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

 
Date: January 17th 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 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


018/18:05:09 698 3 1 3 2 3 2
N/A 0 6 -0 3 221 0
000/00:08:19 397 -0 5 -0 1 217 9

020/01:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 8
000/00:00:00 000 0 0 0 0 217 9

025/12:55:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 6
000/00:00:00 000 0 0 0 0 217 5

026/08:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 217 4

Coasting Arc #1 (Orbit 3167)
---------------------------------------

Vector Time (GMT): 2019/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -415942
98                 A    =         6780879
85  meter
 Y    =       -4840895
92  meter          E    =           
0009374
 Z    =       -4739115
20                 I    =           51
85213
 XDOT =       6816
569021                 Wp   =           60
15521
 YDOT =       2127
757980  meter/sec      RA   =           35
08293  deg
 ZDOT =      -2771
292022                 TA   =          182
45189
                                          MA   =          182
45648
                                          Ha   =            220
800  n
mi
                                          Hp   =            216
062

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1364642
32                 X    =         -338759
92
 Y    =      -15882204
46  feet           Y    =        -4845115
42  meter
 Z    =      -15548278
22                 Z    =        -4740948
54
 XDOT =      22364
071590                 XDOT =        6805
730548
 YDOT =       6980
833268  feet/sec       YDOT =        2203
925181  meter/sec
 ZDOT =      -9092
165428                 ZDOT =       -2738
206021

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13896053
09                 X    =         4235516
98
 Y    =       -7795491
42  feet           Y    =        -2376065
78  meter
 Z    =      -15555887
79                 Z    =        -4741434
60
 XDOT =       2482
061724                 XDOT =         756
532414
 YDOT =      22273
297421  feet/sec       YDOT =        6788
901054  meter/sec
 ZDOT =      -8943
107409                 ZDOT =       -2725
859138


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
52092079  
00016717  00000-0  10270-3 0  9008
2 25544  51
6412  35
5970 0002480 294
6806  65
4088 15
53763179 31685


Satellite: ISS
Catalog Number: 25544
Epoch time:      19016
52092079   =   yrday
fracday
Element set:     900
Inclination:       51
6412  deg
RA of node:        35
5970  deg
Eccentricity:     
0002480     
Arg of perigee:   294
6806  deg
Mean anomaly:      65
4088  deg
Mean motion:   15
53763179  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3168
Checksum:              317


Coasting Arc #2 (Orbit 3183)
---------------------------------------

Vector Time (GMT): 2019/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1033713
39                 A    =         6778736
89  meter
 Y    =        4168073
78  meter          E    =           
0001171
 Z    =        5244229
14                 I    =           51
81633
 XDOT =      -6949
970482                 Wp   =          122
34572
 YDOT =      -3062
512630  meter/sec      RA   =           30
10248  deg
 ZDOT =       1063
338148                 TA   =          317
48961
                                          MA   =          317
49868
                                          Ha   =            220
941  n
mi
                                          Hp   =            215
994

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3391448
11                 X    =        -1105718
52
 Y    =       13674782
73  feet           Y    =         4156111
02  meter
 Z    =       17205476
18                 Z    =         5239033
25
 XDOT =     -22801
740427                 XDOT =       -6920
373145
 YDOT =     -10047
613615  feet/sec       YDOT =       -3140
066640  meter/sec
 ZDOT =       3488
642219                 ZDOT =        1029
649626

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13841807
78                 X    =        -4218983
01
 Y    =        2780719
43  feet           Y    =          847563
28  meter
 Z    =       17181442
62                 Z    =         5236903
71
 XDOT =       -658
797745                 XDOT =        -200
801553
 YDOT =     -23913
854416  feet/sec       YDOT =       -7288
942826  meter/sec
 ZDOT =       3337
001793                 ZDOT =        1017
118147


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
54999475  
00016717  00000-0  10270-3 0  9018
2 25544  51
6404  30
4692 0002473 302
3646  57
7267 15
53768810 31840


Satellite: ISS
Catalog Number: 25544
Epoch time:      19017
54999475   =   yrday
fracday
Element set:     901
Inclination:       51
6404  deg
RA of node:        30
4692  deg
Eccentricity:     
0002473     
Arg of perigee:   302
3646  deg
Mean anomaly:      57
7267  deg
Mean motion:   15
53768810  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3184
Checksum:              322


Coasting Arc #3 (Orbit 3198)
---------------------------------------

Vector Time (GMT): 2019/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928709
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2524280
56                 A    =         6778669
09  meter
 Y    =       -3418345
52  meter          E    =           
0012389
 Z    =       -5292095
62                 I    =           51
78565
 XDOT =       6634
207695                 Wp   =           89
75994
 YDOT =       3754
504075  meter/sec      RA   =           25
11846  deg
 ZDOT =        740
841760                 TA   =          187
30283
                                          MA   =          187
32090
                                          Ha   =            220
950  n
mi
                                          Hp   =            216
103

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8281760
38                 X    =         2588023
66
 Y    =      -11215044
34  feet           Y    =        -3389760
31  meter
 Z    =      -17362518
43                 Z    =        -5279679
26
 XDOT =      21765
773279                 XDOT =        6588
132148
 YDOT =      12317
926756  feet/sec       YDOT =        3828
434705  meter/sec
 ZDOT =       2430
583202                 ZDOT =         772
956413

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13794563
14                 X    =         4204582
85
 Y    =        2456508
58  feet           Y    =          748743
82  meter
 Z    =      -17305993
59                 Z    =        -5274866
85
 XDOT =      -1042
538873                 XDOT =        -317
765848
 YDOT =      23959
355516  feet/sec       YDOT =        7302
811561  meter/sec
 ZDOT =       2575
016318                 ZDOT =         784
864974


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   19018
51475110  
00016717  00000-0  10270-3 0  9022
2 25544  51
6396  25
6635 0002563 305
6792  54
4122 15
53747440 31997


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
51475110   =   yrday
fracday
Element set:     902
Inclination:       51
6396  deg
RA of node:        25
6635  deg
Eccentricity:     
0002563     
Arg of perigee:   305
6792  deg
Mean anomaly:      54
4122  deg
Mean motion:   15
53747440  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3199
Checksum:              303


Coasting Arc #4 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2019/018/18:09:19
397
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1978558
02                 A    =         6780171
19  meter
 Y    =       -3711730
04  meter          E    =           
0010235
 Z    =       -5326608
92                 I    =           51
77910
 XDOT =       6910
970304                 Wp   =           86
86763
 YDOT =       3291
298565  meter/sec      RA   =           23
84693  deg
 ZDOT =        274
597325                 TA   =          185
74194
                                          MA   =          185
75368
                                          Ha   =            220
953  n
mi
                                          Hp   =            217
935

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6491332
10                 X    =         2045790
00
 Y    =      -12177592
01  feet           Y    =        -3689227
96  meter
 Z    =      -17475751
06                 Z    =        -5316835
03
 XDOT =      22673
787086                 XDOT =        6872
318617
 YDOT =      10798
223637  feet/sec       YDOT =        3368
365702  meter/sec
 ZDOT =        900
909858                 ZDOT =         308
074324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -199542
08                 X    =          -60820
43
 Y    =      -13854585
28  feet           Y    =        -4222877
59  meter
 Z    =      -17431111
96                 Z    =        -5313002
93
 XDOT =      24041
390062                 XDOT =        7327
815691
 YDOT =      -1665
131537  feet/sec       YDOT =        -507
532093  meter/sec
 ZDOT =       1051
556221                 ZDOT =         320
514336


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   19018
77202277  
00016717  00000-0  10270-3 0  9033
2 25544  51
6413  24
3813 0004715 283
8226  76
2402 15
53173002 32037


Satellite: ISS
Catalog Number: 25544
Epoch time:      19018
77202277   =   yrday
fracday
Element set:     903
Inclination:       51
6413  deg
RA of node:        24
3813  deg
Eccentricity:     
0004715     
Arg of perigee:   283
8226  deg
Mean anomaly:      76
2402  deg
Mean motion:   15
53173002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              274


Coasting Arc #5 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2019/019/18:09:19
397
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3248389
28                 A    =         6781230
78  meter
 Y    =        3116075
65  meter          E    =           
0004617
 Z    =        5073166
47                 I    =           51
75182
 XDOT =      -6443
067076                 Wp   =          358
62420
 YDOT =      -3727
559557  meter/sec      RA   =           18
86718  deg
 ZDOT =      -1831
508506                 TA   =          109
11272
                                          MA   =          109
06272
                                          Ha   =            221
063  n
mi
                                          Hp   =            217
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10657445
15                 X    =        -3307634
90
 Y    =       10223345
31  feet           Y    =         3079418
10  meter
 Z    =       16644246
93                 Z    =         5057243
71
 XDOT =     -21138
671510                 XDOT =       -6392
009300
 YDOT =     -12229
526105  feet/sec       YDOT =       -3799
324743  meter/sec
 ZDOT =      -6008
886175                 ZDOT =       -1862
682372

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4140353
73                 X    =        -1261979
82
 Y    =       14260340
16  feet           Y    =         4346551
68  meter
 Z    =       16571935
67                 Z    =         5051125
99
 XDOT =     -23346
458776                 XDOT =       -7116
000635
 YDOT =        384
535787  feet/sec       YDOT =         117
206508  meter/sec
 ZDOT =      -6149
072281                 ZDOT =       -1874
237231


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   19019
80149532  
00016717  00000-0  10270-3 0  9043
2 25544  51
6411  19
2573 0004922 287
4621  72
5993 15
53196396 32192


Satellite: ISS
Catalog Number: 25544
Epoch time:      19019
80149532   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:        19
2573  deg
Eccentricity:     
0004922     
Arg of perigee:   287
4621  deg
Mean anomaly:      72
5993  deg
Mean motion:   15
53196396  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3219
Checksum:              319


Coasting Arc #6 (Orbit 3223)
---------------------------------------

Vector Time (GMT): 2019/020/01:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2285744
68                 A    =         6783215
62  meter
 Y    =        4475627
68  meter          E    =           
0004069
 Z    =        4554297
71                 I    =           51
74656
 XDOT =      -6992
641574                 Wp   =          125
98679
 YDOT =        392
714656  meter/sec      RA   =           17
34351  deg
 ZDOT =       3119
305226                 TA   =          292
78681
                                          MA   =          292
82980
                                          Ha   =            220
846  n
mi
                                          Hp   =            217
861

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7499162
35                 X    =         2213405
25
 Y    =       14683817
84  feet           Y    =         4500783
52  meter
 Z    =       14941921
63                 Z    =         4565225
56
 XDOT =     -22941
737447                 XDOT =       -7011
664881
 YDOT =       1288
433910  feet/sec       YDOT =         314
411380  meter/sec
 ZDOT =      10233
941031                 ZDOT =        3085
292070

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2851658
15                 X    =          869185
40
 Y    =      -16194518
89  feet           Y    =        -4936089
36  meter
 Z    =       14990616
00                 Z    =         4569139
76
 XDOT =      18031
710932                 XDOT =        5496
065492
 YDOT =      12519
111854  feet/sec       YDOT =        3815
825293  meter/sec
 ZDOT =      10080
358139                 ZDOT =        3072
493161


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   19020
12320502  
00016717  00000-0  10270-3 0  9059
2 25544  51
6390  17
6499 0004748 282
6444  77
4177 15
53188799 32245


Satellite: ISS
Catalog Number: 25544
Epoch time:      19020
12320502   =   yrday
fracday
Element set:     905
Inclination:       51
6390  deg
RA of node:        17
6499  deg
Eccentricity:     
0004748     
Arg of perigee:   282
6444  deg
Mean anomaly:      77
4177  deg
Mean motion:   15
53188799  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3224
Checksum:              318


Coasting Arc #7 (Orbit 3238)
---------------------------------------

Vector Time (GMT): 2019/021/01:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -974766
93                 A    =         6780980
25  meter
 Y    =       -4350475
27  meter          E    =           
0009853
 Z    =       -5118019
02                 I    =           51
70775
 XDOT =       7470
212749                 Wp   =           63
73077
 YDOT =        289
855178  meter/sec      RA   =           12
36439  deg
 ZDOT =      -1667
379965                 TA   =          190
15669
                                          MA   =          190
17661
                                          Ha   =            221
082  n
mi
                                          Hp   =            217
733

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3198054
23                 X    =         -901186
37
 Y    =      -14273212
82  feet           Y    =        -4360963
93  meter
 Z    =      -16791400
98                 Z    =        -5122575
62
 XDOT =      24508
572011                 XDOT =        7474
515316
 YDOT =        950
968431  feet/sec       YDOT =         373
416501  meter/sec
 ZDOT =      -5470
406708                 ZDOT =       -1631
082888

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5833824
47                 X    =        -1778149
70
 Y    =       13388357
39  feet           Y    =         4080771
33  meter
 Z    =      -16811355
70                 Z    =        -5124101
22
 XDOT =     -18389
930186                 XDOT =       -5605
250721
 YDOT =     -14683
826134  feet/sec       YDOT =       -4475
630206  meter/sec
 ZDOT =      -5306
613238                 ZDOT =       -1617
455715


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   19021
08833466  
00016717  00000-0  10270-3 0  9064
2 25544  51
6398  12
8465 0004558 288
3080  71
7576 15
53181749 32395


Satellite: ISS
Catalog Number: 25544
Epoch time:      19021
08833466   =   yrday
fracday
Element set:     906
Inclination:       51
6398  deg
RA of node:        12
8465  deg
Eccentricity:     
0004558     
Arg of perigee:   288
3080  deg
Mean anomaly:      71
7576  deg
Mean motion:   15
53181749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3239
Checksum:              333


Coasting Arc #8 (Orbit 3254)
---------------------------------------

Vector Time (GMT): 2019/022/01:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -424945
77                 A    =         6780180
84  meter
 Y    =        4185071
52  meter          E    =           
0002454
 Z    =        5319052
14                 I    =           51
67177
 XDOT =      -7611
937905                 Wp   =          310
62996
 YDOT =       -902
852786  meter/sec      RA   =            7
37786  deg
 ZDOT =        103
837031                 TA   =          138
39002
                                          MA   =          138
37135
                                          Ha   =            221
261  n
mi
                                          Hp   =            217
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1394179
02                 X    =         -497549
10
 Y    =       13730549
62  feet           Y    =         4179913
22  meter
 Z    =       17450958
46                 Z    =         5316811
88
 XDOT =     -24973
549556                 XDOT =       -7601
780591
 YDOT =      -2962
115438  feet/sec       YDOT =        -987
917991  meter/sec
 ZDOT =        340
672675                 ZDOT =          66
886750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9069716
06                 X    =         2764449
46
 Y    =      -10420423
24  feet           Y    =        -3176145
00  meter
 Z    =       17440261
15                 Z    =         5315791
60
 XDOT =      18070
466854                 XDOT =        5507
878297
 YDOT =      16010
653977  feet/sec       YDOT =        4880
047332  meter/sec
 ZDOT =        174
021353                 ZDOT =          53
041708


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   19022
11780521  
00016717  00000-0  10270-3 0  9073
2 25544  51
6395   7
7210 0004594 292
1610  67
9054 15
53156728 32550


Satellite: ISS
Catalog Number: 25544
Epoch time:      19022
11780521   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:         7
7210  deg
Eccentricity:     
0004594     
Arg of perigee:   292
1610  deg
Mean anomaly:      67
9054  deg
Mean motion:   15
53156728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3255
Checksum:              297


Coasting Arc #9 (Orbit 3269)
---------------------------------------

Vector Time (GMT): 2019/023/01:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1821100
78                 A    =         6780859
80  meter
 Y    =       -4012699
15  meter          E    =           
0009261
 Z    =       -5161964
38                 I    =           51
64196
 XDOT =       7374
554658                 Wp   =           94
38664
 YDOT =       1466
758728  meter/sec      RA   =            2
39070  deg
 ZDOT =       1463
060633                 TA   =          189
70209
                                          MA   =          189
71999
                                          Ha   =            221
272  n
mi
                                          Hp   =            217
763

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5974740
11                 X    =         1890909
80
 Y    =      -13165023
47  feet           Y    =        -3991943
87  meter
 Z    =      -16935578
66                 Z    =        -5152948
96
 XDOT =      24194
733129                 XDOT =        7350
498332
 YDOT =       4812
200550  feet/sec       YDOT =        1549
091591  meter/sec
 ZDOT =       4800
067695                 ZDOT =        1498
824040

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12379426
70                 X    =        -3773249
26
 Y    =        7560458
42  feet           Y    =         2304427
73  meter
 Z    =      -16894331
90                 Z    =        -5149392
36
 XDOT =     -16858
437023                 XDOT =       -5138
451605
 YDOT =     -16529
123046  feet/sec       YDOT =       -5038
076704  meter/sec
 ZDOT =       4961
276550                 ZDOT =        1512
197092


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   19023
08293147  
00016717  00000-0  10270-3 0  9084
2 25544  51
6404   2
9178 0004607 294
8562  65
2111 15
53184421 32704


Satellite: ISS
Catalog Number: 25544
Epoch time:      19023
08293147   =   yrday
fracday
Element set:     908
Inclination:       51
6404  deg
RA of node:         2
9178  deg
Eccentricity:     
0004607     
Arg of perigee:   294
8562  deg
Mean anomaly:      65
2111  deg
Mean motion:   15
53184421  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3270
Checksum:              292


Coasting Arc #10 (Orbit 3285)
---------------------------------------

Vector Time (GMT): 2019/024/01:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3150442
00                 A    =         6783160
48  meter
 Y    =        3819207
29  meter          E    =           
0006795
 Z    =        4636405
98                 I    =           51
61699
 XDOT =      -6785
887148                 Wp   =           32
36460
 YDOT =      -2021
787287  meter/sec      RA   =          357
40294  deg
 ZDOT =      -2937
973284                 TA   =           86
94338
                                          MA   =           86
86562
                                          Ha   =            221
540  n
mi
                                          Hp   =            217
682

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10336095
79                 X    =        -3215435
79
 Y    =       12530207
65  feet           Y    =         3783613
45  meter
 Z    =       15211305
70                 Z    =         4620944
86
 XDOT =     -22263
409277                 XDOT =       -6748
503951
 YDOT =      -6633
160391  feet/sec       YDOT =       -2097
462786  meter/sec
 ZDOT =      -9639
019959                 ZDOT =       -2970
844916

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15560537
55                 X    =         4742851
85
 Y    =       -4883081
57  feet           Y    =        -1488363
26  meter
 Z    =       15141003
48                 Z    =         4614977
86
 XDOT =      14713
898261                 XDOT =        4484
796190
 YDOT =      16462
963740  feet/sec       YDOT =        5017
911348  meter/sec
 ZDOT =      -9787
092206                 ZDOT =       -2983
105704


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   19024
11239907  
00016717  00000-0  10270-3 0  9094
2 25544  51
6414 357
7926 0004532 299
4380  60
6320 15
53147594 32861


Satellite: ISS
Catalog Number: 25544
Epoch time:      19024
11239907   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:       357
7926  deg
Eccentricity:     
0004532     
Arg of perigee:   299
4380  deg
Mean anomaly:      60
6320  deg
Mean motion:   15
53147594  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3286
Checksum:              319


Coasting Arc #11 (Orbit 3300)
---------------------------------------

Vector Time (GMT): 2019/025/01:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928366
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4304438
54                 A    =         6786108
65  meter
 Y    =       -3614334
00  meter          E    =           
0002287
 Z    =       -3803120
75                 I    =           51
59378
 XDOT =       5870
603806                 Wp   =           55
46796
 YDOT =       2576
745583  meter/sec      RA   =          352
42046  deg
 ZDOT =       4198
684391                 TA   =          258
87733
                                          MA   =          258
90305
                                          Ha   =            221
641  n
mi
                                          Hp   =            217
708

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14122173
67                 X    =         4363008
16
 Y    =      -11858051
18  feet           Y    =        -3565871
34  meter
 Z    =      -12477430
28                 Z    =        -3782069
56
 XDOT =      19260
511175                 XDOT =        5820
959180
 YDOT =       8453
889709  feet/sec       YDOT =        2642
117253  meter/sec
 ZDOT =      13775
211256                 ZDOT =        4227
080330

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18322080
29                 X    =        -5584570
07
 Y    =        2593140
21  feet           Y    =          790389
14  meter
 Z    =      -12381939
71                 Z    =        -3774015
22
 XDOT =     -11646
184802                 XDOT =       -3549
757128
 YDOT =     -15950
480357  feet/sec       YDOT =       -4861
706413  meter/sec
 ZDOT =      13903
000337                 ZDOT =        4237
634503


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   19025
07752164  
00016717  00000-0  10270-3 0  9107
2 25544  51
6413 352
9894 0004705 303
7276  56
3427 15
53161635 33016


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
07752164   =   yrday
fracday
Element set:     910
Inclination:       51
6413  deg
RA of node:       352
9894  deg
Eccentricity:     
0004705     
Arg of perigee:   303
7276  deg
Mean anomaly:      56
3427  deg
Mean motion:   15
53161635  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3301
Checksum:              297


Coasting Arc #12 (Orbit 3308)
---------------------------------------

Vector Time (GMT): 2019/025/12:55:00
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4234021
70                 A    =         6783463
40  meter
 Y    =        2856288
50  meter          E    =           
0004538
 Z    =        4460476
23                 I    =           51
56885
 XDOT =      -5902
038149                 Wp   =           92
12918
 YDOT =       3652
147403  meter/sec      RA   =          350
13778  deg
 ZDOT =       3260
690920                 TA   =          324
98093
                                          MA   =          325
01077
                                          Ha   =            221
596  n
mi
                                          Hp   =            217
500

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13891147
31                 X    =         4180101
12
 Y    =        9371025
26  feet           Y    =         2903334
88  meter
 Z    =       14634108
37                 Z    =         4480912
09
 XDOT =     -19363
642221                 XDOT =       -5958
277145
 YDOT =      11982
110902  feet/sec       YDOT =        3585
832305  meter/sec
 ZDOT =      10697
804856                 ZDOT =        3231
884958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3812558
50                 X    =         1162067
83
 Y    =       16234174
73  feet           Y    =         4948176
46  meter
 Z    =       14725935
77                 Z    =         4488465
22
 XDOT =     -21233
791807                 XDOT =       -6472
059743
 YDOT =      -4607
830525  feet/sec       YDOT =       -1404
466744  meter/sec
 ZDOT =      10567
321129                 ZDOT =        3220
919480


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   19025
59225264  
00016717  00000-0  10270-3 0  9111
2 25544  51
6399 350
4307 0004941 309
3121  50
7592 15
53208604 33091


Satellite: ISS
Catalog Number: 25544
Epoch time:      19025
59225264   =   yrday
fracday
Element set:     911
Inclination:       51
6399  deg
RA of node:       350
4307  deg
Eccentricity:     
0004941     
Arg of perigee:   309
3121  deg
Mean anomaly:      50
7592  deg
Mean motion:   15
53208604  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3309
Checksum:              296


Coasting Arc #13 (Orbit 3321)
---------------------------------------

Vector Time (GMT): 2019/026/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4747806
62                 A    =         6784316
52  meter
 Y    =        2300997
63  meter          E    =           
0005898
 Z    =        4259667
79                 I    =           51
54308
 XDOT =      -5280
110983                 Wp   =           85
57063
 YDOT =       4252
914730  meter/sec      RA   =          345
97425  deg
 ZDOT =       3584
000312                 TA   =          327
77005
                                          MA   =          327
80607
                                          Ha   =            221
785  n
mi
                                          Hp   =            217
421

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15576793
38                 X    =         4701032
61
 Y    =        7549204
83  feet           Y    =         2353829
46  meter
 Z    =       13975288
03                 Z    =         4282616
82
 XDOT =     -17323
198764                 XDOT =       -5344
684634
 YDOT =      13953
132316  feet/sec       YDOT =        4193
507852  meter/sec
 ZDOT =      11758
531206                 ZDOT =        3558
195046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10339298
91                 X    =        -3151418
31
 Y    =       13777868
76  feet           Y    =         4199494
40  meter
 Z    =       14078525
91                 Z    =         4291134
70
 XDOT =      -9410
528999                 XDOT =       -2868
329239
 YDOT =     -18970
252286  feet/sec       YDOT =       -5782
132897  meter/sec
 ZDOT =      11641
517138                 ZDOT =        3548
334424


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   19026
42869263  
00016717  00000-0  10270-3 0  9128
2 25544  51
6389 346
2668 0004836 313
6018  46
4732 15
53167840 33228


Satellite: ISS
Catalog Number: 25544
Epoch time:      19026
42869263   =   yrday
fracday
Element set:     912
Inclination:       51
6389  deg
RA of node:       346
2668  deg
Eccentricity:     
0004836     
Arg of perigee:   313
6018  deg
Mean anomaly:      46
4732  deg
Mean motion:   15
53167840  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3322
Checksum:              320


Coasting Arc #14 (Orbit 3336)
---------------------------------------

Vector Time (GMT): 2019/027/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3633148
95                 A    =         6781659
16  meter
 Y    =       -2906795
17  meter          E    =           
0011229
 Z    =       -4943722
96                 I    =           51
50268
 XDOT =       6168
901778                 Wp   =           51
32632
 YDOT =      -3972
355793  meter/sec      RA   =          340
98224  deg
 ZDOT =      -2194
389200                 TA   =          197
17842
                                          MA   =          197
21645
                                          Ha   =            222
024  n
mi
                                          Hp   =            217
131

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11919780
03                 X    =        -3576360
81
 Y    =       -9536729
55  feet           Y    =        -2947106
08  meter
 Z    =      -16219563
52                 Z    =        -4961233
24
 XDOT =      20239
179063                 XDOT =        6223
522271
 YDOT =     -13032
663364  feet/sec       YDOT =       -3903
065445  meter/sec
 ZDOT =      -7199
439633                 ZDOT =       -2164
290724

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11427259
77                 X    =         3483028
78
 Y    =       -9994590
78  feet           Y    =        -3046351
27  meter
 Z    =      -16298174
63                 Z    =        -4967683
63
 XDOT =       8620
781678                 XDOT =        2627
614255
 YDOT =      21392
915571  feet/sec       YDOT =        6520
560666  meter/sec
 ZDOT =      -7063
104898                 ZDOT =       -2152
834373


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   19027
39381261  
00016717  00000-0  10270-3 0  9133
2 25544  51
6393 341
4628 0004752 318
4334  41
6456 15
53179431 33372


Satellite: ISS
Catalog Number: 25544
Epoch time:      19027
39381261   =   yrday
fracday
Element set:     913
Inclination:       51
6393  deg
RA of node:       341
4628  deg
Eccentricity:     
0004752     
Arg of perigee:   318
4334  deg
Mean anomaly:      41
6456  deg
Mean motion:   15
53179431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3337
Checksum:              309


Coasting Arc #15 (Orbit 3352)
---------------------------------------

Vector Time (GMT): 2019/028/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2383124
70                 A    =         6780253
14  meter
 Y    =        3535042
89  meter          E    =           
0002683
 Z    =        5272301
52                 I    =           51
46561
 XDOT =      -6749
524310                 Wp   =          351
08240
 YDOT =       3578
082722  meter/sec      RA   =          335
98283  deg
 ZDOT =        654
404272                 TA   =           92
66889
                                          MA   =           92
63817
                                          Ha   =            222
119  n
mi
                                          Hp   =            217
196

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7818650
58                 X    =         2317808
15
 Y    =       11597909
74  feet           Y    =         3561327
40  meter
 Z    =       17297577
16                 Z    =         5283719
08
 XDOT =     -22144
108627                 XDOT =       -6792
212495
 YDOT =      11739
116543  feet/sec       YDOT =        3502
366147  meter/sec
 ZDOT =       2146
995642                 ZDOT =         621
514376

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12653084
43                 X    =        -3856660
13
 Y    =        5811544
91  feet           Y    =         1771358
89  meter
 Z    =       17348613
29                 Z    =         5287857
33
 XDOT =      -7738
407726                 XDOT =       -2358
666675
 YDOT =     -22787
322147  feet/sec       YDOT =       -6945
575790  meter/sec
 ZDOT =       1998
131401                 ZDOT =         609
030451


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   19028
42327195  
00016717  00000-0  10270-3 0  9145
2 25544  51
6381 336
3379 0004915 321
8957  38
1847 15
53173158 33538


Satellite: ISS
Catalog Number: 25544
Epoch time:      19028
42327195   =   yrday
fracday
Element set:     914
Inclination:       51
6381  deg
RA of node:       336
3379  deg
Eccentricity:     
0004915     
Arg of perigee:   321
8957  deg
Mean anomaly:      38
1847  deg
Mean motion:   15
53173158  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3353
Checksum:              327


Coasting Arc #16 (Orbit 3367)
---------------------------------------

Vector Time (GMT): 2019/029/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1114107
47                 A    =         6780473
37  meter
 Y    =       -4163222
13  meter          E    =           
0011671
 Z    =       -5244229
64                 I    =           51
43607
 XDOT =       6974
613726                 Wp   =           78
70392
 YDOT =      -3026
167249  meter/sec      RA   =          330
98054  deg
 ZDOT =        924
647847                 TA   =          200
15516
                                          MA   =          200
20128
                                          Ha   =            222
282  n
mi
                                          Hp   =            217
042

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3655208
23                 X    =        -1041997
13
 Y    =      -13658865
27  feet           Y    =        -4175277
55  meter
 Z    =      -17205477
83                 Z    =        -5249466
44
 XDOT =      22882
590964                 XDOT =        7003
443450
 YDOT =      -9928
370241  feet/sec       YDOT =       -2948
011080  meter/sec
 ZDOT =       3033
621545                 ZDOT =         958
597417

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14017958
66                 X    =         4272673
80
 Y    =       -1620994
17  feet           Y    =         -494079
02  meter
 Z    =      -17228546
89                 Z    =        -5251261
09
 XDOT =       6559
699280                 XDOT =        1999
396340
 YDOT =      22991
037079  feet/sec       YDOT =        7007
668102  meter/sec
 ZDOT =       3187
182773                 ZDOT =         971
453309


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   19029
38838906  
00016717  00000-0  10270-3 0  9159
2 25544  51
6379 331
5341 0004937 325
5591  34
5241 15
53164858 33681


Satellite: ISS
Catalog Number: 25544
Epoch time:      19029
38838906   =   yrday
fracday
Element set:     915
Inclination:       51
6379  deg
RA of node:       331
5341  deg
Eccentricity:     
0004937     
Arg of perigee:   325
5591  deg
Mean anomaly:      34
5241  deg
Mean motion:   15
53164858  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3368
Checksum:              334


Coasting Arc #17 (Orbit 3383)
---------------------------------------

Vector Time (GMT): 2019/030/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -146188
84                 A    =         6782154
52  meter
 Y    =        4753566
98  meter          E    =           
0008632
 Z    =        4835250
74                 I    =           51
41365
 XDOT =      -6892
368501                 Wp   =           24
30152
 YDOT =       2292
005195  meter/sec      RA   =          325
97745  deg
 ZDOT =      -2452
387153                 TA   =           89
90515
                                          MA   =           89
80624
                                          Ha   =            222
391  n
mi
                                          Hp   =            216
955

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -479622
18                 X    =         -222820
31
 Y    =       15595692
20  feet           Y    =         4751503
56  meter
 Z    =       15863683
51                 Z    =         4834354
65
 XDOT =     -22612
757548                 XDOT =       -6905
573943
 YDOT =       7519
702084  feet/sec       YDOT =        2214
856171  meter/sec
 ZDOT =      -8045
889611                 ZDOT =       -2485
899188

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15411473
87                 X    =        -4697417
24
 Y    =       -2467861
59  feet           Y    =         -752204
21  meter
 Z    =       15859011
30                 Z    =         4833826
65
 XDOT =      -4915
285966                 XDOT =       -1498
179162
 YDOT =     -22178
513151  feet/sec       YDOT =       -6760
010808  meter/sec
 ZDOT =      -8197
371613                 ZDOT =       -2498
558868


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   19030
41784478  
00016717  00000-0  10270-3 0  9160
2 25544  51
6382 326
4091 0005020 328
8231  31
2623 15
53191696 33847


Satellite: ISS
Catalog Number: 25544
Epoch time:      19030
41784478   =   yrday
fracday
Element set:     916
Inclination:       51
6382  deg
RA of node:       326
4091  deg
Eccentricity:     
0005020     
Arg of perigee:   328
8231  deg
Mean anomaly:      31
2623  deg
Mean motion:   15
53191696  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3384
Checksum:              301


Coasting Arc #18 (Orbit 3398)
---------------------------------------

Vector Time (GMT): 2019/031/08:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 913933
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1274493
96                 A    =         6785004
56  meter
 Y    =       -5251619
09  meter          E    =           
0005214
 Z    =       -4105245
15                 I    =           51
39652
 XDOT =       6513
452257                 Wp   =           64
69830
 YDOT =      -1380
097777  meter/sec      RA   =          320
97830  deg
 ZDOT =       3793
586232                 TA   =          244
58215
                                          MA   =          244
63613
                                          Ha   =            222
580  n
mi
                                          Hp   =            216
841

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4181410
64                 X    =         1353064
96
 Y    =      -17229721
41  feet           Y    =        -5236927
33  meter
 Z    =      -13468652
08                 Z    =        -4098863
63
 XDOT =      21369
594020                 XDOT =        6509
974010
 YDOT =      -4527
879845  feet/sec       YDOT =       -1307
279413  meter/sec
 ZDOT =      12446
149054                 ZDOT =        3825
217067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16693855
34                 X    =         5088287
11
 Y    =        6037866
61  feet           Y    =         1840341
74  meter
 Z    =      -13439175
74                 Z    =        -4096260
77
 XDOT =       2731
963582                 XDOT =         832
702500
 YDOT =      20423
660573  feet/sec       YDOT =        6225
131743  meter/sec
 ZDOT =      12589
018968                 ZDOT =        3837
132981


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   19031
38295734  
00016717  00000-0  10270-3 0  9170
2 25544  51
6387 321
6050 0005104 333
7895  26
2998 15
53172272 33992


Satellite: ISS
Catalog Number: 25544
Epoch time:      19031
38295734   =   yrday
fracday
Element set:     917
Inclination:       51
6387  deg
RA of node:       321
6050  deg
Eccentricity:     
0005104     
Arg of perigee:   333
7895  deg
Mean anomaly:      26
2998  deg
Mean motion:   15
53172272  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3399
Checksum:              326
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