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

 
Date: November 22nd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


329/11:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 227 5
000/00:00:00 000 0 0 0 0 222 2

333/10:24:30 000 0 0 0 0 0 0
N/A 0 0 0 0 227 8
000/00:00:00 000 0 0 0 0 221 6

335/11:30:08 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 221 1

336/14:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 221 0

337/13:40:13 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 220 8

338/17:51:47 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 220 6

339/18:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 220 5

341/11:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 220 3

Coasting Arc #1 (Orbit 3980)
---------------------------------------

Vector Time (GMT): 2019/326/11:23:54
315
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4413968
23                 A    =         6789998
56  meter
 Y    =         352483
30  meter          E    =           
0002280
 Z    =        5148250
55                 I    =           51
27445
 XDOT =      -2217
614075                 Wp   =          324
67917
 YDOT =       7196
259180  meter/sec      RA   =          295
76758  deg
 ZDOT =       1410
759016                 TA   =          111
68034
                                          MA   =          111
65606
                                          Ha   =            226
931  n
mi
                                          Hp   =            222
849

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14481523
08                 X    =         4384690
86
 Y    =        1156441
27  feet           Y    =          401679
62  meter
 Z    =       16890585
80                 Z    =         5169621
20
 XDOT =      -7275
636728                 XDOT =       -2304
772717
 YDOT =      23609
774213  feet/sec       YDOT =        7170
972892  meter/sec
 ZDOT =       4628
474461                 ZDOT =        1399
774940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9896358
18                 X    =        -3016409
97
 Y    =       10479287
47  feet           Y    =         3194086
82  meter
 Z    =       16987948
22                 Z    =         5177926
62
 XDOT =     -13073
634412                 XDOT =       -3984
843769
 YDOT =     -19756
100036  feet/sec       YDOT =       -6021
659291  meter/sec
 ZDOT =       4577
783196                 ZDOT =        1395
308318


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   19326
52570918  
00016717  00000-0  10270-3 0  9005
2 25544  51
6396 296
2635 0006647 311
7905  48
2677 15
50014018 39814


Satellite: ISS
Catalog Number: 25544
Epoch time:      19326
52570918   =   yrday
fracday
Element set:     900
Inclination:       51
6396  deg
RA of node:       296
2635  deg
Eccentricity:     
0006647     
Arg of perigee:   311
7905  deg
Mean anomaly:      48
2677  deg
Mean motion:   15
50014018  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3981
Checksum:              323


Coasting Arc #2 (Orbit 3995)
---------------------------------------

Vector Time (GMT): 2019/327/11:23:54
315
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4331720
32                 A    =         6789678
48  meter
 Y    =        -395422
00  meter          E    =           
0011698
 Z    =       -5222740
50                 I    =           51
26051
 XDOT =       1909
042012                 Wp   =           54
69126
 YDOT =      -7341
181100  meter/sec      RA   =          290
78540  deg
 ZDOT =      -1022
532738                 TA   =          205
41790
                                          MA   =          205
47548
                                          Ha   =            227
174  n
mi
                                          Hp   =            222
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14211680
85                 X    =        -4301606
96
 Y    =       -1297316
26  feet           Y    =         -443693
84  meter
 Z    =      -17134975
38                 Z    =        -5243709
67
 XDOT =       6263
261194                 XDOT =        1995
958350
 YDOT =     -24085
239828  feet/sec       YDOT =       -7319
346837  meter/sec
 ZDOT =      -3354
766201                 ZDOT =       -1013
048218

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9659724
21                 X    =         2944283
94
 Y    =      -10347066
69  feet           Y    =        -3153785
93  meter
 Z    =      -17230502
68                 Z    =        -5251857
22
 XDOT =      14434
581264                 XDOT =        4399
660369
 YDOT =      19016
421963  feet/sec       YDOT =        5796
205414  meter/sec
 ZDOT =      -3310
910521                 ZDOT =       -1009
165527


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   19327
49279371  
00016717  00000-0  10270-3 0  9012
2 25544  51
6402 291
4720 0006650 316
1950  43
8672 15
50022040 39963


Satellite: ISS
Catalog Number: 25544
Epoch time:      19327
49279371   =   yrday
fracday
Element set:     901
Inclination:       51
6402  deg
RA of node:       291
4720  deg
Eccentricity:     
0006650     
Arg of perigee:   316
1950  deg
Mean anomaly:      43
8672  deg
Mean motion:   15
50022040  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3996
Checksum:              299


Coasting Arc #3 (Orbit 4011)
---------------------------------------

Vector Time (GMT): 2019/328/11:23:54
315
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4259301
53                 A    =         6789455
28  meter
 Y    =         474280
03  meter          E    =           
0004321
 Z    =        5267069
20                 I    =           51
24860
 XDOT =      -1595
023673                 Wp   =          336
63979
 YDOT =       7467
480341  meter/sec      RA   =          285
80256  deg
 ZDOT =        621
495587                 TA   =          107
41308
                                          MA   =          107
36583
                                          Ha   =            227
284  n
mi
                                          Hp   =            222
472

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13974086
40                 X    =         4228096
33
 Y    =        1556036
85  feet           Y    =          521735
84  meter
 Z    =       17280410
76                 Z    =         5287684
01
 XDOT =      -5233
017300                 XDOT =       -1681
427618
 YDOT =      24499
607418  feet/sec       YDOT =        7449
160517  meter/sec
 ZDOT =       2039
027517                 ZDOT =         613
537839

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9544671
83                 X    =        -2909215
97
 Y    =       10165692
88  feet           Y    =         3098503
19  meter
 Z    =       17374316
26                 Z    =         5295691
60
 XDOT =     -15738
804438                 XDOT =       -4797
187593
 YDOT =     -18176
476686  feet/sec       YDOT =       -5540
190094  meter/sec
 ZDOT =       2002
130322                 ZDOT =         610
249322


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   19328
52434982  
00016717  00000-0  10270-3 0  9029
2 25544  51
6398 286
3614 0006765 320
0685  39
9967 15
50021681 40121


Satellite: ISS
Catalog Number: 25544
Epoch time:      19328
52434982   =   yrday
fracday
Element set:     902
Inclination:       51
6398  deg
RA of node:       286
3614  deg
Eccentricity:     
0006765     
Arg of perigee:   320
0685  deg
Mean anomaly:      39
9967  deg
Mean motion:   15
50021681  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4012
Checksum:              324


Coasting Arc #4 (Orbit 4026)
---------------------------------------

Vector Time (GMT): 2019/329/11:23:54
315
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4225605
51                 A    =         6789346
47  meter
 Y    =        -540623
29  meter          E    =           
0012242
 Z    =       -5296055
64                 I    =           51
24052
 XDOT =       1256
660225                 Wp   =           61
24638
 YDOT =      -7546
562690  meter/sec      RA   =          280
81877  deg
 ZDOT =       -226
925796                 TA   =          206
54323
                                          MA   =          206
60597
                                          Ha   =            227
465  n
mi
                                          Hp   =            222
149

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13863535
14                 X    =        -4193520
11
 Y    =       -1773698
45  feet           Y    =         -587697
23  meter
 Z    =      -17375510
61                 Z    =        -5316504
66
 XDOT =       4122
901000                 XDOT =        1342
056994
 YDOT =     -24759
063944  feet/sec       YDOT =       -7532
032329  meter/sec
 ZDOT =       -744
507205                 ZDOT =        -220
614357

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9479903
10                 X    =         2889474
46
 Y    =      -10110857
47  feet           Y    =        -3081789
36  meter
 Z    =      -17468657
08                 Z    =        -5324446
68
 XDOT =      16929
818449                 XDOT =        5160
208663
 YDOT =      17139
181462  feet/sec       YDOT =        5224
022510  meter/sec
 ZDOT =       -715
115405                 ZDOT =        -217
967175


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   19329
49143210  
00016717  00000-0  10270-3 0  9038
2 25544  51
6401 281
5700 0006782 323
2306  36
8379 15
50024988 40275


Satellite: ISS
Catalog Number: 25544
Epoch time:      19329
49143210   =   yrday
fracday
Element set:     903
Inclination:       51
6401  deg
RA of node:       281
5700  deg
Eccentricity:     
0006782     
Arg of perigee:   323
2306  deg
Mean anomaly:      36
8379  deg
Mean motion:   15
50024988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4027
Checksum:              297


Coasting Arc #5 (Orbit 4026)
---------------------------------------

Vector Time (GMT): 2019/329/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3426209
01                 A    =         6790957
68  meter
 Y    =       -3177933
87  meter          E    =           
0008007
 Z    =       -4933407
95                 I    =           51
24575
 XDOT =       3053
878815                 Wp   =           75
19520
 YDOT =      -6673
067974  meter/sec      RA   =          280
77860  deg
 ZDOT =       2182
664237                 TA   =          216
21977
                                          MA   =          216
27401
                                          Ha   =            227
458  n
mi
                                          Hp   =            222
231

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11240843
22                 X    =        -3366453
44
 Y    =      -10426292
21  feet           Y    =        -3215913
70  meter
 Z    =      -16185721
62                 Z    =        -4949906
68
 XDOT =      10019
287452                 XDOT =        3117
669599
 YDOT =     -21893
267632  feet/sec       YDOT =       -6638
560817  meter/sec
 ZDOT =       7160
971905                 ZDOT =        2197
653688

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14885006
44                 X    =         4536949
96
 Y    =       -3327114
51  feet           Y    =        -1014104
50  meter
 Z    =      -16260645
81                 Z    =        -4956244
84
 XDOT =      12234
852819                 XDOT =        3729
183139
 YDOT =      19482
090770  feet/sec       YDOT =        5938
141267  meter/sec
 ZDOT =       7229
838768                 ZDOT =        2203
654856


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   19329
49143210  
00016717  00000-0  10270-3 0  9049
2 25544  51
6400 281
5702 0006820 323
1028  36
9653 15
50015509 40274


Satellite: ISS
Catalog Number: 25544
Epoch time:      19329
49143210   =   yrday
fracday
Element set:     904
Inclination:       51
6400  deg
RA of node:       281
5702  deg
Eccentricity:     
0006820     
Arg of perigee:   323
1028  deg
Mean anomaly:      36
9653  deg
Mean motion:   15
50015509  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4027
Checksum:              277


Coasting Arc #6 (Orbit 4042)
---------------------------------------

Vector Time (GMT): 2019/330/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3525582
28                 A    =         6791487
78  meter
 Y    =        3290738
67  meter          E    =           
0009671
 Z    =        4783332
99                 I    =           51
24401
 XDOT =      -2743
986810                 Wp   =           15
92842
 YDOT =       6677
225158  meter/sec      RA   =          275
79548  deg
 ZDOT =      -2560
812734                 TA   =           99
51214
                                          MA   =           99
40283
                                          Ha   =            227
598  n
mi
                                          Hp   =            222
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11566871
01                 X    =         3465286
94
 Y    =       10796386
73  feet           Y    =         3329826
64  meter
 Z    =       15693349
70                 Z    =         4800313
21
 XDOT =      -9002
581397                 XDOT =       -2806
010249
 YDOT =      21906
906685  feet/sec       YDOT =        6646
193406  meter/sec
 ZDOT =      -8401
616583                 ZDOT =       -2574
292325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15315675
70                 X    =        -4668217
95
 Y    =        3654882
75  feet           Y    =         1114008
26  meter
 Z    =       15770466
26                 Z    =         4806838
12
 XDOT =     -13136
789911                 XDOT =       -4004
093565
 YDOT =     -18383
549337  feet/sec       YDOT =       -5603
305838  meter/sec
 ZDOT =      -8463
596620                 ZDOT =       -2579
704250


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   19330
52298401  
00016717  00000-0  10270-3 0  9059
2 25544  51
6414 276
4596 0006874 326
7356  33
3362 15
50042505 40437


Satellite: ISS
Catalog Number: 25544
Epoch time:      19330
52298401   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:       276
4596  deg
Eccentricity:     
0006874     
Arg of perigee:   326
7356  deg
Mean anomaly:      33
3362  deg
Mean motion:   15
50042505  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4043
Checksum:              300


Coasting Arc #7 (Orbit 4057)
---------------------------------------

Vector Time (GMT): 2019/331/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3667649
66                 A    =         6792146
30  meter
 Y    =       -3362391
00  meter          E    =           
0006896
 Z    =       -4627752
07                 I    =           51
24394
 XDOT =       2431
846477                 Wp   =           68
31673
 YDOT =      -6651
580247  meter/sec      RA   =          270
81264  deg
 ZDOT =       2911
539653                 TA   =          230
83478
                                          MA   =          230
89607
                                          Ha   =            227
748  n
mi
                                          Hp   =            221
862

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12032971
31                 X    =        -3607298
34
 Y    =      -11031466
55  feet           Y    =        -3403067
27  meter
 Z    =      -15182913
61                 Z    =        -4645422
30
 XDOT =       7978
498940                 XDOT =        2491
902721
 YDOT =     -21822
769839  feet/sec       YDOT =       -6624
050164  meter/sec
 ZDOT =       9552
295450                 ZDOT =        2923
497986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15700112
71                 X    =         4785394
35
 Y    =       -4189073
92  feet           Y    =        -1276829
73  meter
 Z    =      -15263179
19                 Z    =        -4652217
02
 XDOT =      13911
459656                 XDOT =        4240
212903
 YDOT =      17204
899901  feet/sec       YDOT =        5244
053490  meter/sec
 ZDOT =       9607
333785                 ZDOT =        2928
315338


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   19331
49006124  
00016717  00000-0  10270-3 0  9066
2 25544  51
6415 271
6685 0006946 330
7828  29
2934 15
50028882 40580


Satellite: ISS
Catalog Number: 25544
Epoch time:      19331
49006124   =   yrday
fracday
Element set:     906
Inclination:       51
6415  deg
RA of node:       271
6685  deg
Eccentricity:     
0006946     
Arg of perigee:   330
7828  deg
Mean anomaly:      29
2934  deg
Mean motion:   15
50028882  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4058
Checksum:              320


Coasting Arc #8 (Orbit 4073)
---------------------------------------

Vector Time (GMT): 2019/332/11:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3818237
06                 A    =         6792835
33  meter
 Y    =        3454101
67  meter          E    =           
0011068
 Z    =        4431451
67                 I    =           51
24698
 XDOT =      -2149
907887                 Wp   =           30
41317
 YDOT =       6585
753268  meter/sec      RA   =          265
83060  deg
 ZDOT =      -3267
886289                 TA   =           92
81569
                                          MA   =           92
68901
                                          Ha   =            227
910  n
mi
                                          Hp   =            221
697

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12527024
49                 X    =         3757802
66
 Y    =       11332354
56  feet           Y    =         3496461
41  meter
 Z    =       14538883
44                 Z    =         4449853
18
 XDOT =      -7053
503567                 XDOT =       -2207
518098
 YDOT =      21606
802059  feet/sec       YDOT =        6561
389780  meter/sec
 ZDOT =     -10721
411709                 ZDOT =       -3278
468976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16141781
49                 X    =        -4920015
00
 Y    =        4727946
47  feet           Y    =         1441078
09  meter
 Z    =       14622487
69                 Z    =         4456934
25
 XDOT =     -14485
968277                 XDOT =       -4415
323131
 YDOT =     -16016
155814  feet/sec       YDOT =       -4881
724292  meter/sec
 ZDOT =     -10770
166868                 ZDOT =       -3282
746861


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   19332
52160860  
00016717  00000-0  10270-3 0  9070
2 25544  51
6414 266
5585 0006972 334
8757  25
2053 15
50049792 40745


Satellite: ISS
Catalog Number: 25544
Epoch time:      19332
52160860   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       266
5585  deg
Eccentricity:     
0006972     
Arg of perigee:   334
8757  deg
Mean anomaly:      25
2053  deg
Mean motion:   15
50049792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4074
Checksum:              319


Coasting Arc #9 (Orbit 4088)
---------------------------------------

Vector Time (GMT): 2019/333/10:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2724502
94                 A    =         6793498
23  meter
 Y    =       -4556615
79  meter          E    =           
0007751
 Z    =        4230314
85                 I    =           51
25241
 XDOT =       3794
965412                 Wp   =           63
20661
 YDOT =       5607
454872  meter/sec      RA   =          261
12472  deg
 ZDOT =       3594
178825                 TA   =          349
83143
                                          MA   =          349
84710
                                          Ha   =            227
843  n
mi
                                          Hp   =            221
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8938657
95                 X    =         2754705
13
 Y    =      -14949526
86  feet           Y    =        -4525980
15  meter
 Z    =       13878985
72                 Z    =         4243622
36
 XDOT =      12450
673925                 XDOT =        3714
520467
 YDOT =      18397
161653  feet/sec       YDOT =        5649
442592  meter/sec
 ZDOT =      11791
925280                 ZDOT =        3612
418878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3800987
83                 X    =         1158541
09
 Y    =       16948249
77  feet           Y    =         5165826
53  meter
 Z    =       13939997
31                 Z    =         4248911
18
 XDOT =     -20380
689477                 XDOT =       -6212
034153
 YDOT =      -5200
673924  feet/sec       YDOT =       -1585
165412  meter/sec
 ZDOT =      11874
642823                 ZDOT =        3619
391132


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   19333
48868147  
00016717  00000-0  10270-3 0  9080
2 25544  51
6410 261
7678 0006847 337
0390  23
0453 15
50078794 40890


Satellite: ISS
Catalog Number: 25544
Epoch time:      19333
48868147   =   yrday
fracday
Element set:     908
Inclination:       51
6410  deg
RA of node:       261
7678  deg
Eccentricity:     
0006847     
Arg of perigee:   337
0390  deg
Mean anomaly:      23
0453  deg
Mean motion:   15
50078794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4089
Checksum:              334


Coasting Arc #10 (Orbit 4103)
---------------------------------------

Vector Time (GMT): 2019/334/10:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2572850
05                 A    =         6792799
01  meter
 Y    =        4458132
02  meter          E    =           
0011830
 Z    =       -4443843
36                 I    =           51
25660
 XDOT =      -4072
287417                 Wp   =           33
38131
 YDOT =      -5600
897140  meter/sec      RA   =          256
14257  deg
 ZDOT =      -3255
638949                 TA   =          203
53298
                                          MA   =          203
58715
                                          Ha   =            228
182  n
mi
                                          Hp   =            221
284

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8441109
08                 X    =        -2600925
11
 Y    =       14626417
39  feet           Y    =         4429204
16  meter
 Z    =      -14579538
59                 Z    =        -4456409
03
 XDOT =     -13360
523023                 XDOT =       -3993
539713
 YDOT =     -18375
646785  feet/sec       YDOT =       -5645
995631  meter/sec
 ZDOT =     -10681
230148                 ZDOT =       -3275
230137

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4226373
02                 X    =        -1288198
50
 Y    =      -16298429
52  feet           Y    =        -4967761
32  meter
 Z    =      -14637155
47                 Z    =        -4461404
99
 XDOT =      21151
731068                 XDOT =        6447
047629
 YDOT =       4203
705276  feet/sec       YDOT =        1281
289368  meter/sec
 ZDOT =     -10770
129465                 ZDOT =       -3282
735461


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   19334
45575389  
00016717  00000-0  10270-3 0  9092
2 25544  51
6414 256
9763 0006997 341
8334  18
2565 15
50062447 41048


Satellite: ISS
Catalog Number: 25544
Epoch time:      19334
45575389   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       256
9763  deg
Eccentricity:     
0006997     
Arg of perigee:   341
8334  deg
Mean anomaly:      18
2565  deg
Mean motion:   15
50062447  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4104
Checksum:              334


Coasting Arc #11 (Orbit 4119)
---------------------------------------

Vector Time (GMT): 2019/335/10:24:30
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2446490
19                 A    =         6791986
45  meter
 Y    =       -4322517
70  meter          E    =           
0006485
 Z    =        4626207
69                 I    =           51
26305
 XDOT =       4370
709347                 Wp   =           60
22353
 YDOT =       5586
000682  meter/sec      RA   =          251
16140  deg
 ZDOT =       2908
016368                 TA   =             
67698
                                          MA   =             
67610
                                          Ha   =            228
129  n
mi
                                          Hp   =            221
221

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8026542
63                 X    =         2472172
40
 Y    =      -14181488
52  feet           Y    =        -4295016
22  meter
 Z    =       15177846
74                 Z    =         4638153
77
 XDOT =      14339
597596                 XDOT =        4293
794646
 YDOT =      18326
773892  feet/sec       YDOT =        5634
446670  meter/sec
 ZDOT =       9540
736115                 ZDOT =        2929
061500

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4485084
65                 X    =         1367053
80
 Y    =       15612759
41  feet           Y    =         4758769
07  meter
 Z    =       15232622
70                 Z    =         4642903
40
 XDOT =     -21925
706365                 XDOT =       -6682
955300
 YDOT =      -3102
783438  feet/sec       YDOT =        -945
728392  meter/sec
 ZDOT =       9636
288623                 ZDOT =        2937
140772


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   19335
48729228  
00016717  00000-0  10270-3 0  9101
2 25544  51
6412 251
8661 0006996 344
7885  15
3054 15
50088732 41203


Satellite: ISS
Catalog Number: 25544
Epoch time:      19335
48729228   =   yrday
fracday
Element set:     910
Inclination:       51
6412  deg
RA of node:       251
8661  deg
Eccentricity:     
0006996     
Arg of perigee:   344
7885  deg
Mean anomaly:      15
3054  deg
Mean motion:   15
50088732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4120
Checksum:              318


Coasting Arc #12 (Orbit 4119)
---------------------------------------

Vector Time (GMT): 2019/335/11:30:08
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4406584
87                 A    =         6795240
03  meter
 Y    =       -3583195
39  meter          E    =           
0006890
 Z    =       -3729266
34                 I    =           51
27443
 XDOT =       1456
535933                 Wp   =           35
75508
 YDOT =      -6204
180301  meter/sec      RA   =          250
88727  deg
 ZDOT =       4249
575839                 TA   =          279
53311
                                          MA   =          279
61097
                                          Ha   =            228
252  n
mi
                                          Hp   =            221
135

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14457299
46                 X    =        -4348074
27
 Y    =      -11755890
39  feet           Y    =        -3632145
38  meter
 Z    =      -12235125
78                 Z    =        -3750530
22
 XDOT =       4778
661198                 XDOT =        1505
162486
 YDOT =     -20354
922246  feet/sec       YDOT =       -6187
620854  meter/sec
 ZDOT =      13942
177948                 ZDOT =        4256
768609

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17169040
11                 X    =         5233123
43
 Y    =       -7075524
58  feet           Y    =        -2156619
89  meter
 Z    =      -12331819
94                 Z    =        -3758738
72
 XDOT =      15178
913537                 XDOT =        4626
532846
 YDOT =      12528
493937  feet/sec       YDOT =        3818
684952  meter/sec
 ZDOT =      13975
415750                 ZDOT =        4259
706721


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   19335
48729390  
00016717  00000-0  10270-3 0  9112
2 25544  51
6414 251
8664 0007076 345
8437  14
2514 15
50052443 41202


Satellite: ISS
Catalog Number: 25544
Epoch time:      19335
48729390   =   yrday
fracday
Element set:     911
Inclination:       51
6414  deg
RA of node:       251
8664  deg
Eccentricity:     
0007076     
Arg of perigee:   345
8437  deg
Mean anomaly:      14
2514  deg
Mean motion:   15
50052443  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4120
Checksum:              298


Coasting Arc #13 (Orbit 4135)
---------------------------------------

Vector Time (GMT): 2019/336/11:30:08
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4629420
00                 A    =         6796091
24  meter
 Y    =        3585982
18  meter          E    =           
0013105
 Z    =        3446741
91                 I    =           51
28914
 XDOT =      -1283
732497                 Wp   =           56
98849
 YDOT =       6036
706215  meter/sec      RA   =          245
90895  deg
 ZDOT =      -4536
741514                 TA   =           82
46502
                                          MA   =           82
31617
                                          Ha   =            228
422  n
mi
                                          Hp   =            220
981

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15188385
84                 X    =         4572234
04
 Y    =       11765033
41  feet           Y    =         3637431
57  meter
 Z    =       11308208
38                 Z    =         3469091
39
 XDOT =      -4211
720791                 XDOT =       -1329
104277
 YDOT =      19805
466585  feet/sec       YDOT =        6022
097336  meter/sec
 ZDOT =     -14884
322551                 ZDOT =       -4543
087068

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17391469
33                 X    =        -5300919
85
 Y    =        8020616
96  feet           Y    =         2444684
05  meter
 Z    =       11409870
75                 Z    =         3477728
60
 XDOT =     -15119
857282                 XDOT =       -4608
532500
 YDOT =     -11478
636807  feet/sec       YDOT =       -3498
688499  meter/sec
 ZDOT =     -14913
672059                 ZDOT =       -4545
687244


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   19336
51883222  
00016717  00000-0  10270-3 0  9123
2 25544  51
6413 246
7564 0007071 349
5651  10
5352 15
50057757 41366


Satellite: ISS
Catalog Number: 25544
Epoch time:      19336
51883222   =   yrday
fracday
Element set:     912
Inclination:       51
6413  deg
RA of node:       246
7564  deg
Eccentricity:     
0007071     
Arg of perigee:   349
5651  deg
Mean anomaly:      10
5352  deg
Mean motion:   15
50057757  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4136
Checksum:              303


Coasting Arc #14 (Orbit 4137)
---------------------------------------

Vector Time (GMT): 2019/336/14:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 917861
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4726602
70                 A    =         6791505
33  meter
 Y    =        1210528
54  meter          E    =           
0011866
 Z    =        4724218
20                 I    =           51
27715
 XDOT =        889
967149                 Wp   =           26
93811
 YDOT =       7113
934060  meter/sec      RA   =          245
29236  deg
 ZDOT =      -2700
214130                 TA   =           89
98710
                                          MA   =           89
85112
                                          Ha   =            228
295  n
mi
                                          Hp   =            220
959

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15507226
71                 X    =         4689767
25
 Y    =        3971550
34  feet           Y    =         1263178
37  meter
 Z    =       15499403
54                 Z    =         4747088
96
 XDOT =       2919
839729                 XDOT =         823
467091
 YDOT =      23339
678674  feet/sec       YDOT =        7123
514718  meter/sec
 ZDOT =      -8858
970242                 ZDOT =       -2696
051873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         912697
38                 X    =          278190
16
 Y    =       15879962
53  feet           Y    =         4840212
58  meter
 Z    =       15603607
79                 Z    =         4755979
66
 XDOT =     -20161
375586                 XDOT =       -6145
187279
 YDOT =       9887
249709  feet/sec       YDOT =        3013
633711  meter/sec
 ZDOT =      -8840
477873                 ZDOT =       -2694
577656


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   19336
64777181  
00016717  00000-0  10270-3 0  9134
2 25544  51
6424 246
1181 0007182 348
5637  11
5349 15
50105657 41385


Satellite: ISS
Catalog Number: 25544
Epoch time:      19336
64777181   =   yrday
fracday
Element set:     913
Inclination:       51
6424  deg
RA of node:       246
1181  deg
Eccentricity:     
0007182     
Arg of perigee:   348
5637  deg
Mean anomaly:      11
5349  deg
Mean motion:   15
50105657  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4138
Checksum:              313


Coasting Arc #15 (Orbit 4152)
---------------------------------------

Vector Time (GMT): 2019/337/13:40:13
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4541745
43                 A    =         6790175
55  meter
 Y    =        -183297
58  meter          E    =           
0010696
 Z    =        5044152
85                 I    =           51
28770
 XDOT =       2322
389967                 Wp   =           18
89143
 YDOT =       7070
202599  meter/sec      RA   =          240
49205  deg
 ZDOT =      -1823
124822                 TA   =           88
92460
                                          MA   =           88
80206
                                          Ha   =            228
350  n
mi
                                          Hp   =            220
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14900739
58                 X    =         4518955
80
 Y    =        -601370
01  feet           Y    =         -132636
38  meter
 Z    =       16549057
91                 Z    =         5066159
65
 XDOT =       7619
389656                 XDOT =        2252
012049
 YDOT =      23196
202752  feet/sec       YDOT =        7095
779835  meter/sec
 ZDOT =      -5981
380649                 ZDOT =       -1812
013886

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2208719
15                 X    =          673217
60
 Y    =       14634998
45  feet           Y    =         4460747
53  meter
 Z    =       16649425
93                 Z    =         5074745
02
 XDOT =     -21155
527211                 XDOT =       -6448
204694
 YDOT =       9981
289911  feet/sec       YDOT =        3042
297165  meter/sec
 ZDOT =      -5931
178603                 ZDOT =       -1807
823238


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   19337
61483721  
00016717  00000-0  10270-3 0  9147
2 25544  51
6430 241
3270 0007136 351
5825   8
5204 15
50106249 41531


Satellite: ISS
Catalog Number: 25544
Epoch time:      19337
61483721   =   yrday
fracday
Element set:     914
Inclination:       51
6430  deg
RA of node:       241
3270  deg
Eccentricity:     
0007136     
Arg of perigee:   351
5825  deg
Mean anomaly:       8
5204  deg
Mean motion:   15
50106249  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4153
Checksum:              282


Coasting Arc #16 (Orbit 4167)
---------------------------------------

Vector Time (GMT): 2019/338/13:40:13
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4671814
83                 A    =         6790732
85  meter
 Y    =         178282
82  meter          E    =           
0011951
 Z    =       -4933683
68                 I    =           51
30683
 XDOT =      -2576
998206                 Wp   =           71
89148
 YDOT =      -6863
518986  meter/sec      RA   =          235
51180  deg
 ZDOT =       2200
251109                 TA   =          219
67471
                                          MA   =          219
76221
                                          Ha   =            228
566  n
mi
                                          Hp   =            220
563

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15327476
48                 X    =        -4649496
02
 Y    =         584917
38  feet           Y    =          126164
40  meter
 Z    =      -16186626
25                 Z    =        -4956323
49
 XDOT =      -8454
718523                 XDOT =       -2510
744455
 YDOT =     -22518
106910  feet/sec       YDOT =       -6891
966496  meter/sec
 ZDOT =       7218
671617                 ZDOT =        2187
893430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2497947
65                 X    =         -761374
45
 Y    =      -15022659
87  feet           Y    =        -4578906
73  meter
 Z    =      -16289888
91                 Z    =        -4965158
14
 XDOT =      20170
376781                 XDOT =        6147
930843
 YDOT =     -11092
394222  feet/sec       YDOT =       -3380
961759  meter/sec
 ZDOT =       7162
749427                 ZDOT =        2183
206025


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   19338
58190081  
00016717  00000-0  10270-3 0  9159
2 25544  51
6430 236
5353 0007197 355
5902   4
5183 15
50081684 41689


Satellite: ISS
Catalog Number: 25544
Epoch time:      19338
58190081   =   yrday
fracday
Element set:     915
Inclination:       51
6430  deg
RA of node:       236
5353  deg
Eccentricity:     
0007197     
Arg of perigee:   355
5902  deg
Mean anomaly:       4
5183  deg
Mean motion:   15
50081684  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4168
Checksum:              312


Coasting Arc #17 (Orbit 4170)
---------------------------------------

Vector Time (GMT): 2019/338/17:51:47
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3463783
86                 A    =         6800834
76  meter
 Y    =        5813876
72  meter          E    =           
0006684
 Z    =        -671531
35                 I    =           51
34041
 XDOT =      -4427
402827                 Wp   =           98
55907
 YDOT =       1958
704209  meter/sec      RA   =          234
66134  deg
 ZDOT =      -5930
763058                 TA   =           88
70564
                                          MA   =           88
62907
                                          Ha   =            228
626  n
mi
                                          Hp   =            220
570

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11364120
28                 X    =         3401775
90
 Y    =       19074398
70  feet           Y    =         5852264
54  meter
 Z    =       -2203186
85                 Z    =         -654855
74
 XDOT =     -14525
599825                 XDOT =       -4420
168077
 YDOT =       6426
194910  feet/sec       YDOT =        1909
234690  meter/sec
 ZDOT =     -19457
884050                 ZDOT =       -5952
252136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4285631
77                 X    =         1306260
56
 Y    =       21793050
33  feet           Y    =         6642521
74  meter
 Z    =       -2127502
19                 Z    =         -648462
67
 XDOT =     -14127
805733                 XDOT =       -4306
155188
 YDOT =        886
319634  feet/sec       YDOT =         270
150225  meter/sec
 ZDOT =     -19556
012393                 ZDOT =       -5960
672577


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   19338
77531248  
00016717  00000-0  10270-3 0  9165
2 25544  51
6393 235
5723 0007128 357
5915   2
5200 15
50115672 41714


Satellite: ISS
Catalog Number: 25544
Epoch time:      19338
77531248   =   yrday
fracday
Element set:     916
Inclination:       51
6393  deg
RA of node:       235
5723  deg
Eccentricity:     
0007128     
Arg of perigee:   357
5915  deg
Mean anomaly:       2
5200  deg
Mean motion:   15
50115672  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4171
Checksum:              303


Coasting Arc #18 (Orbit 4186)
---------------------------------------

Vector Time (GMT): 2019/339/17:51:47
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3690788
62                 A    =         6800744
10  meter
 Y    =       -5607418
71  meter          E    =           
0018324
 Z    =        1017333
95                 I    =           51
35935
 XDOT =       4538
655686                 Wp   =           38
70635
 YDOT =      -1913
155639  meter/sec      RA   =          229
68851  deg
 ZDOT =       5877
281008                 TA   =          332
35331
                                          MA   =          332
45062
                                          Ha   =            228
677  n
mi
                                          Hp   =            220
540

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12108886
54                 X    =        -3632752
20
 Y    =      -18397043
00  feet           Y    =        -5648367
27  meter
 Z    =        3337709
81                 Z    =          999545
98
 XDOT =      14890
602643                 XDOT =        4531
163039
 YDOT =      -6276
757347  feet/sec       YDOT =       -1862
443416  meter/sec
 ZDOT =      19282
418006                 ZDOT =        5899
309962

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5589807
07                 X    =        -1703773
19
 Y    =      -21315795
92  feet           Y    =        -6497054
60  meter
 Z    =        3256920
71                 Z    =          992709
43
 XDOT =      14438
566871                 XDOT =        4400
875182
 YDOT =       -802
416575  feet/sec       YDOT =        -244
576572  meter/sec
 ZDOT =      19383
010376                 ZDOT =        5907
941563


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   19339
80684564  
00016717  00000-0  10270-3 0  9171
2 25544  51
6388 230
4612 0006765   2
0162 358
1015 15
50069990 41873


Satellite: ISS
Catalog Number: 25544
Epoch time:      19339
80684564   =   yrday
fracday
Element set:     917
Inclination:       51
6388  deg
RA of node:       230
4612  deg
Eccentricity:     
0006765     
Arg of perigee:     2
0162  deg
Mean anomaly:     358
1015  deg
Mean motion:   15
50069990  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4187
Checksum:              318


Coasting Arc #19 (Orbit 4186)
---------------------------------------

Vector Time (GMT): 2019/339/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -292766
28                 A    =         6792802
56  meter
 Y    =        5137352
07  meter          E    =           
0013360
 Z    =       -4447843
83                 I    =           51
33490
 XDOT =      -6146
961967                 Wp   =           42
04034
 YDOT =      -3178
197944  meter/sec      RA   =          229
50178  deg
 ZDOT =      -3262
271035                 TA   =          194
83860
                                          MA   =          194
87784
                                          Ha   =            228
705  n
mi
                                          Hp   =            220
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -960519
29                 X    =         -328586
56
 Y    =       16854829
64  feet           Y    =         5133878
13  meter
 Z    =      -14592663
49                 Z    =        -4449352
70
 XDOT =     -20167
198053                 XDOT =       -6095
119150
 YDOT =     -10427
158608  feet/sec       YDOT =       -3246
647558  meter/sec
 ZDOT =     -10702
988961                 ZDOT =       -3292
005176

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2068539
37                 X    =         -630490
80
 Y    =       16748700
15  feet           Y    =         5105003
81  meter
 Z    =      -14599859
43                 Z    =        -4450037
15
 XDOT =     -18073
337633                 XDOT =       -5508
753311
 YDOT =     -11691
451900  feet/sec       YDOT =       -3563
554539  meter/sec
 ZDOT =     -10838
414551                 ZDOT =       -3303
548755


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   19339
80684586  
00016717  00000-0  10270-3 0  9186
2 25544  51
6399 230
4617 0006754   2
4408 357
6775 15
50077037 41873


Satellite: ISS
Catalog Number: 25544
Epoch time:      19339
80684586   =   yrday
fracday
Element set:     918
Inclination:       51
6399  deg
RA of node:       230
4617  deg
Eccentricity:     
0006754     
Arg of perigee:     2
4408  deg
Mean anomaly:     357
6775  deg
Mean motion:   15
50077037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4187
Checksum:              343


Coasting Arc #20 (Orbit 4202)
---------------------------------------

Vector Time (GMT): 2019/340/18:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 932295
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         240794
19                 A    =         6792007
36  meter
 Y    =       -4955666
49  meter          E    =           
0008630
 Z    =        4629901
95                 I    =           51
35513
 XDOT =       6409
311658                 Wp   =           69
13442
 YDOT =       3035
506091  meter/sec      RA   =          224
52540  deg
 ZDOT =       2914
356106                 TA   =          351
73664
                                          MA   =          351
75085
                                          Ha   =            228
649  n
mi
                                          Hp   =            220
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         790007
18                 X    =          273702
26
 Y    =      -16258748
33  feet           Y    =        -4952790
03  meter
 Z    =       15189967
03                 Z    =         4631151
29
 XDOT =      21027
925388                 XDOT =        6360
734911
 YDOT =       9959
009485  feet/sec       YDOT =        3106
907764  meter/sec
 ZDOT =       9561
535780                 ZDOT =        2945
372676

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1573321
23                 X    =          479548
31
 Y    =      -16196096
80  feet           Y    =        -4936570
30  meter
 Z    =       15195960
51                 Z    =         4631728
76
 XDOT =      19207
156436                 XDOT =        5854
341282
 YDOT =      10973
777379  feet/sec       YDOT =        3344
807345  meter/sec
 ZDOT =       9702
837146                 ZDOT =        2957
424762


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   19340
83837585  
00016717  00000-0  10270-3 0  9191
2 25544  51
6400 225
3503 0006641   4
5504 355
5705 15
50095175 42030


Satellite: ISS
Catalog Number: 25544
Epoch time:      19340
83837585   =   yrday
fracday
Element set:     919
Inclination:       51
6400  deg
RA of node:       225
3503  deg
Eccentricity:     
0006641     
Arg of perigee:     4
5504  deg
Mean anomaly:     355
5705  deg
Mean motion:   15
50095175  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4203
Checksum:              295


Coasting Arc #21 (Orbit 4211)
---------------------------------------

Vector Time (GMT): 2019/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 952754
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1904435
39                 A    =         6795790
72  meter
 Y    =        5463079
85  meter          E    =           
0009711
 Z    =       -3577729
62                 I    =           51
38703
 XDOT =      -6201
272960                 Wp   =           38
03230
 YDOT =       -734
231373  meter/sec      RA   =          221
18497  deg
 ZDOT =      -4421
048674                 TA   =          184
27517
                                          MA   =          184
28347
                                          Ha   =            228
937  n
mi
                                          Hp   =            220
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6248147
61                 X    =         1860582
95
 Y    =       17923490
31  feet           Y    =         5484131
62  meter
 Z    =      -11737958
06                 Z    =        -3568584
63
 XDOT =     -20345
383728                 XDOT =       -6171
126401
 YDOT =      -2408
895580  feet/sec       YDOT =        -803
409549  meter/sec
 ZDOT =     -14504
752867                 ZDOT =       -4451
099353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18687449
17                 X    =        -5695934
51
 Y    =       -3469903
53  feet           Y    =        -1057626
60  meter
 Z    =      -11696560
44                 Z    =        -3565111
62
 XDOT =      11947
006216                 XDOT =        3641
447495
 YDOT =     -14974
433023  feet/sec       YDOT =       -4564
207185  meter/sec
 ZDOT =     -14641
794709                 ZDOT =       -4462
819027


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   19341
48308253  
00016717  00000-0  10270-3 0  9200
2 25544  51
6431 222
1618 0007184   6
0133 354
1102 15
50073695 42123


Satellite: ISS
Catalog Number: 25544
Epoch time:      19341
48308253   =   yrday
fracday
Element set:     920
Inclination:       51
6431  deg
RA of node:       222
1618  deg
Eccentricity:     
0007184     
Arg of perigee:     6
0133  deg
Mean anomaly:     354
1102  deg
Mean motion:   15
50073695  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            4212
Checksum:              267
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