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

 
Date: July 2nd 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19800 2132 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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


184/00:18:16 773 0 9 1 7 1 7
N/A -0 4 -0 2 228 6
000/00:00:33 545 1 3 0 1 217 1

184/09:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 217 0

187/16:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 217 2

194/07:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 2
000/00:00:00 000 0 0 0 0 217 7

Coasting Arc #1 (Orbit 1746)
---------------------------------------

Vector Time (GMT): 2019/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -993620
60                 A    =         6796748
56  meter
 Y    =        6532971
43  meter          E    =           
0021995
 Z    =        1547931
73                 I    =           51
29734
 XDOT =      -5072
581877                 Wp   =          113
71612
 YDOT =        597
239036  meter/sec      RA   =          289
46577  deg
 ZDOT =      -5720
736798                 TA   =           49
29106
                                          MA   =           49
10021
                                          Ha   =            228
488  n
mi
                                          Hp   =            216
300

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3259910
12                 X    =        -1074119
29
 Y    =       21433633
30  feet           Y    =         6521409
67  meter
 Z    =        5078516
19                 Z    =         1542910
86
 XDOT =     -16642
328992                 XDOT =       -5051
095281
 YDOT =       1959
445656  feet/sec       YDOT =         540
635123  meter/sec
 ZDOT =     -18768
821516                 ZDOT =       -5745
325143

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21685152
24                 X    =         6609634
40
 Y    =         140729
03  feet           Y    =           42894
21  meter
 Z    =        5055031
63                 Z    =         1540773
64
 XDOT =       4350
291663                 XDOT =        1325
968899
 YDOT =      14473
941132  feet/sec       YDOT =        4411
657257  meter/sec
 ZDOT =     -18880
370152                 ZDOT =       -5754
736822


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   19182
53529039  
00016717  00000-0  10270-3 0  9004
2 25544  51
6427 290
0903 0008200 107
5802 252
6245 15
51237824 17476


Satellite: ISS
Catalog Number: 25544
Epoch time:      19182
53529039   =   yrday
fracday
Element set:     900
Inclination:       51
6427  deg
RA of node:       290
0903  deg
Eccentricity:     
0008200     
Arg of perigee:   107
5802  deg
Mean anomaly:     252
6245  deg
Mean motion:   15
51237824  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1747
Checksum:              294


Coasting Arc #2 (Orbit 1761)
---------------------------------------

Vector Time (GMT): 2019/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916459
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1027554
44                 A    =         6797436
38  meter
 Y    =       -6664799
37  meter          E    =           
0014987
 Z    =        -838612
39                 I    =           51
29039
 XDOT =       4880
930654                 Wp   =           69
97220
 YDOT =         21
212266  meter/sec      RA   =          284
48444  deg
 ZDOT =       5903
346471                 TA   =          280
92837
                                          MA   =          281
09695
                                          Ha   =            228
446  n
mi
                                          Hp   =            216
351

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3371241
62                 X    =         1106079
25
 Y    =      -21866139
66  feet           Y    =        -6652869
31  meter
 Z    =       -2751352
97                 Z    =         -833431
56
 XDOT =      16013
552015                 XDOT =        4851
655740
 YDOT =         69
594050  feet/sec       YDOT =          75
629389  meter/sec
 ZDOT =      19367
934615                 ZDOT =        5926
984929

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -22126514
77                 X    =        -6744161
70
 Y    =         208131
15  feet           Y    =           63438
38  meter
 Z    =       -2727141
81                 Z    =         -831232
82
 XDOT =      -2495
448659                 XDOT =        -760
612751
 YDOT =     -14070
011932  feet/sec       YDOT =       -4288
539637  meter/sec
 ZDOT =      19475
114339                 ZDOT =        5936
014850


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   19183
50161033  
00016717  00000-0  10270-3 0  9019
2 25544  51
6435 285
2952 0008092 109
9256 250
2768 15
51241213 17621


Satellite: ISS
Catalog Number: 25544
Epoch time:      19183
50161033   =   yrday
fracday
Element set:     901
Inclination:       51
6435  deg
RA of node:       285
2952  deg
Eccentricity:     
0008092     
Arg of perigee:   109
9256  deg
Mean anomaly:     250
2768  deg
Mean motion:   15
51241213  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1762
Checksum:              294


Coasting Arc #3 (Orbit 1769)
---------------------------------------

Vector Time (GMT): 2019/184/00:18:33
545
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -327874
77                 A    =         6796771
18  meter
 Y    =       -6467560
05  meter          E    =           
0011839
 Z    =       -2066167
20                 I    =           51
28065
 XDOT =       4932
623393                 Wp   =           72
27024
 YDOT =      -1999
244375  meter/sec      RA   =          281
91822  deg
 ZDOT =       5505
035712                 TA   =          264
80119
                                          MA   =          264
93631
                                          Ha   =            228
591  n
mi
                                          Hp   =            217
069

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1075704
62                 X    =         -245492
11
 Y    =      -21219029
04  feet           Y    =        -6470765
54  meter
 Z    =       -6778763
78                 Z    =        -2067561
07
 XDOT =      16183
147614                 XDOT =        4927
872796
 YDOT =      -6559
200705  feet/sec       YDOT =       -1944
111975  meter/sec
 ZDOT =      18061
140788                 ZDOT =        5528
984367

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20286129
97                 X    =         6183212
42
 Y    =       -6308795
88  feet           Y    =        -1922920
98  meter
 Z    =       -6784393
67                 Z    =        -2067883
19
 XDOT =       9909
488862                 XDOT =        3020
412205
 YDOT =      12429
270982  feet/sec       YDOT =        3788
441795  meter/sec
 ZDOT =      18169
946339                 ZDOT =        5538
199644


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   19184
01698103  
00016717  00000-0  10270-3 0  9020
2 25544  51
6428 282
7403 0007133 100
9727 259
2227 15
50950203 17708


Satellite: ISS
Catalog Number: 25544
Epoch time:      19184
01698103   =   yrday
fracday
Element set:     902
Inclination:       51
6428  deg
RA of node:       282
7403  deg
Eccentricity:     
0007133     
Arg of perigee:   100
9727  deg
Mean anomaly:     259
2227  deg
Mean motion:   15
50950203  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1770
Checksum:              292


Coasting Arc #4 (Orbit 1776)
---------------------------------------

Vector Time (GMT): 2019/184/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3324596
90                 A    =         6794679
10  meter
 Y    =       -5113194
45  meter          E    =           
0019952
 Z    =        2978264
30                 I    =           51
27137
 XDOT =       3152
812342                 Wp   =           91
46441
 YDOT =       4944
395446  meter/sec      RA   =          279
97660  deg
 ZDOT =       4939
992247                 TA   =          302
76284
                                          MA   =          302
95495
                                          Ha   =            228
504  n
mi
                                          Hp   =            217
013

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10907470
13                 X    =         3367060
44
 Y    =      -16775572
33  feet           Y    =        -5075779
63  meter
 Z    =        9771208
32                 Z    =         2994515
88
 XDOT =      10343
872514                 XDOT =        3073
292947
 YDOT =      16221
769835  feet/sec       YDOT =        4979
206820  meter/sec
 ZDOT =      16207
323644                 ZDOT =        4955
115063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11419929
55                 X    =        -3480794
53
 Y    =      -16386632
85  feet           Y    =        -4994645
69  meter
 Z    =        9845441
42                 Z    =         3000890
54
 XDOT =      17695
515798                 XDOT =        5393
593215
 YDOT =      -2496
207216  feet/sec       YDOT =        -760
843959  meter/sec
 ZDOT =      16275
375454                 ZDOT =        4960
734438


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   19184
46801674  
00016717  00000-0  10270-3 0  9039
2 25544  51
6428 280
4979 0007236 107
3224 252
8719 15
50985924 17778


Satellite: ISS
Catalog Number: 25544
Epoch time:      19184
46801674   =   yrday
fracday
Element set:     903
Inclination:       51
6428  deg
RA of node:       280
4979  deg
Eccentricity:     
0007236     
Arg of perigee:   107
3224  deg
Mean anomaly:     252
8719  deg
Mean motion:   15
50985924  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1777
Checksum:              341


Coasting Arc #5 (Orbit 1791)
---------------------------------------

Vector Time (GMT): 2019/185/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3260871
85                 A    =         6793265
94  meter
 Y    =        4809513
52  meter          E    =           
0012209
 Z    =       -3527646
45                 I    =           51
26145
 XDOT =      -3123
388798                 Wp   =           99
16608
 YDOT =      -5379
164230  meter/sec      RA   =          274
99108  deg
 ZDOT =      -4461
837431                 TA   =          122
53978
                                          MA   =          122
42178
                                          Ha   =            228
589  n
mi
                                          Hp   =            217
027

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10698398
45                 X    =        -3297275
81
 Y    =       15779243
82  feet           Y    =         4772845
25  meter
 Z    =      -11573643
22                 Z    =        -3543573
83
 XDOT =     -10247
338577                 XDOT =       -3041
332563
 YDOT =     -17648
176609  feet/sec       YDOT =       -5413
632551  meter/sec
 ZDOT =     -14638
574250                 ZDOT =       -4476
811087

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10851750
20                 X    =         3307613
46
 Y    =       15620217
53  feet           Y    =         4761042
30  meter
 Z    =      -11646364
42                 Z    =        -3549811
88
 XDOT =     -18989
319327                 XDOT =       -5787
944531
 YDOT =       2264
607279  feet/sec       YDOT =         690
252299  meter/sec
 ZDOT =     -14705
924551                 ZDOT =       -4482
365803


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   19185
43452582  
00016717  00000-0  10270-3 0  9048
2 25544  51
6426 275
7034 0007310 109
6742 250
5198 15
50949998 17922


Satellite: ISS
Catalog Number: 25544
Epoch time:      19185
43452582   =   yrday
fracday
Element set:     904
Inclination:       51
6426  deg
RA of node:       275
7034  deg
Eccentricity:     
0007310     
Arg of perigee:   109
6742  deg
Mean anomaly:     250
5198  deg
Mean motion:   15
50949998  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1792
Checksum:              334


Coasting Arc #6 (Orbit 1807)
---------------------------------------

Vector Time (GMT): 2019/186/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3185076
73                 A    =         6791737
42  meter
 Y    =       -4487950
28  meter          E    =           
0018075
 Z    =        3968758
89                 I    =           51
25446
 XDOT =       3168
775524                 Wp   =          105
89346
 YDOT =       5758
950910  meter/sec      RA   =          270
00407  deg
 ZDOT =       3949
351880                 TA   =          302
69398
                                          MA   =          302
86816
                                          Ha   =            228
455  n
mi
                                          Hp   =            217
073

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10449726
80                 X    =         3215747
92
 Y    =      -14724246
32  feet           Y    =        -4452161
64  meter
 Z    =       13020862
50                 Z    =         3984304
30
 XDOT =      10396
245159                 XDOT =        3084
958406
 YDOT =      18894
195898  feet/sec       YDOT =        5793
917121  meter/sec
 ZDOT =      12957
191208                 ZDOT =        3964
541614

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10218725
88                 X    =        -3114667
65
 Y    =      -14823133
44  feet           Y    =        -4518091
07  meter
 Z    =       13091808
00                 Z    =         3990383
08
 XDOT =      20216
086476                 XDOT =        6161
863158
 YDOT =      -2374
947254  feet/sec       YDOT =        -723
883923  meter/sec
 ZDOT =      13025
505588                 ZDOT =        3970
174103


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   19186
46546460  
00016717  00000-0  10270-3 0  9052
2 25544  51
6422 270
5895 0007281 113
6717 246
5199 15
50989459 18080


Satellite: ISS
Catalog Number: 25544
Epoch time:      19186
46546460   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       270
5895  deg
Eccentricity:     
0007281     
Arg of perigee:   113
6717  deg
Mean anomaly:     246
5199  deg
Mean motion:   15
50989459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1808
Checksum:              346


Coasting Arc #7 (Orbit 1822)
---------------------------------------

Vector Time (GMT): 2019/187/09:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3186044
21                 A    =         6790366
62  meter
 Y    =        4090462
71  meter          E    =           
0014909
 Z    =       -4397679
64                 I    =           51
25066
 XDOT =      -3220
180495                 Wp   =           90
56530
 YDOT =      -6086
356197  meter/sec      RA   =          265
01509  deg
 ZDOT =      -3338
213479                 TA   =          145
47170
                                          MA   =          145
37478
                                          Ha   =            228
522  n
mi
                                          Hp   =            217
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10452900
94                 X    =        -3210187
08
 Y    =       13420153
24  feet           Y    =         4054699
69  meter
 Z    =      -14428082
80                 Z    =        -4413214
06
 XDOT =     -10564
896636                 XDOT =       -3135
666924
 YDOT =     -19968
360226  feet/sec       YDOT =       -6121
893548  meter/sec
 ZDOT =     -10952
143961                 ZDOT =       -3353
651106

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9243349
31                 X    =         2817372
87
 Y    =       14208264
44  feet           Y    =         4330679
00  meter
 Z    =      -14498928
91                 Z    =        -4419273
53
 XDOT =     -21277
975897                 XDOT =       -6485
527054
 YDOT =       2628
931187  feet/sec       YDOT =         801
298226  meter/sec
 ZDOT =     -11021
574011                 ZDOT =       -3359
375758


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   19187
43197118  
00016717  00000-0  10270-3 0  9063
2 25544  51
6422 265
7950 0007244 117
2702 242
9188 15
50946063 18230


Satellite: ISS
Catalog Number: 25544
Epoch time:      19187
43197118   =   yrday
fracday
Element set:     906
Inclination:       51
6422  deg
RA of node:       265
7950  deg
Eccentricity:     
0007244     
Arg of perigee:   117
2702  deg
Mean anomaly:     242
9188  deg
Mean motion:   15
50946063  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1823
Checksum:              317


Coasting Arc #8 (Orbit 1827)
---------------------------------------

Vector Time (GMT): 2019/187/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4200750
66                 A    =         6786587
87  meter
 Y    =        -624274
74  meter          E    =           
0009558
 Z    =        5285799
48                 I    =           51
23639
 XDOT =        966
748149                 Wp   =          109
94412
 YDOT =       7608
395647  meter/sec      RA   =          263
51980  deg
 ZDOT =        126
890213                 TA   =          338
82047
                                          MA   =          338
86002
                                          Ha   =            228
389  n
mi
                                          Hp   =            217
176

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13781990
35                 X    =         4181744
29
 Y    =       -2048145
47  feet           Y    =         -577405
90  meter
 Z    =       17341861
80                 Z    =         5306158
52
 XDOT =       3171
745895                 XDOT =         880
980689
 YDOT =      24961
927976  feet/sec       YDOT =        7618
726932  meter/sec
 ZDOT =        416
306474                 ZDOT =         131
378815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13741489
30                 X    =        -4188405
94
 Y    =        1447924
36  feet           Y    =          441327
34  meter
 Z    =       17434256
95                 Z    =         5313961
52
 XDOT =      -1969
556604                 XDOT =        -600
320853
 YDOT =     -24074
535029  feet/sec       YDOT =       -7337
918277  meter/sec
 ZDOT =        435
940897                 ZDOT =         132
874785


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   19187
75413806  
00016717  00000-0  10270-3 0  9074
2 25544  51
6395 264
1995 0007213 114
6038 245
5865 15
50960168 18288


Satellite: ISS
Catalog Number: 25544
Epoch time:      19187
75413806   =   yrday
fracday
Element set:     907
Inclination:       51
6395  deg
RA of node:       264
1995  deg
Eccentricity:     
0007213     
Arg of perigee:   114
6038  deg
Mean anomaly:     245
5865  deg
Mean motion:   15
50960168  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              336


Coasting Arc #9 (Orbit 1842)
---------------------------------------

Vector Time (GMT): 2019/188/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4291633
79                 A    =         6786791
75  meter
 Y    =         143196
17  meter          E    =           
0021521
 Z    =       -5274391
73                 I    =           51
24206
 XDOT =      -1021
864211                 Wp   =          102
25000
 YDOT =      -7552
969938  meter/sec      RA   =          258
52589  deg
 ZDOT =        624
098273                 TA   =          173
77075
                                          MA   =          173
74394
                                          Ha   =            228
558  n
mi
                                          Hp   =            217
058

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14080163
34                 X    =        -4267296
44
 Y    =         469803
71  feet           Y    =           95340
70  meter
 Z    =      -17304434
80                 Z    =        -5295179
42
 XDOT =      -3352
572870                 XDOT =        -940
360264
 YDOT =     -24780
085100  feet/sec       YDOT =       -7563
941485  meter/sec
 ZDOT =       2047
566514                 ZDOT =         619
331741

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13971028
24                 X    =         4258369
41
 Y    =         -98392
12  feet           Y    =          -29989
92  meter
 Z    =      -17398731
79                 Z    =        -5303133
45
 XDOT =       2701
150747                 XDOT =         823
310748
 YDOT =      23841
678817  feet/sec       YDOT =        7266
943703  meter/sec
 ZDOT =       2026
642169                 ZDOT =         617
720533


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   19188
72064098  
00016717  00000-0  10270-3 0  9088
2 25544  51
6399 259
4046 0007245 117
2278 242
9611 15
50939671 18438


Satellite: ISS
Catalog Number: 25544
Epoch time:      19188
72064098   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:       259
4046  deg
Eccentricity:     
0007245     
Arg of perigee:   117
2278  deg
Mean anomaly:     242
9611  deg
Mean motion:   15
50939671  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1843
Checksum:              340


Coasting Arc #10 (Orbit 1858)
---------------------------------------

Vector Time (GMT): 2019/189/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4401455
14                 A    =         6787189
31  meter
 Y    =         313822
48  meter          E    =           
0009776
 Z    =        5148319
33                 I    =           51
25008
 XDOT =       1065
936067                 Wp   =           96
72806
 YDOT =       7472
699928  meter/sec      RA   =          253
53250  deg
 ZDOT =      -1365
696712                 TA   =            6
47438
                                          MA   =            6
46176
                                          Ha   =            228
293  n
mi
                                          Hp   =            217
307

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14440469
61                 X    =         4372611
38
 Y    =        1029601
32  feet           Y    =          362880
92  meter
 Z    =       16890811
44                 Z    =         5169629
67
 XDOT =       3497
165573                 XDOT =         988
928689
 YDOT =      24516
732046  feet/sec       YDOT =        7484
189517  meter/sec
 ZDOT =      -4480
632256                 ZDOT =       -1360
705236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14316378
67                 X    =        -4363632
22
 Y    =       -1163990
54  feet           Y    =         -354784
32  meter
 Z    =       16987441
85                 Z    =         5177772
28
 XDOT =      -3383
829181                 XDOT =       -1031
391134
 YDOT =     -23504
223972  feet/sec       YDOT =       -7164
087467  meter/sec
 ZDOT =      -4458
659314                 ZDOT =       -1358
999359


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   19189
75157562  
00016717  00000-0  10270-3 0  9092
2 25544  51
6386 254
2896 0007108 120
7527 239
4335 15
50961510 18592


Satellite: ISS
Catalog Number: 25544
Epoch time:      19189
75157562   =   yrday
fracday
Element set:     909
Inclination:       51
6386  deg
RA of node:       254
2896  deg
Eccentricity:     
0007108     
Arg of perigee:   120
7527  deg
Mean anomaly:     239
4335  deg
Mean motion:   15
50961510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1859
Checksum:              338


Coasting Arc #11 (Orbit 1873)
---------------------------------------

Vector Time (GMT): 2019/190/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4579609
97                 A    =         6788090
13  meter
 Y    =        -746287
64  meter          E    =           
0019489
 Z    =       -4972734
82                 I    =           51
26341
 XDOT =      -1070
889300                 Wp   =          112
15529
 YDOT =      -7281
865594  meter/sec      RA   =          248
54092  deg
 ZDOT =       2078
433260                 TA   =          178
23749
                                          MA   =          178
23061
                                          Ha   =            228
455  n
mi
                                          Hp   =            217
226

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15024967
08                 X    =        -4546769
80
 Y    =       -2448450
25  feet           Y    =         -797315
98  meter
 Z    =      -16314746
78                 Z    =        -4994900
98
 XDOT =      -3513
416338                 XDOT =        -999
477596
 YDOT =     -23890
635150  feet/sec       YDOT =       -7293
441929  meter/sec
 ZDOT =       6819
006759                 ZDOT =        2073
404108

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14933824
26                 X    =         4551829
64
 Y    =        2331676
69  feet           Y    =          710695
06  meter
 Z    =      -16415227
18                 Z    =        -5003361
25
 XDOT =       3917
776650                 XDOT =        1194
138323
 YDOT =      22772
334854  feet/sec       YDOT =        6941
007664  meter/sec
 ZDOT =       6796
828416                 ZDOT =        2071
673301


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   19190
71807693  
00016717  00000-0  10270-3 0  9109
2 25544  51
6386 249
4949 0007118 123
9058 236
2771 15
50938562 18749


Satellite: ISS
Catalog Number: 25544
Epoch time:      19190
71807693   =   yrday
fracday
Element set:     910
Inclination:       51
6386  deg
RA of node:       249
4949  deg
Eccentricity:     
0007118     
Arg of perigee:   123
9058  deg
Mean anomaly:     236
2771  deg
Mean motion:   15
50938562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1874
Checksum:              342


Coasting Arc #12 (Orbit 1889)
---------------------------------------

Vector Time (GMT): 2019/191/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4765720
77                 A    =         6789096
86  meter
 Y    =        1143900
52  meter          E    =           
0012549
 Z    =        4686751
53                 I    =           51
28071
 XDOT =       1035
781314                 Wp   =           93
59085
 YDOT =       7076
357382  meter/sec      RA   =          243
55070  deg
 ZDOT =      -2774
696385                 TA   =           24
05769
                                          MA   =           23
99912
                                          Ha   =            228
179  n
mi
                                          Hp   =            217
456

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15635566
82                 X    =         4729809
62
 Y    =        3752954
46  feet           Y    =         1196992
88  meter
 Z    =       15376481
38                 Z    =         4709814
40
 XDOT =       3398
232656                 XDOT =         970
052343
 YDOT =      23216
395611  feet/sec       YDOT =        7087
572988  meter/sec
 ZDOT =      -9103
334596                 ZDOT =       -2769
823883

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15621157
30                 X    =        -4761328
75
 Y    =       -3362999
32  feet           Y    =        -1025042
19  meter
 Z    =       15481003
74                 Z    =         4718609
94
 XDOT =      -4286
158160                 XDOT =       -1306
421007
 YDOT =     -21982
542157  feet/sec       YDOT =       -6700
278849  meter/sec
 ZDOT =      -9081
834308                 ZDOT =       -2768
143097


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   19191
74900951  
00016717  00000-0  10270-3 0  9115
2 25544  51
6390 244
3799 0007020 127
9084 232
2703 15
50968816 18900


Satellite: ISS
Catalog Number: 25544
Epoch time:      19191
74900951   =   yrday
fracday
Element set:     911
Inclination:       51
6390  deg
RA of node:       244
3799  deg
Eccentricity:     
0007020     
Arg of perigee:   127
9084  deg
Mean anomaly:     232
2703  deg
Mean motion:   15
50968816  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1890
Checksum:              319


Coasting Arc #13 (Orbit 1904)
---------------------------------------

Vector Time (GMT): 2019/192/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5003398
40                 A    =         6790471
08  meter
 Y    =       -1489554
93  meter          E    =           
0015648
 Z    =       -4359073
61                 I    =           51
30146
 XDOT =       -947
418153                 Wp   =          119
45744
 YDOT =      -6783
173441  meter/sec      RA   =          238
56325  deg
 ZDOT =       3407
099540                 TA   =          185
33249
                                          MA   =          185
34917
                                          Ha   =            228
326  n
mi
                                          Hp   =            217
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16415349
10                 X    =        -4965196
04
 Y    =       -4886991
26  feet           Y    =        -1545292
31  meter
 Z    =      -14301422
61                 Z    =        -4383285
55
 XDOT =      -3108
327272                 XDOT =        -888
046081
 YDOT =     -22254
506040  feet/sec       YDOT =       -6793
436579  meter/sec
 ZDOT =      11178
148096                 ZDOT =        3402
640734

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16510933
71                 X    =         5032532
60
 Y    =        4193467
79  feet           Y    =         1278168
98  meter
 Z    =      -14411139
92                 Z    =        -4392515
45
 XDOT =       4427
458800                 XDOT =        1349
489442
 YDOT =      20895
229248  feet/sec       YDOT =        6368
865875  meter/sec
 ZDOT =      11158
486883                 ZDOT =        3401
106802


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   19192
71550725  
00016717  00000-0  10270-3 0  9124
2 25544  51
6395 239
5850 0007001 130
2895 229
8869 15
50947218 19050


Satellite: ISS
Catalog Number: 25544
Epoch time:      19192
71550725   =   yrday
fracday
Element set:     912
Inclination:       51
6395  deg
RA of node:       239
5850  deg
Eccentricity:     
0007001     
Arg of perigee:   130
2895  deg
Mean anomaly:     229
8869  deg
Mean motion:   15
50947218  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1905
Checksum:              328


Coasting Arc #14 (Orbit 1920)
---------------------------------------

Vector Time (GMT): 2019/193/16:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5230650
65                 A    =         6791866
78  meter
 Y    =        1793809
17  meter          E    =           
0016015
 Z    =        3927633
01                 I    =           51
32398
 XDOT =        796
153139                 Wp   =          100
42714
 YDOT =       6489
290165  meter/sec      RA   =          233
57847  deg
 ZDOT =      -4012
908185                 TA   =           31
69260
                                          MA   =           31
59629
                                          Ha   =            228
065  n
mi
                                          Hp   =            217
617

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17160927
34                 X    =         5191124
85
 Y    =        5885200
69  feet           Y    =         1852080
42  meter
 Z    =       12885935
06                 Z    =         3952945
68
 XDOT =       2612
050982                 XDOT =         743
021248
 YDOT =      21290
322064  feet/sec       YDOT =        6497
896789  meter/sec
 ZDOT =     -13165
709270                 ZDOT =       -4009
168931

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17393718
85                 X    =        -5301605
51
 Y    =       -4860283
37  feet           Y    =        -1481414
37  meter
 Z    =       13000635
63                 Z    =         3962593
74
 XDOT =      -4316
220092                 XDOT =       -1315
583884
 YDOT =     -19822
793410  feet/sec       YDOT =       -6041
987431  meter/sec
 ZDOT =     -13149
276412                 ZDOT =       -4007
899450


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   19193
74643726  
00016717  00000-0  10270-3 0  9133
2 25544  51
6388 234
4704 0006895 134
1181 226
0538 15
50974326 19215


Satellite: ISS
Catalog Number: 25544
Epoch time:      19193
74643726   =   yrday
fracday
Element set:     913
Inclination:       51
6388  deg
RA of node:       234
4704  deg
Eccentricity:     
0006895     
Arg of perigee:   134
1181  deg
Mean anomaly:     226
0538  deg
Mean motion:   15
50974326  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1921
Checksum:              322


Coasting Arc #15 (Orbit 1929)
---------------------------------------

Vector Time (GMT): 2019/194/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5147178
97                 A    =         6797313
86  meter
 Y    =       -4101590
21  meter          E    =           
0009341
 Z    =       -1705948
58                 I    =           51
35770
 XDOT =       1935
097080                 Wp   =           86
95670
 YDOT =      -4772
950716  meter/sec      RA   =          230
51020  deg
 ZDOT =       5664
425190                 TA   =          254
30512
                                          MA   =          254
40819
                                          Ha   =            228
237  n
mi
                                          Hp   =            217
702

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16887070
11                 X    =        -5092644
77
 Y    =      -13456660
78  feet           Y    =        -4158844
40  meter
 Z    =       -5596944
16                 Z    =        -1730819
65
 XDOT =       6348
743702                 XDOT =        1960
811309
 YDOT =     -15659
287126  feet/sec       YDOT =       -4751
168171  meter/sec
 ZDOT =      18584
072146                 ZDOT =        5673
886852

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21371332
04                 X    =        -6513982
00
 Y    =        2872077
44  feet           Y    =          875409
20  meter
 Z    =       -5709463
94                 Z    =        -1740244
61
 XDOT =      -6802
405419                 XDOT =       -2073
373172
 YDOT =     -13762
867540  feet/sec       YDOT =       -4194
922026  meter/sec
 ZDOT =      18627
391958                 ZDOT =        5677
629069


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   19194
32633497  
00016717  00000-0  10270-3 0  9143
2 25544  51
6421 231
5914 0007106 139
1479 221
0206 15
50944564 19303


Satellite: ISS
Catalog Number: 25544
Epoch time:      19194
32633497   =   yrday
fracday
Element set:     914
Inclination:       51
6421  deg
RA of node:       231
5914  deg
Eccentricity:     
0007106     
Arg of perigee:   139
1479  deg
Mean anomaly:     221
0206  deg
Mean motion:   15
50944564  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1930
Checksum:              300


Coasting Arc #16 (Orbit 1945)
---------------------------------------

Vector Time (GMT): 2019/195/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5252909
43                 A    =         6798084
23  meter
 Y    =        4171220
92  meter          E    =           
0020579
 Z    =        1035361
95                 I    =           51
38188
 XDOT =      -2294
086327                 Wp   =          130
70314
 YDOT =       4363
238151  meter/sec      RA   =          225
53496  deg
 ZDOT =      -5875
725208                 TA   =           38
03782
                                          MA   =           37
89269
                                          Ha   =            228
181  n
mi
                                          Hp   =            217
764

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17233954
82                 X    =         5200846
07
 Y    =       13685107
99  feet           Y    =         4229671
36  meter
 Z    =        3396856
79                 Z    =         1060752
59
 XDOT =      -7526
529943                 XDOT =       -2314
166075
 YDOT =      14315
085796  feet/sec       YDOT =        4337
472732  meter/sec
 ZDOT =     -19277
313676                 ZDOT =       -5886
916989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21731906
64                 X    =         6623885
14
 Y    =       -3349904
11  feet           Y    =        -1021050
77  meter
 Z    =        3511750
56                 Z    =         1070381
57
 XDOT =       5246
661361                 XDOT =        1599
182383
 YDOT =      13562
750303  feet/sec       YDOT =        4133
926292  meter/sec
 ZDOT =     -19328
450723                 ZDOT =       -5891
311780


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   19195
35726350  
00016717  00000-0  10270-3 0  9159
2 25544  51
6416 226
4768 0007284 143
6598 216
5049 15
50958017 19465


Satellite: ISS
Catalog Number: 25544
Epoch time:      19195
35726350   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       226
4768  deg
Eccentricity:     
0007284     
Arg of perigee:   143
6598  deg
Mean anomaly:     216
5049  deg
Mean motion:   15
50958017  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1946
Checksum:              338


Coasting Arc #17 (Orbit 1960)
---------------------------------------

Vector Time (GMT): 2019/196/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5355969
48                 A    =         6798472
86  meter
 Y    =       -4166536
83  meter          E    =           
0011718
 Z    =        -397772
32                 I    =           51
40771
 XDOT =       2669
036696                 Wp   =           78
04088
 YDOT =      -3986
361752  meter/sec      RA   =          220
56158  deg
 ZDOT =       5969
469091                 TA   =          277
66540
                                          MA   =          277
79846
                                          Ha   =            228
083  n
mi
                                          Hp   =            217
926

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17572078
35                 X    =        -5307047
88
 Y    =      -13669740
27  feet           Y    =        -4226157
44  meter
 Z    =       -1305027
29                 Z    =         -423671
12
 XDOT =       8756
682073                 XDOT =        2684
418998
 YDOT =     -13078
614671  feet/sec       YDOT =       -3956
429669  meter/sec
 ZDOT =      19584
872346                 ZDOT =        5982
470815

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21894062
11                 X    =        -6673310
13
 Y    =        3996257
87  feet           Y    =         1218059
40  meter
 Z    =       -1422251
79                 Z    =         -433502
35
 XDOT =      -3719
027345                 XDOT =       -1133
559535
 YDOT =     -13546
737191  feet/sec       YDOT =       -4129
045496  meter/sec
 ZDOT =      19644
194948                 ZDOT =        5987
550620


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   19196
32375565  
00016717  00000-0  10270-3 0  9166
2 25544  51
6420 221
6820 0007015 145
6028 214
5578 15
50958567 19610


Satellite: ISS
Catalog Number: 25544
Epoch time:      19196
32375565   =   yrday
fracday
Element set:     916
Inclination:       51
6420  deg
RA of node:       221
6820  deg
Eccentricity:     
0007015     
Arg of perigee:   145
6028  deg
Mean anomaly:     214
5578  deg
Mean motion:   15
50958567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1961
Checksum:              320


Coasting Arc #18 (Orbit 1976)
---------------------------------------

Vector Time (GMT): 2019/197/07:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916291
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5373619
30                 A    =         6798512
09  meter
 Y    =        4138322
44  meter          E    =           
0018584
 Z    =        -298284
55                 I    =           51
43246
 XDOT =      -3120
723740                 Wp   =          142
01516
 YDOT =       3636
169363  meter/sec      RA   =          215
59091  deg
 ZDOT =      -5986
174480                 TA   =           41
20620
                                          MA   =           41
06606
                                          Ha   =            228
056  n
mi
                                          Hp   =            217
989

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17629984
57                 X    =         5328392
89
 Y    =       13577173
36  feet           Y    =         4198161
19  meter
 Z    =        -978623
86                 Z    =         -272291
17
 XDOT =     -10238
594946                 XDOT =       -3132
075485
 YDOT =      11929
689510  feet/sec       YDOT =        3601
208699  meter/sec
 ZDOT =     -19639
680051                 ZDOT =       -6001
360534

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21799714
70                 X    =         6644553
04
 Y    =       -4488308
65  feet           Y    =        -1368036
48  meter
 Z    =        -860942
45                 Z    =         -262415
26
 XDOT =       2105
421394                 XDOT =         641
732441
 YDOT =      13853
939696  feet/sec       YDOT =        4222
680819  meter/sec
 ZDOT =     -19708
893233                 ZDOT =       -6007
270658


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   19197
35468118  
00016717  00000-0  10270-3 0  9178
2 25544  51
6406 216
5677 0007148 149
8314 210
3250 15
50966140 19772


Satellite: ISS
Catalog Number: 25544
Epoch time:      19197
35468118   =   yrday
fracday
Element set:     917
Inclination:       51
6406  deg
RA of node:       216
5677  deg
Eccentricity:     
0007148     
Arg of perigee:   149
8314  deg
Mean anomaly:     210
3250  deg
Mean motion:   15
50966140  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1977
Checksum:              324
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list