[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: January 2nd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


010/09:34:56 900 0 0 0 0 0 0
N/A 0 0 0 0 220 6
000/00:00:00 000 0 0 0 0 216 3

016/05:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 216 2

Coasting Arc #1 (Orbit 2950)
---------------------------------------

Vector Time (GMT): 2019/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1856091
50                 A    =         6790501
43  meter
 Y    =        6523744
67  meter          E    =           
0009563
 Z    =         211648
34                 I    =           52
03057
 XDOT =      -4486
031627                 Wp   =           47
80630
 YDOT =      -1477
699018  meter/sec      RA   =          104
48631  deg
 ZDOT =       6039
073258                 TA   =          314
46109
                                          MA   =          314
53927
                                          Ha   =            221
068  n
mi
                                          Hp   =            216
086

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6089539
06                 X    =        -1929931
97
 Y    =       21403361
79  feet           Y    =         6502575
68  meter
 Z    =         694384
30                 Z    =          202453
44
 XDOT =     -14717
951533                 XDOT =       -4498
508659
 YDOT =      -4848
093890  feet/sec       YDOT =       -1527
935316  meter/sec
 ZDOT =      19813
232475                 ZDOT =        6017
251323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22171462
41                 X    =        -6757861
74
 Y    =       -1915600
50  feet           Y    =         -583875
03  meter
 Z    =         652135
77                 Z    =          198770
98
 XDOT =       1796
636257                 XDOT =         547
614731
 YDOT =     -13883
522093  feet/sec       YDOT =       -4231
697534  meter/sec
 ZDOT =      19714
916469                 ZDOT =        6009
106540


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   19002
56393925  
00016717  00000-0  10270-3 0  9001
2 25544  51
6413 105
1284 0002909 226
7669 133
3241 15
53719632 29517


Satellite: ISS
Catalog Number: 25544
Epoch time:      19002
56393925   =   yrday
fracday
Element set:     900
Inclination:       51
6413  deg
RA of node:       105
1284  deg
Eccentricity:     
0002909     
Arg of perigee:   226
7669  deg
Mean anomaly:     133
3241  deg
Mean motion:   15
53719632  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2951
Checksum:              302


Coasting Arc #2 (Orbit 2965)
---------------------------------------

Vector Time (GMT): 2019/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2434282
98                 A    =         6789178
70  meter
 Y    =       -6076158
53  meter          E    =           
0008109
 Z    =       -1785255
91                 I    =           52
03360
 XDOT =       3961
913162                 Wp   =          163
35612
 YDOT =       3257
623085  meter/sec      RA   =           99
54420  deg
 ZDOT =      -5699
059904                 TA   =           36
14115
                                          MA   =           36
08637
                                          Ha   =            221
030  n
mi
                                          Hp   =            216
155

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7986492
72                 X    =         2510719
14
 Y    =      -19934903
32  feet           Y    =        -6048509
10  meter
 Z    =       -5857138
81                 Z    =        -1773246
14
 XDOT =      12998
402762                 XDOT =        3952
873862
 YDOT =      10687
739781  feet/sec       YDOT =        3301
878062  meter/sec
 ZDOT =     -18697
703098                 ZDOT =       -5679
836032

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21164411
50                 X    =         6450912
63
 Y    =        3727258
91  feet           Y    =         1136068
52  meter
 Z    =       -5802218
38                 Z    =        -1768516
16
 XDOT =      -7468
285816                 XDOT =       -2276
333517
 YDOT =      13506
595021  feet/sec       YDOT =        4116
810163  meter/sec
 ZDOT =     -18611
317773                 ZDOT =       -5672
729657


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   19003
52871953  
00016717  00000-0  10270-3 0  9011
2 25544  51
6415 100
3224 0002992 230
1734 129
9155 15
53723662 29663


Satellite: ISS
Catalog Number: 25544
Epoch time:      19003
52871953   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       100
3224  deg
Eccentricity:     
0002992     
Arg of perigee:   230
1734  deg
Mean anomaly:     129
9155  deg
Mean motion:   15
53723662  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2966
Checksum:              298


Coasting Arc #3 (Orbit 2981)
---------------------------------------

Vector Time (GMT): 2019/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2908636
14                 A    =         6786215
55  meter
 Y    =        5239026
21  meter          E    =           
0010536
 Z    =        3176834
81                 I    =           52
02912
 XDOT =      -3414
654868                 Wp   =           93
47142
 YDOT =      -4851
050330  meter/sec      RA   =           94
59670  deg
 ZDOT =       4859
192981                 TA   =          302
98219
                                          MA   =          303
08341
                                          Ha   =            220
919  n
mi
                                          Hp   =            216
138

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9542769
48                 X    =        -2982435
44
 Y    =       17188406
19  feet           Y    =         5206086
79  meter
 Z    =       10422686
38                 Z    =         3162527
21
 XDOT =     -11202
935918                 XDOT =       -3383
758408
 YDOT =     -15915
519456  feet/sec       YDOT =       -4889
063213  meter/sec
 ZDOT =      15942
234190                 ZDOT =        4842
680408

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18903762
21                 X    =        -5761866
72
 Y    =       -5523460
78  feet           Y    =        -1683550
85  meter
 Z    =       10357475
71                 Z    =         3156958
60
 XDOT =      12578
522087                 XDOT =        3833
933532
 YDOT =     -13203
970381  feet/sec       YDOT =       -4024
570172  meter/sec
 ZDOT =      15868
278284                 ZDOT =        4836
651221


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   19004
55781448  
00016717  00000-0  10270-3 0  9025
2 25544  51
6422  95
1957 0002841 235
7397 124
3487 15
53747257 29825


Satellite: ISS
Catalog Number: 25544
Epoch time:      19004
55781448   =   yrday
fracday
Element set:     902
Inclination:       51
6422  deg
RA of node:        95
1957  deg
Eccentricity:     
0002841     
Arg of perigee:   235
7397  deg
Mean anomaly:     124
3487  deg
Mean motion:   15
53747257  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2982
Checksum:              334


Coasting Arc #4 (Orbit 2996)
---------------------------------------

Vector Time (GMT): 2019/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3340177
01                 A    =         6782723
14  meter
 Y    =       -4039560
30  meter          E    =           
0005542
 Z    =       -4310223
73                 I    =           52
01777
 XDOT =       2831
579601                 Wp   =           74
97469
 YDOT =       6155
651705  meter/sec      RA   =           89
64183  deg
 ZDOT =      -3577
219451                 TA   =          158
71414
                                          MA   =          158
69108
                                          Ha   =            220
877  n
mi
                                          Hp   =            216
306

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10958585
98                 X    =         3406036
73
 Y    =      -13253150
59  feet           Y    =        -4001839
35  meter
 Z    =      -14141153
96                 Z    =        -4293839
08
 XDOT =       9289
959320                 XDOT =        2779
910910
 YDOT =      20195
707692  feet/sec       YDOT =        6187
027933  meter/sec
 ZDOT =     -11736
284287                 ZDOT =       -3563
589571

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15522777
51                 X    =         4731342
58
 Y    =        7541899
33  feet           Y    =         2298770
92  meter
 Z    =      -14066697
38                 Z    =        -4287529
36
 XDOT =     -16800
186814                 XDOT =       -5120
696941
 YDOT =      12816
723680  feet/sec       YDOT =        3906
537378  meter/sec
 ZDOT =     -11675
504454                 ZDOT =       -3558
693758


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   19005
52259098  
00016717  00000-0  10270-3 0  9035
2 25544  51
6411  90
3904 0002895 239
6752 120
4115 15
53723391 29973


Satellite: ISS
Catalog Number: 25544
Epoch time:      19005
52259098   =   yrday
fracday
Element set:     903
Inclination:       51
6411  deg
RA of node:        90
3904  deg
Eccentricity:     
0002895     
Arg of perigee:   239
6752  deg
Mean anomaly:     120
4115  deg
Mean motion:   15
53723391  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2997
Checksum:              312


Coasting Arc #5 (Orbit 3012)
---------------------------------------

Vector Time (GMT): 2019/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3714704
52                 A    =         6779706
74  meter
 Y    =        2593155
16  meter          E    =           
0005004
 Z    =        5043335
74                 I    =           52
00748
 XDOT =      -2220
459705                 Wp   =          153
63426
 YDOT =      -7064
236393  meter/sec      RA   =           84
67768  deg
 ZDOT =       1991
637116                 TA   =          277
09481
                                          MA   =          277
15172
                                          Ha   =            220
809  n
mi
                                          Hp   =            216
208

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12187350
78                 X    =        -3767923
23
 Y    =        8507726
91  feet           Y    =         2551316
61  meter
 Z    =       16546377
09                 Z    =         5025162
37
 XDOT =      -7284
972785                 XDOT =       -2150
974543
 YDOT =     -23176
628585  feet/sec       YDOT =       -7088
678829  meter/sec
 ZDOT =       6534
242505                 ZDOT =        1981
019054

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11384480
80                 X    =        -3469989
75
 Y    =       -9696671
80  feet           Y    =        -2955545
56  meter
 Z    =       16464011
78                 Z    =         5018230
79
 XDOT =      19806
026893                 XDOT =        6036
876997
 YDOT =     -12210
218311  feet/sec       YDOT =       -3721
674541  meter/sec
 ZDOT =       6487
178671                 ZDOT =        1977
292059


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   19006
55168115  
00016717  00000-0  10270-3 0  9049
2 25544  51
6418  85
2636 0002916 245
2149 114
8701 15
53764176 30136


Satellite: ISS
Catalog Number: 25544
Epoch time:      19006
55168115   =   yrday
fracday
Element set:     904
Inclination:       51
6418  deg
RA of node:        85
2636  deg
Eccentricity:     
0002916     
Arg of perigee:   245
2149  deg
Mean anomaly:     114
8701  deg
Mean motion:   15
53764176  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3013
Checksum:              299


Coasting Arc #6 (Orbit 3027)
---------------------------------------

Vector Time (GMT): 2019/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4064793
15                 A    =         6778538
22  meter
 Y    =        -987291
73  meter          E    =           
0012198
 Z    =       -5344450
66                 I    =           51
99838
 XDOT =       1535
528471                 Wp   =           92
11209
 YDOT =       7500
321768  meter/sec      RA   =           79
70786  deg
 ZDOT =       -218
549988                 TA   =          175
81775
                                          MA   =          175
80755
                                          Ha   =            220
705  n
mi
                                          Hp   =            216
410

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13335935
54                 X    =         4101491
18
 Y    =       -3239146
11  feet           Y    =         -941630
66  meter
 Z    =      -17534286
95                 Z    =        -5324616
70
 XDOT =       5037
823067                 XDOT =        1452
605222
 YDOT =      24607
354883  feet/sec       YDOT =        7517
029485  meter/sec
 ZDOT =       -717
027519                 ZDOT =        -211
291729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6798350
69                 X    =         2072137
29
 Y    =       12052312
27  feet           Y    =         3673544
78  meter
 Z    =      -17444616
93                 Z    =        -5317119
24
 XDOT =     -21409
019267                 XDOT =       -6525
469073
 YDOT =      11088
567845  feet/sec       YDOT =        3379
795479  meter/sec
 ZDOT =       -685
195367                 ZDOT =        -208
847548


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   19007
51645215  
00016717  00000-0  10270-3 0  9058
2 25544  51
6412  80
4575 0002801 251
5956 108
4892 15
53727259 30285


Satellite: ISS
Catalog Number: 25544
Epoch time:      19007
51645215   =   yrday
fracday
Element set:     905
Inclination:       51
6412  deg
RA of node:        80
4575  deg
Eccentricity:     
0002801     
Arg of perigee:   251
5956  deg
Mean anomaly:     108
4892  deg
Mean motion:   15
53727259  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3028
Checksum:              307


Coasting Arc #7 (Orbit 3043)
---------------------------------------

Vector Time (GMT): 2019/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4352497
06                 A    =         6779192
57  meter
 Y    =        -642035
87  meter          E    =           
0002480
 Z    =        5157008
58                 I    =           51
99404
 XDOT =       -764
056021                 Wp   =           31
05378
 YDOT =      -7466
632850  meter/sec      RA   =           74
73710  deg
 ZDOT =      -1572
035829                 TA   =           74
03999
                                          MA   =           74
01266
                                          Ha   =            220
742  n
mi
                                          Hp   =            216
211

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14279845
98                 X    =        -4370043
59
 Y    =       -2106416
91  feet           Y    =         -690807
07  meter
 Z    =       16919319
50                 Z    =         5135823
48
 XDOT =      -2506
745476                 XDOT =        -672
869307
 YDOT =     -24496
826937  feet/sec       YDOT =       -7474
667066  meter/sec
 ZDOT =      -5157
597863                 ZDOT =       -1575
526424

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2161755
74                 X    =         -658903
15
 Y    =      -14384109
06  feet           Y    =        -4384276
44  meter
 Z    =       16823750
61                 Z    =         5127879
19
 XDOT =      21676
882914                 XDOT =        6607
113912
 YDOT =      -9316
736933  feet/sec       YDOT =       -2839
741417  meter/sec
 ZDOT =      -5172
414434                 ZDOT =       -1576
551919


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   19008
54553676  
00016717  00000-0  10270-3 0  9062
2 25544  51
6412  75
3309 0002794 255
9900 104
0942 15
53777739 30445


Satellite: ISS
Catalog Number: 25544
Epoch time:      19008
54553676   =   yrday
fracday
Element set:     906
Inclination:       51
6412  deg
RA of node:        75
3309  deg
Eccentricity:     
0002794     
Arg of perigee:   255
9900  deg
Mean anomaly:     104
0942  deg
Mean motion:   15
53777739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3044
Checksum:              321


Coasting Arc #8 (Orbit 3058)
---------------------------------------

Vector Time (GMT): 2019/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949740
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4568771
19                 A    =         6781838
14  meter
 Y    =        2173332
67  meter          E    =           
0007447
 Z    =       -4523802
27                 I    =           51
99188
 XDOT =       -119
463476                 Wp   =          120
62727
 YDOT =       6950
685256  meter/sec      RA   =           69
76995  deg
 ZDOT =       3218
847716                 TA   =          181
59797
                                          MA   =          181
60035
                                          Ha   =            220
665  n
mi
                                          Hp   =            216
285

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14989406
78                 X    =         4566102
54
 Y    =        7130356
51  feet           Y    =         2224409
23  meter
 Z    =      -14841870
95                 Z    =        -4501615
62
 XDOT =       -391
940538                 XDOT =        -212
814206
 YDOT =      22804
085485  feet/sec       YDOT =        6948
827157  meter/sec
 ZDOT =      10560
524001                 ZDOT =        3218
041162

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2159985
57                 X    =         -658363
60
 Y    =       16547328
40  feet           Y    =         5043625
69  meter
 Z    =      -14741974
71                 Z    =        -4493353
89
 XDOT =     -20641
721411                 XDOT =       -6291
596686
 YDOT =       6709
165778  feet/sec       YDOT =        2044
953729  meter/sec
 ZDOT =      10555
995654                 ZDOT =        3217
467475


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   19009
51030414  
00016717  00000-0  10270-3 0  9071
2 25544  51
6401  70
5245 0002569 259
1481 100
9382 15
53765778 30598


Satellite: ISS
Catalog Number: 25544
Epoch time:      19009
51030414   =   yrday
fracday
Element set:     907
Inclination:       51
6401  deg
RA of node:        70
5245  deg
Eccentricity:     
0002569     
Arg of perigee:   259
1481  deg
Mean anomaly:     100
9382  deg
Mean motion:   15
53765778  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3059
Checksum:              303


Coasting Arc #9 (Orbit 3072)
---------------------------------------

Vector Time (GMT): 2019/010/09:34:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4650407
87                 A    =         6780623
79  meter
 Y    =        1091378
53  meter          E    =           
0009065
 Z    =       -4821083
77                 I    =           51
97848
 XDOT =       1031
671492                 Wp   =          116
13202
 YDOT =       7128
057330  meter/sec      RA   =           65
31323  deg
 ZDOT =       2608
682133                 TA   =          179
48147
                                          MA   =          179
48053
                                          Ha   =            220
597  n
mi
                                          Hp   =            216
305

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15257243
68                 X    =         4661275
89
 Y    =        3580638
23  feet           Y    =         1143443
66  meter
 Z    =      -15817203
98                 Z    =        -4798467
77
 XDOT =       3384
748990                 XDOT =         939
215567
 YDOT =      23386
014861  feet/sec       YDOT =        7139
077106  meter/sec
 ZDOT =       8558
668415                 ZDOT =        2613
469346

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8038746
66                 X    =        -2450209
98
 Y    =       13571971
66  feet           Y    =         4136736
96  meter
 Z    =      -15715232
54                 Z    =        -4790002
88
 XDOT =     -22313
642934                 XDOT =       -6801
198366
 YDOT =      -3281
940141  feet/sec       YDOT =       -1000
335355  meter/sec
 ZDOT =       8579
365831                 ZDOT =        2614
990705


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   19010
41074951  
00016717  00000-0  10270-3 0  9087
2 25544  51
6417  66
0371 0002655 260
4164  99
6689 15
53783292 30735


Satellite: ISS
Catalog Number: 25544
Epoch time:      19010
41074951   =   yrday
fracday
Element set:     908
Inclination:       51
6417  deg
RA of node:        66
0371  deg
Eccentricity:     
0002655     
Arg of perigee:   260
4164  deg
Mean anomaly:      99
6689  deg
Mean motion:   15
53783292  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3073
Checksum:              316


Coasting Arc #10 (Orbit 3088)
---------------------------------------

Vector Time (GMT): 2019/011/09:34:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4942495
95                 A    =         6783986
09  meter
 Y    =       -2496561
26  meter          E    =           
0008658
 Z    =        3913328
41                 I    =           51
97473
 XDOT =         10
636759                 Wp   =           79
21760
 YDOT =      -6475
775951  meter/sec      RA   =           60
34894  deg
 ZDOT =      -4108
611130                 TA   =           53
67262
                                          MA   =           53
59272
                                          Ha   =            220
725  n
mi
                                          Hp   =            216
205

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16215537
89                 X    =        -4933219
85
 Y    =       -8190817
78  feet           Y    =        -2551779
98  meter
 Z    =       12839003
97                 Z    =         3889342
42
 XDOT =         34
897502                 XDOT =         103
006957
 YDOT =     -21245
984091  feet/sec       YDOT =       -6475
140368  meter/sec
 ZDOT =     -13479
695310                 ZDOT =       -4108
335370

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12490896
60                 X    =         3807225
28
 Y    =      -13295544
16  feet           Y    =        -4052481
86  meter
 Z    =       12731032
79                 Z    =         3880418
79
 XDOT =      19363
044133                 XDOT =        5901
855852
 YDOT =       5256
472013  feet/sec       YDOT =        1602
172670  meter/sec
 ZDOT =     -13477
609271                 ZDOT =       -4107
975306


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   19011
43982801  
00016717  00000-0  10270-3 0  9093
2 25544  51
6417  60
9100 0002603 267
4635  92
6220 15
53770111 30898


Satellite: ISS
Catalog Number: 25544
Epoch time:      19011
43982801   =   yrday
fracday
Element set:     909
Inclination:       51
6417  deg
RA of node:        60
9100  deg
Eccentricity:     
0002603     
Arg of perigee:   267
4635  deg
Mean anomaly:      92
6220  deg
Mean motion:   15
53770111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3089
Checksum:              285


Coasting Arc #11 (Orbit 3103)
---------------------------------------

Vector Time (GMT): 2019/012/09:34:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5058488
16                 A    =         6787489
54  meter
 Y    =        3649494
75  meter          E    =           
0003278
 Z    =       -2672961
93                 I    =           51
96800
 XDOT =      -1190
497669                 Wp   =           23
01390
 YDOT =       5476
226977  meter/sec      RA   =           55
39287  deg
 ZDOT =       5229
016214                 TA   =          306
98178
                                          MA   =          307
01178
                                          Ha   =            220
634  n
mi
                                          Hp   =            216
337

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16596089
77                 X    =         5030286
13
 Y    =       11973407
98  feet           Y    =         3705904
68  meter
 Z    =       -8769560
14                 Z    =        -2648458
39
 XDOT =      -3905
832247                 XDOT =       -1277
045230
 YDOT =      17966
623939  feet/sec       YDOT =        5462
429928  meter/sec
 ZDOT =      17155
565005                 ZDOT =        5223
023255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15999487
19                 X    =        -4876643
70
 Y    =       12834675
79  feet           Y    =         3912009
18  meter
 Z    =       -8659410
28                 Z    =        -2639388
25
 XDOT =     -15296
319175                 XDOT =       -4662
318085
 YDOT =      -7523
625052  feet/sec       YDOT =       -2293
200916  meter/sec
 ZDOT =      17127
789624                 ZDOT =        5220
550277


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   19012
40458778  
00016717  00000-0  10270-3 0  9104
2 25544  51
6409  56
1038 0002741 271
1359  88
9480 15
53744890 31043


Satellite: ISS
Catalog Number: 25544
Epoch time:      19012
40458778   =   yrday
fracday
Element set:     910
Inclination:       51
6409  deg
RA of node:        56
1038  deg
Eccentricity:     
0002741     
Arg of perigee:   271
1359  deg
Mean anomaly:      88
9480  deg
Mean motion:   15
53744890  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3104
Checksum:              311


Coasting Arc #12 (Orbit 3119)
---------------------------------------

Vector Time (GMT): 2019/013/09:38:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4153255
55                 A    =         6790348
80  meter
 Y    =       -5358582
32  meter          E    =           
0009705
 Z    =        -269011
04                 I    =           51
95807
 XDOT =       3881
562458                 Wp   =          147
02322
 YDOT =      -2711
201447  meter/sec      RA   =           50
44277  deg
 ZDOT =      -6031
282325                 TA   =           35
86243
                                          MA   =           35
79731
                                          Ha   =            220
609  n
mi
                                          Hp   =            216
210

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13626166
51                 X    =        -4091719
01
 Y    =      -17580650
64  feet           Y    =        -5404682
83  meter
 Z    =        -882582
16                 Z    =         -289036
49
 XDOT =      12734
784967                 XDOT =        3940
887725
 YDOT =      -8895
017871  feet/sec       YDOT =       -2667
463240  meter/sec
 ZDOT =     -19787
671671                 ZDOT =       -6012
283318

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20284508
01                 X    =         6182718
04
 Y    =       -9117239
19  feet           Y    =        -2778934
51  meter
 Z    =        -972278
77                 Z    =         -296350
57
 XDOT =       4966
120949                 XDOT =        1513
673665
 YDOT =      13114
996579  feet/sec       YDOT =        3997
450957  meter/sec
 ZDOT =     -19701
538923                 ZDOT =       -6005
029064


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   19013
43366305  
00016717  00000-0  10270-3 0  9113
2 25544  51
6409  50
9769 0002620 275
1201  84
9653 15
53764794 31203


Satellite: ISS
Catalog Number: 25544
Epoch time:      19013
43366305   =   yrday
fracday
Element set:     911
Inclination:       51
6409  deg
RA of node:        50
9769  deg
Eccentricity:     
0002620     
Arg of perigee:   275
1201  deg
Mean anomaly:      84
9653  deg
Mean motion:   15
53764794  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3120
Checksum:              300


Coasting Arc #13 (Orbit 3135)
---------------------------------------

Vector Time (GMT): 2019/014/09:38:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3448195
23                 A    =         6788969
04  meter
 Y    =        5548000
46  meter          E    =           
0011996
 Z    =        1825737
24                 I    =           51
93184
 XDOT =      -5010
532462                 Wp   =           58
60159
 YDOT =       1240
369273  meter/sec      RA   =           45
49366  deg
 ZDOT =       5672
678661                 TA   =          321
39180
                                          MA   =          321
47752
                                          Ha   =            220
684  n
mi
                                          Hp   =            216
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11312976
48                 X    =         3377031
30
 Y    =       18202101
23  feet           Y    =         5586162
61  meter
 Z    =        5989951
57                 Z    =         1842314
50
 XDOT =     -16438
754796                 XDOT =       -5051
584758
 YDOT =       4069
452994  feet/sec       YDOT =        1184
108287  meter/sec
 ZDOT =      18611
150461                 ZDOT =        5648
239873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20220448
77                 X    =        -6163192
79
 Y    =        7038484
96  feet           Y    =         2145330
21  meter
 Z    =        6064043
78                 Z    =         1848320
54
 XDOT =        146
776157                 XDOT =          44
737373
 YDOT =     -15577
170107  feet/sec       YDOT =       -4747
921449  meter/sec
 ZDOT =      18500
657365                 ZDOT =        5639
000365


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   19014
46273533  
00016717  00000-0  10270-3 0  9128
2 25544  51
6414  45
8495 0002560 283
2134  76
8733 15
53755488 31362


Satellite: ISS
Catalog Number: 25544
Epoch time:      19014
46273533   =   yrday
fracday
Element set:     912
Inclination:       51
6414  deg
RA of node:        45
8495  deg
Eccentricity:     
0002560     
Arg of perigee:   283
2134  deg
Mean anomaly:      76
8733  deg
Mean motion:   15
53755488  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3136
Checksum:              314


Coasting Arc #14 (Orbit 3150)
---------------------------------------

Vector Time (GMT): 2019/015/09:38:56
900
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2448272
90                 A    =         6785888
83  meter
 Y    =       -5437534
94  meter          E    =           
0002180
 Z    =       -3240417
60                 I    =           51
89682
 XDOT =       5976
200364                 Wp   =           87
56738
 YDOT =        164
427095  meter/sec      RA   =           40
53830  deg
 ZDOT =      -4793
875963                 TA   =          129
78789
                                          MA   =          129
76869
                                          Ha   =            220
705  n
mi
                                          Hp   =            216
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8032391
40                 X    =        -2371546
83
 Y    =      -17839681
55  feet           Y    =        -5464484
08  meter
 Z    =      -10631291
33                 Z    =        -3252124
22
 XDOT =      19606
956576                 XDOT =        5997
203401
 YDOT =        539
458973  feet/sec       YDOT =         231
374781  meter/sec
 ZDOT =     -15727
939510                 ZDOT =       -4764
794948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19076286
06                 X    =         5814451
99
 Y    =       -4214047
96  feet           Y    =        -1284441
82  meter
 Z    =      -10683399
02                 Z    =        -3256300
02
 XDOT =      -4795
397919                 XDOT =       -1461
637286
 YDOT =      17810
294699  feet/sec       YDOT =        5428
577824  meter/sec
 ZDOT =     -15596
684108                 ZDOT =       -4753
869316


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   19015
42748947  
00016717  00000-0  10270-3 0  9132
2 25544  51
6405  41
0436 0002492 285
9289  74
1589 15
53766462 31510


Satellite: ISS
Catalog Number: 25544
Epoch time:      19015
42748947   =   yrday
fracday
Element set:     913
Inclination:       51
6405  deg
RA of node:        41
0436  deg
Eccentricity:     
0002492     
Arg of perigee:   285
9289  deg
Mean anomaly:      74
1589  deg
Mean motion:   15
53766462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3151
Checksum:              326


Coasting Arc #15 (Orbit 3163)
---------------------------------------

Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5939772
18                 A    =         6787028
66  meter
 Y    =       -1588412
68  meter          E    =           
0010915
 Z    =        2862406
59                 I    =           51
87937
 XDOT =       -946
330198                 Wp   =           98
87916
 YDOT =      -5658
724901  meter/sec      RA   =           36
39808  deg
 ZDOT =      -5088
994094                 TA   =           48
67690
                                          MA   =           48
58301
                                          Ha   =            220
782  n
mi
                                          Hp   =            216
170

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19487441
55                 X    =        -5935472
57
 Y    =       -5211327
70  feet           Y    =        -1654811
48  meter
 Z    =        9391097
75                 Z    =         2833563
89
 XDOT =      -3104
757869                 XDOT =        -858
263020
 YDOT =     -18565
370411  feet/sec       YDOT =       -5668
814706  meter/sec
 ZDOT =     -16696
174850                 ZDOT =       -5093
377432

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20230204
53                 X    =         6166166
34
 Y    =        -285569
81  feet           Y    =          -87041
68  meter
 Z    =        9261117
97                 Z    =         2822788
76
 XDOT =       7894
644785                 XDOT =        2406
287731
 YDOT =      15584
177409  feet/sec       YDOT =        4750
057274  meter/sec
 ZDOT =     -16715
185160                 ZDOT =       -5094
788437


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   19016
26360886  
00016717  00000-0  10270-3 0  9148
2 25544  51
6409  36
8751 0002464 281
9968  78
0908 15
53758596 31646


Satellite: ISS
Catalog Number: 25544
Epoch time:      19016
26360886   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:        36
8751  deg
Eccentricity:     
0002464     
Arg of perigee:   281
9968  deg
Mean anomaly:      78
0908  deg
Mean motion:   15
53758596  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3164
Checksum:              348


Coasting Arc #16 (Orbit 3178)
---------------------------------------

Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 929891
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6160400
41                 A    =         6789593
61  meter
 Y    =        2470185
85  meter          E    =           
0008350
 Z    =       -1408457
02                 I    =           51
86194
 XDOT =       -659
204460                 Wp   =           20
44533
 YDOT =       4950
739890  meter/sec      RA   =           31
44101  deg
 ZDOT =       5817
461442                 TA   =          324
25154
                                          MA   =          324
30741
                                          Ha   =            220
815  n
mi
                                          Hp   =            216
116

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20211287
43                 X    =         6139161
71
 Y    =        8104284
29  feet           Y    =         2538957
10  meter
 Z    =       -4620921
98                 Z    =        -1378583
65
 XDOT =      -2162
744290                 XDOT =        -742
773870
 YDOT =      16242
584942  feet/sec       YDOT =        4942
900477  meter/sec
 ZDOT =      19086
159586                 ZDOT =        5814
056713

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21717344
12                 X    =        -6619446
49
 Y    =       -1938426
21  feet           Y    =         -590832
31  meter
 Z    =       -4486418
60                 Z    =        -1367460
39
 XDOT =      -2620
923073                 XDOT =        -798
857353
 YDOT =     -14632
491960  feet/sec       YDOT =       -4459
983549  meter/sec
 ZDOT =      19070
103919                 ZDOT =        5812
567675


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   19017
22835850  
00016717  00000-0  10270-3 0  9154
2 25544  51
6422  32
0686 0002510 291
6942  68
3943 15
53763967 31793


Satellite: ISS
Catalog Number: 25544
Epoch time:      19017
22835850   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:        32
0686  deg
Eccentricity:     
0002510     
Arg of perigee:   291
6942  deg
Mean anomaly:      68
3943  deg
Mean motion:   15
53763967  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3179
Checksum:              321
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