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

 
Date: May 4th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 16466 6302 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 8

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

135/18:45:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 1
000/00:00:00 000 0 0 0 0 222 6

Coasting Arc #1 (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    =        1986160
75                 A    =         6791238
11  meter
 Y    =       -3743993
79  meter          E    =           
0001173
 Z    =        5305483
61                 I    =           51
46461
 XDOT =       6925
707236                 Wp   =          108
14420
 YDOT =       3264
593066  meter/sec      RA   =          203
51380  deg
 ZDOT =       -289
242344                 TA   =          344
62018
                                          MA   =          344
62375
                                          Ha   =            227
956  n
mi
                                          Hp   =            222
639

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6516275
41                 X    =         2002108
33
 Y    =      -12283444
20  feet           Y    =        -3721693
96  meter
 Z    =       17406442
30                 Z    =         5315170
43
 XDOT =      22722
136602                 XDOT =        6890
091842
 YDOT =      10710
607171  feet/sec       YDOT =        3341
842116  meter/sec
 ZDOT =       -948
957822                 ZDOT =        -255
686161

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3448574
35                 X    =        -1051125
46
 Y    =      -13412649
44  feet           Y    =        -4088175
55  meter
 Z    =       17450995
67                 Z    =         5319063
48
 XDOT =      23087
327237                 XDOT =        7037
017342
 YDOT =      -6969
182725  feet/sec       YDOT =       -2124
206894  meter/sec
 ZDOT =       -795
041468                 ZDOT =        -242
328639


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
54797763  
00016717  00000-0  10270-3 0  9005
2 25544  51
6437 204
4619 0001576 237
9201 122
1797 15
49376176 25248


Satellite: ISS
Catalog Number: 25544
Epoch time:      20125
54797763   =   yrday
fracday
Element set:     900
Inclination:       51
6437  deg
RA of node:       204
4619  deg
Eccentricity:     
0001576     
Arg of perigee:   237
9201  deg
Mean anomaly:     122
1797  deg
Mean motion:   15
49376176  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2524
Checksum:              317


Coasting Arc #2 (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    =       -1807461
96                 A    =         6791402
21  meter
 Y    =        3847814
37  meter          E    =           
0013523
 Z    =       -5308040
45                 I    =           51
49504
 XDOT =      -7125
357377                 Wp   =           96
27003
 YDOT =      -2752
753554  meter/sec      RA   =          198
55443  deg
 ZDOT =        430
307569                 TA   =          177
85441
                                          MA   =          177
84860
                                          Ha   =            228
093  n
mi
                                          Hp   =            222
609

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5929993
32                 X    =        -1824571
23
 Y    =       12624062
88  feet           Y    =         3827506
41  meter
 Z    =      -17414830
87                 Z    =        -5316862
06
 XDOT =     -23377
156748                 XDOT =       -7096
135916
 YDOT =      -9031
343681  feet/sec       YDOT =       -2832
270988  meter/sec
 ZDOT =       1411
770240                 ZDOT =         395
765826

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4340104
12                 X    =         1322863
74
 Y    =       13201514
72  feet           Y    =         4023821
69  meter
 Z    =      -17455418
19                 Z    =        -5320411
46
 XDOT =     -22313
392936                 XDOT =       -6801
122167
 YDOT =       8995
006042  feet/sec       YDOT =        2741
677842  meter/sec
 ZDOT =       1253
299281                 ZDOT =         382
005621


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
51548904  
00016717  00000-0  10270-3 0  9015
2 25544  51
6427 199
6743 0001420 244
9109 115
1894 15
49333755 25395


Satellite: ISS
Catalog Number: 25544
Epoch time:      20126
51548904   =   yrday
fracday
Element set:     901
Inclination:       51
6427  deg
RA of node:       199
6743  deg
Eccentricity:     
0001420     
Arg of perigee:   244
9109  deg
Mean anomaly:     115
1894  deg
Mean motion:   15
49333755  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2539
Checksum:              314


Coasting Arc #3 (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    =        1618431
44                 A    =         6791316
88  meter
 Y    =       -3935195
21  meter          E    =           
0001339
 Z    =        5292049
20                 I    =           51
52719
 XDOT =       7306
484756                 Wp   =           69
63611
 YDOT =       2234
932359  meter/sec      RA   =          193
59737  deg
 ZDOT =       -572
011462                 TA   =           25
83909
                                          MA   =           25
83240
                                          Ha   =            227
954  n
mi
                                          Hp   =            222
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5309814
42                 X    =         1636609
44
 Y    =      -12910745
43  feet           Y    =        -3916995
25  meter
 Z    =       17362366
13                 Z    =         5299955
10
 XDOT =      23971
406681                 XDOT =        7283
728601
 YDOT =       7332
455245  feet/sec       YDOT =        2316
511449  meter/sec
 ZDOT =      -1876
678024                 ZDOT =        -536
573967

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5211917
72                 X    =        -1588592
52
 Y    =      -12901643
18  feet           Y    =        -3932420
84  meter
 Z    =       17398757
18                 Z    =         5303141
19
 XDOT =      21423
933496                 XDOT =        6530
014929
 YDOT =     -10968
761176  feet/sec       YDOT =       -3343
278406  meter/sec
 ZDOT =      -1714
063660                 ZDOT =        -522
446604


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
54749850  
00016717  00000-0  10270-3 0  9023
2 25544  51
6424 194
5674 0001452 247
5042 112
5954 15
49373672 25557


Satellite: ISS
Catalog Number: 25544
Epoch time:      20127
54749850   =   yrday
fracday
Element set:     902
Inclination:       51
6424  deg
RA of node:       194
5674  deg
Eccentricity:     
0001452     
Arg of perigee:   247
5042  deg
Mean anomaly:     112
5954  deg
Mean motion:   15
49373672  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2555
Checksum:              314


Coasting Arc #4 (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    =       -1429447
53                 A    =         6791505
13  meter
 Y    =        4028976
11  meter          E    =           
0013341
 Z    =       -5288828
38                 I    =           51
55912
 XDOT =      -7425
518676                 Wp   =           97
88611
 YDOT =      -1699
960624  meter/sec      RA   =          188
64197  deg
 ZDOT =        711
688426                 TA   =          178
93606
                                          MA   =          178
93322
                                          Ha   =            228
076  n
mi
                                          Hp   =            222
641

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4689788
47                 X    =        -1448703
87
 Y    =       13218425
56  feet           Y    =         4012883
64  meter
 Z    =      -17351799
15                 Z    =        -5295818
77
 XDOT =     -24361
937915                 XDOT =       -7409
414376
 YDOT =      -5577
298634  feet/sec       YDOT =       -1782
908052  meter/sec
 ZDOT =       2334
935780                 ZDOT =         675
656451

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6089419
50                 X    =         1856055
06
 Y    =       12590530
56  feet           Y    =         3837593
72  meter
 Z    =      -17383996
50                 Z    =        -5298642
13
 XDOT =     -20288
247034                 XDOT =       -6183
857696
 YDOT =      12809
080177  feet/sec       YDOT =        3904
207638  meter/sec
 ZDOT =       2169
557289                 ZDOT =         661
281062


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
51500848  
00016717  00000-0  10270-3 0  9034
2 25544  51
6412 189
7793 0001382 252
6059 107
4940 15
49331683 25700


Satellite: ISS
Catalog Number: 25544
Epoch time:      20128
51500848   =   yrday
fracday
Element set:     903
Inclination:       51
6412  deg
RA of node:       189
7793  deg
Eccentricity:     
0001382     
Arg of perigee:   252
6059  deg
Mean anomaly:     107
4940  deg
Mean motion:   15
49331683  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2570
Checksum:              308


Coasting Arc #5 (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    =        1235021
62                 A    =         6791436
64  meter
 Y    =       -4104511
13  meter          E    =           
0001978
 Z    =        5266811
56                 I    =           51
59304
 XDOT =       7524
555678                 Wp   =           49
39645
 YDOT =       1164
639031  meter/sec      RA   =          183
68884  deg
 ZDOT =       -855
351197                 TA   =           48
80235
                                          MA   =           48
78530
                                          Ha   =            227
954  n
mi
                                          Hp   =            222
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4051908
20                 X    =         1255244
06
 Y    =      -13466243
85  feet           Y    =        -4090587
62  meter
 Z    =       17279565
48                 Z    =         5272859
68
 XDOT =      24686
862461                 XDOT =        7515
127980
 YDOT =       3820
994196  feet/sec       YDOT =        1248
731326  meter/sec
 ZDOT =      -2806
270333                 ZDOT =        -818
821965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6926737
12                 X    =        -2111269
48
 Y    =      -12198921
27  feet           Y    =        -3718231
20  meter
 Z    =       17307446
36                 Z    =         5275309
65
 XDOT =      19053
381569                 XDOT =        5807
470702
 YDOT =     -14569
156684  feet/sec       YDOT =       -4440
678957  meter/sec
 ZDOT =      -2638
569545                 ZDOT =        -804
235997


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
54701439  
00016717  00000-0  10270-3 0  9048
2 25544  51
6415 184
6719 0001370 258
9296 101
1700 15
49375277 25863


Satellite: ISS
Catalog Number: 25544
Epoch time:      20129
54701439   =   yrday
fracday
Element set:     904
Inclination:       51
6415  deg
RA of node:       184
6719  deg
Eccentricity:     
0001370     
Arg of perigee:   258
9296  deg
Mean anomaly:     101
1700  deg
Mean motion:   15
49375277  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2586
Checksum:              315


Coasting Arc #6 (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    =        6603910
82                 A    =         6802749
72  meter
 Y    =        1076336
91  meter          E    =           
0008457
 Z    =       -1204315
10                 I    =           51
64855
 XDOT =      -1811
935153                 Wp   =          149
65838
 YDOT =       4597
287140  meter/sec      RA   =          181
06966  deg
 ZDOT =      -5852
177932                 TA   =           43
39648
                                          MA   =           43
32993
                                          Ha   =            228
083  n
mi
                                          Hp   =            222
752

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21666374
10                 X    =         6597234
06
 Y    =        3531289
07  feet           Y    =         1150149
33  meter
 Z    =       -3951165
02                 Z    =        -1172251
45
 XDOT =      -5944
669136                 XDOT =       -1834
781708
 YDOT =      15082
963058  feet/sec       YDOT =        4576
897637  meter/sec
 ZDOT =     -19200
058833                 ZDOT =       -5861
034781

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14410049
00                 X    =        -4392182
93
 Y    =       16594996
19  feet           Y    =         5058154
84  meter
 Z    =       -3803953
65                 Z    =        -1159445
07
 XDOT =      -8561
338305                 XDOT =       -2609
495915
 YDOT =     -11824
958877  feet/sec       YDOT =       -3604
247466  meter/sec
 ZDOT =     -19240
855151                 ZDOT =       -5864
612650


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
06301813  
00016717  00000-0  10270-3 0  9050
2 25544  51
6419 182
1195 0001394 271
4083  88
6908 15
49328268 25944


Satellite: ISS
Catalog Number: 25544
Epoch time:      20130
06301813   =   yrday
fracday
Element set:     905
Inclination:       51
6419  deg
RA of node:       182
1195  deg
Eccentricity:     
0001394     
Arg of perigee:   271
4083  deg
Mean anomaly:      88
6908  deg
Mean motion:   15
49328268  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2594
Checksum:              308


Coasting Arc #7 (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    =       -6641703
00                 A    =         6802489
08  meter
 Y    =        -590170
39  meter          E    =           
0012678
 Z    =        1313538
44                 I    =           51
68019
 XDOT =       1578
072605                 Wp   =           55
71920
 YDOT =      -4721
048741  meter/sec      RA   =          176
12117  deg
 ZDOT =       5824
878849                 TA   =          318
54271
                                          MA   =          318
63882
                                          Ha   =            228
001  n
mi
                                          Hp   =            222
675

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21790364
17                 X    =        -6640990
41
 Y    =       -1936254
57  feet           Y    =         -664438
81  meter
 Z    =        4309509
32                 Z    =         1281276
92
 XDOT =       5177
403560                 XDOT =        1602
453222
 YDOT =     -15489
005056  feet/sec       YDOT =       -4703
265979  meter/sec
 ZDOT =      19110
494910                 ZDOT =        5832
603258

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12816108
04                 X    =         3906349
73
 Y    =      -17764331
25  feet           Y    =        -5414568
17  meter
 Z    =        4161349
89                 Z    =         1268379
45
 XDOT =       9436
947387                 XDOT =        2876
381564
 YDOT =      11319
794026  feet/sec       YDOT =        3450
273219  meter/sec
 ZDOT =      19146
103872                 ZDOT =        5835
732460


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
09502147  
00016717  00000-0  10270-3 0  9068
2 25544  51
6403 177
0110 0001355 276
9738  83
1258 15
49381230 26106


Satellite: ISS
Catalog Number: 25544
Epoch time:      20131
09502147   =   yrday
fracday
Element set:     906
Inclination:       51
6403  deg
RA of node:       177
0110  deg
Eccentricity:     
0001355     
Arg of perigee:   276
9738  deg
Mean anomaly:      83
1258  deg
Mean motion:   15
49381230  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2610
Checksum:              278


Coasting Arc #8 (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    =        6640761
91                 A    =         6802444
75  meter
 Y    =         128966
53  meter          E    =           
0007561
 Z    =       -1451863
54                 I    =           51
71272
 XDOT =      -1354
533136                 Wp   =          150
21383
 YDOT =       4832
149773  meter/sec      RA   =          171
17637  deg
 ZDOT =      -5785
701036                 TA   =           45
57321
                                          MA   =           45
51136
                                          Ha   =            228
059  n
mi
                                          Hp   =            222
751

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21787276
60                 X    =         6645878
58
 Y    =         423118
55  feet           Y    =          203257
04  meter
 Z    =       -4763331
82                 Z    =        -1419592
65
 XDOT =      -4444
006351                 XDOT =       -1380
363180
 YDOT =      15853
509755  feet/sec       YDOT =        4816
858706  meter/sec
 ZDOT =     -18981
958780                 ZDOT =       -5792
343017

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11194948
80                 X    =        -3412220
39
 Y    =       18733068
38  feet           Y    =         5709839
24  meter
 Z    =       -4615089
54                 Z    =        -1406679
29
 XDOT =     -10255
482358                 XDOT =       -3125
871023
 YDOT =     -10796
522701  feet/sec       YDOT =       -3290
780119  meter/sec
 ZDOT =     -19012
607238                 ZDOT =       -5795
042686


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
06252689  
00016717  00000-0  10270-3 0  9070
2 25544  51
6399 172
2231 0001438 279
5476  80
5512 15
49340995 26254


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
06252689   =   yrday
fracday
Element set:     907
Inclination:       51
6399  deg
RA of node:       172
2231  deg
Eccentricity:     
0001438     
Arg of perigee:   279
5476  deg
Mean anomaly:      80
5512  deg
Mean motion:   15
49340995  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2625
Checksum:              318


Coasting Arc #9 (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    =        3852226
31                 A    =         6796622
26  meter
 Y    =       -3986480
63  meter          E    =           
0009915
 Z    =        3925550
36                 I    =           51
71308
 XDOT =       6189
639323                 Wp   =           77
48476
 YDOT =       1966
368184  meter/sec      RA   =          168
00392  deg
 ZDOT =      -4066
360043                 TA   =           55
10164
                                          MA   =           55
00849
                                          Ha   =            227
994  n
mi
                                          Hp   =            222
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12638537
75                 X    =         3877449
86
 Y    =      -13079004
69  feet           Y    =        -3943261
73  meter
 Z    =       12879102
22                 Z    =         3944323
83
 XDOT =      20307
215627                 XDOT =        6186
942913
 YDOT =       6451
339187  feet/sec       YDOT =        2035
570544  meter/sec
 ZDOT =     -13341
076257                 ZDOT =       -4036
299387

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16451488
95                 X    =        -5014413
83
 Y    =       -7609825
61  feet           Y    =        -2319474
85  meter
 Z    =       12965467
19                 Z    =         3951874
40
 XDOT =      -1095
443895                 XDOT =        -333
891299
 YDOT =     -20186
667929  feet/sec       YDOT =       -6152
896385  meter/sec
 ZDOT =     -13203
024019                 ZDOT =       -4024
281721


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
70752970  
00016717  00000-0  10270-3 0  9080
2 25544  51
6382 169
0300 0001238 285
0918  75
0095 15
49366105 26355


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
70752970   =   yrday
fracday
Element set:     908
Inclination:       51
6382  deg
RA of node:       169
0300  deg
Eccentricity:     
0001238     
Arg of perigee:   285
0918  deg
Mean anomaly:      75
0095  deg
Mean motion:   15
49366105  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2635
Checksum:              299


Coasting Arc #10 (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    =        6432419
25                 A    =         6801361
07  meter
 Y    =         254311
64  meter          E    =           
0005211
 Z    =       -2188831
73                 I    =           51
74143
 XDOT =      -2058
062552                 Wp   =          148
00744
 YDOT =       4930
868077  meter/sec      RA   =          166
71109  deg
 ZDOT =      -5485
521274                 TA   =           56
19532
                                          MA   =           56
14571
                                          Ha   =            228
076  n
mi
                                          Hp   =            222
787

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21103737
68                 X    =         6439729
51
 Y    =         834355
78  feet           Y    =          326284
66  meter
 Z    =       -7181206
47                 Z    =        -2157567
67
 XDOT =      -6752
173726                 XDOT =       -2086
402420
 YDOT =      16177
388704  feet/sec       YDOT =        4907
695541  meter/sec
 ZDOT =     -17997
117040                 ZDOT =       -5495
586823

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19261577
11                 X    =        -5870928
70
 Y    =        8780539
63  feet           Y    =         2676308
48  meter
 Z    =       -7037569
96                 Z    =        -2145051
33
 XDOT =       -724
853855                 XDOT =        -220
935455
 YDOT =     -16024
259425  feet/sec       YDOT =       -4884
194273  meter/sec
 ZDOT =     -18043
504364                 ZDOT =       -5499
660130


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
96553052  
00016717  00000-0  10270-3 0  9099
2 25544  51
6424 167
7550 0001441 281
7645  78
3343 15
49333624 26396


Satellite: ISS
Catalog Number: 25544
Epoch time:      20132
96553052   =   yrday
fracday
Element set:     909
Inclination:       51
6424  deg
RA of node:       167
7550  deg
Eccentricity:     
0001441     
Arg of perigee:   281
7645  deg
Mean anomaly:      78
3343  deg
Mean motion:   15
49333624  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2639
Checksum:              309


Coasting Arc #11 (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    =       -6392939
49                 A    =         6801089
24  meter
 Y    =         204576
35  meter          E    =           
0012816
 Z    =        2292475
85                 I    =           51
77322
 XDOT =       1792
509621                 Wp   =           67
64807
 YDOT =      -5096
896382  meter/sec      RA   =          161
76882  deg
 ZDOT =       5434
001432                 TA   =          317
78728
                                          MA   =          317
88589
                                          Ha   =            228
103  n
mi
                                          Hp   =            222
692

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20974210
92                 X    =        -6405887
52
 Y    =         671182
26  feet           Y    =          133013
32  meter
 Z    =        7521246
23                 Z    =         2261390
02
 XDOT =       5880
937076                 XDOT =        1822
976135
 YDOT =     -16722
100990  feet/sec       YDOT =       -5076
681476  meter/sec
 ZDOT =      17828
088689                 ZDOT =        5442
782215

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18294110
39                 X    =         5576044
85
 Y    =      -10383738
01  feet           Y    =        -3164963
34  meter
 Z    =        7378391
71                 Z    =         2248933
79
 XDOT =       1931
179754                 XDOT =         588
623589
 YDOT =      16145
706759  feet/sec       YDOT =        4921
211420  meter/sec
 ZDOT =      17868
585884                 ZDOT =        5446
344977


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
99753093  
00016717  00000-0  10270-3 0  9102
2 25544  51
6424 162
6464 0001456 295
9666  64
1334 15
49362755 26558


Satellite: ISS
Catalog Number: 25544
Epoch time:      20133
99753093   =   yrday
fracday
Element set:     910
Inclination:       51
6424  deg
RA of node:       162
6464  deg
Eccentricity:     
0001456     
Arg of perigee:   295
9666  deg
Mean anomaly:      64
1334  deg
Mean motion:   15
49362755  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2655
Checksum:              324


Coasting Arc #12 (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    =        6321927
47                 A    =         6800901
48  meter
 Y    =        -632089
18  meter          E    =           
0004296
 Z    =       -2422783
92                 I    =           51
80303
 XDOT =      -1528
224012                 Wp   =          140
80256
 YDOT =       5245
506617  meter/sec      RA   =          156
82989  deg
 ZDOT =      -5364
656426                 TA   =           66
15817
                                          MA   =           66
11315
                                          Ha   =            228
108  n
mi
                                          Hp   =            222
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20741231
87                 X    =         6340294
31
 Y    =       -2073783
40  feet           Y    =         -561289
98  meter
 Z    =       -7948766
14                 Z    =        -2392029
95
 XDOT =      -5013
858306                 XDOT =       -1560
708839
 YDOT =      17209
667380  feet/sec       YDOT =        5228
235762  meter/sec
 ZDOT =     -17600
578824                 ZDOT =       -5372
158375

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17236727
41                 X    =        -5253754
51
 Y    =       11816169
01  feet           Y    =         3601568
31  meter
 Z    =       -7807402
81                 Z    =        -2379696
38
 XDOT =      -3120
342677                 XDOT =        -951
080448
 YDOT =     -16185
408593  feet/sec       YDOT =       -4933
312539  meter/sec
 ZDOT =     -17635
210506                 ZDOT =       -5375
212162


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
96503122  
00016717  00000-0  10270-3 0  9117
2 25544  51
6415 157
8583 0001451 294
0384  66
0614 15
49337901 26702


Satellite: ISS
Catalog Number: 25544
Epoch time:      20134
96503122   =   yrday
fracday
Element set:     911
Inclination:       51
6415  deg
RA of node:       157
8583  deg
Eccentricity:     
0001451     
Arg of perigee:   294
0384  deg
Mean anomaly:      66
0614  deg
Mean motion:   15
49337901  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2670
Checksum:              293


Coasting Arc #13 (Orbit 2682)
---------------------------------------

Vector Time (GMT): 2020/135/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4964445
36                 A    =         6794985
54  meter
 Y    =        1367531
42  meter          E    =           
0008319
 Z    =       -4442111
37                 I    =           51
80968
 XDOT =      -4441
069288                 Wp   =           62
53076
 YDOT =       5258
125184  meter/sec      RA   =          152
66624  deg
 ZDOT =      -3345
608455                 TA   =          173
67867
                                          MA   =          173
66817
                                          Ha   =            228
125  n
mi
                                          Hp   =            222
647

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16287550
41                 X    =         4970361
48
 Y    =        4486651
64  feet           Y    =         1423080
79  meter
 Z    =      -14573856
18                 Z    =        -4417981
58
 XDOT =     -14570
437297                 XDOT =       -4483
286094
 YDOT =      17251
066877  feet/sec       YDOT =        5208
226186  meter/sec
 ZDOT =     -10976
405693                 ZDOT =       -3367
283564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12626823
28                 X    =        -3848655
73
 Y    =      -11366488
48  feet           Y    =        -3464505
69  meter
 Z    =      -14462983
74                 Z    =        -4408317
44
 XDOT =      19869
289882                 XDOT =        6056
159556
 YDOT =      -7983
344794  feet/sec       YDOT =       -2433
323493  meter/sec
 ZDOT =     -11076
190894                 ZDOT =       -3376
022984


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   20135
80353233  
00016717  00000-0  10270-3 0  9128
2 25544  51
6417 153
7081 0001287 305
8618  54
2412 15
49381745 26834


Satellite: ISS
Catalog Number: 25544
Epoch time:      20135
80353233   =   yrday
fracday
Element set:     912
Inclination:       51
6417  deg
RA of node:       153
7081  deg
Eccentricity:     
0001287     
Arg of perigee:   305
8618  deg
Mean anomaly:      54
2412  deg
Mean motion:   15
49381745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2683
Checksum:              296


Coasting Arc #14 (Orbit 2698)
---------------------------------------

Vector Time (GMT): 2020/136/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4974305
10                 A    =         6794780
14  meter
 Y    =       -1045182
24  meter          E    =           
0007836
 Z    =        4504207
96                 I    =           51
83829
 XDOT =       4110
836374                 Wp   =          109
04555
 YDOT =      -5600
679311  meter/sec      RA   =          147
72976  deg
 ZDOT =       3233
178950                 TA   =          308
46564
                                          MA   =          308
53592
                                          Ha   =            228
276  n
mi
                                          Hp   =            222
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16319898
61                 X    =        -4984126
75
 Y    =       -3429075
59  feet           Y    =        -1100863
66  meter
 Z    =       14777585
17                 Z    =         4480020
78
 XDOT =      13486
995977                 XDOT =        4157
454353
 YDOT =     -18374
932123  feet/sec       YDOT =       -5554
448558  meter/sec
 ZDOT =      10607
542486                 ZDOT =        3253
260684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13309462
58                 X    =         4056724
19
 Y    =       10209250
94  feet           Y    =         3111779
69  meter
 Z    =       14666426
79                 Z    =         4470326
88
 XDOT =     -19310
787484                 XDOT =       -5885
928025
 YDOT =       9769
717637  feet/sec       YDOT =        2977
809936  meter/sec
 ZDOT =      10700
028955                 ZDOT =        3261
368826


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   20136
83553098  
00016717  00000-0  10270-3 0  9134
2 25544  51
6418 148
6005 0001314 305
9029  54
1999 15
49364945 26991


Satellite: ISS
Catalog Number: 25544
Epoch time:      20136
83553098   =   yrday
fracday
Element set:     913
Inclination:       51
6418  deg
RA of node:       148
6005  deg
Eccentricity:     
0001314     
Arg of perigee:   305
9029  deg
Mean anomaly:      54
1999  deg
Mean motion:   15
49364945  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2699
Checksum:              329


Coasting Arc #15 (Orbit 2713)
---------------------------------------

Vector Time (GMT): 2020/137/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4967490
37                 A    =         6794429
64  meter
 Y    =         747275
64  meter          E    =           
0009261
 Z    =       -4584244
99                 I    =           51
86622
 XDOT =      -3750
515219                 Wp   =           62
22951
 YDOT =       5904
915382  meter/sec      RA   =          142
79500  deg
 ZDOT =      -3102
099295                 TA   =          176
75071
                                          MA   =          176
74469
                                          Ha   =            228
140  n
mi
                                          Hp   =            222
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16297540
58                 X    =         4981032
65
 Y    =        2451691
73  feet           Y    =          802901
63  meter
 Z    =      -15040173
84                 Z    =        -4560081
83
 XDOT =     -12304
839958                 XDOT =       -3801
198702
 YDOT =      19373
081963  feet/sec       YDOT =        5862
691237  meter/sec
 ZDOT =     -10177
491125                 ZDOT =       -3120
440674

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13873026
23                 X    =        -4228498
39
 Y    =       -9082312
13  feet           Y    =        -2768288
74  meter
 Z    =      -14929105
81                 Z    =        -4550391
45
 XDOT =      18551
327346                 XDOT =        5654
444575
 YDOT =     -11471
745809  feet/sec       YDOT =       -3496
588123  meter/sec
 ZDOT =     -10262
001536                 ZDOT =       -3127
858068


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   20137
80302684  
00016717  00000-0  10270-3 0  9146
2 25544  51
6429 143
8123 0001407 314
3515  45
7519 15
49389248 27143


Satellite: ISS
Catalog Number: 25544
Epoch time:      20137
80302684   =   yrday
fracday
Element set:     914
Inclination:       51
6429  deg
RA of node:       143
8123  deg
Eccentricity:     
0001407     
Arg of perigee:   314
3515  deg
Mean anomaly:      45
7519  deg
Mean motion:   15
49389248  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2714
Checksum:              303


Coasting Arc #16 (Orbit 2729)
---------------------------------------

Vector Time (GMT): 2020/138/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4937338
16                 A    =         6794253
77  meter
 Y    =        -442608
36  meter          E    =           
0007257
 Z    =        4641700
43                 I    =           51
89074
 XDOT =       3367
317102                 Wp   =          110
07406
 YDOT =      -6203
129414  meter/sec      RA   =          137
86182  deg
 ZDOT =       2984
080372                 TA   =          310
23049
                                          MA   =          310
29396
                                          Ha   =            228
377  n
mi
                                          Hp   =            222
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16198616
00                 X    =        -4954568
72
 Y    =       -1452127
17  feet           Y    =         -497917
80  meter
 Z    =       15228675
97                 Z    =         4617674
72
 XDOT =      11047
628286                 XDOT =        3421
937003
 YDOT =     -20351
474456  feet/sec       YDOT =       -6165
168446  meter/sec
 ZDOT =       9790
289935                 ZDOT =        3000
569919

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14340011
62                 X    =         4370835
54
 Y    =        7887958
31  feet           Y    =         2404249
69  meter
 Z    =       15118220
33                 Z    =         4608033
56
 XDOT =     -17666
015510                 XDOT =       -5384
601527
 YDOT =      13166
852122  feet/sec       YDOT =        4013
256527  meter/sec
 ZDOT =       9866
312142                 ZDOT =        3007
251941


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   20138
83502282  
00016717  00000-0  10270-3 0  9157
2 25544  51
6422 138
7045 0001343 319
7525  40
3525 15
49364096 27301


Satellite: ISS
Catalog Number: 25544
Epoch time:      20138
83502282   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:       138
7045  deg
Eccentricity:     
0001343     
Arg of perigee:   319
7525  deg
Mean anomaly:      40
3525  deg
Mean motion:   15
49364096  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2730
Checksum:              292


Coasting Arc #17 (Orbit 2744)
---------------------------------------

Vector Time (GMT): 2020/139/18:45:00
000
Vector Time (MET): N/A
Weight (LBS)     : 921014
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4897529
08                 A    =         6793919
25  meter
 Y    =         161417
52  meter          E    =           
0010097
 Z    =       -4715796
23                 I    =           51
91398
 XDOT =      -2956
453753                 Wp   =           62
78497
 YDOT =       6456
870937  meter/sec      RA   =          132
93085  deg
 ZDOT =      -2849
572726                 TA   =          178
97791
                                          MA   =          178
97584
                                          Ha   =            228
151  n
mi
                                          Hp   =            222
633

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16068008
79                 X    =         4918266
96
 Y    =         529585
05  feet           Y    =          216301
43  meter
 Z    =      -15471772
41                 Z    =        -4691955
31
 XDOT =      -9699
651419                 XDOT =       -3014
594921
 YDOT =      21183
959766  feet/sec       YDOT =        6423
484857  meter/sec
 ZDOT =      -9348
991883                 ZDOT =       -2864
074991

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14711271
79                 X    =        -4483995
64
 Y    =       -6739436
80  feet           Y    =        -2054180
34  meter
 Z    =      -15362147
72                 Z    =        -4682382
62
 XDOT =      16584
013587                 XDOT =        5054
807341
 YDOT =     -14739
145246  feet/sec       YDOT =       -4492
491471  meter/sec
 ZDOT =      -9415
902968                 ZDOT =       -2869
967225


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   20139
80251720  
00016717  00000-0  10270-3 0  9164
2 25544  51
6422 133
9166 0001522 318
5892  41
5142 15
49388958 27452


Satellite: ISS
Catalog Number: 25544
Epoch time:      20139
80251720   =   yrday
fracday
Element set:     916
Inclination:       51
6422  deg
RA of node:       133
9166  deg
Eccentricity:     
0001522     
Arg of perigee:   318
5892  deg
Mean anomaly:      41
5142  deg
Mean motion:   15
49388958  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2745
Checksum:              310
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