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

 
Date: August 27th 2020

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ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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


238/20:27:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 221 8

245/23:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 221 8

249/11:15:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 221 8

Coasting Arc #1 (Orbit 259)
---------------------------------------

Vector Time (GMT): 2020/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2363839
79                 A    =         6794119
29  meter
 Y    =       -4233354
78  meter          E    =           
0012546
 Z    =       -4771387
74                 I    =           51
69947
 XDOT =       7099
467029                 Wp   =           69
98379
 YDOT =       -930
251770  meter/sec      RA   =            9
81777  deg
 ZDOT =      -2693
444219                 TA   =          173
36766
                                          MA   =          173
35104
                                          Ha   =            229
241  n
mi
                                          Hp   =            221
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7755379
88                 X    =        -2293148
86
 Y    =      -13888959
25  feet           Y    =        -4259393
72  meter
 Z    =      -15654159
26                 Z    =        -4782698
58
 XDOT =      23292
214661                 XDOT =        7122
424907
 YDOT =      -3052
007121  feet/sec       YDOT =        -850
732113  meter/sec
 ZDOT =      -8836
759250                 ZDOT =       -2658
902127

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         321324
30                 X    =           97939
65
 Y    =       15852973
94  feet           Y    =         4831986
46  meter
 Z    =      -15706106
34                 Z    =        -4787221
21
 XDOT =     -20941
782088                 XDOT =       -6383
055181
 YDOT =      -8167
291743  feet/sec       YDOT =       -2489
390523  meter/sec
 ZDOT =      -8677
276845                 ZDOT =       -2644
833982


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   20237
52084312  
00016717  00000-0  10270-3 0  9006
2 25544  51
6432  10
2947 0001355  62
5167 297
6121 15
49180070  2608


Satellite: ISS
Catalog Number: 25544
Epoch time:      20237
52084312   =   yrday
fracday
Element set:     900
Inclination:       51
6432  deg
RA of node:        10
2947  deg
Eccentricity:     
0001355     
Arg of perigee:    62
5167  deg
Mean anomaly:     297
6121  deg
Mean motion:   15
49180070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             260
Checksum:              268


Coasting Arc #2 (Orbit 275)
---------------------------------------

Vector Time (GMT): 2020/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2643917
77                 A    =         6793907
92  meter
 Y    =        4024483
23  meter          E    =           
0008188
 Z    =        4787357
85                 I    =           51
66667
 XDOT =      -7042
375067                 Wp   =          110
94495
 YDOT =       1488
128544  meter/sec      RA   =            4
87284  deg
 ZDOT =       2631
806155                 TA   =          313
05850
                                          MA   =          313
12702
                                          Ha   =            229
114  n
mi
                                          Hp   =            221
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8674270
90                 X    =         2575464
12
 Y    =       13203685
14  feet           Y    =         4053666
61  meter
 Z    =       15706554
63                 Z    =         4800034
71
 XDOT =     -23104
905076                 XDOT =       -7071
276131
 YDOT =       4882
311496  feet/sec       YDOT =        1409
214043  meter/sec
 ZDOT =       8634
534630                 ZDOT =        2597
526988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1722414
84                 X    =         -524992
04
 Y    =      -15645450
56  feet           Y    =        -4768733
33  meter
 Z    =       15764812
06                 Z    =         4805114
71
 XDOT =      21747
318132                 XDOT =        6628
582567
 YDOT =       6168
142250  feet/sec       YDOT =        1880
049758  meter/sec
 ZDOT =       8476
241625                 ZDOT =        2583
558447


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   20238
55296258  
00016717  00000-0  10270-3 0  9015
2 25544  51
6443   5
1875 0001304  64
4486 295
6799 15
49213573  2763


Satellite: ISS
Catalog Number: 25544
Epoch time:      20238
55296258   =   yrday
fracday
Element set:     901
Inclination:       51
6443  deg
RA of node:         5
1875  deg
Eccentricity:     
0001304     
Arg of perigee:    64
4486  deg
Mean anomaly:     295
6799  deg
Mean motion:   15
49213573  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             276
Checksum:              322


Coasting Arc #3 (Orbit 280)
---------------------------------------

Vector Time (GMT): 2020/238/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4100534
74                 A    =         6796443
91  meter
 Y    =       -3506426
71  meter          E    =           
0009444
 Z    =       -4143172
57                 I    =           51
66112
 XDOT =       6094
874899                 Wp   =           67
54618
 YDOT =      -2661
885447  meter/sec      RA   =            3
13872  deg
 ZDOT =      -3782
753303                 TA   =          163
39569
                                          MA   =          163
36475
                                          Ha   =            229
367  n
mi
                                          Hp   =            221
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13453197
98                 X    =        -4040894
99
 Y    =      -11504024
64  feet           Y    =        -3551948
28  meter
 Z    =      -13593085
86                 Z    =        -4162946
49
 XDOT =      19996
308723                 XDOT =        6142
562297
 YDOT =      -8733
219970  feet/sec       YDOT =       -2593
461492  meter/sec
 ZDOT =     -12410
607948                 ZDOT =       -3753
031125

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8869355
48                 X    =         2703379
55
 Y    =      -15237530
21  feet           Y    =        -4644399
21  meter
 Z    =      -13684126
15                 Z    =        -4170921
65
 XDOT =      11145
382633                 XDOT =        3397
112627
 YDOT =      17499
560412  feet/sec       YDOT =        5333
866013  meter/sec
 ZDOT =     -12273
275987                 ZDOT =       -3740
894521


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   20238
87550004  
00016717  00000-0  10270-3 0  9023
2 25544  51
6425   3
5956 0001793  57
2989 302
8334 15
49176915  2815


Satellite: ISS
Catalog Number: 25544
Epoch time:      20238
87550004   =   yrday
fracday
Element set:     902
Inclination:       51
6425  deg
RA of node:         3
5956  deg
Eccentricity:     
0001793     
Arg of perigee:    57
2989  deg
Mean anomaly:     302
8334  deg
Mean motion:   15
49176915  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             281
Checksum:              312


Coasting Arc #4 (Orbit 296)
---------------------------------------

Vector Time (GMT): 2020/239/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4322668
47                 A    =         6796265
36  meter
 Y    =        3167881
05  meter          E    =           
0011356
 Z    =        4170840
49                 I    =           51
62593
 XDOT =      -5912
065633                 Wp   =           97
97498
 YDOT =       3142
110449  meter/sec      RA   =          358
19187  deg
 ZDOT =       3730
494350                 TA   =          313
59934
                                          MA   =          313
69352
                                          Ha   =            229
215  n
mi
                                          Hp   =            221
905

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14181983
16                 X    =         4266663
59
 Y    =       10393310
52  feet           Y    =         3215906
94  meter
 Z    =       13683859
88                 Z    =         4191702
25
 XDOT =     -19396
540790                 XDOT =       -5964
882741
 YDOT =      10308
761314  feet/sec       YDOT =        3075
702064  meter/sec
 ZDOT =      12239
154690                 ZDOT =        3701
647865

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7372222
86                 X    =        -2247053
53
 Y    =       15879586
70  feet           Y    =         4840098
03  meter
 Z    =       13779935
68                 Z    =         4200124
40
 XDOT =     -12832
742482                 XDOT =       -3911
419909
 YDOT =     -16491
859899  feet/sec       YDOT =       -5026
718897  meter/sec
 ZDOT =      12105
840402                 ZDOT =        3689
860154


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   20239
90761717  
00016717  00000-0  10270-3 0  9034
2 25544  51
6415 358
4893 0001708  55
0542 305
0768 15
49194867  2972


Satellite: ISS
Catalog Number: 25544
Epoch time:      20239
90761717   =   yrday
fracday
Element set:     903
Inclination:       51
6415  deg
RA of node:       358
4893  deg
Eccentricity:     
0001708     
Arg of perigee:    55
0542  deg
Mean anomaly:     305
0768  deg
Mean motion:   15
49194867  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             297
Checksum:              330


Coasting Arc #5 (Orbit 311)
---------------------------------------

Vector Time (GMT): 2020/240/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4509978
09                 A    =         6796141
13  meter
 Y    =       -2840398
22  meter          E    =           
0009920
 Z    =       -4227085
08                 I    =           51
59122
 XDOT =       5682
976603                 Wp   =           67
63660
 YDOT =      -3590
601311  meter/sec      RA   =          353
24170  deg
 ZDOT =      -3653
791313                 TA   =          164
82953
                                          MA   =          164
79977
                                          Ha   =            229
385  n
mi
                                          Hp   =            221
782

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14796516
05                 X    =        -4457348
18
 Y    =       -9318891
79  feet           Y    =        -2890537
59  meter
 Z    =      -13868389
36                 Z    =        -4248864
82
 XDOT =      18644
936362                 XDOT =        5740
453247
 YDOT =     -11780
188028  feet/sec       YDOT =       -3526
728696  meter/sec
 ZDOT =     -11987
504307                 ZDOT =       -3626
046473

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5916299
13                 X    =         1803287
98
 Y    =      -16370191
68  feet           Y    =        -4989634
43  meter
 Z    =      -13968718
04                 Z    =        -4257665
26
 XDOT =      14361
292763                 XDOT =        4377
322034
 YDOT =      15300
901185  feet/sec       YDOT =        4663
714681  meter/sec
 ZDOT =     -11859
252622                 ZDOT =       -3614
700199


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   20240
87522716  
00016717  00000-0  10270-3 0  9047
2 25544  51
6411 353
7013 0001805  60
0450 300
0879 15
49175605  3127


Satellite: ISS
Catalog Number: 25544
Epoch time:      20240
87522716   =   yrday
fracday
Element set:     904
Inclination:       51
6411  deg
RA of node:       353
7013  deg
Eccentricity:     
0001805     
Arg of perigee:    60
0450  deg
Mean anomaly:     300
0879  deg
Mean motion:   15
49175605  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             312
Checksum:              268


Coasting Arc #6 (Orbit 327)
---------------------------------------

Vector Time (GMT): 2020/241/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4675637
60                 A    =         6795887
78  meter
 Y    =        2480042
42  meter          E    =           
0011037
 Z    =        4254732
33                 I    =           51
55786
 XDOT =      -5427
339400                 Wp   =          100
44246
 YDOT =       4041
918630  meter/sec      RA   =          348
29040  deg
 ZDOT =       3598
333677                 TA   =          312
68211
                                          MA   =          312
77503
                                          Ha   =            229
156  n
mi
                                          Hp   =            221
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15340018
38                 X    =         4626890
78
 Y    =        8136622
10  feet           Y    =         2532056
05  meter
 Z    =       13959095
58                 Z    =         4277326
09
 XDOT =     -17806
231627                 XDOT =       -5489
612359
 YDOT =      13260
887895  feet/sec       YDOT =        3980
877938  meter/sec
 ZDOT =      11805
556683                 ZDOT =        3571
819063

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4357562
14                 X    =        -1328184
94
 Y    =       16721697
91  feet           Y    =         5096773
52  meter
 Z    =       14063200
34                 Z    =         4286463
46
 XDOT =     -15847
942085                 XDOT =       -4830
452748
 YDOT =     -13982
577098  feet/sec       YDOT =       -4261
889500  meter/sec
 ZDOT =      11682
962694                 ZDOT =        3560
967029


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   20241
90734045  
00016717  00000-0  10270-3 0  9053
2 25544  51
6416 348
5952 0001608  60
9506 299
1805 15
49218088  3285


Satellite: ISS
Catalog Number: 25544
Epoch time:      20241
90734045   =   yrday
fracday
Element set:     905
Inclination:       51
6416  deg
RA of node:       348
5952  deg
Eccentricity:     
0001608     
Arg of perigee:    60
9506  deg
Mean anomaly:     299
1805  deg
Mean motion:   15
49218088  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             328
Checksum:              312


Coasting Arc #7 (Orbit 342)
---------------------------------------

Vector Time (GMT): 2020/242/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4808489
91                 A    =         6795780
16  meter
 Y    =       -2137099
97  meter          E    =           
0010442
 Z    =       -4311325
92                 I    =           51
52522
 XDOT =       5130
717856                 Wp   =           67
93240
 YDOT =      -4453
931797  meter/sec      RA   =          343
33511  deg
 ZDOT =      -3517
609284                 TA   =          166
11804
                                          MA   =          166
08931
                                          Ha   =            229
386  n
mi
                                          Hp   =            221
709

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15775885
54                 X    =        -4763293
28
 Y    =       -7011482
83  feet           Y    =        -2190619
16  meter
 Z    =      -14144770
07                 Z    =        -4334573
51
 XDOT =      16833
063832                 XDOT =        5197
227955
 YDOT =     -14612
637128  feet/sec       YDOT =       -4396
184501  meter/sec
 ZDOT =     -11540
712873                 ZDOT =       -3492
525256

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2871242
78                 X    =          875154
80
 Y    =      -16933782
48  feet           Y    =        -5161416
90  meter
 Z    =      -14251910
48                 Z    =        -4343982
31
 XDOT =      17141
119784                 XDOT =        5224
613310
 YDOT =      12513
430827  feet/sec       YDOT =        3814
093716  meter/sec
 ZDOT =     -11424
706570                 ZDOT =       -3482
250563


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   20242
87494598  
00016717  00000-0  10270-3 0  9067
2 25544  51
6424 343
8068 0001852  63
0385 297
0954 15
49192555  3439


Satellite: ISS
Catalog Number: 25544
Epoch time:      20242
87494598   =   yrday
fracday
Element set:     906
Inclination:       51
6424  deg
RA of node:       343
8068  deg
Eccentricity:     
0001852     
Arg of perigee:    63
0385  deg
Mean anomaly:     297
0954  deg
Mean motion:   15
49192555  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             343
Checksum:              330


Coasting Arc #8 (Orbit 358)
---------------------------------------

Vector Time (GMT): 2020/243/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4915699
77                 A    =         6795524
50  meter
 Y    =        1765630
99  meter          E    =           
0010769
 Z    =        4339384
47                 I    =           51
49254
 XDOT =      -4808
134645                 Wp   =          102
15955
 YDOT =       4864
978633  meter/sec      RA   =          338
37965  deg
 ZDOT =       3457
715619                 TA   =          312
58880
                                          MA   =          312
67960
                                          Ha   =            229
151  n
mi
                                          Hp   =            221
805

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16127623
92                 X    =         4874512
78
 Y    =        5792752
58  feet           Y    =         1820371
59  meter
 Z    =       14236825
69                 Z    =         4363162
50
 XDOT =     -15774
719965                 XDOT =       -4878
974219
 YDOT =      15961
215988  feet/sec       YDOT =        4810
814557  meter/sec
 ZDOT =      11344
211349                 ZDOT =        3434
187974

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1311312
56                 X    =         -399688
07
 Y    =       16994227
65  feet           Y    =         5179840
59  meter
 Z    =       14346432
57                 Z    =         4372792
65
 XDOT =     -18370
188414                 XDOT =       -5599
233428
 YDOT =     -10928
443022  feet/sec       YDOT =       -3330
989433  meter/sec
 ZDOT =      11235
376643                 ZDOT =        3424
542801


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   20243
90705378  
00016717  00000-0  10270-3 0  9074
2 25544  51
6422 338
7011 0001669  64
4855 295
6467 15
49234178  3599


Satellite: ISS
Catalog Number: 25544
Epoch time:      20243
90705378   =   yrday
fracday
Element set:     907
Inclination:       51
6422  deg
RA of node:       338
7011  deg
Eccentricity:     
0001669     
Arg of perigee:    64
4855  deg
Mean anomaly:     295
6467  deg
Mean motion:   15
49234178  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             359
Checksum:              327


Coasting Arc #9 (Orbit 373)
---------------------------------------

Vector Time (GMT): 2020/244/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4995434
81                 A    =         6795439
42  meter
 Y    =       -1415497
04  meter          E    =           
0010904
 Z    =       -4395256
58                 I    =           51
46075
 XDOT =       4448
318745                 Wp   =           68
39471
 YDOT =      -5230
770136  meter/sec      RA   =          333
42034  deg
 ZDOT =      -3374
009397                 TA   =          167
29866
                                          MA   =          167
27116
                                          Ha   =            229
376  n
mi
                                          Hp   =            221
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16389221
82                 X    =        -4957885
81
 Y    =       -4644019
18  feet           Y    =        -1471149
74  meter
 Z    =      -14420133
14                 Z    =        -4419430
73
 XDOT =      14594
221604                 XDOT =        4522
868866
 YDOT =     -17161
319343  feet/sec       YDOT =       -5180
609107  meter/sec
 ZDOT =     -11069
584637                 ZDOT =       -3352
220425

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -156642
49                 X    =          -47744
63
 Y    =      -16938780
81  feet           Y    =        -5162940
39  meter
 Z    =      -14531583
32                 Z    =        -4429226
60
 XDOT =      19377
267692                 XDOT =        5906
191193
 YDOT =       9222
849142  feet/sec       YDOT =        2811
124418  meter/sec
 ZDOT =     -10968
768174                 ZDOT =       -3343
280539


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   20244
87465680  
00016717  00000-0  10270-3 0  9081
2 25544  51
6419 333
9132 0001834  65
7889 294
3452 15
49201807  3741


Satellite: ISS
Catalog Number: 25544
Epoch time:      20244
87465680   =   yrday
fracday
Element set:     908
Inclination:       51
6419  deg
RA of node:       333
9132  deg
Eccentricity:     
0001834     
Arg of perigee:    65
7889  deg
Mean anomaly:     294
3452  deg
Mean motion:   15
49201807  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             374
Checksum:              326


Coasting Arc #10 (Orbit 389)
---------------------------------------

Vector Time (GMT): 2020/245/20:27:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5046002
96                 A    =         6795179
10  meter
 Y    =        1041265
99  meter          E    =           
0010420
 Z    =        4423106
16                 I    =           51
43145
 XDOT =      -4063
820589                 Wp   =          104
58971
 YDOT =       5591
599823  meter/sec      RA   =          328
46049  deg
 ZDOT =       3310
643201                 TA   =          311
82898
                                          MA   =          311
91791
                                          Ha   =            229
119  n
mi
                                          Hp   =            221
790

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16555127
83                 X    =         5012499
65
 Y    =        3416227
02  feet           Y    =         1097506
90  meter
 Z    =       14511503
15                 Z    =         4447535
81
 XDOT =     -13332
744714                 XDOT =       -4142
126433
 YDOT =      18345
143777  feet/sec       YDOT =        5545
717595  meter/sec
 ZDOT =      10861
690292                 ZDOT =        3290
712648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1668913
67                 X    =          508684
89
 Y    =       16723505
95  feet           Y    =         5097324
61  meter
 Z    =       14624146
62                 Z    =         4457439
89
 XDOT =     -20299
556378                 XDOT =       -6187
304784
 YDOT =      -7417
728406  feet/sec       YDOT =       -2260
923618  meter/sec
 ZDOT =      10769
446719                 ZDOT =        3282
527360


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   20245
90676121  
00016717  00000-0  10270-3 0  9091
2 25544  51
6428 328
8075 0001603  70
2551 289
8772 15
49244273  3907


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
90676121   =   yrday
fracday
Element set:     909
Inclination:       51
6428  deg
RA of node:       328
8075  deg
Eccentricity:     
0001603     
Arg of perigee:    70
2551  deg
Mean anomaly:     289
8772  deg
Mean motion:   15
49244273  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             390
Checksum:              312


Coasting Arc #11 (Orbit 390)
---------------------------------------

Vector Time (GMT): 2020/245/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -419841
42                 A    =         6792849
81  meter
 Y    =       -4513177
82  meter          E    =           
0014510
 Z    =       -5072505
39                 I    =           51
42155
 XDOT =       6941
926919                 Wp   =           99
03638
 YDOT =      -2663
023705  meter/sec      RA   =          327
89690  deg
 ZDOT =       1796
999156                 TA   =          188
43958
                                          MA   =          188
46401
                                          Ha   =            229
357  n
mi
                                          Hp   =            221
785

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1377432
48                 X    =         -344703
61
 Y    =      -14807013
83  feet           Y    =        -4517452
92  meter
 Z    =      -16642078
06                 Z    =        -5074362
06
 XDOT =      22775
350784                 XDOT =        6962
461073
 YDOT =      -8736
954412  feet/sec       YDOT =       -2585
279202  meter/sec
 ZDOT =       5895
666523                 ZDOT =        1830
769733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7309976
90                 X    =         2228080
96
 Y    =      -12939554
69  feet           Y    =        -3943976
27  meter
 Z    =      -16650402
49                 Z    =        -5075042
68
 XDOT =      22756
698024                 XDOT =        6936
241558
 YDOT =       5078
137452  feet/sec       YDOT =        1547
816295  meter/sec
 ZDOT =       6051
598151                 ZDOT =        1844
527116


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   20245
97126965  
00016717  00000-0  10270-3 0  9106
2 25544  51
6443 328
4885 0001778  65
7932 294
3404 15
49207194  3919


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
97126965   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:       328
4885  deg
Eccentricity:     
0001778     
Arg of perigee:    65
7932  deg
Mean anomaly:     294
3404  deg
Mean motion:   15
49207194  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             391
Checksum:              329


Coasting Arc #12 (Orbit 406)
---------------------------------------

Vector Time (GMT): 2020/246/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         709693
03                 A    =         6792882
22  meter
 Y    =        4500860
92  meter          E    =           
0007520
 Z    =        5033640
48                 I    =           51
39384
 XDOT =      -6712
469741                 Wp   =           58
07728
 YDOT =       3178
957209  meter/sec      RA   =          322
93421  deg
 ZDOT =      -1890
110626                 TA   =           50
35277
                                          MA   =           50
28645
                                          Ha   =            229
301  n
mi
                                          Hp   =            221
770

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2328389
19                 X    =          634860
10
 Y    =       14766604
08  feet           Y    =         4508379
13  meter
 Z    =       16514568
51                 Z    =         5036905
80
 XDOT =     -22022
538519                 XDOT =       -6738
337965
 YDOT =      10429
649637  feet/sec       YDOT =        3103
748803  meter/sec
 ZDOT =      -6201
150347                 ZDOT =       -1922
779751

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6269075
71                 X    =        -1910814
28
 Y    =       13552954
55  feet           Y    =         4130940
55  meter
 Z    =       16529400
41                 Z    =         5038161
25
 XDOT =     -23105
140308                 XDOT =       -7042
446766
 YDOT =      -2916
620808  feet/sec       YDOT =        -888
986022  meter/sec
 ZDOT =      -6352
009034                 ZDOT =       -1936
092354


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   20247
00337181  
00016717  00000-0  10270-3 0  9117
2 25544  51
6441 323
3826 0001798  66
3115 293
8224 15
49232560  4075


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
00337181   =   yrday
fracday
Element set:     911
Inclination:       51
6441  deg
RA of node:       323
3826  deg
Eccentricity:     
0001798     
Arg of perigee:    66
3115  deg
Mean anomaly:     293
8224  deg
Mean motion:   15
49232560  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             407
Checksum:              286


Coasting Arc #13 (Orbit 421)
---------------------------------------

Vector Time (GMT): 2020/247/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1022178
78                 A    =         6793043
75  meter
 Y    =       -4477798
39  meter          E    =           
0014304
 Z    =       -5018009
40                 I    =           51
36813
 XDOT =       6417
787757                 Wp   =          100
28869
 YDOT =      -3667
676046  meter/sec      RA   =          317
96858  deg
 ZDOT =       1967
822647                 TA   =          188
92596
                                          MA   =          188
95142
                                          Ha   =            229
390  n
mi
                                          Hp   =            221
707

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3353604
92                 X    =         -947656
34
 Y    =      -14690939
59  feet           Y    =        -4488812
80  meter
 Z    =      -16463285
44                 Z    =        -5022793
37
 XDOT =      21055
734111                 XDOT =        6448
765366
 YDOT =     -12033
057894  feet/sec       YDOT =       -3595
734396  meter/sec
 ZDOT =       6456
111045                 ZDOT =        1999
072948

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5128325
71                 X    =         1563113
68
 Y    =      -14143933
82  feet           Y    =        -4311071
03  meter
 Z    =      -16485131
20                 Z    =        -5024667
99
 XDOT =      23156
923313                 XDOT =        7058
230226
 YDOT =        712
091101  feet/sec       YDOT =         217
045368  meter/sec
 ZDOT =       6600
430428                 ZDOT =        2011
811195


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   20247
97096720  
00016717  00000-0  10270-3 0  9125
2 25544  51
6443 318
5948 0001861  70
3154 289
8197 15
49213832  4229


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
97096720   =   yrday
fracday
Element set:     912
Inclination:       51
6443  deg
RA of node:       318
5948  deg
Eccentricity:     
0001861     
Arg of perigee:    70
3154  deg
Mean anomaly:     289
8197  deg
Mean motion:   15
49213832  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             422
Checksum:              318


Coasting Arc #14 (Orbit 437)
---------------------------------------

Vector Time (GMT): 2020/248/23:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1312964
14                 A    =         6793056
25  meter
 Y    =        4428514
05  meter          E    =           
0007850
 Z    =        4976308
94                 I    =           51
34358
 XDOT =      -6113
268414                 Wp   =           59
93972
 YDOT =       4136
711409  meter/sec      RA   =          313
00207  deg
 ZDOT =      -2062
088913                 TA   =           50
24927
                                          MA   =           50
18013
                                          Ha   =            229
248  n
mi
                                          Hp   =            221
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4307625
12                 X    =         1239173
64
 Y    =       14529245
57  feet           Y    =         4442784
33  meter
 Z    =       16326472
89                 Z    =         4982507
22
 XDOT =     -20056
654901                 XDOT =       -6149
055616
 YDOT =      13571
887824  feet/sec       YDOT =        4068
148211  meter/sec
 ZDOT =      -6765
383574                 ZDOT =       -2091
871850

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3984842
75                 X    =        -1214580
07
 Y    =       14589318
37  feet           Y    =         4446824
24  meter
 Z    =       16354850
83                 Z    =         4984958
53
 XDOT =     -23086
235866                 XDOT =       -7036
684692
 YDOT =       1455
819105  feet/sec       YDOT =         443
733663  meter/sec
 ZDOT =      -6902
939073                 ZDOT =       -2104
015829


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   20249
00306676  
00016717  00000-0  10270-3 0  9136
2 25544  51
6436 313
4887 0001738  71
8864 288
2476 15
49250058  4385


Satellite: ISS
Catalog Number: 25544
Epoch time:      20249
00306676   =   yrday
fracday
Element set:     913
Inclination:       51
6436  deg
RA of node:       313
4887  deg
Eccentricity:     
0001738     
Arg of perigee:    71
8864  deg
Mean anomaly:     288
2476  deg
Mean motion:   15
49250058  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             438
Checksum:              325


Coasting Arc #15 (Orbit 445)
---------------------------------------

Vector Time (GMT): 2020/249/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4027837
75                 A    =         6792048
10  meter
 Y    =        1688934
38  meter          E    =           
0005231
 Z    =        5197732
02                 I    =           51
32867
 XDOT =      -4167
215073                 Wp   =          113
72600
 YDOT =       6324
499109  meter/sec      RA   =          310
49000  deg
 ZDOT =       1171
200067                 TA   =          324
96915
                                          MA   =          325
00355
                                          Ha   =            229
113  n
mi
                                          Hp   =            221
806

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13214690
78                 X    =         3983404
68
 Y    =        5541123
31  feet           Y    =         1733728
48  meter
 Z    =       17052926
56                 Z    =         5217189
58
 XDOT =     -13671
965462                 XDOT =       -4243
316811
 YDOT =      20749
668993  feet/sec       YDOT =        6277
472897  meter/sec
 ZDOT =       3842
519906                 ZDOT =        1150
772136

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9129310
96                 X    =        -2782613
98
 Y    =      -10905131
02  feet           Y    =        -3323883
93  meter
 Z    =       17142584
49                 Z    =         5225059
75
 XDOT =      20857
998474                 XDOT =        6357
517935
 YDOT =     -11554
226723  feet/sec       YDOT =       -3521
728305  meter/sec
 ZDOT =       3748
016310                 ZDOT =        1142
395371


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   20249
51911496  
00016717  00000-0  10270-3 0  9145
2 25544  51
6437 310
9327 0001522  89
2832 270
8493 15
49240148  4460


Satellite: ISS
Catalog Number: 25544
Epoch time:      20249
51911496   =   yrday
fracday
Element set:     914
Inclination:       51
6437  deg
RA of node:       310
9327  deg
Eccentricity:     
0001522     
Arg of perigee:    89
2832  deg
Mean anomaly:     270
8493  deg
Mean motion:   15
49240148  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             446
Checksum:              309


Coasting Arc #16 (Orbit 460)
---------------------------------------

Vector Time (GMT): 2020/250/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4115657
13                 A    =         6792122
52  meter
 Y    =       -1434975
38  meter          E    =           
0015806
 Z    =       -5223115
48                 I    =           51
30679
 XDOT =       3671
194755                 Wp   =           82
31978
 YDOT =      -6623
436239  meter/sec      RA   =          305
51997  deg
 ZDOT =      -1073
834216                 TA   =          177
32173
                                          MA   =          177
31325
                                          Ha   =            229
336  n
mi
                                          Hp   =            221
701

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13502812
10                 X    =        -4073933
99
 Y    =       -4707924
46  feet           Y    =        -1480766
65  meter
 Z    =      -17136205
65                 Z    =        -5243006
32
 XDOT =      12044
602216                 XDOT =        3750
203237
 YDOT =     -21730
433856  feet/sec       YDOT =       -6581
940614  meter/sec
 ZDOT =      -3523
078136                 ZDOT =       -1055
808651

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9940816
12                 X    =         3029960
75
 Y    =       10125250
05  feet           Y    =         3086176
21  meter
 Z    =      -17227870
38                 Z    =        -5251054
89
 XDOT =     -19670
866106                 XDOT =       -5995
679989
 YDOT =      13464
154377  feet/sec       YDOT =        4103
874254  meter/sec
 ZDOT =      -3439
657010                 ZDOT =       -1048
407457


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   20250
48670702  
00016717  00000-0  10270-3 0  9156
2 25544  51
6430 306
1449 0001555  88
9030 271
2298 15
49196018  4618


Satellite: ISS
Catalog Number: 25544
Epoch time:      20250
48670702   =   yrday
fracday
Element set:     915
Inclination:       51
6430  deg
RA of node:       306
1449  deg
Eccentricity:     
0001555     
Arg of perigee:    88
9030  deg
Mean anomaly:     271
2298  deg
Mean motion:   15
49196018  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             461
Checksum:              298


Coasting Arc #17 (Orbit 476)
---------------------------------------

Vector Time (GMT): 2020/251/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4174868
04                 A    =         6791922
39  meter
 Y    =        1165760
51  meter          E    =           
0004994
 Z    =        5225141
91                 I    =           51
28812
 XDOT =      -3163
668990                 Wp   =          111
30103
 YDOT =       6911
013656  meter/sec      RA   =          300
54875  deg
 ZDOT =        983
326909                 TA   =          329
22030
                                          MA   =          329
24957
                                          Ha   =            229
146  n
mi
                                          Hp   =            221
766

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13697073
64                 X    =         4136141
03
 Y    =        3824673
59  feet           Y    =         1212230
61  meter
 Z    =       17142854
02                 Z    =         5245327
73
 XDOT =     -10379
491438                 XDOT =       -3245
491349
 YDOT =      22673
929317  feet/sec       YDOT =        6875
177796  meter/sec
 ZDOT =       3226
138153                 ZDOT =         967
759898

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10664808
95                 X    =        -3250633
77
 Y    =       -9235874
97  feet           Y    =        -2815094
69  meter
 Z    =       17235888
78                 Z    =         5253498
90
 XDOT =      18380
817501                 XDOT =        5602
473174
 YDOT =     -15323
059684  feet/sec       YDOT =       -4670
468592  meter/sec
 ZDOT =       3154
057190                 ZDOT =         961
356632


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   20251
51880123  
00016717  00000-0  10270-3 0  9162
2 25544  51
6432 301
0380 0001633  89
6808 270
4529 15
49239908  4777


Satellite: ISS
Catalog Number: 25544
Epoch time:      20251
51880123   =   yrday
fracday
Element set:     916
Inclination:       51
6432  deg
RA of node:       301
0380  deg
Eccentricity:     
0001633     
Arg of perigee:    89
6808  deg
Mean anomaly:     270
4529  deg
Mean motion:   15
49239908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             477
Checksum:              303


Coasting Arc #18 (Orbit 491)
---------------------------------------

Vector Time (GMT): 2020/252/11:15:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4232020
27                 A    =         6792001
66  meter
 Y    =        -907708
45  meter          E    =           
0016140
 Z    =       -5248450
49                 I    =           51
27079
 XDOT =       2625
387788                 Wp   =           84
11917
 YDOT =      -7128
983031  meter/sec      RA   =          295
57638  deg
 ZDOT =       -884
743798                 TA   =          177
35767
                                          MA   =          177
34913
                                          Ha   =            229
393  n
mi
                                          Hp   =            221
630

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13884580
94                 X    =        -4196061
37
 Y    =       -2978046
11  feet           Y    =         -954833
07  meter
 Z    =      -17219325
76                 Z    =        -5268920
72
 XDOT =       8613
476995                 XDOT =        2709
208695
 YDOT =     -23389
051940  feet/sec       YDOT =       -7099
155424  meter/sec
 ZDOT =      -2902
702749                 ZDOT =        -871
786787

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11339385
80                 X    =         3456244
79
 Y    =        8355254
09  feet           Y    =         2546681
45  meter
 Z    =      -17313682
02                 Z    =        -5277210
28
 XDOT =     -16844
989529                 XDOT =       -5134
352809
 YDOT =      16975
740948  feet/sec       YDOT =        5174
205841  meter/sec
 ZDOT =      -2842
662068                 ZDOT =        -866
443398


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   20252
48639155  
00016717  00000-0  10270-3 0  9177
2 25544  51
6421 296
2506 0001720  93
0552 267
0795 15
49198067  4926


Satellite: ISS
Catalog Number: 25544
Epoch time:      20252
48639155   =   yrday
fracday
Element set:     917
Inclination:       51
6421  deg
RA of node:       296
2506  deg
Eccentricity:     
0001720     
Arg of perigee:    93
0552  deg
Mean anomaly:     267
0795  deg
Mean motion:   15
49198067  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             492
Checksum:              317
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