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

 
Date: October 26th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14601 2445 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


301/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 9
000/00:00:00 000 0 0 0 0 221 2

304/19:44:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 3
000/00:00:00 000 0 0 0 0 221 8

305/15:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 2
000/00:00:00 000 0 0 0 0 221 9

306/13:59:43 634 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 222 1

308/07:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 3

308/09:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 7
000/00:00:00 000 0 0 0 0 222 3

311/22:40:58 115 1 0 1 3 1 3
N/A 0 6 -0 0 226 0
000/00:05:52 230 0 6 0 0 223 7

312/03:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 0
000/00:00:00 000 0 0 0 0 223 6

Coasting Arc #1 (Orbit 3546)
---------------------------------------

Vector Time (GMT): 2019/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4303316
29                 A    =         6789324
13  meter
 Y    =        -160203
91  meter          E    =           
0005233
 Z    =        5245972
16                 I    =           51
99493
 XDOT =      -1150
055131                 Wp   =          152
00519
 YDOT =      -7486
193503  meter/sec      RA   =           74
29718  deg
 ZDOT =      -1176
037114                 TA   =          309
20018
                                          MA   =          309
24664
                                          Ha   =            228
457  n
mi
                                          Hp   =            220
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14118491
77                 X    =        -4326687
43
 Y    =        -525603
36  feet           Y    =         -208456
94  meter
 Z    =       17211194
76                 Z    =         5225011
18
 XDOT =      -3773
146755                 XDOT =       -1060
544242
 YDOT =     -24561
002307  feet/sec       YDOT =       -7498
553825  meter/sec
 ZDOT =      -3858
389480                 ZDOT =       -1181
405816

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12262220
44                 X    =         3737524
79
 Y    =       -7247652
48  feet           Y    =        -2209084
48  meter
 Z    =       17115571
19                 Z    =         5216826
10
 XDOT =      15892
336245                 XDOT =        4843
984087
 YDOT =      17751
207628  feet/sec       YDOT =        5410
568085  meter/sec
 ZDOT =      -3882
298261                 ZDOT =       -1183
324510


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   19298
54632874  
00016717  00000-0  10270-3 0  9005
2 25544  51
6402  74
8919 0006900 187
3660 172
7390 15
50181118 35473


Satellite: ISS
Catalog Number: 25544
Epoch time:      19298
54632874   =   yrday
fracday
Element set:     900
Inclination:       51
6402  deg
RA of node:        74
8919  deg
Eccentricity:     
0006900     
Arg of perigee:   187
3660  deg
Mean anomaly:     172
7390  deg
Mean motion:   15
50181118  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3547
Checksum:              322


Coasting Arc #2 (Orbit 3561)
---------------------------------------

Vector Time (GMT): 2019/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4421620
09                 A    =         6789636
60  meter
 Y    =         306038
25  meter          E    =           
0015160
 Z    =       -5155857
47                 I    =           51
98725
 XDOT =       1402
083825                 Wp   =          129
39759
 YDOT =       7342
670483  meter/sec      RA   =           69
36339  deg
 ZDOT =       1632
111279                 TA   =          156
34554
                                          MA   =          156
27577
                                          Ha   =            228
123  n
mi
                                          Hp   =            221
007

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14506627
60                 X    =         4442914
08
 Y    =        1004062
50  feet           Y    =          355602
63  meter
 Z    =      -16915542
87                 Z    =        -5134326
75
 XDOT =       4600
012548                 XDOT =        1311
943688
 YDOT =      24090
126257  feet/sec       YDOT =        7357
845683  meter/sec
 ZDOT =       5354
695796                 ZDOT =        1638
702768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12722403
03                 X    =        -3877788
44
 Y    =        7273491
79  feet           Y    =         2216960
30  meter
 Z    =      -16817334
95                 Z    =        -5125923
69
 XDOT =     -16627
304092                 XDOT =       -5068
002287
 YDOT =     -16587
723221  feet/sec       YDOT =       -5055
938038  meter/sec
 ZDOT =       5384
177725                 ZDOT =        1641
097370


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   19299
51329462  
00016717  00000-0  10270-3 0  9010
2 25544  51
6412  70
1004 0006921 192
0124 168
0862 15
50227754 35625


Satellite: ISS
Catalog Number: 25544
Epoch time:      19299
51329462   =   yrday
fracday
Element set:     901
Inclination:       51
6412  deg
RA of node:        70
1004  deg
Eccentricity:     
0006921     
Arg of perigee:   192
0124  deg
Mean anomaly:     168
0862  deg
Mean motion:   15
50227754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3562
Checksum:              289


Coasting Arc #3 (Orbit 3577)
---------------------------------------

Vector Time (GMT): 2019/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4548036
09                 A    =         6790267
10  meter
 Y    =        -407718
23  meter          E    =           
0004678
 Z    =        5021695
05                 I    =           51
97755
 XDOT =      -1643
745475                 Wp   =          133
97403
 YDOT =      -7193
447138  meter/sec      RA   =           64
42827  deg
 ZDOT =      -2074
710859                 TA   =          336
11118
                                          MA   =          336
13289
                                          Ha   =            228
186  n
mi
                                          Hp   =            221
050

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14921378
26                 X    =        -4567532
09
 Y    =       -1337658
23  feet           Y    =         -458686
30  meter
 Z    =       16475377
46                 Z    =         4999554
50
 XDOT =      -5392
865733                 XDOT =       -1553
106039
 YDOT =     -23600
548353  feet/sec       YDOT =       -7211
321983  meter/sec
 ZDOT =      -6806
794156                 ZDOT =       -2082
475198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13123843
29                 X    =         4000147
43
 Y    =       -7451085
83  feet           Y    =        -2271090
96  meter
 Z    =       16374400
10                 Z    =         4990917
15
 XDOT =      17278
701100                 XDOT =        5266
548095
 YDOT =      15412
733529  feet/sec       YDOT =        4697
801180  meter/sec
 ZDOT =      -6841
619244                 ZDOT =       -2085
325546


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   19300
54472559  
00016717  00000-0  10270-3 0  9023
2 25544  51
6425  64
9884 0006824 195
0804 165
0144 15
50192044 35786


Satellite: ISS
Catalog Number: 25544
Epoch time:      19300
54472559   =   yrday
fracday
Element set:     902
Inclination:       51
6425  deg
RA of node:        64
9884  deg
Eccentricity:     
0006824     
Arg of perigee:   195
0804  deg
Mean anomaly:     165
0144  deg
Mean motion:   15
50192044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3578
Checksum:              313


Coasting Arc #4 (Orbit 3592)
---------------------------------------

Vector Time (GMT): 2019/301/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3186924
32                 A    =         6800624
61  meter
 Y    =        5996218
59  meter          E    =           
0007713
 Z    =         339282
93                 I    =           51
99757
 XDOT =      -4312
349656                 Wp   =           75
49226
 YDOT =       1944
874885  meter/sec      RA   =           59
77247  deg
 ZDOT =       6021
767040                 TA   =          288
13863
                                          MA   =          288
22261
                                          Ha   =            227
855  n
mi
                                          Hp   =            221
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10455788
44                 X    =         3117987
90
 Y    =       19672633
17  feet           Y    =         6031471
59  meter
 Z    =        1113132
97                 Z    =          354596
60
 XDOT =     -14148
128794                 XDOT =       -4363
028551
 YDOT =       6380
823113  feet/sec       YDOT =        1896
367999  meter/sec
 ZDOT =      19756
453543                 ZDOT =        6000
695496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15702367
89                 X    =        -4786081
73
 Y    =      -15799128
23  feet           Y    =        -4815574
29  meter
 Z    =        1182481
40                 Z    =          360420
33
 XDOT =      10665
684968                 XDOT =        3250
900778
 YDOT =      -9102
910618  feet/sec       YDOT =       -2774
567156  meter/sec
 ZDOT =      19660
155250                 ZDOT =        5992
415320


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   19301
51168836  
00016717  00000-0  10270-3 0  9032
2 25544  51
6422  60
1963 0006775 198
4695 161
6211 15
50230858 35939


Satellite: ISS
Catalog Number: 25544
Epoch time:      19301
51168836   =   yrday
fracday
Element set:     903
Inclination:       51
6422  deg
RA of node:        60
1963  deg
Eccentricity:     
0006775     
Arg of perigee:   198
4695  deg
Mean anomaly:     161
6211  deg
Mean motion:   15
50230858  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3593
Checksum:              315


Coasting Arc #5 (Orbit 3607)
---------------------------------------

Vector Time (GMT): 2019/302/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3380231
77                 A    =         6800408
25  meter
 Y    =       -5840253
16  meter          E    =           
0014665
 Z    =        -766434
14                 I    =           51
97850
 XDOT =       4450
947735                 Wp   =          163
97120
 YDOT =      -1797
042857  meter/sec      RA   =           54
84351  deg
 ZDOT =      -5977
533351                 TA   =           24
26517
                                          MA   =           24
19617
                                          Ha   =            227
688  n
mi
                                          Hp   =            221
342

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11089999
24                 X    =        -3310950
11
 Y    =      -19160935
58  feet           Y    =        -5877665
93  meter
 Z    =       -2514547
70                 Z    =         -782686
19
 XDOT =      14602
846901                 XDOT =        4499
748375
 YDOT =      -5895
809899  feet/sec       YDOT =       -1746
996407  meter/sec
 ZDOT =     -19611
329891                 ZDOT =       -5955
793133

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16409806
16                 X    =         5001708
92
 Y    =       14848303
42  feet           Y    =         4525762
88  meter
 Z    =       -2588171
74                 Z    =         -788874
74
 XDOT =     -11137
482701                 XDOT =       -3394
704727
 YDOT =       8930
370191  feet/sec       YDOT =        2721
976834  meter/sec
 ZDOT =     -19511
990755                 ZDOT =       -5947
254782


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   19302
47865224  
00016717  00000-0  10270-3 0  9044
2 25544  51
6416  55
4049 0006725 202
8422 157
2431 15
50235865 36082


Satellite: ISS
Catalog Number: 25544
Epoch time:      19302
47865224   =   yrday
fracday
Element set:     904
Inclination:       51
6416  deg
RA of node:        55
4049  deg
Eccentricity:     
0006725     
Arg of perigee:   202
8422  deg
Mean anomaly:     157
2431  deg
Mean motion:   15
50235865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3608
Checksum:              300


Coasting Arc #6 (Orbit 3623)
---------------------------------------

Vector Time (GMT): 2019/303/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3577541
81                 A    =         6800070
96  meter
 Y    =        5662451
07  meter          E    =           
0008680
 Z    =        1162119
22                 I    =           51
95881
 XDOT =      -4598
321423                 Wp   =           81
94644
 YDOT =       1689
605289  meter/sec      RA   =           49
91284  deg
 ZDOT =       5886
737402                 TA   =          290
59004
                                          MA   =          290
68312
                                          Ha   =            227
572  n
mi
                                          Hp   =            221
490

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11737341
89                 X    =         3508311
66
 Y    =       18577595
36  feet           Y    =         5702070
55  meter
 Z    =        3812727
12                 Z    =         1179330
00
 XDOT =     -15086
356374                 XDOT =       -4645
468604
 YDOT =       5543
324439  feet/sec       YDOT =        1637
919900  meter/sec
 ZDOT =      19313
442920                 ZDOT =        5864
285381

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17079021
38                 X    =        -5205685
72
 Y    =      -13805738
96  feet           Y    =        -4207989
24  meter
 Z    =        3890723
92                 Z    =         1185892
65
 XDOT =      11606
977530                 XDOT =        3537
806751
 YDOT =      -8911
979104  feet/sec       YDOT =       -2716
371231  meter/sec
 ZDOT =      19210
862796                 ZDOT =        5855
470980


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   19303
51007870  
00016717  00000-0  10270-3 0  9056
2 25544  51
6431  50
2939 0006773 206
4447 153
6358 15
50236882 36246


Satellite: ISS
Catalog Number: 25544
Epoch time:      19303
51007870   =   yrday
fracday
Element set:     905
Inclination:       51
6431  deg
RA of node:        50
2939  deg
Eccentricity:     
0006773     
Arg of perigee:   206
4447  deg
Mean anomaly:     153
6358  deg
Mean motion:   15
50236882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3624
Checksum:              306


Coasting Arc #7 (Orbit 3638)
---------------------------------------

Vector Time (GMT): 2019/304/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3716822
38                 A    =         6799577
39  meter
 Y    =       -5461434
86  meter          E    =           
0012132
 Z    =       -1578098
02                 I    =           51
93517
 XDOT =       4789
623869                 Wp   =          172
38248
 YDOT =      -1598
118150  meter/sec      RA   =           44
98061  deg
 ZDOT =      -5766
820555                 TA   =           24
78162
                                          MA   =           24
72339
                                          Ha   =            227
385  n
mi
                                          Hp   =            221
669

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12194299
14                 X    =        -3647809
08
 Y    =      -17918093
38  feet           Y    =        -5502613
06  meter
 Z    =       -5177486
95                 Z    =        -1595985
94
 XDOT =      15713
989073                 XDOT =        4835
151188
 YDOT =      -5243
169784  feet/sec       YDOT =       -1544
302444  meter/sec
 ZDOT =     -18920
014944                 ZDOT =       -5743
443279

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17511754
03                 X    =         5337582
63
 Y    =       12737786
61  feet           Y    =         3882477
36  meter
 Z    =       -5258577
39                 Z    =        -1602814
39
 XDOT =     -12197
980815                 XDOT =       -3717
944552
 YDOT =       9025
266795  feet/sec       YDOT =        2750
901319  meter/sec
 ZDOT =     -18813
219307                 ZDOT =       -5734
269245


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   19304
47703949  
00016717  00000-0  10270-3 0  9063
2 25544  51
6435  45
5024 0006654 210
3216 149
7551 15
50238101 36391


Satellite: ISS
Catalog Number: 25544
Epoch time:      19304
47703949   =   yrday
fracday
Element set:     906
Inclination:       51
6435  deg
RA of node:        45
5024  deg
Eccentricity:     
0006654     
Arg of perigee:   210
3216  deg
Mean anomaly:     149
7551  deg
Mean motion:   15
50238101  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3639
Checksum:              298


Coasting Arc #8 (Orbit 3644)
---------------------------------------

Vector Time (GMT): 2019/304/19:44:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949211
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5284386
80                 A    =         6793179
46  meter
 Y    =        -387605
80  meter          E    =           
0006824
 Z    =        4244042
67                 I    =           51
90208
 XDOT =      -2484
679591                 Wp   =          111
00614
 YDOT =      -6258
017454  meter/sec      RA   =           43
09776  deg
 ZDOT =      -3662
930935                 TA   =           16
39513
                                          MA   =           16
37307
                                          Ha   =            227
327  n
mi
                                          Hp   =            221
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17337227
05                 X    =        -5300275
39
 Y    =       -1271672
58  feet           Y    =         -446788
54  meter
 Z    =       13924024
51                 Z    =         4218333
93
 XDOT =      -8151
835928                 XDOT =       -2396
723078
 YDOT =     -20531
553326  feet/sec       YDOT =       -6285
310963  meter/sec
 ZDOT =     -12017
489943                 ZDOT =       -3674
787441

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15249772
31                 X    =        -4648130
60
 Y    =       -8537699
66  feet           Y    =        -2602290
86  meter
 Z    =       13806780
24                 Z    =         4208306
62
 XDOT =        768
278208                 XDOT =         234
171198
 YDOT =     -20905
552913  feet/sec       YDOT =       -6372
012528  meter/sec
 ZDOT =     -12070
985568                 ZDOT =       -3679
236401


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   19304
86382237  
00016717  00000-0  10270-3 0  9070
2 25544  51
6408  43
5896 0006211 213
7948 146
2807 15
50237831 36456


Satellite: ISS
Catalog Number: 25544
Epoch time:      19304
86382237   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:        43
5896  deg
Eccentricity:     
0006211     
Arg of perigee:   213
7948  deg
Mean anomaly:     146
2807  deg
Mean motion:   15
50237831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3645
Checksum:              320


Coasting Arc #9 (Orbit 3657)
---------------------------------------

Vector Time (GMT): 2019/305/15:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5816943
77                 A    =         6796523
02  meter
 Y    =       -1521223
32  meter          E    =           
0011110
 Z    =        3153652
67                 I    =           51
89428
 XDOT =      -1121
748684                 Wp   =          123
55380
 YDOT =      -5815
184517  meter/sec      RA   =           38
94541  deg
 ZDOT =      -4867
794632                 TA   =           20
26768
                                          MA   =           20
22361
                                          Ha   =            227
203  n
mi
                                          Hp   =            221
896

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19084461
20                 X    =        -5814819
66
 Y    =       -4990890
14  feet           Y    =        -1586260
73  meter
 Z    =       10346629
48                 Z    =         3125400
71
 XDOT =      -3680
277834                 XDOT =       -1032
992751
 YDOT =     -19078
689361  feet/sec       YDOT =       -5827
232244  meter/sec
 ZDOT =     -15970
454828                 ZDOT =       -4873
028423

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2102215
39                 X    =          640755
25
 Y    =      -19681303
66  feet           Y    =        -5998861
35  meter
 Z    =       10217894
20                 Z    =         3114414
15
 XDOT =      16906
183589                 XDOT =        5153
004758
 YDOT =      -6508
593492  feet/sec       YDOT =       -1983
819296  meter/sec
 ZDOT =     -15993
771075                 ZDOT =       -4874
901424


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   19305
70185324  
00016717  00000-0  10270-3 0  9083
2 25544  51
6428  39
4368 0006244 216
1894 143
8835 15
50252696 36583


Satellite: ISS
Catalog Number: 25544
Epoch time:      19305
70185324   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:        39
4368  deg
Eccentricity:     
0006244     
Arg of perigee:   216
1894  deg
Mean anomaly:     143
8835  deg
Mean motion:   15
50252696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3658
Checksum:              330


Coasting Arc #10 (Orbit 3671)
---------------------------------------

Vector Time (GMT): 2019/306/13:59:43
634
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -607078
59                 A    =         6791441
34  meter
 Y    =       -4880997
35  meter          E    =           
0006138
 Z    =       -4687520
87                 I    =           51
85239
 XDOT =       6823
763387                 Wp   =          103
64276
 YDOT =       1925
081208  meter/sec      RA   =           34
44601  deg
 ZDOT =      -2892
871012                 TA   =          137
67089
                                          MA   =          137
62351
                                          Ha   =            227
076  n
mi
                                          Hp   =            222
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1991727
67                 X    =         -529683
03
 Y    =      -16013770
83  feet           Y    =        -4887353
22  meter
 Z    =      -15379005
49                 Z    =        -4690282
07
 XDOT =      22387
675155                 XDOT =        6815
781585
 YDOT =       6315
883229  feet/sec       YDOT =        2001
344821  meter/sec
 ZDOT =      -9491
046627                 ZDOT =       -2859
742543

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15732186
58                 X    =         4795170
47
 Y    =        3540226
23  feet           Y    =         1079060
95  meter
 Z    =      -15391125
65                 Z    =        -4691215
10
 XDOT =     -13157
782637                 XDOT =       -4010
492148
 YDOT =      17930
349842  feet/sec       YDOT =        5465
170632  meter/sec
 ZDOT =      -9340
109317                 ZDOT =       -2846
865320


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   19306
60434842  
00016717  00000-0  10270-3 0  9096
2 25544  51
6425  34
9638 0006487 219
1963 140
8718 15
50217295 36728


Satellite: ISS
Catalog Number: 25544
Epoch time:      19306
60434842   =   yrday
fracday
Element set:     909
Inclination:       51
6425  deg
RA of node:        34
9638  deg
Eccentricity:     
0006487     
Arg of perigee:   219
1963  deg
Mean anomaly:     140
8718  deg
Mean motion:   15
50217295  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3672
Checksum:              328


Coasting Arc #11 (Orbit 3687)
---------------------------------------

Vector Time (GMT): 2019/307/13:59:43
634
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         550424
21                 A    =         6790644
63  meter
 Y    =        4706964
68  meter          E    =           
0008313
 Z    =        4865331
46                 I    =           51
82218
 XDOT =      -7035
990376                 Wp   =          168
59714
 YDOT =      -1744
799015  meter/sec      RA   =           29
50208  deg
 ZDOT =       2475
334198                 TA   =          257
08380
                                          MA   =          257
17667
                                          Ha   =            226
807  n
mi
                                          Hp   =            222
250

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1805853
70                 X    =          474115
28
 Y    =       15442797
51  feet           Y    =         4712693
12  meter
 Z    =       15962373
55                 Z    =         4867820
03
 XDOT =     -23083
957925                 XDOT =       -7027
980544
 YDOT =      -5724
406217  feet/sec       YDOT =       -1823
435705  meter/sec
 ZDOT =       8121
175189                 ZDOT =        2441
174976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15189091
23                 X    =        -4629635
01
 Y    =       -3268773
78  feet           Y    =         -996322
25  meter
 Z    =       15973261
96                 Z    =         4868650
25
 XDOT =      12503
420853                 XDOT =        3811
042676
 YDOT =     -19036
593883  feet/sec       YDOT =       -5802
353816  meter/sec
 ZDOT =       7965
524924                 ZDOT =        2427
891997


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   19307
63576741  
00016717  00000-0  10270-3 0  9107
2 25544  51
6429  29
8523 0006418 223
9735 136
0905 15
50243944 36884


Satellite: ISS
Catalog Number: 25544
Epoch time:      19307
63576741   =   yrday
fracday
Element set:     910
Inclination:       51
6429  deg
RA of node:        29
8523  deg
Eccentricity:     
0006418     
Arg of perigee:   223
9735  deg
Mean anomaly:     136
0905  deg
Mean motion:   15
50243944  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3688
Checksum:              325


Coasting Arc #12 (Orbit 3698)
---------------------------------------

Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 919680
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1192776
89                 A    =         6791134
45  meter
 Y    =        4724420
69  meter          E    =           
0008430
 Z    =        4731970
02                 I    =           51
80136
 XDOT =      -7065
323012                 Wp   =          163
53072
 YDOT =      -1010
888664  meter/sec      RA   =           25
99801  deg
 ZDOT =       2781
118526                 TA   =          258
90575
                                          MA   =          259
00056
                                          Ha   =            226
731  n
mi
                                          Hp   =            222
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3913310
00                 X    =         1116872
85
 Y    =       15500067
89  feet           Y    =         4737334
68  meter
 Z    =       15524836
01                 Z    =         4737579
87
 XDOT =     -23180
193609                 XDOT =       -7067
003134
 YDOT =      -3316
563857  feet/sec       YDOT =       -1089
907537  meter/sec
 ZDOT =       9124
404612                 ZDOT =        2746
793343

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5157094
00                 X    =         1571882
25
 Y    =      -15105953
46  feet           Y    =        -4604294
62  meter
 Z    =       15549957
70                 Z    =         4739627
11
 XDOT =      16677
312206                 XDOT =        5083
244760
 YDOT =      14955
743740  feet/sec       YDOT =        4558
510692  meter/sec
 ZDOT =       8967
930442                 ZDOT =        2733
425199


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   19308
34486785  
00016717  00000-0  10270-3 0  9115
2 25544  51
6412  26
3346 0006439 225
3487 134
7140 15
50255605 36999


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
34486785   =   yrday
fracday
Element set:     911
Inclination:       51
6412  deg
RA of node:        26
3346  deg
Eccentricity:     
0006439     
Arg of perigee:   225
3487  deg
Mean anomaly:     134
7140  deg
Mean motion:   15
50255605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3699
Checksum:              318


Coasting Arc #13 (Orbit 3699)
---------------------------------------

Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4659195
92                 A    =         6798142
26  meter
 Y    =       -4320605
77  meter          E    =           
0008314
 Z    =       -2401801
07                 I    =           51
82423
 XDOT =       4932
410040                 Wp   =          183
03145
 YDOT =      -2331
531751  meter/sec      RA   =           25
55188  deg
 ZDOT =      -5381
301529                 TA   =           23
69743
                                          MA   =           23
65916
                                          Ha   =            226
744  n
mi
                                          Hp   =            222
264

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15286075
85                 X    =        -4598868
62
 Y    =      -14175215
78  feet           Y    =        -4372370
84  meter
 Z    =       -7879924
76                 Z    =        -2424287
50
 XDOT =      16182
447637                 XDOT =        4984
254989
 YDOT =      -7649
382385  feet/sec       YDOT =       -2276
084088  meter/sec
 ZDOT =     -17655
188744                 ZDOT =       -5357
215572

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15216645
53                 X    =         4638033
56
 Y    =       14192757
26  feet           Y    =         4325952
41  meter
 Z    =       -7982068
14                 Z    =        -2432934
37
 XDOT =     -15274
861864                 XDOT =       -4655
777896
 YDOT =       6522
561767  feet/sec       YDOT =        1988
076826  meter/sec
 ZDOT =     -17545
090200                 ZDOT =       -5347
743493


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   19308
40933190  
00016717  00000-0  10270-3 0  9120
2 25544  51
6435  26
0156 0006469 224
8506 135
2122 15
50244754 37001


Satellite: ISS
Catalog Number: 25544
Epoch time:      19308
40933190   =   yrday
fracday
Element set:     912
Inclination:       51
6435  deg
RA of node:        26
0156  deg
Eccentricity:     
0006469     
Arg of perigee:   224
8506  deg
Mean anomaly:     135
2122  deg
Mean motion:   15
50244754  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3700
Checksum:              285


Coasting Arc #14 (Orbit 3715)
---------------------------------------

Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4679500
34                 A    =         6797296
65  meter
 Y    =        4081497
98  meter          E    =           
0008592
 Z    =        2760692
10                 I    =           51
79117
 XDOT =      -5138
663522                 Wp   =          102
46377
 YDOT =       2398
165867  meter/sec      RA   =           20
60928  deg
 ZDOT =       5149
401296                 TA   =          288
66907
                                          MA   =          288
76232
                                          Ha   =            226
614  n
mi
                                          Hp   =            222
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15352691
41                 X    =         4620101
99
 Y    =       13390741
39  feet           Y    =         4133495
32  meter
 Z    =        9057388
78                 Z    =         2783279
36
 XDOT =     -16859
132289                 XDOT =       -5190
111810
 YDOT =       7867
998252  feet/sec       YDOT =        2340
414018  meter/sec
 ZDOT =      16894
361208                 ZDOT =        5124
314359

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15504570
62                 X    =        -4725793
12
 Y    =      -13143664
90  feet           Y    =        -4006189
06  meter
 Z    =        9160007
79                 Z    =         2791970
38
 XDOT =      15885
602330                 XDOT =        4841
931590
 YDOT =      -7010
325708  feet/sec       YDOT =       -2136
747276  meter/sec
 ZDOT =      16779
695684                 ZDOT =        5114
451244


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   19309
44074739  
00016717  00000-0  10270-3 0  9131
2 25544  51
6437  20
9046 0006458 228
2929 131
7669 15
50265174 37162


Satellite: ISS
Catalog Number: 25544
Epoch time:      19309
44074739   =   yrday
fracday
Element set:     913
Inclination:       51
6437  deg
RA of node:        20
9046  deg
Eccentricity:     
0006458     
Arg of perigee:   228
2929  deg
Mean anomaly:     131
7669  deg
Mean motion:   15
50265174  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3716
Checksum:              327


Coasting Arc #15 (Orbit 3730)
---------------------------------------

Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4641612
51                 A    =         6796459
98  meter
 Y    =       -3855946
76  meter          E    =           
0005041
 Z    =       -3120570
80                 I    =           51
75654
 XDOT =       5352
036194                 Wp   =          187
52108
 YDOT =      -2495
089091  meter/sec      RA   =           15
66448  deg
 ZDOT =      -4881
661687                 TA   =           28
27281
                                          MA   =           28
24545
                                          Ha   =            226
429  n
mi
                                          Hp   =            222
553

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15228387
50                 X    =        -4582991
02
 Y    =      -12650743
95  feet           Y    =        -3907524
80  meter
 Z    =      -10238093
17                 Z    =        -3142975
89
 XDOT =      17559
173865                 XDOT =        5403
251937
 YDOT =      -8185
987830  feet/sec       YDOT =       -2434
952515  meter/sec
 ZDOT =     -16015
950417                 ZDOT =       -4855
538753

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15571542
17                 X    =         4746206
05
 Y    =       12139905
49  feet           Y    =         3700243
19  meter
 Z    =      -10339895
03                 Z    =        -3151600
01
 XDOT =     -16499
404954                 XDOT =       -5029
018630
 YDOT =       7634
834302  feet/sec       YDOT =        2327
097495  meter/sec
 ZDOT =     -15896
557693                 ZDOT =       -4845
270785


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   19310
40770070  
00016717  00000-0  10270-3 0  9141
2 25544  51
6437  16
1135 0006480 232
2351 127
8213 15
50240808 37312


Satellite: ISS
Catalog Number: 25544
Epoch time:      19310
40770070   =   yrday
fracday
Element set:     914
Inclination:       51
6437  deg
RA of node:        16
1135  deg
Eccentricity:     
0006480     
Arg of perigee:   232
2351  deg
Mean anomaly:     127
8213  deg
Mean motion:   15
50240808  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3731
Checksum:              267


Coasting Arc #16 (Orbit 3746)
---------------------------------------

Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934394
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4590905
96                 A    =         6795465
98  meter
 Y    =        3635694
13  meter          E    =           
0007899
 Z    =        3445104
49                 I    =           51
72193
 XDOT =      -5539
028783                 Wp   =          118
47336
 YDOT =       2636
191914  meter/sec      RA   =           10
71616  deg
 ZDOT =       4587
533651                 TA   =          281
76105
                                          MA   =          281
84965
                                          Ha   =            226
250  n
mi
                                          Hp   =            222
668

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15062027
42                 X    =         4533174
70
 Y    =       11928130
35  feet           Y    =         3686710
15  meter
 Z    =       11302836
24                 Z    =         3467265
45
 XDOT =     -18172
666612                 XDOT =       -5590
379809
 YDOT =       8648
923603  feet/sec       YDOT =        2573
963539  meter/sec
 ZDOT =      15050
963422                 ZDOT =        4560
501942

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15568273
33                 X    =        -4745209
71
 Y    =      -11157386
54  feet           Y    =        -3400771
42  meter
 Z    =       11403537
24                 Z    =         3475798
15
 XDOT =      17000
452225                 XDOT =        5181
737838
 YDOT =      -8425
731241  feet/sec       YDOT =       -2568
162882  meter/sec
 ZDOT =      14927
421478                 ZDOT =        4549
878066


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   19311
43911320  
00016717  00000-0  10270-3 0  9151
2 25544  51
6446  11
0021 0006455 236
2921 123
7615 15
50272921 37478


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
43911320   =   yrday
fracday
Element set:     915
Inclination:       51
6446  deg
RA of node:        11
0021  deg
Eccentricity:     
0006455     
Arg of perigee:   236
2921  deg
Mean anomaly:     123
7615  deg
Mean motion:   15
50272921  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3747
Checksum:              273


Coasting Arc #17 (Orbit 3754)
---------------------------------------

Vector Time (GMT): 2019/311/22:43:54
230
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5300298
66                 A    =         6795793
03  meter
 Y    =       -2180112
62  meter          E    =           
0003053
 Z    =       -3653851
02                 I    =           51
70200
 XDOT =       4723
988628                 Wp   =          197
26482
 YDOT =       4142
575986  meter/sec      RA   =            7
87120  deg
 ZDOT =       4377
145036                 TA   =          119
49995
                                          MA   =          119
46950
                                          Ha   =            225
966  n
mi
                                          Hp   =            223
723

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17389431
29                 X    =         5342032
06
 Y    =       -7152600
46  feet           Y    =        -2120607
66  meter
 Z    =      -11987700
20                 Z    =        -3628002
30
 XDOT =      15498
650355                 XDOT =        4656
051934
 YDOT =      13591
128564  feet/sec       YDOT =        4195
023195  meter/sec
 ZDOT =      14360
712062                 ZDOT =        4399
927705

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12336855
84                 X    =         3760273
66
 Y    =      -14288857
21  feet           Y    =        -4355243
68  meter
 Z    =      -11869604
77                 Z    =        -3617855
53
 XDOT =      18844
728836                 XDOT =        5743
873349
 YDOT =       4244
676280  feet/sec       YDOT =        1293
777330  meter/sec
 ZDOT =      14464
191605                 ZDOT =        4408
685601


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   19311
95482037  
00016717  00000-0  10270-3 0  9167
2 25544  51
6450   8
4505 0006631 250
9973 109
0459 15
50015593 37558


Satellite: ISS
Catalog Number: 25544
Epoch time:      19311
95482037   =   yrday
fracday
Element set:     916
Inclination:       51
6450  deg
RA of node:         8
4505  deg
Eccentricity:     
0006631     
Arg of perigee:   250
9973  deg
Mean anomaly:     109
0459  deg
Mean motion:   15
50015593  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3755
Checksum:              309


Coasting Arc #18 (Orbit 3757)
---------------------------------------

Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1913317
76                 A    =         6790816
73  meter
 Y    =       -4204148
60  meter          E    =           
0005946
 Z    =       -4983344
05                 I    =           51
67539
 XDOT =       7310
171501                 Wp   =           78
25540
 YDOT =       -799
559945  meter/sec      RA   =            7
01313  deg
 ZDOT =      -2133
122138                 TA   =          170
94971
                                          MA   =          170
93898
                                          Ha   =            225
964  n
mi
                                          Hp   =            223
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6277289
24                 X    =        -1841956
79
 Y    =      -13793138
47  feet           Y    =        -4225145
78  meter
 Z    =      -16349553
95                 Z    =        -4992464
98
 XDOT =      23983
502300                 XDOT =        7328
930812
 YDOT =      -2623
228166  feet/sec       YDOT =        -717
707598  meter/sec
 ZDOT =      -6998
432210                 ZDOT =       -2097
565850

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13526325
85                 X    =        -4122824
12
 Y    =        6733911
96  feet           Y    =         2052496
37  meter
 Z    =      -16390725
49                 Z    =        -4995893
13
 XDOT =      -3127
577137                 XDOT =        -953
285511
 YDOT =     -22914
263747  feet/sec       YDOT =       -6984
267590  meter/sec
 ZDOT =      -6836
208735                 ZDOT =       -2083
676422


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   19312
14823929  
00016717  00000-0  10270-3 0  9179
2 25544  51
6409   7
4896 0006672 251
0571 108
9856 15
50006660 37582


Satellite: ISS
Catalog Number: 25544
Epoch time:      19312
14823929   =   yrday
fracday
Element set:     917
Inclination:       51
6409  deg
RA of node:         7
4896  deg
Eccentricity:     
0006672     
Arg of perigee:   251
0571  deg
Mean anomaly:     108
9856  deg
Mean motion:   15
50006660  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3758
Checksum:              325


Coasting Arc #19 (Orbit 3773)
---------------------------------------

Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 934263
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1857040
55                 A    =         6790487
54  meter
 Y    =        4097503
91  meter          E    =           
0005139
 Z    =        5089549
03                 I    =           51
64006
 XDOT =      -7364
896213                 Wp   =          203
59836
 YDOT =       1135
975158  meter/sec      RA   =            2
05904  deg
 ZDOT =       1768
719961                 TA   =          229
25119
                                          MA   =          229
29582
                                          Ha   =            225
768  n
mi
                                          Hp   =            223
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6092652
72                 X    =         1786360
31
 Y    =       13443254
29  feet           Y    =         4117875
55  meter
 Z    =       16697995
51                 Z    =         5098398
28
 XDOT =     -24163
045317                 XDOT =       -7385
643284
 YDOT =       3726
952617  feet/sec       YDOT =        1053
499717  meter/sec
 ZDOT =       5802
887012                 ZDOT =        1732
892873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13070204
90                 X    =         3983798
45
 Y    =       -6758392
78  feet           Y    =        -2059958
12  meter
 Z    =       16737933
80                 Z    =         5101722
22
 XDOT =       4648
191509                 XDOT =        1416
768772
 YDOT =      22988
154287  feet/sec       YDOT =        7006
789427  meter/sec
 ZDOT =       5639
409921                 ZDOT =        1718
892144


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   19313
17981351  
00016717  00000-0  10270-3 0  9188
2 25544  51
6404   2
3792 0006614 255
1704 104
8714 15
49963270 37748


Satellite: ISS
Catalog Number: 25544
Epoch time:      19313
17981351   =   yrday
fracday
Element set:     918
Inclination:       51
6404  deg
RA of node:         2
3792  deg
Eccentricity:     
0006614     
Arg of perigee:   255
1704  deg
Mean anomaly:     104
8714  deg
Mean motion:   15
49963270  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3774
Checksum:              310
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