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

 
Date: August 21st 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14538 8138 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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


234/09:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 222 1

238/20:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 221 8

245/23:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 221 8

Coasting Arc #1 (Orbit 183)
---------------------------------------

Vector Time (GMT): 2020/232/14:41:08
714
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5948823
32                 A    =         6799830
86  meter
 Y    =        1041491
98  meter          E    =           
0005633
 Z    =       -3126741
97                 I    =           51
86967
 XDOT =       1570
169367                 Wp   =           67
60362
 YDOT =       5678
586671  meter/sec      RA   =           33
90910  deg
 ZDOT =       4887
963272                 TA   =          256
62923
                                          MA   =          256
69204
                                          Ha   =            229
242  n
mi
                                          Hp   =            222
267

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19517136
87                 X    =         5951922
48
 Y    =        3416968
43  feet           Y    =         1108033
30  meter
 Z    =      -10258339
81                 Z    =        -3097838
08
 XDOT =       5151
474300                 XDOT =        1482
810647
 YDOT =      18630
533697  feet/sec       YDOT =        5695
656986  meter/sec
 ZDOT =      16036
624908                 ZDOT =        4895
378172

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19869091
11                 X    =        -6056098
97
 Y    =        -729854
92  feet           Y    =         -222459
78  meter
 Z    =      -10124938
07                 Z    =        -3086081
12
 XDOT =      -7574
056500                 XDOT =       -2308
572421
 YDOT =     -16327
028568  feet/sec       YDOT =       -4976
478308  meter/sec
 ZDOT =      16070
533258                 ZDOT =        4898
298537


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   20232
61824917  
00016717  00000-0  10270-3 0  9004
2 25544  51
6431  34
5514 0001221  47
1989 312
9263 15
49148138  1841


Satellite: ISS
Catalog Number: 25544
Epoch time:      20232
61824917   =   yrday
fracday
Element set:     900
Inclination:       51
6431  deg
RA of node:        34
5514  deg
Eccentricity:     
0001221     
Arg of perigee:    47
1989  deg
Mean anomaly:     312
9263  deg
Mean motion:   15
49148138  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             184
Checksum:              289


Coasting Arc #2 (Orbit 199)
---------------------------------------

Vector Time (GMT): 2020/233/14:41:08
714
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6037858
93                 A    =         6800000
15  meter
 Y    =        -597586
31  meter          E    =           
0014017
 Z    =        3057236
06                 I    =           51
84184
 XDOT =      -1963
003223                 Wp   =           93
41506
 YDOT =      -5521
645879  meter/sec      RA   =           28
97576  deg
 ZDOT =      -4937
399732                 TA   =           51
67586
                                          MA   =           51
54993
                                          Ha   =            229
293  n
mi
                                          Hp   =            222
182

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19809248
45                 X    =        -6045577
80
 Y    =       -1960585
00  feet           Y    =         -665149
05  meter
 Z    =       10030302
03                 Z    =         3027888
36
 XDOT =      -6440
299289                 XDOT =       -1877
130050
 YDOT =     -18115
636087  feet/sec       YDOT =       -5543
117564  meter/sec
 ZDOT =     -16198
818019                 ZDOT =       -4946
726335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19943642
81                 X    =         6078822
33
 Y    =       -1095676
29  feet           Y    =         -333962
13  meter
 Z    =        9894836
10                 Z    =         3015946
04
 XDOT =       8939
640009                 XDOT =        2724
802275
 YDOT =      15484
256360  feet/sec       YDOT =        4719
601339  meter/sec
 ZDOT =     -16241
558425                 ZDOT =       -4950
427008


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   20233
65037980  
00016717  00000-0  10270-3 0  9016
2 25544  51
6434  29
4447 0001151  58
8822 301
2440 15
49152661  2002


Satellite: ISS
Catalog Number: 25544
Epoch time:      20233
65037980   =   yrday
fracday
Element set:     901
Inclination:       51
6434  deg
RA of node:        29
4447  deg
Eccentricity:     
0001151     
Arg of perigee:    58
8822  deg
Mean anomaly:     301
2440  deg
Mean motion:   15
49152661  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             200
Checksum:              272


Coasting Arc #3 (Orbit 211)
---------------------------------------

Vector Time (GMT): 2020/234/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5178752
09                 A    =         6802288
78  meter
 Y    =       -4013879
35  meter          E    =           
0006963
 Z    =       -1822094
69                 I    =           51
82478
 XDOT =       4248
980822                 Wp   =          128
34980
 YDOT =      -2921
280169  meter/sec      RA   =           25
14883  deg
 ZDOT =      -5660
048499                 TA   =           71
57682
                                          MA   =           71
50113
                                          Ha   =            229
148  n
mi
                                          Hp   =            222
096

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16990656
46                 X    =        -5124632
24
 Y    =      -13168895
51  feet           Y    =        -4071489
33  meter
 Z    =       -5978000
95                 Z    =        -1847119
04
 XDOT =      13940
225794                 XDOT =        4308
824499
 YDOT =      -9584
252524  feet/sec       YDOT =       -2873
430628  meter/sec
 ZDOT =     -18569
712923                 ZDOT =       -5639
263491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5946374
79                 X    =        -1812455
03
 Y    =       20624040
90  feet           Y    =         6286207
67  meter
 Z    =       -6093297
57                 Z    =        -1857237
10
 XDOT =     -12613
491796                 XDOT =       -3844
592299
 YDOT =      -9076
756368  feet/sec       YDOT =       -2766
595341  meter/sec
 ZDOT =     -18473
583114                 ZDOT =       -5630
748133


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   20234
42447446  
00016717  00000-0  10270-3 0  9025
2 25544  51
6417  25
6166 0001520  36
9922 323
1333 15
49181930  2125


Satellite: ISS
Catalog Number: 25544
Epoch time:      20234
42447446   =   yrday
fracday
Element set:     902
Inclination:       51
6417  deg
RA of node:        25
6166  deg
Eccentricity:     
0001520     
Arg of perigee:    36
9922  deg
Mean anomaly:     323
1333  deg
Mean motion:   15
49181930  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             212
Checksum:              274


Coasting Arc #4 (Orbit 227)
---------------------------------------

Vector Time (GMT): 2020/235/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5468994
79                 A    =         6802247
03  meter
 Y    =        3576045
94  meter          E    =           
0015281
 Z    =        1863027
94                 I    =           51
79315
 XDOT =      -4050
495861                 Wp   =           64
47506
 YDOT =       3240
300696  meter/sec      RA   =           20
21116  deg
 ZDOT =       5641
037063                 TA   =          315
94701
                                          MA   =          316
06866
                                          Ha   =            229
189  n
mi
                                          Hp   =            222
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17942896
29                 X    =         5419550
48
 Y    =       11732434
18  feet           Y    =         3636927
77  meter
 Z    =        6112296
41                 Z    =         1889473
66
 XDOT =     -13289
028414                 XDOT =       -4113
829481
 YDOT =      10630
907795  feet/sec       YDOT =        3194
651262  meter/sec
 ZDOT =      18507
339446                 ZDOT =        5621
207591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3898165
20                 X    =         1188160
75
 Y    =      -21045122
50  feet           Y    =        -6414553
34  meter
 Z    =        6234166
61                 Z    =         1900173
98
 XDOT =      13457
556827                 XDOT =        4101
863321
 YDOT =       7976
225730  feet/sec       YDOT =        2431
153602  meter/sec
 ZDOT =      18415
609803                 ZDOT =        5613
077868


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   20235
45660166  
00016717  00000-0  10270-3 0  9036
2 25544  51
6414  20
5090 0001461  45
7802 314
3468 15
49175792  2288


Satellite: ISS
Catalog Number: 25544
Epoch time:      20235
45660166   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:        20
5090  deg
Eccentricity:     
0001461     
Arg of perigee:    45
7802  deg
Mean anomaly:     314
3468  deg
Mean motion:   15
49175792  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             228
Checksum:              288


Coasting Arc #5 (Orbit 242)
---------------------------------------

Vector Time (GMT): 2020/236/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5708510
10                 A    =         6802044
12  meter
 Y    =       -3145257
31  meter          E    =           
0006963
 Z    =       -1942137
96                 I    =           51
76030
 XDOT =       3843
997817                 Wp   =          125
82127
 YDOT =      -3527
818554  meter/sec      RA   =           15
27257  deg
 ZDOT =      -5603
462510                 TA   =           75
49947
                                          MA   =           75
42224
                                          Ha   =            229
231  n
mi
                                          Hp   =            221
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18728707
67                 X    =        -5663480
88
 Y    =      -10319085
67  feet           Y    =        -3208842
25  meter
 Z    =       -6371843
70                 Z    =        -1969758
04
 XDOT =      12611
541393                 XDOT =        3910
379506
 YDOT =     -11574
207855  feet/sec       YDOT =       -3484
461232  meter/sec
 ZDOT =     -18384
063353                 ZDOT =       -5584
628645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1926222
50                 X    =         -587112
62
 Y    =       21257920
52  feet           Y    =         6479414
17  meter
 Z    =       -6499145
68                 Z    =        -1980939
60
 XDOT =     -14172
414147                 XDOT =       -4319
751832
 YDOT =      -6860
304710  feet/sec       YDOT =       -2091
020876  meter/sec
 ZDOT =     -18296
918373                 ZDOT =       -5576
900720


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   20236
42422004  
00016717  00000-0  10270-3 0  9042
2 25544  51
6410  15
7217 0001651  48
9933 311
1359 15
49197195  2434


Satellite: ISS
Catalog Number: 25544
Epoch time:      20236
42422004   =   yrday
fracday
Element set:     904
Inclination:       51
6410  deg
RA of node:        15
7217  deg
Eccentricity:     
0001651     
Arg of perigee:    48
9933  deg
Mean anomaly:     311
1359  deg
Mean motion:   15
49197195  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             243
Checksum:              280


Coasting Arc #6 (Orbit 258)
---------------------------------------

Vector Time (GMT): 2020/237/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5924852
98                 A    =         6802047
40  meter
 Y    =        2670481
70  meter          E    =           
0015335
 Z    =        1983079
44                 I    =           51
72658
 XDOT =      -3600
281467                 Wp   =           67
11463
 YDOT =       3820
939525  meter/sec      RA   =           10
33108  deg
 ZDOT =       5582
581041                 TA   =          314
70969
                                          MA   =          314
83448
                                          Ha   =            229
240  n
mi
                                          Hp   =            221
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19438494
03                 X    =         5884917
87
 Y    =        8761422
89  feet           Y    =         2736514
38  meter
 Z    =        6506166
13                 Z    =         2011762
93
 XDOT =     -11811
947069                 XDOT =       -3669
857676
 YDOT =      12535
890831  feet/sec       YDOT =        3780
289648  meter/sec
 ZDOT =      18315
554596                 ZDOT =        5564
923305

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -151072
88                 X    =          -46047
01
 Y    =      -21280430
37  feet           Y    =        -6486275
18  meter
 Z    =        6638391
33                 Z    =         2023381
68
 XDOT =      14827
869463                 XDOT =        4519
534612
 YDOT =       5611
416311  feet/sec       YDOT =        1710
359692  meter/sec
 ZDOT =      18233
824483                 ZDOT =        5557
669702


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   20237
45634627  
00016717  00000-0  10270-3 0  9053
2 25544  51
6405  10
6146 0001461  58
4021 301
7271 15
49174359  2598


Satellite: ISS
Catalog Number: 25544
Epoch time:      20237
45634627   =   yrday
fracday
Element set:     905
Inclination:       51
6405  deg
RA of node:        10
6146  deg
Eccentricity:     
0001461     
Arg of perigee:    58
4021  deg
Mean anomaly:     301
7271  deg
Mean motion:   15
49174359  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             259
Checksum:              285


Coasting Arc #7 (Orbit 273)
---------------------------------------

Vector Time (GMT): 2020/238/09:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6091117
63                 A    =         6801799
02  meter
 Y    =       -2211711
51  meter          E    =           
0006847
 Z    =       -2063535
19                 I    =           51
69405
 XDOT =       3353
702408                 Wp   =          124
46905
 YDOT =      -4081
059211  meter/sec      RA   =            5
38759  deg
 ZDOT =      -5542
222508                 TA   =           78
27829
                                          MA   =           78
20148
                                          Ha   =            229
243  n
mi
                                          Hp   =            221
874

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19983981
71                 X    =        -6055909
46
 Y    =       -7256271
34  feet           Y    =        -2279629
86  meter
 Z    =       -6770128
58                 Z    =        -2093037
87
 XDOT =      11002
960655                 XDOT =        3426
009644
 YDOT =     -13389
301873  feet/sec       YDOT =       -4043
151367  meter/sec
 ZDOT =     -18183
144712                 ZDOT =       -5525
756002

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2109100
21                 X    =          642853
74
 Y    =       21111712
68  feet           Y    =         6434850
03  meter
 Z    =       -6906151
15                 Z    =        -2104994
87
 XDOT =     -15351
764118                 XDOT =       -4679
217703
 YDOT =      -4371
739204  feet/sec       YDOT =       -1332
506109  meter/sec
 ZDOT =     -18106
899028                 ZDOT =       -5518
982824


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   20238
42396166  
00016717  00000-0  10270-3 0  9065
2 25544  51
6419   5
8269 0001633  56
8985 303
2321 15
49208024  2744


Satellite: ISS
Catalog Number: 25544
Epoch time:      20238
42396166   =   yrday
fracday
Element set:     906
Inclination:       51
6419  deg
RA of node:         5
8269  deg
Eccentricity:     
0001633     
Arg of perigee:    56
8985  deg
Mean anomaly:     303
2321  deg
Mean motion:   15
49208024  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             274
Checksum:              303


Coasting Arc #8 (Orbit 280)
---------------------------------------

Vector Time (GMT): 2020/238/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4108214
74                 A    =         6796473
59  meter
 Y    =       -3503102
97  meter          E    =           
0009415
 Z    =       -4138370
76                 I    =           51
66108
 XDOT =       6088
313686                 Wp   =           67
84479
 YDOT =      -2667
460003  meter/sec      RA   =            3
13943  deg
 ZDOT =      -3789
423868                 TA   =          163
01538
                                          MA   =          162
98384
                                          Ha   =            229
376  n
mi
                                          Hp   =            221
820

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13478394
81                 X    =        -4048634
90
 Y    =      -11493119
97  feet           Y    =        -3548710
76  meter
 Z    =      -13577331
88                 Z    =        -4158182
13
 XDOT =      19974
782435                 XDOT =        6136
096310
 YDOT =      -8751
509197  feet/sec       YDOT =       -2599
108888  meter/sec
 ZDOT =     -12432
493006                 ZDOT =       -3759
733331

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8854009
35                 X    =         2698702
05
 Y    =      -15260414
94  feet           Y    =        -4651374
47  meter
 Z    =      -13668545
22                 Z    =        -4166172
58
 XDOT =      11157
789545                 XDOT =        3400
894253
 YDOT =      17476
320603  feet/sec       YDOT =        5326
782520  meter/sec
 ZDOT =     -12295
306720                 ZDOT =       -3747
609488


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   20238
87551490  
00016717  00000-0  10270-3 0  9078
2 25544  51
6423   3
5961 0001780  58
6755 301
4570 15
49172451  2819


Satellite: ISS
Catalog Number: 25544
Epoch time:      20238
87551490   =   yrday
fracday
Element set:     907
Inclination:       51
6423  deg
RA of node:         3
5961  deg
Eccentricity:     
0001780     
Arg of perigee:    58
6755  deg
Mean anomaly:     301
4570  deg
Mean motion:   15
49172451  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             281
Checksum:              301


Coasting Arc #9 (Orbit 296)
---------------------------------------

Vector Time (GMT): 2020/239/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4331781
67                 A    =         6796299
98  meter
 Y    =        3163088
58  meter          E    =           
0011395
 Z    =        4165080
91                 I    =           51
62590
 XDOT =      -5903
601575                 Wp   =           98
09690
 YDOT =       3148
245260  meter/sec      RA   =          358
19261  deg
 ZDOT =       3738
669125                 TA   =          313
37742
                                          MA   =          313
47227
                                          Ha   =            229
224  n
mi
                                          Hp   =            221
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14211882
10                 X    =         4275857
67
 Y    =       10377587
19  feet           Y    =         3211216
83  meter
 Z    =       13664963
60                 Z    =         4185987
13
 XDOT =     -19368
771571                 XDOT =       -5956
527621
 YDOT =      10328
888649  feet/sec       YDOT =        3081
930917  meter/sec
 ZDOT =      12265
974818                 ZDOT =        3709
863490

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7350820
57                 X    =        -2240530
11
 Y    =       15905870
46  feet           Y    =         4848109
32  meter
 Z    =       13761244
90                 Z    =         4194427
44
 XDOT =     -12845
042230                 XDOT =       -3915
168872
 YDOT =     -16462
372124  feet/sec       YDOT =       -5017
731023  meter/sec
 ZDOT =      12132
848662                 ZDOT =        3698
092272


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   20239
90763518  
00016717  00000-0  10270-3 0  9080
2 25544  51
6413 358
4898 0001690  56
4843 303
6468 15
49189983  2978


Satellite: ISS
Catalog Number: 25544
Epoch time:      20239
90763518   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       358
4898  deg
Eccentricity:     
0001690     
Arg of perigee:    56
4843  deg
Mean anomaly:     303
6468  deg
Mean motion:   15
49189983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             297
Checksum:              352


Coasting Arc #10 (Orbit 311)
---------------------------------------

Vector Time (GMT): 2020/240/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4520347
95                 A    =         6796181
54  meter
 Y    =       -2833873
88  meter          E    =           
0009874
 Z    =       -4220378
68                 I    =           51
59120
 XDOT =       5672
543187                 Wp   =           67
92556
 YDOT =      -3597
131912  meter/sec      RA   =          353
24247  deg
 ZDOT =      -3663
620334                 TA   =          164
42246
                                          MA   =          164
39205
                                          Ha   =            229
393  n
mi
                                          Hp   =            221
789

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14830537
88                 X    =        -4467822
80
 Y    =       -9297486
50  feet           Y    =        -2884129
81  meter
 Z    =      -13846386
75                 Z    =        -4242209
05
 XDOT =      18610
705994                 XDOT =        5730
141377
 YDOT =     -11801
613883  feet/sec       YDOT =       -3533
375291  meter/sec
 ZDOT =     -12019
751751                 ZDOT =       -3635
925880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5888003
47                 X    =         1794663
46
 Y    =      -16398919
21  feet           Y    =        -4998390
58  meter
 Z    =      -13946949
46                 Z    =        -4251030
19
 XDOT =      14372
755584                 XDOT =        4380
815902
 YDOT =      15265
123400  feet/sec       YDOT =        4652
809612  meter/sec
 ZDOT =     -11891
732170                 ZDOT =       -3624
599965


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   20240
87524856  
00016717  00000-0  10270-3 0  9099
2 25544  51
6409 353
7019 0001788  61
4404 298
6925 15
49169890  3127


Satellite: ISS
Catalog Number: 25544
Epoch time:      20240
87524856   =   yrday
fracday
Element set:     909
Inclination:       51
6409  deg
RA of node:       353
7019  deg
Eccentricity:     
0001788     
Arg of perigee:    61
4404  deg
Mean anomaly:     298
6925  deg
Mean motion:   15
49169890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             312
Checksum:              330


Coasting Arc #11 (Orbit 327)
---------------------------------------

Vector Time (GMT): 2020/241/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4687475
82                 A    =         6795934
35  meter
 Y    =        2471280
48  meter          E    =           
0011083
 Z    =        4246876
41                 I    =           51
55786
 XDOT =      -5414
387759                 Wp   =          100
55077
 YDOT =       4048
708069  meter/sec      RA   =          348
29122  deg
 ZDOT =       3610
130174                 TA   =          312
43245
                                          MA   =          312
52613
                                          Ha   =            229
165  n
mi
                                          Hp   =            221
876

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15378857
69                 X    =         4638864
26
 Y    =        8107875
57  feet           Y    =         2523427
25  meter
 Z    =       13933321
56                 Z    =         4269528
00
 XDOT =     -17763
739368                 XDOT =       -5476
794902
 YDOT =      13283
162957  feet/sec       YDOT =        3987
811461  meter/sec
 ZDOT =      11844
259102                 ZDOT =        3583
678148

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4320508
02                 X    =        -1316890
84
 Y    =       16752931
85  feet           Y    =         5106293
63  meter
 Z    =       14037693
72                 Z    =         4278689
05
 XDOT =     -15857
478763                 XDOT =       -4833
359527
 YDOT =     -13939
021291  feet/sec       YDOT =       -4248
613690  meter/sec
 ZDOT =      11721
953498                 ZDOT =        3572
851426


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   20241
90736589  
00016717  00000-0  10270-3 0  9104
2 25544  51
6414 348
5958 0001589  62
5432 297
5880 15
49211839  3285


Satellite: ISS
Catalog Number: 25544
Epoch time:      20241
90736589   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:       348
5958  deg
Eccentricity:     
0001589     
Arg of perigee:    62
5432  deg
Mean anomaly:     297
5880  deg
Mean motion:   15
49211839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             328
Checksum:              333


Coasting Arc #12 (Orbit 342)
---------------------------------------

Vector Time (GMT): 2020/242/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4821506
44                 A    =         6795832
80  meter
 Y    =       -2125820
06  meter          E    =           
0010377
 Z    =       -4302350
93                 I    =           51
52523
 XDOT =       5115
259480                 Wp   =           68
19806
 YDOT =      -4460
750978  meter/sec      RA   =          343
33598  deg
 ZDOT =      -3531
526628                 TA   =          165
68826
                                          MA   =          165
65884
                                          Ha   =            229
395  n
mi
                                          Hp   =            221
720

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15818590
67                 X    =        -4776478
56
 Y    =       -6974475
25  feet           Y    =        -2179485
76  meter
 Z    =      -14115324
58                 Z    =        -4325662
17
 XDOT =      16782
347375                 XDOT =        5181
914583
 YDOT =     -14635
009770  feet/sec       YDOT =       -4403
175738  meter/sec
 ZDOT =     -11586
373450                 ZDOT =       -3506
517337

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2824685
42                 X    =          860964
12
 Y    =      -16966077
16  feet           Y    =        -5171260
32  meter
 Z    =      -14222759
30                 Z    =        -4335097
03
 XDOT =      17147
833039                 XDOT =        5226
659510
 YDOT =      12462
430179  feet/sec       YDOT =        3798
548719  meter/sec
 ZDOT =     -11470
711587                 ZDOT =       -3496
272892


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   20242
87497564  
00016717  00000-0  10270-3 0  9119
2 25544  51
6422 343
8074 0001831  64
4014 295
7325 15
49185619  3435


Satellite: ISS
Catalog Number: 25544
Epoch time:      20242
87497564   =   yrday
fracday
Element set:     911
Inclination:       51
6422  deg
RA of node:       343
8074  deg
Eccentricity:     
0001831     
Arg of perigee:    64
4014  deg
Mean anomaly:     295
7325  deg
Mean motion:   15
49185619  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             343
Checksum:              308


Coasting Arc #13 (Orbit 358)
---------------------------------------

Vector Time (GMT): 2020/243/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4929968
97                 A    =         6795584
71  meter
 Y    =        1751245
87  meter          E    =           
0010824
 Z    =        4329109
61                 I    =           51
49257
 XDOT =      -4789
602777                 Wp   =          102
24750
 YDOT =       4871
534737  meter/sec      RA   =          338
38057  deg
 ZDOT =       3474
088203                 TA   =          312
30859
                                          MA   =          312
40026
                                          Ha   =            229
161  n
mi
                                          Hp   =            221
818

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16174438
87                 X    =         4888991
69
 Y    =        5745557
31  feet           Y    =         1806147
21  meter
 Z    =       14203115
53                 Z    =         4352957
46
 XDOT =     -15713
919871                 XDOT =       -4860
596567
 YDOT =      15982
725516  feet/sec       YDOT =        4817
577036  meter/sec
 ZDOT =      11397
927176                 ZDOT =        3450
650202

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1253284
08                 X    =         -382000
99
 Y    =       17026990
42  feet           Y    =         5189826
68  meter
 Z    =       14313045
40                 Z    =         4362616
24
 XDOT =     -18372
426080                 XDOT =       -5599
915469
 YDOT =     -10868
695310  feet/sec       YDOT =       -3312
778331  meter/sec
 ZDOT =      11289
505696                 ZDOT =        3441
041336


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   20243
90708836  
00016717  00000-0  10270-3 0  9122
2 25544  51
6420 338
7017 0001646  66
0417 294
0905 15
49226500  3590


Satellite: ISS
Catalog Number: 25544
Epoch time:      20243
90708836   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:       338
7017  deg
Eccentricity:     
0001646     
Arg of perigee:    66
0417  deg
Mean anomaly:     294
0905  deg
Mean motion:   15
49226500  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             359
Checksum:              296


Coasting Arc #14 (Orbit 373)
---------------------------------------

Vector Time (GMT): 2020/244/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5010534
48                 A    =         6795505
95  meter
 Y    =       -1397743
09  meter          E    =           
0010817
 Z    =       -4383729
52                 I    =           51
46080
 XDOT =       4426
827533                 Wp   =           68
62628
 YDOT =      -5236
789079  meter/sec      RA   =          333
42133  deg
 ZDOT =      -3392
980637                 TA   =          166
84748
                                          MA   =          166
81925
                                          Ha   =            229
385  n
mi
                                          Hp   =            221
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16438761
42                 X    =        -4973238
88
 Y    =       -4585771
30  feet           Y    =        -1453566
06  meter
 Z    =      -14382314
70                 Z    =        -4407977
63
 XDOT =      14523
712380                 XDOT =        4501
538707
 YDOT =     -17181
066533  feet/sec       YDOT =       -5186
867481  meter/sec
 ZDOT =     -11131
826237                 ZDOT =       -3371
295667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -226605
87                 X    =          -69069
47
 Y    =      -16970051
88  feet           Y    =        -5172471
81  meter
 Z    =      -14494107
10                 Z    =        -4417803
84
 XDOT =      19374
091196                 XDOT =        5905
222996
 YDOT =       9155
144486  feet/sec       YDOT =        2790
488039  meter/sec
 ZDOT =     -11031
489258                 ZDOT =       -3362
397926


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   20244
87469642  
00016717  00000-0  10270-3 0  9139
2 25544  51
6418 333
9138 0001809  67
1470 292
9871 15
49193554  3748


Satellite: ISS
Catalog Number: 25544
Epoch time:      20244
87469642   =   yrday
fracday
Element set:     913
Inclination:       51
6418  deg
RA of node:       333
9138  deg
Eccentricity:     
0001809     
Arg of perigee:    67
1470  deg
Mean anomaly:     292
9871  deg
Mean motion:   15
49193554  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             374
Checksum:              331


Coasting Arc #15 (Orbit 389)
---------------------------------------

Vector Time (GMT): 2020/245/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5061847
95                 A    =         6795254
52  meter
 Y    =        1019505
55  meter          E    =           
0010487
 Z    =        4410164
78                 I    =           51
43152
 XDOT =      -4038
812955                 Wp   =          104
64689
 YDOT =       5596
629927  meter/sec      RA   =          328
46155  deg
 ZDOT =       3332
579359                 TA   =          311
51914
                                          MA   =          311
60907
                                          Ha   =            229
130  n
mi
                                          Hp   =            221
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16607112
70                 X    =         5028649
65
 Y    =        3344834
49  feet           Y    =         1075925
35  meter
 Z    =       14469044
56                 Z    =         4434672
14
 XDOT =     -13250
698671                 XDOT =       -4117
283458
 YDOT =      18361
646743  feet/sec       YDOT =        5551
026433  meter/sec
 ZDOT =      10933
659313                 ZDOT =        3312
769880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1752687
86                 X    =          534219
26
 Y    =       16751994
84  feet           Y    =         5106008
03  meter
 Z    =       14582047
69                 Z    =         4444608
14
 XDOT =     -20288
800044                 XDOT =       -6184
026253
 YDOT =      -7341
085218  feet/sec       YDOT =       -2237
562775  meter/sec
 ZDOT =      10841
974012                 ZDOT =        3304
633679


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   20245
90680664  
00016717  00000-0  10270-3 0  9144
2 25544  51
6426 328
8081 0001579  71
9138 288
2184 15
49235066  3903


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
90680664   =   yrday
fracday
Element set:     914
Inclination:       51
6426  deg
RA of node:       328
8081  deg
Eccentricity:     
0001579     
Arg of perigee:    71
9138  deg
Mean anomaly:     288
2184  deg
Mean motion:   15
49235066  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             390
Checksum:              321


Coasting Arc #16 (Orbit 390)
---------------------------------------

Vector Time (GMT): 2020/245/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -447150
28                 A    =         6792846
16  meter
 Y    =       -4502669
53  meter          E    =           
0014559
 Z    =       -5079555
32                 I    =           51
42136
 XDOT =       6939
784415                 Wp   =           99
09800
 YDOT =      -2685
393475  meter/sec      RA   =          327
89806  deg
 ZDOT =       1771
618361                 TA   =          188
12373
                                          MA   =          188
14733
                                          Ha   =            229
366  n
mi
                                          Hp   =            221
803

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1467028
48                 X    =         -372093
70
 Y    =      -14772537
84  feet           Y    =        -4507250
48  meter
 Z    =      -16665207
73                 Z    =        -5081544
84
 XDOT =      22768
321572                 XDOT =        6960
692157
 YDOT =      -8810
346047  feet/sec       YDOT =       -2607
670844  meter/sec
 ZDOT =       5812
396197                 ZDOT =        1805
379439

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7216682
40                 X    =         2199644
79
 Y    =      -12961541
55  feet           Y    =        -3950677
87  meter
 Z    =      -16674145
59                 Z    =        -5082279
58
 XDOT =      22791
164681                 XDOT =        6946
746995
 YDOT =       5020
694197  feet/sec       YDOT =        1530
307591  meter/sec
 ZDOT =       5968
285202                 ZDOT =        1819
133330


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   20245
97131545  
00016717  00000-0  10270-3 0  9151
2 25544  51
6441 328
4891 0001748  67
1638 292
9696 15
49197972  3919


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
97131545   =   yrday
fracday
Element set:     915
Inclination:       51
6441  deg
RA of node:       328
4891  deg
Eccentricity:     
0001748     
Arg of perigee:    67
1638  deg
Mean anomaly:     292
9696  deg
Mean motion:   15
49197972  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             391
Checksum:              344


Coasting Arc #17 (Orbit 406)
---------------------------------------

Vector Time (GMT): 2020/246/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         739719
31                 A    =         6792871
85  meter
 Y    =        4486587
88  meter          E    =           
0007409
 Z    =        5042060
68                 I    =           51
39362
 XDOT =      -6708
379606                 Wp   =           58
25767
 YDOT =       3204
419105  meter/sec      RA   =          322
93545  deg
 ZDOT =      -1861
366406                 TA   =           49
88220
                                          MA   =           49
81730
                                          Ha   =            229
307  n
mi
                                          Hp   =            221
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2426900
62                 X    =          665002
85
 Y    =       14719776
49  feet           Y    =         4494442
51  meter
 Z    =       16542193
84                 Z    =         5045472
14
 XDOT =     -22009
119443                 XDOT =       -6734
672478
 YDOT =      10513
186039  feet/sec       YDOT =        3129
254065  meter/sec
 ZDOT =      -6106
845163                 ZDOT =       -1894
016696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6161204
63                 X    =        -1877935
17
 Y    =       13567901
56  feet           Y    =         4135496
39  meter
 Z    =       16557700
58                 Z    =         5046787
14
 XDOT =     -23139
313899                 XDOT =       -7052
862876
 YDOT =      -2847
683656  feet/sec       YDOT =        -867
973978  meter/sec
 ZDOT =      -6257
618276                 ZDOT =       -1907
322051


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   20247
00342382  
00016717  00000-0  10270-3 0  9161
2 25544  51
6439 323
3832 0001764  67
5916 292
5421 15
49223557  4075


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
00342382   =   yrday
fracday
Element set:     916
Inclination:       51
6439  deg
RA of node:       323
3832  deg
Eccentricity:     
0001764     
Arg of perigee:    67
5916  deg
Mean anomaly:     292
5421  deg
Mean motion:   15
49223557  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             407
Checksum:              300
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