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

 
Date: December 12th 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) : 15144 822 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


342/18:30:00 000 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

345/02:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 5
000/00:00:00 000 0 0 0 0 221 8

351/15:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 0

354/02:00:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 222 1

355/04:48:45 000 0 0 -0 0 0 1
N/A 0 0 -0 1 229 0
000/00:07:30 000 0 1 -0 0 222 1

Coasting Arc #1 (Orbit 1887)
---------------------------------------

Vector Time (GMT): 2020/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966705
0

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5108923
51                 A    =         6795588
38  meter
 Y    =       -1070812
26  meter          E    =           
0010852
 Z    =        4343671
90                 I    =           51
43838
 XDOT =       4087
135900                 Wp   =           75
35892
 YDOT =       5493
574408  meter/sec      RA   =          209
71973  deg
 ZDOT =      -3442
984913                 TA   =           49
75429
                                          MA   =           49
65941
                                          Ha   =            229
176  n
mi
                                          Hp   =            221
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16761560
08                 X    =         5099418
87
 Y    =       -3513163
57  feet           Y    =        -1013734
14  meter
 Z    =       14250892
05                 Z    =         4368465
89
 XDOT =      13409
238518                 XDOT =        4042
125385
 YDOT =      18023
538085  feet/sec       YDOT =        5539
028338  meter/sec
 ZDOT =     -11295
882262                 ZDOT =       -3423
240016

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -679110
63                 X    =         -206992
92
 Y    =       17016062
97  feet           Y    =         5186495
99  meter
 Z    =       14365672
58                 Z    =         4378657
00
 XDOT =     -19538
058988                 XDOT =       -5955
200380
 YDOT =       8706
820686  feet/sec       YDOT =        2653
838945  meter/sec
 ZDOT =     -11204
528769                 ZDOT =       -3415
140369


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
54220293  
00016717  00000-0  10270-3 0  9005
2 25544  51
6435 210
7131 0001528 100
2176 259
9147 15
49205090 18881


Satellite: ISS
Catalog Number: 25544
Epoch time:      20342
54220293   =   yrday
fracday
Element set:     900
Inclination:       51
6435  deg
RA of node:       210
7131  deg
Eccentricity:     
0001528     
Arg of perigee:   100
2176  deg
Mean anomaly:     259
9147  deg
Mean motion:   15
49205090  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1888
Checksum:              280


Coasting Arc #2 (Orbit 1891)
---------------------------------------

Vector Time (GMT): 2020/342/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5156829
46                 A    =         6802840
12  meter
 Y    =        4163294
09  meter          E    =           
0010129
 Z    =       -1517627
51                 I    =           51
46805
 XDOT =      -4092
617015                 Wp   =          138
43265
 YDOT =       2986
379762  meter/sec      RA   =          208
40849  deg
 ZDOT =      -5743
522811                 TA   =           58
14626
                                          MA   =           58
04771
                                          Ha   =            229
475  n
mi
                                          Hp   =            221
858

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16918731
83                 X    =         5117262
76
 Y    =       13659101
35  feet           Y    =         4220740
36  meter
 Z    =       -4979092
89                 Z    =        -1492673
36
 XDOT =     -13427
221177                 XDOT =       -4097
808660
 YDOT =       9797
833866  feet/sec       YDOT =        2940
584642  meter/sec
 ZDOT =     -18843
578775                 ZDOT =       -5763
415527

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15318460
90                 X    =         4669066
88
 Y    =       15469194
18  feet           Y    =         4715010
39  meter
 Z    =       -4863608
68                 Z    =        -1482427
92
 XDOT =     -13181
939054                 XDOT =       -4017
855024
 YDOT =       7131
154804  feet/sec       YDOT =        2173
575984  meter/sec
 ZDOT =     -18935
688733                 ZDOT =       -5771
597926


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
80023906  
00016717  00000-0  10270-3 0  9017
2 25544  51
6415 209
4311 0001930 119
3170 240
8173 15
49173981 18922


Satellite: ISS
Catalog Number: 25544
Epoch time:      20342
80023906   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       209
4311  deg
Eccentricity:     
0001930     
Arg of perigee:   119
3170  deg
Mean anomaly:     240
8173  deg
Mean motion:   15
49173981  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1892
Checksum:              283


Coasting Arc #3 (Orbit 1907)
---------------------------------------

Vector Time (GMT): 2020/343/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5468585
49                 A    =         6802788
13  meter
 Y    =       -3723007
11  meter          E    =           
0014831
 Z    =        1558037
50                 I    =           51
49957
 XDOT =       3880
833509                 Wp   =           69
22590
 YDOT =      -3285
693811  meter/sec      RA   =          203
44966  deg
 ZDOT =       5730
956608                 TA   =          307
80679
                                          MA   =          307
94097
                                          Ha   =            229
430  n
mi
                                          Hp   =            221
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17941553
46                 X    =        -5434115
35
 Y    =      -12214590
27  feet           Y    =        -3783968
14  meter
 Z    =        5111671
60                 Z    =         1531556
57
 XDOT =      12732
393403                 XDOT =        3889
448861
 YDOT =     -10779
835337  feet/sec       YDOT =       -3242
247794  meter/sec
 ZDOT =      18802
351075                 ZDOT =        5749
828952

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16738233
19                 X    =        -5101813
48
 Y    =      -13862366
97  feet           Y    =        -4225249
45  meter
 Z    =        4989095
51                 Z    =         1520676
31
 XDOT =      12556
733756                 XDOT =        3827
292449
 YDOT =      -8315
938581  feet/sec       YDOT =       -2534
698080  meter/sec
 ZDOT =      18889
745478                 ZDOT =        5757
594422


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
83237316  
00016717  00000-0  10270-3 0  9024
2 25544  51
6428 204
3248 0001944 125
3660 234
7672 15
49177698 19088


Satellite: ISS
Catalog Number: 25544
Epoch time:      20343
83237316   =   yrday
fracday
Element set:     902
Inclination:       51
6428  deg
RA of node:       204
3248  deg
Eccentricity:     
0001944     
Arg of perigee:   125
3660  deg
Mean anomaly:     234
7672  deg
Mean motion:   15
49177698  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1908
Checksum:              316


Coasting Arc #4 (Orbit 1922)
---------------------------------------

Vector Time (GMT): 2020/344/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5720025
21                 A    =         6802666
08  meter
 Y    =        3288585
51  meter          E    =           
0009776
 Z    =       -1641756
18                 I    =           51
53130
 XDOT =      -3672
153144                 Wp   =          139
53146
 YDOT =       3551
982751  meter/sec      RA   =          198
49295  deg
 ZDOT =      -5705
573257                 TA   =           58
43158
                                          MA   =           58
33617
                                          Ha   =            229
422  n
mi
                                          Hp   =            221
915

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18766486
90                 X    =         5690800
90
 Y    =       10789322
53  feet           Y    =         3352387
65  meter
 Z    =       -5386339
18                 Z    =        -1614041
03
 XDOT =     -12047
746534                 XDOT =       -3683
884911
 YDOT =      11653
486715  feet/sec       YDOT =        3510
852914  meter/sec
 ZDOT =     -18719
072364                 ZDOT =       -5723
439537

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17909109
06                 X    =         5458696
44
 Y    =       12215568
78  feet           Y    =         3723305
36  meter
 Z    =       -5258027
47                 Z    =        -1602646
77
 XDOT =     -11896
563758                 XDOT =       -3626
072633
 YDOT =       9386
628723  feet/sec       YDOT =        2861
044435  meter/sec
 ZDOT =     -18801
817159                 ZDOT =       -5730
793870


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
79999646  
00016717  00000-0  10270-3 0  9032
2 25544  51
6433 199
5374 0001876 126
0787 234
0537 15
49180037 19232


Satellite: ISS
Catalog Number: 25544
Epoch time:      20344
79999646   =   yrday
fracday
Element set:     903
Inclination:       51
6433  deg
RA of node:       199
5374  deg
Eccentricity:     
0001876     
Arg of perigee:   126
0787  deg
Mean anomaly:     234
0537  deg
Mean motion:   15
49180037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1923
Checksum:              338


Coasting Arc #5 (Orbit 1927)
---------------------------------------

Vector Time (GMT): 2020/345/02:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4029163
66                 A    =         6794248
70  meter
 Y    =        2731794
15  meter          E    =           
0012963
 Z    =       -4752238
12                 I    =           51
51221
 XDOT =      -5915
661283                 Wp   =          109
62033
 YDOT =      -4027
329375  meter/sec      RA   =          196
77557  deg
 ZDOT =       2702
262724                 TA   =          187
19777
                                          MA   =          187
21640
                                          Ha   =            229
467  n
mi
                                          Hp   =            221
771

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13219040
88                 X    =        -4036328
06
 Y    =        8962579
24  feet           Y    =         2686697
45  meter
 Z    =      -15591332
42                 Z    =        -4771827
62
 XDOT =     -19408
337543                 XDOT =       -5883
312981
 YDOT =     -13213
022883  feet/sec       YDOT =       -4093
301881  meter/sec
 ZDOT =       8865
691352                 ZDOT =        2673
604722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14117644
25                 X    =         4303057
97
 Y    =        7275010
37  feet           Y    =         2217423
16  meter
 Z    =      -15682055
36                 Z    =        -4779890
47
 XDOT =      -1838
293218                 XDOT =        -560
311773
 YDOT =      22379
740029  feet/sec       YDOT =        6821
344761  meter/sec
 ZDOT =       8733
011463                 ZDOT =        2661
821894


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
12253619  
00016717  00000-0  10270-3 0  9044
2 25544  51
6414 197
9457 0001809 112
3269 247
8072 15
49146263 19288


Satellite: ISS
Catalog Number: 25544
Epoch time:      20345
12253619   =   yrday
fracday
Element set:     904
Inclination:       51
6414  deg
RA of node:       197
9457  deg
Eccentricity:     
0001809     
Arg of perigee:   112
3269  deg
Mean anomaly:     247
8072  deg
Mean motion:   15
49146263  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1928
Checksum:              316


Coasting Arc #6 (Orbit 1943)
---------------------------------------

Vector Time (GMT): 2020/346/02:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3848020
81                 A    =         6794288
48  meter
 Y    =       -3017202
31  meter          E    =           
0008863
 Z    =        4711104
74                 I    =           51
54398
 XDOT =       6196
556191                 Wp   =           71
83228
 YDOT =       3552
056674  meter/sec      RA   =          191
82065  deg
 ZDOT =      -2779
425119                 TA   =           45
79179
                                          MA   =           45
71903
                                          Ha   =            229
259  n
mi
                                          Hp   =            221
904

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12624740
18                 X    =         3858589
92
 Y    =       -9898957
70  feet           Y    =        -2974112
31  meter
 Z    =       15456380
40                 Z    =         4729822
58
 XDOT =      20329
908763                 XDOT =        6169
876517
 YDOT =      11653
729247  feet/sec       YDOT =        3621
202094  meter/sec
 ZDOT =      -9118
848817                 ZDOT =       -2749
388733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14765701
14                 X    =        -4500585
71
 Y    =       -6054739
52  feet           Y    =        -1845484
61  meter
 Z    =       15543079
57                 Z    =         4737530
65
 XDOT =       -287
458029                 XDOT =         -87
617207
 YDOT =     -22409
606351  feet/sec       YDOT =       -6830
448016  meter/sec
 ZDOT =      -8979
764973                 ZDOT =       -2737
032364


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
15466341  
00016717  00000-0  10270-3 0  9057
2 25544  51
6399 192
8389 0001670 115
7647 244
3676 15
49176453 19445


Satellite: ISS
Catalog Number: 25544
Epoch time:      20346
15466341   =   yrday
fracday
Element set:     905
Inclination:       51
6399  deg
RA of node:       192
8389  deg
Eccentricity:     
0001670     
Arg of perigee:   115
7647  deg
Mean anomaly:     244
3676  deg
Mean motion:   15
49176453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1944
Checksum:              336


Coasting Arc #7 (Orbit 1958)
---------------------------------------

Vector Time (GMT): 2020/347/02:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3642360
42                 A    =         6794474
03  meter
 Y    =        3312261
41  meter          E    =           
0012465
 Z    =       -4694805
73                 I    =           51
57732
 XDOT =      -6420
459446                 Wp   =          110
81216
 YDOT =      -3040
645006  meter/sec      RA   =          186
86851  deg
 ZDOT =       2837
737414                 TA   =          187
43946
                                          MA   =          187
45798
                                          Ha   =            229
402  n
mi
                                          Hp   =            221
842

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11950001
39                 X    =        -3656323
40
 Y    =       10866999
39  feet           Y    =         3271452
40  meter
 Z    =      -15402905
93                 Z    =        -4712532
69
 XDOT =     -21064
499496                 XDOT =       -6399
765163
 YDOT =      -9975
869441  feet/sec       YDOT =       -3112
327815  meter/sec
 ZDOT =       9310
162118                 ZDOT =        2806
598761

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15362183
87                 X    =         4682393
64
 Y    =        4728724
46  feet           Y    =         1441315
22  meter
 Z    =      -15485031
21                 Z    =        -4719837
51
 XDOT =       2414
516518                 XDOT =         735
944635
 YDOT =      22152
329781  feet/sec       YDOT =        6752
030117  meter/sec
 ZDOT =       9165
950564                 ZDOT =        2793
781732


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   20347
12228213  
00016717  00000-0  10270-3 0  9060
2 25544  51
6394 188
0519 0001694 117
3641 242
7681 15
49150862 19590


Satellite: ISS
Catalog Number: 25544
Epoch time:      20347
12228213   =   yrday
fracday
Element set:     906
Inclination:       51
6394  deg
RA of node:       188
0519  deg
Eccentricity:     
0001694     
Arg of perigee:   117
3641  deg
Mean anomaly:     242
7681  deg
Mean motion:   15
49150862  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1959
Checksum:              314


Coasting Arc #8 (Orbit 1974)
---------------------------------------

Vector Time (GMT): 2020/348/02:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3421139
81                 A    =         6794518
44  meter
 Y    =       -3572847
87  meter          E    =           
0009040
 Z    =        4651650
74                 I    =           51
61145
 XDOT =       6619
742787                 Wp   =           73
25237
 YDOT =       2533
030785  meter/sec      RA   =          181
91783  deg
 ZDOT =      -2915
785173                 TA   =           45
82177
                                          MA   =           45
74752
                                          Ha   =            229
214  n
mi
                                          Hp   =            221
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11224211
99                 X    =         3438242
84
 Y    =      -11721941
85  feet           Y    =        -3534495
28  meter
 Z    =       15261321
34                 Z    =         4668310
56
 XDOT =      21718
316230                 XDOT =        6605
089086
 YDOT =       8310
468456  feet/sec       YDOT =        2606
975991  meter/sec
 ZDOT =      -9566
224321                 ZDOT =       -2883
663824

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15794439
23                 X    =        -4814145
08
 Y    =       -3400037
54  feet           Y    =        -1036331
44  meter
 Z    =       15338520
74                 Z    =         4675181
12
 XDOT =      -4481
022243                 XDOT =       -1365
815580
 YDOT =     -21775
411776  feet/sec       YDOT =       -6637
145509  meter/sec
 ZDOT =      -9417
434668                 ZDOT =       -2870
434087


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   20348
15440519  
00016717  00000-0  10270-3 0  9070
2 25544  51
6393 182
9447 0001589 122
3331 237
7973 15
49182702 19751


Satellite: ISS
Catalog Number: 25544
Epoch time:      20348
15440519   =   yrday
fracday
Element set:     907
Inclination:       51
6393  deg
RA of node:       182
9447  deg
Eccentricity:     
0001589     
Arg of perigee:   122
3331  deg
Mean anomaly:     237
7973  deg
Mean motion:   15
49182702  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1975
Checksum:              325


Coasting Arc #9 (Orbit 1989)
---------------------------------------

Vector Time (GMT): 2020/349/02:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3174944
83                 A    =         6794686
13  meter
 Y    =        3838814
82  meter          E    =           
0011951
 Z    =       -4632529
86                 I    =           51
64632
 XDOT =      -6757
821597                 Wp   =          111
75217
 YDOT =      -2000
262238  meter/sec      RA   =          176
96966  deg
 ZDOT =       2975
850359                 TA   =          187
97666
                                          MA   =          187
99568
                                          Ha   =            229
328  n
mi
                                          Hp   =            221
889

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10416485
65                 X    =        -3195133
26
 Y    =       12594536
80  feet           Y    =         3803198
21  meter
 Z    =      -15198588
77                 Z    =        -4648001
03
 XDOT =     -22171
330699                 XDOT =       -6749
406916
 YDOT =      -6562
540151  feet/sec       YDOT =       -2075
786504  meter/sec
 ZDOT =       9763
288579                 ZDOT =        2943
043286

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16156233
92                 X    =         4924420
10
 Y    =        1979061
87  feet           Y    =          603218
06  meter
 Z    =      -15270299
63                 Z    =        -4654387
33
 XDOT =       6491
145936                 XDOT =        1978
501281
 YDOT =      21122
036076  feet/sec       YDOT =        6437
996596  meter/sec
 ZDOT =       9611
291559                 ZDOT =        2929
521667


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   20349
12201745  
00016717  00000-0  10270-3 0  9085
2 25544  51
6398 178
1570 0001592 121
2688 238
8618 15
49166134 19903


Satellite: ISS
Catalog Number: 25544
Epoch time:      20349
12201745   =   yrday
fracday
Element set:     908
Inclination:       51
6398  deg
RA of node:       178
1570  deg
Eccentricity:     
0001592     
Arg of perigee:   121
2688  deg
Mean anomaly:     238
8618  deg
Mean motion:   15
49166134  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1990
Checksum:              322


Coasting Arc #10 (Orbit 2005)
---------------------------------------

Vector Time (GMT): 2020/350/02:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2918180
82                 A    =         6794759
54  meter
 Y    =       -4069097
04  meter          E    =           
0009325
 Z    =        4586518
63                 I    =           51
68014
 XDOT =       6872
014801                 Wp   =           74
06207
 YDOT =       1475
555945  meter/sec      RA   =          172
02374  deg
 ZDOT =      -3055
566193                 TA   =           46
51828
                                          MA   =           46
44078
                                          Ha   =            229
178  n
mi
                                          Hp   =            221
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9574084
05                 X    =         2941187
06
 Y    =      -13350055
90  feet           Y    =        -4036336
04  meter
 Z    =       15047633
31                 Z    =         4600749
20
 XDOT =      22545
980318                 XDOT =        6869
846182
 YDOT =       4841
062813  feet/sec       YDOT =        1552
392177  meter/sec
 ZDOT =     -10024
823468                 ZDOT =       -3022
189520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16357181
38                 X    =        -4985668
89
 Y    =        -582810
12  feet           Y    =         -177640
53  meter
 Z    =       15113612
93                 Z    =         4606629
22
 XDOT =      -8417
348632                 XDOT =       -2565
607863
 YDOT =     -20364
028207  feet/sec       YDOT =       -6206
955797  meter/sec
 ZDOT =      -9870
153284                 ZDOT =       -3008
422721


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   20350
15413456  
00016717  00000-0  10270-3 0  9095
2 25544  51
6393 173
0499 0001488 123
9180 236
2111 15
49192299 20062


Satellite: ISS
Catalog Number: 25544
Epoch time:      20350
15413456   =   yrday
fracday
Element set:     909
Inclination:       51
6393  deg
RA of node:       173
0499  deg
Eccentricity:     
0001488     
Arg of perigee:   123
9180  deg
Mean anomaly:     236
2111  deg
Mean motion:   15
49192299  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2006
Checksum:              301


Coasting Arc #11 (Orbit 2020)
---------------------------------------

Vector Time (GMT): 2020/351/02:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 995365
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2633430
42                 A    =         6794939
87  meter
 Y    =        4301154
12  meter          E    =           
0011353
 Z    =       -4565095
87                 I    =           51
71408
 XDOT =      -6924
505733                 Wp   =          112
86924
 YDOT =       -934
786877  meter/sec      RA   =          167
08034  deg
 ZDOT =       3115
631698                 TA   =          188
37527
                                          MA   =          188
39424
                                          Ha   =            229
242  n
mi
                                          Hp   =            221
977

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8639863
60                 X    =        -2659156
97
 Y    =       14111398
02  feet           Y    =         4271562
18  meter
 Z    =      -14977348
65                 Z    =        -4577949
72
 XDOT =     -22718
194661                 XDOT =       -6928
671923
 YDOT =      -3066
886080  feet/sec       YDOT =       -1012
245525  meter/sec
 ZDOT =      10221
888773                 ZDOT =        3081
984979

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16467582
25                 X    =         5019319
07
 Y    =        -899026
44  feet           Y    =         -274023
26  meter
 Z    =      -15036962
99                 Z    =        -4583266
32
 XDOT =      10242
340216                 XDOT =        3121
865298
 YDOT =      19352
350055  feet/sec       YDOT =        5898
596297  meter/sec
 ZDOT =      10065
931853                 ZDOT =        3068
096029


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   20351
12174323  
00016717  00000-0  10270-3 0  9102
2 25544  51
6395 168
2624 0001451 127
9742 232
1540 15
49173412 20212


Satellite: ISS
Catalog Number: 25544
Epoch time:      20351
12174323   =   yrday
fracday
Element set:     910
Inclination:       51
6395  deg
RA of node:       168
2624  deg
Eccentricity:     
0001451     
Arg of perigee:   127
9742  deg
Mean anomaly:     232
1540  deg
Mean motion:   15
49173412  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2021
Checksum:              268


Coasting Arc #12 (Orbit 2029)
---------------------------------------

Vector Time (GMT): 2020/351/15:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3810196
96                 A    =         6793929
32  meter
 Y    =       -2888781
95  meter          E    =           
0009051
 Z    =        4822101
91                 I    =           51
73117
 XDOT =       6138
380964                 Wp   =          124
49175
 YDOT =      -3805
064756  meter/sec      RA   =          164
45927  deg
 ZDOT =       2562
321021                 TA   =          300
25666
                                          MA   =          300
34622
                                          Ha   =            229
275  n
mi
                                          Hp   =            222
029

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12500646
20                 X    =        -3801033
40
 Y    =       -9477631
07  feet           Y    =        -2931339
90  meter
 Z    =       15820544
31                 Z    =         4803615
33
 XDOT =      20139
045156                 XDOT =        6168
027928
 YDOT =     -12483
808255  feet/sec       YDOT =       -3736
255648  meter/sec
 ZDOT =       8406
565030                 ZDOT =        2592
210037

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3185287
30                 X    =         -970875
57
 Y    =      -15448275
43  feet           Y    =        -4708634
35  meter
 Z    =       15734865
73                 Z    =         4795987
07
 XDOT =      22190
380464                 XDOT =        6763
627965
 YDOT =       4156
569516  feet/sec       YDOT =        1266
922389  meter/sec
 ZDOT =       8545
154134                 ZDOT =        2604
562980


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   20351
70230612  
00016717  00000-0  10270-3 0  9111
2 25544  51
6420 165
3859 0001800 146
7571 213
3692 15
49220022 20305


Satellite: ISS
Catalog Number: 25544
Epoch time:      20351
70230612   =   yrday
fracday
Element set:     911
Inclination:       51
6420  deg
RA of node:       165
3859  deg
Eccentricity:     
0001800     
Arg of perigee:   146
7571  deg
Mean anomaly:     213
3692  deg
Mean motion:   15
49220022  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2030
Checksum:              260


Coasting Arc #13 (Orbit 2044)
---------------------------------------

Vector Time (GMT): 2020/352/15:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3968629
87                 A    =         6793867
43  meter
 Y    =        2611815
56  meter          E    =           
0012100
 Z    =       -4867546
15                 I    =           51
76423
 XDOT =      -5845
465352                 Wp   =           80
60779
 YDOT =       4268
343615  meter/sec      RA   =          159
51950  deg
 ZDOT =      -2478
996296                 TA   =          165
04700
                                          MA   =          165
01119
                                          Ha   =            229
201  n
mi
                                          Hp   =            222
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13020439
21                 X    =         3962772
30
 Y    =        8568948
68  feet           Y    =         2656163
62  meter
 Z    =      -15969639
59                 Z    =        -4848282
13
 XDOT =     -19178
035933                 XDOT =       -5880
719403
 YDOT =      14003
752018  feet/sec       YDOT =        4202
778684  meter/sec
 ZDOT =      -8133
189949                 ZDOT =       -2507
475958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4436320
97                 X    =         1352190
63
 Y    =       15037354
02  feet           Y    =         4583385
51  meter
 Z    =      -15880338
40                 Z    =        -4840327
14
 XDOT =     -22540
205917                 XDOT =       -6870
254764
 YDOT =      -2067
162693  feet/sec       YDOT =        -630
071189  meter/sec
 ZDOT =      -8265
273427                 ZDOT =       -2519
255340


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   20352
66991102  
00016717  00000-0  10270-3 0  9126
2 25544  51
6432 160
5988 0001751 147
7067 212
4191 15
49191790 20453


Satellite: ISS
Catalog Number: 25544
Epoch time:      20352
66991102   =   yrday
fracday
Element set:     912
Inclination:       51
6432  deg
RA of node:       160
5988  deg
Eccentricity:     
0001751     
Arg of perigee:   147
7067  deg
Mean anomaly:     212
4191  deg
Mean motion:   15
49191790  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2045
Checksum:              303


Coasting Arc #14 (Orbit 2060)
---------------------------------------

Vector Time (GMT): 2020/353/15:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4113539
66                 A    =         6793646
60  meter
 Y    =       -2303822
90  meter          E    =           
0008605
 Z    =        4887188
57                 I    =           51
79562
 XDOT =       5525
628169                 Wp   =          125
94812
 YDOT =      -4729
205035  meter/sec      RA   =          154
58157  deg
 ZDOT =       2413
662792                 TA   =          300
37973
                                          MA   =          300
46477
                                          Ha   =            229
248  n
mi
                                          Hp   =            222
040

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13495865
03                 X    =        -4111210
76
 Y    =       -7558474
07  feet           Y    =        -2349811
06  meter
 Z    =       16034083
22                 Z    =         4867212
20
 XDOT =      18128
701342                 XDOT =        5566
376854
 YDOT =     -15515
764552  feet/sec       YDOT =       -4667
185962  meter/sec
 ZDOT =       7918
841182                 ZDOT =        2440
602164

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5703835
94                 X    =        -1738529
19
 Y    =      -14480911
03  feet           Y    =        -4413781
68  meter
 Z    =       15941461
65                 Z    =         4858957
51
 XDOT =      22758
892464                 XDOT =        6936
910423
 YDOT =        -80
609681  feet/sec       YDOT =         -24
569831  meter/sec
 ZDOT =       8043
807164                 ZDOT =        2451
752423


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   20353
70201804  
00016717  00000-0  10270-3 0  9136
2 25544  51
6436 155
4920 0001732 147
9148 212
2108 15
49228764 20613


Satellite: ISS
Catalog Number: 25544
Epoch time:      20353
70201804   =   yrday
fracday
Element set:     913
Inclination:       51
6436  deg
RA of node:       155
4920  deg
Eccentricity:     
0001732     
Arg of perigee:   147
9148  deg
Mean anomaly:     212
2108  deg
Mean motion:   15
49228764  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2061
Checksum:              283


Coasting Arc #15 (Orbit 2066)
---------------------------------------

Vector Time (GMT): 2020/354/02:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4125144
52                 A    =         6800387
45  meter
 Y    =        4631899
66  meter          E    =           
0005240
 Z    =       -2790623
04                 I    =           51
82848
 XDOT =      -5407
710911                 Wp   =           74
88853
 YDOT =      -1728
029281  meter/sec      RA   =          152
40114  deg
 ZDOT =       5134
950907                 TA   =          253
65144
                                          MA   =          253
70906
                                          Ha   =            229
140  n
mi
                                          Hp   =            222
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13533938
70                 X    =        -4163078
16
 Y    =       15196521
19  feet           Y    =         4585557
56  meter
 Z    =       -9155587
42                 Z    =        -2810752
72
 XDOT =     -17741
833699                 XDOT =       -5412
927994
 YDOT =      -5669
387404  feet/sec       YDOT =       -1788
531970  meter/sec
 ZDOT =      16846
951796                 ZDOT =        5108
669812

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19675578
98                 X    =         5997116
47
 Y    =        5025385
82  feet           Y    =         1531737
60  meter
 Z    =       -9248979
58                 Z    =        -2819088
98
 XDOT =       3496
211378                 XDOT =        1065
645228
 YDOT =      17037
124592  feet/sec       YDOT =        5192
915576  meter/sec
 ZDOT =      16725
079998                 ZDOT =        5097
804384


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   20354
08905915  
00016717  00000-0  10270-3 0  9143
2 25544  51
6409 153
5805 0001304 133
2526 226
8733 15
49184769 20674


Satellite: ISS
Catalog Number: 25544
Epoch time:      20354
08905915   =   yrday
fracday
Element set:     914
Inclination:       51
6409  deg
RA of node:       153
5805  deg
Eccentricity:     
0001304     
Arg of perigee:   133
2526  deg
Mean anomaly:     226
8733  deg
Mean motion:   15
49184769  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2067
Checksum:              311


Coasting Arc #16 (Orbit 2082)
---------------------------------------

Vector Time (GMT): 2020/355/02:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3791106
87                 A    =         6800522
47  meter
 Y    =       -4942894
03  meter          E    =           
0014518
 Z    =        2710585
32                 I    =           51
85929
 XDOT =       5475
741074                 Wp   =          104
59835
 YDOT =       1342
248576  meter/sec      RA   =          147
46719  deg
 ZDOT =      -5191
207247                 TA   =           44
91701
                                          MA   =           44
79963
                                          Ha   =            229
074  n
mi
                                          Hp   =            222
072

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12438014
67                 X    =         3832931
73
 Y    =      -16216843
94  feet           Y    =        -4900265
56  meter
 Z    =        8892996
45                 Z    =         2729101
91
 XDOT =      17965
029769                 XDOT =        5485
540301
 YDOT =       4403
702678  feet/sec       YDOT =        1403
537557  meter/sec
 ZDOT =     -17031
519838                 ZDOT =       -5164
584606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20140973
95                 X    =        -6138968
86
 Y    =       -3239709
95  feet           Y    =         -987463
59  meter
 Z    =        8978923
66                 Z    =         2736775
93
 XDOT =      -4904
706458                 XDOT =       -1494
954528
 YDOT =     -16546
041971  feet/sec       YDOT =       -5043
233593  meter/sec
 ZDOT =     -16908
044700                 ZDOT =       -5153
572024


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   20355
12116507  
00016717  00000-0  10270-3 0  9151
2 25544  51
6416 148
4739 0001303 137
4587 222
6665 15
49205563 20835


Satellite: ISS
Catalog Number: 25544
Epoch time:      20355
12116507   =   yrday
fracday
Element set:     915
Inclination:       51
6416  deg
RA of node:       148
4739  deg
Eccentricity:     
0001303     
Arg of perigee:   137
4587  deg
Mean anomaly:     222
6665  deg
Mean motion:   15
49205563  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2083
Checksum:              300


Coasting Arc #17 (Orbit 2084)
---------------------------------------

Vector Time (GMT): 2020/355/04:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1482222
29                 A    =         6791800
19  meter
 Y    =       -3993722
09  meter          E    =           
0003572
 Z    =        5286786
65                 I    =           51
83579
 XDOT =       6715
386098                 Wp   =           81
73707
 YDOT =      -3596
910424  meter/sec      RA   =          146
89307  deg
 ZDOT =       -833
431834                 TA   =           16
21934
                                          MA   =           16
20791
                                          Ha   =            229
049  n
mi
                                          Hp   =            222
087

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4862934
04                 X    =        -1463133
02
 Y    =      -13102762
76  feet           Y    =        -4010191
15  meter
 Z    =       17345100
57                 Z    =         5279632
65
 XDOT =      22032
106620                 XDOT =        6759
157032
 YDOT =     -11800
887219  feet/sec       YDOT =       -3521
569331  meter/sec
 ZDOT =      -2734
356410                 ZDOT =        -800
705520

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         556549
32                 X    =          169636
23
 Y    =       14006058
62  feet           Y    =         4269046
67  meter
 Z    =       17311949
86                 Z    =         5276682
32
 XDOT =     -23637
202889                 XDOT =       -7204
619441
 YDOT =       4135
332800  feet/sec       YDOT =        1260
449438  meter/sec
 ZDOT =      -2582
527516                 ZDOT =        -787
154387


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   20355
25017674  
00016717  00000-0  10270-3 0  9161
2 25544  51
6434 147
8369 0001227 144
4697 215
6535 15
49247116 20852


Satellite: ISS
Catalog Number: 25544
Epoch time:      20355
25017674   =   yrday
fracday
Element set:     916
Inclination:       51
6434  deg
RA of node:       147
8369  deg
Eccentricity:     
0001227     
Arg of perigee:   144
4697  deg
Mean anomaly:     215
6535  deg
Mean motion:   15
49247116  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2085
Checksum:              317


Coasting Arc #18 (Orbit 2099)
---------------------------------------

Vector Time (GMT): 2020/356/04:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1741394
70                 A    =         6791916
17  meter
 Y    =        3908642
13  meter          E    =           
0015257
 Z    =       -5287815
25                 I    =           51
86474
 XDOT =      -6397
508264                 Wp   =          100
56821
 YDOT =       4091
431055  meter/sec      RA   =          141
95973  deg
 ZDOT =        916
986898                 TA   =          178
20136
                                          MA   =          178
19587
                                          Ha   =            228
997  n
mi
                                          Hp   =            222
186

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        5713237
21                 X    =         1723242
61
 Y    =       12823629
05  feet           Y    =         3928014
62  meter
 Z    =      -17348475
23                 Z    =        -5279400
06
 XDOT =     -20989
200342                 XDOT =       -6447
238573
 YDOT =      13423
330232  feet/sec       YDOT =        4019
611380  meter/sec
 ZDOT =       3008
487199                 ZDOT =         885
790143

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1692291
31                 X    =         -515810
39
 Y    =      -13984793
48  feet           Y    =        -4262565
05  meter
 Z    =      -17309472
43                 Z    =        -5275927
20
 XDOT =      23060
206091                 XDOT =        7028
750817
 YDOT =      -6336
960009  feet/sec       YDOT =       -1931
505411  meter/sec
 ZDOT =       2863
728480                 ZDOT =         872
864441


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   20356
21777307  
00016717  00000-0  10270-3 0  9175
2 25544  51
6445 143
0492 0001209 145
8910 214
2318 15
49228210 21008


Satellite: ISS
Catalog Number: 25544
Epoch time:      20356
21777307   =   yrday
fracday
Element set:     917
Inclination:       51
6445  deg
RA of node:       143
0492  deg
Eccentricity:     
0001209     
Arg of perigee:   145
8910  deg
Mean anomaly:     214
2318  deg
Mean motion:   15
49228210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2100
Checksum:              277


Coasting Arc #19 (Orbit 2115)
---------------------------------------

Vector Time (GMT): 2020/357/04:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 980089
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1986218
78                 A    =         6791867
96  meter
 Y    =       -3795980
92  meter          E    =           
0003670
 Z    =        5267238
10                 I    =           51
89110
 XDOT =       6066
649955                 Wp   =           76
48714
 YDOT =      -4572
793480  meter/sec      RA   =          137
02829  deg
 ZDOT =      -1006
418110                 TA   =           23
12908
                                          MA   =           23
11256
                                          Ha   =            228
988  n
mi
                                          Hp   =            222
130

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6516465
81                 X    =        -1969208
44
 Y    =      -12454005
64  feet           Y    =        -3818097
57  meter
 Z    =       17280964
90                 Z    =         5257630
88
 XDOT =      19903
707200                 XDOT =        6122
222011
 YDOT =     -15002
603280  feet/sec       YDOT =       -4504
641033  meter/sec
 ZDOT =      -3301
896686                 ZDOT =        -976
814262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2807425
39                 X    =          855703
26
 Y    =       13828309
07  feet           Y    =         4214868
60  meter
 Z    =       17236431
25                 Z    =         5253664
25
 XDOT =     -22368
921379                 XDOT =       -6818
047236
 YDOT =       8491
604231  feet/sec       YDOT =        2588
240970  meter/sec
 ZDOT =      -3164
502649                 ZDOT =        -964
540408


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   20357
24986989  
00016717  00000-0  10270-3 0  9188
2 25544  51
6447 137
9423 0001117 150
7614 209
3599 15
49259074 21165


Satellite: ISS
Catalog Number: 25544
Epoch time:      20357
24986989   =   yrday
fracday
Element set:     918
Inclination:       51
6447  deg
RA of node:       137
9423  deg
Eccentricity:     
0001117     
Arg of perigee:   150
7614  deg
Mean anomaly:     209
3599  deg
Mean motion:   15
49259074  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2116
Checksum:              337
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