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

 
Date: April 5th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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


094/11:01:35 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 216 8

094/14:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 224 0
000/00:00:00 000 0 0 0 0 216 9

097/20:12:00 000 0 0 0 0 0 0
N/A 0 0 0 0 223 9
000/00:00:00 000 0 0 0 0 216 8

107/20:46:01 000 0 0 0 0 0 0
N/A 0 0 0 0 223 3
000/00:00:00 000 0 0 0 0 217 3

Coasting Arc #1 (Orbit 364)
---------------------------------------

Vector Time (GMT): 2019/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1664468
49                 A    =         6782259
66  meter
 Y    =        3911241
95  meter          E    =           
0003873
 Z    =        5281650
08                 I    =           51
70452
 XDOT =      -7330
096425                 Wp   =           85
82542
 YDOT =      -2134
018705  meter/sec      RA   =           11
90788  deg
 ZDOT =       -728
969911                 TA   =           11
13519
                                          MA   =           11
12662
                                          Ha   =            224
037  n
mi
                                          Hp   =            216
807

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5460854
63                 X    =        -1733736
69
 Y    =       12832158
63  feet           Y    =         3892241
98  meter
 Z    =       17328248
29                 Z    =         5273396
05
 XDOT =     -24048
872785                 XDOT =       -7302
147510
 YDOT =      -7001
373704  feet/sec       YDOT =       -2215
832783  meter/sec
 ZDOT =      -2391
633566                 ZDOT =        -764
508591

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3110058
60                 X    =         -947945
86
 Y    =       13642628
14  feet           Y    =         4158273
06  meter
 Z    =       17290449
68                 Z    =         5270129
06
 XDOT =     -23917
270316                 XDOT =       -7289
983992
 YDOT =      -2214
704361  feet/sec       YDOT =        -675
041889  meter/sec
 ZDOT =      -2552
153650                 ZDOT =        -777
896433


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   19093
54697014  
00016717  00000-0  10270-3 0  9005
2 25544  51
6419  12
2716 0001658 140
2742 219
8532 15
52510467  3657


Satellite: ISS
Catalog Number: 25544
Epoch time:      19093
54697014   =   yrday
fracday
Element set:     900
Inclination:       51
6419  deg
RA of node:        12
2716  deg
Eccentricity:     
0001658     
Arg of perigee:   140
2742  deg
Mean anomaly:     219
8532  deg
Mean motion:   15
52510467  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             365
Checksum:              296


Coasting Arc #2 (Orbit 379)
---------------------------------------

Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2627020
53                 A    =         6784514
14  meter
 Y    =        4093982
76  meter          E    =           
0009281
 Z    =        4724896
39                 I    =           51
68018
 XDOT =      -7032
151217                 Wp   =          122
40966
 YDOT =       1315
163271  meter/sec      RA   =            7
16867  deg
 ZDOT =       2761
471637                 TA   =          300
22265
                                          MA   =          300
31451
                                          Ha   =            223
898  n
mi
                                          Hp   =            216
836

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8618833
76                 X    =         2558094
23
 Y    =       13431701
96  feet           Y    =         4122975
07  meter
 Z    =       15501628
57                 Z    =         4737489
63
 XDOT =     -23071
362259                 XDOT =       -7059
748830
 YDOT =       4314
840127  feet/sec       YDOT =        1236
370832  meter/sec
 ZDOT =       9059
946316                 ZDOT =        2727
244835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7797006
93                 X    =         2376527
71
 Y    =       13861719
24  feet           Y    =         4225052
03  meter
 Z    =       15558111
19                 Z    =         4742112
29
 XDOT =     -22315
553418                 XDOT =       -6801
780682
 YDOT =       2525
035250  feet/sec       YDOT =         769
630744  meter/sec
 ZDOT =       8904
970951                 ZDOT =        2714
235146


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   19094
51252585  
00016717  00000-0  10270-3 0  9014
2 25544  51
6413   7
4704 0001757 146
9794 213
1468 15
52508377  3803


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
51252585   =   yrday
fracday
Element set:     901
Inclination:       51
6413  deg
RA of node:         7
4704  deg
Eccentricity:     
0001757     
Arg of perigee:   146
9794  deg
Mean anomaly:     213
1468  deg
Mean motion:   15
52508377  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             380
Checksum:              311


Coasting Arc #3 (Orbit 381)
---------------------------------------

Vector Time (GMT): 2019/094/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4924857
01                 A    =         6787662
19  meter
 Y    =        2549587
65  meter          E    =           
0012082
 Z    =        3903755
25                 I    =           51
68738
 XDOT =      -5234
609849                 Wp   =           87
57817
 YDOT =      -3837
820362  meter/sec      RA   =            6
42150  deg
 ZDOT =      -4085
877069                 TA   =           45
23239
                                          MA   =           45
13416
                                          Ha   =            224
022  n
mi
                                          Hp   =            216
859

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16157667
35                 X    =        -4971963
53
 Y    =        8364788
89  feet           Y    =         2494251
50  meter
 Z    =       12807595
96                 Z    =         3879717
38
 XDOT =     -17173
916826                 XDOT =       -5171
458225
 YDOT =     -12591
274153  feet/sec       YDOT =       -3896
004784  meter/sec
 ZDOT =     -13405
108494                 ZDOT =       -4111
151100

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4657913
53                 X    =        -1419732
04
 Y    =       17667051
26  feet           Y    =         5384917
22  meter
 Z    =       12698565
38                 Z    =         3870522
73
 XDOT =     -19502
232770                 XDOT =       -5944
280548
 YDOT =       4602
454504  feet/sec       YDOT =        1402
828133  meter/sec
 ZDOT =     -13518
979245                 ZDOT =       -4120
584874


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   19094
64126569  
00016717  00000-0  10270-3 0  9021
2 25544  51
6429   6
8311 0001568 143
6272 216
4987 15
52520180  3822


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
64126569   =   yrday
fracday
Element set:     902
Inclination:       51
6429  deg
RA of node:         6
8311  deg
Eccentricity:     
0001568     
Arg of perigee:   143
6272  deg
Mean anomaly:     216
4987  deg
Mean motion:   15
52520180  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             382
Checksum:              307


Coasting Arc #4 (Orbit 396)
---------------------------------------

Vector Time (GMT): 2019/095/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5644645
16                 A    =         6790311
93  meter
 Y    =       -2254533
32  meter          E    =           
0004920
 Z    =       -3030948
85                 I    =           51
66270
 XDOT =       4254
697605                 Wp   =           86
18059
 YDOT =       4017
674289  meter/sec      RA   =            1
45264  deg
 ZDOT =       4942
430716                 TA   =          239
14395
                                          MA   =          239
19235
                                          Ha   =            223
906  n
mi
                                          Hp   =            217
056

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18519177
02                 X    =         5684159
24
 Y    =       -7396762
86  feet           Y    =        -2191190
32  meter
 Z    =       -9944057
91                 Z    =        -3003432
89
 XDOT =      13958
981644                 XDOT =        4185
446862
 YDOT =      13181
346093  feet/sec       YDOT =        4064
866605  meter/sec
 ZDOT =      16215
323870                 ZDOT =        4962
929965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6621395
77                 X    =         2018201
43
 Y    =      -18875750
44  feet           Y    =        -5753328
73  meter
 Z    =       -9819341
60                 Z    =        -2992935
32
 XDOT =      17659
999426                 XDOT =        5382
767825
 YDOT =      -2275
890705  feet/sec       YDOT =        -693
691487  meter/sec
 ZDOT =      16307
564764                 ZDOT =        4970
545740


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   19095
60681684  
00016717  00000-0  10270-3 0  9033
2 25544  51
6428   2
0298 0001503 153
1261 206
9969 15
52487679  3971


Satellite: ISS
Catalog Number: 25544
Epoch time:      19095
60681684   =   yrday
fracday
Element set:     903
Inclination:       51
6428  deg
RA of node:         2
0298  deg
Eccentricity:     
0001503     
Arg of perigee:   153
1261  deg
Mean anomaly:     206
9969  deg
Mean motion:   15
52487679  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             397
Checksum:              328


Coasting Arc #5 (Orbit 412)
---------------------------------------

Vector Time (GMT): 2019/096/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6191297
09                 A    =         6792473
35  meter
 Y    =        1947913
05  meter          E    =           
0015164
 Z    =        1976854
41                 I    =           51
63688
 XDOT =      -3122
400182                 Wp   =          115
69273
 YDOT =      -4233
689598  meter/sec      RA   =          356
48594  deg
 ZDOT =      -5580
384004                 TA   =           42
49349
                                          MA   =           42
37620
                                          Ha   =            223
919  n
mi
                                          Hp   =            216
968

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20312654
49                 X    =        -6222221
62
 Y    =        6390790
86  feet           Y    =         1878504
91  meter
 Z    =        6485742
82                 Z    =         1946703
81
 XDOT =     -10244
095084                 XDOT =       -3047
719109
 YDOT =     -13890
057736  feet/sec       YDOT =       -4268
189403  meter/sec
 ZDOT =     -18308
346470                 ZDOT =       -5595
369835

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8205034
22                 X    =        -2500894
43
 Y    =       19694582
79  feet           Y    =         6002908
83  meter
 Z    =        6349159
20                 Z    =         1935223
72
 XDOT =     -15710
004522                 XDOT =       -4788
409378
 YDOT =       -591
955781  feet/sec       YDOT =        -180
428122  meter/sec
 ZDOT =     -18375
617244                 ZDOT =       -5600
888136


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   19096
63673259  
00016717  00000-0  10270-3 0  9047
2 25544  51
6429 356
9080 0001531 151
2104 208
9132 15
52504266  4133


Satellite: ISS
Catalog Number: 25544
Epoch time:      19096
63673259   =   yrday
fracday
Element set:     904
Inclination:       51
6429  deg
RA of node:       356
9080  deg
Eccentricity:     
0001531     
Arg of perigee:   151
2104  deg
Mean anomaly:     208
9132  deg
Mean motion:   15
52504266  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             413
Checksum:              294


Coasting Arc #6 (Orbit 427)
---------------------------------------

Vector Time (GMT): 2019/097/14:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6527246
18                 A    =         6793778
84  meter
 Y    =       -1661925
63  meter          E    =           
0009624
 Z    =        -859691
15                 I    =           51
60623
 XDOT =       1911
252360                 Wp   =           46
93696
 YDOT =       4464
790397  meter/sec      RA   =          351
52008  deg
 ZDOT =       5928
495122                 TA   =          303
76674
                                          MA   =          303
85838
                                          Ha   =            223
850  n
mi
                                          Hp   =            217
002

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21414849
67                 X    =         6549521
14
 Y    =       -5452511
93  feet           Y    =        -1588808
92  meter
 Z    =       -2820509
01                 Z    =         -827929
60
 XDOT =       6270
512991                 XDOT =        1832
386048
 YDOT =      14648
262457  feet/sec       YDOT =        4485
722824  meter/sec
 ZDOT =      19450
443313                 ZDOT =        5937
587506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9272857
27                 X    =         2826366
89
 Y    =      -20078107
86  feet           Y    =        -6119807
28  meter
 Z    =       -2676685
78                 Z    =         -815853
82
 XDOT =      13779
944071                 XDOT =        4200
126953
 YDOT =       3788
005265  feet/sec       YDOT =        1154
584005  meter/sec
 ZDOT =      19491
028801                 ZDOT =        5940
865579


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   19097
60227418  
00016717  00000-0  10270-3 0  9058
2 25544  51
6410 352
1064 0001489 157
6035 202
5182 15
52500824  4285


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
60227418   =   yrday
fracday
Element set:     905
Inclination:       51
6410  deg
RA of node:       352
1064  deg
Eccentricity:     
0001489     
Arg of perigee:   157
6035  deg
Mean anomaly:     202
5182  deg
Mean motion:   15
52500824  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             428
Checksum:              287


Coasting Arc #7 (Orbit 431)
---------------------------------------

Vector Time (GMT): 2019/097/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2026801
58                 A    =         6782494
60  meter
 Y    =       -3852695
84  meter          E    =           
0014689
 Z    =       -5213838
59                 I    =           51
56053
 XDOT =       7235
996020                 Wp   =           88
79754
 YDOT =      -2193
936852  meter/sec      RA   =          350
33486  deg
 ZDOT =      -1194
320843                 TA   =          169
72795
                                          MA   =          169
69790
                                          Ha   =            223
901  n
mi
                                          Hp   =            216
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6649611
50                 X    =        -1958242
74
 Y    =      -12640078
22  feet           Y    =        -3874977
98  meter
 Z    =      -17105769
64                 Z    =        -5223517
38
 XDOT =      23740
144424                 XDOT =        7265
792875
 YDOT =      -7197
955551  feet/sec       YDOT =       -2112
852357  meter/sec
 ZDOT =      -3918
375470                 ZDOT =       -1159
098103

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3620316
91                 X    =        -1103472
60
 Y    =       13762219
17  feet           Y    =         4194724
40  meter
 Z    =      -17149078
53                 Z    =        -5227039
14
 XDOT =     -21460
566006                 XDOT =       -6541
180519
 YDOT =     -10318
676397  feet/sec       YDOT =       -3145
132566  meter/sec
 ZDOT =      -3758
840330                 ZDOT =       -1145
694533


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   19097
85975298  
00016717  00000-0  10270-3 0  9062
2 25544  51
6407 350
8223 0002093 161
3015 198
8214 15
52514494  4321


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
85975298   =   yrday
fracday
Element set:     906
Inclination:       51
6407  deg
RA of node:       350
8223  deg
Eccentricity:     
0002093     
Arg of perigee:   161
3015  deg
Mean anomaly:     198
8214  deg
Mean motion:   15
52514494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             432
Checksum:              317


Coasting Arc #8 (Orbit 447)
---------------------------------------

Vector Time (GMT): 2019/098/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         928039
14                 A    =         6782021
56  meter
 Y    =        4116347
66  meter          E    =           
0003292
 Z    =        5306918
24                 I    =           51
52707
 XDOT =      -7443
176026                 Wp   =          118
71135
 YDOT =       1841
249895  meter/sec      RA   =          345
34502  deg
 ZDOT =       -128
052951                 TA   =          332
50208
                                          MA   =          332
51950
                                          Ha   =            223
762  n
mi
                                          Hp   =            216
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3044747
84                 X    =          856161
58
 Y    =       13505077
61  feet           Y    =         4126324
00  meter
 Z    =       17411149
08                 Z    =         5311251
59
 XDOT =     -24419
868853                 XDOT =       -7462
590194
 YDOT =       6040
846113  feet/sec       YDOT =        1757
906535  meter/sec
 ZDOT =       -420
121231                 ZDOT =        -164
256844

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6669982
44                 X    =         2033010
65
 Y    =      -12103857
03  feet           Y    =        -3689255
62  meter
 Z    =       17430252
50                 Z    =         5312740
96
 XDOT =      21489
910067                 XDOT =        6550
124588
 YDOT =      11008
259081  feet/sec       YDOT =        3355
317368  meter/sec
 ZDOT =       -584
040270                 ZDOT =        -178
015474


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   19098
88965932  
00016717  00000-0  10270-3 0  9071
2 25544  51
6414 345
6999 0002011 167
3732 192
7471 15
52527185  4489


Satellite: ISS
Catalog Number: 25544
Epoch time:      19098
88965932   =   yrday
fracday
Element set:     907
Inclination:       51
6414  deg
RA of node:       345
6999  deg
Eccentricity:     
0002011     
Arg of perigee:   167
3732  deg
Mean anomaly:     192
7471  deg
Mean motion:   15
52527185  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             448
Checksum:              344


Coasting Arc #9 (Orbit 462)
---------------------------------------

Vector Time (GMT): 2019/099/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         169088
39                 A    =         6782734
56  meter
 Y    =       -4416897
64  meter          E    =           
0014651
 Z    =       -5157757
21                 I    =           51
49806
 XDOT =       7382
632548                 Wp   =          108
16103
 YDOT =      -1411
162598  meter/sec      RA   =          340
35464  deg
 ZDOT =       1449
419343                 TA   =          175
84684
                                          MA   =          175
83467
                                          Ha   =            223
793  n
mi
                                          Hp   =            216
947

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         554751
94                 X    =          243520
65
 Y    =      -14491134
01  feet           Y    =        -4414590
74  meter
 Z    =      -16921775
62                 Z    =        -5156754
93
 XDOT =      24221
235393                 XDOT =        7390
823315
 YDOT =      -4629
798549  feet/sec       YDOT =       -1328
558999  meter/sec
 ZDOT =       4755
312805                 ZDOT =        1485
301772

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9846574
42                 X    =        -3001235
88
 Y    =       10654428
14  feet           Y    =         3247469
70  meter
 Z    =      -16916717
70                 Z    =        -5156215
56
 XDOT =     -20706
733596                 XDOT =       -6311
412400
 YDOT =     -11322
922674  feet/sec       YDOT =       -3451
226831  meter/sec
 ZDOT =       4917
718473                 ZDOT =        1498
920590


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   19099
85519314  
00016717  00000-0  10270-3 0  9089
2 25544  51
6419 340
8993 0002029 166
9290 193
1915 15
52539044  4630


Satellite: ISS
Catalog Number: 25544
Epoch time:      19099
85519314   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:       340
8993  deg
Eccentricity:     
0002029     
Arg of perigee:   166
9290  deg
Mean anomaly:     193
1915  deg
Mean motion:   15
52539044  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              333


Coasting Arc #10 (Orbit 478)
---------------------------------------

Vector Time (GMT): 2019/100/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1211526
24                 A    =         6784588
85  meter
 Y    =        4701707
03  meter          E    =           
0007541
 Z    =        4733201
38                 I    =           51
47252
 XDOT =      -7120
068758                 Wp   =           77
37806
 YDOT =        894
878259  meter/sec      RA   =          335
36328  deg
 ZDOT =      -2706
138195                 TA   =           39
45955
                                          MA   =           39
40465
                                          Ha   =            223
855  n
mi
                                          Hp   =            217
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3974823
61                 X    =        -1287003
49
 Y    =       15425548
00  feet           Y    =         4687736
93  meter
 Z    =       15528875
92                 Z    =         4727132
81
 XDOT =     -23359
805635                 XDOT =       -7116
401327
 YDOT =       2935
952294  feet/sec       YDOT =         815
277146  meter/sec
 ZDOT =      -8878
406150                 ZDOT =       -2740
716232

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12897482
32                 X    =         3931152
61
 Y    =       -9395233
02  feet           Y    =        -2863667
03  meter
 Z    =       15500880
21                 Z    =         4724668
29
 XDOT =      19243
888755                 XDOT =        5865
537292
 YDOT =      11482
581814  feet/sec       YDOT =        3499
890937  meter/sec
 ZDOT =      -9034
846314                 ZDOT =       -2753
821156


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   19100
88509320  
00016717  00000-0  10270-3 0  9092
2 25544  51
6415 335
7774 0002022 167
8318 192
2883 15
52505429  4791


Satellite: ISS
Catalog Number: 25544
Epoch time:      19100
88509320   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       335
7774  deg
Eccentricity:     
0002022     
Arg of perigee:   167
8318  deg
Mean anomaly:     192
2883  deg
Mean motion:   15
52505429  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             479
Checksum:              317


Coasting Arc #11 (Orbit 493)
---------------------------------------

Vector Time (GMT): 2019/101/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2149233
76                 A    =         6786945
09  meter
 Y    =       -4975337
54  meter          E    =           
0008217
 Z    =       -4094427
92                 I    =           51
45125
 XDOT =       6633
045477                 Wp   =          121
11198
 YDOT =       -273
867879  meter/sec      RA   =          330
37500  deg
 ZDOT =       3816
124842                 TA   =          188
46637
                                          MA   =          188
48024
                                          Ha   =            223
684  n
mi
                                          Hp   =            217
141

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7051291
88                 X    =         2224598
22
 Y    =      -16323285
90  feet           Y    =        -4950881
93  meter
 Z    =      -13433162
46                 Z    =        -4083804
63
 XDOT =      21761
960228                 XDOT =        6617
078260
 YDOT =       -898
516665  feet/sec       YDOT =        -199
781789  meter/sec
 ZDOT =      12520
094625                 ZDOT =        3848
307066

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15697020
52                 X    =        -4784451
85
 Y    =        8430758
20  feet           Y    =         2569695
10  meter
 Z    =      -13384546
93                 Z    =        -4079609
90
 XDOT =     -16990
730419                 XDOT =       -5178
774632
 YDOT =     -11534
903538  feet/sec       YDOT =       -3515
838598  meter/sec
 ZDOT =      12665
624744                 ZDOT =        3860
482422


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   19101
85062004  
00016717  00000-0  10270-3 0  9105
2 25544  51
6419 330
9768 0001981 177
0247 183
0917 15
52531020  4941


Satellite: ISS
Catalog Number: 25544
Epoch time:      19101
85062004   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       330
9768  deg
Eccentricity:     
0001981     
Arg of perigee:   177
0247  deg
Mean anomaly:     183
0917  deg
Mean motion:   15
52531020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             494
Checksum:              290


Coasting Arc #12 (Orbit 509)
---------------------------------------

Vector Time (GMT): 2019/102/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2969248
31                 A    =         6789650
44  meter
 Y    =        5175073
54  meter          E    =           
0013159
 Z    =        3226407
30                 I    =           51
43202
 XDOT =      -5998
694905                 Wp   =          101
69928
 YDOT =       -467
944310  meter/sec      RA   =          325
38865  deg
 ZDOT =      -4756
143076                 TA   =           40
82869
                                          MA   =           40
73017
                                          Ha   =            223
721  n
mi
                                          Hp   =            217
140

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9741628
30                 X    =        -3042568
88
 Y    =       16978587
72  feet           Y    =         5141459
39  meter
 Z    =       10585325
77                 Z    =         3211805
67
 XDOT =     -19680
757562                 XDOT =       -5969
913663
 YDOT =      -1535
250362  feet/sec       YDOT =        -534
865024  meter/sec
 ZDOT =     -15604
143950                 ZDOT =       -4785
212604

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18074458
98                 X    =         5509095
10
 Y    =       -7608651
71  feet           Y    =        -2319117
04  meter
 Z    =       10518708
86                 Z    =         3206102
46
 XDOT =      14121
059179                 XDOT =        4304
098838
 YDOT =      11727
695150  feet/sec       YDOT =        3574
601482  meter/sec
 ZDOT =     -15735
511322                 ZDOT =       -4796
183851


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   19102
88051317  
00016717  00000-0  10270-3 0  9115
2 25544  51
6421 325
8550 0001972 177
5375 182
5787 15
52522334  5109


Satellite: ISS
Catalog Number: 25544
Epoch time:      19102
88051317   =   yrday
fracday
Element set:     911
Inclination:       51
6421  deg
RA of node:       325
8550  deg
Eccentricity:     
0001972     
Arg of perigee:   177
5375  deg
Mean anomaly:     182
5787  deg
Mean motion:   15
52522334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             510
Checksum:              298


Coasting Arc #13 (Orbit 524)
---------------------------------------

Vector Time (GMT): 2019/103/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3621459
15                 A    =         6791986
53  meter
 Y    =       -5297555
23  meter          E    =           
0004921
 Z    =       -2223364
11                 I    =           51
41330
 XDOT =       5236
205399                 Wp   =           54
25225
 YDOT =       1301
391924  meter/sec      RA   =          320
40568  deg
 ZDOT =       5439
344710                 TA   =          280
98725
                                          MA   =          281
04261
                                          Ha   =            223
597  n
mi
                                          Hp   =            217
263

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11881427
67                 X    =         3691228
62
 Y    =      -17380430
55  feet           Y    =        -5256667
48  meter
 Z    =       -7294501
68                 Z    =        -2205602
88
 XDOT =      17179
151570                 XDOT =        5194
842435
 YDOT =       4269
658544  feet/sec       YDOT =        1359
715679  meter/sec
 ZDOT =      17845
619126                 ZDOT =        5464
679692

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19887636
17                 X    =        -6061751
51
 Y    =        6993095
03  feet           Y    =         2131495
36  meter
 Z    =       -7213597
83                 Z    =        -2198704
62
 XDOT =     -10742
847414                 XDOT =       -3274
419892
 YDOT =     -12063
920736  feet/sec       YDOT =       -3677
083040  meter/sec
 ZDOT =      17960
004898                 ZDOT =        5474
209493


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   19103
84603336  
00016717  00000-0  10270-3 0  9127
2 25544  51
6424 321
0540 0001673 185
2918 174
8216 15
52510617  5254


Satellite: ISS
Catalog Number: 25544
Epoch time:      19103
84603336   =   yrday
fracday
Element set:     912
Inclination:       51
6424  deg
RA of node:       321
0540  deg
Eccentricity:     
0001673     
Arg of perigee:   185
2918  deg
Mean anomaly:     174
8216  deg
Mean motion:   15
52510617  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             525
Checksum:              285


Coasting Arc #14 (Orbit 540)
---------------------------------------

Vector Time (GMT): 2019/104/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4129223
04                 A    =         6793517
85  meter
 Y    =        5275959
72  meter          E    =           
0014568
 Z    =        1077271
04                 I    =           51
39248
 XDOT =      -4402
317978                 Wp   =          129
69860
 YDOT =      -2238
673250  meter/sec      RA   =          315
42528  deg
 ZDOT =      -5866
472811                 TA   =           38
57979
                                          MA   =           38
47578
                                          Ha   =            223
566  n
mi
                                          Hp   =            217
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13547319
70                 X    =        -4193146
20
 Y    =       17309579
15  feet           Y    =         5229426
49  meter
 Z    =        3534353
81                 Z    =         1057057
41
 XDOT =     -14443
300452                 XDOT =       -4348
461322
 YDOT =      -7344
728512  feet/sec       YDOT =       -2287
602163  meter/sec
 ZDOT =     -19246
958040                 ZDOT =       -5887
726659

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21064502
21                 X    =         6420460
27
 Y    =       -6330862
86  feet           Y    =        -1929647
00  meter
 Z    =        3442380
02                 Z    =         1049237
43
 XDOT =       7006
493213                 XDOT =        2135
579131
 YDOT =      12714
661247  feet/sec       YDOT =        3875
428748  meter/sec
 ZDOT =     -19342
787586                 ZDOT =       -5895
681656


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   19104
87592110  
00016717  00000-0  10270-3 0  9139
2 25544  51
6412 315
9330 0001865 185
0607 175
0526 15
52529836  5414


Satellite: ISS
Catalog Number: 25544
Epoch time:      19104
87592110   =   yrday
fracday
Element set:     913
Inclination:       51
6412  deg
RA of node:       315
9330  deg
Eccentricity:     
0001865     
Arg of perigee:   185
0607  deg
Mean anomaly:     175
0526  deg
Mean motion:   15
52529836  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             541
Checksum:              297


Coasting Arc #15 (Orbit 556)
---------------------------------------

Vector Time (GMT): 2019/105/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4458765
66                 A    =         6793987
18  meter
 Y    =       -5119033
36  meter          E    =           
0011003
 Z    =          90791
35                 I    =           51
37140
 XDOT =       3551
683824                 Wp   =           51
28327
 YDOT =       3208
363612  meter/sec      RA   =          310
44407  deg
 ZDOT =       5987
000451                 TA   =          309
69758
                                          MA   =          309
79454
                                          Ha   =            223
495  n
mi
                                          Hp   =            217
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14628496
26                 X    =         4515235
75
 Y    =      -16794728
87  feet           Y    =        -5068856
57  meter
 Z    =         297871
88                 Z    =          112587
80
 XDOT =      11652
505983                 XDOT =        3486
461539
 YDOT =      10526
127335  feet/sec       YDOT =        3247
716716  meter/sec
 ZDOT =      19642
389931                 ZDOT =        6004
094563

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21536094
37                 X    =        -6564201
56
 Y    =        5673059
52  feet           Y    =         1729148
54  meter
 Z    =         396967
27                 Z    =          120995
62
 XDOT =      -3200
088362                 XDOT =        -975
386933
 YDOT =     -13611
566017  feet/sec       YDOT =       -4148
805322  meter/sec
 ZDOT =      19719
309310                 ZDOT =        6010
445478


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   19105
90580516  
00016717  00000-0  10270-3 0  9142
2 25544  51
6414 310
8113 0001655 192
2649 167
8463 15
52525407  5578


Satellite: ISS
Catalog Number: 25544
Epoch time:      19105
90580516   =   yrday
fracday
Element set:     914
Inclination:       51
6414  deg
RA of node:       310
8113  deg
Eccentricity:     
0001655     
Arg of perigee:   192
2649  deg
Mean anomaly:     167
8463  deg
Mean motion:   15
52525407  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             557
Checksum:              304


Coasting Arc #16 (Orbit 571)
---------------------------------------

Vector Time (GMT): 2019/106/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4660215
21                 A    =         6793188
18  meter
 Y    =        4764541
38  meter          E    =           
0009924
 Z    =       -1289815
81                 I    =           51
34745
 XDOT =      -2704
196578                 Wp   =          149
55322
 YDOT =      -4209
538919  meter/sec      RA   =          305
46159  deg
 ZDOT =      -5807
475020                 TA   =           44
52809
                                          MA   =           44
44838
                                          Ha   =            223
382  n
mi
                                          Hp   =            217
261

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15289419
97                 X    =        -4706882
08
 Y    =       15631697
44  feet           Y    =         4712166
56  meter
 Z    =       -4231679
16                 Z    =        -1312567
14
 XDOT =      -8872
036018                 XDOT =       -2628
713786
 YDOT =     -13810
823224  feet/sec       YDOT =       -4239
357533  meter/sec
 ZDOT =     -19053
395736                 ZDOT =       -5820
427363

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21329213
24                 X    =         6501144
20
 Y    =       -4721817
59  feet           Y    =        -1439210
00  meter
 Z    =       -4335036
03                 Z    =        -1321318
98
 XDOT =       -591
833320                 XDOT =        -180
390796
 YDOT =      14790
092319  feet/sec       YDOT =        4508
020139  meter/sec
 ZDOT =     -19111
488096                 ZDOT =       -5825
181572


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   19106
87131720  
00016717  00000-0  10270-3 0  9159
2 25544  51
6406 306
0099 0001659 194
4017 165
7087 15
52547402  5721


Satellite: ISS
Catalog Number: 25544
Epoch time:      19106
87131720   =   yrday
fracday
Element set:     915
Inclination:       51
6406  deg
RA of node:       306
0099  deg
Eccentricity:     
0001659     
Arg of perigee:   194
4017  deg
Mean anomaly:     165
7087  deg
Mean motion:   15
52547402  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             572
Checksum:              304


Coasting Arc #17 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2019/107/20:12:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4720660
08                 A    =         6791425
10  meter
 Y    =       -4248654
07  meter          E    =           
0012959
 Z    =        2390747
96                 I    =           51
32288
 XDOT =       1924
832814                 Wp   =           79
78134
 YDOT =       5155
392207  meter/sec      RA   =          300
47465  deg
 ZDOT =       5338
589592                 TA   =          307
04406
                                          MA   =          307
16252
                                          Ha   =            223
345  n
mi
                                          Hp   =            217
256

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15487729
93                 X    =         4756205
88
 Y    =      -13939153
78  feet           Y    =        -4195665
40  meter
 Z    =        7843661
28                 Z    =         2413766
00
 XDOT =       6315
068288                 XDOT =        1841
108608
 YDOT =      16914
016427  feet/sec       YDOT =        5176
449340  meter/sec
 ZDOT =      17515
057715                 ZDOT =        5347
736000

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20489612
95                 X    =        -6245234
03
 Y    =        3563062
93  feet           Y    =         1086021
58  meter
 Z    =        7948154
02                 Z    =         2422597
35
 XDOT =       4035
043313                 XDOT =        1229
881202
 YDOT =     -16120
670392  feet/sec       YDOT =       -4913
580335  meter/sec
 ZDOT =      17555
851930                 ZDOT =        5351
023668


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   19107
90119417  
00016717  00000-0  10270-3 0  9164
2 25544  51
6402 300
8880 0001569 197
5256 162
5841 15
52555528  5884


Satellite: ISS
Catalog Number: 25544
Epoch time:      19107
90119417   =   yrday
fracday
Element set:     916
Inclination:       51
6402  deg
RA of node:       300
8880  deg
Eccentricity:     
0001569     
Arg of perigee:   197
5256  deg
Mean anomaly:     162
5841  deg
Mean motion:   15
52555528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             588
Checksum:              322


Coasting Arc #18 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2019/107/20:46:01
000
Vector Time (MET): N/A
Weight (LBS)     : 929253
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1896955
97                 A    =         6792352
25  meter
 Y    =        6235258
46  meter          E    =           
0014121
 Z    =        1886731
20                 I    =           51
32543
 XDOT =      -5246
301189                 Wp   =          118
84158
 YDOT =        103
762514  meter/sec      RA   =          300
31939  deg
 ZDOT =      -5592
489822                 TA   =           40
29263
                                          MA   =           40
18808
                                          Ha   =            223
325  n
mi
                                          Hp   =            217
260

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6223608
83                 X    =        -1975704
18
 Y    =       20456884
72  feet           Y    =         6213605
22  meter
 Z    =        6190062
99                 Z    =         1877324
66
 XDOT =     -17212
274243                 XDOT =       -5219
906170
 YDOT =        340
428195  feet/sec       YDOT =          45
241828  meter/sec
 ZDOT =     -18348
063722                 ZDOT =       -5617
910465

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13956982
05                 X    =         4254088
13
 Y    =      -16215819
21  feet           Y    =        -4942581
70  meter
 Z    =        6146883
63                 Z    =         1873570
13
 XDOT =      14602
555767                 XDOT =        4450
858998
 YDOT =       5538
231019  feet/sec       YDOT =        1688
052814  meter/sec
 ZDOT =     -18462
975818                 ZDOT =       -5627
515029


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   19107
90119405  
00016717  00000-0  10270-3 0  9172
2 25544  51
6400 300
8884 0001405 199
0084 161
1015 15
52579820  5880


Satellite: ISS
Catalog Number: 25544
Epoch time:      19107
90119405   =   yrday
fracday
Element set:     917
Inclination:       51
6400  deg
RA of node:       300
8884  deg
Eccentricity:     
0001405     
Arg of perigee:   199
0084  deg
Mean anomaly:     161
1015  deg
Mean motion:   15
52579820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             588
Checksum:              296
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