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

 
Date: March 17th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13861 7638 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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


079/17:18:26 637 1 0 1 9 1 9
N/A 1 5 0 0 230 6
000/00:08:53 274 -0 6 -0 0 221 9

081/01:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 7
000/00:00:00 000 0 0 0 0 221 7

085/12:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 9
000/00:00:00 000 0 0 0 0 221 4

089/03:22:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 9
000/00:00:00 000 0 0 0 0 221 2

Coasting Arc #1 (Orbit 1763)
---------------------------------------

Vector Time (GMT): 2020/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4182721
87                 A    =         6791667
75  meter
 Y    =        -215070
14  meter          E    =           
0018647
 Z    =       -5361948
74                 I    =           52
00956
 XDOT =        461
619916                 Wp   =           74
15035
 YDOT =       7633
052823  meter/sec      RA   =           86
19365  deg
 ZDOT =         59
044997                 TA   =          196
38080
                                          MA   =          196
44114
                                          Ha   =            230
453  n
mi
                                          Hp   =            221
159

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13722840
77                 X    =         4210861
01
 Y    =        -705610
70  feet           Y    =         -168138
83  meter
 Z    =      -17591695
34                 Z    =        -5341562
56
 XDOT =       1514
501036                 XDOT =         375
943756
 YDOT =      25042
824224  feet/sec       YDOT =        7637
735942  meter/sec
 ZDOT =        193
717181                 ZDOT =          61
078976

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13834993
35                 X    =         4216905
97
 Y    =         831481
17  feet           Y    =          253435
46  meter
 Z    =      -17498102
42                 Z    =        -5333421
62
 XDOT =      -1210
265684                 XDOT =        -368
888980
 YDOT =      24047
433666  feet/sec       YDOT =        7329
657781  meter/sec
 ZDOT =        202
651256                 ZDOT =          61
768103


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   20076
51604214  
00016717  00000-0  10270-3 0  9005
2 25544  51
6412  86
9962 0006063  30
9353 329
2153 15
49228202 17647


Satellite: ISS
Catalog Number: 25544
Epoch time:      20076
51604214   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:        86
9962  deg
Eccentricity:     
0006063     
Arg of perigee:    30
9353  deg
Mean anomaly:     329
2153  deg
Mean motion:   15
49228202  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1764
Checksum:              286


Coasting Arc #2 (Orbit 1779)
---------------------------------------

Vector Time (GMT): 2020/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4156973
49                 A    =         6791592
59  meter
 Y    =         448002
64  meter          E    =           
0007995
 Z    =        5347125
44                 I    =           52
00547
 XDOT =      -1036
349837                 Wp   =           47
33983
 YDOT =      -7593
198429  meter/sec      RA   =           81
26985  deg
 ZDOT =       -164
068946                 TA   =           44
24846
                                          MA   =           44
18456
                                          Ha   =            230
639  n
mi
                                          Hp   =            220
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13638364
47                 X    =        -4187647
17
 Y    =        1469824
95  feet           Y    =          401345
11  meter
 Z    =       17543062
46                 Z    =         5326858
24
 XDOT =      -3400
097892                 XDOT =        -950
566487
 YDOT =     -24912
068337  feet/sec       YDOT =       -7604
307991  meter/sec
 ZDOT =       -538
283943                 ZDOT =        -168
894425

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13834420
90                 X    =        -4216731
49
 Y    =         175416
54  feet           Y    =           53466
96  meter
 Z    =       17449998
24                 Z    =         5318759
46
 XDOT =      -1034
679557                 XDOT =        -315
370329
 YDOT =     -24111
901569  feet/sec       YDOT =       -7349
307598  meter/sec
 ZDOT =       -560
018412                 ZDOT =        -170
693612


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   20077
54812008  
00016717  00000-0  10270-3 0  9012
2 25544  51
6404  81
8884 0006130  34
4716 325
6831 15
49251001 17806


Satellite: ISS
Catalog Number: 25544
Epoch time:      20077
54812008   =   yrday
fracday
Element set:     901
Inclination:       51
6404  deg
RA of node:        81
8884  deg
Eccentricity:     
0006130     
Arg of perigee:    34
4716  deg
Mean anomaly:     325
6831  deg
Mean motion:   15
49251001  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1780
Checksum:              282


Coasting Arc #3 (Orbit 1794)
---------------------------------------

Vector Time (GMT): 2020/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4134729
11                 A    =         6791679
21  meter
 Y    =        -709646
48  meter          E    =           
0019145
 Z    =       -5357001
02                 I    =           51
99965
 XDOT =       1608
399872                 Wp   =           76
68309
 YDOT =       7471
332940  meter/sec      RA   =           76
34701  deg
 ZDOT =        256
738037                 TA   =          195
72905
                                          MA   =          195
78861
                                          Ha   =            230
622  n
mi
                                          Hp   =            220
910

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13565384
20                 X    =         4168378
11
 Y    =       -2328236
49  feet           Y    =         -663221
11  meter
 Z    =      -17575462
67                 Z    =        -5336834
69
 XDOT =       5276
902466                 XDOT =        1523
486618
 YDOT =      24512
247180  feet/sec       YDOT =        7488
844443  meter/sec
 ZDOT =        842
316394                 ZDOT =         264
344303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13822527
03                 X    =         4213106
24
 Y    =       -1274822
83  feet           Y    =         -388566
00  meter
 Z    =      -17482842
88                 Z    =        -5328770
51
 XDOT =       3286
265363                 XDOT =        1001
653683
 YDOT =      23835
907593  feet/sec       YDOT =        7265
184634  meter/sec
 ZDOT =        876
810021                 ZDOT =         267
251695


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   20078
51569135  
00016717  00000-0  10270-3 0  9021
2 25544  51
6408  77
1009 0006237  38
2141 321
9450 15
49231924 17953


Satellite: ISS
Catalog Number: 25544
Epoch time:      20078
51569135   =   yrday
fracday
Element set:     902
Inclination:       51
6408  deg
RA of node:        77
1009  deg
Eccentricity:     
0006237     
Arg of perigee:    38
2141  deg
Mean anomaly:     321
9450  deg
Mean motion:   15
49231924  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1795
Checksum:              298


Coasting Arc #4 (Orbit 1810)
---------------------------------------

Vector Time (GMT): 2020/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4086451
68                 A    =         6791631
15  meter
 Y    =         936784
90  meter          E    =           
0008571
 Z    =        5337816
02                 I    =           51
98926
 XDOT =      -2167
483713                 Wp   =           49
94193
 YDOT =      -7343
836800  meter/sec      RA   =           71
42263  deg
 ZDOT =       -364
758133                 TA   =           43
55424
                                          MA   =           43
48659
                                          Ha   =            230
775  n
mi
                                          Hp   =            220
679

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13406993
70                 X    =        -4122550
97
 Y    =        3073441
27  feet           Y    =          890885
77  meter
 Z    =       17512519
76                 Z    =         5317878
26
 XDOT =      -7111
167036                 XDOT =       -2083
429917
 YDOT =     -24093
952756  feet/sec       YDOT =       -7367
605192  meter/sec
 ZDOT =      -1196
713035                 ZDOT =        -375
082136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13684278
54                 X    =        -4170968
10
 Y    =        2265714
44  feet           Y    =          690589
76  meter
 Z    =       17420933
63                 Z    =         5309900
57
 XDOT =      -5494
278704                 XDOT =       -1674
656149
 YDOT =     -23475
433170  feet/sec       YDOT =       -7155
312030  meter/sec
 ZDOT =      -1243
679029                 ZDOT =        -379
073368


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   20079
54776502  
00016717  00000-0  10270-3 0  9034
2 25544  51
6395  71
9934 0006245  40
8160 319
3456 15
49250983 18118


Satellite: ISS
Catalog Number: 25544
Epoch time:      20079
54776502   =   yrday
fracday
Element set:     903
Inclination:       51
6395  deg
RA of node:        71
9934  deg
Eccentricity:     
0006245     
Arg of perigee:    40
8160  deg
Mean anomaly:     319
3456  deg
Mean motion:   15
49250983  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1811
Checksum:              316


Coasting Arc #5 (Orbit 1813)
---------------------------------------

Vector Time (GMT): 2020/079/17:22:53
274
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3721277
88                 A    =         6792705
05  meter
 Y    =       -1987029
38  meter          E    =           
0018172
 Z    =       -5339373
82                 I    =           51
99053
 XDOT =       2964
910517                 Wp   =           72
95046
 YDOT =       7027
404502  meter/sec      RA   =           70
32726  deg
 ZDOT =       -545
189960                 TA   =          191
83640
                                          MA   =          191
87917
                                          Ha   =            230
649  n
mi
                                          Hp   =            221
873

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12208916
91                 X    =         3769156
01
 Y    =       -6519125
26  feet           Y    =        -1945148
05  meter
 Z    =      -17517630
63                 Z    =        -5321181
22
 XDOT =       9727
396708                 XDOT =        2888
755823
 YDOT =      23055
789048  feet/sec       YDOT =        7060
134396  meter/sec
 ZDOT =      -1788
680972                 ZDOT =        -530
973264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3706342
71                 X    =        -1129693
26
 Y    =      -13444065
71  feet           Y    =        -4097751
23  meter
 Z    =      -17433994
10                 Z    =        -5313881
40
 XDOT =      23633
767712                 XDOT =        7203
572399
 YDOT =      -4264
520150  feet/sec       YDOT =       -1299
825742  meter/sec
 ZDOT =      -1723
828024                 ZDOT =        -525
422782


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   20079
74128176  
00016717  00000-0  10270-3 0  9045
2 25544  51
6430  71
0368 0005042  32
9998 327
1466 15
48904919 18140


Satellite: ISS
Catalog Number: 25544
Epoch time:      20079
74128176   =   yrday
fracday
Element set:     904
Inclination:       51
6430  deg
RA of node:        71
0368  deg
Eccentricity:     
0005042     
Arg of perigee:    32
9998  deg
Mean anomaly:     327
1466  deg
Mean motion:   15
48904919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1814
Checksum:              319


Coasting Arc #6 (Orbit 1829)
---------------------------------------

Vector Time (GMT): 2020/080/17:22:53
274
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3514612
94                 A    =         6792638
70  meter
 Y    =        2322829
92  meter          E    =           
0006136
 Z    =        5323501
01                 I    =           51
97786
 XDOT =      -3586
842932                 Wp   =           61
83848
 YDOT =      -6748
855916  meter/sec      RA   =           65
40651  deg
 ZDOT =        579
013533                 TA   =           22
67228
                                          MA   =           22
64519
                                          Ha   =            230
734  n
mi
                                          Hp   =            221
705

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11530882
36                 X    =        -3566184
37
 Y    =        7620833
07  feet           Y    =         2283239
10  meter
 Z    =       17465554
51                 Z    =         5306303
26
 XDOT =     -11767
857388                 XDOT =       -3513
921121
 YDOT =     -22141
915734  feet/sec       YDOT =       -6788
558764  meter/sec
 ZDOT =       1899
650699                 ZDOT =         561
768029

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5151693
25                 X    =         1570236
10
 Y    =       12932706
61  feet           Y    =         3941888
97  meter
 Z    =       17386462
99                 Z    =         5299393
92
 XDOT =     -23099
907021                 XDOT =       -7040
851660
 YDOT =       6764
031575  feet/sec       YDOT =        2061
676824  meter/sec
 ZDOT =       1820
887179                 ZDOT =         555
006412


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   20080
77359581  
00016717  00000-0  10270-3 0  9057
2 25544  51
6427  65
9315 0004866  35
4273 324
7199 15
48924579 18305


Satellite: ISS
Catalog Number: 25544
Epoch time:      20080
77359581   =   yrday
fracday
Element set:     905
Inclination:       51
6427  deg
RA of node:        65
9315  deg
Eccentricity:     
0004866     
Arg of perigee:    35
4273  deg
Mean anomaly:     324
7199  deg
Mean motion:   15
48924579  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1830
Checksum:              336


Coasting Arc #7 (Orbit 1834)
---------------------------------------

Vector Time (GMT): 2020/081/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2854292
66                 A    =         6793361
70  meter
 Y    =        3353256
19  meter          E    =           
0006858
 Z    =        5166799
80                 I    =           51
97332
 XDOT =      -4358
861676                 Wp   =           83
24573
 YDOT =      -6110
030035  meter/sec      RA   =           63
82941  deg
 ZDOT =       1556
466227                 TA   =          351
81048
                                          MA   =          351
82166
                                          Ha   =            230
702  n
mi
                                          Hp   =            221
724

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9364477
22                 X    =        -2916674
55
 Y    =       11001496
68  feet           Y    =         3320989
11  meter
 Z    =       16951442
93                 Z    =         5152783
20
 XDOT =     -14300
727283                 XDOT =       -4297
773853
 YDOT =     -20046
030298  feet/sec       YDOT =       -6158
432225  meter/sec
 ZDOT =       5106
516492                 ZDOT =        1535
441854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6452543
43                 X    =         1966735
24
 Y    =      -13010585
32  feet           Y    =        -3965626
41  meter
 Z    =       16886892
35                 Z    =         5147124
79
 XDOT =      17912
375308                 XDOT =        5459
691994
 YDOT =      15390
901349  feet/sec       YDOT =        4691
146731  meter/sec
 ZDOT =       5010
369916                 ZDOT =        1527
160750


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   20081
09619434  
00016717  00000-0  10270-3 0  9060
2 25544  51
6404  64
3305 0004564  39
8863 320
2621 15
48906907 18351


Satellite: ISS
Catalog Number: 25544
Epoch time:      20081
09619434   =   yrday
fracday
Element set:     906
Inclination:       51
6404  deg
RA of node:        64
3305  deg
Eccentricity:     
0004564     
Arg of perigee:    39
8863  deg
Mean anomaly:     320
2621  deg
Mean motion:   15
48906907  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1835
Checksum:              305


Coasting Arc #8 (Orbit 1849)
---------------------------------------

Vector Time (GMT): 2020/082/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2538375
95                 A    =         6793399
27  meter
 Y    =       -3624515
38  meter          E    =           
0017650
 Z    =       -5170315
70                 I    =           51
95888
 XDOT =       4871
890799                 Wp   =           69
41614
 YDOT =       5676
199709  meter/sec      RA   =           58
90761  deg
 ZDOT =      -1585
642131                 TA   =          185
30839
                                          MA   =          185
32713
                                          Ha   =            230
667  n
mi
                                          Hp   =            221
690

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8328005
08                 X    =         2603831
75
 Y    =      -11891454
66  feet           Y    =        -3595764
00  meter
 Z    =      -16962978
02                 Z    =        -5157826
10
 XDOT =      15983
893698                 XDOT =        4815
757799
 YDOT =      18622
702457  feet/sec       YDOT =        5730
366635  meter/sec
 ZDOT =      -5202
237961                 ZDOT =       -1562
113666

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4992767
08                 X    =        -1521795
40
 Y    =       13703433
71  feet           Y    =         4176806
60  meter
 Z    =      -16905418
28                 Z    =        -5152771
49
 XDOT =     -19378
709144                 XDOT =       -5906
630547
 YDOT =     -13352
203426  feet/sec       YDOT =       -4069
751604  meter/sec
 ZDOT =      -5094
581296                 ZDOT =       -1552
828379


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   20082
06398687  
00016717  00000-0  10270-3 0  9073
2 25544  51
6417  59
5446 0004686  44
2158 315
9365 15
48909741 18501


Satellite: ISS
Catalog Number: 25544
Epoch time:      20082
06398687   =   yrday
fracday
Element set:     907
Inclination:       51
6417  deg
RA of node:        59
5446  deg
Eccentricity:     
0004686     
Arg of perigee:    44
2158  deg
Mean anomaly:     315
9365  deg
Mean motion:   15
48909741  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1850
Checksum:              338


Coasting Arc #9 (Orbit 1865)
---------------------------------------

Vector Time (GMT): 2020/083/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2187910
62                 A    =         6793352
34  meter
 Y    =        3845648
18  meter          E    =           
0007390
 Z    =        5148505
13                 I    =           51
94096
 XDOT =      -5368
329597                 Wp   =           86
93257
 YDOT =      -5226
270866  meter/sec      RA   =           53
98329  deg
 ZDOT =       1620
789635                 TA   =          347
48102
                                          MA   =          347
49937
                                          Ha   =            230
749  n
mi
                                          Hp   =            221
539

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7178184
44                 X    =        -2255759
38
 Y    =       12616955
97  feet           Y    =         3820802
61  meter
 Z    =       16891421
03                 Z    =         5137712
03
 XDOT =     -17612
629913                 XDOT =       -5317
361688
 YDOT =     -17146
557959  feet/sec       YDOT =       -5286
018186  meter/sec
 ZDOT =       5317
551295                 ZDOT =        1594
837074

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3448386
99                 X    =         1051068
36
 Y    =      -14159874
63  feet           Y    =        -4315929
79  meter
 Z    =       16841632
70                 Z    =         5133329
65
 XDOT =      20726
733074                 XDOT =        6317
508241
 YDOT =      11237
313050  feet/sec       YDOT =        3425
133018  meter/sec
 ZDOT =       5198
752746                 ZDOT =        1584
579837


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   20083
09629534  
00016717  00000-0  10270-3 0  9086
2 25544  51
6421  54
4381 0004626  47
0147 313
1390 15
48930171 18667


Satellite: ISS
Catalog Number: 25544
Epoch time:      20083
09629534   =   yrday
fracday
Element set:     908
Inclination:       51
6421  deg
RA of node:        54
4381  deg
Eccentricity:     
0004626     
Arg of perigee:    47
0147  deg
Mean anomaly:     313
1390  deg
Mean motion:   15
48930171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1866
Checksum:              297


Coasting Arc #10 (Orbit 1880)
---------------------------------------

Vector Time (GMT): 2020/084/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1829172
62                 A    =         6793467
74  meter
 Y    =       -4052321
62  meter          E    =           
0017813
 Z    =       -5152504
11                 I    =           51
92036
 XDOT =       5793
834111                 Wp   =           70
75861
 YDOT =       4710
213790  meter/sec      RA   =           49
05955  deg
 ZDOT =      -1646
566062                 TA   =          183
35860
                                          MA   =          183
37057
                                          Ha   =            230
756  n
mi
                                          Hp   =            221
545

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6001222
51                 X    =         1899378
66
 Y    =      -13295018
43  feet           Y    =        -4031474
55  meter
 Z    =      -16904541
04                 Z    =        -5143447
79
 XDOT =      19008
642096                 XDOT =        5748
730517
 YDOT =      15453
457316  feet/sec       YDOT =        4774
752186  meter/sec
 ZDOT =      -5402
119626                 ZDOT =       -1618
532192

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1878932
89                 X    =         -572698
74
 Y    =       14513936
83  feet           Y    =         4423847
95  meter
 Z    =      -16862708
66                 Z    =        -5139753
60
 XDOT =     -21724
312919                 XDOT =       -6621
570578
 YDOT =      -8943
596859  feet/sec       YDOT =       -2726
008323  meter/sec
 ZDOT =      -5273
750474                 ZDOT =       -1607
439145


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   20084
06408546  
00016717  00000-0  10270-3 0  9093
2 25544  51
6420  49
6527 0004698  51
4204 308
7366 15
48905772 18815


Satellite: ISS
Catalog Number: 25544
Epoch time:      20084
06408546   =   yrday
fracday
Element set:     909
Inclination:       51
6420  deg
RA of node:        49
6527  deg
Eccentricity:     
0004698     
Arg of perigee:    51
4204  deg
Mean anomaly:     308
7366  deg
Mean motion:   15
48905772  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1881
Checksum:              322


Coasting Arc #11 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2020/085/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1442543
00                 A    =         6793382
72  meter
 Y    =        4205160
50  meter          E    =           
0007829
 Z    =        5129994
46                 I    =           51
89856
 XDOT =      -6201
673502                 Wp   =           91
28931
 YDOT =      -4180
582718  meter/sec      RA   =           44
13278  deg
 ZDOT =       1680
628213                 TA   =          342
52018
                                          MA   =          342
54711
                                          Ha   =            230
762  n
mi
                                          Hp   =            221
426

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4732752
62                 X    =        -1514377
63
 Y    =       13796458
33  feet           Y    =         4188627
88  meter
 Z    =       16830690
47                 Z    =         5122812
23
 XDOT =     -20346
697842                 XDOT =       -6162
627576
 YDOT =     -13715
822566  feet/sec       YDOT =       -4249
715735  meter/sec
 ZDOT =       5513
872089                 ZDOT =        1650
598318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         266768
15                 X    =           81310
93
 Y    =      -14621491
05  feet           Y    =        -4456630
47  meter
 Z    =       16797445
81                 Z    =         5119861
48
 XDOT =      22594
377277                 XDOT =        6886
766194
 YDOT =       6597
657454  feet/sec       YDOT =        2010
965992  meter/sec
 ZDOT =       5376
324333                 ZDOT =        1638
703657


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   20085
09639090  
00016717  00000-0  10270-3 0  9109
2 25544  51
6430  44
5466 0004560  54
6332 305
5243 15
48939559 18973


Satellite: ISS
Catalog Number: 25544
Epoch time:      20085
09639090   =   yrday
fracday
Element set:     910
Inclination:       51
6430  deg
RA of node:        44
5466  deg
Eccentricity:     
0004560     
Arg of perigee:    54
6332  deg
Mean anomaly:     305
5243  deg
Mean motion:   15
48939559  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1897
Checksum:              316


Coasting Arc #12 (Orbit 1903)
---------------------------------------

Vector Time (GMT): 2020/085/12:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         574514
97                 A    =         6794379
68  meter
 Y    =       -4664039
86  meter          E    =           
0016799
 Z    =       -4922954
92                 I    =           51
88913
 XDOT =       6480
337030                 Wp   =           66
55538
 YDOT =       3297
054636  meter/sec      RA   =           41
76289  deg
 ZDOT =      -2367
302966                 TA   =          180
27338
                                          MA   =          180
27430
                                          Ha   =            230
863  n
mi
                                          Hp   =            221
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1884891
65                 X    =          650539
82
 Y    =      -15301968
06  feet           Y    =        -4657190
68  meter
 Z    =      -16151426
90                 Z    =        -4919979
00
 XDOT =      21260
948262                 XDOT =        6454
485751
 YDOT =      10817
108387  feet/sec       YDOT =        3369
377573  meter/sec
 ZDOT =      -7766
742013                 ZDOT =       -2335
887216

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1374695
73                 X    =         -419007
26
 Y    =      -15370895
66  feet           Y    =        -4685049
00  meter
 Z    =      -16137453
70                 Z    =        -4918695
89
 XDOT =      22032
064915                 XDOT =        6715
373386
 YDOT =       6032
792286  feet/sec       YDOT =        1838
795089  meter/sec
 ZDOT =      -7622
783076                 ZDOT =       -2323
424282


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   20085
54802571  
00016717  00000-0  10270-3 0  9116
2 25544  51
6423  42
3165 0005019  51
9271 308
2331 15
48912442 19048


Satellite: ISS
Catalog Number: 25544
Epoch time:      20085
54802571   =   yrday
fracday
Element set:     911
Inclination:       51
6423  deg
RA of node:        42
3165  deg
Eccentricity:     
0005019     
Arg of perigee:    51
9271  deg
Mean anomaly:     308
2331  deg
Mean motion:   15
48912442  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1904
Checksum:              278


Coasting Arc #13 (Orbit 1919)
---------------------------------------

Vector Time (GMT): 2020/086/12:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -139672
55                 A    =         6794305
91  meter
 Y    =        4699080
78  meter          E    =           
0009828
 Z    =        4897020
53                 I    =           51
86406
 XDOT =      -6758
420438                 Wp   =           93
39148
 YDOT =      -2707
524116  meter/sec      RA   =           36
83498  deg
 ZDOT =       2400
604125                 TA   =          333
12214
                                          MA   =          333
17302
                                          Ha   =            230
828  n
mi
                                          Hp   =            221
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -458243
29                 X    =         -215995
67
 Y    =       15416931
70  feet           Y    =         4697092
60  meter
 Z    =       16066340
33                 Z    =         4896156
22
 XDOT =     -22173
295399                 XDOT =       -6739
302597
 YDOT =      -8882
953135  feet/sec       YDOT =       -2782
994449  meter/sec
 ZDOT =       7875
997786                 ZDOT =        2367
820986

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3053403
06                 X    =          930677
25
 Y    =       15123042
44  feet           Y    =         4609503
34  meter
 Z    =       16062047
77                 Z    =         4895712
16
 XDOT =     -22584
272192                 XDOT =       -6883
686164
 YDOT =      -3662
026704  feet/sec       YDOT =       -1116
185739  meter/sec
 ZDOT =       7725
740575                 ZDOT =        2354
805727


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   20086
58032669  
00016717  00000-0  10270-3 0  9125
2 25544  51
6429  37
2117 0004907  54
7378 305
4230 15
48948256 19205


Satellite: ISS
Catalog Number: 25544
Epoch time:      20086
58032669   =   yrday
fracday
Element set:     912
Inclination:       51
6429  deg
RA of node:        37
2117  deg
Eccentricity:     
0004907     
Arg of perigee:    54
7378  deg
Mean anomaly:     305
4230  deg
Mean motion:   15
48948256  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1920
Checksum:              314


Coasting Arc #14 (Orbit 1934)
---------------------------------------

Vector Time (GMT): 2020/087/12:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -285326
77                 A    =         6794417
78  meter
 Y    =       -4714264
04  meter          E    =           
0016970
 Z    =       -4900525
87                 I    =           51
83643
 XDOT =       6947
568334                 Wp   =           68
04884
 YDOT =       2089
455457  meter/sec      RA   =           31
90438  deg
 ZDOT =      -2415
096852                 TA   =          178
26869
                                          MA   =          178
26280
                                          Ha   =            230
960  n
mi
                                          Hp   =            221
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -936111
45                 X    =         -208785
19
 Y    =      -15466745
55  feet           Y    =        -4717027
21  meter
 Z    =      -16077840
77                 Z    =        -4901725
58
 XDOT =      22793
859363                 XDOT =        6935
418291
 YDOT =       6855
168822  feet/sec       YDOT =        2167
079970  meter/sec
 ZDOT =      -7923
546101                 ZDOT =       -2381
377792

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4675353
79                 X    =        -1425047
84
 Y    =      -14767238
74  feet           Y    =        -4501054
37  meter
 Z    =      -16083010
08                 Z    =        -4902101
47
 XDOT =      22758
969183                 XDOT =        6936
933807
 YDOT =       1253
678770  feet/sec       YDOT =         382
121289  meter/sec
 ZDOT =      -7768
966990                 ZDOT =       -2367
981139


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   20087
54811012  
00016717  00000-0  10270-3 0  9130
2 25544  51
6428  32
4252 0005172  58
2932 301
8721 15
48922869 19354


Satellite: ISS
Catalog Number: 25544
Epoch time:      20087
54811012   =   yrday
fracday
Element set:     913
Inclination:       51
6428  deg
RA of node:        32
4252  deg
Eccentricity:     
0005172     
Arg of perigee:    58
2932  deg
Mean anomaly:     301
8721  deg
Mean motion:   15
48922869  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1935
Checksum:              298


Coasting Arc #15 (Orbit 1950)
---------------------------------------

Vector Time (GMT): 2020/088/12:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         720531
89                 A    =         6794379
11  meter
 Y    =        4669400
87  meter          E    =           
0010336
 Z    =        4874287
04                 I    =           51
80757
 XDOT =      -7116
631301                 Wp   =           96
23633
 YDOT =      -1461
929565  meter/sec      RA   =           26
97322  deg
 ZDOT =       2446
930142                 TA   =          329
77275
                                          MA   =          329
83234
                                          Ha   =            230
865  n
mi
                                          Hp   =            221
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2363949
77                 X    =          644587
06
 Y    =       15319556
67  feet           Y    =         4677034
06  meter
 Z    =       15991755
36                 Z    =         4877602
36
 XDOT =     -23348
527892                 XDOT =       -7111
640519
 YDOT =      -4796
356839  feet/sec       YDOT =       -1541
484732  meter/sec
 ZDOT =       8027
986031                 ZDOT =        2412
372318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6265842
10                 X    =         1909828
67
 Y    =       14161230
39  feet           Y    =         4316343
02  meter
 Z    =       16006626
48                 Z    =         4878819
75
 XDOT =     -22800
554606                 XDOT =       -6949
609044
 YDOT =       1172
840881  feet/sec       YDOT =         357
481900  meter/sec
 ZDOT =       7869
527428                 ZDOT =        2398
631960


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   20088
58040815  
00016717  00000-0  10270-3 0  9141
2 25544  51
6428  27
3208 0004915  62
1442 298
0205 15
48947090 19517


Satellite: ISS
Catalog Number: 25544
Epoch time:      20088
58040815   =   yrday
fracday
Element set:     914
Inclination:       51
6428  deg
RA of node:        27
3208  deg
Eccentricity:     
0004915     
Arg of perigee:    62
1442  deg
Mean anomaly:     298
0205  deg
Mean motion:   15
48947090  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1951
Checksum:              302


Coasting Arc #16 (Orbit 1959)
---------------------------------------

Vector Time (GMT): 2020/089/03:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1223315
92                 A    =         6794880
56  meter
 Y    =       -4672956
73  meter          E    =           
0016042
 Z    =       -4794241
97                 I    =           51
79051
 XDOT =       7115
667533                 Wp   =           69
90006
 YDOT =        867
173575  meter/sec      RA   =           23
95079  deg
 ZDOT =      -2662
777333                 TA   =          173
80408
                                          MA   =          173
78421
                                          Ha   =            230
912  n
mi
                                          Hp   =            221
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4013503
66                 X    =        -1147682
77
 Y    =      -15331222
87  feet           Y    =        -4686214
08  meter
 Z    =      -15729140
32                 Z    =        -4800000
45
 XDOT =      23345
365921                 XDOT =        7118
376029
 YDOT =       2845
057661  feet/sec       YDOT =         946
761030  meter/sec
 ZDOT =      -8736
146105                 ZDOT =       -2628
205438

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14950181
74                 X    =         4556815
40
 Y    =        5179354
09  feet           Y    =         1578667
13  meter
 Z    =      -15755215
59                 Z    =        -4802189
71
 XDOT =     -14881
594571                 XDOT =       -4535
910025
 YDOT =      16882
019624  feet/sec       YDOT =        5145
639581  meter/sec
 ZDOT =      -8577
586797                 ZDOT =       -2614
448456


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   20089
16107565  
00016717  00000-0  10270-3 0  9153
2 25544  51
6431  24
4474 0004768  67
5070 292
6584 15
48903006 19605


Satellite: ISS
Catalog Number: 25544
Epoch time:      20089
16107565   =   yrday
fracday
Element set:     915
Inclination:       51
6431  deg
RA of node:        24
4474  deg
Eccentricity:     
0004768     
Arg of perigee:    67
5070  deg
Mean anomaly:     292
6584  deg
Mean motion:   15
48903006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1960
Checksum:              312


Coasting Arc #17 (Orbit 1975)
---------------------------------------

Vector Time (GMT): 2020/090/03:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1649451
78                 A    =         6794815
73  meter
 Y    =        4542421
22  meter          E    =           
0011311
 Z    =        4767637
34                 I    =           51
76009
 XDOT =      -7174
240775                 Wp   =           99
05169
 YDOT =       -228
238595  meter/sec      RA   =           19
01496  deg
 ZDOT =       2692
327865                 TA   =          324
35026
                                          MA   =          324
42575
                                          Ha   =            230
871  n
mi
                                          Hp   =            221
154

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5411587
20                 X    =         1575375
91
 Y    =       14902956
76  feet           Y    =         4560452
55  meter
 Z    =       15641854
80                 Z    =         4775469
70
 XDOT =     -23537
535351                 XDOT =       -7184
233202
 YDOT =       -748
814288  feet/sec       YDOT =        -308
521830  meter/sec
 ZDOT =       8833
096669                 ZDOT =        2657
453757

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15425319
54                 X    =        -4701637
40
 Y    =       -3511154
32  feet           Y    =        -1070199
84  meter
 Z    =       15677446
54                 Z    =         4778485
70
 XDOT =      13025
627127                 XDOT =        3970
211148
 YDOT =     -18393
733046  feet/sec       YDOT =       -5606
409832  meter/sec
 ZDOT =       8673
113229                 ZDOT =        2643
564912


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   20090
19336858  
00016717  00000-0  10270-3 0  9168
2 25544  51
6436  19
3417 0004845  69
7582 290
4089 15
48938201 19766


Satellite: ISS
Catalog Number: 25544
Epoch time:      20090
19336858   =   yrday
fracday
Element set:     916
Inclination:       51
6436  deg
RA of node:        19
3417  deg
Eccentricity:     
0004845     
Arg of perigee:    69
7582  deg
Mean anomaly:     290
4089  deg
Mean motion:   15
48938201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1976
Checksum:              338


Coasting Arc #18 (Orbit 1990)
---------------------------------------

Vector Time (GMT): 2020/091/03:22:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2048771
68                 A    =         6794899
26  meter
 Y    =       -4396775
65  meter          E    =           
0016199
 Z    =       -4773858
74                 I    =           51
72777
 XDOT =       7143
891486                 Wp   =           71
50393
 YDOT =       -402
727267  meter/sec      RA   =           14
07727  deg
 ZDOT =      -2697
510191                 TA   =          171
80832
                                          MA   =          171
78184
                                          Ha   =            231
008  n
mi
                                          Hp   =            221
042

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6721691
86                 X    =        -1976264
62
 Y    =      -14425116
95  feet           Y    =        -4419281
17  meter
 Z    =      -15662266
21                 Z    =        -4783634
69
 XDOT =      23437
964194                 XDOT =        7160
966952
 YDOT =      -1321
283685  feet/sec       YDOT =        -322
743781  meter/sec
 ZDOT =      -8850
099051                 ZDOT =       -2662
766384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15758820
44                 X    =         4803288
47
 Y    =        1878401
24  feet           Y    =          572536
70  meter
 Z    =      -15706779
13                 Z    =        -4787426
28
 XDOT =     -10988
780087                 XDOT =       -3349
380171
 YDOT =      19589
652173  feet/sec       YDOT =        5970
925982  meter/sec
 ZDOT =      -8690
673635                 ZDOT =       -2648
917324


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   20091
16114263  
00016717  00000-0  10270-3 0  9171
2 25544  51
6434  14
5556 0005011  73
3228 286
8472 15
48916906 19919


Satellite: ISS
Catalog Number: 25544
Epoch time:      20091
16114263   =   yrday
fracday
Element set:     917
Inclination:       51
6434  deg
RA of node:        14
5556  deg
Eccentricity:     
0005011     
Arg of perigee:    73
3228  deg
Mean anomaly:     286
8472  deg
Mean motion:   15
48916906  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1991
Checksum:              304
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