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

 
Date: November 30th 2020

  • spaceflight nasa gov will be taken offline in the next 30 days *
  • *
  • Current information about the International Space Station can be *
  • found at www nasa gov/station *
  • *
  • Predicted ISS and visiting vehicle sightings opportunities can be *
  • found at spotthestation nasa gov *
  • *
  • Updated ISS trajectory information will be made available as a CCSDS *
  • Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
  • system *
  • Included in the OEM are a sequence of events with ISS maneuver *
  • details (in the comment section), predicted post-maneuver state *
  • vectors, predicted coasting state vectors at 4-minute intervals, *
  • and ISS ballistic details *
  • *
  • OEMs will be provided in xml and txt formats *
  • Links to the OEMs and more details to follow *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 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


335/15:02:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 221 8

338/19:32:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 221 9

340/16:39:40 000 0 0 0 0 0 0
N/A 0 0 0 0 229 4
000/00:00:00 000 0 0 0 0 222 0

341/16:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 6
000/00:00:00 000 0 0 0 0 221 7

341/22:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 221 9

Coasting Arc #1 (Orbit 1732)
---------------------------------------

Vector Time (GMT): 2020/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4254822
88                 A    =         6794939
68  meter
 Y    =        2584348
99  meter          E    =           
0010027
 Z    =        4618586
27                 I    =           51
24650
 XDOT =      -1074
755877                 Wp   =           67
64235
 YDOT =       7003
773320  meter/sec      RA   =          259
40776  deg
 ZDOT =      -2920
027875                 TA   =           51
64965
                                          MA   =           51
55958
                                          Ha   =            229
494  n
mi
                                          Hp   =            221
949

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13959392
65                 X    =         4203172
76
 Y    =        8478835
27  feet           Y    =         2631640
35  meter
 Z    =       15152842
08                 Z    =         4639129
70
 XDOT =      -3526
101960                 XDOT =       -1138
810190
 YDOT =      22978
258924  feet/sec       YDOT =        6991
396688  meter/sec
 ZDOT =      -9580
143948                 ZDOT =       -2925
403804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13389065
14                 X    =        -4080987
06
 Y    =        9197981
03  feet           Y    =         2803544
62  meter
 Z    =       15247753
73                 Z    =         4647515
34
 XDOT =     -18903
326446                 XDOT =       -5761
733901
 YDOT =     -11546
021779  feet/sec       YDOT =       -3519
227438  meter/sec
 ZDOT =      -9605
189097                 ZDOT =       -2927
661637


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   20332
54318786  
00016717  00000-0  10270-3 0  9009
2 25544  51
6437 260
1794 0001835  80
0152 280
1205 15
49076550 17334


Satellite: ISS
Catalog Number: 25544
Epoch time:      20332
54318786   =   yrday
fracday
Element set:     900
Inclination:       51
6437  deg
RA of node:       260
1794  deg
Eccentricity:     
0001835     
Arg of perigee:    80
0152  deg
Mean anomaly:     280
1205  deg
Mean motion:   15
49076550  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1733
Checksum:              287


Coasting Arc #2 (Orbit 1747)
---------------------------------------

Vector Time (GMT): 2020/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4467905
46                 A    =         6794940
78  meter
 Y    =       -2244093
31  meter          E    =           
0012037
 Z    =       -4613132
12                 I    =           51
25464
 XDOT =        495
105019                 Wp   =          105
60021
 YDOT =      -7041
448135  meter/sec      RA   =          254
43370  deg
 ZDOT =       2949
137717                 TA   =          194
00496
                                          MA   =          194
03836
                                          Ha   =            229
611  n
mi
                                          Hp   =            221
759

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14658482
47                 X    =        -4420070
81
 Y    =       -7362510
87  feet           Y    =        -2293788
76  meter
 Z    =      -15134947
91                 Z    =        -4634719
96
 XDOT =       1624
360297                 XDOT =         559
482286
 YDOT =     -23101
863960  feet/sec       YDOT =       -7035
551828  meter/sec
 ZDOT =       9675
648677                 ZDOT =        2951
698518

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12475596
27                 X    =         3802561
74
 Y    =      -10507498
30  feet           Y    =        -3202685
48  meter
 Z    =      -15234707
09                 Z    =        -4643538
72
 XDOT =      19879
177128                 XDOT =        6059
173189
 YDOT =       9572
132561  feet/sec       YDOT =        2917
586005  meter/sec
 ZDOT =       9687
668536                 ZDOT =        2952
801370


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   20333
51086124  
00016717  00000-0  10270-3 0  9016
2 25544  51
6442 255
3919 0001911  81
3902 278
7465 15
49093513 17482


Satellite: ISS
Catalog Number: 25544
Epoch time:      20333
51086124   =   yrday
fracday
Element set:     901
Inclination:       51
6442  deg
RA of node:       255
3919  deg
Eccentricity:     
0001911     
Arg of perigee:    81
3902  deg
Mean anomaly:     278
7465  deg
Mean motion:   15
49093513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1748
Checksum:              302


Coasting Arc #3 (Orbit 1763)
---------------------------------------

Vector Time (GMT): 2020/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4637275
85                 A    =         6795050
78  meter
 Y    =        1908741
48  meter          E    =           
0010298
 Z    =        4578759
64                 I    =           51
26492
 XDOT =         70
430929                 Wp   =           69
31396
 YDOT =       7051
340595  meter/sec      RA   =          249
46192  deg
 ZDOT =      -3001
739749                 TA   =           50
87132
                                          MA   =           50
77982
                                          Ha   =            229
514  n
mi
                                          Hp   =            221
881

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15214159
63                 X    =         4593345
60
 Y    =        6262275
19  feet           Y    =         1960352
69  meter
 Z    =       15022177
28                 Z    =         4601179
71
 XDOT =        231
072602                 XDOT =           6
156519
 YDOT =      23134
319537  feet/sec       YDOT =        7051
769157  meter/sec
 ZDOT =      -9848
227522                 ZDOT =       -3001
552944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11482518
22                 X    =        -3499871
55
 Y    =       11649651
30  feet           Y    =         3550813
72  meter
 Z    =       15125804
24                 Z    =         4610345
13
 XDOT =     -20700
896073                 XDOT =       -6309
633123
 YDOT =      -7579
568876  feet/sec       YDOT =       -2310
252593  meter/sec
 ZDOT =      -9847
532641                 ZDOT =       -3001
527949


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   20334
54304296  
00016717  00000-0  10270-3 0  9024
2 25544  51
6439 250
2869 0001947  84
3370 275
8003 15
49088145 17646


Satellite: ISS
Catalog Number: 25544
Epoch time:      20334
54304296   =   yrday
fracday
Element set:     902
Inclination:       51
6439  deg
RA of node:       250
2869  deg
Eccentricity:     
0001947     
Arg of perigee:    84
3370  deg
Mean anomaly:     275
8003  deg
Mean motion:   15
49088145  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1764
Checksum:              314


Coasting Arc #4 (Orbit 1778)
---------------------------------------

Vector Time (GMT): 2020/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4796468
29                 A    =         6795056
26  meter
 Y    =       -1540599
47  meter          E    =           
0011850
 Z    =       -4571607
23                 I    =           51
27861
 XDOT =       -642
190773                 Wp   =          106
80800
 YDOT =      -6993
528299  meter/sec      RA   =          244
48962  deg
 ZDOT =       3033
752076                 TA   =          193
72521
                                          MA   =          193
75746
                                          Ha   =            229
585  n
mi
                                          Hp   =            221
738

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15736444
53                 X    =        -4756677
67
 Y    =       -5054460
20  feet           Y    =        -1594013
94  meter
 Z    =      -14998711
39                 Z    =        -4594810
62
 XDOT =      -2106
925107                 XDOT =        -578
675814
 YDOT =     -22944
646650  feet/sec       YDOT =       -7000
354996  meter/sec
 ZDOT =       9953
254841                 ZDOT =        3030
785863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10341472
73                 X    =         3152080
89
 Y    =      -12767452
17  feet           Y    =        -3891519
42  meter
 Z    =      -15105982
42                 Z    =        -4604303
44
 XDOT =      21259
174879                 XDOT =        6479
796503
 YDOT =       5471
727053  feet/sec       YDOT =        1667
782406  meter/sec
 ZDOT =       9939
694289                 ZDOT =        3029
618819


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   20335
51070959  
00016717  00000-0  10270-3 0  9039
2 25544  51
6444 245
4997 0001882  87
8343 272
3023 15
49106064 17797


Satellite: ISS
Catalog Number: 25544
Epoch time:      20335
51070959   =   yrday
fracday
Element set:     903
Inclination:       51
6444  deg
RA of node:       245
4997  deg
Eccentricity:     
0001882     
Arg of perigee:    87
8343  deg
Mean anomaly:     272
3023  deg
Mean motion:   15
49106064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1779
Checksum:              320


Coasting Arc #5 (Orbit 1780)
---------------------------------------

Vector Time (GMT): 2020/335/15:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4554317
77                 A    =         6793084
60  meter
 Y    =         -83390
50  meter          E    =           
0014778
 Z    =       -5053019
25                 I    =           51
27377
 XDOT =      -1892
728800                 Wp   =          101
92706
 YDOT =      -7182
504382  meter/sec      RA   =          243
86734  deg
 ZDOT =       1826
024068                 TA   =          185
88314
                                          MA   =          185
90051
                                          Ha   =            229
520  n
mi
                                          Hp   =            221
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14941987
43                 X    =        -4528501
63
 Y    =        -273590
87  feet           Y    =         -134175
13  meter
 Z    =      -16578147
13                 Z    =        -5075080
08
 XDOT =      -6209
740159                 XDOT =       -1821
141141
 YDOT =     -23564
646922  feet/sec       YDOT =       -7203
270202  meter/sec
 ZDOT =       5990
892610                 ZDOT =        1817
002681

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5937844
69                 X    =        -1809855
06
 Y    =      -13589951
47  feet           Y    =        -4142217
21  meter
 Z    =      -16680168
53                 Z    =        -5084115
37
 XDOT =      17815
739260                 XDOT =        5430
237326
 YDOT =     -15080
111375  feet/sec       YDOT =       -4596
417947  meter/sec
 ZDOT =       5949
331771                 ZDOT =        1813
356324


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   20335
63972992  
00016717  00000-0  10270-3 0  9041
2 25544  51
6442 244
8617 0001714  87
2733 272
8613 15
49114415 17810


Satellite: ISS
Catalog Number: 25544
Epoch time:      20335
63972992   =   yrday
fracday
Element set:     904
Inclination:       51
6442  deg
RA of node:       244
8617  deg
Eccentricity:     
0001714     
Arg of perigee:    87
2733  deg
Mean anomaly:     272
8613  deg
Mean motion:   15
49114415  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1781
Checksum:              315


Coasting Arc #6 (Orbit 1796)
---------------------------------------

Vector Time (GMT): 2020/336/15:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4556198
78                 A    =         6793076
34  meter
 Y    =        -248438
57  meter          E    =           
0006925
 Z    =        5027945
05                 I    =           51
29048
 XDOT =       2465
618514                 Wp   =           63
10147
 YDOT =       7007
856740  meter/sec      RA   =          238
89641  deg
 ZDOT =      -1882
923004                 TA   =           45
27869
                                          MA   =           45
22232
                                          Ha   =            229
279  n
mi
                                          Hp   =            221
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14948158
73                 X    =         4534215
00
 Y    =        -815087
17  feet           Y    =         -197611
53  meter
 Z    =       16495882
72                 Z    =         5050024
21
 XDOT =       8089
299586                 XDOT =        2396
217595
 YDOT =      22991
655972  feet/sec       YDOT =        7035
041284  meter/sec
 ZDOT =      -6177
568912                 ZDOT =       -1871
113347

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7155058
03                 X    =         2180861
69
 Y    =       13020646
33  feet           Y    =         3968693
00  meter
 Z    =       16598008
23                 Z    =         5059072
91
 XDOT =     -16257
003250                 XDOT =       -4955
134591
 YDOT =      16760
028334  feet/sec       YDOT =        5108
456636  meter/sec
 ZDOT =      -6123
091404                 ZDOT =       -1866
318260


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   20336
67190209  
00016717  00000-0  10270-3 0  9050
2 25544  51
6447 239
7558 0001558  89
2359 270
8969 15
49135839 17976


Satellite: ISS
Catalog Number: 25544
Epoch time:      20336
67190209   =   yrday
fracday
Element set:     905
Inclination:       51
6447  deg
RA of node:       239
7558  deg
Eccentricity:     
0001558     
Arg of perigee:    89
2359  deg
Mean anomaly:     270
8969  deg
Mean motion:   15
49135839  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1797
Checksum:              360


Coasting Arc #7 (Orbit 1811)
---------------------------------------

Vector Time (GMT): 2020/337/15:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4546124
68                 A    =         6793170
23  meter
 Y    =         595926
96  meter          E    =           
0014570
 Z    =       -5025802
65                 I    =           51
30782
 XDOT =      -3015
217508                 Wp   =          103
13498
 YDOT =      -6760
218755  meter/sec      RA   =          233
92504  deg
 ZDOT =       1927
351341                 TA   =          185
69099
                                          MA   =          185
70756
                                          Ha   =            229
484  n
mi
                                          Hp   =            221
772

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14915107
22                 X    =        -4528037
88
 Y    =        1955140
95  feet           Y    =          545190
83  meter
 Z    =      -16488853
82                 Z    =        -5047842
18
 XDOT =      -9892
445891                 XDOT =       -2948
760675
 YDOT =     -22179
195392  feet/sec       YDOT =       -6793
565791  meter/sec
 ZDOT =       6323
331171                 ZDOT =        1912
864804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8382260
02                 X    =        -2554912
85
 Y    =      -12355073
48  feet           Y    =        -3765826
40  meter
 Z    =      -16590816
02                 Z    =        -5056880
72
 XDOT =      14470
719666                 XDOT =        4410
675354
 YDOT =     -18212
424052  feet/sec       YDOT =       -5551
146851  meter/sec
 ZDOT =       6256
446202                 ZDOT =        1906
964803


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   20337
63956113  
00016717  00000-0  10270-3 0  9062
2 25544  51
6433 234
9674 0001659  92
1374 267
9966 15
49124646 18125


Satellite: ISS
Catalog Number: 25544
Epoch time:      20337
63956113   =   yrday
fracday
Element set:     906
Inclination:       51
6433  deg
RA of node:       234
9674  deg
Eccentricity:     
0001659     
Arg of perigee:    92
1374  deg
Mean anomaly:     267
9966  deg
Mean motion:   15
49124646  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1812
Checksum:              331


Coasting Arc #8 (Orbit 1827)
---------------------------------------

Vector Time (GMT): 2020/338/15:02:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4500732
30                 A    =         6793219
59  meter
 Y    =        -923630
38  meter          E    =           
0007135
 Z    =        4999111
28                 I    =           51
32822
 XDOT =       3546
761696                 Wp   =           64
99803
 YDOT =       6496
594374  meter/sec      RA   =          228
95685  deg
 ZDOT =      -1987
672212                 TA   =           44
43234
                                          MA   =           44
37512
                                          Ha   =            229
318  n
mi
                                          Hp   =            221
941

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14766182
08                 X    =         4486443
11
 Y    =       -3030283
40  feet           Y    =         -873380
61  meter
 Z    =       16401283
72                 Z    =         5020939
39
 XDOT =      11636
357270                 XDOT =        3483
506250
 YDOT =      21314
286004  feet/sec       YDOT =        6535
903425  meter/sec
 ZDOT =      -6521
234290                 ZDOT =       -1970
595959

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9477414
17                 X    =         2888715
84
 Y    =       11579205
88  feet           Y    =         3529341
95  meter
 Z    =       16502286
81                 Z    =         5029897
02
 XDOT =     -12625
799812                 XDOT =       -3848
343783
 YDOT =      19539
588000  feet/sec       YDOT =        5955
666422  meter/sec
 ZDOT =      -6442
340378                 ZDOT =       -1963
625347


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   20338
67172690  
00016717  00000-0  10270-3 0  9078
2 25544  51
6425 229
8616 0001630  96
3859 263
7477 15
49129333 18284


Satellite: ISS
Catalog Number: 25544
Epoch time:      20338
67172690   =   yrday
fracday
Element set:     907
Inclination:       51
6425  deg
RA of node:       229
8616  deg
Eccentricity:     
0001630     
Arg of perigee:    96
3859  deg
Mean anomaly:     263
7477  deg
Mean motion:   15
49129333  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1828
Checksum:              336


Coasting Arc #9 (Orbit 1830)
---------------------------------------

Vector Time (GMT): 2020/338/19:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1934943
89                 A    =         6792681
78  meter
 Y    =       -3996487
79  meter          E    =           
0006572
 Z    =        5136391
34                 I    =           51
32964
 XDOT =       5843
671631                 Wp   =          121
75458
 YDOT =       4733
407111  meter/sec      RA   =          228
04957  deg
 ZDOT =       1476
758518                 TA   =          313
92995
                                          MA   =          313
98417
                                          Ha   =            229
436  n
mi
                                          Hp   =            221
891

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6348241
11                 X    =         1954540
21
 Y    =      -13111836
57  feet           Y    =        -3974741
05  meter
 Z    =       16851677
62                 Z    =         5145837
60
 XDOT =      19172
151021                 XDOT =        5783
133632
 YDOT =      15529
550889  feet/sec       YDOT =        4798
416530  meter/sec
 ZDOT =       4845
008261                 ZDOT =        1504
998648

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4993945
56                 X    =         1522154
61
 Y    =      -13630987
63  feet           Y    =        -4154725
03  meter
 Z    =       16895447
50                 Z    =         5149732
40
 XDOT =      19498
059247                 XDOT =        5943
008459
 YDOT =      13330
067898  feet/sec       YDOT =        4063
004695  meter/sec
 ZDOT =       4975
586797                 ZDOT =        1516
558856


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   20338
86525937  
00016717  00000-0  10270-3 0  9086
2 25544  51
6416 228
9001 0001865 112
4839 247
6508 15
49137020 18312


Satellite: ISS
Catalog Number: 25544
Epoch time:      20338
86525937   =   yrday
fracday
Element set:     908
Inclination:       51
6416  deg
RA of node:       228
9001  deg
Eccentricity:     
0001865     
Arg of perigee:   112
4839  deg
Mean anomaly:     247
6508  deg
Mean motion:   15
49137020  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1831
Checksum:              312


Coasting Arc #10 (Orbit 1845)
---------------------------------------

Vector Time (GMT): 2020/339/19:32:30
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1643148
76                 A    =         6792656
53  meter
 Y    =        4114949
33  meter          E    =           
0015326
 Z    =       -5162155
41                 I    =           51
35341
 XDOT =      -6200
359549                 Wp   =           83
52163
 YDOT =      -4249
113643  meter/sec      RA   =          223
08326  deg
 ZDOT =      -1415
456789                 TA   =          172
78305
                                          MA   =          172
76096
                                          Ha   =            229
527  n
mi
                                          Hp   =            221
816

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5390907
99                 X    =        -1663966
39
 Y    =       13500489
93  feet           Y    =         4096458
78  meter
 Z    =      -16936205
42                 Z    =        -5170187
20
 XDOT =     -20342
386971                 XDOT =       -6145
508353
 YDOT =     -13940
661558  feet/sec       YDOT =       -4318
143624  meter/sec
 ZDOT =      -4643
887103                 ZDOT =       -1445
443160

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3764026
14                 X    =        -1147275
17
 Y    =       13996248
51  feet           Y    =         4266056
55  meter
 Z    =      -16973429
41                 Z    =        -5173501
28
 XDOT =     -20694
421917                 XDOT =       -6307
659800
 YDOT =     -11357
555674  feet/sec       YDOT =       -3461
782969  meter/sec
 ZDOT =      -4782
582596                 ZDOT =       -1457
731175


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   20339
83291284  
00016717  00000-0  10270-3 0  9090
2 25544  51
6419 224
1137 0001924 115
0672 245
0678 15
49129383 18462


Satellite: ISS
Catalog Number: 25544
Epoch time:      20339
83291284   =   yrday
fracday
Element set:     909
Inclination:       51
6419  deg
RA of node:       224
1137  deg
Eccentricity:     
0001924     
Arg of perigee:   115
0672  deg
Mean anomaly:     245
0678  deg
Mean motion:   15
49129383  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1846
Checksum:              316


Coasting Arc #11 (Orbit 1859)
---------------------------------------

Vector Time (GMT): 2020/340/16:39:40
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5311112
86                 A    =         6796280
46  meter
 Y    =         -77480
87  meter          E    =           
0011347
 Z    =        4231405
81                 I    =           51
38585
 XDOT =       2972
565521                 Wp   =           79
50865
 YDOT =       6072
444137  meter/sec      RA   =          218
67756  deg
 ZDOT =      -3609
568783                 TA   =           47
60618
                                          MA   =           47
51021
                                          Ha   =            229
381  n
mi
                                          Hp   =            221
960

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17424910
95                 X    =         5291030
79
 Y    =        -254202
32  feet           Y    =          -18201
00  meter
 Z    =       13882565
00                 Z    =         4257156
35
 XDOT =       9752
511552                 XDOT =        2921
973908
 YDOT =      19922
716986  feet/sec       YDOT =        6105
403074  meter/sec
 ZDOT =     -11842
417266                 ZDOT =       -3595
251335

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14159712
57                 X    =         4315880
39
 Y    =        9993581
19  feet           Y    =         3046043
55  meter
 Z    =       14001736
55                 Z    =         4267729
30
 XDOT =      -3045
488169                 XDOT =        -928
264794
 YDOT =      20861
395453  feet/sec       YDOT =        6358
553334  meter/sec
 ZDOT =     -11776
231784                 ZDOT =       -3589
395448


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   20340
73605221  
00016717  00000-0  10270-3 0  9103
2 25544  51
6399 219
6454 0001761 113
1882 246
9454 15
49107121 18605


Satellite: ISS
Catalog Number: 25544
Epoch time:      20340
73605221   =   yrday
fracday
Element set:     910
Inclination:       51
6399  deg
RA of node:       219
6454  deg
Eccentricity:     
0001761     
Arg of perigee:   113
1882  deg
Mean anomaly:     246
9454  deg
Mean motion:   15
49107121  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1860
Checksum:              292


Coasting Arc #12 (Orbit 1874)
---------------------------------------

Vector Time (GMT): 2020/341/16:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 997900
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2374972
40                 A    =         6791942
45  meter
 Y    =        3517896
21  meter          E    =           
0016701
 Z    =       -5316807
14                 I    =           51
39905
 XDOT =      -6350
352861                 Wp   =           92
87909
 YDOT =      -4261
990428  meter/sec      RA   =          213
77214  deg
 ZDOT =         15
900305                 TA   =          177
27789
                                          MA   =          177
26879
                                          Ha   =            229
562  n
mi
                                          Hp   =            221
741

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7791904
21                 X    =        -2388308
07
 Y    =       11541654
24  feet           Y    =         3491263
56  meter
 Z    =      -17443592
97                 Z    =        -5328375
84
 XDOT =     -20834
491015                 XDOT =       -6302
299256
 YDOT =     -13982
908228  feet/sec       YDOT =       -4332
735951  meter/sec
 ZDOT =         52
166354                 ZDOT =         -14
830956

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13111451
57                 X    =        -3996370
44
 Y    =        4487897
52  feet           Y    =         1367911
16  meter
 Z    =      -17497174
15                 Z    =        -5333138
68
 XDOT =      -7693
909275                 XDOT =       -2345
103547
 YDOT =     -22818
951060  feet/sec       YDOT =       -6955
216283  meter/sec
 ZDOT =        -90
031258                 ZDOT =         -27
441528


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   20341
70369966  
00016717  00000-0  10270-3 0  9115
2 25544  51
6404 214
8582 0002011 112
6759 247
4604 15
49133847 18750


Satellite: ISS
Catalog Number: 25544
Epoch time:      20341
70369966   =   yrday
fracday
Element set:     911
Inclination:       51
6404  deg
RA of node:       214
8582  deg
Eccentricity:     
0002011     
Arg of perigee:   112
6759  deg
Mean anomaly:     247
4604  deg
Mean motion:   15
49133847  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1875
Checksum:              309


Coasting Arc #13 (Orbit 1878)
---------------------------------------

Vector Time (GMT): 2020/341/22:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 997900
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1675194
29                 A    =         6792154
06  meter
 Y    =        3937260
93  meter          E    =           
0016036
 Z    =       -5288920
95                 I    =           51
40935
 XDOT =      -6680
883848                 Wp   =           88
51227
 YDOT =      -3671
698824  meter/sec      RA   =          212
50460  deg
 ZDOT =       -618
487696                 TA   =          175
55654
                                          MA   =          175
54228
                                          Ha   =            229
461  n
mi
                                          Hp   =            221
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5496044
26                 X    =        -1693406
88
 Y    =       12917522
74  feet           Y    =         3918426
40  meter
 Z    =      -17352102
85                 Z    =        -5297102
23
 XDOT =     -21918
910262                 XDOT =       -6636
325003
 YDOT =     -12046
255983  feet/sec       YDOT =       -3746
160058  meter/sec
 ZDOT =      -2029
159109                 ZDOT =        -650
832960

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7550983
06                 X    =         2301539
64
 Y    =       11778566
35  feet           Y    =         3590107
02  meter
 Z    =      -17390008
60                 Z    =        -5300474
62
 XDOT =     -21521
730072                 XDOT =       -6559
823326
 YDOT =      10586
166422  feet/sec       YDOT =        3226
663526  meter/sec
 ZDOT =      -2178
840120                 ZDOT =        -664
110469


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   20341
96173740  
00016717  00000-0  10270-3 0  9127
2 25544  51
6430 213
5837 0001672 117
6512 242
4808 15
49110800 18791


Satellite: ISS
Catalog Number: 25544
Epoch time:      20341
96173740   =   yrday
fracday
Element set:     912
Inclination:       51
6430  deg
RA of node:       213
5837  deg
Eccentricity:     
0001672     
Arg of perigee:   117
6512  deg
Mean anomaly:     242
4808  deg
Mean motion:   15
49110800  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1879
Checksum:              292


Coasting Arc #14 (Orbit 1894)
---------------------------------------

Vector Time (GMT): 2020/342/22:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 997900
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1382558
03                 A    =         6791985
10  meter
 Y    =       -4030973
81  meter          E    =           
0004607
 Z    =        5285374
89                 I    =           51
43864
 XDOT =       6972
253037                 Wp   =          117
58799
 YDOT =       3131
197757  meter/sec      RA   =          207
54368  deg
 ZDOT =        561
774077                 TA   =          327
01854
                                          MA   =          327
04727
                                          Ha   =            229
335  n
mi
                                          Hp   =            221
964

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4535951
55                 X    =         1401857
47
 Y    =      -13224979
69  feet           Y    =        -4015405
58  meter
 Z    =       17340468
81                 Z    =         5292137
37
 XDOT =      22874
845921                 XDOT =        6933
992060
 YDOT =      10272
958521  feet/sec       YDOT =        3208
952521  meter/sec
 ZDOT =       1843
090805                 ZDOT =         595
549954

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8541466
93                 X    =        -2603439
12
 Y    =      -11019553
16  feet           Y    =        -3358759
80  meter
 Z    =       17371804
56                 Z    =         5294926
03
 XDOT =      20439
549381                 XDOT =        6229
974651
 YDOT =     -12678
345778  feet/sec       YDOT =       -3864
359793  meter/sec
 ZDOT =       1999
424612                 ZDOT =         609
424622


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   20342
99389097  
00016717  00000-0  10270-3 0  9136
2 25544  51
6431 208
4777 0001701 122
0222 238
1094 15
49155956 18957


Satellite: ISS
Catalog Number: 25544
Epoch time:      20342
99389097   =   yrday
fracday
Element set:     913
Inclination:       51
6431  deg
RA of node:       208
4777  deg
Eccentricity:     
0001701     
Arg of perigee:   122
0222  deg
Mean anomaly:     238
1094  deg
Mean motion:   15
49155956  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1895
Checksum:              317


Coasting Arc #15 (Orbit 1909)
---------------------------------------

Vector Time (GMT): 2020/343/22:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 997900
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1100583
07                 A    =         6792100
01  meter
 Y    =        4116212
28  meter          E    =           
0016029
 Z    =       -5303360
88                 I    =           51
46859
 XDOT =      -7189
593985                 Wp   =           89
98453
 YDOT =      -2561
464397  meter/sec      RA   =          202
58428  deg
 ZDOT =       -497
363167                 TA   =          175
25471
                                          MA   =          175
23950
                                          Ha   =            229
433  n
mi
                                          Hp   =            221
990

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3610836
83                 X    =        -1120769
17
 Y    =       13504633
45  feet           Y    =         4103792
28  meter
 Z    =      -17399477
94                 Z    =        -5308755
84
 XDOT =     -23587
906774                 XDOT =       -7158
000648
 YDOT =      -8403
754583  feet/sec       YDOT =       -2641
686916  meter/sec
 ZDOT =      -1631
768919                 ZDOT =        -532
211047

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9465788
34                 X    =         2885172
29
 Y    =       10244092
02  feet           Y    =         3122399
25  meter
 Z    =      -17424480
75                 Z    =        -5310981
73
 XDOT =     -19079
014575                 XDOT =       -5815
283643
 YDOT =      14586
806197  feet/sec       YDOT =        4446
058529  meter/sec
 ZDOT =      -1793
092933                 ZDOT =        -546
534726


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   20343
96153475  
00016717  00000-0  10270-3 0  9144
2 25544  51
6425 203
6905 0001685 124
4038 235
7272 15
49113211 19109


Satellite: ISS
Catalog Number: 25544
Epoch time:      20343
96153475   =   yrday
fracday
Element set:     914
Inclination:       51
6425  deg
RA of node:       203
6905  deg
Eccentricity:     
0001685     
Arg of perigee:   124
4038  deg
Mean anomaly:     235
7272  deg
Mean motion:   15
49113211  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1910
Checksum:              287


Coasting Arc #16 (Orbit 1925)
---------------------------------------

Vector Time (GMT): 2020/344/22:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 997900
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         803219
93                 A    =         6791927
66  meter
 Y    =       -4167512
96  meter          E    =           
0004382
 Z    =        5299259
08                 I    =           51
50101
 XDOT =       7389
719997                 Wp   =          116
38223
 YDOT =       1983
063184  meter/sec      RA   =          197
62719  deg
 ZDOT =        437
283121                 TA   =          329
42397
                                          MA   =          329
44951
                                          Ha   =            229
327  n
mi
                                          Hp   =            221
982

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2635235
99                 X    =          824021
61
 Y    =      -13672942
79  feet           Y    =        -4158414
86  meter
 Z    =       17386020
60                 Z    =         5303211
06
 XDOT =      24244
488178                 XDOT =        7364
871471
 YDOT =       6506
112807  feet/sec       YDOT =        2065
561372  meter/sec
 ZDOT =       1434
655909                 ZDOT =         473
119633

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10297416
80                 X    =        -3138652
64
 Y    =       -9339145
97  feet           Y    =        -2846571
69  meter
 Z    =       17404341
56                 Z    =         5304843
31
 XDOT =      17612
614549                 XDOT =        5368
324915
 YDOT =     -16423
615704  feet/sec       YDOT =       -5005
918067  meter/sec
 ZDOT =       1600
582552                 ZDOT =         487
857562


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   20344
99368219  
00016717  00000-0  10270-3 0  9153
2 25544  51
6433 198
5841 0001667 124
6641 235
4666 15
49160425 19261


Satellite: ISS
Catalog Number: 25544
Epoch time:      20344
99368219   =   yrday
fracday
Element set:     915
Inclination:       51
6433  deg
RA of node:       198
5841  deg
Eccentricity:     
0001667     
Arg of perigee:   124
6641  deg
Mean anomaly:     235
4666  deg
Mean motion:   15
49160425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1926
Checksum:              328


Coasting Arc #17 (Orbit 1940)
---------------------------------------

Vector Time (GMT): 2020/345/22:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 997900
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -516913
98                 A    =         6792030
41  meter
 Y    =        4213022
41  meter          E    =           
0016153
 Z    =       -5316356
18                 I    =           51
53319
 XDOT =      -7512
344184                 Wp   =           90
82260
 YDOT =      -1387
551392  meter/sec      RA   =          192
67215  deg
 ZDOT =       -370
357290                 TA   =          175
63871
                                          MA   =          175
62462
                                          Ha   =            229
433  n
mi
                                          Hp   =            221
980

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1695912
00                 X    =         -538162
69
 Y    =       13822252
01  feet           Y    =         4207123
56  meter
 Z    =      -17442113
46                 Z    =        -5318918
42
 XDOT =     -24646
798504                 XDOT =       -7494
470821
 YDOT =      -4552
333963  feet/sec       YDOT =       -1471
459853  meter/sec
 ZDOT =      -1215
082973                 ZDOT =        -406
806519

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11065866
47                 X    =         3372876
10
 Y    =        8429861
80  feet           Y    =         2569421
88  meter
 Z    =      -17454000
10                 Z    =        -5319979
23
 XDOT =     -15909
179836                 XDOT =       -4849
118014
 YDOT =      18026
827507  feet/sec       YDOT =        5494
577024  meter/sec
 ZDOT =      -1383
872127                 ZDOT =        -421
804224


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   20345
96132018  
00016717  00000-0  10270-3 0  9168
2 25544  51
6428 193
7969 0001715 123
1273 237
0042 15
49123351 19412


Satellite: ISS
Catalog Number: 25544
Epoch time:      20345
96132018   =   yrday
fracday
Element set:     916
Inclination:       51
6428  deg
RA of node:       193
7969  deg
Eccentricity:     
0001715     
Arg of perigee:   123
1273  deg
Mean anomaly:     237
0042  deg
Mean motion:   15
49123351  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1941
Checksum:              294


Coasting Arc #18 (Orbit 1956)
---------------------------------------

Vector Time (GMT): 2020/346/22:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 997900
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         219636
00                 A    =         6791898
99  meter
 Y    =       -4223551
46  meter          E    =           
0004290
 Z    =        5311133
35                 I    =           51
56541
 XDOT =       7617
077211                 Wp   =          114
46826
 YDOT =        785
891094  meter/sec      RA   =          187
71996  deg
 ZDOT =        308
030694                 TA   =          332
57918
                                          MA   =          332
60182
                                          Ha   =            229
376  n
mi
                                          Hp   =            221
967

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         720590
55                 X    =          241049
87
 Y    =      -13856796
14  feet           Y    =        -4220976
20  meter
 Z    =       17424978
17                 Z    =         5312251
81
 XDOT =      24990
410797                 XDOT =        7606
226759
 YDOT =       2578
382855  feet/sec       YDOT =         871
010019  meter/sec
 ZDOT =       1010
599390                 ZDOT =         345
005778

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11723966
51                 X    =        -3573464
99
 Y    =       -7409272
85  feet           Y    =        -2258346
37  meter
 Z    =       17430180
70                 Z    =         5312719
08
 XDOT =      14115
895705                 XDOT =        4302
525011
 YDOT =     -19540
892305  feet/sec       YDOT =       -5956
063975  meter/sec
 ZDOT =       1181
851566                 ZDOT =         360
228357


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   20346
99346381  
00016717  00000-0  10270-3 0  9173
2 25544  51
6418 188
6910 0001751 125
8891 234
2421 15
49158071 19579


Satellite: ISS
Catalog Number: 25544
Epoch time:      20346
99346381   =   yrday
fracday
Element set:     917
Inclination:       51
6418  deg
RA of node:       188
6910  deg
Eccentricity:     
0001751     
Arg of perigee:   125
8891  deg
Mean anomaly:     234
2421  deg
Mean motion:   15
49158071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1957
Checksum:              326
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