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

 
Date: April 2nd 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 9

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 9

Coasting Arc #1 (Orbit 333)
---------------------------------------

Vector Time (GMT): 2019/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         490386
38                 A    =         6783217
15  meter
 Y    =        4489460
42  meter          E    =           
0007265
 Z    =        5057580
09                 I    =           51
77044
 XDOT =      -7312
827047                 Wp   =          127
95377
 YDOT =      -1332
756530  meter/sec      RA   =           21
85764  deg
 ZDOT =       1885
897780                 TA   =          303
76804
                                          MA   =          303
83722
                                          Ha   =            224
033  n
mi
                                          Hp   =            216
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1608879
21                 X    =          415580
78
 Y    =       14729200
86  feet           Y    =         4494526
48  meter
 Z    =       16593110
53                 Z    =         5059780
07
 XDOT =     -23992
214721                 XDOT =       -7306
540861
 YDOT =      -4372
560793  feet/sec       YDOT =       -1414
498353  meter/sec
 ZDOT =       6187
328673                 ZDOT =        1850
390468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3702188
40                 X    =         1128427
02
 Y    =       14335921
17  feet           Y    =         4369588
77  meter
 Z    =       16602539
95                 Z    =         5060454
18
 XDOT =     -23372
214179                 XDOT =       -7123
850882
 YDOT =       -967
511073  feet/sec       YDOT =        -294
897375  meter/sec
 ZDOT =       6026
826618                 ZDOT =        1836
976753


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   19091
55147747  
00016717  00000-0  10270-3 0  9007
2 25544  51
6412  22
1935 0001813 140
7302 219
3981 15
52498385  3346


Satellite: ISS
Catalog Number: 25544
Epoch time:      19091
55147747   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:        22
1935  deg
Eccentricity:     
0001813     
Arg of perigee:   140
7302  deg
Mean anomaly:     219
3981  deg
Mean motion:   15
52498385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             334
Checksum:              297


Coasting Arc #2 (Orbit 348)
---------------------------------------

Vector Time (GMT): 2019/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 914819
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         578449
09                 A    =         6782267
97  meter
 Y    =       -4199481
55  meter          E    =           
0015907
 Z    =       -5307969
13                 I    =           51
73665
 XDOT =       7424
004005                 Wp   =           90
48631
 YDOT =       1766
651079  meter/sec      RA   =           16
88330  deg
 ZDOT =       -590
326133                 TA   =          173
88631
                                          MA   =          173
86688
                                          Ha   =            224
101  n
mi
                                          Hp   =            216
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1897798
86                 X    =          651148
94
 Y    =      -13777826
59  feet           Y    =        -4192606
99  meter
 Z    =      -17414596
88                 Z    =        -5304982
24
 XDOT =      24356
968519                 XDOT =        7406
564508
 YDOT =       5796
099341  feet/sec       YDOT =        1849
573916  meter/sec
 ZDOT =      -1936
765529                 ZDOT =        -554
305832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -326301
90                 X    =          -99456
82
 Y    =      -13921611
59  feet           Y    =        -4243307
21  meter
 Z    =      -17400591
61                 Z    =        -5303700
32
 XDOT =      23981
244324                 XDOT =        7309
483270
 YDOT =       1648
421845  feet/sec       YDOT =         502
438978  meter/sec
 ZDOT =      -1774
007535                 ZDOT =        -540
717497


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   19092
51704267  
00016717  00000-0  10270-3 0  9011
2 25544  51
6422  17
3916 0001821 137
4121 222
7172 15
52476843  3494


Satellite: ISS
Catalog Number: 25544
Epoch time:      19092
51704267   =   yrday
fracday
Element set:     901
Inclination:       51
6422  deg
RA of node:        17
3916  deg
Eccentricity:     
0001821     
Arg of perigee:   137
4121  deg
Mean anomaly:     222
7172  deg
Mean motion:   15
52476843  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             349
Checksum:              289


Coasting Arc #3 (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    =       -1662299
57                 A    =         6782272
61  meter
 Y    =        3911880
83  meter          E    =           
0003839
 Z    =        5281893
82                 I    =           51
70463
 XDOT =      -7330
692625                 Wp   =           86
87980
 YDOT =      -2132
556464  meter/sec      RA   =           11
90783  deg
 ZDOT =       -727
014719                 TA   =           10
06163
                                          MA   =           10
05395
                                          Ha   =            224
039  n
mi
                                          Hp   =            216
823

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5453738
73                 X    =        -1731576
25
 Y    =       12834254
69  feet           Y    =         3892905
07  meter
 Z    =       17329047
95                 Z    =         5273650
31
 XDOT =     -24050
828821                 XDOT =       -7302
769514
 YDOT =      -6996
576324  feet/sec       YDOT =       -2214
377353  meter/sec
 ZDOT =      -2385
218893                 ZDOT =        -762
556358

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3102683
38                 X    =         -945697
89
 Y    =       13643374
67  feet           Y    =         4158500
60  meter
 Z    =       17291296
84                 Z    =         5270387
28
 XDOT =     -23918
294112                 XDOT =       -7290
296045
 YDOT =      -2210
157676  feet/sec       YDOT =        -673
656060  meter/sec
 ZDOT =      -2545
752534                 ZDOT =        -775
945372


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
54697351  
00016717  00000-0  10270-3 0  9021
2 25544  51
6420  12
2714 0001694 142
4883 217
6387 15
52505662  3652


Satellite: ISS
Catalog Number: 25544
Epoch time:      19093
54697351   =   yrday
fracday
Element set:     902
Inclination:       51
6420  deg
RA of node:        12
2714  deg
Eccentricity:     
0001694     
Arg of perigee:   142
4883  deg
Mean anomaly:     217
6387  deg
Mean motion:   15
52505662  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             365
Checksum:              307


Coasting Arc #4 (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    =        2631484
65                 A    =         6784544
34  meter
 Y    =        4093176
81  meter          E    =           
0009300
 Z    =        4723201
97                 I    =           51
68032
 XDOT =      -7029
996261                 Wp   =          122
79449
 YDOT =       1318
429308  meter/sec      RA   =            7
16867  deg
 ZDOT =       2765
245126                 TA   =          299
79690
                                          MA   =          299
88936
                                          Ha   =            223
906  n
mi
                                          Hp   =            216
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8633479
83                 X    =         2562575
27
 Y    =       13429057
76  feet           Y    =         4122219
14  meter
 Z    =       15496069
47                 Z    =         4735816
94
 XDOT =     -23064
292196                 XDOT =       -7057
648886
 YDOT =       4325
555472  feet/sec       YDOT =        1239
660661  meter/sec
 ZDOT =       9072
326529                 ZDOT =        2731
028658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7811808
61                 X    =         2381039
26
 Y    =       13859850
12  feet           Y    =         4224482
32  meter
 Z    =       15552650
46                 Z    =         4740447
86
 XDOT =     -22309
275641                 XDOT =       -6799
867215
 YDOT =       2535
024499  feet/sec       YDOT =         772
675467  meter/sec
 ZDOT =       8917
397525                 ZDOT =        2718
022765


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
51253329  
00016717  00000-0  10270-3 0  9033
2 25544  51
6415   7
4703 0001795 148
8530 211
2729 15
52500393  3804


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
51253329   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:         7
4703  deg
Eccentricity:     
0001795     
Arg of perigee:   148
8530  deg
Mean anomaly:     211
2729  deg
Mean motion:   15
52500393  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             380
Checksum:              291


Coasting Arc #5 (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    =       -4921200
47                 A    =         6787677
03  meter
 Y    =        2552269
86  meter          E    =           
0012042
 Z    =        3906621
52                 I    =           51
68745
 XDOT =      -5238
972757                 Wp   =           87
82380
 YDOT =      -3835
552100  meter/sec      RA   =            6
42150  deg
 ZDOT =      -4082
418691                 TA   =           44
94144
                                          MA   =           44
84403
                                          Ha   =            224
030  n
mi
                                          Hp   =            216
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16145670
84                 X    =        -4968351
18
 Y    =        8373588
78  feet           Y    =         2496974
35  meter
 Z    =       12816999
73                 Z    =         3882601
30
 XDOT =     -17188
230831                 XDOT =       -5175
862973
 YDOT =     -12583
832348  feet/sec       YDOT =       -3893
785544  meter/sec
 ZDOT =     -13393
762110                 ZDOT =       -4107
714018

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4643387
53                 X    =        -1415304
52
 Y    =       17664076
78  feet           Y    =         5384010
60  meter
 Z    =       12708048
70                 Z    =         3873413
24
 XDOT =     -19506
552714                 XDOT =       -5945
597267
 YDOT =       4617
067484  feet/sec       YDOT =        1407
282169  meter/sec
 ZDOT =     -13507
729453                 ZDOT =       -4117
155937


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
64127381  
00016717  00000-0  10270-3 0  9046
2 25544  51
6430   6
8310 0001603 145
7994 214
3262 15
52511820  3821


Satellite: ISS
Catalog Number: 25544
Epoch time:      19094
64127381   =   yrday
fracday
Element set:     904
Inclination:       51
6430  deg
RA of node:         6
8310  deg
Eccentricity:     
0001603     
Arg of perigee:   145
7994  deg
Mean anomaly:     214
3262  deg
Mean motion:   15
52511820  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             382
Checksum:              281


Coasting Arc #6 (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    =        5639436
02                 A    =         6790329
81  meter
 Y    =       -2259499
64  meter          E    =           
0004892
 Z    =       -3037072
67                 I    =           51
66276
 XDOT =       4263
565462                 Wp   =           87
12026
 YDOT =       4014
085646  meter/sec      RA   =            1
45270  deg
 ZDOT =       4937
615413                 TA   =          238
12452
                                          MA   =          238
17213
                                          Ha   =            223
917  n
mi
                                          Hp   =            217
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18502086
70                 X    =         5679035
77
 Y    =       -7413056
56  feet           Y    =        -2196214
42  meter
 Z    =       -9964149
17                 Z    =        -3009581
80
 XDOT =      13988
075662                 XDOT =        4194
377579
 YDOT =      13169
572330  feet/sec       YDOT =        4061
377479  meter/sec
 ZDOT =      16199
525634                 ZDOT =        4958
157893

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6597972
76                 X    =         2011062
10
 Y    =      -18873658
43  feet           Y    =        -5752691
09  meter
 Z    =       -9839545
78                 Z    =        -2999093
55
 XDOT =      17670
439464                 XDOT =        5385
949948
 YDOT =      -2303
938408  feet/sec       YDOT =        -702
240427  meter/sec
 ZDOT =      16291
962474                 ZDOT =        4965
790162


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
60683123  
00016717  00000-0  10270-3 0  9055
2 25544  51
6429   2
0297 0001542 155
0888 205
0338 15
52476222  3972


Satellite: ISS
Catalog Number: 25544
Epoch time:      19095
60683123   =   yrday
fracday
Element set:     905
Inclination:       51
6429  deg
RA of node:         2
0297  deg
Eccentricity:     
0001542     
Arg of perigee:   155
0888  deg
Mean anomaly:     205
0338  deg
Mean motion:   15
52476222  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             397
Checksum:              301


Coasting Arc #7 (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    =       -6185100
66                 A    =         6792497
02  meter
 Y    =        1956306
90  meter          E    =           
0015156
 Z    =        1987937
16                 I    =           51
63694
 XDOT =      -3138
055788                 Wp   =          115
77998
 YDOT =      -4228
744829  meter/sec      RA   =          356
48605  deg
 ZDOT =      -5575
364973                 TA   =           42
27764
                                          MA   =           42
16090
                                          Ha   =            223
936  n
mi
                                          Hp   =            217
000

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20292325
01                 X    =        -6216173
35
 Y    =        6418329
71  feet           Y    =         1886967
21  meter
 Z    =        6522103
55                 Z    =         1957816
30
 XDOT =     -10295
458622                 XDOT =       -3063
453225
 YDOT =     -13873
834740  feet/sec       YDOT =       -4263
420144  meter/sec
 ZDOT =     -18291
879832                 ZDOT =       -5590
427045

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8171027
62                 X    =        -2490529
22
 Y    =       19696928
27  feet           Y    =         6003623
74  meter
 Z    =        6385653
42                 Z    =         1946347
16
 XDOT =     -15730
533226                 XDOT =       -4794
666527
 YDOT =       -544
594087  feet/sec       YDOT =        -165
992278  meter/sec
 ZDOT =     -18359
495984                 ZDOT =       -5595
974376


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
63675576  
00016717  00000-0  10270-3 0  9063
2 25544  51
6430 356
9081 0001562 153
0880 207
0353 15
52489865  4133


Satellite: ISS
Catalog Number: 25544
Epoch time:      19096
63675576   =   yrday
fracday
Element set:     906
Inclination:       51
6430  deg
RA of node:       356
9081  deg
Eccentricity:     
0001562     
Arg of perigee:   153
0880  deg
Mean anomaly:     207
0353  deg
Mean motion:   15
52489865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             413
Checksum:              320


Coasting Arc #8 (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    =        6521791
60                 A    =         6793819
63  meter
 Y    =       -1674772
41  meter          E    =           
0009523
 Z    =        -876767
61                 I    =           51
60630
 XDOT =       1935
199444                 Wp   =           46
96195
 YDOT =       4458
617259  meter/sec      RA   =          351
52024  deg
 ZDOT =       5925
257211                 TA   =          303
55556
                                          MA   =          303
64646
                                          Ha   =            223
872  n
mi
                                          Hp   =            217
041

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21396954
06                 X    =         6544293
57
 Y    =       -5494660
14  feet           Y    =        -1601715
42  meter
 Z    =       -2876534
16                 Z    =         -845032
01
 XDOT =       6349
079540                 XDOT =        1856
416111
 YDOT =      14628
009379  feet/sec       YDOT =        4479
817943  meter/sec
 ZDOT =      19439
820246                 ZDOT =        5934
466125

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9229087
52                 X    =         2813025
88
 Y    =      -20091067
26  feet           Y    =        -6123757
30  meter
 Z    =       -2732826
72                 Z    =         -832965
58
 XDOT =      13812
827042                 XDOT =        4210
149682
 YDOT =       3717
376344  feet/sec       YDOT =        1133
056310  meter/sec
 ZDOT =      19480
933414                 ZDOT =        5937
788505


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
60230755  
00016717  00000-0  10270-3 0  9078
2 25544  51
6411 352
1065 0001522 159
3241 200
7973 15
52482697  4288


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
60230755   =   yrday
fracday
Element set:     907
Inclination:       51
6411  deg
RA of node:       352
1065  deg
Eccentricity:     
0001522     
Arg of perigee:   159
3241  deg
Mean anomaly:     200
7973  deg
Mean motion:   15
52482697  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             428
Checksum:              300


Coasting Arc #9 (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    =       -2049385
96                 A    =         6782565
19  meter
 Y    =       -3845831
36  meter          E    =           
0014628
 Z    =       -5210106
00                 I    =           51
56070
 XDOT =       7227
917285                 Wp   =           88
84601
 YDOT =      -2209
180173  meter/sec      RA   =          350
33538  deg
 ZDOT =      -1215
055522                 TA   =          169
47757
                                          MA   =          169
44692
                                          Ha   =            223
925  n
mi
                                          Hp   =            216
880

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6723707
20                 X    =        -1980920
32
 Y    =      -12617556
97  feet           Y    =        -3868366
57  meter
 Z    =      -17093523
63                 Z    =        -5219894
73
 XDOT =      23713
639385                 XDOT =        7257
985913
 YDOT =      -7247
966446  feet/sec       YDOT =       -2128
184502  meter/sec
 ZDOT =      -3986
402630                 ZDOT =       -1179
871365

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3550166
47                 X    =        -1082090
74
 Y    =       13795207
70  feet           Y    =         4204779
31  meter
 Z    =      -17137330
45                 Z    =        -5223458
32
 XDOT =     -21472
340889                 XDOT =       -6544
769503
 YDOT =     -10269
211619  feet/sec       YDOT =       -3130
055701  meter/sec
 ZDOT =      -3827
040145                 ZDOT =       -1166
481836


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
85978939  
00016717  00000-0  10270-3 0  9089
2 25544  51
6408 350
8225 0002129 162
4726 197
6499 15
52495701  4326


Satellite: ISS
Catalog Number: 25544
Epoch time:      19097
85978939   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:       350
8225  deg
Eccentricity:     
0002129     
Arg of perigee:   162
4726  deg
Mean anomaly:     197
6499  deg
Mean motion:   15
52495701  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             432
Checksum:              349


Coasting Arc #10 (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    =         959620
22                 A    =         6782078
28  meter
 Y    =        4108525
73  meter          E    =           
0003310
 Z    =        5307472
34                 I    =           51
52717
 XDOT =      -7438
023709                 Wp   =          120
57307
 YDOT =       1863
444218  meter/sec      RA   =          345
34579  deg
 ZDOT =        -99
263633                 TA   =          330
36491
                                          MA   =          330
38366
                                          Ha   =            223
787  n
mi
                                          Hp   =            217
032

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3148360
31                 X    =          887825
09
 Y    =       13479415
11  feet           Y    =         4118855
69  meter
 Z    =       17412966
99                 Z    =         5311959
30
 XDOT =     -24402
964924                 XDOT =       -7457
826287
 YDOT =       6113
662134  feet/sec       YDOT =        1780
156305  meter/sec
 ZDOT =       -325
668088                 ZDOT =        -135
443442

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6575036
22                 X    =         2004071
04
 Y    =      -12152604
45  feet           Y    =        -3704113
84  meter
 Z    =       17432765
91                 Z    =         5313507
05
 XDOT =      21521
953831                 XDOT =        6559
891528
 YDOT =      10949
603854  feet/sec       YDOT =        3337
439255  meter/sec
 ZDOT =       -489
480875                 ZDOT =        -149
193771


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
88970895  
00016717  00000-0  10270-3 0  9097
2 25544  51
6415 345
7002 0002048 168
5132 191
6067 15
52506676  4484


Satellite: ISS
Catalog Number: 25544
Epoch time:      19098
88970895   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       345
7002  deg
Eccentricity:     
0002048     
Arg of perigee:   168
5132  deg
Mean anomaly:     191
6067  deg
Mean motion:   15
52506676  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             448
Checksum:              335


Coasting Arc #11 (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    =         128696
29                 A    =         6782767
69  meter
 Y    =       -4409112
48  meter          E    =           
0014684
 Z    =       -5165646
54                 I    =           51
49807
 XDOT =       7383
651069                 Wp   =          108
07642
 YDOT =      -1441
781867  meter/sec      RA   =          340
35562  deg
 ZDOT =       1413
439908                 TA   =          175
57754
                                          MA   =          175
56455
                                          Ha   =            223
825  n
mi
                                          Hp   =            216
992

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         422231
92                 X    =          203082
82
 Y    =      -14465592
13  feet           Y    =        -4407257
53  meter
 Z    =      -16947659
27                 Z    =        -5164840
59
 XDOT =      24224
576999                 XDOT =        7392
358925
 YDOT =      -4730
255470  feet/sec       YDOT =       -1359
163989  meter/sec
 ZDOT =       4637
270041                 ZDOT =        1449
328542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9728895
55                 X    =        -2965367
36
 Y    =       10720146
02  feet           Y    =         3267500
51  meter
 Z    =      -16943489
92                 Z    =        -5164375
73
 XDOT =     -20769
819037                 XDOT =       -6330
640843
 YDOT =     -11257
322649  feet/sec       YDOT =       -3431
231943  meter/sec
 ZDOT =       4799
707412                 ZDOT =        1462
950819


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
85525676  
00016717  00000-0  10270-3 0  9100
2 25544  51
6420 340
8997 0002062 167
9476 192
1725 15
52515587  4634


Satellite: ISS
Catalog Number: 25544
Epoch time:      19099
85525676   =   yrday
fracday
Element set:     910
Inclination:       51
6420  deg
RA of node:       340
8997  deg
Eccentricity:     
0002062     
Arg of perigee:   167
9476  deg
Mean anomaly:     192
1725  deg
Mean motion:   15
52515587  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             463
Checksum:              338


Coasting Arc #12 (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    =       -1162604
49                 A    =         6784587
49  meter
 Y    =        4695450
56  meter          E    =           
0007386
 Z    =        4751725
90                 I    =           51
47240
 XDOT =      -7130
432928                 Wp   =           77
35601
 YDOT =        936
004012  meter/sec      RA   =          335
36441  deg
 ZDOT =      -2664
433196                 TA   =           39
03572
                                          MA   =           38
98243
                                          Ha   =            223
888  n
mi
                                          Hp   =            217
079

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3814319
18                 X    =        -1238105
39
 Y    =       15405021
51  feet           Y    =         4682027
40  meter
 Z    =       15589651
91                 Z    =         4745894
92
 XDOT =     -23393
808820                 XDOT =       -7127
427189
 YDOT =       3070
879303  feet/sec       YDOT =         856
283299  meter/sec
 ZDOT =      -8741
578728                 ZDOT =       -2699
063187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12760326
51                 X    =         3889347
52
 Y    =       -9480318
16  feet           Y    =        -2889600
97  meter
 Z    =       15562731
13                 Z    =         4743520
45
 XDOT =      19349
910388                 XDOT =        5897
852686
 YDOT =      11409
925237  feet/sec       YDOT =        3477
745212  meter/sec
 ZDOT =      -8898
258672                 ZDOT =       -2712
189243


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
88517334  
00016717  00000-0  10270-3 0  9119
2 25544  51
6416 335
7778 0002050 168
8378 191
2820 15
52479989  4795


Satellite: ISS
Catalog Number: 25544
Epoch time:      19100
88517334   =   yrday
fracday
Element set:     911
Inclination:       51
6416  deg
RA of node:       335
7778  deg
Eccentricity:     
0002050     
Arg of perigee:   168
8378  deg
Mean anomaly:     191
2820  deg
Mean motion:   15
52479989  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             479
Checksum:              338


Coasting Arc #13 (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    =        2093655
65                 A    =         6786914
86  meter
 Y    =       -4972852
30  meter          E    =           
0008380
 Z    =       -4126271
97                 I    =           51
45100
 XDOT =       6655
590596                 Wp   =          121
49354
 YDOT =       -326
762254  meter/sec      RA   =          330
37622  deg
 ZDOT =       3772
214205                 TA   =          187
54333
                                          MA   =          187
55595
                                          Ha   =            223
724  n
mi
                                          Hp   =            217
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6868948
99                 X    =         2169151
13
 Y    =      -16315132
21  feet           Y    =        -4949017
47  meter
 Z    =      -13537637
70                 Z    =        -4115918
34
 XDOT =      21835
927152                 XDOT =        6640
426477
 YDOT =      -1072
054638  feet/sec       YDOT =        -252
419557  meter/sec
 ZDOT =      12376
030857                 ZDOT =        3804
507896

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15549116
17                 X    =        -4739370
61
 Y    =        8536509
91  feet           Y    =         2601928
22  meter
 Z    =      -13490241
60                 Z    =        -4111825
64
 XDOT =     -17149
120823                 XDOT =       -5227
052027
 YDOT =     -11455
447995  feet/sec       YDOT =       -3491
620549  meter/sec
 ZDOT =      12522
071170                 ZDOT =        3816
727293


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
85071722  
00016717  00000-0  10270-3 0  9124
2 25544  51
6420 330
9774 0002017 177
7777 182
3384 15
52503303  4949


Satellite: ISS
Catalog Number: 25544
Epoch time:      19101
85071722   =   yrday
fracday
Element set:     912
Inclination:       51
6420  deg
RA of node:       330
9774  deg
Eccentricity:     
0002017     
Arg of perigee:   177
7777  deg
Mean anomaly:     182
3384  deg
Mean motion:   15
52503303  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             494
Checksum:              297


Coasting Arc #14 (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    =       -2908932
59                 A    =         6789608
32  meter
 Y    =        5179456
76  meter          E    =           
0013028
 Z    =        3274001
53                 I    =           51
43171
 XDOT =      -6036
325121                 Wp   =          101
14019
 YDOT =       -401
647268  meter/sec      RA   =          325
38986  deg
 ZDOT =      -4714
342023                 TA   =           40
73696
                                          MA   =           40
63960
                                          Ha   =            223
764  n
mi
                                          Hp   =            217
197

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9543742
09                 X    =        -2982537
84
 Y    =       16992968
38  feet           Y    =         5146515
52  meter
 Z    =       10741474
85                 Z    =         3259692
21
 XDOT =     -19804
216275                 XDOT =       -6008
485480
 YDOT =      -1317
740381  feet/sec       YDOT =        -468
994054  meter/sec
 ZDOT =     -15467
001388                 ZDOT =       -4743
596632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17926254
05                 X    =         5463922
23
 Y    =       -7738985
03  feet           Y    =        -2358842
64  meter
 Z    =       10676178
90                 Z    =         3254099
33
 XDOT =      14342
044537                 XDOT =        4371
455175
 YDOT =      11640
226329  feet/sec       YDOT =        3547
940985  meter/sec
 ZDOT =     -15599
213240                 ZDOT =       -4754
640196


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
88063003  
00016717  00000-0  10270-3 0  9132
2 25544  51
6422 325
8557 0002004 178
3271 181
7887 15
52491679  5107


Satellite: ISS
Catalog Number: 25544
Epoch time:      19102
88063003   =   yrday
fracday
Element set:     913
Inclination:       51
6422  deg
RA of node:       325
8557  deg
Eccentricity:     
0002004     
Arg of perigee:   178
3271  deg
Mean anomaly:     181
7887  deg
Mean motion:   15
52491679  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             510
Checksum:              303


Coasting Arc #15 (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    =        3559538
63                 A    =         6791958
72  meter
 Y    =       -5312455
11  meter          E    =           
0004721
 Z    =       -2287347
26                 I    =           51
41302
 XDOT =       5290
061348                 Wp   =           56
25134
 YDOT =       1221
772875  meter/sec      RA   =          320
40685  deg
 ZDOT =       5405
332248                 TA   =          278
22580
                                          MA   =          278
27934
                                          Ha   =            223
642  n
mi
                                          Hp   =            217
324

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11678276
34                 X    =         3629790
10
 Y    =      -17429314
67  feet           Y    =        -5272257
11  meter
 Z    =       -7504420
14                 Z    =        -2269885
65
 XDOT =      17355
844316                 XDOT =        5249
749918
 YDOT =       4008
441192  feet/sec       YDOT =        1280
704764  meter/sec
 ZDOT =      17734
029686                 ZDOT =        5430
931398

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19753612
72                 X    =        -6020901
16
 Y    =        7151613
32  feet           Y    =         2179811
74  meter
 Z    =       -7424869
08                 Z    =        -2263100
10
 XDOT =     -11028
681759                 XDOT =       -3361
542200
 YDOT =     -11967
491455  feet/sec       YDOT =       -3647
691396  meter/sec
 ZDOT =      17849
618859                 ZDOT =        5440
563828


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
84616998  
00016717  00000-0  10270-3 0  9147
2 25544  51
6425 321
0548 0001712 186
1264 173
9867 15
52478504  5251


Satellite: ISS
Catalog Number: 25544
Epoch time:      19103
84616998   =   yrday
fracday
Element set:     914
Inclination:       51
6425  deg
RA of node:       321
0548  deg
Eccentricity:     
0001712     
Arg of perigee:   186
1264  deg
Mean anomaly:     173
9867  deg
Mean motion:   15
52478504  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             525
Checksum:              322


Coasting Arc #16 (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    =       -4068633
41                 A    =         6793544
53  meter
 Y    =        5305954
10  meter          E    =           
0014611
 Z    =        1157444
81                 I    =           51
39236
 XDOT =      -4473
886211                 Wp   =          128
94783
 YDOT =      -2146
259727  meter/sec      RA   =          315
42643  deg
 ZDOT =      -5846
869860                 TA   =           38
44433
                                          MA   =           38
34033
                                          Ha   =            223
618  n
mi
                                          Hp   =            217
288

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13348534
81                 X    =        -4133285
92
 Y    =       17407985
90  feet           Y    =         5260094
35  meter
 Z    =        3797391
10                 Z    =         1137523
72
 XDOT =     -14678
104368                 XDOT =       -4421
152851
 YDOT =      -7041
534537  feet/sec       YDOT =       -2195
995245  meter/sec
 ZDOT =     -19182
643897                 ZDOT =       -5868
474091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20960163
23                 X    =         6388657
75
 Y    =       -6524813
87  feet           Y    =        -1988763
27  meter
 Z    =        3706736
44                 Z    =         1129813
27
 XDOT =       7359
292806                 XDOT =        2243
112447
 YDOT =      12609
953058  feet/sec       YDOT =        3843
513692  meter/sec
 ZDOT =     -19280
067825                 ZDOT =       -5876
564673


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
87608017  
00016717  00000-0  10270-3 0  9155
2 25544  51
6413 315
9341 0001896 185
6813 174
4318 15
52495188  5410


Satellite: ISS
Catalog Number: 25544
Epoch time:      19104
87608017   =   yrday
fracday
Element set:     915
Inclination:       51
6413  deg
RA of node:       315
9341  deg
Eccentricity:     
0001896     
Arg of perigee:   185
6813  deg
Mean anomaly:     174
4318  deg
Mean motion:   15
52495188  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             541
Checksum:              319


Coasting Arc #17 (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    =        4402588
12                 A    =         6794104
16  meter
 Y    =       -5168526
30  meter          E    =           
0010776
 Z    =          -3073
43                 I    =           51
37153
 XDOT =       3640
177374                 Wp   =           50
41232
 YDOT =       3105
528728  meter/sec      RA   =          310
44532  deg
 ZDOT =       5987
826570                 TA   =          309
55448
                                          MA   =          309
64964
                                          Ha   =            223
549  n
mi
                                          Hp   =            217
341

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14444186
74                 X    =         4460071
77
 Y    =      -16957107
30  feet           Y    =        -5118972
07  meter
 Z    =         -10083
44                 Z    =           18452
59
 XDOT =      11942
839153                 XDOT =        3576
094428
 YDOT =      10188
742546  feet/sec       YDOT =        3145
877799  meter/sec
 ZDOT =      19645
100295                 ZDOT =        6005
353323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21476607
11                 X    =        -6546069
85
 Y    =        5909801
96  feet           Y    =         1801307
64  meter
 Z    =          87794
97                 Z    =           26759
91
 XDOT =      -3612
552101                 XDOT =       -1101
105880
 YDOT =     -13499
965181  feet/sec       YDOT =       -4114
789387  meter/sec
 ZDOT =      19723
986770                 ZDOT =        6011
871167


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
90598819  
00016717  00000-0  10270-3 0  9169
2 25544  51
6415 310
8125 0001686 192
9782 167
1326 15
52487172  5578


Satellite: ISS
Catalog Number: 25544
Epoch time:      19105
90598819   =   yrday
fracday
Element set:     916
Inclination:       51
6415  deg
RA of node:       310
8125  deg
Eccentricity:     
0001686     
Arg of perigee:   192
9782  deg
Mean anomaly:     167
1326  deg
Mean motion:   15
52487172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             557
Checksum:              331
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