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

 
Date: July 21st 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14504 3693 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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


201/16:28:21 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 218 5

201/22:50:29 000 0 0 -0 0 0 0
N/A -0 0 0 0 227 4
000/00:00:58 000 0 0 -0 0 218 6

203/20:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 4
000/00:00:00 000 0 0 0 0 218 9

203/23:12:38 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 218 8

204/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 4
000/00:00:00 000 0 0 0 0 218 9

210/10:44:30 000 0 0 0 0 0 0
N/A 0 0 0 0 226 6
000/00:00:00 000 0 0 0 0 219 8

212/15:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 226 2
000/00:00:00 000 0 0 0 0 220 2

213/11:38:30 000 0 0 0 0 0 0
N/A 0 0 0 0 226 2
000/00:00:00 000 0 0 0 0 220 3

Coasting Arc #1 (Orbit 2025)
---------------------------------------

Vector Time (GMT): 2019/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3942658
45                 A    =         6788550
53  meter
 Y    =        2682010
11  meter          E    =           
0016953
 Z    =       -4847685
52                 I    =           51
49056
 XDOT =      -5896
314466                 Wp   =          125
58905
 YDOT =      -4204
001225  meter/sec      RA   =          199
76622  deg
 ZDOT =       2466
075820                 TA   =          168
75826
                                          MA   =          168
72034
                                          Ha   =            227
781  n
mi
                                          Hp   =            218
222

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12935231
15                 X    =        -3948809
60
 Y    =        8799245
76  feet           Y    =         2637886
63  meter
 Z    =      -15904480
05                 Z    =        -4866851
72
 XDOT =     -19344
863734                 XDOT =       -5860
844453
 YDOT =     -13792
654939  feet/sec       YDOT =       -4269
739878  meter/sec
 ZDOT =       8090
799935                 ZDOT =        2437
520094

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13545340
62                 X    =         4128619
82
 Y    =        7647765
20  feet           Y    =         2331038
83  meter
 Z    =      -15991711
95                 Z    =        -4874273
80
 XDOT =      -3291
239270                 XDOT =       -1003
169730
 YDOT =      22501
062246  feet/sec       YDOT =        6858
323772  meter/sec
 ZDOT =       7961
406939                 ZDOT =        2426
636835


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   19200
51186303  
00016717  00000-0  10270-3 0  9006
2 25544  51
6388 200
9039 0006757 157
1527 202
9926 15
50962425 20268


Satellite: ISS
Catalog Number: 25544
Epoch time:      19200
51186303   =   yrday
fracday
Element set:     900
Inclination:       51
6388  deg
RA of node:       200
9039  deg
Eccentricity:     
0006757     
Arg of perigee:   157
1527  deg
Mean anomaly:     202
9926  deg
Mean motion:   15
50962425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2026
Checksum:              298


Coasting Arc #2 (Orbit 2041)
---------------------------------------

Vector Time (GMT): 2019/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4354233
11                 A    =         6789665
25  meter
 Y    =       -2567560
29  meter          E    =           
0010504
 Z    =        4522641
70                 I    =           51
52530
 XDOT =       5678
750789                 Wp   =          106
70630
 YDOT =       4084
847614  meter/sec      RA   =          194
79297  deg
 ZDOT =      -3145
170269                 TA   =           14
89634
                                          MA   =           14
86542
                                          Ha   =            227
492  n
mi
                                          Hp   =            218
469

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14285541
69                 X    =         4360652
67
 Y    =       -8423754
25  feet           Y    =        -2518832
69  meter
 Z    =       14838063
33                 Z    =         4543807
87
 XDOT =      18631
072141                 XDOT =        5647
927964
 YDOT =      13401
731018  feet/sec       YDOT =        4148
179316  meter/sec
 ZDOT =     -10318
800096                 ZDOT =       -3117
660124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13958864
96                 X    =        -4254662
04
 Y    =       -8793116
16  feet           Y    =        -2680141
80  meter
 Z    =       14934378
37                 Z    =         4551998
53
 XDOT =       2773
187974                 XDOT =         845
267694
 YDOT =     -21733
424969  feet/sec       YDOT =       -6624
347931  meter/sec
 ZDOT =     -10194
124598                 ZDOT =       -3107
169178


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   19201
54277955  
00016717  00000-0  10270-3 0  9015
2 25544  51
6376 195
7889 0006680 161
9844 198
1545 15
50999599 20422


Satellite: ISS
Catalog Number: 25544
Epoch time:      19201
54277955   =   yrday
fracday
Element set:     901
Inclination:       51
6376  deg
RA of node:       195
7889  deg
Eccentricity:     
0006680     
Arg of perigee:   161
9844  deg
Mean anomaly:     198
1545  deg
Mean motion:   15
50999599  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2042
Checksum:              361


Coasting Arc #3 (Orbit 2044)
---------------------------------------

Vector Time (GMT): 2019/201/16:28:21
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         169138
26                 A    =         6786614
51  meter
 Y    =       -4271292
62  meter          E    =           
0009170
 Z    =        5268064
81                 I    =           51
52348
 XDOT =       7527
183701                 Wp   =          149
69026
 YDOT =       1242
391846  meter/sec      RA   =          193
89745  deg
 ZDOT =        757
318362                 TA   =          293
01244
                                          MA   =          293
10913
                                          Ha   =            227
498  n
mi
                                          Hp   =            218
515

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         554915
56                 X    =          191299
71
 Y    =      -14013427
24  feet           Y    =        -4269277
71  meter
 Z    =       17283677
21                 Z    =         5268939
89
 XDOT =      24695
484582                 XDOT =        7509
052932
 YDOT =       4076
088732  feet/sec       YDOT =        1326
464662  meter/sec
 ZDOT =       2484
640296                 ZDOT =         793
837911

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         628574
43                 X    =          191589
49
 Y    =       14005052
58  feet           Y    =         4268740
03  meter
 Z    =       17287942
86                 Z    =         5269364
98
 XDOT =     -23895
527887                 XDOT =       -7283
356900
 YDOT =      -2232
966495  feet/sec       YDOT =        -680
608188  meter/sec
 ZDOT =       2650
436085                 ZDOT =         807
852919


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   19201
73607669  
00016717  00000-0  10270-3 0  9026
2 25544  51
6399 194
8308 0006564 163
7824 196
3538 15
51025570 20457


Satellite: ISS
Catalog Number: 25544
Epoch time:      19201
73607669   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:       194
8308  deg
Eccentricity:     
0006564     
Arg of perigee:   163
7824  deg
Mean anomaly:     196
3538  deg
Mean motion:   15
51025570  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2045
Checksum:              327


Coasting Arc #4 (Orbit 2048)
---------------------------------------

Vector Time (GMT): 2019/201/22:50:58
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4749313
92                 A    =         6790787
20  meter
 Y    =       -2376617
91  meter          E    =           
0011764
 Z    =        4219955
44                 I    =           51
54454
 XDOT =       5320
707357                 Wp   =          108
27869
 YDOT =       4150
203487  meter/sec      RA   =          192
54351  deg
 ZDOT =      -3646
066182                 TA   =           19
11943
                                          MA   =           19
07531
                                          Ha   =            227
379  n
mi
                                          Hp   =            218
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15581738
59                 X    =         4755039
18
 Y    =       -7797302
86  feet           Y    =        -2323476
06  meter
 Z    =       13844998
15                 Z    =         4243039
08
 XDOT =      17456
388966                 XDOT =        5291
613355
 YDOT =      13616
153174  feet/sec       YDOT =        4209
540979  meter/sec
 ZDOT =     -11962
159391                 ZDOT =       -3620
291041

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10434973
28                 X    =         3180579
86
 Y    =       13848499
09  feet           Y    =         4221022
52  meter
 Z    =       13950013
94                 Z    =         4251964
25
 XDOT =      -9257
814929                 XDOT =       -2821
781990
 YDOT =      18923
605278  feet/sec       YDOT =        5767
914889  meter/sec
 ZDOT =     -11845
359783                 ZDOT =       -3610
465662


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   19201
99380444  
00016717  00000-0  10270-3 0  9034
2 25544  51
6385 193
5493 0006607 165
9564 194
1772 15
50999060 20499


Satellite: ISS
Catalog Number: 25544
Epoch time:      19201
99380444   =   yrday
fracday
Element set:     903
Inclination:       51
6385  deg
RA of node:       193
5493  deg
Eccentricity:     
0006607     
Arg of perigee:   165
9564  deg
Mean anomaly:     194
1772  deg
Mean motion:   15
50999060  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2049
Checksum:              337


Coasting Arc #5 (Orbit 2063)
---------------------------------------

Vector Time (GMT): 2019/202/22:50:58
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5132431
31                 A    =         6792273
27  meter
 Y    =        2350356
00  meter          E    =           
0010928
 Z    =       -3790731
04                 I    =           51
58206
 XDOT =      -4957
253689                 Wp   =          138
22073
 YDOT =      -4029
561244  meter/sec      RA   =          187
57509  deg
 ZDOT =       4212
460703                 TA   =          176
41937
                                          MA   =          176
41154
                                          Ha   =            227
488  n
mi
                                          Hp   =            218
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16838685
41                 X    =        -5139919
27
 Y    =        7711141
73  feet           Y    =         2292919
93  meter
 Z    =      -12436781
64                 Z    =        -3815680
08
 XDOT =     -16263
955671                 XDOT =       -4932
286987
 YDOT =     -13220
345288  feet/sec       YDOT =       -4084
857411  meter/sec
 ZDOT =      13820
409132                 ZDOT =        4188
441016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10834607
81                 X    =        -3302388
46
 Y    =      -14925760
30  feet           Y    =        -4549371
74  meter
 Z    =      -12550279
82                 Z    =        -3825325
29
 XDOT =       8681
319929                 XDOT =        2646
066314
 YDOT =     -17833
654212  feet/sec       YDOT =       -5435
697804  meter/sec
 ZDOT =      13711
557641                 ZDOT =        4179
282769


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   19202
96028664  
00016717  00000-0  10270-3 0  9046
2 25544  51
6382 188
7530 0006755 168
0131 192
1182 15
50999691 20642


Satellite: ISS
Catalog Number: 25544
Epoch time:      19202
96028664   =   yrday
fracday
Element set:     904
Inclination:       51
6382  deg
RA of node:       188
7530  deg
Eccentricity:     
0006755     
Arg of perigee:   168
0131  deg
Mean anomaly:     192
1182  deg
Mean motion:   15
50999691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2064
Checksum:              322


Coasting Arc #6 (Orbit 2078)
---------------------------------------

Vector Time (GMT): 2019/203/20:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4009952
23                 A    =         6791201
96  meter
 Y    =       -3535161
99  meter          E    =           
0014108
 Z    =        4185069
24                 I    =           51
61052
 XDOT =       6181
843148                 Wp   =          129
26787
 YDOT =      -2607
543107  meter/sec      RA   =          183
06369  deg
 ZDOT =       3703
450113                 TA   =          282
58877
                                          MA   =          282
74650
                                          Ha   =            227
393  n
mi
                                          Hp   =            218
937

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13156011
24                 X    =        -3990451
46
 Y    =      -11598300
48  feet           Y    =        -3579895
30  meter
 Z    =       13730542
12                 Z    =         4165637
83
 XDOT =      20281
637626                 XDOT =        6192
552952
 YDOT =      -8554
931453  feet/sec       YDOT =       -2538
353728  meter/sec
 ZDOT =      12150
426880                 ZDOT =        3733
504626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14934949
43                 X    =         4552172
59
 Y    =       -9325167
06  feet           Y    =        -2842310
92  meter
 Z    =       13642490
15                 Z    =         4158231
00
 XDOT =       1662
775909                 XDOT =         506
814097
 YDOT =      20721
518176  feet/sec       YDOT =        6315
918740  meter/sec
 ZDOT =      12287
148732                 ZDOT =        3745
122934


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   19203
92676530  
00016717  00000-0  10270-3 0  9055
2 25544  51
6403 183
9604 0006362 171
4264 188
6997 15
50977705 20796


Satellite: ISS
Catalog Number: 25544
Epoch time:      19203
92676530   =   yrday
fracday
Element set:     905
Inclination:       51
6403  deg
RA of node:       183
9604  deg
Eccentricity:     
0006362     
Arg of perigee:   171
4264  deg
Mean anomaly:     188
6997  deg
Mean motion:   15
50977705  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2079
Checksum:              335


Coasting Arc #7 (Orbit 2079)
---------------------------------------

Vector Time (GMT): 2019/203/23:12:38
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4565199
66                 A    =         6792262
19  meter
 Y    =        3250661
64  meter          E    =           
0008801
 Z    =       -3839332
22                 I    =           51
61591
 XDOT =      -5661
141022                 Wp   =          126
52181
 YDOT =       3046
130475  meter/sec      RA   =          182
58713  deg
 ZDOT =      -4164
123921                 TA   =           99
61539
                                          MA   =           99
51595
                                          Ha   =            227
471  n
mi
                                          Hp   =            218
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14977689
17                 X    =         4547159
62
 Y    =       10664900
40  feet           Y    =         3301612
26  meter
 Z    =      -12596234
32                 Z    =        -3817200
13
 XDOT =     -18573
297315                 XDOT =       -5674
556262
 YDOT =       9993
866389  feet/sec       YDOT =        2982
748852  meter/sec
 ZDOT =     -13661
823887                 ZDOT =       -4191
655649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5585539
02                 X    =        -1702472
29
 Y    =       17589509
08  feet           Y    =         5361282
37  meter
 Z    =      -12495892
00                 Z    =        -3808747
88
 XDOT =     -13851
409092                 XDOT =       -4221
909491
 YDOT =     -14165
478959  feet/sec       YDOT =       -4317
637987  meter/sec
 ZDOT =     -13787
113825                 ZDOT =       -4202
312294


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   19203
99119734  
00016717  00000-0  10270-3 0  9061
2 25544  51
6386 183
6379 0006724 169
6948 190
4342 15
51016624 20804


Satellite: ISS
Catalog Number: 25544
Epoch time:      19203
99119734   =   yrday
fracday
Element set:     906
Inclination:       51
6386  deg
RA of node:       183
6379  deg
Eccentricity:     
0006724     
Arg of perigee:   169
6948  deg
Mean anomaly:     190
4342  deg
Mean motion:   15
51016624  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2080
Checksum:              329


Coasting Arc #8 (Orbit 2087)
---------------------------------------

Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          77593
95                 A    =         6786485
02  meter
 Y    =       -4212465
63  meter          E    =           
0007299
 Z    =        5317414
21                 I    =           51
61260
 XDOT =       7665
817050                 Wp   =          153
53797
 YDOT =         67
985426  meter/sec      RA   =          180
12703  deg
 ZDOT =        -64
361569                 TA   =          297
03848
                                          MA   =          297
11296
                                          Ha   =            227
363  n
mi
                                          Hp   =            218
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         254573
34                 X    =           98864
46
 Y    =      -13820425
29  feet           Y    =        -4211479
29  meter
 Z    =       17445584
67                 Z    =         5317842
55
 XDOT =      25150
318405                 XDOT =        7664
799710
 YDOT =        223
049297  feet/sec       YDOT =         153
704292  meter/sec
 ZDOT =       -211
160004                 ZDOT =         -27
126819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13383468
22                 X    =        -4079281
11
 Y    =        3445892
90  feet           Y    =         1050308
16  meter
 Z    =       17447807
54                 Z    =         5318091
74
 XDOT =      -6046
029504                 XDOT =       -1842
829793
 YDOT =     -23375
140200  feet/sec       YDOT =       -7124
742733  meter/sec
 ZDOT =        -41
980024                 ZDOT =         -12
795511


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   19204
50665133  
00016717  00000-0  10270-3 0  9079
2 25544  51
6382 181
0836 0006588 172
3543 187
7709 15
50994983 20886


Satellite: ISS
Catalog Number: 25544
Epoch time:      19204
50665133   =   yrday
fracday
Element set:     907
Inclination:       51
6382  deg
RA of node:       181
0836  deg
Eccentricity:     
0006588     
Arg of perigee:   172
3543  deg
Mean anomaly:     187
7709  deg
Mean motion:   15
50994983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2088
Checksum:              339


Coasting Arc #9 (Orbit 2102)
---------------------------------------

Vector Time (GMT): 2019/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931973
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -592015
77                 A    =         6786745
94  meter
 Y    =        4241791
87  meter          E    =           
0016987
 Z    =       -5278533
34                 I    =           51
64667
 XDOT =      -7606
043278                 Wp   =          118
90856
 YDOT =        -17
481323  meter/sec      RA   =          175
16014  deg
 ZDOT =        833
031868                 TA   =          159
10641
                                          MA   =          159
03690
                                          Ha   =            227
262  n
mi
                                          Hp   =            219
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1942308
97                 X    =         -613764
76
 Y    =       13916640
00  feet           Y    =         4235050
25  meter
 Z    =      -17318022
76                 Z    =        -5281461
67
 XDOT =     -24954
210230                 XDOT =       -7609
328873
 YDOT =        -57
353422  feet/sec       YDOT =        -102
555864  meter/sec
 ZDOT =       2733
044187                 ZDOT =         796
076905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13879943
78                 X    =         4230606
86
 Y    =       -2078909
75  feet           Y    =         -633651
69  meter
 Z    =      -17331608
13                 Z    =        -5282674
16
 XDOT =       6673
735869                 XDOT =        2034
154693
 YDOT =      23009
108809  feet/sec       YDOT =        7013
176365  meter/sec
 ZDOT =       2565
112228                 ZDOT =         781
846207


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   19205
47312779  
00016717  00000-0  10270-3 0  9082
2 25544  51
6382 176
2887 0006570 175
7220 184
3988 15
50980688 21035


Satellite: ISS
Catalog Number: 25544
Epoch time:      19205
47312779   =   yrday
fracday
Element set:     908
Inclination:       51
6382  deg
RA of node:       176
2887  deg
Eccentricity:     
0006570     
Arg of perigee:   175
7220  deg
Mean anomaly:     184
3988  deg
Mean motion:   15
50980688  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2103
Checksum:              341


Coasting Arc #10 (Orbit 2118)
---------------------------------------

Vector Time (GMT): 2019/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951979
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1064132
69                 A    =         6787219
95  meter
 Y    =       -4302722
92  meter          E    =           
0005425
 Z    =        5135858
27                 I    =           51
68197
 XDOT =       7502
215441                 Wp   =          134
69101
 YDOT =        -28
491810  meter/sec      RA   =          170
19583  deg
 ZDOT =      -1581
005417                 TA   =          330
53148
                                          MA   =          330
56205
                                          Ha   =            227
096  n
mi
                                          Hp   =            219
173

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3491248
97                 X    =         1087220
90
 Y    =      -14116545
01  feet           Y    =        -4290694
33  meter
 Z    =       16849928
70                 Z    =         5141083
15
 XDOT =      24613
567721                 XDOT =        7509
656063
 YDOT =        -93
477068  feet/sec       YDOT =          55
444952  meter/sec
 ZDOT =      -5187
025646                 ZDOT =       -1544
544631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14486572
97                 X    =        -4415507
44
 Y    =         891336
81  feet           Y    =          271679
46  meter
 Z    =       16873958
69                 Z    =         5143182
61
 XDOT =      -7222
283346                 XDOT =       -2201
351964
 YDOT =     -22489
824213  feet/sec       YDOT =       -6854
898420  meter/sec
 ZDOT =      -5021
315635                 ZDOT =       -1530
497006


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   19206
50403257  
00016717  00000-0  10270-3 0  9090
2 25544  51
6384 171
1737 0006519 180
2684 179
8465 15
51007643 21191


Satellite: ISS
Catalog Number: 25544
Epoch time:      19206
50403257   =   yrday
fracday
Element set:     909
Inclination:       51
6384  deg
RA of node:       171
1737  deg
Eccentricity:     
0006519     
Arg of perigee:   180
2684  deg
Mean anomaly:     179
8465  deg
Mean motion:   15
51007643  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2119
Checksum:              315


Coasting Arc #11 (Orbit 2133)
---------------------------------------

Vector Time (GMT): 2019/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951979
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1538858
06                 A    =         6788201
15  meter
 Y    =        4425500
36  meter          E    =           
0015003
 Z    =       -4925187
70                 I    =           51
71813
 XDOT =      -7295
284535                 Wp   =          131
46039
 YDOT =         38
413836  meter/sec      RA   =          165
23431  deg
 ZDOT =       2308
782440                 TA   =          161
17225
                                          MA   =          161
11671
                                          Ha   =            226
993  n
mi
                                          Hp   =            219
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5048746
93                 X    =        -1564307
22
 Y    =       14519358
15  feet           Y    =         4408149
92  meter
 Z    =      -16158752
30                 Z    =        -4932724
26
 XDOT =     -23934
660547                 XDOT =       -7306
386610
 YDOT =        126
029645  feet/sec       YDOT =         -43
229445  meter/sec
 ZDOT =       7574
745539                 ZDOT =        2273
317916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15334105
83                 X    =         4673835
46
 Y    =         221310
77  feet           Y    =           67455
52  meter
 Z    =      -16193304
25                 Z    =        -4935719
13
 XDOT =       7534
050264                 XDOT =        2296
378521
 YDOT =      21658
584636  feet/sec       YDOT =        6601
536597  meter/sec
 ZDOT =       7413
541030                 ZDOT =        2259
647306


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   19207
47050299  
00016717  00000-0  10270-3 0  9103
2 25544  51
6388 166
3783 0006395 183
2636 176
8474 15
50992958 21349


Satellite: ISS
Catalog Number: 25544
Epoch time:      19207
47050299   =   yrday
fracday
Element set:     910
Inclination:       51
6388  deg
RA of node:       166
3783  deg
Eccentricity:     
0006395     
Arg of perigee:   183
2636  deg
Mean anomaly:     176
8474  deg
Mean motion:   15
50992958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2134
Checksum:              346


Coasting Arc #12 (Orbit 2149)
---------------------------------------

Vector Time (GMT): 2019/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951979
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1956571
94                 A    =         6789307
88  meter
 Y    =       -4568605
94  meter          E    =           
0007236
 Z    =        4618240
38                 I    =           51
75347
 XDOT =       7055
287281                 Wp   =          113
18505
 YDOT =        -14
923463  meter/sec      RA   =          160
27657  deg
 ZDOT =      -3002
864014                 TA   =            6
73098
                                          MA   =            6
72126
                                          Ha   =            226
799  n
mi
                                          Hp   =            219
490

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6419199
28                 X    =         1985081
29
 Y    =      -14988864
62  feet           Y    =        -4546567
27  meter
 Z    =       15151707
29                 Z    =         4627813
36
 XDOT =      23147
267982                 XDOT =        7069
515950
 YDOT =        -48
961492  feet/sec       YDOT =          64
053600  meter/sec
 ZDOT =      -9851
916056                 ZDOT =       -2968
557728

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16226995
68                 X    =        -4945988
28
 Y    =       -1107574
32  feet           Y    =         -337588
65  meter
 Z    =       15195535
74                 Z    =         4631599
29
 XDOT =      -7665
890157                 XDOT =       -2336
563320
 YDOT =     -20755
555673  feet/sec       YDOT =       -6326
293369  meter/sec
 ZDOT =      -9695
955088                 ZDOT =       -2955
327111


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   19208
50140278  
00016717  00000-0  10270-3 0  9116
2 25544  51
6381 161
2635 0006355 187
9560 172
1491 15
51017646 21504


Satellite: ISS
Catalog Number: 25544
Epoch time:      19208
50140278   =   yrday
fracday
Element set:     911
Inclination:       51
6381  deg
RA of node:       161
2635  deg
Eccentricity:     
0006355     
Arg of perigee:   187
9560  deg
Mean anomaly:     172
1491  deg
Mean motion:   15
51017646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2150
Checksum:              294


Coasting Arc #13 (Orbit 2164)
---------------------------------------

Vector Time (GMT): 2019/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2345059
87                 A    =         6790767
14  meter
 Y    =        4759340
42  meter          E    =           
0011087
 Z    =       -4249855
52                 I    =           51
78961
 XDOT =      -6731
370757                 Wp   =          145
11522
 YDOT =        -61
583215  meter/sec      RA   =          155
32196  deg
 ZDOT =       3641
227545                 TA   =          162
16918
                                          MA   =          162
13024
                                          Ha   =            226
729  n
mi
                                          Hp   =            219
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7693765
96                 X    =        -2377462
63
 Y    =       15614633
93  feet           Y    =         4732935
67  meter
 Z    =      -13943095
54                 Z    =        -4261324
95
 XDOT =     -22084
549729                 XDOT =       -6747
868732
 YDOT =       -202
044670  feet/sec       YDOT =        -136
950829  meter/sec
 ZDOT =      11946
284595                 ZDOT =        3608
489274

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17269330
77                 X    =         5263692
02
 Y    =        1820697
46  feet           Y    =          554948
58  meter
 Z    =      -13995571
32                 Z    =        -4265850
14
 XDOT =       7500
779886                 XDOT =        2286
237709
 YDOT =      19645
599949  feet/sec       YDOT =        5987
978864  meter/sec
 ZDOT =      11797
433849                 ZDOT =        3595
857837


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   19209
46786969  
00016717  00000-0  10270-3 0  9126
2 25544  51
6385 156
4681 0006355 191
7397 168
3606 15
51001391 21657


Satellite: ISS
Catalog Number: 25544
Epoch time:      19209
46786969   =   yrday
fracday
Element set:     912
Inclination:       51
6385  deg
RA of node:       156
4681  deg
Eccentricity:     
0006355     
Arg of perigee:   191
7397  deg
Mean anomaly:     168
3606  deg
Mean motion:   15
51001391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2165
Checksum:              337


Coasting Arc #14 (Orbit 2180)
---------------------------------------

Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3581942
44                 A    =         6787251
61  meter
 Y    =       -2615798
90  meter          E    =           
0009304
 Z    =        5137717
78                 I    =           51
80904
 XDOT =       5796
340792                 Wp   =          165
82610
 YDOT =      -4745
205492  meter/sec      RA   =          150
46350  deg
 ZDOT =       1615
752108                 TA   =          268
55952
                                          MA   =          268
66610
                                          Ha   =            226
613  n
mi
                                          Hp   =            219
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11751779
65                 X    =        -3577381
46
 Y    =       -8582017
39  feet           Y    =        -2655829
87  meter
 Z    =       16856029
46                 Z    =         5120329
00
 XDOT =      19016
866117                 XDOT =        5841
123926
 YDOT =     -15568
259487  feet/sec       YDOT =       -4680
136555  meter/sec
 ZDOT =       5301
023978                 ZDOT =        1644
016341

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4728418
91                 X    =        -1441222
09
 Y    =       13858242
32  feet           Y    =         4223992
26  meter
 Z    =       16777134
78                 Z    =         5113670
68
 XDOT =     -19434
958051                 XDOT =       -5923
775214
 YDOT =     -13242
321419  feet/sec       YDOT =       -4036
259569  meter/sec
 ZDOT =       5429
886974                 ZDOT =        1655
029550


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   19210
49876332  
00016717  00000-0  10270-3 0  9136
2 25544  51
6400 151
3534 0006364 196
7691 163
3251 15
51046508 21816


Satellite: ISS
Catalog Number: 25544
Epoch time:      19210
49876332   =   yrday
fracday
Element set:     913
Inclination:       51
6400  deg
RA of node:       151
3534  deg
Eccentricity:     
0006364     
Arg of perigee:   196
7691  deg
Mean anomaly:     163
3251  deg
Mean motion:   15
51046508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2181
Checksum:              296


Coasting Arc #15 (Orbit 2195)
---------------------------------------

Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3140418
57                 A    =         6786681
42  meter
 Y    =        2885771
61  meter          E    =           
0012950
 Z    =       -5289157
13                 I    =           51
83552
 XDOT =      -5868
459899                 Wp   =          109
21459
 YDOT =       4841
335611  meter/sec      RA   =          145
50859  deg
 ZDOT =       -848
782931                 TA   =          152
71222
                                          MA   =          152
64412
                                          Ha   =            226
467  n
mi
                                          Hp   =            220
085

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10303210
53                 X    =         3133606
96
 Y    =        9467754
61  feet           Y    =         2920852
57  meter
 Z    =      -17352877
71                 Z    =        -5273918
60
 XDOT =     -19253
477358                 XDOT =       -5918
038111
 YDOT =      15883
647018  feet/sec       YDOT =        4775
433272  meter/sec
 ZDOT =      -2784
720901                 ZDOT =        -877
408985

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5778687
48                 X    =         1761343
94
 Y    =      -12837247
80  feet           Y    =        -3912793
13  meter
 Z    =      -17283770
69                 Z    =        -5268093
31
 XDOT =      20118
610227                 XDOT =        6132
152397
 YDOT =      12955
511028  feet/sec       YDOT =        3948
839761  meter/sec
 ZDOT =      -2915
261280                 ZDOT =        -888
571638


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   19211
46522480  
00016717  00000-0  10270-3 0  9147
2 25544  51
6401 146
5573 0006251 199
5121 160
5792 15
51019794 21962


Satellite: ISS
Catalog Number: 25544
Epoch time:      19211
46522480   =   yrday
fracday
Element set:     914
Inclination:       51
6401  deg
RA of node:       146
5573  deg
Eccentricity:     
0006251     
Arg of perigee:   199
5121  deg
Mean anomaly:     160
5792  deg
Mean motion:   15
51019794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2196
Checksum:              303


Coasting Arc #16 (Orbit 2211)
---------------------------------------

Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2739096
46                 A    =         6786360
70  meter
 Y    =       -3173081
81  meter          E    =           
0005953
 Z    =        5337189
53                 I    =           51
86201
 XDOT =       5875
588841                 Wp   =          181
28270
 YDOT =      -4919
682646  meter/sec      RA   =          140
55777  deg
 ZDOT =         84
746491                 TA   =          267
87764
                                          MA   =          267
94581
                                          Ha   =            226
356  n
mi
                                          Hp   =            220
133

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8986536
93                 X    =        -2729335
07
 Y    =      -10410373
40  feet           Y    =        -3203658
34  meter
 Z    =       17510464
35                 Z    =         5323907
68
 XDOT =      19276
866277                 XDOT =        5929
753822
 YDOT =     -16140
691097  feet/sec       YDOT =       -4853
674840  meter/sec
 ZDOT =        278
039669                 ZDOT =         113
418234

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6876690
89                 X    =        -2096015
38
 Y    =       11997887
99  feet           Y    =         3656956
26  meter
 Z    =       17450269
00                 Z    =         5318841
99
 XDOT =     -20663
098772                 XDOT =       -6298
112506
 YDOT =     -12465
589508  feet/sec       YDOT =       -3799
511682  meter/sec
 ZDOT =        408
816494                 ZDOT =         124
607267


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   19212
49611430  
00016717  00000-0  10270-3 0  9156
2 25544  51
6406 141
4438 0006228 204
0095 156
0767 15
51040120 22125


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
49611430   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:       141
4438  deg
Eccentricity:     
0006228     
Arg of perigee:   204
0095  deg
Mean anomaly:     156
0767  deg
Mean motion:   15
51040120  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2212
Checksum:              265


Coasting Arc #17 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1866658
88                 A    =         6792482
22  meter
 Y    =       -5386884
43  meter          E    =           
0010142
 Z    =        3680584
25                 I    =           51
89036
 XDOT =       6246
936084                 Wp   =          116
90946
 YDOT =       -823
983568  meter/sec      RA   =          139
53526  deg
 ZDOT =      -4369
412953                 TA   =           19
51408
                                          MA   =           19
47529
                                          Ha   =            226
151  n
mi
                                          Hp   =            220
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6124208
91                 X    =         1908880
03
 Y    =      -17673505
35  feet           Y    =        -5365774
47  meter
 Z    =       12075407
63                 Z    =         3689753
51
 XDOT =      20495
197125                 XDOT =        6276
909491
 YDOT =      -2703
358162  feet/sec       YDOT =        -753
957872  meter/sec
 ZDOT =     -14335
344333                 ZDOT =       -4338
995699

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5475191
00                 X    =        -1668838
22
 Y    =       17856725
22  feet           Y    =         5442729
85  meter
 Z    =       12117501
53                 Z    =         3693414
47
 XDOT =     -19192
183283                 XDOT =       -5849
777465
 YDOT =       3759
916444  feet/sec       YDOT =        1146
022532  meter/sec
 ZDOT =     -14196
912302                 ZDOT =       -4327
218870


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   19212
68940476  
00016717  00000-0  10270-3 0  9163
2 25544  51
6429 140
4861 0006160 205
4021 154
6828 15
51063957 22156


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
68940476   =   yrday
fracday
Element set:     916
Inclination:       51
6429  deg
RA of node:       140
4861  deg
Eccentricity:     
0006160     
Arg of perigee:   205
4021  deg
Mean anomaly:     154
6828  deg
Mean motion:   15
51063957  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              303


Coasting Arc #18 (Orbit 2227)
---------------------------------------

Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         475796
99                 A    =         6790456
77  meter
 Y    =       -5217579
22  meter          E    =           
0006846
 Z    =        4312710
16                 I    =           51
90301
 XDOT =       6367
550467                 Wp   =          112
45041
 YDOT =      -2361
494935  meter/sec      RA   =          135
40374  deg
 ZDOT =      -3557
513629                 TA   =           13
68980
                                          MA   =           13
67124
                                          Ha   =            226
165  n
mi
                                          Hp   =            220
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1561013
75                 X    =          513157
91
 Y    =      -17118042
06  feet           Y    =        -5212050
00  meter
 Z    =       14149311
56                 Z    =         4315111
63
 XDOT =      20890
913605                 XDOT =        6410
764100
 YDOT =      -7747
686794  feet/sec       YDOT =       -2290
046580  meter/sec
 ZDOT =     -11671
632640                 ZDOT =       -3526
478529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15078522
48                 X    =        -4595933
65
 Y    =        8233011
91  feet           Y    =         2509422
03  meter
 Z    =       14160608
05                 Z    =         4316153
33
 XDOT =     -17441
260440                 XDOT =       -5316
096182
 YDOT =     -12100
337270  feet/sec       YDOT =       -3688
182800  meter/sec
 ZDOT =     -11530
264166                 ZDOT =       -3514
424518


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   19213
52700155  
00016717  00000-0  10270-3 0  9176
2 25544  51
6419 136
3295 0006269 208
1012 151
9802 15
51034680 22287


Satellite: ISS
Catalog Number: 25544
Epoch time:      19213
52700155   =   yrday
fracday
Element set:     917
Inclination:       51
6419  deg
RA of node:       136
3295  deg
Eccentricity:     
0006269     
Arg of perigee:   208
1012  deg
Mean anomaly:     151
9802  deg
Mean motion:   15
51034680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2228
Checksum:              287


Coasting Arc #19 (Orbit 2242)
---------------------------------------

Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -729192
49                 A    =         6791952
89  meter
 Y    =        5534495
01  meter          E    =           
0007529
 Z    =       -3877073
07                 I    =           51
93156
 XDOT =      -6075
048403                 Wp   =          157
66092
 YDOT =       2111
362578  meter/sec      RA   =          130
45941  deg
 ZDOT =       4152
410921                 TA   =          155
90540
                                          MA   =          155
87016
                                          Ha   =            225
971  n
mi
                                          Hp   =            220
463

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2392363
80                 X    =         -772194
45
 Y    =       18157792
02  feet           Y    =         5526100
45  meter
 Z    =      -12720056
00                 Z    =        -3880719
24
 XDOT =     -19931
261166                 XDOT =       -6118
376320
 YDOT =       6927
042579  feet/sec       YDOT =        2043
184621  meter/sec
 ZDOT =      13623
395411                 ZDOT =        4122
796298

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16267982
32                 X    =         4958481
01
 Y    =       -8387440
63  feet           Y    =        -2556491
90  meter
 Z    =      -12737041
69                 Z    =        -3882250
31
 XDOT =      16441
991662                 XDOT =        5011
519059
 YDOT =      11386
343658  feet/sec       YDOT =        3470
557547  meter/sec
 ZDOT =      13488
491179                 ZDOT =        4111
292111


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   19214
49345386  
00016717  00000-0  10270-3 0  9185
2 25544  51
6424 131
5338 0006186 211
6253 148
4527 15
51044567 22439


Satellite: ISS
Catalog Number: 25544
Epoch time:      19214
49345386   =   yrday
fracday
Element set:     918
Inclination:       51
6424  deg
RA of node:       131
5338  deg
Eccentricity:     
0006186     
Arg of perigee:   211
6253  deg
Mean anomaly:     148
4527  deg
Mean motion:   15
51044567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2243
Checksum:              308


Coasting Arc #20 (Orbit 2257)
---------------------------------------

Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936703
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         921981
28                 A    =         6793513
51  meter
 Y    =       -5822128
71  meter          E    =           
0010343
 Z    =        3363816
98                 I    =           51
95732
 XDOT =       5792
427411                 Wp   =          120
38789
 YDOT =      -1796
424960  meter/sec      RA   =          125
51967  deg
 ZDOT =      -4691
277279                 TA   =           20
61130
                                          MA   =           20
56961
                                          Ha   =            225
865  n
mi
                                          Hp   =            220
598

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3024872
97                 X    =          970678
32
 Y    =      -19101472
16  feet           Y    =        -5811546
29  meter
 Z    =       11036144
95                 Z    =         3368413
61
 XDOT =      19004
026939                 XDOT =        5834
872110
 YDOT =      -5893
782676  feet/sec       YDOT =       -1731
412503  meter/sec
 ZDOT =     -15391
329655                 ZDOT =       -4663
037493

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17263527
80                 X    =        -5261923
27
 Y    =        8689954
54  feet           Y    =         2648698
14  meter
 Z    =       11057481
11                 Z    =         3370320
24
 XDOT =     -15261
045780                 XDOT =       -4651
566754
 YDOT =     -10873
338922  feet/sec       YDOT =       -3314
193703  meter/sec
 ZDOT =     -15262
691141                 ZDOT =       -4652
068260


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   19215
52433335  
00016717  00000-0  10270-3 0  9193
2 25544  51
6422 126
4198 0006141 215
2873 144
7872 15
51041991 22589


Satellite: ISS
Catalog Number: 25544
Epoch time:      19215
52433335   =   yrday
fracday
Element set:     919
Inclination:       51
6422  deg
RA of node:       126
4198  deg
Eccentricity:     
0006141     
Arg of perigee:   215
2873  deg
Mean anomaly:     144
7872  deg
Mean motion:   15
51041991  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2258
Checksum:              306
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