[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: July 23rd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14481 7651 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


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 0 219 0

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

205/22:24:29 000 0 0 0 0 0 0
N/A 0 0 0 0 227 2
000/00:00:00 000 0 0 0 0 219 2

207/04:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 1
000/00:00:00 000 0 0 0 0 219 4

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 9

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 4

216/18:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 225 8
000/00:00:00 000 0 0 0 0 220 9

Coasting Arc #1 (Orbit 2072)
---------------------------------------

Vector Time (GMT): 2019/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5123823
74                 A    =         6792574
74  meter
 Y    =       -2492837
07  meter          E    =           
0013910
 Z    =        3681528
13                 I    =           51
60183
 XDOT =       5004
341998                 Wp   =          112
61470
 YDOT =       3872
963914  meter/sec      RA   =          184
85742  deg
 ZDOT =      -4334
559540                 TA   =           23
56064
                                          MA   =           23
49699
                                          Ha   =            227
268  n
mi
                                          Hp   =            218
742

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16810445
33                 X    =         5133436
01
 Y    =       -8178599
30  feet           Y    =        -2435485
35  meter
 Z    =       12078504
38                 Z    =         3706440
56
 XDOT =      16418
444874                 XDOT =        4981
716028
 YDOT =      12706
574522  feet/sec       YDOT =        3928
799733  meter/sec
 ZDOT =     -14220
995867                 ZDOT =       -4310
305418

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15274449
68                 X    =        -4655652
26
 Y    =      -10649918
40  feet           Y    =        -3246095
13  meter
 Z    =       12191851
86                 Z    =         3716076
45
 XDOT =       2307
377129                 XDOT =         703
288549
 YDOT =     -19492
628050  feet/sec       YDOT =       -5941
353030  meter/sec
 ZDOT =     -14111
060123                 ZDOT =       -4301
051126


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
54017763  
00016717  00000-0  10270-3 0  9005
2 25544  51
6388 185
8785 0006487 168
9886 191
1408 15
51007000 20731


Satellite: ISS
Catalog Number: 25544
Epoch time:      19203
54017763   =   yrday
fracday
Element set:     900
Inclination:       51
6388  deg
RA of node:       185
8785  deg
Eccentricity:     
0006487     
Arg of perigee:   168
9886  deg
Mean anomaly:     191
1408  deg
Mean motion:   15
51007000  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2073
Checksum:              320


Coasting Arc #2 (Orbit 2078)
---------------------------------------

Vector Time (GMT): 2019/203/20:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4012480
37                 A    =         6791220
63  meter
 Y    =       -3534074
52  meter          E    =           
0014070
 Z    =        4183574
95                 I    =           51
61067
 XDOT =       6179
742290                 Wp   =          129
13263
 YDOT =      -2609
410903  meter/sec      RA   =          183
06342  deg
 ZDOT =       3705
646529                 TA   =          282
69775
                                          MA   =          282
85500
                                          Ha   =            227
384  n
mi
                                          Hp   =            218
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13164305
69                 X    =        -3992984
32
 Y    =      -11594732
69  feet           Y    =        -3578836
13  meter
 Z    =       13725639
60                 Z    =         4164131
25
 XDOT =      20274
745046                 XDOT =        6190
462467
 YDOT =      -8561
059393  feet/sec       YDOT =       -2540
244959  meter/sec
 ZDOT =      12157
632968                 ZDOT =        3735
690862

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14933925
27                 X    =         4551860
42
 Y    =       -9334107
23  feet           Y    =        -2845035
88  meter
 Z    =       13637531
71                 Z    =         4156719
67
 XDOT =       1669
997850                 XDOT =         509
015345
 YDOT =      20716
722112  feet/sec       YDOT =        6314
456900  meter/sec
 ZDOT =      12294
308692                 ZDOT =        3747
305289


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
92677024  
00016717  00000-0  10270-3 0  9010
2 25544  51
6404 183
9602 0006315 171
4996 188
6263 15
50973135 20794


Satellite: ISS
Catalog Number: 25544
Epoch time:      19203
92677024   =   yrday
fracday
Element set:     901
Inclination:       51
6404  deg
RA of node:       183
9602  deg
Eccentricity:     
0006315     
Arg of perigee:   171
4996  deg
Mean anomaly:     188
6263  deg
Mean motion:   15
50973135  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2079
Checksum:              318


Coasting Arc #3 (Orbit 2087)
---------------------------------------

Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          73181
09                 A    =         6786501
53  meter
 Y    =       -4212507
64  meter          E    =           
0007258
 Z    =        5317479
33                 I    =           51
61273
 XDOT =       7665
853658                 Wp   =          153
48806
 YDOT =         64
853637  meter/sec      RA   =          180
12682  deg
 ZDOT =        -60
443969                 TA   =          297
05125
                                          MA   =          297
12530
                                          Ha   =            227
356  n
mi
                                          Hp   =            218
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         240095
44                 X    =           94452
07
 Y    =      -13820563
11  feet           Y    =        -4211570
65  meter
 Z    =       17445798
34                 Z    =         5317886
24
 XDOT =      25150
438511                 XDOT =        7664
852307
 YDOT =        212
774399  feet/sec       YDOT =         150
573002  meter/sec
 ZDOT =       -198
306986                 ZDOT =         -23
209003

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13379852
08                 X    =        -4078178
91
 Y    =        3459913
75  feet           Y    =         1054581
71  meter
 Z    =       17447923
82                 Z    =         5318127
18
 XDOT =      -6054
939430                 XDOT =       -1845
545538
 YDOT =     -23372
775978  feet/sec       YDOT =       -7124
022118  meter/sec
 ZDOT =        -29
125816                 ZDOT =          -8
877549


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
50665823  
00016717  00000-0  10270-3 0  9020
2 25544  51
6383 181
0835 0006539 172
4086 187
7165 15
50989319 20888


Satellite: ISS
Catalog Number: 25544
Epoch time:      19204
50665823   =   yrday
fracday
Element set:     902
Inclination:       51
6383  deg
RA of node:       181
0835  deg
Eccentricity:     
0006539     
Arg of perigee:   172
4086  deg
Mean anomaly:     187
7165  deg
Mean motion:   15
50989319  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2088
Checksum:              332


Coasting Arc #4 (Orbit 2102)
---------------------------------------

Vector Time (GMT): 2019/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -584740
79                 A    =         6786764
20  meter
 Y    =        4241803
50  meter          E    =           
0016955
 Z    =       -5279343
51                 I    =           51
64679
 XDOT =      -7606
750402                 Wp   =          118
73068
 YDOT =        -12
348496  meter/sec      RA   =          175
16002  deg
 ZDOT =        826
667975                 TA   =          159
22267
                                          MA   =          159
15366
                                          Ha   =            227
257  n
mi
                                          Hp   =            219
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1918440
90                 X    =         -606486
50
 Y    =       13916678
14  feet           Y    =         4235143
25  meter
 Z    =      -17320680
80                 Z    =        -5282236
49
 XDOT =     -24956
530189                 XDOT =       -7610
062429
 YDOT =        -40
513437  feet/sec       YDOT =         -97
431092  meter/sec
 ZDOT =       2712
165271                 ZDOT =         789
709512

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13873399
37                 X    =         4228612
13
 Y    =       -2101881
15  feet           Y    =         -640653
37  meter
 Z    =      -17334105
53                 Z    =        -5283435
37
 XDOT =       6688
848133                 XDOT =        2038
760911
 YDOT =      23007
041745  feet/sec       YDOT =        7012
546324  meter/sec
 ZDOT =       2544
217075                 ZDOT =         775
477364


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
47313881  
00016717  00000-0  10270-3 0  9032
2 25544  51
6383 176
2887 0006520 175
7692 184
3515 15
50973280 21030


Satellite: ISS
Catalog Number: 25544
Epoch time:      19205
47313881   =   yrday
fracday
Element set:     903
Inclination:       51
6383  deg
RA of node:       176
2887  deg
Eccentricity:     
0006520     
Arg of perigee:   175
7692  deg
Mean anomaly:     184
3515  deg
Mean motion:   15
50973280  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2103
Checksum:              316


Coasting Arc #5 (Orbit 2110)
---------------------------------------

Vector Time (GMT): 2019/205/22:24:29
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4421323
51                 A    =         6790748
92  meter
 Y    =       -2858876
38  meter          E    =           
0013538
 Z    =        4286562
04                 I    =           51
67549
 XDOT =       5773
481166                 Wp   =          135
19938
 YDOT =      -3563
851377  meter/sec      RA   =          172
83087  deg
 ZDOT =       3561
864522                 TA   =          278
38995
                                          MA   =          278
54339
                                          Ha   =            227
236  n
mi
                                          Hp   =            219
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14505654
55                 X    =        -4409847
71
 Y    =       -9379515
67  feet           Y    =        -2908254
84  meter
 Z    =       14063523
76                 Z    =         4265112
75
 XDOT =      18941
867342                 XDOT =        5795
602653
 YDOT =     -11692
425777  feet/sec       YDOT =       -3499
164803  meter/sec
 ZDOT =      11685
907223                 ZDOT =        3589
963209

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7370117
78                 X    =         2246411
90
 Y    =      -15709795
66  feet           Y    =        -4788345
72  meter
 Z    =       13966234
74                 Z    =         4256908
35
 XDOT =      12932
819266                 XDOT =        3941
923312
 YDOT =      16617
725784  feet/sec       YDOT =        5065
082819  meter/sec
 ZDOT =      11813
836630                 ZDOT =        3600
857405


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
98859355  
00016717  00000-0  10270-3 0  9040
2 25544  51
6377 173
7280 0006714 179
8502 180
2652 15
51012961 21119


Satellite: ISS
Catalog Number: 25544
Epoch time:      19205
98859355   =   yrday
fracday
Element set:     904
Inclination:       51
6377  deg
RA of node:       173
7280  deg
Eccentricity:     
0006714     
Arg of perigee:   179
8502  deg
Mean anomaly:     180
2652  deg
Mean motion:   15
51012961  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2111
Checksum:              313


Coasting Arc #6 (Orbit 2125)
---------------------------------------

Vector Time (GMT): 2019/206/22:24:29
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3983348
19                 A    =         6789301
12  meter
 Y    =        2914524
44  meter          E    =           
0010181
 Z    =       -4668690
34                 I    =           51
70511
 XDOT =      -6069
591805                 Wp   =          108
45194
 YDOT =       3652
229696  meter/sec      RA   =          167
87074  deg
 ZDOT =      -2906
973650                 TA   =          132
66136
                                          MA   =          132
57552
                                          Ha   =            227
163  n
mi
                                          Hp   =            219
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13068727
67                 X    =         3973138
86
 Y    =        9562088
05  feet           Y    =         2959012
33  meter
 Z    =      -15317225
51                 Z    =        -4649365
39
 XDOT =     -19913
358941                 XDOT =       -6095
860604
 YDOT =      11982
380893  feet/sec       YDOT =        3584
208617  meter/sec
 ZDOT =      -9537
315126                 ZDOT =       -2936
520786

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7492065
75                 X    =        -2283581
64
 Y    =       14448919
49  feet           Y    =         4404030
66  meter
 Z    =      -15229584
52                 Z    =        -4641977
36
 XDOT =     -13751
515178                 XDOT =       -4191
461826
 YDOT =     -17295
827725  feet/sec       YDOT =       -5271
768290  meter/sec
 ZDOT =      -9671
852102                 ZDOT =       -2947
980521


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
95507224  
00016717  00000-0  10270-3 0  9054
2 25544  51
6391 168
9327 0006650 180
6268 179
4875 15
51015556 21267


Satellite: ISS
Catalog Number: 25544
Epoch time:      19206
95507224   =   yrday
fracday
Element set:     905
Inclination:       51
6391  deg
RA of node:       168
9327  deg
Eccentricity:     
0006650     
Arg of perigee:   180
6268  deg
Mean anomaly:     179
4875  deg
Mean motion:   15
51015556  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2126
Checksum:              325


Coasting Arc #7 (Orbit 2129)
---------------------------------------

Vector Time (GMT): 2019/207/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929147
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3905746
88                 A    =         6789123
09  meter
 Y    =        2911649
59  meter          E    =           
0010180
 Z    =       -4735487
51                 I    =           51
71470
 XDOT =      -6104
982106                 Wp   =          108
58290
 YDOT =       3701
021204  meter/sec      RA   =          166
59341  deg
 ZDOT =      -2767
726672                 TA   =          134
03936
                                          MA   =          133
95546
                                          Ha   =            227
135  n
mi
                                          Hp   =            219
444

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12814130
20                 X    =         3895899
94
 Y    =        9552656
12  feet           Y    =         2955271
74  meter
 Z    =      -15536376
34                 Z    =        -4716538
63
 XDOT =     -20029
468853                 XDOT =       -6132
470254
 YDOT =      12142
458019  feet/sec       YDOT =        3632
597549  meter/sec
 ZDOT =      -9080
468085                 ZDOT =       -2797
448666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14587075
16                 X    =         4446140
51
 Y    =        6733145
19  feet           Y    =         2052262
65  meter
 Z    =      -15450441
93                 Z    =        -4709294
70
 XDOT =     -16599
449477                 XDOT =       -5059
512200
 YDOT =      14875
541076  feet/sec       YDOT =        4534
064920  meter/sec
 ZDOT =      -9215
808449                 ZDOT =       -2808
978415


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
21279851  
00016717  00000-0  10270-3 0  9067
2 25544  51
6412 167
6560 0006738 184
2593 175
8502 15
50985722 21306


Satellite: ISS
Catalog Number: 25544
Epoch time:      19207
21279851   =   yrday
fracday
Element set:     906
Inclination:       51
6412  deg
RA of node:       167
6560  deg
Eccentricity:     
0006738     
Arg of perigee:   184
2593  deg
Mean anomaly:     175
8502  deg
Mean motion:   15
50985722  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2130
Checksum:              317


Coasting Arc #8 (Orbit 2145)
---------------------------------------

Vector Time (GMT): 2019/208/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3476439
49                 A    =         6787924
94  meter
 Y    =       -2999277
27  meter          E    =           
0010863
 Z    =        4998970
65                 I    =           51
74317
 XDOT =       6307
238161                 Wp   =          156
94801
 YDOT =      -3823
028728  meter/sec      RA   =          161
63505  deg
 ZDOT =       2081
222630                 TA   =          272
75599
                                          MA   =          272
88032
                                          Ha   =            226
999  n
mi
                                          Hp   =            219
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11405641
38                 X    =        -3466924
42
 Y    =       -9840148
51  feet           Y    =        -3038100
57  meter
 Z    =       16400822
36                 Z    =         4982106
31
 XDOT =      20693
038585                 XDOT =        6339
410238
 YDOT =     -12542
745172  feet/sec       YDOT =       -3752
317095  meter/sec
 ZDOT =       6828
158234                 ZDOT =        2111
938389

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13395473
75                 X    =        -4082940
40
 Y    =       -7069702
75  feet           Y    =        -2154845
40  meter
 Z    =       16324360
26                 Z    =         4975665
01
 XDOT =      16872
391202                 XDOT =        5142
704839
 YDOT =     -15793
772064  feet/sec       YDOT =       -4813
941725  meter/sec
 ZDOT =       6968
046897                 ZDOT =        2123
860694


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
24370544  
00016717  00000-0  10270-3 0  9073
2 25544  51
6411 162
5413 0006654 187
9083 172
1964 15
51017746 21469


Satellite: ISS
Catalog Number: 25544
Epoch time:      19208
24370544   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       162
5413  deg
Eccentricity:     
0006654     
Arg of perigee:   187
9083  deg
Mean anomaly:     172
1964  deg
Mean motion:   15
51017746  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2146
Checksum:              306


Coasting Arc #9 (Orbit 2160)
---------------------------------------

Vector Time (GMT): 2019/209/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3006688
58                 A    =         6787161
49  meter
 Y    =        3168484
16  meter          E    =           
0012985
 Z    =       -5204647
46                 I    =           51
77074
 XDOT =      -6436
382741                 Wp   =          108
46449
 YDOT =       3922
131517  meter/sec      RA   =          156
67742  deg
 ZDOT =      -1337
283372                 TA   =          148
72485
                                          MA   =          148
64753
                                          Ha   =            226
898  n
mi
                                          Hp   =            219
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9864463
84                 X    =         2996315
30
 Y    =       10395289
23  feet           Y    =         3202049
69  meter
 Z    =      -17075615
01                 Z    =        -5190067
01
 XDOT =     -21116
741276                 XDOT =       -6473
267052
 YDOT =      12867
885555  feet/sec       YDOT =        3849
949295  meter/sec
 ZDOT =      -4387
412639                 ZDOT =       -1368
637772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12153257
97                 X    =         3704313
03
 Y    =        7740813
40  feet           Y    =         2359399
92  meter
 Z    =      -17009539
72                 Z    =        -5184507
71
 XDOT =     -16883
152091                 XDOT =       -5145
984757
 YDOT =      16601
082973  feet/sec       YDOT =        5060
010090  meter/sec
 ZDOT =      -4530
237080                 ZDOT =       -1380
816262


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
21018242  
00016717  00000-0  10270-3 0  9086
2 25544  51
6403 157
7464 0006668 191
1615 168
9389 15
50981359 21615


Satellite: ISS
Catalog Number: 25544
Epoch time:      19209
21018242   =   yrday
fracday
Element set:     908
Inclination:       51
6403  deg
RA of node:       157
7464  deg
Eccentricity:     
0006668     
Arg of perigee:   191
1615  deg
Mean anomaly:     168
9389  deg
Mean motion:   15
50981359  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2161
Checksum:              325


Coasting Arc #10 (Orbit 2176)
---------------------------------------

Vector Time (GMT): 2019/210/04:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2570179
80                 A    =         6786550
02  meter
 Y    =       -3359448
31  meter          E    =           
0007669
 Z    =        5306976
49                 I    =           51
80013
 XDOT =       6496
047450                 Wp   =          173
10945
 YDOT =      -4023
329501  meter/sec      RA   =          151
72136  deg
 ZDOT =        591
667265                 TA   =          271
20888
                                          MA   =          271
29674
                                          Ha   =            226
752  n
mi
                                          Hp   =            219
777

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8432348
43                 X    =        -2558200
50
 Y    =      -11021812
05  feet           Y    =        -3388123
58  meter
 Z    =       17411340
20                 Z    =         5294520
32
 XDOT =      21312
491634                 XDOT =        6537
680722
 YDOT =     -13199
899937  feet/sec       YDOT =       -3950
453429  meter/sec
 ZDOT =       1941
165567                 ZDOT =         623
322854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11059870
90                 X    =        -3371048
65
 Y    =       -8498544
72  feet           Y    =        -2590356
43  meter
 Z    =       17354930
19                 Z    =         5289782
72
 XDOT =      16645
750319                 XDOT =        5073
624697
 YDOT =     -17353
411244  feet/sec       YDOT =       -5289
319747  meter/sec
 ZDOT =       2085
393759                 ZDOT =         635
628018


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
24108698  
00016717  00000-0  10270-3 0  9097
2 25544  51
6411 152
6316 0006570 195
1857 164
9098 15
51019942 21779


Satellite: ISS
Catalog Number: 25544
Epoch time:      19210
24108698   =   yrday
fracday
Element set:     909
Inclination:       51
6411  deg
RA of node:       152
6316  deg
Eccentricity:     
0006570     
Arg of perigee:   195
1857  deg
Mean anomaly:     164
9098  deg
Mean motion:   15
51019942  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2177
Checksum:              320


Coasting Arc #11 (Orbit 2180)
---------------------------------------

Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3606766
29                 A    =         6787330
49  meter
 Y    =       -2595422
71  meter          E    =           
0009297
 Z    =        5130758
65                 I    =           51
80927
 XDOT =       5776
724776                 Wp   =          165
37283
 YDOT =      -4759
413544  meter/sec      RA   =          150
46405  deg
 ZDOT =       1643
862551                 TA   =          268
73505
                                          MA   =          268
84156
                                          Ha   =            226
622  n
mi
                                          Hp   =            219
855

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11833222
75                 X    =        -3602397
52
 Y    =       -8515166
36  feet           Y    =        -2635732
35  meter
 Z    =       16833197
66                 Z    =         5113248
82
 XDOT =      18952
509109                 XDOT =        5821
531703
 YDOT =     -15614
873832  feet/sec       YDOT =       -4694
563838  meter/sec
 ZDOT =       5393
249840                 ZDOT =        1672
031554

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4640688
20                 X    =        -1414481
76
 Y    =       13916378
84  feet           Y    =         4241712
27  meter
 Z    =       16753751
09                 Z    =         5106543
33
 XDOT =     -19456
246326                 XDOT =       -5930
263880
 YDOT =     -13172
939087  feet/sec       YDOT =       -4015
111834  meter/sec
 ZDOT =       5521
680756                 ZDOT =        1683
008295


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
49881366  
00016717  00000-0  10270-3 0  9106
2 25544  51
6401 151
3537 0006303 196
8202 163
2741 15
51030120 21818


Satellite: ISS
Catalog Number: 25544
Epoch time:      19210
49881366   =   yrday
fracday
Element set:     910
Inclination:       51
6401  deg
RA of node:       151
3537  deg
Eccentricity:     
0006303     
Arg of perigee:   196
8202  deg
Mean anomaly:     163
2741  deg
Mean motion:   15
51030120  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2181
Checksum:              268


Coasting Arc #12 (Orbit 2195)
---------------------------------------

Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3171554
70                 A    =         6786758
20  meter
 Y    =        2860034
20  meter          E    =           
0012889
 Z    =       -5284621
83                 I    =           51
83572
 XDOT =      -5847
214454                 Wp   =          108
71599
 YDOT =       4860
600008  meter/sec      RA   =          145
50936  deg
 ZDOT =       -884
431440                 TA   =          152
86754
                                          MA   =          152
80013
                                          Ha   =            226
480  n
mi
                                          Hp   =            220
118

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10405363
19                 X    =         3165006
55
 Y    =        9383314
29  feet           Y    =         2895464
82  meter
 Z    =      -17337998
14                 Z    =        -5269231
42
 XDOT =     -19183
774457                 XDOT =       -5896
836508
 YDOT =      15946
850419  feet/sec       YDOT =        4794
935010  meter/sec
 ZDOT =      -2901
677952                 ZDOT =        -912
954398

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5666819
56                 X    =         1727246
60
 Y    =      -12908168
96  feet           Y    =        -3934409
90  meter
 Z    =      -17268198
51                 Z    =        -5263346
91
 XDOT =      20151
727350                 XDOT =        6142
246496
 YDOT =      12877
087473  feet/sec       YDOT =        3924
936262  meter/sec
 ZDOT =      -3031
750765                 ZDOT =        -924
077633


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
46528643  
00016717  00000-0  10270-3 0  9111
2 25544  51
6402 146
5576 0006185 199
5356 160
5558 15
51000768 21963


Satellite: ISS
Catalog Number: 25544
Epoch time:      19211
46528643   =   yrday
fracday
Element set:     911
Inclination:       51
6402  deg
RA of node:       146
5576  deg
Eccentricity:     
0006185     
Arg of perigee:   199
5356  deg
Mean anomaly:     160
5558  deg
Mean motion:   15
51000768  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2196
Checksum:              318


Coasting Arc #13 (Orbit 2211)
---------------------------------------

Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2776723
67                 A    =         6786424
92  meter
 Y    =       -3141452
94  meter          E    =           
0005976
 Z    =        5336549
77                 I    =           51
86215
 XDOT =       5853
079963                 Wp   =          180
98756
 YDOT =      -4945
426688  meter/sec      RA   =          140
55879  deg
 ZDOT =        128
454616                 TA   =          267
75712
                                          MA   =          267
82555
                                          Ha   =            226
371  n
mi
                                          Hp   =            220
168

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9109985
80                 X    =        -2767310
06
 Y    =      -10306604
14  feet           Y    =        -3172452
19  meter
 Z    =       17508365
40                 Z    =         5323084
31
 XDOT =      19203
018250                 XDOT =        5907
322189
 YDOT =     -16225
153177  feet/sec       YDOT =       -4879
670165  meter/sec
 ZDOT =        421
439030                 ZDOT =         157
017206

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6738380
09                 X    =        -2053858
25
 Y    =       12080795
10  feet           Y    =         3682226
35  meter
 Z    =       17447332
54                 Z    =         5317946
96
 XDOT =     -20712
537030                 XDOT =       -6313
181287
 YDOT =     -12377
438090  feet/sec       YDOT =       -3772
643130  meter/sec
 ZDOT =        551
721133                 ZDOT =         168
164601


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
49618940  
00016717  00000-0  10270-3 0  9126
2 25544  51
6406 141
4442 0006160 204
0657 156
0207 15
51019631 22121


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
49618940   =   yrday
fracday
Element set:     912
Inclination:       51
6406  deg
RA of node:       141
4442  deg
Eccentricity:     
0006160     
Arg of perigee:   204
0657  deg
Mean anomaly:     156
0207  deg
Mean motion:   15
51019631  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2212
Checksum:              271


Coasting Arc #14 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1825060
65                 A    =         6792453
90  meter
 Y    =       -5381294
10  meter          E    =           
0010013
 Z    =        3709629
83                 I    =           51
89019
 XDOT =       6262
568859                 Wp   =          116
20281
 YDOT =       -869
693277  meter/sec      RA   =          139
53593  deg
 ZDOT =      -4337
904848                 TA   =           19
78935
                                          MA   =           19
75054
                                          Ha   =            226
167  n
mi
                                          Hp   =            220
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5987731
80                 X    =         1867081
30
 Y    =      -17655164
37  feet           Y    =        -5360650
44  meter
 Z    =       12170701
53                 Z    =         3718596
55
 XDOT =      20546
485757                 XDOT =        6292
899198
 YDOT =      -2853
324398  feet/sec       YDOT =        -799
490772  meter/sec
 ZDOT =     -14231
971287                 ZDOT =       -4307
410796

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5338731
70                 X    =        -1627245
42
 Y    =       17834007
51  feet           Y    =         5435805
49  meter
 Z    =       12211873
60                 Z    =         3722179
07
 XDOT =     -19239
615610                 XDOT =       -5864
234838
 YDOT =       3901
464703  feet/sec       YDOT =        1189
166441  meter/sec
 ZDOT =     -14093
186654                 ZDOT =       -4295
603292


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
68948257  
00016717  00000-0  10270-3 0  9135
2 25544  51
6430 140
4865 0006090 205
4656 154
6196 15
51042772 22158


Satellite: ISS
Catalog Number: 25544
Epoch time:      19212
68948257   =   yrday
fracday
Element set:     913
Inclination:       51
6430  deg
RA of node:       140
4865  deg
Eccentricity:     
0006090     
Arg of perigee:   205
4656  deg
Mean anomaly:     154
6196  deg
Mean motion:   15
51042772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              307


Coasting Arc #15 (Orbit 2227)
---------------------------------------

Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         426683
14                 A    =         6790428
18  meter
 Y    =       -5199204
56  meter          E    =           
0006704
 Z    =        4340059
73                 I    =           51
90281
 XDOT =       6371
962471                 Wp   =          111
77709
 YDOT =      -2412
682882  meter/sec      RA   =          135
40473  deg
 ZDOT =      -3514
810793                 TA   =           13
86315
                                          MA   =           13
84476
                                          Ha   =            226
187  n
mi
                                          Hp   =            220
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1399879
05                 X    =          463709
39
 Y    =      -17057757
75  feet           Y    =        -5194226
44  meter
 Z    =       14239041
12                 Z    =         4342221
82
 XDOT =      20905
388684                 XDOT =        6415
540753
 YDOT =      -7915
626252  feet/sec       YDOT =       -2341
183154  meter/sec
 ZDOT =     -11531
531473                 ZDOT =       -3483
753380

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14938928
05                 X    =        -4553385
27
 Y    =        8334532
75  feet           Y    =         2540365
58  meter
 Z    =       14249247
19                 Z    =         4343170
54
 XDOT =     -17581
319270                 XDOT =       -5358
786113
 YDOT =     -12029
038318  feet/sec       YDOT =       -3666
450879  meter/sec
 ZDOT =     -11390
057853                 ZDOT =       -3471
689633


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
52709176  
00016717  00000-0  10270-3 0  9145
2 25544  51
6419 136
3301 0006196 208
1115 151
9703 15
51010640 22288


Satellite: ISS
Catalog Number: 25544
Epoch time:      19213
52709176   =   yrday
fracday
Element set:     914
Inclination:       51
6419  deg
RA of node:       136
3301  deg
Eccentricity:     
0006196     
Arg of perigee:   208
1115  deg
Mean anomaly:     151
9703  deg
Mean motion:   15
51010640  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2228
Checksum:              277


Coasting Arc #16 (Orbit 2242)
---------------------------------------

Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -673693
97                 A    =         6791906
37  meter
 Y    =        5514945
77  meter          E    =           
0007651
 Z    =       -3914863
71                 I    =           51
93129
 XDOT =      -6083
162424                 Wp   =          156
65787
 YDOT =       2175
307379  meter/sec      RA   =          130
46048  deg
 ZDOT =       4107
139584                 TA   =          156
31826
                                          MA   =          156
28303
                                          Ha   =            225
995  n
mi
                                          Hp   =            220
501

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2210282
07                 X    =         -716297
90
 Y    =       18093654
10  feet           Y    =         5507174
06  meter
 Z    =      -12844041
05                 Z    =        -3918239
34
 XDOT =     -19957
881969                 XDOT =       -6126
984890
 YDOT =       7136
835232  feet/sec       YDOT =        2107
035922  meter/sec
 ZDOT =      13474
867402                 ZDOT =        4077
484349

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16111485
77                 X    =         4910780
86
 Y    =       -8501810
01  feet           Y    =        -2591351
69  meter
 Z    =      -12859794
29                 Z    =        -3919665
30
 XDOT =      16621
025647                 XDOT =        5066
088617
 YDOT =      11299
998976  feet/sec       YDOT =        3444
239688  meter/sec
 ZDOT =      13339
773822                 ZDOT =        4065
963061


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
49355972  
00016717  00000-0  10270-3 0  9154
2 25544  51
6424 131
5345 0006110 211
6371 148
4413 15
51018442 22432


Satellite: ISS
Catalog Number: 25544
Epoch time:      19214
49355972   =   yrday
fracday
Element set:     915
Inclination:       51
6424  deg
RA of node:       131
5345  deg
Eccentricity:     
0006110     
Arg of perigee:   211
6371  deg
Mean anomaly:     148
4413  deg
Mean motion:   15
51018442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2243
Checksum:              280


Coasting Arc #17 (Orbit 2258)
---------------------------------------

Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         860257
91                 A    =         6793456
84  meter
 Y    =       -5802629
46  meter          E    =           
0010171
 Z    =        3413633
84                 I    =           51
95697
 XDOT =       5804
506789                 Wp   =          119
30197
 YDOT =      -1875
367361  meter/sec      RA   =          125
52083  deg
 ZDOT =      -4645
044263                 TA   =           21
00695
                                          MA   =           20
96521
                                          Ha   =            225
895  n
mi
                                          Hp   =            220
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2822368
47                 X    =          908499
51
 Y    =      -19037498
24  feet           Y    =        -5792739
82  meter
 Z    =       11199586
07                 Z    =         3417929
54
 XDOT =      19043
657444                 XDOT =        5847
608778
 YDOT =      -6152
780056  feet/sec       YDOT =       -1810
216151  meter/sec
 ZDOT =     -15239
646532                 ZDOT =       -4616
744207

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17093204
91                 X    =        -5210008
86
 Y    =        8818551
07  feet           Y    =         2687894
37  meter
 Z    =       11219551
42                 Z    =         3419719
27
 XDOT =     -15484
933335                 XDOT =       -4719
807680
 YDOT =     -10766
794045  feet/sec       YDOT =       -3281
718825  meter/sec
 ZDOT =     -15110
728081                 ZDOT =       -4605
749919


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
52445773  
00016717  00000-0  10270-3 0  9169
2 25544  51
6422 126
4206 0006061 215
2934 144
7816 15
51012817 22592


Satellite: ISS
Catalog Number: 25544
Epoch time:      19215
52445773   =   yrday
fracday
Element set:     916
Inclination:       51
6422  deg
RA of node:       126
4206  deg
Eccentricity:     
0006061     
Arg of perigee:   215
2934  deg
Mean anomaly:     144
7816  deg
Mean motion:   15
51012817  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2259
Checksum:              295


Coasting Arc #18 (Orbit 2273)
---------------------------------------

Vector Time (GMT): 2019/216/11:38:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -989487
53                 A    =         6794863
32  meter
 Y    =        6081681
42  meter          E    =           
0002669
 Z    =       -2868131
28                 I    =           51
98043
 XDOT =      -5515
676871                 Wp   =          174
71432
 YDOT =       1505
764952  meter/sec      RA   =          120
58276  deg
 ZDOT =       5093
541341                 TA   =          152
89619
                                          MA   =          152
88225
                                          Ha   =            225
704  n
mi
                                          Hp   =            220
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3246350
17                 X    =        -1043489
59
 Y    =       19953023
04  feet           Y    =         6070314
37  meter
 Z    =       -9409879
52                 Z    =        -2873068
82
 XDOT =     -18096
052728                 XDOT =       -5556
845931
 YDOT =       4940
173727  feet/sec       YDOT =        1443
854523  meter/sec
 ZDOT =      16711
093639                 ZDOT =        5066
648819

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17934429
98                 X    =         5466414
26
 Y    =       -9305180
30  feet           Y    =        -2836218
95  meter
 Z    =       -9432793
42                 Z    =        -2875115
43
 XDOT =      14121
272616                 XDOT =        4304
163893
 YDOT =      10393
352684  feet/sec       YDOT =        3167
893898  meter/sec
 ZDOT =      16588
596941                 ZDOT =        5056
204348


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   19216
49092339  
00016717  00000-0  10270-3 0  9173
2 25544  51
6423 121
6251 0006121 219
2887 140
7820 15
51029037 22748


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
49092339   =   yrday
fracday
Element set:     917
Inclination:       51
6423  deg
RA of node:       121
6251  deg
Eccentricity:     
0006121     
Arg of perigee:   219
2887  deg
Mean anomaly:     140
7820  deg
Mean motion:   15
51029037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2274
Checksum:              295


Coasting Arc #19 (Orbit 2278)
---------------------------------------

Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3790893
45                 A    =         6798169
62  meter
 Y    =        5592698
47  meter          E    =           
0007161
 Z    =         728012
44                 I    =           51
99216
 XDOT =      -3563
015256                 Wp   =           64
93721
 YDOT =      -3199
029454  meter/sec      RA   =          119
30006  deg
 ZDOT =       5979
155841                 TA   =          302
87726
                                          MA   =          302
94616
                                          Ha   =            225
786  n
mi
                                          Hp   =            220
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12437314
46                 X    =        -3856687
08
 Y    =       18348748
25  feet           Y    =         5549938
15  meter
 Z    =        2388492
25                 Z    =          709438
30
 XDOT =     -11689
682598                 XDOT =       -3556
020850
 YDOT =     -10495
503458  feet/sec       YDOT =       -3238
834546  meter/sec
 ZDOT =      19616
653022                 ZDOT =        5961
865332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3070205
00                 X    =         -935798
48
 Y    =      -21962143
38  feet           Y    =        -6694061
30  meter
 Z    =        2303551
09                 Z    =          702122
37
 XDOT =      14205
301981                 XDOT =        4329
776044
 YDOT =         78
813605  feet/sec       YDOT =          24
022387  meter/sec
 ZDOT =      19538
197529                 ZDOT =        5955
242607


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   19216
81307733  
00016717  00000-0  10270-3 0  9187
2 25544  51
6387 120
0227 0006378 219
0991 140
9700 15
51020273 22798


Satellite: ISS
Catalog Number: 25544
Epoch time:      19216
81307733   =   yrday
fracday
Element set:     918
Inclination:       51
6387  deg
RA of node:       120
0227  deg
Eccentricity:     
0006378     
Arg of perigee:   219
0991  deg
Mean anomaly:     140
9700  deg
Mean motion:   15
51020273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2279
Checksum:              299


Coasting Arc #20 (Orbit 2293)
---------------------------------------

Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949153
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3705752
48                 A    =         6797452
82  meter
 Y    =       -5512427
87  meter          E    =           
0011316
 Z    =       -1409927
95                 I    =           52
00655
 XDOT =       3314
923979                 Wp   =          174
92693
 YDOT =       3715
511026  meter/sec      RA   =          114
36731  deg
 ZDOT =      -5828
425315                 TA   =           20
34947
                                          MA   =           20
30442
                                          Ha   =            225
567  n
mi
                                          Hp   =            220
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12157980
57                 X    =         3773967
17
 Y    =      -18085393
28  feet           Y    =        -5470606
12  meter
 Z    =       -4625747
85                 Z    =        -1391761
41
 XDOT =      10875
734840                 XDOT =        3301
440548
 YDOT =      12189
996805  feet/sec       YDOT =        3752
505496  meter/sec
 ZDOT =     -19122
130297                 ZDOT =       -5812
355601

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3460590
57                 X    =         1054788
01
 Y    =       21533325
21  feet           Y    =         6563357
52  meter
 Z    =       -4542653
78                 Z    =        -1384600
87
 XDOT =     -14793
079670                 XDOT =       -4508
930683
 YDOT =      -1631
016555  feet/sec       YDOT =        -497
133846  meter/sec
 ZDOT =     -19049
270695                 ZDOT =       -5806
217708


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   19217
77953971  
00016717  00000-0  10270-3 0  9195
2 25544  51
6398 115
2271 0006135 223
6891 136
3775 15
51060440 22944


Satellite: ISS
Catalog Number: 25544
Epoch time:      19217
77953971   =   yrday
fracday
Element set:     919
Inclination:       51
6398  deg
RA of node:       115
2271  deg
Eccentricity:     
0006135     
Arg of perigee:   223
6891  deg
Mean anomaly:     136
3775  deg
Mean motion:   15
51060440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2294
Checksum:              323
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