[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: August 23rd 2020

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 213)
---------------------------------------

Vector Time (GMT): 2020/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1448012
37                 A    =         6794446
49  meter
 Y    =        4709718
59  meter          E    =           
0008676
 Z    =        4672447
78                 I    =           51
79596
 XDOT =      -7055
235918                 Wp   =          108
22739
 YDOT =       -720
078642  meter/sec      RA   =           24
63634  deg
 ZDOT =       2905
196035                 TA   =          312
89393
                                          MA   =          312
96674
                                          Ha   =            229
116  n
mi
                                          Hp   =            222
070

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4750696
74                 X    =         1372543
53
 Y    =       15451832
64  feet           Y    =         4725489
51  meter
 Z    =       15329553
09                 Z    =         4679298
07
 XDOT =     -23147
099468                 XDOT =       -7060
770988
 YDOT =      -2362
462737  feet/sec       YDOT =        -799
006177  meter/sec
 ZDOT =       9531
483055                 ZDOT =        2870
911578

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3876588
85                 X    =         1181584
28
 Y    =      -15663273
92  feet           Y    =        -4774165
89  meter
 Z    =       15360903
57                 Z    =         4682003
41
 XDOT =      17626
337182                 XDOT =        5372
507573
 YDOT =      13577
456146  feet/sec       YDOT =        4138
408633  meter/sec
 ZDOT =       9373
244126                 ZDOT =        2856
964809


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   20234
55348663  
00016717  00000-0  10270-3 0  9008
2 25544  51
6420  24
9750 0001230  52
3978 307
7283 15
49198389  2141


Satellite: ISS
Catalog Number: 25544
Epoch time:      20234
55348663   =   yrday
fracday
Element set:     900
Inclination:       51
6420  deg
RA of node:        24
9750  deg
Eccentricity:     
0001230     
Arg of perigee:    52
3978  deg
Mean anomaly:     307
7283  deg
Mean motion:   15
49198389  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             214
Checksum:              303


Coasting Arc #2 (Orbit 228)
---------------------------------------

Vector Time (GMT): 2020/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1763055
63                 A    =         6794349
09  meter
 Y    =       -4576455
43  meter          E    =           
0012249
 Z    =       -4714151
62                 I    =           51
76515
 XDOT =       7105
344878                 Wp   =           68
75480
 YDOT =        175
865620  meter/sec      RA   =           19
69936  deg
 ZDOT =      -2829
684199                 TA   =          173
16034
                                          MA   =          173
14361
                                          Ha   =            229
251  n
mi
                                          Hp   =            221
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5784303
24                 X    =        -1688850
87
 Y    =      -15014617
57  feet           Y    =        -4595756
47  meter
 Z    =      -15466376
70                 Z    =        -4722535
35
 XDOT =      23311
498942                 XDOT =        7116
595065
 YDOT =        576
986943  feet/sec       YDOT =         255
385461  meter/sec
 ZDOT =      -9283
740810                 ZDOT =       -2795
142242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2492860
29                 X    =         -759823
82
 Y    =       15858508
48  feet           Y    =         4833673
38  meter
 Z    =      -15504807
93                 Z    =        -4725865
46
 XDOT =     -18872
381097                 XDOT =       -5752
301758
 YDOT =     -11882
256821  feet/sec       YDOT =       -3621
711879  meter/sec
 ZDOT =      -9124
297253                 ZDOT =       -2781
085803


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   20235
52110466  
00016717  00000-0  10270-3 0  9015
2 25544  51
6429  20
1884 0001461  57
3158 302
8133 15
49185219  2291


Satellite: ISS
Catalog Number: 25544
Epoch time:      20235
52110466   =   yrday
fracday
Element set:     901
Inclination:       51
6429  deg
RA of node:        20
1884  deg
Eccentricity:     
0001461     
Arg of perigee:    57
3158  deg
Mean anomaly:     302
8133  deg
Mean motion:   15
49185219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             229
Checksum:              280


Coasting Arc #3 (Orbit 244)
---------------------------------------

Vector Time (GMT): 2020/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922462
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2077650
89                 A    =         6794179
56  meter
 Y    =        4406183
07  meter          E    =           
0008493
 Z    =        4730372
44                 I    =           51
73229
 XDOT =      -7134
974765                 Wp   =          109
66095
 YDOT =        381
335361  meter/sec      RA   =           14
75934  deg
 ZDOT =       2771
744134                 TA   =          312
87494
                                          MA   =          312
94623
                                          Ha   =            229
134  n
mi
                                          Hp   =            222
004

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6816439
94                 X    =         2005247
90
 Y    =       14455981
19  feet           Y    =         4429012
16  meter
 Z    =       15519594
61                 Z    =         4740288
81
 XDOT =     -23408
709860                 XDOT =       -7152
172161
 YDOT =       1251
100265  feet/sec       YDOT =         301
450893  meter/sec
 ZDOT =       9093
648732                 ZDOT =        2737
043631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1046438
37                 X    =          318954
42
 Y    =      -15903760
51  feet           Y    =        -4847466
20  meter
 Z    =       15565102
98                 Z    =         4744243
39
 XDOT =      20034
655240                 XDOT =        6106
562917
 YDOT =      10083
377864  feet/sec       YDOT =        3073
413573  meter/sec
 ZDOT =       8933
455418                 ZDOT =        2722
917211


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   20236
55322812  
00016717  00000-0  10270-3 0  9020
2 25544  51
6426  15
0815 0001291  60
7115 299
4164 15
49204779  2453


Satellite: ISS
Catalog Number: 25544
Epoch time:      20236
55322812   =   yrday
fracday
Element set:     902
Inclination:       51
6426  deg
RA of node:        15
0815  deg
Eccentricity:     
0001291     
Arg of perigee:    60
7115  deg
Mean anomaly:     299
4164  deg
Mean motion:   15
49204779  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             245
Checksum:              287


Coasting Arc #4 (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    =       -2364837
57                 A    =         6794123
83  meter
 Y    =       -4233244
50  meter          E    =           
0012544
 Z    =       -4770993
44                 I    =           51
69926
 XDOT =       7099
039552                 Wp   =           70
10008
 YDOT =       -931
023116  meter/sec      RA   =            9
81785  deg
 ZDOT =      -2694
306424                 TA   =          173
24223
                                          MA   =          173
22530
                                          Ha   =            229
246  n
mi
                                          Hp   =            221
948

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7758653
45                 X    =        -2294149
72
 Y    =      -13888597
43  feet           Y    =        -4259294
61  meter
 Z    =      -15652865
62                 Z    =        -4782309
13
 XDOT =      23290
812179                 XDOT =        7122
010276
 YDOT =      -3054
537781  feet/sec       YDOT =        -851
508166  meter/sec
 ZDOT =      -8839
588006                 ZDOT =       -2659
766377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         324399
14                 X    =           98876
86
 Y    =       15854178
10  feet           Y    =         4832353
49  meter
 Z    =      -15704835
11                 Z    =        -4786833
74
 XDOT =     -20941
644975                 XDOT =       -6383
013388
 YDOT =      -8164
632297  feet/sec       YDOT =       -2488
579924  meter/sec
 ZDOT =      -8680
114995                 ZDOT =       -2645
699050


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
52084486  
00016717  00000-0  10270-3 0  9031
2 25544  51
6430  10
2947 0001353  63
6269 296
5020 15
49179055  2606


Satellite: ISS
Catalog Number: 25544
Epoch time:      20237
52084486   =   yrday
fracday
Element set:     903
Inclination:       51
6430  deg
RA of node:        10
2947  deg
Eccentricity:     
0001353     
Arg of perigee:    63
6269  deg
Mean anomaly:     296
5020  deg
Mean motion:   15
49179055  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             260
Checksum:              291


Coasting Arc #5 (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    =        2645475
44                 A    =         6793914
88  meter
 Y    =        4024177
59  meter          E    =           
0008209
 Z    =        4786765
27                 I    =           51
66647
 XDOT =      -7041
636211                 Wp   =          111
08065
 YDOT =       1489
251588  meter/sec      RA   =            4
87291  deg
 ZDOT =       2633
133416                 TA   =          312
90845
                                          MA   =          312
97732
                                          Ha   =            229
119  n
mi
                                          Hp   =            221
971

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8679381
35                 X    =         2577027
97
 Y    =       13202682
38  feet           Y    =         4053378
42  meter
 Z    =       15704610
45                 Z    =         4799449
71
 XDOT =     -23102
481006                 XDOT =       -7070
556334
 YDOT =       4885
996024  feet/sec       YDOT =        1410
345243  meter/sec
 ZDOT =       8638
889161                 ZDOT =        2598
857791

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1727442
93                 X    =         -526524
60
 Y    =      -15646856
10  feet           Y    =        -4769161
74  meter
 Z    =       15762902
89                 Z    =         4804532
80
 XDOT =      21746
731702                 XDOT =        6628
403823
 YDOT =       6164
141341  feet/sec       YDOT =        1878
830281  meter/sec
 ZDOT =       8480
612438                 ZDOT =        2584
890671


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
55296518  
00016717  00000-0  10270-3 0  9047
2 25544  51
6440   5
1874 0001301  65
6362 294
4924 15
49212021  2766


Satellite: ISS
Catalog Number: 25544
Epoch time:      20238
55296518   =   yrday
fracday
Element set:     904
Inclination:       51
6440  deg
RA of node:         5
1874  deg
Eccentricity:     
0001301     
Arg of perigee:    65
6362  deg
Mean anomaly:     294
4924  deg
Mean motion:   15
49212021  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             276
Checksum:              287


Coasting Arc #6 (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    =       -4102019
18                 A    =         6796452
32  meter
 Y    =       -3505793
96  meter          E    =           
0009437
 Z    =       -4142234
84                 I    =           51
66092
 XDOT =       6093
602460                 Wp   =           67
71826
 YDOT =      -2662
989965  meter/sec      RA   =            3
13878  deg
 ZDOT =      -3784
040311                 TA   =          163
20785
                                          MA   =          163
17659
                                          Ha   =            229
371  n
mi
                                          Hp   =            221
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13458068
18                 X    =        -4042390
94
 Y    =      -11501948
68  feet           Y    =        -3551332
19  meter
 Z    =      -13590009
33                 Z    =        -4162016
00
 XDOT =      19992
134056                 XDOT =        6141
308556
 YDOT =      -8736
843716  feet/sec       YDOT =       -2594
580134  meter/sec
 ZDOT =     -12414
830417                 ZDOT =       -3754
324269

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8866420
46                 X    =         2702484
96
 Y    =      -15241959
53  feet           Y    =        -4645749
26  meter
 Z    =      -13681083
07                 Z    =        -4169994
12
 XDOT =      11147
864920                 XDOT =        3397
869228
 YDOT =      17495
036246  feet/sec       YDOT =        5332
487048  meter/sec
 ZDOT =     -12277
526704                 ZDOT =       -3742
190139


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
87550298  
00016717  00000-0  10270-3 0  9051
2 25544  51
6422   3
5956 0001786  58
1496 301
9828 15
49175154  2819


Satellite: ISS
Catalog Number: 25544
Epoch time:      20238
87550298   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:         3
5956  deg
Eccentricity:     
0001786     
Arg of perigee:    58
1496  deg
Mean anomaly:     301
9828  deg
Mean motion:   15
49175154  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             281
Checksum:              324


Coasting Arc #7 (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    =        4324854
79                 A    =         6796277
16  meter
 Y    =        3166747
95  meter          E    =           
0011372
 Z    =        4169462
56                 I    =           51
62574
 XDOT =      -5910
044419                 Wp   =           98
08578
 YDOT =       3143
589868  meter/sec      RA   =          358
19193  deg
 ZDOT =       3732
423508                 TA   =          313
46469
                                          MA   =          313
55922
                                          Ha   =            229
220  n
mi
                                          Hp   =            221
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14189156
14                 X    =         4268869
11
 Y    =       10389593
00  feet           Y    =         3214798
40  meter
 Z    =       13679339
10                 Z    =         4190334
99
 XDOT =     -19389
909510                 XDOT =       -5962
887591
 YDOT =      10313
615053  feet/sec       YDOT =        3077
203940  meter/sec
 ZDOT =      12245
483950                 ZDOT =        3703
586778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7367141
83                 X    =        -2245504
83
 Y    =       15885903
19  feet           Y    =         4842023
29  meter
 Z    =       13775464
20                 Z    =         4198761
49
 XDOT =     -12835
723025                 XDOT =       -3912
328378
 YDOT =     -16484
806099  feet/sec       YDOT =       -5024
568899  meter/sec
 ZDOT =      12112
214587                 ZDOT =        3691
803006


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
90762149  
00016717  00000-0  10270-3 0  9067
2 25544  51
6412 358
4892 0001698  55
9494 304
1817 15
49192508  2976


Satellite: ISS
Catalog Number: 25544
Epoch time:      20239
90762149   =   yrday
fracday
Element set:     906
Inclination:       51
6412  deg
RA of node:       358
4892  deg
Eccentricity:     
0001698     
Arg of perigee:    55
9494  deg
Mean anomaly:     304
1817  deg
Mean motion:   15
49192508  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             297
Checksum:              337


Coasting Arc #8 (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    =       -4512883
10                 A    =         6796156
77  meter
 Y    =       -2838579
31  meter          E    =           
0009904
 Z    =       -4225203
95                 I    =           51
59102
 XDOT =       5680
050727                 Wp   =           67
81101
 YDOT =      -3592
459265  meter/sec      RA   =          353
24175  deg
 ZDOT =      -3656
535195                 TA   =          164
62216
                                          MA   =          164
59205
                                          Ha   =            229
390  n
mi
                                          Hp   =            221
786

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14806046
92                 X    =        -4460282
45
 Y    =       -9312924
24  feet           Y    =        -2888751
33  meter
 Z    =      -13862217
67                 Z    =        -4246997
87
 XDOT =      18635
337031                 XDOT =        5737
561693
 YDOT =     -11786
283677  feet/sec       YDOT =       -3528
619177  meter/sec
 ZDOT =     -11996
506546                 ZDOT =       -3628
804485

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5908400
62                 X    =         1800880
51
 Y    =      -16378245
72  feet           Y    =        -4992089
29  meter
 Z    =      -13962611
91                 Z    =        -4255804
11
 XDOT =      14364
592473                 XDOT =        4378
327786
 YDOT =      15290
846110  feet/sec       YDOT =        4660
649894  meter/sec
 ZDOT =     -11868
319947                 ZDOT =       -3617
463920


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
87523319  
00016717  00000-0  10270-3 0  9070
2 25544  51
6409 353
7013 0001794  60
9314 299
2015 15
49172534  3128


Satellite: ISS
Catalog Number: 25544
Epoch time:      20240
87523319   =   yrday
fracday
Element set:     907
Inclination:       51
6409  deg
RA of node:       353
7013  deg
Eccentricity:     
0001794     
Arg of perigee:    60
9314  deg
Mean anomaly:     299
2015  deg
Mean motion:   15
49172534  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             312
Checksum:              292


Coasting Arc #9 (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    =        4679504
96                 A    =         6795907
80  meter
 Y    =        2477197
68  meter          E    =           
0011056
 Z    =        4252178
45                 I    =           51
55768
 XDOT =      -5423
119620                 Wp   =          100
55179
 YDOT =       4044
149282  meter/sec      RA   =          348
29046  deg
 ZDOT =       3602
149274                 TA   =          312
52686
                                          MA   =          312
62017
                                          Ha   =            229
161  n
mi
                                          Hp   =            221
872

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15352706
57                 X    =         4630802
07
 Y    =        8127288
96  feet           Y    =         2529254
80  meter
 Z    =       13950716
69                 Z    =         4274791
09
 XDOT =     -17792
387206                 XDOT =       -5485
436370
 YDOT =      13268
206306  feet/sec       YDOT =        3983
155534  meter/sec
 ZDOT =      11818
075047                 ZDOT =        3575
655052

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4345513
51                 X    =        -1324512
52
 Y    =       16731914
77  feet           Y    =         5099887
62  meter
 Z    =       14054908
79                 Z    =         4283936
20
 XDOT =     -15851
105412                 XDOT =       -4831
416930
 YDOT =     -13968
369589  feet/sec       YDOT =       -4257
559051  meter/sec
 ZDOT =      11695
575016                 ZDOT =        3564
811265


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
90734876  
00016717  00000-0  10270-3 0  9088
2 25544  51
6413 348
5951 0001596  61
9657 298
1654 15
49214404  3284


Satellite: ISS
Catalog Number: 25544
Epoch time:      20241
90734876   =   yrday
fracday
Element set:     908
Inclination:       51
6413  deg
RA of node:       348
5951  deg
Eccentricity:     
0001596     
Arg of perigee:    61
9657  deg
Mean anomaly:     298
1654  deg
Mean motion:   15
49214404  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             328
Checksum:              326


Coasting Arc #10 (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    =       -4813245
36                 A    =         6795804
72  meter
 Y    =       -2132988
82  meter          E    =           
0010414
 Z    =       -4308052
86                 I    =           51
52505
 XDOT =       5125
069601                 Wp   =           68
10103
 YDOT =      -4456
454407  meter/sec      RA   =          343
33518  deg
 ZDOT =      -3522
676653                 TA   =          165
88967
                                          MA   =          165
86056
                                          Ha   =            229
392  n
mi
                                          Hp   =            221
716

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15791487
41                 X    =        -4768110
24
 Y    =       -6997994
83  feet           Y    =        -2186561
54  meter
 Z    =      -14134031
68                 Z    =        -4331323
70
 XDOT =      16814
532813                 XDOT =        5191
632943
 YDOT =     -14620
913408  feet/sec       YDOT =       -4398
769976  meter/sec
 ZDOT =     -11557
338099                 ZDOT =       -3497
619932

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2854264
88                 X    =          869979
93
 Y    =      -16945588
96  feet           Y    =        -5165015
51  meter
 Z    =      -14241279
61                 Z    =        -4340742
02
 XDOT =      17143
670561                 XDOT =        5225
390787
 YDOT =      12494
767738  feet/sec       YDOT =        3808
405206  meter/sec
 ZDOT =     -11441
457646                 ZDOT =       -3487
356290


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
87495683  
00016717  00000-0  10270-3 0  9096
2 25544  51
6421 343
8068 0001839  63
9276 296
2063 15
49188199  3430


Satellite: ISS
Catalog Number: 25544
Epoch time:      20242
87495683   =   yrday
fracday
Element set:     909
Inclination:       51
6421  deg
RA of node:       343
8068  deg
Eccentricity:     
0001839     
Arg of perigee:    63
9276  deg
Mean anomaly:     296
2063  deg
Mean motion:   15
49188199  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             343
Checksum:              340


Coasting Arc #11 (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    =        4921483
91                 A    =         6795554
51  meter
 Y    =        1759820
96  meter          E    =           
0010794
 Z    =        4335241
48                 I    =           51
49238
 XDOT =      -4800
637568                 Wp   =          102
25947
 YDOT =       4867
655626  meter/sec      RA   =          338
37974  deg
 ZDOT =       3464
308248                 TA   =          312
41131
                                          MA   =          312
50258
                                          Ha   =            229
158  n
mi
                                          Hp   =            221
814

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16146600
75                 X    =         4880381
59
 Y    =        5773690
80  feet           Y    =         1814626
72  meter
 Z    =       14223233
20                 Z    =         4359047
81
 XDOT =     -15750
123254                 XDOT =       -4871
539656
 YDOT =      15969
998772  feet/sec       YDOT =        4813
575038  meter/sec
 ZDOT =      11365
840710                 ZDOT =        3440
816868

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1287857
08                 X    =         -392538
84
 Y    =       17007526
29  feet           Y    =         5183894
01  meter
 Z    =       14332971
00                 Z    =         4368689
56
 XDOT =     -18371
168392                 XDOT =       -5599
532126
 YDOT =     -10904
248316  feet/sec       YDOT =       -3323
614887  meter/sec
 ZDOT =      11257
173173                 ZDOT =        3431
186383


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
90706778  
00016717  00000-0  10270-3 0  9103
2 25544  51
6419 338
7011 0001655  65
4979 294
6343 15
49229140  3593


Satellite: ISS
Catalog Number: 25544
Epoch time:      20243
90706778   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       338
7011  deg
Eccentricity:     
0001655     
Arg of perigee:    65
4979  deg
Mean anomaly:     294
6343  deg
Mean motion:   15
49229140  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             359
Checksum:              320


Coasting Arc #12 (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    =       -5002059
72                 A    =         6795474
54  meter
 Y    =       -1407722
27  meter          E    =           
0010861
 Z    =       -4390215
52                 I    =           51
46061
 XDOT =       4438
894030                 Wp   =           68
54926
 YDOT =      -5233
446820  meter/sec      RA   =          333
42046  deg
 ZDOT =      -3382
306836                 TA   =          167
04809
                                          MA   =          167
02017
                                          Ha   =            229
382  n
mi
                                          Hp   =            221
685

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16410957
10                 X    =        -4964621
65
 Y    =       -4618511
40  feet           Y    =        -1463449
68  meter
 Z    =      -14403594
22                 Z    =        -4414422
12
 XDOT =      14563
300623                 XDOT =        4513
515086
 YDOT =     -17170
101116  feet/sec       YDOT =       -5183
390789  meter/sec
 ZDOT =     -11096
807206                 ZDOT =       -3360
563473

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -187292
26                 X    =          -57086
68
 Y    =      -16952514
14  feet           Y    =        -5167126
31  meter
 Z    =      -14515194
54                 Z    =        -4424231
30
 XDOT =      19375
989984                 XDOT =        5905
801747
 YDOT =       9193
120772  feet/sec       YDOT =        2802
063211  meter/sec
 ZDOT =     -10996
201010                 ZDOT =       -3351
642068


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
87467417  
00016717  00000-0  10270-3 0  9115
2 25544  51
6417 333
9131 0001818  66
6939 293
4402 15
49196145  3749


Satellite: ISS
Catalog Number: 25544
Epoch time:      20244
87467417   =   yrday
fracday
Element set:     911
Inclination:       51
6417  deg
RA of node:       333
9131  deg
Eccentricity:     
0001818     
Arg of perigee:    66
6939  deg
Mean anomaly:     293
4402  deg
Mean motion:   15
49196145  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             374
Checksum:              318


Coasting Arc #13 (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    =        5053479
30                 A    =         6795220
76  meter
 Y    =        1031028
18  meter          E    =           
0010453
 Z    =        4417034
11                 I    =           51
43132
 XDOT =      -4052
043689                 Wp   =          104
67127
 YDOT =       5594
001822  meter/sec      RA   =          328
46064  deg
 ZDOT =       3320
940961                 TA   =          311
62873
                                          MA   =          311
71822
                                          Ha   =            229
127  n
mi
                                          Hp   =            221
802

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16579656
51                 X    =         5020119
41
 Y    =        3382638
38  feet           Y    =         1087353
49  meter
 Z    =       14491581
71                 Z    =         4441500
42
 XDOT =     -13294
106590                 XDOT =       -4130
427288
 YDOT =      18353
024349  feet/sec       YDOT =        5548
250857  meter/sec
 ZDOT =      10895
475594                 ZDOT =        3301
067425

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1708348
74                 X    =          520704
70
 Y    =       16736976
66  feet           Y    =         5101430
49  meter
 Z    =       14604394
88                 Z    =         4451419
56
 XDOT =     -20294
590483                 XDOT =       -6185
791179
 YDOT =      -7381
600144  feet/sec       YDOT =       -2249
911724  meter/sec
 ZDOT =      10803
494927                 ZDOT =        3292
905254


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
90678261  
00016717  00000-0  10270-3 0  9122
2 25544  51
6425 328
8074 0001587  71
3532 288
7791 15
49237825  3909


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
90678261   =   yrday
fracday
Element set:     912
Inclination:       51
6425  deg
RA of node:       328
8074  deg
Eccentricity:     
0001587     
Arg of perigee:    71
3532  deg
Mean anomaly:     288
7791  deg
Mean motion:   15
49237825  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             390
Checksum:              325


Coasting Arc #14 (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    =        -432772
44                 A    =         6792854
36  meter
 Y    =       -4508241
92  meter          E    =           
0014533
 Z    =       -5075840
45                 I    =           51
42129
 XDOT =       6940
913803                 Wp   =           99
10498
 YDOT =      -2673
633651  meter/sec      RA   =          327
89710  deg
 ZDOT =       1785
008683                 TA   =          188
25094
                                          MA   =          188
27486
                                          Ha   =            229
364  n
mi
                                          Hp   =            221
797

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1419857
09                 X    =         -357672
66
 Y    =      -14790819
95  feet           Y    =        -4512661
84  meter
 Z    =      -16653019
84                 Z    =        -5077760
02
 XDOT =      22772
026914                 XDOT =        6961
624918
 YDOT =      -8771
763946  feet/sec       YDOT =       -2595
899489  meter/sec
 ZDOT =       5856
327701                 ZDOT =        1818
774769

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7265874
76                 X    =         2214638
63
 Y    =      -12950073
77  feet           Y    =        -3947182
48  meter
 Z    =      -16661634
73                 Z    =        -5078466
27
 XDOT =      22773
046319                 XDOT =        6941
224518
 YDOT =       5050
886555  feet/sec       YDOT =        1539
510222  meter/sec
 ZDOT =       6012
239178                 ZDOT =        1832
530502


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
97129131  
00016717  00000-0  10270-3 0  9137
2 25544  51
6440 328
4884 0001758  66
7134 293
4201 15
49200699  3916


Satellite: ISS
Catalog Number: 25544
Epoch time:      20245
97129131   =   yrday
fracday
Element set:     913
Inclination:       51
6440  deg
RA of node:       328
4884  deg
Eccentricity:     
0001758     
Arg of perigee:    66
7134  deg
Mean anomaly:     293
4201  deg
Mean motion:   15
49200699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             391
Checksum:              307


Coasting Arc #15 (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    =         724783
07                 A    =         6792883
27  meter
 Y    =        4493731
88  meter          E    =           
0007458
 Z    =        5037869
28                 I    =           51
39356
 XDOT =      -6710
421651                 Wp   =           58
21616
 YDOT =       3191
763337  meter/sec      RA   =          322
93445  deg
 ZDOT =      -1875
710351                 TA   =           50
06845
                                          MA   =           50
00294
                                          Ha   =            229
306  n
mi
                                          Hp   =            221
784

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2377897
22                 X    =          650008
20
 Y    =       14743214
84  feet           Y    =         4501419
16  meter
 Z    =       16528442
51                 Z    =         5041208
04
 XDOT =     -22015
819065                 XDOT =       -6736
503177
 YDOT =      10471
664493  feet/sec       YDOT =        3116
576643  meter/sec
 ZDOT =      -6153
905350                 ZDOT =       -1908
370046

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6214943
28                 X    =        -1894314
71
 Y    =       13560587
06  feet           Y    =         4133266
94  meter
 Z    =       16543613
55                 Z    =         5042493
41
 XDOT =     -23122
343375                 XDOT =       -7047
690261
 YDOT =      -2881
955457  feet/sec       YDOT =        -878
420023  meter/sec
 ZDOT =      -6304
721196                 ZDOT =       -1921
679021


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
00339791  
00016717  00000-0  10270-3 0  9149
2 25544  51
6439 323
3825 0001776  67
1807 292
9530 15
49225908  4072


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
00339791   =   yrday
fracday
Element set:     914
Inclination:       51
6439  deg
RA of node:       323
3825  deg
Eccentricity:     
0001776     
Arg of perigee:    67
1807  deg
Mean anomaly:     292
9530  deg
Mean motion:   15
49225908  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             407
Checksum:              315


Coasting Arc #16 (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    =       -1039110
99                 A    =         6793043
43  meter
 Y    =       -4468136
91  meter          E    =           
0014336
 Z    =       -5023178
06                 I    =           51
36784
 XDOT =       6414
345530                 Wp   =          100
34255
 YDOT =      -3682
577182  meter/sec      RA   =          317
96886  deg
 ZDOT =       1951
024788                 TA   =          188
70205
                                          MA   =          188
72694
                                          Ha   =            229
397  n
mi
                                          Hp   =            221
722

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3409156
81                 X    =         -964670
22
 Y    =      -14659241
83  feet           Y    =        -4479341
13  meter
 Z    =      -16480242
98                 Z    =        -5028044
48
 XDOT =      21044
440716                 XDOT =        6445
571618
 YDOT =     -12081
946136  feet/sec       YDOT =       -3610
672637  meter/sec
 ZDOT =       6400
999959                 ZDOT =        1982
258972

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5064535
04                 X    =         1543670
28
 Y    =      -14146841
16  feet           Y    =        -4311957
19  meter
 Z    =      -16502469
51                 Z    =        -5029952
71
 XDOT =      23173
666531                 XDOT =        7063
333559
 YDOT =        669
604659  feet/sec       YDOT =         204
095500  meter/sec
 ZDOT =       6545
245741                 ZDOT =        1994
990902


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
97099783  
00016717  00000-0  10270-3 0  9150
2 25544  51
6441 318
5947 0001840  71
2003 288
9346 15
49206377  4228


Satellite: ISS
Catalog Number: 25544
Epoch time:      20247
97099783   =   yrday
fracday
Element set:     915
Inclination:       51
6441  deg
RA of node:       318
5947  deg
Eccentricity:     
0001840     
Arg of perigee:    71
2003  deg
Mean anomaly:     288
9346  deg
Mean motion:   15
49206377  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             422
Checksum:              322


Coasting Arc #17 (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    =        1331811
64                 A    =         6793051
91  meter
 Y    =        4415767
76  meter          E    =           
0007772
 Z    =        4982636
35                 I    =           51
34328
 XDOT =      -6108
092559                 Wp   =           60
02480
 YDOT =       4153
990603  meter/sec      RA   =          313
00240  deg
 ZDOT =      -2042
549125                 TA   =           49
96468
                                          MA   =           49
89652
                                          Ha   =            229
254  n
mi
                                          Hp   =            221
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4369460
75                 X    =         1258131
53
 Y    =       14487427
03  feet           Y    =         4430249
43  meter
 Z    =       16347232
12                 Z    =         4988926
46
 XDOT =     -20039
673750                 XDOT =       -6144
168280
 YDOT =      13628
578095  feet/sec       YDOT =        4085
483673  meter/sec
 ZDOT =      -6701
276657                 ZDOT =       -2072
307621

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3910398
86                 X    =        -1191889
57
 Y    =       14585746
93  feet           Y    =         4445735
66  meter
 Z    =       16376034
15                 Z    =         4991415
21
 XDOT =     -23101
898511                 XDOT =       -7041
458666
 YDOT =       1507
404238  feet/sec       YDOT =         459
456812  meter/sec
 ZDOT =      -6838
720253                 ZDOT =       -2084
441933


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
00310255  
00016717  00000-0  10270-3 0  9167
2 25544  51
6433 313
4887 0001714  72
8123 287
3215 15
49242260  4382


Satellite: ISS
Catalog Number: 25544
Epoch time:      20249
00310255   =   yrday
fracday
Element set:     916
Inclination:       51
6433  deg
RA of node:       313
4887  deg
Eccentricity:     
0001714     
Arg of perigee:    72
8123  deg
Mean anomaly:     287
3215  deg
Mean motion:   15
49242260  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             438
Checksum:              283


Coasting Arc #18 (Orbit 444)
---------------------------------------

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

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4041651
80                 A    =         6792089
44  meter
 Y    =        1667994
04  meter          E    =           
0005277
 Z    =        5193829
14                 I    =           51
32852
 XDOT =      -4150
233943                 Wp   =          114
33027
 YDOT =       6331
533266  meter/sec      RA   =          310
49039  deg
 ZDOT =       1193
101854                 TA   =          324
15037
                                          MA   =          324
18577
                                          Ha   =            229
121  n
mi
                                          Hp   =            221
824

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13260012
47                 X    =         3997470
83
 Y    =        5472421
39  feet           Y    =         1712944
03  meter
 Z    =       17040121
85                 Z    =         5213354
42
 XDOT =     -13616
253095                 XDOT =       -4226
521988
 YDOT =      20772
746937  feet/sec       YDOT =        6284
695909  meter/sec
 ZDOT =       3914
376163                 ZDOT =        1172
755958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9201053
04                 X    =        -2804480
97
 Y    =      -10864695
78  feet           Y    =        -3311559
27  meter
 Z    =       17130093
05                 Z    =         5221252
36
 XDOT =      20822
329077                 XDOT =        6346
645903
 YDOT =     -11594
718765  feet/sec       YDOT =       -3534
070280  meter/sec
 ZDOT =       3820
250574                 ZDOT =        1164
412375


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
51915349  
00016717  00000-0  10270-3 0  9179
2 25544  51
6434 310
9326 0001508  90
5419 269
5904 15
49231831  4456


Satellite: ISS
Catalog Number: 25544
Epoch time:      20249
51915349   =   yrday
fracday
Element set:     917
Inclination:       51
6434  deg
RA of node:       310
9326  deg
Eccentricity:     
0001508     
Arg of perigee:    90
5419  deg
Mean anomaly:     269
5904  deg
Mean motion:   15
49231831  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             445
Checksum:              309
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