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

 
Date: April 7th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16491 3871 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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


098/13:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 9
000/00:00:00 000 0 0 0 0 221 9

100/06:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 231 0
000/00:00:00 000 0 0 0 0 221 9

100/08:05:06 000 0 0 0 0 0 0
N/A 0 0 0 0 230 7
000/00:00:00 000 0 0 0 0 221 9

100/14:16:50 000 0 0 0 0 0 0
N/A 0 0 0 0 230 8
000/00:00:00 000 0 0 0 0 222 0

108/01:53:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 5
000/00:00:00 000 0 0 0 0 222 1

110/05:09:33 245 0 9 -3 1 3 1
N/A -2 9 -0 0 228 5
000/00:01:02 490 0 6 -0 0 222 2

Coasting Arc #1 (Orbit 2089)
---------------------------------------

Vector Time (GMT): 2020/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1692257
31                 A    =         6793210
92  meter
 Y    =        3887777
56  meter          E    =           
0006172
 Z    =        5302168
59                 I    =           51
51125
 XDOT =      -7203
195843                 Wp   =           95
64440
 YDOT =       2588
815923  meter/sec      RA   =          342
61168  deg
 ZDOT =        399
768254                 TA   =          350
52906
                                          MA   =          350
54070
                                          Ha   =            230
821  n
mi
                                          Hp   =            221
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5552025
28                 X    =         1622902
41
 Y    =       12755175
71  feet           Y    =         3906314
30  meter
 Z    =       17395566
23                 Z    =         5310220
07
 XDOT =     -23632
532294                 XDOT =       -7233
551234
 YDOT =       8493
490561  feet/sec       YDOT =        2508
094971  meter/sec
 ZDOT =       1311
575635                 ZDOT =         364
704063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8423138
18                 X    =         2567372
52
 Y    =       11013364
06  feet           Y    =         3356873
36  meter
 Z    =       17432205
02                 Z    =         5313336
09
 XDOT =     -19998
437412                 XDOT =       -6095
523723
 YDOT =      13468
675315  feet/sec       YDOT =        4105
252236  meter/sec
 ZDOT =       1150
590276                 ZDOT =         350
699916


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   20097
54902275  
00016717  00000-0  10270-3 0  9009
2 25544  51
6454 342
9712 0003646  89
4988 270
6580 15
48708136 20902


Satellite: ISS
Catalog Number: 25544
Epoch time:      20097
54902275   =   yrday
fracday
Element set:     900
Inclination:       51
6454  deg
RA of node:       342
9712  deg
Eccentricity:     
0003646     
Arg of perigee:    89
4988  deg
Mean anomaly:     270
6580  deg
Mean motion:   15
48708136  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2090
Checksum:              325


Coasting Arc #2 (Orbit 2104)
---------------------------------------

Vector Time (GMT): 2020/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2136142
04                 A    =         6793255
93  meter
 Y    =       -3688391
05  meter          E    =           
0018388
 Z    =       -5305732
39                 I    =           51
47921
 XDOT =       6894
145443                 Wp   =           86
77221
 YDOT =      -3267
521085  meter/sec      RA   =          337
65953  deg
 ZDOT =       -504
674823                 TA   =          178
39126
                                          MA   =          178
38534
                                          Ha   =            230
886  n
mi
                                          Hp   =            221
762

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7008340
03                 X    =        -2068966
29
 Y    =      -12101020
51  feet           Y    =        -3711903
84  meter
 Z    =      -17407258
49                 Z    =        -5315945
44
 XDOT =      22618
587411                 XDOT =        6932
622874
 YDOT =     -10720
213534  feet/sec       YDOT =       -3190
210753  meter/sec
 ZDOT =      -1655
757294                 ZDOT =        -471
091870

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9842921
58                 X    =        -3000122
50
 Y    =       -9851149
03  feet           Y    =        -3002630
22  meter
 Z    =      -17453822
88                 Z    =        -5319925
21
 XDOT =      18273
833155                 XDOT =        5569
864346
 YDOT =     -15601
161634  feet/sec       YDOT =       -4755
234066  meter/sec
 ZDOT =      -1501
533857                 ZDOT =        -457
667520


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   20098
51694599  
00016717  00000-0  10270-3 0  9015
2 25544  51
6449 338
1856 0003674  90
4439 269
7132 15
48708806 21059


Satellite: ISS
Catalog Number: 25544
Epoch time:      20098
51694599   =   yrday
fracday
Element set:     901
Inclination:       51
6449  deg
RA of node:       338
1856  deg
Eccentricity:     
0003674     
Arg of perigee:    90
4439  deg
Mean anomaly:     269
7132  deg
Mean motion:   15
48708806  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2105
Checksum:              338


Coasting Arc #3 (Orbit 2105)
---------------------------------------

Vector Time (GMT): 2020/098/13:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5149601
18                 A    =         6803424
40  meter
 Y    =        3923000
35  meter          E    =           
0017386
 Z    =        2067943
09                 I    =           51
51121
 XDOT =      -4445
848318                 Wp   =          106
33796
 YDOT =      -2906
753788  meter/sec      RA   =          337
41344  deg
 ZDOT =      -5522
916848                 TA   =           50
78490
                                          MA   =           50
63067
                                          Ha   =            230
941  n
mi
                                          Hp   =            221
894

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16895016
98                 X    =        -5203131
52
 Y    =       12870736
07  feet           Y    =         3865114
75  meter
 Z    =        6784590
20                 Z    =         2042797
85
 XDOT =     -14586
116529                 XDOT =       -4386
186437
 YDOT =      -9536
593793  feet/sec       YDOT =       -2956
137386  meter/sec
 ZDOT =     -18119
805932                 ZDOT =       -5544
367922

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7678856
27                 X    =        -2340515
39
 Y    =       19841562
08  feet           Y    =         6047708
12  meter
 Z    =        6669009
72                 Z    =         2032714
16
 XDOT =     -15869
109540                 XDOT =       -4836
904588
 YDOT =         19
825074  feet/sec       YDOT =           6
042683  meter/sec
 ZDOT =     -18217
955856                 ZDOT =       -5552
832945


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   20098
58147405  
00016717  00000-0  10270-3 0  9022
2 25544  51
6447 337
8662 0003702  89
8642 270
2932 15
48698173 21069


Satellite: ISS
Catalog Number: 25544
Epoch time:      20098
58147405   =   yrday
fracday
Element set:     902
Inclination:       51
6447  deg
RA of node:       337
8662  deg
Eccentricity:     
0003702     
Arg of perigee:    89
8642  deg
Mean anomaly:     270
2932  deg
Mean motion:   15
48698173  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2106
Checksum:              325


Coasting Arc #4 (Orbit 2120)
---------------------------------------

Vector Time (GMT): 2020/099/13:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4702036
13                 A    =         6803264
10  meter
 Y    =       -4407309
14  meter          E    =           
0008975
 Z    =       -2177606
75                 I    =           51
47792
 XDOT =       4784
132583                 Wp   =           59
73973
 YDOT =       2413
393762  meter/sec      RA   =          332
45702  deg
 ZDOT =       5467
038353                 TA   =          276
10822
                                          MA   =          276
21047
                                          Ha   =            230
919  n
mi
                                          Hp   =            221
963

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15426627
73                 X    =         4761548
17
 Y    =      -14459675
65  feet           Y    =        -4354395
06  meter
 Z    =       -7144379
10                 Z    =        -2154620
96
 XDOT =      15695
973041                 XDOT =        4730
233738
 YDOT =       7917
958536  feet/sec       YDOT =        2466
592440  meter/sec
 ZDOT =      17936
477537                 ZDOT =        5490
146891

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5245352
38                 X    =         1598783
41
 Y    =      -20519466
48  feet           Y    =        -6254333
38  meter
 Z    =       -7038678
12                 Z    =        -2145389
09
 XDOT =      15890
281458                 XDOT =        4843
357788
 YDOT =      -2102
555638  feet/sec       YDOT =        -640
858959  meter/sec
 ZDOT =      18042
254263                 ZDOT =        5499
279099


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   20099
54939555  
00016717  00000-0  10270-3 0  9035
2 25544  51
6426 333
0803 0003581  93
6022 266
5538 15
48682025 21217


Satellite: ISS
Catalog Number: 25544
Epoch time:      20099
54939555   =   yrday
fracday
Element set:     903
Inclination:       51
6426  deg
RA of node:       333
0803  deg
Eccentricity:     
0003581     
Arg of perigee:    93
6022  deg
Mean anomaly:     266
5538  deg
Mean motion:   15
48682025  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2121
Checksum:              306


Coasting Arc #5 (Orbit 2131)
---------------------------------------

Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1896603
24                 A    =         6797951
49  meter
 Y    =       -5027198
68  meter          E    =           
0011332
 Z    =       -4175933
69                 I    =           51
43733
 XDOT =       6666
466650                 Wp   =          104
84241
 YDOT =       -561
247255  meter/sec      RA   =          328
95685  deg
 ZDOT =       3709
026011                 TA   =          203
45552
                                          MA   =          203
50724
                                          Ha   =            230
970  n
mi
                                          Hp   =            221
921

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6222451
58                 X    =         1972962
44
 Y    =      -16493433
99  feet           Y    =        -5005562
85  meter
 Z    =      -13700569
85                 Z    =        -4166534
82
 XDOT =      21871
609743                 XDOT =        6654
230674
 YDOT =      -1841
362386  feet/sec       YDOT =        -486
766242  meter/sec
 ZDOT =      12168
720508                 ZDOT =        3741
379796

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17620860
41                 X    =         5370838
25
 Y    =        1202567
77  feet           Y    =          366542
65  meter
 Z    =      -13657122
40                 Z    =        -4162690
91
 XDOT =       8234
912402                 XDOT =        2510
001300
 YDOT =      19006
636544  feet/sec       YDOT =        5793
222819  meter/sec
 ZDOT =      12317
089139                 ZDOT =        3754
248770


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   20100
25920596  
00016717  00000-0  10270-3 0  9042
2 25544  51
6405 329
5705 0003750  96
9711 263
1866 15
48673033 21322


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
25920596   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       329
5705  deg
Eccentricity:     
0003750     
Arg of perigee:    96
9711  deg
Mean anomaly:     263
1866  deg
Mean motion:   15
48673033  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2132
Checksum:              298


Coasting Arc #6 (Orbit 2133)
---------------------------------------

Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS)     : 915727
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3806002
66                 A    =         6794100
64  meter
 Y    =        2418536
36  meter          E    =           
0008606
 Z    =        5075877
24                 I    =           51
42435
 XDOT =      -5526
964382                 Wp   =          113
62672
 YDOT =       5013
674107  meter/sec      RA   =          328
56595  deg
 ZDOT =       1749
597391                 TA   =          319
36423
                                          MA   =          319
42842
                                          Ha   =            230
715  n
mi
                                          Hp   =            221
859

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12486885
37                 X    =         3754018
99
 Y    =        7934830
58  feet           Y    =         2460807
47  meter
 Z    =       16653140
56                 Z    =         5094239
11
 XDOT =     -18133
085244                 XDOT =       -5591
116639
 YDOT =      16449
062032  feet/sec       YDOT =        4951
509076  meter/sec
 ZDOT =       5740
148919                 ZDOT =        1722
593093

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3985999
43                 X    =         1214932
63
 Y    =       14148871
29  feet           Y    =         4312575
97  meter
 Z    =       16737149
78                 Z    =         5101483
25
 XDOT =     -23478
105046                 XDOT =       -7156
126418
 YDOT =        -51
288613  feet/sec       YDOT =         -15
632769  meter/sec
 ZDOT =       5615
989642                 ZDOT =        1711
753643


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   20100
38826109  
00016717  00000-0  10270-3 0  9052
2 25544  51
6422 328
9333 0003629  98
7839 261
3721 15
48723431 21347


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
38826109   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:       328
9333  deg
Eccentricity:     
0003629     
Arg of perigee:    98
7839  deg
Mean anomaly:     261
3721  deg
Mean motion:   15
48723431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2134
Checksum:              303


Coasting Arc #7 (Orbit 2137)
---------------------------------------

Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3841764
38                 A    =         6794282
53  meter
 Y    =        2350531
00  meter          E    =           
0008598
 Z    =        5081129
61                 I    =           51
41503
 XDOT =      -5429
404284                 Wp   =          113
84010
 YDOT =       5126
367066  meter/sec      RA   =          327
28371  deg
 ZDOT =       1727
900837                 TA   =          319
36518
                                          MA   =          319
42931
                                          Ha   =            230
833  n
mi
                                          Hp   =            221
961

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12604213
86                 X    =         3790512
99
 Y    =        7711715
87  feet           Y    =         2393206
07  meter
 Z    =       16670372
73                 Z    =         5099667
01
 XDOT =     -17813
006181                 XDOT =       -5494
718571
 YDOT =      16818
789587  feet/sec       YDOT =        5065
286510  meter/sec
 ZDOT =       5668
966002                 ZDOT =        1701
367651

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13803293
90                 X    =         4207243
98
 Y    =       -4997076
51  feet           Y    =        -1523108
92  meter
 Z    =       16755190
23                 Z    =         5106981
98
 XDOT =       1726
428705                 XDOT =         526
215469
 YDOT =      23430
545461  feet/sec       YDOT =        7141
630257  meter/sec
 ZDOT =       5546
961134                 ZDOT =        1690
713754


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   20100
64637420  
00016717  00000-0  10270-3 0  9068
2 25544  51
6403 327
6549 0003659  99
5129 260
6434 15
48653431 21384


Satellite: ISS
Catalog Number: 25544
Epoch time:      20100
64637420   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       327
6549  deg
Eccentricity:     
0003659     
Arg of perigee:    99
5129  deg
Mean anomaly:     260
6434  deg
Mean motion:   15
48653431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2138
Checksum:              306


Coasting Arc #8 (Orbit 2152)
---------------------------------------

Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4110305
40                 A    =         6794281
36  meter
 Y    =       -1937737
37  meter          E    =           
0016542
 Z    =       -5065908
64                 I    =           51
38736
 XDOT =       4877
936208                 Wp   =           82
11628
 YDOT =      -5601
462353  meter/sec      RA   =          322
32368  deg
 ZDOT =      -1818
102885                 TA   =          170
18539
                                          MA   =          170
15304
                                          Ha   =            230
886  n
mi
                                          Hp   =            221
754

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13485253
93                 X    =        -4063723
97
 Y    =       -6357406
08  feet           Y    =        -1983441
42  meter
 Z    =      -16620435
18                 Z    =        -5085761
95
 XDOT =      16003
727715                 XDOT =        4949
042291
 YDOT =     -18377
501158  feet/sec       YDOT =       -5546
516272  meter/sec
 ZDOT =      -5964
904479                 ZDOT =       -1794
234624

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13175234
95                 X    =        -4015811
61
 Y    =        6756687
73  feet           Y    =         2059438
42  meter
 Z    =      -16711310
72                 Z    =        -5093607
51
 XDOT =      -4354
262393                 XDOT =       -1327
179177
 YDOT =     -22948
591016  feet/sec       YDOT =       -6994
730542  meter/sec
 ZDOT =      -5855
091117                 ZDOT =       -1784
631772


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   20101
61429259  
00016717  00000-0  10270-3 0  9076
2 25544  51
6399 322
8681 0003696 104
0732 256
0828 15
48694638 21532


Satellite: ISS
Catalog Number: 25544
Epoch time:      20101
61429259   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       322
8681  deg
Eccentricity:     
0003696     
Arg of perigee:   104
0732  deg
Mean anomaly:     256
0828  deg
Mean motion:   15
48694638  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2153
Checksum:              322


Coasting Arc #9 (Orbit 2168)
---------------------------------------

Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4327632
88                 A    =         6794498
95  meter
 Y    =        1471365
52  meter          E    =           
0009243
 Z    =        5021137
86                 I    =           51
36202
 XDOT =      -4296
951977                 Wp   =          116
48981
 YDOT =       6047
654115  meter/sec      RA   =          317
36241  deg
 ZDOT =       1924
497378                 TA   =          314
72103
                                          MA   =          314
79625
                                          Ha   =            230
805  n
mi
                                          Hp   =            221
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14198270
59                 X    =         4286467
94
 Y    =        4827314
69  feet           Y    =         1519530
03  meter
 Z    =       16473549
40                 Z    =         5042060
03
 XDOT =     -14097
611474                 XDOT =       -4373
607475
 YDOT =      19841
384893  feet/sec       YDOT =        5999
173939  meter/sec
 ZDOT =       6313
967775                 ZDOT =        1903
438061

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12250061
08                 X    =         3733818
62
 Y    =       -8465467
18  feet           Y    =        -2580274
40  meter
 Z    =       16569355
86                 Z    =         5050339
67
 XDOT =       6948
577821                 XDOT =        2117
926520
 YDOT =      22266
926004  feet/sec       YDOT =        6786
959046  meter/sec
 ZDOT =       6217
006613                 ZDOT =        1894
943616


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   20102
64673887  
00016717  00000-0  10270-3 0  9089
2 25544  51
6399 317
7625 0003713 106
0122 254
1437 15
48662851 21692


Satellite: ISS
Catalog Number: 25544
Epoch time:      20102
64673887   =   yrday
fracday
Element set:     908
Inclination:       51
6399  deg
RA of node:       317
7625  deg
Eccentricity:     
0003713     
Arg of perigee:   106
0122  deg
Mean anomaly:     254
1437  deg
Mean motion:   15
48662851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2169
Checksum:              315


Coasting Arc #10 (Orbit 2183)
---------------------------------------

Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4499807
87                 A    =         6794512
54  meter
 Y    =       -1009657
58  meter          E    =           
0016124
 Z    =       -5004302
15                 I    =           51
33819
 XDOT =       3667
941695                 Wp   =           83
06918
 YDOT =      -6402
041470  meter/sec      RA   =          312
39982  deg
 ZDOT =      -2010
204293                 TA   =          167
27882
                                          MA   =          167
23809
                                          Ha   =            230
922  n
mi
                                          Hp   =            221
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14763149
19                 X    =        -4463874
96
 Y    =       -3312524
88  feet           Y    =        -1059776
66  meter
 Z    =      -16418314
14                 Z    =        -5026073
33
 XDOT =      12033
929444                 XDOT =        3749
023088
 YDOT =     -21004
073064  feet/sec       YDOT =       -6360
570559  meter/sec
 ZDOT =      -6595
158440                 ZDOT =       -1992
189903

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11196432
26                 X    =        -3412672
55
 Y    =       10013917
36  feet           Y    =         3052242
01  meter
 Z    =      -16518044
62                 Z    =        -5034700
00
 XDOT =      -9375
840752                 XDOT =       -2857
756261
 YDOT =     -21204
944538  feet/sec       YDOT =       -6463
267095  meter/sec
 ZDOT =      -6512
138751                 ZDOT =       -1984
899891


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   20103
61465490  
00016717  00000-0  10270-3 0  9097
2 25544  51
6396 312
9768 0003913 111
0168 249
1401 15
48700691 21849


Satellite: ISS
Catalog Number: 25544
Epoch time:      20103
61465490   =   yrday
fracday
Element set:     909
Inclination:       51
6396  deg
RA of node:       312
9768  deg
Eccentricity:     
0003913     
Arg of perigee:   111
0168  deg
Mean anomaly:     249
1401  deg
Mean motion:   15
48700691  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2184
Checksum:              300


Coasting Arc #11 (Orbit 2199)
---------------------------------------

Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4613935
71                 A    =         6794704
17  meter
 Y    =         501992
14  meter          E    =           
0009872
 Z    =        4956760
90                 I    =           51
31641
 XDOT =      -3012
694740                 Wp   =          119
65885
 YDOT =       6722
005307  meter/sec      RA   =          307
43555  deg
 ZDOT =       2115
578545                 TA   =          309
58863
                                          MA   =          309
67577
                                          Ha   =            230
739  n
mi
                                          Hp   =            221
966

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15137584
35                 X    =         4583902
21
 Y    =        1646955
85  feet           Y    =          553420
45  meter
 Z    =       16262338
90                 Z    =         4979100
70
 XDOT =      -9884
169095                 XDOT =       -3097
914572
 YDOT =      22053
823187  feet/sec       YDOT =        6687
838687  meter/sec
 ZDOT =       6940
874493                 ZDOT =        2100
737142

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9861727
19                 X    =         3005854
45
 Y    =      -11457100
32  feet           Y    =        -3492124
18  meter
 Z    =       16364711
40                 Z    =         4987964
03
 XDOT =      11728
550702                 XDOT =        3574
862254
 YDOT =      19948
707363  feet/sec       YDOT =        6080
366004  meter/sec
 ZDOT =       6872
388670                 ZDOT =        2094
704067


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   20104
64709911  
00016717  00000-0  10270-3 0  9102
2 25544  51
6391 307
8716 0003759 115
2647 244
8893 15
48683599 22009


Satellite: ISS
Catalog Number: 25544
Epoch time:      20104
64709911   =   yrday
fracday
Element set:     910
Inclination:       51
6391  deg
RA of node:       307
8716  deg
Eccentricity:     
0003759     
Arg of perigee:   115
2647  deg
Mean anomaly:     244
8893  deg
Mean motion:   15
48683599  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2200
Checksum:              325


Coasting Arc #12 (Orbit 2214)
---------------------------------------

Vector Time (GMT): 2020/105/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4681605
93                 A    =         6794740
50  meter
 Y    =         -12653
45  meter          E    =           
0015395
 Z    =       -4938415
03                 I    =           51
29925
 XDOT =       2332
143914                 Wp   =           83
96077
 YDOT =      -6944
191444  meter/sec      RA   =          302
47032  deg
 ZDOT =      -2197
427010                 TA   =          164
46021
                                          MA   =          164
41289
                                          Ha   =            230
848  n
mi
                                          Hp   =            221
743

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15359599
52                 X    =        -4657128
54
 Y    =         -41513
95  feet           Y    =          -64869
60  meter
 Z    =      -16202149
05                 Z    =        -4961096
95
 XDOT =       7651
390793                 XDOT =        2420
296414
 YDOT =     -22782
780329  feet/sec       YDOT =       -6917
618842  meter/sec
 ZDOT =      -7209
406202                 ZDOT =       -2185
884340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8446753
90                 X    =        -2574570
59
 Y    =       12696116
05  feet           Y    =         3869776
17  meter
 Z    =      -16306122
79                 Z    =        -4970106
23
 XDOT =     -13830
457141                 XDOT =       -4215
523337
 YDOT =     -18373
994957  feet/sec       YDOT =       -5600
393663  meter/sec
 ZDOT =      -7156
040995                 ZDOT =       -2181
161295


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   20105
61501322  
00016717  00000-0  10270-3 0  9117
2 25544  51
6410 303
0863 0003903 118
4545 241
6998 15
48714678 22155


Satellite: ISS
Catalog Number: 25544
Epoch time:      20105
61501322   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:       303
0863  deg
Eccentricity:     
0003903     
Arg of perigee:   118
4545  deg
Mean anomaly:     241
6998  deg
Mean motion:   15
48714678  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2215
Checksum:              286


Coasting Arc #13 (Orbit 2230)
---------------------------------------

Vector Time (GMT): 2020/106/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4685071
74                 A    =         6794890
66  meter
 Y    =        -511556
96  meter          E    =           
0010413
 Z    =        4889060
03                 I    =           51
28214
 XDOT =      -1631
372582                 Wp   =          121
71488
 YDOT =       7126
151014  meter/sec      RA   =          297
50263  deg
 ZDOT =       2299
931294                 TA   =          305
61563
                                          MA   =          305
71258
                                          Ha   =            230
651  n
mi
                                          Hp   =            221
976

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15370970
28                 X    =         4666695
75
 Y    =       -1678336
49  feet           Y    =         -459267
89  meter
 Z    =       16040223
19                 Z    =         4911773
56
 XDOT =      -5352
272250                 XDOT =       -1722
109772
 YDOT =      23379
760545  feet/sec       YDOT =        7107
400510  meter/sec
 ZDOT =       7545
706345                 ZDOT =        2291
786347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6783149
93                 X    =         2067504
10
 Y    =      -13773900
86  feet           Y    =        -4198284
98  meter
 Z    =       16144374
65                 Z    =         4920805
39
 XDOT =      15813
641571                 XDOT =        4819
997951
 YDOT =      16622
081990  feet/sec       YDOT =        5066
410590  meter/sec
 ZDOT =       7507
921570                 ZDOT =        2288
414494


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   20106
64745256  
00016717  00000-0  10270-3 0  9128
2 25544  51
6403 297
9805 0003793 122
8617 237
2898 15
48716372 22311


Satellite: ISS
Catalog Number: 25544
Epoch time:      20106
64745256   =   yrday
fracday
Element set:     912
Inclination:       51
6403  deg
RA of node:       297
9805  deg
Eccentricity:     
0003793     
Arg of perigee:   122
8617  deg
Mean anomaly:     237
2898  deg
Mean motion:   15
48716372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2231
Checksum:              323


Coasting Arc #14 (Orbit 2245)
---------------------------------------

Vector Time (GMT): 2020/107/14:16:50
000
Vector Time (MET): N/A
Weight (LBS)     : 931644
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4645443
45                 A    =         6795022
32  meter
 Y    =        1005116
78  meter          E    =           
0014655
 Z    =       -4869336
61                 I    =           51
26832
 XDOT =        927
083327                 Wp   =           84
89851
 YDOT =      -7210
056112  meter/sec      RA   =          292
53580  deg
 ZDOT =      -2377
678221                 TA   =          161
64276
                                          MA   =          161
58981
                                          Ha   =            230
799  n
mi
                                          Hp   =            221
813

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15240956
20                 X    =        -4632685
36
 Y    =        3297627
24  feet           Y    =          953239
38  meter
 Z    =      -15975513
81                 Z    =        -4891871
29
 XDOT =       3041
611964                 XDOT =        1019
188755
 YDOT =     -23655
039739  feet/sec       YDOT =       -7199
173856  meter/sec
 ZDOT =      -7800
781565                 ZDOT =       -2372
950998

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5096906
53                 X    =        -1553537
11
 Y    =       14624278
15  feet           Y    =         4457479
98  meter
 Z    =      -16078873
27                 Z    =        -4900840
57
 XDOT =     -17484
853947                 XDOT =       -5329
383483
 YDOT =     -14628
559180  feet/sec       YDOT =       -4458
784838  meter/sec
 ZDOT =      -7778
677377                 ZDOT =       -2370
940865


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   20107
61536449  
00016717  00000-0  10270-3 0  9139
2 25544  51
6405 293
1961 0003924 125
0730 235
0789 15
48715712 22469


Satellite: ISS
Catalog Number: 25544
Epoch time:      20107
61536449   =   yrday
fracday
Element set:     913
Inclination:       51
6405  deg
RA of node:       293
1961  deg
Eccentricity:     
0003924     
Arg of perigee:   125
0730  deg
Mean anomaly:     235
0789  deg
Mean motion:   15
48715712  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2246
Checksum:              302


Coasting Arc #15 (Orbit 2253)
---------------------------------------

Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916536
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4613496
75                 A    =         6795461
89  meter
 Y    =       -1526857
23  meter          E    =           
0011057
 Z    =        4744035
58                 I    =           51
26287
 XDOT =       -364
336037                 Wp   =          119
83687
 YDOT =       7179
651575  meter/sec      RA   =          290
13888  deg
 ZDOT =       2654
984730                 TA   =          303
74170
                                          MA   =          303
84701
                                          Ha   =            230
544  n
mi
                                          Hp   =            222
060

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15136144
19                 X    =         4607183
92
 Y    =       -5009374
10  feet           Y    =        -1475301
00  meter
 Z    =       15564421
20                 Z    =         4766430
76
 XDOT =      -1195
328204                 XDOT =        -457
490292
 YDOT =      23555
287320  feet/sec       YDOT =        7175
056518  meter/sec
 ZDOT =       8710
579823                 ZDOT =        2652
988503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5041970
16                 X    =        -1536792
50
 Y    =       15018861
87  feet           Y    =         4577749
10  meter
 Z    =       15667170
20                 Z    =         4775353
48
 XDOT =     -16965
668877                 XDOT =       -5171
135874
 YDOT =     -14806
402048  feet/sec       YDOT =       -4512
991344  meter/sec
 ZDOT =       8701
005737                 ZDOT =        2652
066549


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   20108
13158255  
00016717  00000-0  10270-3 0  9143
2 25544  51
6395 290
6474 0003528 124
1539 235
9946 15
48725235 22549


Satellite: ISS
Catalog Number: 25544
Epoch time:      20108
13158255   =   yrday
fracday
Element set:     914
Inclination:       51
6395  deg
RA of node:       290
6474  deg
Eccentricity:     
0003528     
Arg of perigee:   124
1539  deg
Mean anomaly:     235
9946  deg
Mean motion:   15
48725235  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2254
Checksum:              316


Coasting Arc #16 (Orbit 2268)
---------------------------------------

Vector Time (GMT): 2020/109/01:53:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916536
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4469533
93                 A    =         6795675
71  meter
 Y    =        2009846
05  meter          E    =           
0013341
 Z    =       -4720187
90                 I    =           51
25315
 XDOT =       -333
650034                 Wp   =           83
69223
 YDOT =      -7138
063393  meter/sec      RA   =          285
16848  deg
 ZDOT =      -2728
690540                 TA   =          159
11578
                                          MA   =          159
06122
                                          Ha   =            230
694  n
mi
                                          Hp   =            221
975

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14663825
24                 X    =        -4468748
52
 Y    =        6593983
10  feet           Y    =         1959868
75  meter
 Z    =      -15486180
76                 Z    =        -4741897
26
 XDOT =      -1094
652343                 XDOT =        -240
550911
 YDOT =     -23418
843153  feet/sec       YDOT =       -7141
274058  meter/sec
 ZDOT =      -8952
396785                 ZDOT =       -2730
084890

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3223610
34                 X    =          982556
43
 Y    =      -15653150
00  feet           Y    =        -4771080
12  meter
 Z    =      -15585807
97                 Z    =        -4750554
27
 XDOT =      18412
457497                 XDOT =        5612
117045
 YDOT =      12694
666211  feet/sec       YDOT =        3869
334261  meter/sec
 ZDOT =      -8958
386746                 ZDOT =       -2730
516280


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   20109
09949370  
00016717  00000-0  10270-3 0  9156
2 25544  51
6398 285
8608 0003589 126
4070 233
7411 15
48699628 22694


Satellite: ISS
Catalog Number: 25544
Epoch time:      20109
09949370   =   yrday
fracday
Element set:     915
Inclination:       51
6398  deg
RA of node:       285
8608  deg
Eccentricity:     
0003589     
Arg of perigee:   126
4070  deg
Mean anomaly:     233
7411  deg
Mean motion:   15
48699628  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2269
Checksum:              344


Coasting Arc #17 (Orbit 2284)
---------------------------------------

Vector Time (GMT): 2020/110/01:53:00
000
Vector Time (MET): N/A
Weight (LBS)     : 916536
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4254655
25                 A    =         6795723
24  meter
 Y    =       -2503472
67  meter          E    =           
0011350
 Z    =        4664594
30                 I    =           51
24702
 XDOT =       1036
694029                 Wp   =          120
79828
 YDOT =       7047
228601  meter/sec      RA   =          280
19919  deg
 ZDOT =       2825
781930                 TA   =          300
92664
                                          MA   =          301
03815
                                          Ha   =            230
426  n
mi
                                          Hp   =            222
146

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13958842
68                 X    =         4259675
66
 Y    =       -8213493
02  feet           Y    =        -2455865
80  meter
 Z    =       15303787
09                 Z    =         4685274
08
 XDOT =       3401
227130                 XDOT =         944
086741
 YDOT =      23120
828742  feet/sec       YDOT =        7058
303980  meter/sec
 ZDOT =       9270
938091                 ZDOT =        2830
592540

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1223700
97                 X    =         -372984
06
 Y    =       16059227
73  feet           Y    =         4894852
61  meter
 Z    =       15398714
77                 Z    =         4693528
26
 XDOT =     -19680
557139                 XDOT =       -5998
633816
 YDOT =     -10443
995095  feet/sec       YDOT =       -3183
329705  meter/sec
 ZDOT =       9292
611277                 ZDOT =        2832
387917


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   20110
13192715  
00016717  00000-0  10270-3 0  9167
2 25544  51
6406 280
7566 0003435 132
0097 228
1345 15
48748241 22851


Satellite: ISS
Catalog Number: 25544
Epoch time:      20110
13192715   =   yrday
fracday
Element set:     916
Inclination:       51
6406  deg
RA of node:       280
7566  deg
Eccentricity:     
0003435     
Arg of perigee:   132
0097  deg
Mean anomaly:     228
1345  deg
Mean motion:   15
48748241  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2285
Checksum:              292


Coasting Arc #18 (Orbit 2286)
---------------------------------------

Vector Time (GMT): 2020/110/05:10:04
490
Vector Time (MET): N/A
Weight (LBS)     : 916214
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3745872
56                 A    =         6792182
68  meter
 Y    =        2450702
49  meter          E    =           
0004345
 Z    =        5105147
19                 I    =           51
24174
 XDOT =      -2471
135700                 Wp   =           72
61194
 YDOT =       7079
289397  meter/sec      RA   =          279
48540  deg
 ZDOT =      -1582
803116                 TA   =           32
76043
                                          MA   =           32
73350
                                          Ha   =            228
525  n
mi
                                          Hp   =            222
156

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12289608
13                 X    =         3693391
76
 Y    =        8040362
50  feet           Y    =         2492298
30  meter
 Z    =       16749170
59                 Z    =         5123215
62
 XDOT =      -8107
400590                 XDOT =       -2542
426388
 YDOT =      23226
015083  feet/sec       YDOT =        7051
256714  meter/sec
 ZDOT =      -5192
923610                 ZDOT =       -1594
980419

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4763691
15                 X    =        -1451973
06
 Y    =       13791745
36  feet           Y    =         4203723
99  meter
 Z    =       16831863
21                 Z    =         5130351
91
 XDOT =     -23497
310933                 XDOT =       -7161
980372
 YDOT =      -1700
279593  feet/sec       YDOT =        -518
245220  meter/sec
 ZDOT =      -5249
119877                 ZDOT =       -1599
931738


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   20110
26095963  
00016717  00000-0  10270-3 0  9179
2 25544  51
6423 280
1193 0001539 176
1499 183
9663 15
49336405 22877


Satellite: ISS
Catalog Number: 25544
Epoch time:      20110
26095963   =   yrday
fracday
Element set:     917
Inclination:       51
6423  deg
RA of node:       280
1193  deg
Eccentricity:     
0001539     
Arg of perigee:   176
1499  deg
Mean anomaly:     183
9663  deg
Mean motion:   15
49336405  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2287
Checksum:              320


Coasting Arc #19 (Orbit 2301)
---------------------------------------

Vector Time (GMT): 2020/111/05:10:04
490
Vector Time (MET): N/A
Weight (LBS)     : 916214
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3915815
52                 A    =         6792393
67  meter
 Y    =       -2257224
45  meter          E    =           
0013830
 Z    =       -5082866
98                 I    =           51
23837
 XDOT =       1939
571005                 Wp   =          108
93595
 YDOT =      -7201
297760  meter/sec      RA   =          274
50841  deg
 ZDOT =       1703
172178                 TA   =          177
65743
                                          MA   =          177
65094
                                          Ha   =            228
707  n
mi
                                          Hp   =            222
038

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12847163
77                 X    =        -3865593
75
 Y    =       -7405592
03  feet           Y    =        -2300733
32  meter
 Z    =      -16676072
75                 Z    =        -5101766
48
 XDOT =       6363
421933                 XDOT =        2011
680818
 YDOT =     -23626
304988  feet/sec       YDOT =       -7179
204824  meter/sec
 ZDOT =       5587
835229                 ZDOT =        1712
769384

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3765749
25                 X    =         1147800
37
 Y    =      -14241436
86  feet           Y    =        -4340789
95  meter
 Z    =      -16762589
94                 Z    =        -5109237
41
 XDOT =      23419
026677                 XDOT =        7138
119331
 YDOT =       -438
977520  feet/sec       YDOT =        -133
800348  meter/sec
 ZDOT =       5632
193345                 ZDOT =        1716
692531


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   20111
22849435  
00016717  00000-0  10270-3 0  9188
2 25544  51
6428 275
3306 0001528 175
8007 184
3157 15
49312338 23023


Satellite: ISS
Catalog Number: 25544
Epoch time:      20111
22849435   =   yrday
fracday
Element set:     918
Inclination:       51
6428  deg
RA of node:       275
3306  deg
Eccentricity:     
0001528     
Arg of perigee:   175
8007  deg
Mean anomaly:     184
3157  deg
Mean motion:   15
49312338  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2302
Checksum:              295


Coasting Arc #20 (Orbit 2317)
---------------------------------------

Vector Time (GMT): 2020/112/05:10:04
490
Vector Time (MET): N/A
Weight (LBS)     : 916214
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4063140
87                 A    =         6792422
57  meter
 Y    =        2049369
15  meter          E    =           
0004706
 Z    =        5039215
65                 I    =           51
23697
 XDOT =      -1410
655607                 Wp   =           69
98860
 YDOT =       7306
448525  meter/sec      RA   =          269
53245  deg
 ZDOT =      -1831
017037                 TA   =           37
87183
                                          MA   =           37
83873
                                          Ha   =            228
412  n
mi
                                          Hp   =            222
223

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13330514
66                 X    =         4015444
39
 Y    =        6723652
06  feet           Y    =         2094539
60  meter
 Z    =       16532859
74                 Z    =         5058837
04
 XDOT =      -4628
135192                 XDOT =       -1483
359520
 YDOT =      23971
287811  feet/sec       YDOT =        7290
266979  meter/sec
 ZDOT =      -6007
273744                 ZDOT =       -1838
046404

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2729474
01                 X    =         -831943
68
 Y    =       14576740
34  feet           Y    =         4442990
45  meter
 Z    =       16622700
80                 Z    =         5066599
20
 XDOT =     -23229
588903                 XDOT =       -7080
378698
 YDOT =       2548
980862  feet/sec       YDOT =         776
929367  meter/sec
 ZDOT =      -6039
850696                 ZDOT =       -1840
946492


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   20112
26052922  
00016717  00000-0  10270-3 0  9191
2 25544  51
6424 270
2238 0001504 184
9313 175
1822 15
49348474 23186


Satellite: ISS
Catalog Number: 25544
Epoch time:      20112
26052922   =   yrday
fracday
Element set:     919
Inclination:       51
6424  deg
RA of node:       270
2238  deg
Eccentricity:     
0001504     
Arg of perigee:   184
9313  deg
Mean anomaly:     175
1822  deg
Mean motion:   15
49348474  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2318
Checksum:              291
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