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

 
Date: June 9th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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


There are no maneuvers



Coasting Arc #1 (Orbit 3065)
---------------------------------------

Vector Time (GMT): 2020/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5963526
14                 A    =         6798803
65  meter
 Y    =         624869
64  meter          E    =           
0006147
 Z    =       -3205843
22                 I    =           51
85234
 XDOT =       1999
452087                 Wp   =           61
09293
 YDOT =       5601
541990  meter/sec      RA   =           30
81230  deg
 ZDOT =       4821
107263                 TA   =          262
07016
                                          MA   =          262
13992
                                          Ha   =            228
934  n
mi
                                          Hp   =            221
775

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19565374
49                 X    =         5971667
51
 Y    =        2050097
23  feet           Y    =          691604
18  meter
 Z    =      -10517858
34                 Z    =        -3176855
00
 XDOT =       6559
882176                 XDOT =        1913
247324
 YDOT =      18377
762434  feet/sec       YDOT =        5623
418334  meter/sec
 ZDOT =      15817
281046                 ZDOT =        4830
611501

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6599680
13                 X    =         2011582
50
 Y    =      -18607482
61  feet           Y    =        -5671560
70  meter
 Z    =      -10384504
55                 Z    =        -3165196
99
 XDOT =      18022
564043                 XDOT =        5493
277520
 YDOT =      -2440
939818  feet/sec       YDOT =        -743
998457  meter/sec
 ZDOT =      15860
561511                 ZDOT =        4834
299148


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   20160
50652981  
00016717  00000-0  10270-3 0  9002
2 25544  51
6446  31
4434 0002187  26
4102 333
7159 15
49427741 30660


Satellite: ISS
Catalog Number: 25544
Epoch time:      20160
50652981   =   yrday
fracday
Element set:     900
Inclination:       51
6446  deg
RA of node:        31
4434  deg
Eccentricity:     
0002187     
Arg of perigee:    26
4102  deg
Mean anomaly:     333
7159  deg
Mean motion:   15
49427741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3066
Checksum:              286


Coasting Arc #2 (Orbit 3081)
---------------------------------------

Vector Time (GMT): 2020/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6058212
79                 A    =         6799072
31  meter
 Y    =        -261241
82  meter          E    =           
0014204
 Z    =        3063747
81                 I    =           51
82405
 XDOT =      -2270
157722                 Wp   =           87
48434
 YDOT =      -5409
091287  meter/sec      RA   =           25
87543  deg
 ZDOT =      -4929
862936                 TA   =           57
51037
                                          MA   =           57
37316
                                          Ha   =            228
978  n
mi
                                          Hp   =            221
588

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19876026
20                 X    =        -6069723
05
 Y    =        -857092
59  feet           Y    =         -329053
98  meter
 Z    =       10051666
05                 Z    =         3034291
63
 XDOT =      -7448
024023                 XDOT =       -2185
556687
 YDOT =     -17746
362491  feet/sec       YDOT =       -5434
003886  meter/sec
 ZDOT =     -16174
090998                 ZDOT =       -4940
685878

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5181304
40                 X    =        -1579261
58
 Y    =       19278262
92  feet           Y    =         5876014
54  meter
 Z    =        9916132
26                 Z    =         3022437
11
 XDOT =     -17513
829532                 XDOT =       -5338
215241
 YDOT =       3672
542831  feet/sec       YDOT =        1119
391055  meter/sec
 ZDOT =     -16223
451758                 ZDOT =       -4944
908096


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   20161
53848338  
00016717  00000-0  10270-3 0  9010
2 25544  51
6447  26
3349 0002354  30
7207 329
4080 15
49464320 30826


Satellite: ISS
Catalog Number: 25544
Epoch time:      20161
53848338   =   yrday
fracday
Element set:     901
Inclination:       51
6447  deg
RA of node:        26
3349  deg
Eccentricity:     
0002354     
Arg of perigee:    30
7207  deg
Mean anomaly:     329
4080  deg
Mean motion:   15
49464320  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3082
Checksum:              290


Coasting Arc #3 (Orbit 3096)
---------------------------------------

Vector Time (GMT): 2020/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6121518
96                 A    =         6799434
17  meter
 Y    =        -148780
78  meter          E    =           
0006584
 Z    =       -2955537
37                 I    =           51
79254
 XDOT =       2541
672509                 Wp   =           54
59372
 YDOT =       5198
317966  meter/sec      RA   =           20
93673  deg
 ZDOT =       5014
231072                 TA   =          271
82017
                                          MA   =          271
89558
                                          Ha   =            229
005  n
mi
                                          Hp   =            221
663

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20083723
61                 X    =         6137083
87
 Y    =        -488125
91  feet           Y    =          -80238
09  meter
 Z    =       -9696644
92                 Z    =        -2925763
93
 XDOT =       8338
820567                 XDOT =        2458
998445
 YDOT =      17054
848971  feet/sec       YDOT =        5226
277699  meter/sec
 ZDOT =      16450
889345                 ZDOT =        5026
377436

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3572471
05                 X    =         1088889
18
 Y    =      -19836083
34  feet           Y    =        -6046038
20  meter
 Z    =       -9559623
00                 Z    =        -2913773
09
 XDOT =      16915
015664                 XDOT =        5155
696775
 YDOT =      -4889
944240  feet/sec       YDOT =       -1490
455004  meter/sec
 ZDOT =      16506
354277                 ZDOT =        5031
136784


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   20162
50594026  
00016717  00000-0  10270-3 0  9021
2 25544  51
6430  21
5460 0002212  33
9806 326
1486 15
49432009 30971


Satellite: ISS
Catalog Number: 25544
Epoch time:      20162
50594026   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:        21
5460  deg
Eccentricity:     
0002212     
Arg of perigee:    33
9806  deg
Mean anomaly:     326
1486  deg
Mean motion:   15
49432009  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3097
Checksum:              276


Coasting Arc #4 (Orbit 3112)
---------------------------------------

Vector Time (GMT): 2020/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6164148
13                 A    =         6799674
06  meter
 Y    =         533830
77  meter          E    =           
0014469
 Z    =        2807037
18                 I    =           51
76258
 XDOT =      -2771
288673                 Wp   =           92
00187
 YDOT =      -4987
271098  meter/sec      RA   =           15
99673  deg
 ZDOT =      -5114
889627                 TA   =           56
26222
                                          MA   =           56
12442
                                          Ha   =            228
961  n
mi
                                          Hp   =            221
552

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20223583
09                 X    =        -6183294
30
 Y    =        1751413
28  feet           Y    =          464791
43  meter
 Z    =        9209439
56                 Z    =         2777048
00
 XDOT =      -9092
154440                 XDOT =       -2690
468582
 YDOT =     -16362
437984  feet/sec       YDOT =       -5017
809006  meter/sec
 ZDOT =     -16781
133948                 ZDOT =       -5128
155750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2014234
79                 X    =         -613938
76
 Y    =       20261467
83  feet           Y    =         6175695
39  meter
 Z    =        9071401
11                 Z    =         2764963
06
 XDOT =     -16259
424229                 XDOT =       -4955
872505
 YDOT =       5957
210172  feet/sec       YDOT =        1815
757661  meter/sec
 ZDOT =     -16841
765400                 ZDOT =       -5133
370094


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   20163
53789227  
00016717  00000-0  10270-3 0  9035
2 25544  51
6438  16
4383 0002258  34
3756 325
7540 15
49473544 31139


Satellite: ISS
Catalog Number: 25544
Epoch time:      20163
53789227   =   yrday
fracday
Element set:     903
Inclination:       51
6438  deg
RA of node:        16
4383  deg
Eccentricity:     
0002258     
Arg of perigee:    34
3756  deg
Mean anomaly:     325
7540  deg
Mean motion:   15
49473544  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3113
Checksum:              308


Coasting Arc #5 (Orbit 3127)
---------------------------------------

Vector Time (GMT): 2020/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6168762
64                 A    =         6800023
44  meter
 Y    =        -959811
22  meter          E    =           
0007070
 Z    =       -2693207
46                 I    =           51
73012
 XDOT =       3001
792042                 Wp   =           49
08920
 YDOT =       4760
199599  meter/sec      RA   =           11
05306  deg
 ZDOT =       5192
552626                 TA   =          280
61041
                                          MA   =          280
69003
                                          Ha   =            229
008  n
mi
                                          Hp   =            221
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20238722
57                 X    =         6192119
03
 Y    =       -3148986
95  feet           Y    =         -890696
79  meter
 Z    =       -8835982
49                 Z    =        -2663185
63
 XDOT =       9848
399088                 XDOT =        2923
116709
 YDOT =      15617
452752  feet/sec       YDOT =        4793
327212  meter/sec
 ZDOT =      17035
933812                 ZDOT =        5206
943576

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         289651
07                 X    =           88285
65
 Y    =      -20539267
74  feet           Y    =        -6260368
81  meter
 Z    =       -8697768
66                 Z    =        -2651079
89
 XDOT =      15528
298083                 XDOT =        4733
025256
 YDOT =      -7004
143175  feet/sec       YDOT =       -2134
862840  meter/sec
 ZDOT =      17101
755285                 ZDOT =        5212
615011


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   20164
50534689  
00016717  00000-0  10270-3 0  9044
2 25544  51
6432  11
6487 0002136  38
9313 321
1990 15
49440900 31284


Satellite: ISS
Catalog Number: 25544
Epoch time:      20164
50534689   =   yrday
fracday
Element set:     904
Inclination:       51
6432  deg
RA of node:        11
6487  deg
Eccentricity:     
0002136     
Arg of perigee:    38
9313  deg
Mean anomaly:     321
1990  deg
Mean motion:   15
49440900  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3128
Checksum:              292


Coasting Arc #6 (Orbit 3143)
---------------------------------------

Vector Time (GMT): 2020/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6155278
23                 A    =         6800244
84  meter
 Y    =        1356671
21  meter          E    =           
0014808
 Z    =        2537240
89                 I    =           51
69779
 XDOT =      -3189
477548                 Wp   =           96
11456
 YDOT =      -4539
548184  meter/sec      RA   =            6
10841  deg
 ZDOT =      -5285
264328                 TA   =           55
47075
                                          MA   =           55
33105
                                          Ha   =            229
002  n
mi
                                          Hp   =            221
458

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20194482
37                 X    =        -6182315
87
 Y    =        4451021
02  feet           Y    =         1287687
02  meter
 Z    =        8324281
14                 Z    =         2507275
58
 XDOT =     -10464
165184                 XDOT =       -3112
805243
 YDOT =     -14893
530788  feet/sec       YDOT =       -4574
785856  meter/sec
 ZDOT =     -17340
106063                 ZDOT =       -5300
571823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1358088
40                 X    =          413945
34
 Y    =       20689667
79  feet           Y    =         6306210
74  meter
 Z    =        8186305
96                 Z    =         2495186
06
 XDOT =     -14771
216398                 XDOT =       -4502
266758
 YDOT =       7891
308683  feet/sec       YDOT =        2405
270886  meter/sec
 ZDOT =     -17410
157315                 ZDOT =       -5306
615950


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   20165
53729498  
00016717  00000-0  10270-3 0  9053
2 25544  51
6430   6
5406 0002319  40
0340 320
0981 15
49483080 31445


Satellite: ISS
Catalog Number: 25544
Epoch time:      20165
53729498   =   yrday
fracday
Element set:     905
Inclination:       51
6430  deg
RA of node:         6
5406  deg
Eccentricity:     
0002319     
Arg of perigee:    40
0340  deg
Mean anomaly:     320
0981  deg
Mean motion:   15
49483080  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3144
Checksum:              282


Coasting Arc #7 (Orbit 3158)
---------------------------------------

Vector Time (GMT): 2020/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6097170
98                 A    =         6800609
66  meter
 Y    =       -1789499
85  meter          E    =           
0007784
 Z    =       -2418676
48                 I    =           51
66312
 XDOT =       3381
280686                 Wp   =           46
53396
 YDOT =       4304
300788  meter/sec      RA   =            1
16111  deg
 ZDOT =       5355
221858                 TA   =          286
49597
                                          MA   =          286
58148
                                          Ha   =            229
085  n
mi
                                          Hp   =            221
494

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20003841
79                 X    =         6128477
08
 Y    =       -5871062
49  feet           Y    =        -1721141
61  meter
 Z    =       -7935290
29                 Z    =        -2388983
01
 XDOT =      11093
440570                 XDOT =        3306
884832
 YDOT =      14121
721747  feet/sec       YDOT =        4341
696064  meter/sec
 ZDOT =      17569
625518                 ZDOT =        5371
466605

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3146889
22                 X    =         -959171
83
 Y    =      -20660874
26  feet           Y    =        -6297434
47  meter
 Z    =       -7798541
94                 Z    =        -2376995
58
 XDOT =      13952
174309                 XDOT =        4252
622729
 YDOT =      -8764
647275  feet/sec       YDOT =       -2671
464489  meter/sec
 ZDOT =      17644
001788                 ZDOT =        5377
891745


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   20166
50474826  
00016717  00000-0  10270-3 0  9064
2 25544  51
6411   1
7518 0002144  49
2678 310
8658 15
49438857 31592


Satellite: ISS
Catalog Number: 25544
Epoch time:      20166
50474826   =   yrday
fracday
Element set:     906
Inclination:       51
6411  deg
RA of node:         1
7518  deg
Eccentricity:     
0002144     
Arg of perigee:    49
2678  deg
Mean anomaly:     310
8658  deg
Mean motion:   15
49438857  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3159
Checksum:              320


Coasting Arc #8 (Orbit 3174)
---------------------------------------

Vector Time (GMT): 2020/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6023365
19                 A    =         6800786
06  meter
 Y    =        2189624
01  meter          E    =           
0014921
 Z    =        2257006
81                 I    =           51
63112
 XDOT =      -3532
075983                 Wp   =          100
93709
 YDOT =      -4081
462340  meter/sec      RA   =          356
21181  deg
 ZDOT =      -5438
763108                 TA   =           53
99673
                                          MA   =           53
85850
                                          Ha   =            228
969  n
mi
                                          Hp   =            221
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19761696
83                 X    =        -6058365
82
 Y    =        7183805
82  feet           Y    =         2122070
47  meter
 Z    =        7404878
00                 Z    =         2227662
86
 XDOT =     -11588
175797                 XDOT =       -3459
754889
 YDOT =     -13390
624475  feet/sec       YDOT =       -4120
555475  meter/sec
 ZDOT =     -17843
710984                 ZDOT =       -5455
745450

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4834193
02                 X    =         1473462
03
 Y    =       20512087
97  feet           Y    =         6252084
41  meter
 Z    =        7269715
99                 Z    =         2215809
43
 XDOT =     -13137
144777                 XDOT =       -4004
201728
 YDOT =       9480
630069  feet/sec       YDOT =        2889
696045  meter/sec
 ZDOT =     -17921
491922                 ZDOT =       -5462
470738


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   20167
53669462  
00016717  00000-0  10270-3 0  9071
2 25544  51
6418 356
6435 0002132  45
6543 314
4782 15
49487798 31751


Satellite: ISS
Catalog Number: 25544
Epoch time:      20167
53669462   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:       356
6435  deg
Eccentricity:     
0002132     
Arg of perigee:    45
6543  deg
Mean anomaly:     314
4782  deg
Mean motion:   15
49487798  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3175
Checksum:              336


Coasting Arc #9 (Orbit 3189)
---------------------------------------

Vector Time (GMT): 2020/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5900856
44                 A    =         6801131
52  meter
 Y    =       -2618173
86  meter          E    =           
0008549
 Z    =       -2133392
38                 I    =           51
59742
 XDOT =       3687
783316                 Wp   =           44
85945
 YDOT =       3844
806141  meter/sec      RA   =          351
25937  deg
 ZDOT =       5501
143457                 TA   =          291
53728
                                          MA   =          291
62838
                                          Ha   =            229
127  n
mi
                                          Hp   =            221
404

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19359765
23                 X    =         5940057
93
 Y    =       -8589809
26  feet           Y    =        -2551966
80  meter
 Z    =       -6999318
82                 Z    =        -2104633
33
 XDOT =      12099
026627                 XDOT =        3617
793933
 YDOT =      12614
193377  feet/sec       YDOT =        3885
653468  meter/sec
 ZDOT =      18048
370923                 ZDOT =        5518
887893

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6625467
71                 X    =        -2019442
56
 Y    =      -20162483
11  feet           Y    =        -6145524
85  meter
 Z    =       -6866822
35                 Z    =        -2093007
45
 XDOT =      12269
196518                 XDOT =        3739
651099
 YDOT =     -10184
107099  feet/sec       YDOT =       -3104
115844  meter/sec
 ZDOT =      18129
670181                 ZDOT =        5525
923471


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   20168
50414567  
00016717  00000-0  10270-3 0  9084
2 25544  51
6409 351
8539 0002158  57
7744 302
3615 15
49443248 31908


Satellite: ISS
Catalog Number: 25544
Epoch time:      20168
50414567   =   yrday
fracday
Element set:     908
Inclination:       51
6409  deg
RA of node:       351
8539  deg
Eccentricity:     
0002158     
Arg of perigee:    57
7744  deg
Mean anomaly:     302
3615  deg
Mean motion:   15
49443248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3190
Checksum:              316


Coasting Arc #10 (Orbit 3205)
---------------------------------------

Vector Time (GMT): 2020/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5766449
86                 A    =         6801301
23  meter
 Y    =        3010032
62  meter          E    =           
0015197
 Z    =        1964870
89                 I    =           51
56496
 XDOT =      -3804
108851                 Wp   =          105
35301
 YDOT =      -3627
172191  meter/sec      RA   =          346
30559  deg
 ZDOT =      -5575
519202                 TA   =           52
98369
                                          MA   =           52
84474
                                          Ha   =            229
037  n
mi
                                          Hp   =            221
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18918798
75                 X    =        -5809224
64
 Y    =        9875435
11  feet           Y    =         2945308
60  meter
 Z    =        6446426
80                 Z    =         1936756
13
 XDOT =     -12480
672083                 XDOT =       -3736
183155
 YDOT =     -11900
171230  feet/sec       YDOT =       -3669
331785  meter/sec
 ZDOT =     -18292
385834                 ZDOT =       -5593
833776

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8289019
16                 X    =         2526493
04
 Y    =       19707635
45  feet           Y    =         6006887
29  meter
 Z    =        6316870
23                 Z    =         1925382
04
 XDOT =     -11436
365762                 XDOT =       -3485
804284
 YDOT =      10734
748419  feet/sec       YDOT =        3271
951318  meter/sec
 ZDOT =     -18376
319463                 ZDOT =       -5601
102172


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   20169
53608827  
00016717  00000-0  10270-3 0  9093
2 25544  51
6406 346
7456 0002169  55
6586 304
4769 15
49485049 32065


Satellite: ISS
Catalog Number: 25544
Epoch time:      20169
53608827   =   yrday
fracday
Element set:     909
Inclination:       51
6406  deg
RA of node:       346
7456  deg
Eccentricity:     
0002169     
Arg of perigee:    55
6586  deg
Mean anomaly:     304
4769  deg
Mean motion:   15
49485049  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3206
Checksum:              342


Coasting Arc #11 (Orbit 3220)
---------------------------------------

Vector Time (GMT): 2020/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5579163
16                 A    =         6801608
65  meter
 Y    =       -3423840
21  meter          E    =           
0009365
 Z    =       -1837391
69                 I    =           51
53243
 XDOT =       3929
070332                 Wp   =           45
20874
 YDOT =       3394
378036  meter/sec      RA   =          341
34925  deg
 ZDOT =       5629
411658                 TA   =          294
59972
                                          MA   =          294
69726
                                          Ha   =            229
201  n
mi
                                          Hp   =            221
289

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18304341
08                 X    =         5625959
96
 Y    =      -11233071
55  feet           Y    =        -3361188
05  meter
 Z    =       -6028187
96                 Z    =        -1810177
06
 XDOT =      12890
650697                 XDOT =        3863
476744
 YDOT =      11136
410879  feet/sec       YDOT =        3437
947959  meter/sec
 ZDOT =      18469
198352                 ZDOT =        5648
338943

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10021538
00                 X    =        -3054564
78
 Y    =      -19034080
86  feet           Y    =        -5801587
85  meter
 Z    =       -5902744
35                 Z    =        -1799156
48
 XDOT =      10552
861256                 XDOT =        3216
512111
 YDOT =     -11285
545380  feet/sec       YDOT =       -3439
834232  meter/sec
 ZDOT =      18555
964681                 ZDOT =        5655
858035


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   20170
50353772  
00016717  00000-0  10270-3 0  9100
2 25544  51
6398 341
9566 0002253  69
3585 290
7806 15
49444881 32214


Satellite: ISS
Catalog Number: 25544
Epoch time:      20170
50353772   =   yrday
fracday
Element set:     910
Inclination:       51
6398  deg
RA of node:       341
9566  deg
Eccentricity:     
0002253     
Arg of perigee:    69
3585  deg
Mean anomaly:     290
7806  deg
Mean motion:   15
49444881  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3221
Checksum:              318


Coasting Arc #12 (Orbit 3236)
---------------------------------------

Vector Time (GMT): 2020/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5383935
30                 A    =         6801779
95  meter
 Y    =        3797470
69  meter          E    =           
0015367
 Z    =        1663849
94                 I    =           51
50192
 XDOT =      -4018
342789                 Wp   =          110
09534
 YDOT =      -3185
931947  meter/sec      RA   =          336
39101  deg
 ZDOT =      -5693
604531                 TA   =           51
67298
                                          MA   =           51
53493
                                          Ha   =            229
088  n
mi
                                          Hp   =            221
299

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17663829
72                 X    =        -5434081
67
 Y    =       12458893
33  feet           Y    =         3736982
98  meter
 Z    =        5458825
27                 Z    =         1637575
70
 XDOT =     -13183
539333                 XDOT =       -3954
761704
 YDOT =     -10452
532633  feet/sec       YDOT =       -3230
511317  meter/sec
 ZDOT =     -18679
804892                 ZDOT =       -5712
970347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11602540
16                 X    =         3536454
24
 Y    =       18273584
58  feet           Y    =         5569788
58  meter
 Z    =        5337681
64                 Z    =         1626925
36
 XDOT =      -9730
637485                 XDOT =       -2965
898306
 YDOT =      11697
538104  feet/sec       YDOT =        3565
409614  meter/sec
 ZDOT =     -18768
602676                 ZDOT =       -5720
670096


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   20171
53547913  
00016717  00000-0  10270-3 0  9117
2 25544  51
6400 336
8482 0002140  67
4671 292
6705 15
49474161 32378


Satellite: ISS
Catalog Number: 25544
Epoch time:      20171
53547913   =   yrday
fracday
Element set:     911
Inclination:       51
6400  deg
RA of node:       336
8482  deg
Eccentricity:     
0002140     
Arg of perigee:    67
4671  deg
Mean anomaly:     292
6705  deg
Mean motion:   15
49474161  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3237
Checksum:              299


Coasting Arc #13 (Orbit 3251)
---------------------------------------

Vector Time (GMT): 2020/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5134647
40                 A    =         6801992
87  meter
 Y    =       -4184730
87  meter          E    =           
0010192
 Z    =       -1531862
08                 I    =           51
47373
 XDOT =       4116
657927                 Wp   =           45
54305
 YDOT =       2961
422124  meter/sec      RA   =          331
43024  deg
 ZDOT =       5739
281561                 TA   =          297
71824
                                          MA   =          297
82159
                                          Ha   =            229
220  n
mi
                                          Hp   =            221
204

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16845956
02                 X    =         5188501
60
 Y    =      -13729431
99  feet           Y    =        -4127010
15  meter
 Z    =       -5025794
23                 Z    =        -1506789
99
 XDOT =      13506
095560                 XDOT =        4055
358284
 YDOT =       9715
951849  feet/sec       YDOT =        3007
113594  meter/sec
 ZDOT =      18829
663914                 ZDOT =        5759
130432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13210041
92                 X    =        -4026420
78
 Y    =      -17289515
22  feet           Y    =        -5269844
24  meter
 Z    =       -4910152
81                 Z    =        -1496614
58
 XDOT =       8858
540895                 XDOT =        2700
083265
 YDOT =     -12112
532031  feet/sec       YDOT =       -3691
899763  meter/sec
 ZDOT =      18920
701363                 ZDOT =        5767
029775


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   20172
50292481  
00016717  00000-0  10270-3 0  9123
2 25544  51
6416 332
0591 0002321  76
7969 283
3440 15
49457260 32529


Satellite: ISS
Catalog Number: 25544
Epoch time:      20172
50292481   =   yrday
fracday
Element set:     912
Inclination:       51
6416  deg
RA of node:       332
0591  deg
Eccentricity:     
0002321     
Arg of perigee:    76
7969  deg
Mean anomaly:     283
3440  deg
Mean motion:   15
49457260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3252
Checksum:              296


Coasting Arc #14 (Orbit 3267)
---------------------------------------

Vector Time (GMT): 2020/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4882441
68                 A    =         6802186
99  meter
 Y    =        4528933
80  meter          E    =           
0015524
 Z    =        1352713
88                 I    =           51
44427
 XDOT =      -4183
798645                 Wp   =          114
22154
 YDOT =      -2766
279596  meter/sec      RA   =          326
46803  deg
 ZDOT =      -5792
850891                 TA   =           51
03150
                                          MA   =           50
89330
                                          Ha   =            229
179  n
mi
                                          Hp   =            221
207

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16018509
45                 X    =        -4939293
38
 Y    =       14858706
71  feet           Y    =         4474016
70  meter
 Z    =        4438037
65                 Z    =         1328859
83
 XDOT =     -13726
373507                 XDOT =       -4124
416063
 YDOT =      -9075
720458  feet/sec       YDOT =       -2812
732549  meter/sec
 ZDOT =     -19005
416308                 ZDOT =       -5813
030457

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14645619
00                 X    =         4463984
67
 Y    =       16243289
60  feet           Y    =         4950954
67  meter
 Z    =        4327975
89                 Z    =         1319167
05
 XDOT =      -8071
143242                 XDOT =       -2460
084460
 YDOT =      12407
484353  feet/sec       YDOT =        3781
801231  meter/sec
 ZDOT =     -19097
992428                 ZDOT =       -5821
068092


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   20173
53486328  
00016717  00000-0  10270-3 0  9133
2 25544  51
6405 326
9507 0002302  77
8087 282
3321 15
49465601 32680


Satellite: ISS
Catalog Number: 25544
Epoch time:      20173
53486328   =   yrday
fracday
Element set:     913
Inclination:       51
6405  deg
RA of node:       326
9507  deg
Eccentricity:     
0002302     
Arg of perigee:    77
8087  deg
Mean anomaly:     282
3321  deg
Mean motion:   15
49465601  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3268
Checksum:              307


Coasting Arc #15 (Orbit 3282)
---------------------------------------

Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4574924
88                 A    =         6802345
04  meter
 Y    =       -4879424
91  meter          E    =           
0010954
 Z    =       -1217462
18                 I    =           51
41862
 XDOT =       4262
356782                 Wp   =           46
62382
 YDOT =       2551
980824  meter/sec      RA   =          321
50450  deg
 ZDOT =       5829
393457                 TA   =          300
13340
                                          MA   =          300
24191
                                          Ha   =            229
235  n
mi
                                          Hp   =            221
166

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15009596
05                 X    =         4635061
73
 Y    =      -16008611
92  feet           Y    =        -4827928
34  meter
 Z    =       -3994298
49                 Z    =        -1195094
12
 XDOT =      13984
110178                 XDOT =        4205
187345
 YDOT =       8372
640499  feet/sec       YDOT =        2599
324640  meter/sec
 ZDOT =      19125
306618                 ZDOT =        5849
959859

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16068692
59                 X    =        -4897737
50
 Y    =      -14972471
24  feet           Y    =        -4563609
23  meter
 Z    =       -3891050
38                 Z    =        -1185992
15
 XDOT =       7226
553657                 XDOT =        2202
653555
 YDOT =     -12715
024047  feet/sec       YDOT =       -3875
539329  meter/sec
 ZDOT =      19219
682684                 ZDOT =        5858
159282


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   20174
50230656  
00016717  00000-0  10270-3 0  9143
2 25544  51
6418 322
1628 0002349  84
4695 275
6723 15
49457060 32834


Satellite: ISS
Catalog Number: 25544
Epoch time:      20174
50230656   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:       322
1628  deg
Eccentricity:     
0002349     
Arg of perigee:    84
4695  deg
Mean anomaly:     275
6723  deg
Mean motion:   15
49457060  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3283
Checksum:              311


Coasting Arc #16 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2020/175/11:57:30
000
Vector Time (MET): N/A
Weight (LBS)     : 980069
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3564628
41                 A    =         6801475
87  meter
 Y    =        5464514
44  meter          E    =           
0015968
 Z    =        1896500
42                 I    =           51
39003
 XDOT =      -5064
141255                 Wp   =          109
48690
 YDOT =      -1351
643718  meter/sec      RA   =          316
53978  deg
 ZDOT =      -5590
544932                 TA   =           49
58432
                                          MA   =           49
44512
                                          Ha   =            229
196  n
mi
                                          Hp   =            221
218

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11694975
08                 X    =        -3634681
31
 Y    =       17928196
97  feet           Y    =         5424260
15  meter
 Z    =        6222114
24                 Z    =         1879016
02
 XDOT =     -16614
636663                 XDOT =       -5021
495053
 YDOT =      -4434
526635  feet/sec       YDOT =       -1408
034966  meter/sec
 ZDOT =     -18341
682847                 ZDOT =       -5615
040961

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18047941
42                 X    =         5501012
54
 Y    =       11552651
77  feet           Y    =         3521248
26  meter
 Z    =        6141289
95                 Z    =         1871865
18
 XDOT =      -3423
802691                 XDOT =       -1043
575060
 YDOT =      15217
804834  feet/sec       YDOT =        4638
386913  meter/sec
 ZDOT =     -18454
227316                 ZDOT =       -5624
848486


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   20175
53424390  
00016717  00000-0  10270-3 0  9158
2 25544  51
6417 317
0543 0002255  87
2881 272
8527 15
49454732 32986


Satellite: ISS
Catalog Number: 25544
Epoch time:      20175
53424390   =   yrday
fracday
Element set:     915
Inclination:       51
6417  deg
RA of node:       317
0543  deg
Eccentricity:     
0002255     
Arg of perigee:    87
2881  deg
Mean anomaly:     272
8527  deg
Mean motion:   15
49454732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3298
Checksum:              318
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