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

 
Date: October 1st 2019

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16520 4497 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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


271/11:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 3

272/00:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 0
000/00:00:00 000 0 0 0 0 218 4

275/04:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 218 3

276/07:36:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 4

278/06:48:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 9
000/00:00:00 000 0 0 0 0 218 6

281/10:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 218 7

284/20:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 219 2

Coasting Arc #1 (Orbit 3113)
---------------------------------------

Vector Time (GMT): 2019/270/15:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 931323
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5806103
93                 A    =         6795642
55  meter
 Y    =        -319713
29  meter          E    =           
0012545
 Z    =       -3528161
86                 I    =           51
43664
 XDOT =      -2399
628238                 Wp   =           92
29008
 YDOT =      -5720
075897  meter/sec      RA   =          212
08067  deg
 ZDOT =       4480
633520                 TA   =          226
14980
                                          MA   =          226
25354
                                          Ha   =            229
968  n
mi
                                          Hp   =            218
178

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19048897
42                 X    =        -5784959
43
 Y    =       -1048928
10  feet           Y    =         -384523
40  meter
 Z    =      -11575334
20                 Z    =        -3556314
35
 XDOT =      -7872
796055                 XDOT =       -2357
250784
 YDOT =     -18766
653205  feet/sec       YDOT =       -5746
672789  meter/sec
 ZDOT =      14700
241206                 ZDOT =        4469
080585

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12944194
72                 X    =         3945390
55
 Y    =      -13907784
30  feet           Y    =        -4239092
65  meter
 Z    =      -11703438
13                 Z    =        -3567207
94
 XDOT =      18508
322358                 XDOT =        5641
336655
 YDOT =       4936
181066  feet/sec       YDOT =        1504
547989  meter/sec
 ZDOT =      14647
938102                 ZDOT =        4464
691533


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   19270
63253005  
00016717  00000-0  10270-3 0  9000
2 25544  51
6434 213
2203 0007338  88
9269 271
2723 15
50120314 31146


Satellite: ISS
Catalog Number: 25544
Epoch time:      19270
63253005   =   yrday
fracday
Element set:     900
Inclination:       51
6434  deg
RA of node:       213
2203  deg
Eccentricity:     
0007338     
Arg of perigee:    88
9269  deg
Mean anomaly:     271
2723  deg
Mean motion:   15
50120314  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3114
Checksum:              270


Coasting Arc #2 (Orbit 3126)
---------------------------------------

Vector Time (GMT): 2019/271/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964595
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6260139
29                 A    =         6800634
29  meter
 Y    =       -2481645
67  meter          E    =           
0015438
 Z    =        -925209
95                 I    =           51
47430
 XDOT =       1031
345139                 Wp   =           61
81551
 YDOT =      -4771
437959  meter/sec      RA   =          207
90437  deg
 ZDOT =       5902
429757                 TA   =          288
16490
                                          MA   =          288
33292
                                          Ha   =            230
001  n
mi
                                          Hp   =            218
270

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20538514
72                 X    =        -6227429
36
 Y    =       -8141882
12  feet           Y    =        -2551468
18  meter
 Z    =       -3035465
72                 Z    =         -955539
76
 XDOT =       3383
678277                 XDOT =        1055
953222
 YDOT =     -15654
324011  feet/sec       YDOT =       -4759
766427  meter/sec
 ZDOT =      19364
927023                 ZDOT =        5907
500011

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19695848
61                 X    =         6003294
66
 Y    =        9966846
89  feet           Y    =         3037894
93  meter
 Z    =       -3173388
43                 Z    =         -967248
79
 XDOT =      -3930
557529                 XDOT =       -1198
033935
 YDOT =      13857
983004  feet/sec       YDOT =        4223
913219  meter/sec
 ZDOT =      19388
224166                 ZDOT =        5909
530726


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   19271
47062617  
00016717  00000-0  10270-3 0  9011
2 25544  51
6403 209
0670 0007394  91
9381 268
2617 15
50110367 31273


Satellite: ISS
Catalog Number: 25544
Epoch time:      19271
47062617   =   yrday
fracday
Element set:     901
Inclination:       51
6403  deg
RA of node:       209
0670  deg
Eccentricity:     
0007394     
Arg of perigee:    91
9381  deg
Mean anomaly:     268
2617  deg
Mean motion:   15
50110367  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3127
Checksum:              298


Coasting Arc #3 (Orbit 3135)
---------------------------------------

Vector Time (GMT): 2019/272/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964595
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         271392
47                 A    =         6790399
25  meter
 Y    =        4562000
14  meter          E    =           
0019705
 Z    =       -5039981
88                 I    =           51
45928
 XDOT =      -7206
062800                 Wp   =           84
01934
 YDOT =      -1689
555855  meter/sec      RA   =          205
13274  deg
 ZDOT =      -1921
846293                 TA   =          167
26303
                                          MA   =          167
21318
                                          Ha   =            229
987  n
mi
                                          Hp   =            218
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         890395
24                 X    =          244840
33
 Y    =       14967192
05  feet           Y    =         4564885
97  meter
 Z    =      -16535373
61                 Z    =        -5038728
58
 XDOT =     -23641
938319                 XDOT =       -7177
298787
 YDOT =      -5543
162255  feet/sec       YDOT =       -1769
978538  meter/sec
 ZDOT =      -6305
269989                 ZDOT =       -1956
780858

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5543140
38                 X    =         1689549
19
 Y    =       13937896
17  feet           Y    =         4248270
75  meter
 Z    =      -16529878
01                 Z    =        -5038306
82
 XDOT =     -23145
488988                 XDOT =       -7054
745043
 YDOT =       1556
194999  feet/sec       YDOT =         474
328236  meter/sec
 ZDOT =      -6464
195438                 ZDOT =       -1970
286770


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   19272
05084559  
00016717  00000-0  10270-3 0  9026
2 25544  51
6430 206
1896 0007247  98
2953 261
9019 15
50099999 31366


Satellite: ISS
Catalog Number: 25544
Epoch time:      19272
05084559   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:       206
1896  deg
Eccentricity:     
0007247     
Arg of perigee:    98
2953  deg
Mean anomaly:     261
9019  deg
Mean motion:   15
50099999  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3136
Checksum:              336


Coasting Arc #4 (Orbit 3151)
---------------------------------------

Vector Time (GMT): 2019/273/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964595
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -211048
86                 A    =         6789778
25  meter
 Y    =       -4429110
95  meter          E    =           
0011884
 Z    =        5133348
34                 I    =           51
48890
 XDOT =       7381
355570                 Wp   =          111
61725
 YDOT =       1420
488157  meter/sec      RA   =          200
16484  deg
 ZDOT =       1521
953478                 TA   =          323
65118
                                          MA   =          323
73184
                                          Ha   =            229
914  n
mi
                                          Hp   =            218
314

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -692417
53                 X    =         -186440
87
 Y    =      -14531203
89  feet           Y    =        -4431332
89  meter
 Z    =       16841694
03                 Z    =         5132383
39
 XDOT =      24217
045833                 XDOT =        7357
529755
 YDOT =       4660
394216  feet/sec       YDOT =        1502
898633  meter/sec
 ZDOT =       4993
285689                 ZDOT =        1557
751791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5455837
83                 X    =        -1662939
37
 Y    =      -13491121
85  feet           Y    =        -4112093
94  meter
 Z    =       16837501
34                 Z    =         5132070
41
 XDOT =      23408
265918                 XDOT =        7134
839452
 YDOT =      -3002
019989  feet/sec       YDOT =        -915
015693  meter/sec
 ZDOT =       5156
170611                 ZDOT =        1571
600802


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   19273
08234390  
00016717  00000-0  10270-3 0  9031
2 25544  51
6434 201
0789 0007253 102
0835 258
1129 15
50147597 31521


Satellite: ISS
Catalog Number: 25544
Epoch time:      19273
08234390   =   yrday
fracday
Element set:     903
Inclination:       51
6434  deg
RA of node:       201
0789  deg
Eccentricity:     
0007253     
Arg of perigee:   102
0835  deg
Mean anomaly:     258
1129  deg
Mean motion:   15
50147597  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3152
Checksum:              296


Coasting Arc #5 (Orbit 3166)
---------------------------------------

Vector Time (GMT): 2019/274/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964595
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         101928
17                 A    =         6789517
43  meter
 Y    =        4341557
87  meter          E    =           
0020932
 Z    =       -5237197
01                 I    =           51
51931
 XDOT =      -7482
670267                 Wp   =           89
59123
 YDOT =      -1134
929003  meter/sec      RA   =          195
19896  deg
 ZDOT =      -1090
110237                 TA   =          169
93656
                                          MA   =          169
89458
                                          Ha   =            229
919  n
mi
                                          Hp   =            218
406

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         334410
00                 X    =           78811
86
 Y    =       14243956
27  feet           Y    =         4342567
98  meter
 Z    =      -17182404
87                 Z    =        -5236758
40
 XDOT =     -24549
443132                 XDOT =       -7464
127792
 YDOT =      -3723
520351  feet/sec       YDOT =       -1218
501921  meter/sec
 ZDOT =      -3576
477156                 ZDOT =       -1126
413716

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5255037
69                 X    =         1601735
49
 Y    =       13245701
38  feet           Y    =         4037289
78  meter
 Z    =      -17180603
35                 Z    =        -5236647
90
 XDOT =     -23367
903965                 XDOT =       -7122
537129
 YDOT =       4433
130742  feet/sec       YDOT =        1351
218250  meter/sec
 ZDOT =      -3741
692132                 ZDOT =       -1140
467762


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   19274
04937138  
00016717  00000-0  10270-3 0  9049
2 25544  51
6434 196
2880 0007168 104
8805 255
3140 15
50109919 31674


Satellite: ISS
Catalog Number: 25544
Epoch time:      19274
04937138   =   yrday
fracday
Element set:     904
Inclination:       51
6434  deg
RA of node:       196
2880  deg
Eccentricity:     
0007168     
Arg of perigee:   104
8805  deg
Mean anomaly:     255
3140  deg
Mean motion:   15
50109919  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3167
Checksum:              317


Coasting Arc #6 (Orbit 3182)
---------------------------------------

Vector Time (GMT): 2019/275/00:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964595
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          -1241
92                 A    =         6789094
98  meter
 Y    =       -4259321
53  meter          E    =           
0010277
 Z    =        5278829
64                 I    =           51
55087
 XDOT =       7594
732941                 Wp   =          111
17351
 YDOT =        832
001126  meter/sec      RA   =          190
23499  deg
 ZDOT =        668
416036                 TA   =          332
40984
                                          MA   =          332
46435
                                          Ha   =            229
854  n
mi
                                          Hp   =            218
361

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =          -4074
53                 X    =           20745
07
 Y    =      -13974151
99  feet           Y    =        -4259212
13  meter
 Z    =       17318994
89                 Z    =         5278877
29
 XDOT =      24917
102825                 XDOT =        7581
617954
 YDOT =       2729
662488  feet/sec       YDOT =         916
857501  meter/sec
 ZDOT =       2192
965999                 ZDOT =         705
277140

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5078319
72                 X    =        -1547871
85
 Y    =      -13018196
14  feet           Y    =        -3967946
18  meter
 Z    =       17319404
21                 Z    =         5278954
40
 XDOT =      23297
223618                 XDOT =        7100
993759
 YDOT =      -5926
905802  feet/sec       YDOT =       -1806
520889  meter/sec
 ZDOT =       2360
753893                 ZDOT =         719
557787


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   19275
08086182  
00016717  00000-0  10270-3 0  9059
2 25544  51
6433 191
1773 0007216 108
0739 252
1198 15
50159160 31833


Satellite: ISS
Catalog Number: 25544
Epoch time:      19275
08086182   =   yrday
fracday
Element set:     905
Inclination:       51
6433  deg
RA of node:       191
1773  deg
Eccentricity:     
0007216     
Arg of perigee:   108
0739  deg
Mean anomaly:     252
1198  deg
Mean motion:   15
50159160  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3183
Checksum:              306


Coasting Arc #7 (Orbit 3184)
---------------------------------------

Vector Time (GMT): 2019/275/04:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964595
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3940568
95                 A    =         6791832
58  meter
 Y    =       -3044982
92  meter          E    =           
0014669
 Z    =        4606347
87                 I    =           51
56282
 XDOT =       6167
154417                 Wp   =           84
66648
 YDOT =       3442
777466  meter/sec      RA   =          189
53746  deg
 ZDOT =      -2990
420673                 TA   =           35
23336
                                          MA   =           35
13647
                                          Ha   =            229
817  n
mi
                                          Hp   =            218
298

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12928375
81                 X    =         3951950
48
 Y    =       -9990101
45  feet           Y    =        -3000852
78  meter
 Z    =       15112689
85                 Z    =         4625517
84
 XDOT =      20233
446250                 XDOT =        6142
723983
 YDOT =      11295
201659  feet/sec       YDOT =        3511
606152  meter/sec
 ZDOT =      -9811
091447                 ZDOT =       -2960
521978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4918469
32                 X    =        -1499149
45
 Y    =      -15495282
73  feet           Y    =        -4722962
18  meter
 Z    =       15200108
40                 Z    =         4632993
04
 XDOT =      16506
082435                 XDOT =        5031
053926
 YDOT =     -14760
680091  feet/sec       YDOT =       -4499
055292  meter/sec
 ZDOT =      -9675
118296                 ZDOT =       -2948
976057


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   19275
20979874  
00016717  00000-0  10270-3 0  9063
2 25544  51
6416 190
5403 0007353 106
0388 254
1573 15
50151197 31850


Satellite: ISS
Catalog Number: 25544
Epoch time:      19275
20979874   =   yrday
fracday
Element set:     906
Inclination:       51
6416  deg
RA of node:       190
5403  deg
Eccentricity:     
0007353     
Arg of perigee:   106
0388  deg
Mean anomaly:     254
1573  deg
Mean motion:   15
50151197  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3185
Checksum:              317


Coasting Arc #8 (Orbit 3199)
---------------------------------------

Vector Time (GMT): 2019/276/04:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 964595
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4064610
12                 A    =         6792652
75  meter
 Y    =        3192667
79  meter          E    =           
0016600
 Z    =       -4424364
60                 I    =           51
59872
 XDOT =      -6112
704572                 Wp   =          110
41111
 YDOT =      -3150
596718  meter/sec      RA   =          184
57748  deg
 ZDOT =       3346
732589                 TA   =          193
51085
                                          MA   =          193
55535
                                          Ha   =            229
950  n
mi
                                          Hp   =            218
252

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13335335
05                 X    =        -4078517
92
 Y    =       10474631
87  feet           Y    =         3147136
50  meter
 Z    =      -14515631
88                 Z    =        -4444143
18
 XDOT =     -20054
805026                 XDOT =       -6093
276203
 YDOT =     -10336
603406  feet/sec       YDOT =       -3218
844517  meter/sec
 ZDOT =      10980
093795                 ZDOT =        3317
086217

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5505627
42                 X    =         1678115
24
 Y    =       15956506
00  feet           Y    =         4863543
03  meter
 Z    =      -14605842
17                 Z    =        -4451860
69
 XDOT =     -15248
581247                 XDOT =       -4647
767564
 YDOT =      15174
955641  feet/sec       YDOT =        4625
326479  meter/sec
 ZDOT =      10845
237984                 ZDOT =        3305
628538


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   19276
17682028  
00016717  00000-0  10270-3 0  9073
2 25544  51
6418 185
7488 0007401 109
2097 250
9855 15
50126957 32008


Satellite: ISS
Catalog Number: 25544
Epoch time:      19276
17682028   =   yrday
fracday
Element set:     907
Inclination:       51
6418  deg
RA of node:       185
7488  deg
Eccentricity:     
0007401     
Arg of perigee:   109
2097  deg
Mean anomaly:     250
9855  deg
Mean motion:   15
50126957  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3200
Checksum:              325


Coasting Arc #9 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2019/276/07:36:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2772620
60                 A    =         6791425
11  meter
 Y    =       -3966363
21  meter          E    =           
0014900
 Z    =        4755745
38                 I    =           51
59652
 XDOT =       6990
617929                 Wp   =          114
27466
 YDOT =      -1656
592838  meter/sec      RA   =          183
87678  deg
 ZDOT =       2681
309825                 TA   =          309
15943
                                          MA   =          309
29173
                                          Ha   =            229
918  n
mi
                                          Hp   =            218
412

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9096524
27                 X    =        -2751162
64
 Y    =      -13013002
67  feet           Y    =        -3997248
44  meter
 Z    =       15602839
18                 Z    =         4742329
11
 XDOT =      22935
098193                 XDOT =        6995
598355
 YDOT =      -5435
015874  feet/sec       YDOT =       -1578
390860  meter/sec
 ZDOT =       8796
948246                 ZDOT =        2715
280315

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5392291
43                 X    =        -1643570
43
 Y    =       14996843
72  feet           Y    =         4571037
97  meter
 Z    =       15541925
70                 Z    =         4737178
95
 XDOT =     -16467
121269                 XDOT =       -5019
178563
 YDOT =     -15241
131752  feet/sec       YDOT =       -4645
496958  meter/sec
 ZDOT =       8951
717073                 ZDOT =        2728
483364


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   19276
37022357  
00016717  00000-0  10270-3 0  9089
2 25544  51
6388 184
7910 0007192 110
1058 250
0867 15
50151263 32033


Satellite: ISS
Catalog Number: 25544
Epoch time:      19276
37022357   =   yrday
fracday
Element set:     908
Inclination:       51
6388  deg
RA of node:       184
7910  deg
Eccentricity:     
0007192     
Arg of perigee:   110
1058  deg
Mean anomaly:     250
0867  deg
Mean motion:   15
50151263  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              296


Coasting Arc #10 (Orbit 3217)
---------------------------------------

Vector Time (GMT): 2019/277/07:36:30
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2641226
36                 A    =         6790806
67  meter
 Y    =        3861047
77  meter          E    =           
0018257
 Z    =       -4938515
69                 I    =           51
62819
 XDOT =      -7045
429544                 Wp   =           88
48576
 YDOT =       1928
522030  meter/sec      RA   =          178
91733  deg
 ZDOT =      -2267
084974                 TA   =          159
33631
                                          MA   =          159
26239
                                          Ha   =            229
894  n
mi
                                          Hp   =            218
513

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8665440
80                 X    =         2621843
57
 Y    =       12667479
55  feet           Y    =         3890475
29  meter
 Z    =      -16202479
31                 Z    =        -4925732
65
 XDOT =     -23114
926327                 XDOT =       -7055
458827
 YDOT =       6327
172014  feet/sec       YDOT =        1849
678918  meter/sec
 ZDOT =      -7437
942829                 ZDOT =       -2301
333875

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5104415
00                 X    =         1555825
69
 Y    =      -14538822
09  feet           Y    =        -4431432
97  meter
 Z    =      -16144436
75                 Z    =        -4920824
32
 XDOT =      17600
141273                 XDOT =        5364
523060
 YDOT =      14587
023263  feet/sec       YDOT =        4446
124691  meter/sec
 ZDOT =      -7594
016679                 ZDOT =       -2314
656284


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   19277
33724118  
00016717  00000-0  10270-3 0  9091
2 25544  51
6394 179
9984 0007278 113
0760 247
1158 15
50126727 32187


Satellite: ISS
Catalog Number: 25544
Epoch time:      19277
33724118   =   yrday
fracday
Element set:     909
Inclination:       51
6394  deg
RA of node:       179
9984  deg
Eccentricity:     
0007278     
Arg of perigee:   113
0760  deg
Mean anomaly:     247
1158  deg
Mean motion:   15
50126727  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3218
Checksum:              332


Coasting Arc #11 (Orbit 3232)
---------------------------------------

Vector Time (GMT): 2019/278/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3358008
61                 A    =         6791397
96  meter
 Y    =        3465714
42  meter          E    =           
0017092
 Z    =       -4793572
48                 I    =           51
66254
 XDOT =      -6620
985531                 Wp   =           89
22407
 YDOT =       2777
512778  meter/sec      RA   =          174
13277  deg
 ZDOT =      -2637
964772                 TA   =          154
73481
                                          MA   =          154
65112
                                          Ha   =            229
879  n
mi
                                          Hp   =            218
557

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11017088
60                 X    =         3342289
14
 Y    =       11370454
13  feet           Y    =         3503178
00  meter
 Z    =      -15726943
82                 Z    =        -4777298
67
 XDOT =     -21722
393475                 XDOT =       -6638
738512
 YDOT =       9112
574731  feet/sec       YDOT =        2703
372905  meter/sec
 ZDOT =      -8654
740064                 ZDOT =       -2670
170534

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5663192
27                 X    =         1726141
00
 Y    =      -14863138
63  feet           Y    =        -4530284
66  meter
 Z    =      -15652973
95                 Z    =        -4771026
46
 XDOT =      16266
460624                 XDOT =        4958
017198
 YDOT =      15439
649876  feet/sec       YDOT =        4706
005282  meter/sec
 ZDOT =      -8801
570432                 ZDOT =       -2682
718668


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   19278
30425381  
00016717  00000-0  10270-3 0  9101
2 25544  51
6395 175
2067 0007300 116
0044 244
1859 15
50131901 32335


Satellite: ISS
Catalog Number: 25544
Epoch time:      19278
30425381   =   yrday
fracday
Element set:     910
Inclination:       51
6395  deg
RA of node:       175
2067  deg
Eccentricity:     
0007300     
Arg of perigee:   116
0044  deg
Mean anomaly:     244
1859  deg
Mean motion:   15
50131901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3233
Checksum:              280


Coasting Arc #12 (Orbit 3248)
---------------------------------------

Vector Time (GMT): 2019/279/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3232964
63                 A    =         6790660
78  meter
 Y    =       -3351116
33  meter          E    =           
0013762
 Z    =        4935068
35                 I    =           51
69315
 XDOT =       6650
136546                 Wp   =          121
14531
 YDOT =      -3082
135888  meter/sec      RA   =          169
18010  deg
 ZDOT =       2252
001893                 TA   =          306
81203
                                          MA   =          306
93821
                                          Ha   =            229
814  n
mi
                                          Hp   =            218
556

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10606839
33                 X    =        -3219223
16
 Y    =      -10994476
16  feet           Y    =        -3387192
62  meter
 Z    =       16191169
12                 Z    =         4919397
21
 XDOT =      21818
033287                 XDOT =        6673
168588
 YDOT =     -10111
994383  feet/sec       YDOT =       -3007
640511  meter/sec
 ZDOT =       7388
457653                 ZDOT =        2284
362009

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5244939
99                 X    =        -1598657
71
 Y    =       14428305
77  feet           Y    =         4397747
60  meter
 Z    =       16119928
69                 Z    =         4913354
27
 XDOT =     -17513
755330                 XDOT =       -5338
192625
 YDOT =     -14828
862326  feet/sec       YDOT =       -4519
837237  meter/sec
 ZDOT =       7536
028323                 ZDOT =        2296
981433


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   19279
33573081  
00016717  00000-0  10270-3 0  9117
2 25544  51
6391 170
0966 0007119 120
0893 240
0964 15
50166623 32495


Satellite: ISS
Catalog Number: 25544
Epoch time:      19279
33573081   =   yrday
fracday
Element set:     911
Inclination:       51
6391  deg
RA of node:       170
0966  deg
Eccentricity:     
0007119     
Arg of perigee:   120
0893  deg
Mean anomaly:     240
0964  deg
Mean motion:   15
50166623  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3249
Checksum:              306


Coasting Arc #13 (Orbit 3263)
---------------------------------------

Vector Time (GMT): 2019/280/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3073631
18                 A    =         6790152
12  meter
 Y    =        3304645
63  meter          E    =           
0018646
 Z    =       -5089143
69                 I    =           51
72399
 XDOT =      -6622
668530                 Wp   =           92
91492
 YDOT =       3364
435074  meter/sec      RA   =          164
22709  deg
 ZDOT =      -1821
813451                 TA   =          159
45953
                                          MA   =          159
38446
                                          Ha   =            229
746  n
mi
                                          Hp   =            218
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10084091
81                 X    =         3061169
58
 Y    =       10842013
21  feet           Y    =         3338947
24  meter
 Z    =      -16696665
66                 Z    =        -5074243
50
 XDOT =     -21727
915126                 XDOT =       -6650
949013
 YDOT =      11038
172815  feet/sec       YDOT =        3290
217515  meter/sec
 ZDOT =      -5977
078250                 ZDOT =       -1854
052861

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5093472
76                 X    =         1552490
50
 Y    =      -13983996
67  feet           Y    =        -4262322
18  meter
 Z    =      -16628925
85                 Z    =        -5068496
60
 XDOT =      18595
991692                 XDOT =        5668
058268
 YDOT =      14029
532958  feet/sec       YDOT =        4276
201645  meter/sec
 ZDOT =      -6124
133794                 ZDOT =       -1866
635981


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   19280
30274039  
00016717  00000-0  10270-3 0  9128
2 25544  51
6393 165
3042 0007158 123
4080 236
7756 15
50138656 32640


Satellite: ISS
Catalog Number: 25544
Epoch time:      19280
30274039   =   yrday
fracday
Element set:     912
Inclination:       51
6393  deg
RA of node:       165
3042  deg
Eccentricity:     
0007158     
Arg of perigee:   123
4080  deg
Mean anomaly:     236
7756  deg
Mean motion:   15
50138656  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3264
Checksum:              302


Coasting Arc #14 (Orbit 3279)
---------------------------------------

Vector Time (GMT): 2019/281/06:48:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2933919
69                 A    =         6789569
19  meter
 Y    =       -3254880
23  meter          E    =           
0011589
 Z    =        5179580
69                 I    =           51
75558
 XDOT =       6580
141358                 Wp   =          126
88948
 YDOT =      -3676
024441  meter/sec      RA   =          159
27809  deg
 ZDOT =       1408
246098                 TA   =          309
53568
                                          MA   =          309
63805
                                          Ha   =            229
677  n
mi
                                          Hp   =            218
712

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9625720
78                 X    =        -2922464
24
 Y    =      -10678740
92  feet           Y    =        -3287625
05  meter
 Z    =       16993374
97                 Z    =         5165356
77
 XDOT =      21588
390282                 XDOT =        6613
918177
 YDOT =     -12060
447641  feet/sec       YDOT =       -3602
251718  meter/sec
 ZDOT =       4620
229980                 ZDOT =        1440
292316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4919961
96                 X    =        -1499604
41
 Y    =       13589616
71  feet           Y    =         4142115
17  meter
 Z    =       16928706
19                 Z    =         5159869
65
 XDOT =     -19713
869875                 XDOT =       -6008
787538
 YDOT =     -13111
574238  feet/sec       YDOT =       -3996
407828  meter/sec
 ZDOT =       4766
439723                 ZDOT =        1452
810828


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   19281
33421208  
00016717  00000-0  10270-3 0  9135
2 25544  51
6406 160
1941 0006995 127
5794 232
5992 15
50179728 32800


Satellite: ISS
Catalog Number: 25544
Epoch time:      19281
33421208   =   yrday
fracday
Element set:     913
Inclination:       51
6406  deg
RA of node:       160
1941  deg
Eccentricity:     
0006995     
Arg of perigee:   127
5794  deg
Mean anomaly:     232
5992  deg
Mean motion:   15
50179728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3280
Checksum:              319


Coasting Arc #15 (Orbit 3281)
---------------------------------------

Vector Time (GMT): 2019/281/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         918932
46                 A    =         6789003
08  meter
 Y    =        4142382
76  meter          E    =           
0020920
 Z    =       -5317623
80                 I    =           51
76157
 XDOT =      -7247
853715                 Wp   =          105
22338
 YDOT =       2365
444369  meter/sec      RA   =          158
44830  deg
 ZDOT =        586
748359                 TA   =          170
40303
                                          MA   =          170
36300
                                          Ha   =            229
590  n
mi
                                          Hp   =            218
733

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3014870
28                 X    =          898373
00
 Y    =       13590494
61  feet           Y    =         4152543
64  meter
 Z    =      -17446272
32                 Z    =        -5313210
14
 XDOT =     -23779
047623                 XDOT =       -7276
616233
 YDOT =       7760
644254  feet/sec       YDOT =        2284
232967  meter/sec
 ZDOT =       1925
027424                 ZDOT =         551
470880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2450338
26                 X    =         -746863
10
 Y    =      -13728857
63  feet           Y    =        -4184555
80  meter
 Z    =      -17426351
17                 Z    =        -5311551
84
 XDOT =      23148
040206                 XDOT =        7055
522655
 YDOT =      -6385
012113  feet/sec       YDOT =       -1946
151692  meter/sec
 ZDOT =       1764
149940                 ZDOT =         537
712902


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   19281
46314660  
00016717  00000-0  10270-3 0  9143
2 25544  51
6434 159
5560 0007021 127
4165 232
7626 15
50172179 32823


Satellite: ISS
Catalog Number: 25544
Epoch time:      19281
46314660   =   yrday
fracday
Element set:     914
Inclination:       51
6434  deg
RA of node:       159
5560  deg
Eccentricity:     
0007021     
Arg of perigee:   127
4165  deg
Mean anomaly:     232
7626  deg
Mean motion:   15
50172179  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3282
Checksum:              300


Coasting Arc #16 (Orbit 3297)
---------------------------------------

Vector Time (GMT): 2019/282/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -809439
39                 A    =         6789108
39  meter
 Y    =       -4215814
57  meter          E    =           
0008670
 Z    =        5252114
99                 I    =           51
79293
 XDOT =       7123
706078                 Wp   =          108
39236
 YDOT =      -2647
247625  meter/sec      RA   =          153
50047  deg
 ZDOT =      -1028
312482                 TA   =          351
42545
                                          MA   =          351
44026
                                          Ha   =            229
517  n
mi
                                          Hp   =            218
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2655641
05                 X    =         -787748
75
 Y    =      -13831412
63  feet           Y    =        -4224744
62  meter
 Z    =       17231348
40                 Z    =         5248236
02
 XDOT =      23371
739100                 XDOT =        7157
773914
 YDOT =      -8685
195621  feet/sec       YDOT =       -2567
394907  meter/sec
 ZDOT =      -3373
728615                 ZDOT =        -993
625091

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2317772
09                 X    =          706456
93
 Y    =       13913680
24  feet           Y    =         4240889
74  meter
 Z    =       17213866
71                 Z    =         5246786
57
 XDOT =     -22651
024755                 XDOT =       -6904
032345
 YDOT =       7746
255173  feet/sec       YDOT =        2361
058577  meter/sec
 ZDOT =      -3215
507823                 ZDOT =        -980
086784


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   19282
49461408  
00016717  00000-0  10270-3 0  9151
2 25544  51
6433 154
4451 0006925 131
2589 228
9159 15
50203945 32981


Satellite: ISS
Catalog Number: 25544
Epoch time:      19282
49461408   =   yrday
fracday
Element set:     915
Inclination:       51
6433  deg
RA of node:       154
4451  deg
Eccentricity:     
0006925     
Arg of perigee:   131
2589  deg
Mean anomaly:     228
9159  deg
Mean motion:   15
50203945  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3298
Checksum:              326


Coasting Arc #17 (Orbit 3312)
---------------------------------------

Vector Time (GMT): 2019/283/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         711770
43                 A    =         6789560
37  meter
 Y    =        4344617
12  meter          E    =           
0019948
 Z    =       -5186329
73                 I    =           51
82292
 XDOT =      -6928
103012                 Wp   =          112
32736
 YDOT =       2886
702267  meter/sec      RA   =          148
55470  deg
 ZDOT =       1464
532487                 TA   =          171
78979
                                          MA   =          171
75710
                                          Ha   =            229
467  n
mi
                                          Hp   =            218
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2335204
82                 X    =          688327
25
 Y    =       14253993
18  feet           Y    =         4352445
11  meter
 Z    =      -17015517
49                 Z    =        -5182929
51
 XDOT =     -22729
996760                 XDOT =       -6966
981979
 YDOT =       9470
807964  feet/sec       YDOT =        2809
010070  meter/sec
 ZDOT =       4804
896612                 ZDOT =        1430
783447

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2228358
55                 X    =         -679203
69
 Y    =      -14289300
60  feet           Y    =        -4355378
82  meter
 Z    =      -17000224
85                 Z    =        -5181668
53
 XDOT =      21864
177659                 XDOT =        6664
201350
 YDOT =      -8954
098899  feet/sec       YDOT =       -2729
209344  meter/sec
 ZDOT =       4650
923878                 ZDOT =        1417
601598


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   19283
46161573  
00016717  00000-0  10270-3 0  9160
2 25544  51
6428 149
6538 0006942 134
4369 225
7351 15
50176842 33139


Satellite: ISS
Catalog Number: 25544
Epoch time:      19283
46161573   =   yrday
fracday
Element set:     916
Inclination:       51
6428  deg
RA of node:       149
6538  deg
Eccentricity:     
0006942     
Arg of perigee:   134
4369  deg
Mean anomaly:     225
7351  deg
Mean motion:   15
50176842  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3313
Checksum:              323


Coasting Arc #18 (Orbit 3328)
---------------------------------------

Vector Time (GMT): 2019/284/10:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -640002
79                 A    =         6789902
97  meter
 Y    =       -4468715
13  meter          E    =           
0009251
 Z    =        5063483
84                 I    =           51
85256
 XDOT =       6744
393274                 Wp   =          103
03418
 YDOT =      -3118
045541  meter/sec      RA   =          143
61133  deg
 ZDOT =      -1898
449831                 TA   =            5
31817
                                          MA   =            5
30835
                                          Ha   =            229
354  n
mi
                                          Hp   =            218
983

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2099746
70                 X    =         -614580
61
 Y    =      -14661138
87  feet           Y    =        -4475729
46  meter
 Z    =       16612479
79                 Z    =         5060437
09
 XDOT =      22127
274520                 XDOT =        6787
980617
 YDOT =     -10229
808205  feet/sec       YDOT =       -3042
381443  meter/sec
 ZDOT =      -6228
509943                 ZDOT =       -1865
581593

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2236337
09                 X    =          681635
55
 Y    =       14656425
66  feet           Y    =         4467278
54  meter
 Z    =       16598807
10                 Z    =         5059316
41
 XDOT =     -21082
820407                 XDOT =       -6426
043660
 YDOT =      10104
272924  feet/sec       YDOT =        3079
782387  meter/sec
 ZDOT =      -6078
524771                 ZDOT =       -1852
734350


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   19284
49307955  
00016717  00000-0  10270-3 0  9171
2 25544  51
6429 144
5431 0006810 139
2391 220
9270 15
50212319 33292


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
49307955   =   yrday
fracday
Element set:     917
Inclination:       51
6429  deg
RA of node:       144
5431  deg
Eccentricity:     
0006810     
Arg of perigee:   139
2391  deg
Mean anomaly:     220
9270  deg
Mean motion:   15
50212319  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3329
Checksum:              307


Coasting Arc #19 (Orbit 3334)
---------------------------------------

Vector Time (GMT): 2019/284/20:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 949486
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3833292
13                 A    =         6789710
40  meter
 Y    =        2157935
23  meter          E    =           
0017941
 Z    =       -5186537
74                 I    =           51
86163
 XDOT =      -5091
373426                 Wp   =          100
15327
 YDOT =       5514
973919  meter/sec      RA   =          141
59391  deg
 ZDOT =      -1475
791910                 TA   =          155
69011
                                          MA   =          155
60537
                                          Ha   =            229
479  n
mi
                                          Hp   =            219
200

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12576417
76                 X    =         3834070
21
 Y    =        7079839
99  feet           Y    =         2200805
65  meter
 Z    =      -17016199
95                 Z    =        -5167915
15
 XDOT =     -16703
981057                 XDOT =       -5145
496397
 YDOT =      18093
746455  feet/sec       YDOT =        5457
735822  meter/sec
 ZDOT =      -4841
836974                 ZDOT =       -1500
656185

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7288020
49                 X    =         2221388
65
 Y    =       12571937
97  feet           Y    =         3831926
69  meter
 Z    =      -16931409
03                 Z    =        -5160693
47
 XDOT =     -22660
999647                 XDOT =       -6907
072692
 YDOT =       6495
832462  feet/sec       YDOT =        1979
929734  meter/sec
 ZDOT =      -4955
457544                 ZDOT =       -1510
423459


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   19284
87987915  
00016717  00000-0  10270-3 0  9184
2 25544  51
6424 142
6228 0007179 143
3576 216
8067 15
50152800 33353


Satellite: ISS
Catalog Number: 25544
Epoch time:      19284
87987915   =   yrday
fracday
Element set:     918
Inclination:       51
6424  deg
RA of node:       142
6228  deg
Eccentricity:     
0007179     
Arg of perigee:   143
3576  deg
Mean anomaly:     216
8067  deg
Mean motion:   15
50152800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3335
Checksum:              331
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