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

 
Date: May 24th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 13864 993 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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


146/12:14:26 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 2

148/20:33:33 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 3

149/04:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 2

149/15:17:02 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 222 2

152/12:36:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 7
000/00:00:00 000 0 0 0 0 222 0

Coasting Arc #1 (Orbit 2802)
---------------------------------------

Vector Time (GMT): 2020/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2052256
75                 A    =         6793762
18  meter
 Y    =       -4415296
37  meter          E    =           
0008091
 Z    =        4734765
95                 I    =           51
98014
 XDOT =       4815
738838                 Wp   =           51
89924
 YDOT =      -5257
305054  meter/sec      RA   =          114
56119  deg
 ZDOT =      -2807
111999                 TA   =           65
85566
                                          MA   =           65
77107
                                          Ha   =            228
383  n
mi
                                          Hp   =            222
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6733125
81                 X    =        -2025730
23
 Y    =      -14485880
47  feet           Y    =        -4438098
45  meter
 Z    =       15534009
03                 Z    =         4724860
59
 XDOT =      15799
668103                 XDOT =        4887
805239
 YDOT =     -17248
376161  feet/sec       YDOT =       -5203
048730  meter/sec
 ZDOT =      -9209
685035                 ZDOT =       -2783
544255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15955971
96                 X    =        -4863380
25
 Y    =       -1410709
29  feet           Y    =         -429984
19  meter
 Z    =       15488641
35                 Z    =         4720937
88
 XDOT =      -6982
757453                 XDOT =       -2128
344472
 YDOT =     -21237
197523  feet/sec       YDOT =       -6473
097805  meter/sec
 ZDOT =      -9101
041138                 ZDOT =       -2773
997339


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   20143
54347066  
00016717  00000-0  10270-3 0  9002
2 25544  51
6384 115
3987 0001605 336
0011  24
1064 15
49380891 28037


Satellite: ISS
Catalog Number: 25544
Epoch time:      20143
54347066   =   yrday
fracday
Element set:     900
Inclination:       51
6384  deg
RA of node:       115
3987  deg
Eccentricity:     
0001605     
Arg of perigee:   336
0011  deg
Mean anomaly:      24
1064  deg
Mean motion:   15
49380891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2803
Checksum:              283


Coasting Arc #2 (Orbit 2817)
---------------------------------------

Vector Time (GMT): 2020/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2337435
59                 A    =         6794044
97  meter
 Y    =        4340615
86  meter          E    =           
0009534
 Z    =       -4683881
64                 I    =           51
99494
 XDOT =      -4404
029682                 Wp   =          102
17015
 YDOT =       5530
045550  meter/sec      RA   =          109
63555  deg
 ZDOT =       2930
068253                 TA   =          196
88689
                                          MA   =          196
91865
                                          Ha   =            228
410  n
mi
                                          Hp   =            222
428

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7668751
95                 X    =         2311475
78
 Y    =       14240865
68  feet           Y    =         4366610
26  meter
 Z    =      -15367065
73                 Z    =        -4672589
53
 XDOT =     -14448
916279                 XDOT =       -4479
773784
 YDOT =      18143
194061  feet/sec       YDOT =        5480
372617  meter/sec
 ZDOT =       9613
084818                 ZDOT =        2908
491708

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16222177
27                 X    =         4944519
63
 Y    =         201376
59  feet           Y    =           61379
58  meter
 Z    =      -15315323
48                 Z    =        -4668110
60
 XDOT =       8719
426359                 XDOT =        2657
681154
 YDOT =      20359
522345  feet/sec       YDOT =        6205
582411  meter/sec
 ZDOT =       9513
562213                 ZDOT =        2899
733763


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   20144
51096002  
00016717  00000-0  10270-3 0  9012
2 25544  51
6395 110
6103 0001633 340
4182  19
6905 15
49364111 28182


Satellite: ISS
Catalog Number: 25544
Epoch time:      20144
51096002   =   yrday
fracday
Element set:     901
Inclination:       51
6395  deg
RA of node:       110
6103  deg
Eccentricity:     
0001633     
Arg of perigee:   340
4182  deg
Mean anomaly:      19
6905  deg
Mean motion:   15
49364111  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2818
Checksum:              268


Coasting Arc #3 (Orbit 2833)
---------------------------------------

Vector Time (GMT): 2020/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2602073
40                 A    =         6794249
09  meter
 Y    =       -4258563
51  meter          E    =           
0008931
 Z    =        4606665
53                 I    =           52
00721
 XDOT =       3995
130105                 Wp   =           55
15321
 YDOT =      -5772
517945  meter/sec      RA   =          104
71064  deg
 ZDOT =      -3070
496887                 TA   =           65
45597
                                          MA   =           65
36291
                                          Ha   =            228
456  n
mi
                                          Hp   =            222
302

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8536986
23                 X    =        -2576636
30
 Y    =      -13971665
07  feet           Y    =        -4287520
26  meter
 Z    =       15113732
07                 Z    =         4594086
62
 XDOT =      13107
382233                 XDOT =        4074
298081
 YDOT =     -18938
707170  feet/sec       YDOT =       -5727
398408  meter/sec
 ZDOT =     -10073
808686                 ZDOT =       -3050
898514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16397864
46                 X    =        -4998069
09
 Y    =         968082
00  feet           Y    =          295071
39  meter
 Z    =       15056072
33                 Z    =         4589090
85
 XDOT =     -10339
134052                 XDOT =       -3151
368059
 YDOT =     -19393
809766  feet/sec       YDOT =       -5911
233217  meter/sec
 ZDOT =      -9983
349625                 ZDOT =       -3042
924966


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   20145
54294623  
00016717  00000-0  10270-3 0  9026
2 25544  51
6406 105
5025 0001748 343
5172  16
5921 15
49391749 28340


Satellite: ISS
Catalog Number: 25544
Epoch time:      20145
54294623   =   yrday
fracday
Element set:     902
Inclination:       51
6406  deg
RA of node:       105
5025  deg
Eccentricity:     
0001748     
Arg of perigee:   343
5172  deg
Mean anomaly:      16
5921  deg
Mean motion:   15
49391749  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2834
Checksum:              300


Coasting Arc #4 (Orbit 2848)
---------------------------------------

Vector Time (GMT): 2020/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 918884
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2889886
18                 A    =         6794561
16  meter
 Y    =        4146239
31  meter          E    =           
0008838
 Z    =       -4549651
52                 I    =           52
01532
 XDOT =      -3558
876336                 Wp   =          100
52814
 YDOT =       5977
053601  meter/sec      RA   =           99
78680  deg
 ZDOT =       3190
207351                 TA   =          201
38385
                                          MA   =          201
42080
                                          Ha   =            228
498  n
mi
                                          Hp   =            222
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9481253
88                 X    =         2865406
70
 Y    =       13603147
35  feet           Y    =         4178419
97  meter
 Z    =      -14926678
22                 Z    =        -4535672
22
 XDOT =     -11676
103464                 XDOT =       -3640
945342
 YDOT =      19609
755910  feet/sec       YDOT =        5936
796296  meter/sec
 ZDOT =      10466
559549                 ZDOT =        3172
721264

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16485025
43                 X    =         5024635
75
 Y    =       -2256842
11  feet           Y    =         -687885
47  meter
 Z    =      -14862574
33                 Z    =        -4530112
65
 XDOT =      11850
471659                 XDOT =        3612
023762
 YDOT =      18245
180485  feet/sec       YDOT =        5561
131012  meter/sec
 ZDOT =      10385
785145                 ZDOT =        3165
587312


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   20146
51043295  
00016717  00000-0  10270-3 0  9032
2 25544  51
6405 100
7144 0001796 348
2456  11
8652 15
49369673 28494


Satellite: ISS
Catalog Number: 25544
Epoch time:      20146
51043295   =   yrday
fracday
Element set:     903
Inclination:       51
6405  deg
RA of node:       100
7144  deg
Eccentricity:     
0001796     
Arg of perigee:   348
2456  deg
Mean anomaly:      11
8652  deg
Mean motion:   15
49369673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2849
Checksum:              310


Coasting Arc #5 (Orbit 2848)
---------------------------------------

Vector Time (GMT): 2020/146/12:14:26
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -994201
27                 A    =         6803123
17  meter
 Y    =        6720249
94  meter          E    =           
0012733
 Z    =        -204094
95                 I    =           52
04410
 XDOT =      -4689
523813                 Wp   =           37
56584
 YDOT =       -516
727068  meter/sec      RA   =           99
75821  deg
 ZDOT =       6037
143153                 TA   =          320
25151
                                          MA   =          320
34474
                                          Ha   =            228
466  n
mi
                                          Hp   =            222
240

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3261815
20                 X    =        -1068283
83
 Y    =       22048064
10  feet           Y    =         6708717
88  meter
 Z    =        -669602
84                 Z    =         -209103
22
 XDOT =     -15385
576814                 XDOT =       -4712
722297
 YDOT =      -1695
298781  feet/sec       YDOT =        -569
299395  meter/sec
 ZDOT =      19806
900109                 ZDOT =        6014
306665

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18868922
68                 X    =         5751247
63
 Y    =       11861215
84  feet           Y    =         3615298
59  meter
 Z    =        -693002
49                 Z    =         -211227
16
 XDOT =      -6936
496594                 XDOT =       -2114
244162
 YDOT =      12147
299754  feet/sec       YDOT =        3702
496965  meter/sec
 ZDOT =      19701
849711                 ZDOT =        6005
123792


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   20146
51043293  
00016717  00000-0  10270-3 0  9041
2 25544  51
6405 100
7145 0001729 349
3958  10
7155 15
49388627 28496


Satellite: ISS
Catalog Number: 25544
Epoch time:      20146
51043293   =   yrday
fracday
Element set:     904
Inclination:       51
6405  deg
RA of node:       100
7145  deg
Eccentricity:     
0001729     
Arg of perigee:   349
3958  deg
Mean anomaly:      10
7155  deg
Mean motion:   15
49388627  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2849
Checksum:              311


Coasting Arc #6 (Orbit 2864)
---------------------------------------

Vector Time (GMT): 2020/147/12:14:26
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         532477
06                 A    =         6803168
33  meter
 Y    =       -6777463
60  meter          E    =           
0010820
 Z    =          52412
09                 I    =           52
04960
 XDOT =       4700
335401                 Wp   =          128
24118
 YDOT =        316
104845  meter/sec      RA   =           94
83676  deg
 ZDOT =      -6039
615639                 TA   =           51
19866
                                          MA   =           51
10207
                                          Ha   =            228
495  n
mi
                                          Hp   =            222
241

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1746971
98                 X    =          607970
51
 Y    =      -22235772
96  feet           Y    =        -6771086
96  meter
 Z    =         171955
67                 Z    =           55180
87
 XDOT =      15421
047905                 XDOT =        4725
788376
 YDOT =       1037
089388  feet/sec       YDOT =         368
810682  meter/sec
 ZDOT =     -19815
011939                 ZDOT =       -6016
721294

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19828113
80                 X    =        -6043609
09
 Y    =      -10213849
96  feet           Y    =        -3113181
47  meter
 Z    =         185070
43                 Z    =           56409
47
 XDOT =       6229
666600                 XDOT =        1898
802380
 YDOT =     -12497
008263  feet/sec       YDOT =       -3809
088119  meter/sec
 ZDOT =     -19709
675952                 ZDOT =       -6007
509230


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   20147
54241869  
00016717  00000-0  10270-3 0  9055
2 25544  51
6414  95
6071 0001771 351
1017   9
0101 15
49378804 28656


Satellite: ISS
Catalog Number: 25544
Epoch time:      20147
54241869   =   yrday
fracday
Element set:     905
Inclination:       51
6414  deg
RA of node:        95
6071  deg
Eccentricity:     
0001771     
Arg of perigee:   351
1017  deg
Mean anomaly:       9
0101  deg
Mean motion:   15
49378804  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2865
Checksum:              295


Coasting Arc #7 (Orbit 2880)
---------------------------------------

Vector Time (GMT): 2020/148/12:14:26
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -40142
30                 A    =         6803131
98  meter
 Y    =        6795692
53  meter          E    =           
0013336
 Z    =          64353
11                 I    =           52
05145
 XDOT =      -4711
745593                 Wp   =           40
08238
 YDOT =        -91
524908  meter/sec      RA   =           89
91533  deg
 ZDOT =       6041
755378                 TA   =          320
60565
                                          MA   =          320
70256
                                          Ha   =            228
510  n
mi
                                          Hp   =            222
193

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -131700
47                 X    =         -116443
36
 Y    =       22295579
18  feet           Y    =         6794817
00  meter
 Z    =         211132
25                 Z    =           63973
88
 XDOT =     -15458
482918                 XDOT =       -4739
719318
 YDOT =       -300
278569  feet/sec       YDOT =        -144
372380  meter/sec
 ZDOT =      19822
032079                 ZDOT =        6018
799613

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20654761
37                 X    =         6295571
27
 Y    =        8395946
94  feet           Y    =         2559084
63  meter
 Z    =         208998
93                 Z    =           63702
87
 XDOT =      -5451
055561                 XDOT =       -1661
481735
 YDOT =      12862
828038  feet/sec       YDOT =        3920
589986  meter/sec
 ZDOT =      19716
393254                 ZDOT =        6009
556664


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   20148
57440220  
00016717  00000-0  10270-3 0  9062
2 25544  51
6416  90
4998 0001777 353
2531   6
8595 15
49392452 28814


Satellite: ISS
Catalog Number: 25544
Epoch time:      20148
57440220   =   yrday
fracday
Element set:     906
Inclination:       51
6416  deg
RA of node:        90
4998  deg
Eccentricity:     
0001777     
Arg of perigee:   353
2531  deg
Mean anomaly:       6
8595  deg
Mean motion:   15
49392452  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2881
Checksum:              320


Coasting Arc #8 (Orbit 2885)
---------------------------------------

Vector Time (GMT): 2020/148/20:33:33
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3083808
31                 A    =         6797274
75  meter
 Y    =       -4746463
18  meter          E    =           
0011606
 Z    =        3756156
03                 I    =           52
03004
 XDOT =       3184
322228                 Wp   =           76
54808
 YDOT =      -5483
653351  meter/sec      RA   =           88
17945  deg
 ZDOT =      -4301
316234                 TA   =           58
91328
                                          MA   =           58
79944
                                          Ha   =            228
514  n
mi
                                          Hp   =            222
253

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10117481
32                 X    =        -3048747
98
 Y    =      -15572385
77  feet           Y    =        -4780753
07  meter
 Z    =       12323346
55                 Z    =         3741260
53
 XDOT =      10447
251404                 XDOT =        3266
298699
 YDOT =     -17990
988683  feet/sec       YDOT =       -5447
584967  meter/sec
 ZDOT =     -14111
929901                 ZDOT =       -4285
649811

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13519086
33                 X    =         4120617
51
 Y    =       12797463
92  feet           Y    =         3900667
00  meter
 Z    =       12255069
11                 Z    =         3735345
06
 XDOT =      -5173
557868                 XDOT =       -1576
900438
 YDOT =      18953
249686  feet/sec       YDOT =        5776
950504  meter/sec
 ZDOT =     -14039
513735                 ZDOT =       -4279
243787


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   20148
89689563  
00016717  00000-0  10270-3 0  9073
2 25544  51
6399  88
9000 0001551 349
2896  10
8221 15
49383567 28862


Satellite: ISS
Catalog Number: 25544
Epoch time:      20148
89689563   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:        88
9000  deg
Eccentricity:     
0001551     
Arg of perigee:   349
2896  deg
Mean anomaly:      10
8221  deg
Mean motion:   15
49383567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2886
Checksum:              349


Coasting Arc #9 (Orbit 2890)
---------------------------------------

Vector Time (GMT): 2020/149/04:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 954372
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3424203
53                 A    =         6794137
97  meter
 Y    =       -3587076
31  meter          E    =           
0010862
 Z    =       -4654922
38                 I    =           52
02223
 XDOT =       2731
681183                 Wp   =           62
10489
 YDOT =       6490
344938  meter/sec      RA   =           86
54902  deg
 ZDOT =      -2992
392826                 TA   =          178
15063
                                          MA   =          178
14661
                                          Ha   =            228
546  n
mi
                                          Hp   =            222
247

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11234263
54                 X    =         3486671
68
 Y    =      -11768623
05  feet           Y    =        -3548434
45  meter
 Z    =      -15272055
04                 Z    =        -4638137
78
 XDOT =       8962
208606                 XDOT =        2673
436491
 YDOT =      21293
782606  feet/sec       YDOT =        6520
567321  meter/sec
 ZDOT =      -9817
561766                 ZDOT =       -2979
263915

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16325287
42                 X    =         4975947
60
 Y    =        -744301
77  feet           Y    =         -226863
18  meter
 Z    =      -15194598
92                 Z    =        -4631313
75
 XDOT =      -8146
973418                 XDOT =       -2483
197498
 YDOT =      20475
873789  feet/sec       YDOT =        6241
046331  meter/sec
 ZDOT =      -9757
517701                 ZDOT =       -2974
091395


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   20149
21939061  
00016717  00000-0  10270-3 0  9082
2 25544  51
6430  87
3066 0001590 358
5739   1
5406 15
49383229 28918


Satellite: ISS
Catalog Number: 25544
Epoch time:      20149
21939061   =   yrday
fracday
Element set:     908
Inclination:       51
6430  deg
RA of node:        87
3066  deg
Eccentricity:     
0001590     
Arg of perigee:   358
5739  deg
Mean anomaly:       1
5406  deg
Mean motion:   15
49383229  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2891
Checksum:              314


Coasting Arc #10 (Orbit 2897)
---------------------------------------

Vector Time (GMT): 2020/149/15:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1373154
15                 A    =         6802867
62  meter
 Y    =       -6593370
22  meter          E    =           
0012467
 Z    =         921414
52                 I    =           52
05127
 XDOT =       4487
406081                 Wp   =          118
61938
 YDOT =      -1773
747003  meter/sec      RA   =           84
36030  deg
 ZDOT =      -5949
891016                 TA   =           51
48255
                                          MA   =           51
37084
                                          Ha   =            228
605  n
mi
                                          Hp   =            222
184

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4505098
90                 X    =        -1303798
76
 Y    =      -21631792
05  feet           Y    =        -6608338
14  meter
 Z    =        3023013
52                 Z    =          914911
82
 XDOT =      14722
460897                 XDOT =        4535
808210
 YDOT =      -5819
379932  feet/sec       YDOT =       -1723
294165  meter/sec
 ZDOT =     -19520
639816                 ZDOT =       -5927
975706

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17696602
75                 X    =        -5393924
52
 Y    =       13237760
80  feet           Y    =         4034869
49  meter
 Z    =        2993475
26                 Z    =          912411
26
 XDOT =     -10584
230900                 XDOT =       -3226
073578
 YDOT =      -9716
620861  feet/sec       YDOT =       -2961
626038  meter/sec
 ZDOT =     -19419
673077                 ZDOT =       -5919
116354


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   20149
67088333  
00016717  00000-0  10270-3 0  9090
2 25544  51
6442  85
0744 0001746 358
9031   1
2115 15
49362866 28986


Satellite: ISS
Catalog Number: 25544
Epoch time:      20149
67088333   =   yrday
fracday
Element set:     909
Inclination:       51
6442  deg
RA of node:        85
0744  deg
Eccentricity:     
0001746     
Arg of perigee:   358
9031  deg
Mean anomaly:       1
2115  deg
Mean motion:   15
49362866  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2898
Checksum:              320


Coasting Arc #11 (Orbit 2912)
---------------------------------------

Vector Time (GMT): 2020/150/15:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1849022
07                 A    =         6802814
10  meter
 Y    =        6490799
56  meter          E    =           
0011794
 Z    =        -805044
56                 I    =           52
04661
 XDOT =      -4370
183570                 Wp   =           33
61479
 YDOT =       1979
419156  meter/sec      RA   =           79
43784  deg
 ZDOT =       5973
219529                 TA   =          317
74603
                                          MA   =          317
83685
                                          Ha   =            228
576  n
mi
                                          Hp   =            222
093

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6066345
39                 X    =         1780213
04
 Y    =       21295274
14  feet           Y    =         6511092
00  meter
 Z    =       -2641222
31                 Z    =         -796229
11
 XDOT =     -14337
872606                 XDOT =       -4421
007623
 YDOT =       6494
157336  feet/sec       YDOT =        1930
263764  meter/sec
 ZDOT =      19597
176931                 ZDOT =        5951
867738

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16481305
92                 X    =         5023502
05
 Y    =      -14794135
01  feet           Y    =        -4509252
35  meter
 Z    =       -2601043
33                 Z    =         -792798
01
 XDOT =      11096
862735                 XDOT =        3382
323762
 YDOT =       8964
209865  feet/sec       YDOT =        2732
291167  meter/sec
 ZDOT =      19498
785498                 ZDOT =        5943
229820


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   20150
63836400  
00016717  00000-0  10270-3 0  9106
2 25544  51
6437  80
2857 0001912 359
1946    
9201 15
49409680 29131


Satellite: ISS
Catalog Number: 25544
Epoch time:      20150
63836400   =   yrday
fracday
Element set:     910
Inclination:       51
6437  deg
RA of node:        80
2857  deg
Eccentricity:     
0001912     
Arg of perigee:   359
1946  deg
Mean anomaly:        
9201  deg
Mean motion:   15
49409680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2913
Checksum:              291


Coasting Arc #12 (Orbit 2928)
---------------------------------------

Vector Time (GMT): 2020/151/15:17:02
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2290825
64                 A    =         6803053
36  meter
 Y    =       -6367120
09  meter          E    =           
0012203
 Z    =         650959
81                 I    =           52
03951
 XDOT =       4256
474709                 Wp   =          121
07827
 YDOT =      -2152
123851  meter/sec      RA   =           74
51607  deg
 ZDOT =      -5994
208789                 TA   =           51
94571
                                          MA   =           51
83566
                                          Ha   =            228
670  n
mi
                                          Hp   =            222
127

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7515832
14                 X    =        -2222618
34
 Y    =      -20889501
60  feet           Y    =        -6392356
42  meter
 Z    =        2135694
90                 Z    =          639996
89
 XDOT =      13964
812039                 XDOT =        4309
340475
 YDOT =      -7060
773790  feet/sec       YDOT =       -2104
228720  meter/sec
 ZDOT =     -19666
039335                 ZDOT =       -5973
404323

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15207303
63                 X    =        -4635186
15
 Y    =       16180489
60  feet           Y    =         4931813
23  meter
 Z    =        2085635
40                 Z    =          635701
67
 XDOT =     -11505
034713                 XDOT =       -3506
734580
 YDOT =      -8257
237875  feet/sec       YDOT =       -2516
806104  meter/sec
 ZDOT =     -19570
152290                 ZDOT =       -5964
982418


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   20151
67034524  
00016717  00000-0  10270-3 0  9119
2 25544  51
6436  75
1784 0001775   4
5032 355
6134 15
49360851 29294


Satellite: ISS
Catalog Number: 25544
Epoch time:      20151
67034524   =   yrday
fracday
Element set:     911
Inclination:       51
6436  deg
RA of node:        75
1784  deg
Eccentricity:     
0001775     
Arg of perigee:     4
5032  deg
Mean anomaly:     355
6134  deg
Mean motion:   15
49360851  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2929
Checksum:              297


Coasting Arc #13 (Orbit 2942)
---------------------------------------

Vector Time (GMT): 2020/152/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3941987
66                 A    =         6791047
73  meter
 Y    =        1392895
06  meter          E    =           
0003207
 Z    =        5349381
62                 I    =           51
99104
 XDOT =      -2584
607607                 Wp   =           51
35275
 YDOT =      -7214
121054  meter/sec      RA   =           70
14742  deg
 ZDOT =        -24
209622                 TA   =           38
88852
                                          MA   =           38
86545
                                          Ha   =            228
706  n
mi
                                          Hp   =            221
998

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12933030
39                 X    =        -3983254
77
 Y    =        4569865
69  feet           Y    =         1348581
71  meter
 Z    =       17550464
62                 Z    =         5330132
82
 XDOT =      -8479
683750                 XDOT =       -2503
627472
 YDOT =     -23668
376163  feet/sec       YDOT =       -7242
571186  meter/sec
 ZDOT =        -79
427894                 ZDOT =         -36
568664

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1654184
58                 X    =          504195
46
 Y    =       13730096
04  feet           Y    =         4184933
27  meter
 Z    =       17461783
77                 Z    =         5322351
69
 XDOT =     -23937
453301                 XDOT =       -7296
135766
 YDOT =       3064
931999  feet/sec       YDOT =         934
191273  meter/sec
 ZDOT =       -135
847148                 ZDOT =         -41
406211


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   20152
57332489  
00016717  00000-0  10270-3 0  9121
2 25544  51
6433  70
7082 0001913   3
0758 357
0404 15
49434462 29438


Satellite: ISS
Catalog Number: 25544
Epoch time:      20152
57332489   =   yrday
fracday
Element set:     912
Inclination:       51
6433  deg
RA of node:        70
7082  deg
Eccentricity:     
0001913     
Arg of perigee:     3
0758  deg
Mean anomaly:     357
0404  deg
Mean motion:   15
49434462  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2943
Checksum:              293


Coasting Arc #14 (Orbit 2957)
---------------------------------------

Vector Time (GMT): 2020/153/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3885512
24                 A    =         6791126
71  meter
 Y    =       -1573977
38  meter          E    =           
0015295
 Z    =       -5355805
15                 I    =           51
97976
 XDOT =       3078
382761                 Wp   =           83
81825
 YDOT =       7000
616402  meter/sec      RA   =           65
22089  deg
 ZDOT =        177
972120                 TA   =          187
86208
                                          MA   =          187
88608
                                          Ha   =            228
701  n
mi
                                          Hp   =            222
049

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12747743
58                 X    =         3928839
79
 Y    =       -5163967
79  feet           Y    =        -1530284
04  meter
 Z    =      -17571539
20                 Z    =        -5336825
62
 XDOT =      10099
680975                 XDOT =        2999
006503
 YDOT =      22967
901583  feet/sec       YDOT =        7034
597233  meter/sec
 ZDOT =        583
898033                 ZDOT =         192
733696

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2509141
59                 X    =         -764786
36
 Y    =      -13636037
27  feet           Y    =        -4156264
16  meter
 Z    =      -17484084
64                 Z    =        -5329149
00
 XDOT =      23520
059298                 XDOT =        7168
914074
 YDOT =      -5154
462170  feet/sec       YDOT =       -1571
080070  meter/sec
 ZDOT =        651
371079                 ZDOT =         198
537905


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   20153
54080359  
00016717  00000-0  10270-3 0  9136
2 25544  51
6445  65
9195 0002030  11
4599 348
6597 15
49415937 29580


Satellite: ISS
Catalog Number: 25544
Epoch time:      20153
54080359   =   yrday
fracday
Element set:     913
Inclination:       51
6445  deg
RA of node:        65
9195  deg
Eccentricity:     
0002030     
Arg of perigee:    11
4599  deg
Mean anomaly:     348
6597  deg
Mean motion:   15
49415937  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2958
Checksum:              330


Coasting Arc #15 (Orbit 2973)
---------------------------------------

Vector Time (GMT): 2020/154/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3817070
14                 A    =         6791078
36  meter
 Y    =        1737712
75  meter          E    =           
0003946
 Z    =        5338900
50                 I    =           51
96438
 XDOT =      -3561
875662                 Wp   =           47
06926
 YDOT =      -6776
843372  meter/sec      RA   =           60
29417  deg
 ZDOT =       -338
069198                 TA   =           46
15787
                                          MA   =           46
12526
                                          Ha   =            228
805  n
mi
                                          Hp   =            221
879

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12523196
01                 X    =        -3862151
70
 Y    =        5701157
32  feet           Y    =         1694774
90  meter
 Z    =       17516077
76                 Z    =         5320249
15
 XDOT =     -11685
943773                 XDOT =       -3484
188094
 YDOT =     -22233
738097  feet/sec       YDOT =       -6816
240386  meter/sec
 ZDOT =      -1109
150911                 ZDOT =        -355
183659

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3312421
26                 X    =         1009626
00
 Y    =       13467196
22  feet           Y    =         4104801
41  meter
 Z    =       17430120
62                 Z    =         5312700
76
 XDOT =     -23002
298695                 XDOT =       -7011
100642
 YDOT =       7206
400892  feet/sec       YDOT =        2196
510992  meter/sec
 ZDOT =      -1187
447864                 ZDOT =        -361
934109


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   20154
57277780  
00016717  00000-0  10270-3 0  9147
2 25544  51
6442  60
8122 0001992  11
8381 348
2816 15
49438611 29742


Satellite: ISS
Catalog Number: 25544
Epoch time:      20154
57277780   =   yrday
fracday
Element set:     914
Inclination:       51
6442  deg
RA of node:        60
8122  deg
Eccentricity:     
0001992     
Arg of perigee:    11
8381  deg
Mean anomaly:     348
2816  deg
Mean motion:   15
49438611  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2974
Checksum:              313


Coasting Arc #16 (Orbit 2988)
---------------------------------------

Vector Time (GMT): 2020/155/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3752394
57                 A    =         6791188
27  meter
 Y    =       -1919509
07  meter          E    =           
0015191
 Z    =       -5337974
30                 I    =           51
94733
 XDOT =       4016
604694                 Wp   =           86
23405
 YDOT =       6491
779008  meter/sec      RA   =           55
36649  deg
 ZDOT =        491
284382                 TA   =          188
43132
                                          MA   =          188
45688
                                          Ha   =            228
725  n
mi
                                          Hp   =            221
999

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12311005
82                 X    =         3799509
39
 Y    =       -6297601
92  feet           Y    =        -1877282
97  meter
 Z    =      -17513039
06                 Z    =        -5319632
21
 XDOT =      13177
836924                 XDOT =        3941
326759
 YDOT =      21298
487560  feet/sec       YDOT =        6536
274570  meter/sec
 ZDOT =       1611
825401                 ZDOT =         510
613784

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4166824
87                 X    =        -1270048
22
 Y    =      -13297087
17  feet           Y    =        -4052952
17  meter
 Z    =      -17428489
16                 Z    =        -5312203
50
 XDOT =      22205
553547                 XDOT =        6768
252721
 YDOT =      -9177
622875  feet/sec       YDOT =       -2797
339452  meter/sec
 ZDOT =       1700
315434                 ZDOT =         518
256144


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   20155
54025489  
00016717  00000-0  10270-3 0  9153
2 25544  51
6447  56
0243 0002015  14
4665 345
6543 15
49420655 29892


Satellite: ISS
Catalog Number: 25544
Epoch time:      20155
54025489   =   yrday
fracday
Element set:     915
Inclination:       51
6447  deg
RA of node:        56
0243  deg
Eccentricity:     
0002015     
Arg of perigee:    14
4665  deg
Mean anomaly:     345
6543  deg
Mean motion:   15
49420655  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2989
Checksum:              309


Coasting Arc #17 (Orbit 3004)
---------------------------------------

Vector Time (GMT): 2020/156/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3678593
73                 A    =         6791176
54  meter
 Y    =        2081611
56  meter          E    =           
0004591
 Z    =        5313080
65                 I    =           51
92828
 XDOT =      -4457
416702                 Wp   =           44
26782
 YDOT =      -6199
282112  meter/sec      RA   =           50
43719  deg
 ZDOT =       -653
804781                 TA   =           51
97444
                                          MA   =           51
93300
                                          Ha   =            228
823  n
mi
                                          Hp   =            221
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12068877
07                 X    =        -3727405
78
 Y    =        6829434
25  feet           Y    =         2040201
12  meter
 Z    =       17431366
95                 Z    =         5295093
02
 XDOT =     -14624
070546                 XDOT =       -4384
587352
 YDOT =     -20338
852072  feet/sec       YDOT =       -6248
720797  meter/sec
 ZDOT =      -2145
028810                 ZDOT =        -675
281574

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4956761
22                 X    =         1510820
82
 Y    =       13061927
54  feet           Y    =         3981275
52  meter
 Z    =       17348431
82                 Z    =         5287802
02
 XDOT =     -21320
005069                 XDOT =       -6498
337545
 YDOT =      11085
667381  feet/sec       YDOT =        3378
911418  meter/sec
 ZDOT =      -2243
403768                 ZDOT =        -683
789468


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   20156
57222618  
00016717  00000-0  10270-3 0  9161
2 25544  51
6455  50
9168 0001989  14
8900 345
2308 15
49443206 30057


Satellite: ISS
Catalog Number: 25544
Epoch time:      20156
57222618   =   yrday
fracday
Element set:     916
Inclination:       51
6455  deg
RA of node:        50
9168  deg
Eccentricity:     
0001989     
Arg of perigee:    14
8900  deg
Mean anomaly:     345
2308  deg
Mean motion:   15
49443206  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3005
Checksum:              302


Coasting Arc #18 (Orbit 3019)
---------------------------------------

Vector Time (GMT): 2020/157/12:36:00
000
Vector Time (MET): N/A
Weight (LBS)     : 981788
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3604775
91                 A    =         6791313
24  meter
 Y    =       -2264426
54  meter          E    =           
0015103
 Z    =       -5304471
57                 I    =           51
90583
 XDOT =       4860
875725                 Wp   =           88
23873
 YDOT =       5851
262488  meter/sec      RA   =           45
50628  deg
 ZDOT =        807
912205                 TA   =          189
45926
                                          MA   =          189
48774
                                          Ha   =            228
798  n
mi
                                          Hp   =            221
898

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11826692
62                 X    =         3655595
83
 Y    =       -7429220
93  feet           Y    =        -2223830
23  meter
 Z    =      -17403121
94                 Z    =        -5286837
79
 XDOT =      15947
755004                 XDOT =        4791
159485
 YDOT =      19197
055406  feet/sec       YDOT =        5905
230300  meter/sec
 ZDOT =       2650
630594                 ZDOT =         831
356444

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5807008
83                 X    =        -1769976
29
 Y    =      -12812754
26  feet           Y    =        -3905327
50  meter
 Z    =      -17321795
87                 Z    =        -5279683
38
 XDOT =      20178
351626                 XDOT =        6150
361576
 YDOT =     -12863
072417  feet/sec       YDOT =       -3920
664473  meter/sec
 ZDOT =       2758
070636                 ZDOT =         840
659930


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   20157
53969913  
00016717  00000-0  10270-3 0  9175
2 25544  51
6451  46
1284 0002132  19
7903 340
3330 15
49427301 30203


Satellite: ISS
Catalog Number: 25544
Epoch time:      20157
53969913   =   yrday
fracday
Element set:     917
Inclination:       51
6451  deg
RA of node:        46
1284  deg
Eccentricity:     
0002132     
Arg of perigee:    19
7903  deg
Mean anomaly:     340
3330  deg
Mean motion:   15
49427301  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3020
Checksum:              282
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