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

 
Date: May 2nd 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19912 1579 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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


130/00:47:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 7

132/16:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 0
000/00:00:00 000 0 0 0 0 222 6

132/22:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 8

Coasting Arc #1 (Orbit 2445)
---------------------------------------

Vector Time (GMT): 2020/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2863180
87                 A    =         6791415
79  meter
 Y    =        3160286
12  meter          E    =           
0013816
 Z    =       -5297621
18                 I    =           51
32936
 XDOT =      -5314
669120                 Wp   =           92
79248
 YDOT =      -5488
408528  meter/sec      RA   =          228
34256  deg
 ZDOT =       -403
279869                 TA   =          173
34543
                                          MA   =          173
32707
                                          Ha   =            228
299  n
mi
                                          Hp   =            222
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9393638
02                 X    =        -2872574
38
 Y    =       10368392
78  feet           Y    =         3128215
83  meter
 Z    =      -17380646
92                 Z    =        -5311552
07
 XDOT =     -17436
578478                 XDOT =       -5250
942201
 YDOT =     -18006
589659  feet/sec       YDOT =       -5547
484592  meter/sec
 ZDOT =      -1323
096683                 ZDOT =        -428
942173

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1166946
10                 X    =         -355685
17
 Y    =       13861931
86  feet           Y    =         4225116
83  meter
 Z    =      -17444654
58                 Z    =        -5317130
72
 XDOT =     -23744
198101                 XDOT =       -7237
231581
 YDOT =      -3805
336281  feet/sec       YDOT =       -1159
866498  meter/sec
 ZDOT =      -1440
607574                 ZDOT =        -439
097189


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   20120
51689854  
00016717  00000-0  10270-3 0  9008
2 25544  51
6426 229
3601 0001726 211
7181 148
3866 15
49334338 24461


Satellite: ISS
Catalog Number: 25544
Epoch time:      20120
51689854   =   yrday
fracday
Element set:     900
Inclination:       51
6426  deg
RA of node:       229
3601  deg
Eccentricity:     
0001726     
Arg of perigee:   211
7181  deg
Mean anomaly:     148
3866  deg
Mean motion:   15
49334338  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2446
Checksum:              303


Coasting Arc #2 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2020/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2685973
23                 A    =         6791262
67  meter
 Y    =       -3290420
13  meter          E    =           
0002430
 Z    =        5297908
27                 I    =           51
35301
 XDOT =       5712
001726                 Wp   =          144
75311
 YDOT =       5099
897449  meter/sec      RA   =          223
37250  deg
 ZDOT =        269
516937                 TA   =          302
65381
                                          MA   =          302
67725
                                          Ha   =            228
084  n
mi
                                          Hp   =            222
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8812248
13                 X    =         2696833
79
 Y    =      -10795341
64  feet           Y    =        -3260323
25  meter
 Z    =       17381588
82                 Z    =         5310981
90
 XDOT =      18740
163142                 XDOT =        5653
239473
 YDOT =      16731
947012  feet/sec       YDOT =        5163
444540  meter/sec
 ZDOT =        884
241920                 ZDOT =         297
121236

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         207328
15                 X    =           63193
62
 Y    =      -13858568
02  feet           Y    =        -4224091
53  meter
 Z    =       17441670
10                 Z    =         5316221
05
 XDOT =      24052
783276                 XDOT =        7331
288343
 YDOT =       1640
120506  feet/sec       YDOT =         499
908730  meter/sec
 ZDOT =       1010
701101                 ZDOT =         308
061696


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   20121
54891821  
00016717  00000-0  10270-3 0  9012
2 25544  51
6431 224
2519 0001723 218
1696 141
9333 15
49372023 24627


Satellite: ISS
Catalog Number: 25544
Epoch time:      20121
54891821   =   yrday
fracday
Element set:     901
Inclination:       51
6431  deg
RA of node:       224
2519  deg
Eccentricity:     
0001723     
Arg of perigee:   218
1696  deg
Mean anomaly:     141
9333  deg
Mean motion:   15
49372023  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2462
Checksum:              283


Coasting Arc #3 (Orbit 2476)
---------------------------------------

Vector Time (GMT): 2020/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2522441
55                 A    =         6791346
27  meter
 Y    =        3415955
02  meter          E    =           
0013765
 Z    =       -5312016
02                 I    =           51
37807
 XDOT =      -6057
658431                 Wp   =           93
72043
 YDOT =      -4671
181206  meter/sec      RA   =          218
40555  deg
 ZDOT =       -128
508325                 TA   =          175
05445
                                          MA   =          175
04084
                                          Ha   =            228
198  n
mi
                                          Hp   =            222
487

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8275726
86                 X    =        -2534649
54
 Y    =       11207201
49  feet           Y    =         3387679
24  meter
 Z    =      -17427874
09                 Z    =        -5324298
58
 XDOT =     -19874
207452                 XDOT =       -6004
349462
 YDOT =     -15325
397656  feet/sec       YDOT =       -4738
624178  meter/sec
 ZDOT =       -421
615240                 ZDOT =        -157
804800

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         707482
04                 X    =          215640
53
 Y    =       13842596
38  feet           Y    =         4219223
38  meter
 Z    =      -17484330
42                 Z    =        -5329223
91
 XDOT =     -24078
001222                 XDOT =       -7338
974772
 YDOT =        533
291979  feet/sec       YDOT =         162
547395  meter/sec
 ZDOT =       -555
878193                 ZDOT =        -169
431673


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   20122
51643515  
00016717  00000-0  10270-3 0  9026
2 25544  51
6430 219
4646 0001567 223
3538 136
7489 15
49339550 24770


Satellite: ISS
Catalog Number: 25544
Epoch time:      20122
51643515   =   yrday
fracday
Element set:     902
Inclination:       51
6430  deg
RA of node:       219
4646  deg
Eccentricity:     
0001567     
Arg of perigee:   223
3538  deg
Mean anomaly:     136
7489  deg
Mean motion:   15
49339550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2477
Checksum:              310


Coasting Arc #4 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2020/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2342700
13                 A    =         6791216
20  meter
 Y    =       -3529124
42  meter          E    =           
0001694
 Z    =        5307195
66                 I    =           51
40513
 XDOT =       6389
529525                 Wp   =          133
60520
 YDOT =       4228
687326  meter/sec      RA   =          213
43955  deg
 ZDOT =         -9
657616                 TA   =          316
48052
                                          MA   =          316
49388
                                          Ha   =            228
018  n
mi
                                          Hp   =            222
578

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7686024
05                 X    =         2356210
37
 Y    =      -11578492
20  feet           Y    =        -3502851
26  meter
 Z    =       17412059
25                 Z    =         5318608
33
 XDOT =      20963
023376                 XDOT =        6341
815119
 YDOT =      13873
646084  feet/sec       YDOT =        4299
872805  meter/sec
 ZDOT =        -31
685093                 ZDOT =          21
264475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1635862
87                 X    =         -498611
00
 Y    =      -13734281
97  feet           Y    =        -4186209
14  meter
 Z    =       17464527
08                 Z    =         5323187
85
 XDOT =      23976
557537                 XDOT =        7308
054737
 YDOT =      -2711
073504  feet/sec       YDOT =        -826
335204  meter/sec
 ZDOT =        110
075040                 ZDOT =          33
550872


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   20123
54844898  
00016717  00000-0  10270-3 0  9038
2 25544  51
6430 214
3571 0001606 227
4151 132
6863 15
49377219 24934


Satellite: ISS
Catalog Number: 25544
Epoch time:      20123
54844898   =   yrday
fracday
Element set:     903
Inclination:       51
6430  deg
RA of node:       214
3571  deg
Eccentricity:     
0001606     
Arg of perigee:   227
4151  deg
Mean anomaly:     132
6863  deg
Mean motion:   15
49377219  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2493
Checksum:              306


Coasting Arc #5 (Orbit 2507)
---------------------------------------

Vector Time (GMT): 2020/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2172868
40                 A    =         6791343
74  meter
 Y    =        3643005
21  meter          E    =           
0013620
 Z    =       -5315537
35                 I    =           51
43340
 XDOT =      -6665
269973                 Wp   =           95
35178
 YDOT =      -3752
911489  meter/sec      RA   =          208
47619  deg
 ZDOT =        151
642168                 TA   =          176
10613
                                          MA   =          176
09552
                                          Ha   =            228
119  n
mi
                                          Hp   =            222
573

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7128833
34                 X    =        -2187624
11
 Y    =       11952116
84  feet           Y    =         3618624
18  meter
 Z    =      -17439427
01                 Z    =        -5326128
16
 XDOT =     -21867
683638                 XDOT =       -6623
545022
 YDOT =     -12312
701735  feet/sec       YDOT =       -3827
213984  meter/sec
 ZDOT =        497
513673                 ZDOT =         119
366062

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2537714
69                 X    =          773495
44
 Y    =       13621028
95  feet           Y    =         4151689
63  meter
 Z    =      -17488125
98                 Z    =        -5330380
80
 XDOT =     -23595
086876                 XDOT =       -7191
782480
 YDOT =       4848
506420  feet/sec       YDOT =        1477
824757  meter/sec
 ZDOT =        349
504497                 ZDOT =         106
528971


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   20124
51596176  
00016717  00000-0  10270-3 0  9040
2 25544  51
6426 209
5696 0001578 232
9055 127
1951 15
49338516 25086


Satellite: ISS
Catalog Number: 25544
Epoch time:      20124
51596176   =   yrday
fracday
Element set:     904
Inclination:       51
6426  deg
RA of node:       209
5696  deg
Eccentricity:     
0001578     
Arg of perigee:   232
9055  deg
Mean anomaly:     127
1951  deg
Mean motion:   15
49338516  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2508
Checksum:              320


Coasting Arc #6 (Orbit 2523)
---------------------------------------

Vector Time (GMT): 2020/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1990607
77                 A    =         6791221
29  meter
 Y    =       -3741888
60  meter          E    =           
0001149
 Z    =        5305297
12                 I    =           51
46465
 XDOT =       6924
072521                 Wp   =          107
29080
 YDOT =       3267
662694  meter/sec      RA   =          203
51406  deg
 ZDOT =       -293
551454                 TA   =          345
51497
                                          MA   =          345
51826
                                          Ha   =            227
939  n
mi
                                          Hp   =            222
637

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6530865
40                 X    =         2006532
40
 Y    =      -12276537
41  feet           Y    =        -3719539
16  meter
 Z    =       17405830
43                 Z    =         5315005
48
 XDOT =      22716
773364                 XDOT =        6888
443855
 YDOT =      10720
678130  feet/sec       YDOT =        3344
893390  meter/sec
 ZDOT =       -963
095322                 ZDOT =        -260
003244

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3433102
15                 X    =        -1046409
54
 Y    =      -13417263
95  feet           Y    =        -4089582
05  meter
 Z    =       17450482
64                 Z    =         5318907
11
 XDOT =      23089
802114                 XDOT =        7037
771684
 YDOT =      -6959
299778  feet/sec       YDOT =       -2121
194572  meter/sec
 ZDOT =       -809
215640                 ZDOT =        -246
648927


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   20125
54797002  
00016717  00000-0  10270-3 0  9056
2 25544  51
6436 204
4620 0001585 238
7615 121
3380 15
49382172 25249


Satellite: ISS
Catalog Number: 25544
Epoch time:      20125
54797002   =   yrday
fracday
Element set:     905
Inclination:       51
6436  deg
RA of node:       204
4620  deg
Eccentricity:     
0001585     
Arg of perigee:   238
7615  deg
Mean anomaly:     121
3380  deg
Mean motion:   15
49382172  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2524
Checksum:              289


Coasting Arc #7 (Orbit 2538)
---------------------------------------

Vector Time (GMT): 2020/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1814599
51                 A    =         6791382
76  meter
 Y    =        3845025
82  meter          E    =           
0013502
 Z    =       -5307582
74                 I    =           51
49508
 XDOT =      -7123
074181                 Wp   =           96
26058
 YDOT =      -2757
671181  meter/sec      RA   =          198
55463  deg
 ZDOT =        437
047786                 TA   =          177
92842
                                          MA   =          177
92282
                                          Ha   =            228
075  n
mi
                                          Hp   =            222
604

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5953410
48                 X    =        -1831679
29
 Y    =       12614914
11  feet           Y    =         3824638
21  meter
 Z    =      -17413329
21                 Z    =        -5316438
95
 XDOT =     -23369
665948                 XDOT =       -7093
830640
 YDOT =      -9047
477629  feet/sec       YDOT =       -2837
162959  meter/sec
 ZDOT =       1433
883811                 ZDOT =         402
517187

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4316718
36                 X    =         1315735
75
 Y    =       13210767
87  feet           Y    =         4026642
05  meter
 Z    =      -17454075
27                 Z    =        -5320002
14
 XDOT =     -22318
328649                 XDOT =       -6802
626572
 YDOT =       8979
898609  feet/sec       YDOT =        2737
073096  meter/sec
 ZDOT =       1275
464130                 ZDOT =         388
761467


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   20126
51547730  
00016717  00000-0  10270-3 0  9066
2 25544  51
6427 199
6744 0001429 245
8577 114
2424 15
49340988 25399


Satellite: ISS
Catalog Number: 25544
Epoch time:      20126
51547730   =   yrday
fracday
Element set:     906
Inclination:       51
6427  deg
RA of node:       199
6744  deg
Eccentricity:     
0001429     
Arg of perigee:   245
8577  deg
Mean anomaly:     114
2424  deg
Mean motion:   15
49340988  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2539
Checksum:              329


Coasting Arc #8 (Orbit 2554)
---------------------------------------

Vector Time (GMT): 2020/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1628945
25                 A    =         6791296
07  meter
 Y    =       -3931960
16  meter          E    =           
0001344
 Z    =        5291213
85                 I    =           51
52723
 XDOT =       7303
514578                 Wp   =           67
96315
 YDOT =       2242
135359  meter/sec      RA   =          193
59749  deg
 ZDOT =       -581
681061                 TA   =           27
60506
                                          MA   =           27
59793
                                          Ha   =            227
934  n
mi
                                          Hp   =            222
640

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5344308
55                 X    =         1647090
35
 Y    =      -12900131
76  feet           Y    =        -3913642
81  meter
 Z    =       17359625
50                 Z    =         5299170
75
 XDOT =      23961
662002                 XDOT =        7280
725068
 YDOT =       7356
087137  feet/sec       YDOT =        2323
681049  meter/sec
 ZDOT =      -1908
402432                 ZDOT =        -546
258075

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5179692
00                 X    =        -1578770
12
 Y    =      -12917928
95  feet           Y    =        -3937384
74  meter
 Z    =       17396250
54                 Z    =         5302377
17
 XDOT =      21432
267146                 XDOT =        6532
555026
 YDOT =     -10947
477885  feet/sec       YDOT =       -3336
791259  meter/sec
 ZDOT =      -1745
854853                 ZDOT =        -532
136559


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   20127
54748159  
00016717  00000-0  10270-3 0  9079
2 25544  51
6424 194
5675 0001460 248
4593 111
6402 15
49381954 25558


Satellite: ISS
Catalog Number: 25544
Epoch time:      20127
54748159   =   yrday
fracday
Element set:     907
Inclination:       51
6424  deg
RA of node:       194
5675  deg
Eccentricity:     
0001460     
Arg of perigee:   248
4593  deg
Mean anomaly:     111
6402  deg
Mean motion:   15
49381954  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2555
Checksum:              321


Coasting Arc #9 (Orbit 2569)
---------------------------------------

Vector Time (GMT): 2020/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1443696
67                 A    =         6791483
54  meter
 Y    =        4025673
17  meter          E    =           
0013316
 Z    =       -5287423
40                 I    =           51
55917
 XDOT =      -7422
053094                 Wp   =           97
91262
 YDOT =      -1709
770296  meter/sec      RA   =          188
64201  deg
 ZDOT =        724
558303                 TA   =          179
03332
                                          MA   =          179
03075
                                          Ha   =            228
055  n
mi
                                          Hp   =            222
632

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4736537
63                 X    =        -1462921
84
 Y    =       13207589
13  feet           Y    =         4009421
52  meter
 Z    =      -17347189
62                 Z    =        -5294482
92
 XDOT =     -24350
567893                 XDOT =       -7405
901872
 YDOT =      -5609
482597  feet/sec       YDOT =       -1792
678708  meter/sec
 ZDOT =       2377
159787                 ZDOT =         688
543276

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6048630
58                 X    =         1843622
60
 Y    =       12615868
30  feet           Y    =         3845316
66  meter
 Z    =      -17379704
32                 Z    =        -5297333
88
 XDOT =     -20301
260080                 XDOT =       -6187
824072
 YDOT =      12781
433547  feet/sec       YDOT =        3895
780945  meter/sec
 ZDOT =       2211
859360                 ZDOT =         674
174733


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   20128
51498610  
00016717  00000-0  10270-3 0  9082
2 25544  51
6412 189
7793 0001390 253
6313 106
4684 15
49341002 25703


Satellite: ISS
Catalog Number: 25544
Epoch time:      20128
51498610   =   yrday
fracday
Element set:     908
Inclination:       51
6412  deg
RA of node:       189
7793  deg
Eccentricity:     
0001390     
Arg of perigee:   253
6313  deg
Mean anomaly:     106
4684  deg
Mean motion:   15
49341002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2570
Checksum:              299


Coasting Arc #10 (Orbit 2585)
---------------------------------------

Vector Time (GMT): 2020/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1253599
70                 A    =         6791415
53  meter
 Y    =       -4101601
30  meter          E    =           
0002016
 Z    =        5264668
14                 I    =           51
59310
 XDOT =       7520
660057                 Wp   =           48
33950
 YDOT =       1177
511801  meter/sec      RA   =          183
68877  deg
 ZDOT =       -871
883652                 TA   =           50
01902
                                          MA   =           50
00133
                                          Ha   =            227
932  n
mi
                                          Hp   =            222
635

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4112859
90                 X    =         1273798
63
 Y    =      -13456697
17  feet           Y    =        -4087470
17  meter
 Z    =       17272533
28                 Z    =         5270806
46
 XDOT =      24674
081552                 XDOT =        7511
169008
 YDOT =       3863
227693  feet/sec       YDOT =        1261
560180  meter/sec
 ZDOT =      -2860
510668                 ZDOT =        -835
373495

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6877416
77                 X    =        -2096236
63
 Y    =      -12236061
58  feet           Y    =        -3729551
57  meter
 Z    =       17300828
21                 Z    =         5273292
44
 XDOT =      19072
346548                 XDOT =        5813
251228
 YDOT =     -14534
442073  feet/sec       YDOT =       -4430
097944  meter/sec
 ZDOT =      -2692
897818                 ZDOT =        -820
795255


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   20129
54698550  
00016717  00000-0  10270-3 0  9092
2 25544  51
6415 184
6718 0001379 259
9565 100
1430 15
49385552 25867


Satellite: ISS
Catalog Number: 25544
Epoch time:      20129
54698550   =   yrday
fracday
Element set:     909
Inclination:       51
6415  deg
RA of node:       184
6718  deg
Eccentricity:     
0001379     
Arg of perigee:   259
9565  deg
Mean anomaly:     100
1430  deg
Mean motion:   15
49385552  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2586
Checksum:              333


Coasting Arc #11 (Orbit 2593)
---------------------------------------

Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6598833
10                 A    =         6802702
30  meter
 Y    =        1089098
36  meter          E    =           
0008386
 Z    =       -1220534
31                 I    =           51
64853
 XDOT =      -1835
212560                 Wp   =          149
74452
 YDOT =       4593
463963  meter/sec      RA   =          181
06983  deg
 ZDOT =      -5847
898512                 TA   =           43
48934
                                          MA   =           43
42323
                                          Ha   =            228
062  n
mi
                                          Hp   =            222
740

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21649714
90                 X    =         6592092
79
 Y    =        3573157
36  feet           Y    =         1162853
65  meter
 Z    =       -4004377
66                 Z    =        -1188495
49
 XDOT =      -6021
038584                 XDOT =       -1858
035421
 YDOT =      15070
419825  feet/sec       YDOT =        4572
814287  meter/sec
 ZDOT =     -19186
018740                 ZDOT =       -5856
868377

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14437090
12                 X    =        -4400425
07
 Y    =       16559120
28  feet           Y    =         5047219
86  meter
 Z    =       -3857280
61                 Z    =        -1175699
13
 XDOT =      -8513
079796                 XDOT =       -2594
786722
 YDOT =     -11881
430992  feet/sec       YDOT =       -3621
460166  meter/sec
 ZDOT =     -19227
333945                 ZDOT =       -5860
491386


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   20130
06298574  
00016717  00000-0  10270-3 0  9105
2 25544  51
6419 182
1194 0001408 272
3386  87
7603 15
49339007 25940


Satellite: ISS
Catalog Number: 25544
Epoch time:      20130
06298574   =   yrday
fracday
Element set:     910
Inclination:       51
6419  deg
RA of node:       182
1194  deg
Eccentricity:     
0001408     
Arg of perigee:   272
3386  deg
Mean anomaly:      87
7603  deg
Mean motion:   15
49339007  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2594
Checksum:              309


Coasting Arc #12 (Orbit 2609)
---------------------------------------

Vector Time (GMT): 2020/131/00:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6636234
54                 A    =         6802433
37  meter
 Y    =        -606246
54  meter          E    =           
0012690
 Z    =        1333344
84                 I    =           51
68015
 XDOT =       1606
808525                 Wp   =           55
86173
 YDOT =      -4718
474985  meter/sec      RA   =          176
12130  deg
 ZDOT =       5819
167959                 TA   =          318
62005
                                          MA   =          318
71611
                                          Ha   =            227
979  n
mi
                                          Hp   =            222
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21772423
04                 X    =        -6635438
80
 Y    =       -1988997
83  feet           Y    =         -680453
34  meter
 Z    =        4374490
95                 Z    =         1301110
08
 XDOT =       5271
681513                 XDOT =        1631
185967
 YDOT =     -15480
560976  feet/sec       YDOT =       -4700
370895  meter/sec
 ZDOT =      19091
758397                 ZDOT =        5827
031951

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12852494
60                 X    =         3917440
36
 Y    =      -17722334
77  feet           Y    =        -5401767
64  meter
 Z    =        4226454
89                 Z    =         1288223
45
 XDOT =       9384
502142                 XDOT =        2860
396253
 YDOT =      11393
966080  feet/sec       YDOT =        3472
880861  meter/sec
 ZDOT =      19128
008382                 ZDOT =        5830
216955


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   20131
09498159  
00016717  00000-0  10270-3 0  9111
2 25544  51
6403 177
0109 0001369 277
8999  82
1996 15
49392980 26100


Satellite: ISS
Catalog Number: 25544
Epoch time:      20131
09498159   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       177
0109  deg
Eccentricity:     
0001369     
Arg of perigee:   277
8999  deg
Mean anomaly:      82
1996  deg
Mean motion:   15
49392980  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2610
Checksum:              335


Coasting Arc #13 (Orbit 2624)
---------------------------------------

Vector Time (GMT): 2020/132/00:47:30
000
Vector Time (MET): N/A
Weight (LBS)     : 936290
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6635150
26                 A    =         6802379
41  meter
 Y    =         148665
56  meter          E    =           
0007465
 Z    =       -1475419
45                 I    =           51
71266
 XDOT =      -1388
899089                 Wp   =          150
25661
 YDOT =       4831
428362  meter/sec      RA   =          171
17644  deg
 ZDOT =      -5778
110463                 TA   =           45
79345
                                          MA   =           45
73215
                                          Ha   =            228
036  n
mi
                                          Hp   =            222
735

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21768865
69                 X    =         6640161
49
 Y    =         487747
91  feet           Y    =          222892
73  meter
 Z    =       -4840614
99                 Z    =        -1443176
07
 XDOT =      -4556
755541                 XDOT =       -1414
755383
 YDOT =      15851
142919  feet/sec       YDOT =        4815
752842  meter/sec
 ZDOT =     -18957
055326                 ZDOT =       -5784
919445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11242179
45                 X    =        -3426616
30
 Y    =       18685470
64  feet           Y    =         5695331
45  meter
 Z    =       -4692499
66                 Z    =        -1430273
90
 XDOT =     -10200
864682                 XDOT =       -3109
223555
 YDOT =     -10889
935813  feet/sec       YDOT =       -3319
252436  meter/sec
 ZDOT =     -18988
470934                 ZDOT =       -5787
685941


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   20132
06247941  
00016717  00000-0  10270-3 0  9121
2 25544  51
6399 172
2229 0001452 280
4617  79
6369 15
49353685 26254


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
06247941   =   yrday
fracday
Element set:     912
Inclination:       51
6399  deg
RA of node:       172
2229  deg
Eccentricity:     
0001452     
Arg of perigee:   280
4617  deg
Mean anomaly:      79
6369  deg
Mean motion:   15
49353685  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2625
Checksum:              319


Coasting Arc #14 (Orbit 2634)
---------------------------------------

Vector Time (GMT): 2020/132/16:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3880241
44                 A    =         6796644
41  meter
 Y    =       -3977488
80  meter          E    =           
0009966
 Z    =        3907044
05                 I    =           51
71332
 XDOT =       6167
366971                 Wp   =           77
75402
 YDOT =       1989
313728  meter/sec      RA   =          168
00370  deg
 ZDOT =      -4088
991217                 TA   =           55
12569
                                          MA   =           55
03204
                                          Ha   =            227
971  n
mi
                                          Hp   =            222
570

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12730450
90                 X    =         3905452
25
 Y    =      -13049503
95  feet           Y    =        -3933956
69  meter
 Z    =       12818386
00                 Z    =         3925953
58
 XDOT =      20234
143606                 XDOT =        6164
525562
 YDOT =       6526
619841  feet/sec       YDOT =        2058
266214  meter/sec
 ZDOT =     -13415
325514                 ZDOT =       -4059
039101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16453651
48                 X    =        -5015072
97
 Y    =       -7706723
13  feet           Y    =        -2349009
21  meter
 Z    =       12905375
80                 Z    =         3933558
54
 XDOT =      -1007
711591                 XDOT =        -307
150493
 YDOT =     -20142
401236  feet/sec       YDOT =       -6139
403897  meter/sec
 ZDOT =     -13277
772598                 ZDOT =       -4047
065088


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   20132
70747684  
00016717  00000-0  10270-3 0  9132
2 25544  51
6382 169
0298 0001251 286
1320  73
9693 15
49379385 26350


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
70747684   =   yrday
fracday
Element set:     913
Inclination:       51
6382  deg
RA of node:       169
0298  deg
Eccentricity:     
0001251     
Arg of perigee:   286
1320  deg
Mean anomaly:      73
9693  deg
Mean motion:   15
49379385  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2635
Checksum:              326


Coasting Arc #15 (Orbit 2638)
---------------------------------------

Vector Time (GMT): 2020/132/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6422565
80                 A    =         6801273
76  meter
 Y    =         277640
95  meter          E    =           
0005102
 Z    =       -2214746
72                 I    =           51
74131
 XDOT =      -2096
670819                 Wp   =          147
60214
 YDOT =       4929
269464  meter/sec      RA   =          166
71105  deg
 ZDOT =      -5472
268329                 TA   =           56
90598
                                          MA   =           56
85701
                                          Ha   =            228
052  n
mi
                                          Hp   =            222
769

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21071410
10                 X    =         6429741
80
 Y    =         910895
51  feet           Y    =          349503
03  meter
 Z    =       -7266229
41                 Z    =        -2183530
86
 XDOT =      -6878
841271                 XDOT =       -2125
054318
 YDOT =      16172
143912  feet/sec       YDOT =        4905
664937  meter/sec
 ZDOT =     -17953
636251                 ZDOT =       -5482
521529

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19267694
89                 X    =        -5872793
40
 Y    =        8697906
92  feet           Y    =         2651122
03  meter
 Z    =       -7122814
98                 Z    =        -2171034
00
 XDOT =       -615
159928                 XDOT =        -187
500746
 YDOT =     -16076
305000  feet/sec       YDOT =       -4900
057764  meter/sec
 ZDOT =     -18000
885697                 ZDOT =       -5486
669960


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   20132
96547544  
00016717  00000-0  10270-3 0  9144
2 25544  51
6425 167
7548 0001454 282
7243  77
3744 15
49347322 26397


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
96547544   =   yrday
fracday
Element set:     914
Inclination:       51
6425  deg
RA of node:       167
7548  deg
Eccentricity:     
0001454     
Arg of perigee:   282
7243  deg
Mean anomaly:      77
3744  deg
Mean motion:   15
49347322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2639
Checksum:              325


Coasting Arc #16 (Orbit 2654)
---------------------------------------

Vector Time (GMT): 2020/133/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6382879
13                 A    =         6800990
99  meter
 Y    =         176468
73  meter          E    =           
0012801
 Z    =        2322375
60                 I    =           51
77306
 XDOT =       1837
295632                 Wp   =           67
98405
 YDOT =      -5098
255596  meter/sec      RA   =          161
76870  deg
 ZDOT =       5417
813211                 TA   =          317
80767
                                          MA   =          317
90612
                                          Ha   =            228
083  n
mi
                                          Hp   =            222
670

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20941204
49                 X    =        -6395658
84
 Y    =         578965
66  feet           Y    =          105019
14  meter
 Z    =        7619342
52                 Z    =         2291339
04
 XDOT =       6027
872807                 XDOT =        1867
852649
 YDOT =     -16726
560354  feet/sec       YDOT =       -5077
539353  meter/sec
 ZDOT =      17774
977728                 ZDOT =        5426
811767

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18308425
58                 X    =         5580408
12
 Y    =      -10287074
85  feet           Y    =        -3135500
41  meter
 Z    =        7476715
24                 Z    =         2278902
80
 XDOT =       1809
952878                 XDOT =         551
673637
 YDOT =      16217
193224  feet/sec       YDOT =        4943
000495  meter/sec
 ZDOT =      17816
475693                 ZDOT =        5430
461791


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   20133
99746657  
00016717  00000-0  10270-3 0  9155
2 25544  51
6424 162
6462 0001470 296
8297  63
2703 15
49376766 26559


Satellite: ISS
Catalog Number: 25544
Epoch time:      20133
99746657   =   yrday
fracday
Element set:     915
Inclination:       51
6424  deg
RA of node:       162
6462  deg
Eccentricity:     
0001470     
Arg of perigee:   296
8297  deg
Mean anomaly:      63
2703  deg
Mean motion:   15
49376766  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2655
Checksum:              338


Coasting Arc #17 (Orbit 2669)
---------------------------------------

Vector Time (GMT): 2020/134/22:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6312045
48                 A    =         6800786
83  meter
 Y    =        -598815
28  meter          E    =           
0004175
 Z    =       -2456729
96                 I    =           51
80283
 XDOT =      -1579
046240                 Wp   =          139
69579
 YDOT =       5250
463902  meter/sec      RA   =          156
82968  deg
 ZDOT =      -5344
979954                 TA   =           67
67417
                                          MA   =           67
62993
                                          Ha   =            228
082  n
mi
                                          Hp   =            222
737

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20708810
62                 X    =         6330205
86
 Y    =       -1964617
07  feet           Y    =         -528127
74  meter
 Z    =       -8060137
65                 Z    =        -2426024
48
 XDOT =      -5180
597900                 XDOT =       -1611
678301
 YDOT =      17225
931436  feet/sec       YDOT =        5232
623891  meter/sec
 ZDOT =     -17536
023472                 ZDOT =       -5352
729135

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17261443
99                 X    =        -5261288
13
 Y    =       11705229
39  feet           Y    =         3567753
92  meter
 Z    =       -7918998
20                 Z    =        -2413710
65
 XDOT =      -2989
666137                 XDOT =        -911
250239
 YDOT =     -16278
242031  feet/sec       YDOT =       -4961
608171  meter/sec
 ZDOT =     -17571
791572                 ZDOT =       -5355
882071


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   20134
96495748  
00016717  00000-0  10270-3 0  9166
2 25544  51
6415 157
8580 0001466 294
9197  65
1801 15
49353626 26706


Satellite: ISS
Catalog Number: 25544
Epoch time:      20134
96495748   =   yrday
fracday
Element set:     916
Inclination:       51
6415  deg
RA of node:       157
8580  deg
Eccentricity:     
0001466     
Arg of perigee:   294
9197  deg
Mean anomaly:      65
1801  deg
Mean motion:   15
49353626  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2670
Checksum:              336
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