vector Time (GMT): 2018/274/01:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3588162
37                 A    =         6779179
67  meter
 Y    =        2641350
21  meter          E    =           
0011817
 Z    =       -5119687
70                 I    =           51
42789
 XDOT =      -5769
860654                 Wp   =          118
96344
 YDOT =      -4785
410259  meter/sec      RA   =          210
04356  deg
 ZDOT =       1572
099722                 TA   =          166
27325
                                          MA   =          166
24109
                                          Ha   =            220
933  n
mi
                                          Hp   =            216
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11772186
26                 X    =        -3592562
89
 Y    =        8665847
15  feet           Y    =         2601200
06  meter
 Z    =      -16796875
67                 Z    =        -5137128
82
 XDOT =     -18929
989022                 XDOT =       -5723
556582
 YDOT =     -15700
164891  feet/sec       YDOT =       -4849
673871  meter/sec
 ZDOT =       5157
807486                 ZDOT =        1544
184006

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7024348
06                 X    =        -2141021
29
 Y    =       12715955
62  feet           Y    =         3875823
27  meter
 Z    =      -16875405
63                 Z    =        -5143623
64
 XDOT =     -22836
112555                 XDOT =       -6960
447107
 YDOT =      -5923
142646  feet/sec       YDOT =       -1805
373878  meter/sec
 ZDOT =       5032
963912                 ZDOT =        1534
047400


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   18274
05685279  
00016717  00000-0  10270-3 0  9124
2 25544  51
6403 211
1297 0004158 225
9421 134
1389 15
53770459 14973


Satellite: ISS
Catalog Number: 25544
Epoch time:      18274
05685279   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:       211
1297  deg
Eccentricity:     
0004158     
Arg of perigee:   225
9421  deg
Mean anomaly:     134
1389  deg
Mean motion:   15
53770459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1497
Checksum:              321


Coasting Arc #14 (Orbit 1502)
---------------------------------------

Vector Time (GMT): 2018/274/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5513248
50                 A    =         6789943
84  meter
 Y    =       -3839826
67  meter          E    =           
0009514
 Z    =         950860
35                 I    =           51
46988
 XDOT =       3446
325605                 Wp   =           58
05470
 YDOT =      -3477
744816  meter/sec      RA   =          208
38540  deg
 ZDOT =       5899
823403                 TA   =          312
26434
                                          MA   =          312
34498
                                          Ha   =            220
845  n
mi
                                          Hp   =            216
286

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18088085
63                 X    =        -5474519
57
 Y    =      -12597856
53  feet           Y    =        -3901263
05  meter
 Z    =        3119620
56                 Z    =          924172
76
 XDOT =      11306
842535                 XDOT =        3456
299955
 YDOT =     -11409
923937  feet/sec       YDOT =       -3439
149604  meter/sec
 ZDOT =      19356
375994                 ZDOT =        5916
589050

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7985930
34                 X    =         2434111
57
 Y    =       20563088
75  feet           Y    =         6267629
45  meter
 Z    =        3000193
49                 Z    =          914458
98
 XDOT =     -14144
173849                 XDOT =       -4311
144189
 YDOT =       2638
745494  feet/sec       YDOT =         804
289627  meter/sec
 ZDOT =      19431
955565                 ZDOT =        5922
860056


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   18274
44275797  
00016717  00000-0  10270-3 0  9138
2 25544  51
6366 209
2095 0003988 228
4583 131
6228 15
53795519 15038


Satellite: ISS
Catalog Number: 25544
Epoch time:      18274
44275797   =   yrday
fracday
Element set:     913
Inclination:       51
6366  deg
RA of node:       209
2095  deg
Eccentricity:     
0003988     
Arg of perigee:   228
4583  deg
Mean anomaly:     131
6228  deg
Mean motion:   15
53795519  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1503
Checksum:              340


Coasting Arc #15 (Orbit 1517)
---------------------------------------

Vector Time (GMT): 2018/275/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4734170
32                 A    =         6787901
01  meter
 Y    =        4187441
83  meter          E    =           
0005915
 Z    =       -2466703
00                 I    =           51
49310
 XDOT =      -4945
988901                 Wp   =          171
39555
 YDOT =       2466
020444  meter/sec      RA   =          203
40276  deg
 ZDOT =      -5313
586305                 TA   =           36
28924
                                          MA   =           36
24914
                                          Ha   =            220
777  n
mi
                                          Hp   =            216
427

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15532054
84                 X    =         4698975
38
 Y    =       13738326
20  feet           Y    =         4240185
73  meter
 Z    =       -8092857
60                 Z    =        -2443791
46
 XDOT =     -16226
997708                 XDOT =       -4947
386188
 YDOT =       8090
618254  feet/sec       YDOT =        2410
702963  meter/sec
 ZDOT =     -17433
025935                 ZDOT =       -5337
615909

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5601371
32                 X    =        -1707297
98
 Y    =      -20006472
30  feet           Y    =        -6097972
76  meter
 Z    =       -7990393
24                 Z    =        -2435471
86
 XDOT =      16459
690379                 XDOT =        5016
913628
 YDOT =       2387
614658  feet/sec       YDOT =         727
744948  meter/sec
 ZDOT =     -17541
128539                 ZDOT =       -5346
535979


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   18275
40752481  
00016717  00000-0  10270-3 0  9146
2 25544  51
6374 204
4021 0003783 235
5576 124
5219 15
53754296 15181


Satellite: ISS
Catalog Number: 25544
Epoch time:      18275
40752481   =   yrday
fracday
Element set:     914
Inclination:       51
6374  deg
RA of node:       204
4021  deg
Eccentricity:     
0003783     
Arg of perigee:   235
5576  deg
Mean anomaly:     124
5219  deg
Mean motion:   15
53754296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1518
Checksum:              311


Coasting Arc #16 (Orbit 1533)
---------------------------------------

Vector Time (GMT): 2018/276/09:07:30
000
Vector Time (MET): N/A
Weight (LBS)     : 943739
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3625087
22                 A    =         6784463
22  meter
 Y    =       -4342362
19  meter          E    =           
0008836
 Z    =        3741507
59                 I    =           51
51296
 XDOT =       6200
167797                 Wp   =          111
15555
 YDOT =      -1500
628258  meter/sec      RA   =          198
41620  deg
 ZDOT =       4254
382222                 TA   =          293
65745
                                          MA   =          293
75017
                                          Ha   =            220
612  n
mi
                                          Hp   =            216
460

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11893330
78                 X    =        -3594434
66
 Y    =      -14246595
12  feet           Y    =        -4382728
88  meter
 Z    =       12275287
37                 Z    =         3723972
72
 XDOT =      20341
757863                 XDOT =        6195
821773
 YDOT =      -4923
321056  feet/sec       YDOT =       -1431
317798  meter/sec
 ZDOT =      13957
946922                 ZDOT =        4284
490155

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2612800
62                 X    =          796381
63
 Y    =       18425714
72  feet           Y    =         5616157
85  meter
 Z    =       12196957
80                 Z    =         3717632
74
 XDOT =     -18438
893939                 XDOT =       -5620
174873
 YDOT =      -6738
989027  feet/sec       YDOT =       -2054
043855  meter/sec
 ZDOT =      14093
265060                 ZDOT =        4295
627190


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   18276
43660152  
00016717  00000-0  10270-3 0  9154
2 25544  51
6377 199
2755 0003917 239
7645 120
3120 15
53787714 15345


Satellite: ISS
Catalog Number: 25544
Epoch time:      18276
43660152   =   yrday
fracday
Element set:     915
Inclination:       51
6377  deg
RA of node:       199
2755  deg
Eccentricity:     
0003917     
Arg of perigee:   239
7645  deg
Mean anomaly:     120
3120  deg
Mean motion:   15
53787714  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1534
Checksum:              323


Coasting Arc #17 (Orbit 1547)
---------------------------------------

Vector Time (GMT): 2018/277/07:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928631
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6210762
08                 A    =         6787324
35  meter
 Y    =         663922
01  meter          E    =           
0001300
 Z    =       -2654887
91                 I    =           51
55161
 XDOT =      -2747
149315                 Wp   =           35
44628
 YDOT =      -4913
850353  meter/sec      RA   =          193
62118  deg
 ZDOT =       5200
078072                 TA   =          294
58829
                                          MA   =          294
60183
                                          Ha   =            220
553  n
mi
                                          Hp   =            216
397

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20376516
02                 X    =        -6204828
57
 Y    =        2178221
81  feet           Y    =          594501
98  meter
 Z    =       -8710262
16                 Z    =        -2685043
34
 XDOT =      -9012
957071                 XDOT =       -2717
256408
 YDOT =     -16121
556275  feet/sec       YDOT =       -4944
403432  meter/sec
 ZDOT =      17060
623597                 ZDOT =        5186
806234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15084191
63                 X    =         4597661
61
 Y    =       13785349
64  feet           Y    =         4201774
57  meter
 Z    =       -8845734
59                 Z    =        -2696179
90
 XDOT =      -5033
575596                 XDOT =       -1534
233842
 YDOT =      16412
479737  feet/sec       YDOT =        5002
523824  meter/sec
 ZDOT =      17001
473032                 ZDOT =        5182
048980


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   18277
33704292  
00016717  00000-0  10270-3 0  9169
2 25544  51
6366 194
7893 0003707 243
0096 117
0679 15
53757861 15488


Satellite: ISS
Catalog Number: 25544
Epoch time:      18277
33704292   =   yrday
fracday
Element set:     916
Inclination:       51
6366  deg
RA of node:       194
7893  deg
Eccentricity:     
0003707     
Arg of perigee:   243
0096  deg
Mean anomaly:     117
0679  deg
Mean motion:   15
53757861  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1548
Checksum:              341


Coasting Arc #18 (Orbit 1563)
---------------------------------------

Vector Time (GMT): 2018/278/07:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928631
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6682531
59                 A    =         6789728
98  meter
 Y    =          86744
74  meter          E    =           
0011820
 Z    =        1158709
64                 I    =           51
59304
 XDOT =        958
633972                 Wp   =          137
08783
 YDOT =       4848
767899  meter/sec      RA   =          188
64419  deg
 ZDOT =      -5864
882500                 TA   =           30
32044
                                          MA   =           30
25211
                                          Ha   =            220
358  n
mi
                                          Hp   =            216
478

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21924316
24                 X    =         6675436
52
 Y    =         284595
61  feet           Y    =          161433
87  meter
 Z    =        3801540
81                 Z    =         1191153
88
 XDOT =       3145
124580                 XDOT =         932
831018
 YDOT =      15908
031165  feet/sec       YDOT =        4859
343258  meter/sec
 ZDOT =     -19241
740487                 ZDOT =       -5860
288846

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14568528
84                 X    =        -4440487
59
 Y    =      -16351929
40  feet           Y    =        -4984068
08  meter
 Z    =        3947242
35                 Z    =         1203119
47
 XDOT =       8336
769281                 XDOT =        2541
047277
 YDOT =     -12087
892101  feet/sec       YDOT =       -3684
389512  meter/sec
 ZDOT =     -19221
544556                 ZDOT =       -5858
726781


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   18278
36611453  
00016717  00000-0  10270-3 0  9170
2 25544  51
6374 189
6615 0003786 249
0913 110
9834 15
53780819 15645


Satellite: ISS
Catalog Number: 25544
Epoch time:      18278
36611453   =   yrday
fracday
Element set:     917
Inclination:       51
6374  deg
RA of node:       189
6615  deg
Eccentricity:     
0003786     
Arg of perigee:   249
0913  deg
Mean anomaly:     110
9834  deg
Mean motion:   15
53780819  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1564
Checksum:              339


Coasting Arc #19 (Orbit 1579)
---------------------------------------

Vector Time (GMT): 2018/279/07:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 928631
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6727764
54                 A    =         6790208
12  meter
 Y    =        -770264
42  meter          E    =           
0009319
 Z    =         426319
29                 I    =           51
62839
 XDOT =        921
466526                 Wp   =           41
12594
 YDOT =      -4694
740118  meter/sec      RA   =          183
67415  deg
 ZDOT =       5991
711309                 TA   =          323
47080
                                          MA   =          323
53432
                                          Ha   =            220
304  n
mi
                                          Hp   =            216
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22072718
30                 X    =        -6720722
05
 Y    =       -2527114
25  feet           Y    =         -845459
54  meter
 Z    =        1398685
33                 Z    =          393655
22
 XDOT =       3023
184141                 XDOT =         944
791253
 YDOT =     -15402
690677  feet/sec       YDOT =       -4684
304608  meter/sec
 ZDOT =      19657
845501                 ZDOT =        5996
244622

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13345162
92                 X    =         4067605
66
 Y    =       17773197
34  feet           Y    =         5417270
55  meter
 Z    =        1252039
72                 Z    =          381621
71
 XDOT =     -11877
021184                 XDOT =       -3620
116057
 YDOT =       7514
234479  feet/sec       YDOT =        2290
338669  meter/sec
 ZDOT =      19678
623268                 ZDOT =        5998
044372


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   18279
39518044  
00016717  00000-0  10270-3 0  9187
2 25544  51
6381 184
5346 0003818 250
6963 109
3777 15
53805301 15807


Satellite: ISS
Catalog Number: 25544
Epoch time:      18279
39518044   =   yrday
fracday
Element set:     918
Inclination:       51
6381  deg
RA of node:       184
5346  deg
Eccentricity:     
0003818     
Arg of perigee:   250
6963  deg
Mean anomaly:     109
3777  deg
Mean motion:   15
53805301  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1580
Checksum:              328
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