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

 
Date: January 11th 2021

  • 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) : 16464 4774 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


012/13:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 5
000/00:00:00 000 0 0 0 0 222 4

021/16:17:19 647 2 1 2 2 2 2
N/A -0 8 -0 2 228 4
000/00:06:39 293 -0 1 0 0 223 7

026/07:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 6
000/00:00:00 000 0 0 0 0 223 5

Coasting Arc #1 (Orbit 2429)
---------------------------------------

Vector Time (GMT): 2021/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983715
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5986678
28                 A    =         6801230
48  meter
 Y    =        2275011
19  meter          E    =           
0005653
 Z    =       -2285426
79                 I    =           51
89685
 XDOT =         31
665758                 Wp   =           45
11768
 YDOT =       5378
860712  meter/sec      RA   =           37
05812  deg
 ZDOT =       5449
427064                 TA   =          289
59787
                                          MA   =          289
65889
                                          Ha   =            228
585  n
mi
                                          Hp   =            222
344

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19641332
94                 X    =         5971894
59
 Y    =        7463947
46  feet           Y    =         2341876
22  meter
 Z    =       -7498119
38                 Z    =        -2256381
88
 XDOT =        103
890283                 XDOT =         -54
954409
 YDOT =      17647
180815  feet/sec       YDOT =        5378
729662  meter/sec
 ZDOT =      17878
697715                 ZDOT =        5449
371325

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -165135
89                 X    =          -50333
42
 Y    =       21058678
90  feet           Y    =         6418685
33  meter
 Z    =       -7363357
86                 Z    =        -2244351
48
 XDOT =     -15021
995026                 XDOT =       -4578
704084
 YDOT =       6119
289238  feet/sec       YDOT =        1865
159360  meter/sec
 ZDOT =      17878
155033                 ZDOT =        5449
261654


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   21011
50446529  
00016717  00000-0  10270-3 0  9007
2 25544  51
6453  37
7188 0000412 194
9326 165
1812 15
49315091 24302


Satellite: ISS
Catalog Number: 25544
Epoch time:      21011
50446529   =   yrday
fracday
Element set:     900
Inclination:       51
6453  deg
RA of node:        37
7188  deg
Eccentricity:     
0000412     
Arg of perigee:   194
9326  deg
Mean anomaly:     165
1812  deg
Mean motion:   15
49315091  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2430
Checksum:              283


Coasting Arc #2 (Orbit 2445)
---------------------------------------

Vector Time (GMT): 2021/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 983715
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6164183
78                 A    =         6801511
18  meter
 Y    =       -1851445
83  meter          E    =           
0013848
 Z    =        2178388
85                 I    =           51
86782
 XDOT =       -354
066036                 Wp   =          110
64483
 YDOT =      -5322
098995  meter/sec      RA   =           32
12598  deg
 ZDOT =      -5501
727565                 TA   =           45
30266
                                          MA   =           45
18994
                                          Ha   =            228
635  n
mi
                                          Hp   =            222
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20223700
06                 X    =        -6153603
34
 Y    =       -6074297
33  feet           Y    =        -1920319
33  meter
 Z    =        7146945
05                 Z    =         2148471
75
 XDOT =      -1161
633975                 XDOT =        -267
802753
 YDOT =     -17460
954707  feet/sec       YDOT =       -5325
575262  meter/sec
 ZDOT =     -18050
287287                 ZDOT =       -5503
238726

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1702495
95                 X    =         -518920
77
 Y    =      -21094118
07  feet           Y    =        -6429487
19  meter
 Z    =        7008112
86                 Z    =         2136072
80
 XDOT =      14354
727258                 XDOT =        4375
320868
 YDOT =      -7183
786751  feet/sec       YDOT =       -2189
618202  meter/sec
 ZDOT =     -18057
018656                 ZDOT =       -5503
779286


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   21012
53652298  
00016717  00000-0  10270-3 0  9014
2 25544  51
6434  32
6118 0000290 204
3908 155
7229 15
49289697 24460


Satellite: ISS
Catalog Number: 25544
Epoch time:      21012
53652298   =   yrday
fracday
Element set:     901
Inclination:       51
6434  deg
RA of node:        32
6118  deg
Eccentricity:     
0000290     
Arg of perigee:   204
3908  deg
Mean anomaly:     155
7229  deg
Mean motion:   15
49289697  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2446
Checksum:              308


Coasting Arc #3 (Orbit 2446)
---------------------------------------

Vector Time (GMT): 2021/012/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6159983
42                 A    =         6802573
40  meter
 Y    =       -2471115
86  meter          E    =           
0013633
 Z    =        1460527
11                 I    =           51
86786
 XDOT =        612
953806                 Wp   =          119
65693
 YDOT =      -4973
822579  meter/sec      RA   =           31
80585  deg
 ZDOT =      -5796
131698                 TA   =           44
48714
                                          MA   =           44
37774
                                          Ha   =            228
549  n
mi
                                          Hp   =            222
414

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20209919
37                 X    =        -6138987
08
 Y    =       -8107335
49  feet           Y    =        -2539884
04  meter
 Z    =        4791755
61                 Z    =         1430655
63
 XDOT =       2011
003299                 XDOT =         696
680688
 YDOT =     -16318
315547  feet/sec       YDOT =       -4966
499077  meter/sec
 ZDOT =     -19016
180112                 ZDOT =       -5792
951667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8618873
09                 X    =        -2627032
52
 Y    =      -20029820
23  feet           Y    =        -6105089
21  meter
 Z    =        4653168
76                 Z    =         1418285
84
 XDOT =      11574
161731                 XDOT =        3527
804496
 YDOT =      -9421
288761  feet/sec       YDOT =       -2871
608814  meter/sec
 ZDOT =     -19001
144597                 ZDOT =       -5791
548873


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   21012
60102621  
00016717  00000-0  10270-3 0  9023
2 25544  51
6418  32
2924 0000270 249
3245 110
7876 15
49294127 24478


Satellite: ISS
Catalog Number: 25544
Epoch time:      21012
60102621   =   yrday
fracday
Element set:     902
Inclination:       51
6418  deg
RA of node:        32
2924  deg
Eccentricity:     
0000270     
Arg of perigee:   249
3245  deg
Mean anomaly:     110
7876  deg
Mean motion:   15
49294127  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2447
Checksum:              275


Coasting Arc #4 (Orbit 2461)
---------------------------------------

Vector Time (GMT): 2021/013/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6349604
71                 A    =         6802636
17  meter
 Y    =        2001213
58  meter          E    =           
0008452
 Z    =       -1380559
70                 I    =           51
83885
 XDOT =       -306
917089                 Wp   =           37
60033
 YDOT =       4970
394118  meter/sec      RA   =           26
87186  deg
 ZDOT =       5818
616686                 TA   =          307
43392
                                          MA   =          307
51080
                                          Ha   =            228
583  n
mi
                                          Hp   =            222
350

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20832036
43                 X    =         6333460
40
 Y    =        6565661
35  feet           Y    =         2072129
34  meter
 Z    =       -4529395
35                 Z    =        -1349755
61
 XDOT =      -1006
945830                 XDOT =        -390
737454
 YDOT =      16307
067315  feet/sec       YDOT =        4966
492507  meter/sec
 ZDOT =      19089
949757                 ZDOT =        5816
922928

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10478156
69                 X    =         3193742
16
 Y    =       19198029
00  feet           Y    =         5851559
24  meter
 Z    =       -4386455
08                 Z    =        -1336991
51
 XDOT =     -10729
203921                 XDOT =       -3270
261355
 YDOT =      10196
245799  feet/sec       YDOT =        3107
815719  meter/sec
 ZDOT =      19081
814663                 ZDOT =        5816
137109


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   21013
56857831  
00016717  00000-0  10270-3 0  9030
2 25544  51
6420  27
5050 0000310 210
5892 149
5240 15
49302615 24625


Satellite: ISS
Catalog Number: 25544
Epoch time:      21013
56857831   =   yrday
fracday
Element set:     903
Inclination:       51
6420  deg
RA of node:        27
5050  deg
Eccentricity:     
0000310     
Arg of perigee:   210
5892  deg
Mean anomaly:     149
5240  deg
Mean motion:   15
49302615  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2462
Checksum:              269


Coasting Arc #5 (Orbit 2477)
---------------------------------------

Vector Time (GMT): 2021/014/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6496699
10                 A    =         6802766
19  meter
 Y    =       -1544437
38  meter          E    =           
0013407
 Z    =        1263796
44                 I    =           51
80896
 XDOT =         30
875148                 Wp   =          121
49323
 YDOT =      -4948
390711  meter/sec      RA   =           21
93458  deg
 ZDOT =      -5849
618595                 TA   =           44
82102
                                          MA   =           44
71280
                                          Ha   =            228
514  n
mi
                                          Hp   =            222
409

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21314629
59                 X    =        -6485084
50
 Y    =       -5067051
78  feet           Y    =        -1617023
34  meter
 Z    =        4146313
79                 Z    =         1232267
04
 XDOT =        101
296416                 XDOT =         114
620481
 YDOT =     -16234
877660  feet/sec       YDOT =       -4947
576560  meter/sec
 ZDOT =     -19191
662056                 ZDOT =       -5849
265760

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12178817
00                 X    =        -3712103
42
 Y    =      -18244366
28  feet           Y    =        -5560882
84  meter
 Z    =        3999985
21                 Z    =         1219195
49
 XDOT =       9896
583792                 XDOT =        3016
478740
 YDOT =     -10842
614946  feet/sec       YDOT =       -3304
829035  meter/sec
 ZDOT =     -19189
755580                 ZDOT =       -5849
037501


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   21014
60063006  
00016717  00000-0  10270-3 0  9040
2 25544  51
6425  22
3967 0000291 285
3988  74
7130 15
49303770 24781


Satellite: ISS
Catalog Number: 25544
Epoch time:      21014
60063006   =   yrday
fracday
Element set:     904
Inclination:       51
6425  deg
RA of node:        22
3967  deg
Eccentricity:     
0000291     
Arg of perigee:   285
3988  deg
Mean anomaly:      74
7130  deg
Mean motion:   15
49303770  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2478
Checksum:              295


Coasting Arc #6 (Orbit 2492)
---------------------------------------

Vector Time (GMT): 2021/015/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6612849
06                 A    =         6802848
26  meter
 Y    =        1049480
05  meter          E    =           
0009173
 Z    =       -1180066
86                 I    =           51
77653
 XDOT =        262
042914                 Wp   =           36
88077
 YDOT =       4913
807183  meter/sec      RA   =           16
99669  deg
 ZDOT =       5869
304515                 TA   =          310
35509
                                          MA   =          310
43516
                                          Ha   =            228
559  n
mi
                                          Hp   =            222
364

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21695699
02                 X    =         6606353
89
 Y    =        3443176
03  feet           Y    =         1123393
47  meter
 Z    =       -3871610
44                 Z    =        -1147960
93
 XDOT =        859
720845                 XDOT =         178
566931
 YDOT =      16121
414644  feet/sec       YDOT =        4916
270318  meter/sec
 ZDOT =      19256
248408                 ZDOT =        5870
375032

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13858111
03                 X    =         4223952
24
 Y    =       17077567
19  feet           Y    =         5205242
48  meter
 Z    =       -3722585
42                 Z    =        -1134644
03
 XDOT =      -8987
839819                 XDOT =       -2739
493577
 YDOT =      11469
048876  feet/sec       YDOT =        3495
766097  meter/sec
 ZDOT =      19260
954912                 ZDOT =        5870
739057


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   21015
56817754  
00016717  00000-0  10270-3 0  9054
2 25544  51
6418  17
6095 0000223 257
1584 102
9541 15
49302297 24936


Satellite: ISS
Catalog Number: 25544
Epoch time:      21015
56817754   =   yrday
fracday
Element set:     905
Inclination:       51
6418  deg
RA of node:        17
6095  deg
Eccentricity:     
0000223     
Arg of perigee:   257
1584  deg
Mean anomaly:     102
9541  deg
Mean motion:   15
49302297  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2493
Checksum:              304


Coasting Arc #7 (Orbit 2508)
---------------------------------------

Vector Time (GMT): 2021/016/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6688830
98                 A    =         6802974
03  meter
 Y    =        -573551
26  meter          E    =           
0013142
 Z    =        1060439
54                 I    =           51
74458
 XDOT =       -524
644544                 Wp   =          123
83789
 YDOT =      -4865
314205  meter/sec      RA   =           12
05571  deg
 ZDOT =      -5895
358298                 TA   =           44
70162
                                          MA   =           44
59576
                                          Ha   =            228
486  n
mi
                                          Hp   =            222
443

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21944983
52                 X    =        -6687071
08
 Y    =       -1881729
86  feet           Y    =         -648340
80  meter
 Z    =        3479132
35                 Z    =         1027953
04
 XDOT =      -1721
274750                 XDOT =        -441
564715
 YDOT =     -15962
316945  feet/sec       YDOT =       -4870
716295  meter/sec
 ZDOT =     -19341
726700                 ZDOT =       -5897
705235

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15359398
77                 X    =        -4681544
75
 Y    =      -15818934
62  feet           Y    =        -4821611
27  meter
 Z    =        3328325
08                 Z    =         1014473
49
 XDOT =       8108
906454                 XDOT =        2471
594687
 YDOT =     -11977
834125  feet/sec       YDOT =       -3650
843841  meter/sec
 ZDOT =     -19352
364341                 ZDOT =       -5898
600651


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   21016
60022655  
00016717  00000-0  10270-3 0  9069
2 25544  51
6423  12
5018 0000387 292
4204  67
6905 15
49298465 25093


Satellite: ISS
Catalog Number: 25544
Epoch time:      21016
60022655   =   yrday
fracday
Element set:     906
Inclination:       51
6423  deg
RA of node:        12
5018  deg
Eccentricity:     
0000387     
Arg of perigee:   292
4204  deg
Mean anomaly:      67
6905  deg
Mean motion:   15
49298465  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2509
Checksum:              296


Coasting Arc #8 (Orbit 2523)
---------------------------------------

Vector Time (GMT): 2021/017/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6728157
56                 A    =         6803013
97  meter
 Y    =          65286
48  meter          E    =           
0009773
 Z    =        -973331
82                 I    =           51
71186
 XDOT =        803
085596                 Wp   =           36
88820
 YDOT =       4803
429899  meter/sec      RA   =            7
11320  deg
 ZDOT =       5911
980698                 TA   =          312
60208
                                          MA   =          312
68447
                                          Ha   =            228
512  n
mi
                                          Hp   =            222
384

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22074007
73                 X    =         6731655
22
 Y    =         214194
50  feet           Y    =          140545
18  meter
 Z    =       -3193345
87                 Z    =         -940641
46
 XDOT =       2634
795261                 XDOT =         720
596260
 YDOT =      15759
284444  feet/sec       YDOT =        4811
949116  meter/sec
 ZDOT =      19396
262132                 ZDOT =        5915
681514

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16797663
10                 X    =         5119927
71
 Y    =       14355921
18  feet           Y    =         4375684
78  meter
 Z    =       -3041577
85                 Z    =         -927072
93
 XDOT =      -7158
645694                 XDOT =       -2181
955207
 YDOT =      12461
221731  feet/sec       YDOT =        3798
180384  meter/sec
 ZDOT =      19413
190085                 ZDOT =        5917
140338


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   21017
56776994  
00016717  00000-0  10270-3 0  9078
2 25544  51
6428   7
7145 0000323 281
1177  78
9937 15
49307459 25240


Satellite: ISS
Catalog Number: 25544
Epoch time:      21017
56776994   =   yrday
fracday
Element set:     907
Inclination:       51
6428  deg
RA of node:         7
7145  deg
Eccentricity:     
0000323     
Arg of perigee:   281
1177  deg
Mean anomaly:      78
9937  deg
Mean motion:   15
49307459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2524
Checksum:              332


Coasting Arc #9 (Orbit 2539)
---------------------------------------

Vector Time (GMT): 2021/018/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6730779
48                 A    =         6803132
19  meter
 Y    =         416953
19  meter          E    =           
0012835
 Z    =         849337
86                 I    =           51
67930
 XDOT =      -1048
862728                 Wp   =          125
79618
 YDOT =      -4732
285250  meter/sec      RA   =            2
16789  deg
 ZDOT =      -5933
176886                 TA   =           45
03908
                                          MA   =           44
93508
                                          Ha   =            228
474  n
mi
                                          Hp   =            222
442

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22082609
84                 X    =        -6739067
23
 Y    =        1367956
66  feet           Y    =          341638
40  meter
 Z    =        2786541
54                 Z    =          816623
03
 XDOT =      -3441
150682                 XDOT =        -967
047628
 YDOT =     -15525
870244  feet/sec       YDOT =       -4743
556738  meter/sec
 ZDOT =     -19465
803432                 ZDOT =       -5938
073175

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18041824
13                 X    =        -5499147
99
 Y    =      -12838574
11  feet           Y    =        -3913197
39  meter
 Z    =        2634648
66                 Z    =          803040
91
 XDOT =       6259
372848                 XDOT =        1907
856844
 YDOT =     -12835
061560  feet/sec       YDOT =       -3912
126764  meter/sec
 ZDOT =     -19488
285180                 ZDOT =       -5940
029323


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   21018
59981311  
00016717  00000-0  10270-3 0  9084
2 25544  51
6438   2
6069 0000469 307
8539  52
2569 15
49299595 25404


Satellite: ISS
Catalog Number: 25544
Epoch time:      21018
59981311   =   yrday
fracday
Element set:     908
Inclination:       51
6438  deg
RA of node:         2
6069  deg
Eccentricity:     
0000469     
Arg of perigee:   307
8539  deg
Mean anomaly:      52
2569  deg
Mean motion:   15
49299595  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2540
Checksum:              332


Coasting Arc #10 (Orbit 2554)
---------------------------------------

Vector Time (GMT): 2021/019/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6691951
00                 A    =         6803169
56  meter
 Y    =        -925840
68  meter          E    =           
0010513
 Z    =        -758606
79                 I    =           51
64459
 XDOT =       1311
230760                 Wp   =           37
31099
 YDOT =       4647
395685  meter/sec      RA   =          357
22102  deg
 ZDOT =       5946
368940                 TA   =          314
50792
                                          MA   =          314
59378
                                          Ha   =            228
513  n
mi
                                          Hp   =            222
381

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21955219
83                 X    =         6705491
48
 Y    =       -3037535
04  feet           Y    =         -850930
73  meter
 Z    =       -2488867
43                 Z    =         -726067
72
 XDOT =       4301
938189                 XDOT =        1230
281241
 YDOT =      15247
361171  feet/sec       YDOT =        4661
605998  meter/sec
 ZDOT =      19509
084448                 ZDOT =        5952
541803

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19185697
41                 X    =         5847800
57
 Y    =       11130883
43  feet           Y    =         3392693
27  meter
 Z    =       -2337778
22                 Z    =         -712554
80
 XDOT =      -5289
857600                 XDOT =       -1612
348596
 YDOT =      13183
501580  feet/sec       YDOT =        4018
331282  meter/sec
 ZDOT =      19537
495686                 ZDOT =        5955
028685


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   21019
56735170  
00016717  00000-0  10270-3 0  9093
2 25544  51
6429 357
8198 0000442 313
0831  47
0282 15
49305151 25553


Satellite: ISS
Catalog Number: 25544
Epoch time:      21019
56735170   =   yrday
fracday
Element set:     909
Inclination:       51
6429  deg
RA of node:       357
8198  deg
Eccentricity:     
0000442     
Arg of perigee:   313
0831  deg
Mean anomaly:      47
0282  deg
Mean motion:   15
49305151  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2555
Checksum:              300


Coasting Arc #11 (Orbit 2570)
---------------------------------------

Vector Time (GMT): 2021/020/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6620680
38                 A    =         6803263
13  meter
 Y    =        1403600
33  meter          E    =           
0012527
 Z    =         631761
54                 I    =           51
61170
 XDOT =      -1542
077180                 Wp   =          127
99996
 YDOT =      -4557
435634  meter/sec      RA   =          352
27159  deg
 ZDOT =      -5961
966395                 TA   =           45
19001
                                          MA   =           45
08824
                                          Ha   =            228
469  n
mi
                                          Hp   =            222
440

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21721392
33                 X    =        -6638952
49
 Y    =        4604987
95  feet           Y    =         1329460
92  meter
 Z    =        2072708
47                 Z    =          599557
10
 XDOT =      -5059
308333                 XDOT =       -1462
040615
 YDOT =     -14952
216647  feet/sec       YDOT =       -4574
232503  meter/sec
 ZDOT =     -19560
257200                 ZDOT =       -5969
262863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20128767
55                 X    =        -6135248
35
 Y    =       -9405056
42  feet           Y    =        -2866661
20  meter
 Z    =        1923161
46                 Z    =          586179
61
 XDOT =       4381
804008                 XDOT =        1335
573862
 YDOT =     -13437
479762  feet/sec       YDOT =       -4095
743831  meter/sec
 ZDOT =     -19593
886957                 ZDOT =       -5972
216745


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   21020
59939180  
00016717  00000-0  10270-3 0  9107
2 25544  51
6437 352
7127 0000508 313
0443  47
0665 15
49298061 25714


Satellite: ISS
Catalog Number: 25544
Epoch time:      21020
59939180   =   yrday
fracday
Element set:     910
Inclination:       51
6437  deg
RA of node:       352
7127  deg
Eccentricity:     
0000508     
Arg of perigee:   313
0443  deg
Mean anomaly:      47
0665  deg
Mean motion:   15
49298061  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2571
Checksum:              295


Coasting Arc #12 (Orbit 2585)
---------------------------------------

Vector Time (GMT): 2021/021/13:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 957119
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6504537
01                 A    =         6803265
02  meter
 Y    =       -1900705
97  meter          E    =           
0011070
 Z    =        -537725
63                 I    =           51
57838
 XDOT =       1788
588979                 Wp   =           38
33244
 YDOT =       4452
576880  meter/sec      RA   =          347
31965  deg
 ZDOT =       5971
463194                 TA   =          315
87279
                                          MA   =          315
96106
                                          Ha   =            228
477  n
mi
                                          Hp   =            222
386

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21340344
52                 X    =         6527919
78
 Y    =       -6235911
98  feet           Y    =        -1827836
79  meter
 Z    =       -1764191
72                 Z    =         -506072
92
 XDOT =       5868
074079                 XDOT =        1709
660466
 YDOT =      14608
191863  feet/sec       YDOT =        4472
136550  meter/sec
 ZDOT =      19591
414679                 ZDOT =        5979
959854

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       20936776
79                 X    =         6381529
57
 Y    =        7513011
51  feet           Y    =         2289965
91  meter
 Z    =       -1617192
16                 Z    =         -492920
17
 XDOT =      -3406
380875                 XDOT =       -1038
264891
 YDOT =      13660
757844  feet/sec       YDOT =        4163
798991  meter/sec
 ZDOT =      19630
618601                 ZDOT =        5983
412550


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   21021
56692587  
00016717  00000-0  10270-3 0  9113
2 25544  51
6437 347
9251 0000550 315
6241  44
4865 15
49310865 25865


Satellite: ISS
Catalog Number: 25544
Epoch time:      21021
56692587   =   yrday
fracday
Element set:     911
Inclination:       51
6437  deg
RA of node:       347
9251  deg
Eccentricity:     
0000550     
Arg of perigee:   315
6241  deg
Mean anomaly:      44
4865  deg
Mean motion:   15
49310865  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2586
Checksum:              312


Coasting Arc #13 (Orbit 2587)
---------------------------------------

Vector Time (GMT): 2021/021/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -232909
95                 A    =         6792775
03  meter
 Y    =       -4264576
81  meter          E    =           
0012333
 Z    =       -5292898
47                 I    =           51
53807
 XDOT =       7522
064166                 Wp   =           94
84531
 YDOT =      -1231
466504  meter/sec      RA   =          346
74918  deg
 ZDOT =        661
526679                 TA   =          181
49261
                                          MA   =          181
49629
                                          Ha   =            228
414  n
mi
                                          Hp   =            223
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -764140
26                 X    =         -159495
36
 Y    =      -13991393
72  feet           Y    =        -4266770
61  meter
 Z    =      -17365152
45                 Z    =        -5293851
75
 XDOT =      24678
688210                 XDOT =        7532
062478
 YDOT =      -4040
244436  feet/sec       YDOT =       -1147
293497  meter/sec
 ZDOT =       2170
363121                 ZDOT =         698
089596

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1984379
81                 X    =         -604838
97
 Y    =      -13865756
20  feet           Y    =        -4226282
49  meter
 Z    =      -17369357
21                 Z    =        -5294180
08
 XDOT =      23150
621776                 XDOT =        7056
309517
 YDOT =      -6243
287885  feet/sec       YDOT =       -1902
954147  meter/sec
 ZDOT =       2340
115180                 ZDOT =         713
267107


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   21021
69593094  
00016717  00000-0  10270-3 0  9121
2 25544  51
6462 347
2871 0002237 276
5533  83
5363 15
48905071 25884


Satellite: ISS
Catalog Number: 25544
Epoch time:      21021
69593094   =   yrday
fracday
Element set:     912
Inclination:       51
6462  deg
RA of node:       347
2871  deg
Eccentricity:     
0002237     
Arg of perigee:   276
5533  deg
Mean anomaly:      83
5363  deg
Mean motion:   15
48905071  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2588
Checksum:              319


Coasting Arc #14 (Orbit 2603)
---------------------------------------

Vector Time (GMT): 2021/022/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         631369
96                 A    =         6792677
80  meter
 Y    =        4218129
41  meter          E    =           
0001841
 Z    =        5286482
79                 I    =           51
50526
 XDOT =      -7393
712653                 Wp   =           13
93344
 YDOT =       1901
766545  meter/sec      RA   =          341
79691  deg
 ZDOT =       -632
602587                 TA   =           82
13358
                                          MA   =           82
11269
                                          Ha   =            228
345  n
mi
                                          Hp   =            223
685

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2071423
74                 X    =          558476
29
 Y    =       13839007
24  feet           Y    =         4224781
91  meter
 Z    =       17344103
65                 Z    =         5289372
94
 XDOT =     -24257
587445                 XDOT =       -7411
356496
 YDOT =       6239
391552  feet/sec       YDOT =        1818
986117  meter/sec
 ZDOT =      -2075
467805                 ZDOT =        -668
560561

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3504376
64                 X    =         1068134
00
 Y    =       13530347
68  feet           Y    =         4124049
97  meter
 Z    =       17357300
63                 Z    =         5290505
23
 XDOT =     -22395
243315                 XDOT =       -6826
070163
 YDOT =       8684
632521  feet/sec       YDOT =        2647
075992  meter/sec
 ZDOT =      -2242
434892                 ZDOT =        -683
494155


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   21022
72824472  
00016717  00000-0  10270-3 0  9134
2 25544  51
6462 342
1818 0002302 281
1587  78
9304 15
48930740 26046


Satellite: ISS
Catalog Number: 25544
Epoch time:      21022
72824472   =   yrday
fracday
Element set:     913
Inclination:       51
6462  deg
RA of node:       342
1818  deg
Eccentricity:     
0002302     
Arg of perigee:   281
1587  deg
Mean anomaly:      78
9304  deg
Mean motion:   15
48930740  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2604
Checksum:              294


Coasting Arc #15 (Orbit 2618)
---------------------------------------

Vector Time (GMT): 2021/023/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1030503
28                 A    =         6792725
43  meter
 Y    =       -4143596
91  meter          E    =           
0012412
 Z    =       -5293790
29                 I    =           51
47269
 XDOT =       7186
951610                 Wp   =           92
53794
 YDOT =      -2553
864555  meter/sec      RA   =          336
84260  deg
 ZDOT =        600
635315                 TA   =          183
21745
                                          MA   =          183
22544
                                          Ha   =            228
441  n
mi
                                          Hp   =            223
624

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3380916
28                 X    =         -958377
92
 Y    =      -13594478
07  feet           Y    =        -4154717
03  meter
 Z    =      -17368078
37                 Z    =        -5298621
16
 XDOT =      23579
237567                 XDOT =        7212
058058
 YDOT =      -8378
820719  feet/sec       YDOT =       -2473
354559  meter/sec
 ZDOT =       1970
588304                 ZDOT =         635
606949

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5002933
97                 X    =        -1524894
27
 Y    =      -13055234
53  feet           Y    =        -3979235
48  meter
 Z    =      -17390286
89                 Z    =        -5300559
44
 XDOT =      21322
380888                 XDOT =        6499
061695
 YDOT =     -11009
292963  feet/sec       YDOT =       -3355
632495  meter/sec
 ZDOT =       2133
001261                 ZDOT =         650
138784


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   21023
69603945  
00016717  00000-0  10270-3 0  9142
2 25544  51
6455 337
3958 0002253 286
3195  73
7707 15
48912322 26198


Satellite: ISS
Catalog Number: 25544
Epoch time:      21023
69603945   =   yrday
fracday
Element set:     914
Inclination:       51
6455  deg
RA of node:       337
3958  deg
Eccentricity:     
0002253     
Arg of perigee:   286
3195  deg
Mean anomaly:      73
7707  deg
Mean motion:   15
48912322  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2619
Checksum:              324


Coasting Arc #16 (Orbit 2634)
---------------------------------------

Vector Time (GMT): 2021/024/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1410088
94                 A    =         6792662
80  meter
 Y    =        4024589
11  meter          E    =           
0001982
 Z    =        5287021
31                 I    =           51
44215
 XDOT =      -6941
324128                 Wp   =           11
79761
 YDOT =       3189
289360  meter/sec      RA   =          331
88614  deg
 ZDOT =       -574
509431                 TA   =           83
71711
                                          MA   =           83
69454
                                          Ha   =            228
346  n
mi
                                          Hp   =            223
686

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4626276
05                 X    =         1339299
09
 Y    =       13204032
52  feet           Y    =         4039961
43  meter
 Z    =       17345870
45                 Z    =         5293699
30
 XDOT =     -22773
373122                 XDOT =       -6973
681254
 YDOT =      10463
547769  feet/sec       YDOT =        3111
485612  meter/sec
 ZDOT =      -1884
873461                 ZDOT =        -608
305353

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6401213
39                 X    =         1951089
84
 Y    =       12397754
36  feet           Y    =         3778835
53  meter
 Z    =       17376659
06                 Z    =         5296405
68
 XDOT =     -20068
080219                 XDOT =       -6116
750851
 YDOT =      13232
315881  feet/sec       YDOT =        4033
209881  meter/sec
 ZDOT =      -2041
853647                 ZDOT =        -622
356992


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   21024
72835024  
00016717  00000-0  10270-3 0  9153
2 25544  51
6457 332
2906 0002355 287
6796  72
4097 15
48926891 26353


Satellite: ISS
Catalog Number: 25544
Epoch time:      21024
72835024   =   yrday
fracday
Element set:     915
Inclination:       51
6457  deg
RA of node:       332
2906  deg
Eccentricity:     
0002355     
Arg of perigee:   287
6796  deg
Mean anomaly:      72
4097  deg
Mean motion:   15
48926891  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2635
Checksum:              330


Coasting Arc #17 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2021/025/16:20:39
293
Vector Time (MET): N/A
Weight (LBS)     : 956872
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1785686
40                 A    =         6792671
16  meter
 Y    =       -3878072
71  meter          E    =           
0012404
 Z    =       -5293996
69                 I    =           51
41289
 XDOT =       6622
133611                 Wp   =           90
48641
 YDOT =      -3792
834745  meter/sec      RA   =          326
92684  deg
 ZDOT =        545
746300                 TA   =          184
74356
                                          MA   =          184
75532
                                          Ha   =            228
437  n
mi
                                          Hp   =            223
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5858551
18                 X    =        -1716473
25
 Y    =      -12723335
65  feet           Y    =        -3897654
01  meter
 Z    =      -17368755
55                 Z    =        -5302502
96
 XDOT =      21726
160142                 XDOT =        6661
403212
 YDOT =     -12443
683547  feet/sec       YDOT =       -3718
561765  meter/sec
 ZDOT =       1790
506232                 ZDOT =         578
008332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7749977
47                 X    =        -2362193
13
 Y    =      -11609374
39  feet           Y    =        -3538537
31  meter
 Z    =      -17408039
42                 Z    =        -5305970
42
 XDOT =      18529
416738                 XDOT =        5647
766222
 YDOT =     -15274
157966  feet/sec       YDOT =       -4655
563348  meter/sec
 ZDOT =       1940
389663                 ZDOT =         591
430769


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   21025
69614008  
00016717  00000-0  10270-3 0  9168
2 25544  51
6459 327
5040 0002408 293
8638  66
2259 15
48922532 26500


Satellite: ISS
Catalog Number: 25544
Epoch time:      21025
69614008   =   yrday
fracday
Element set:     916
Inclination:       51
6459  deg
RA of node:       327
5040  deg
Eccentricity:     
0002408     
Arg of perigee:   293
8638  deg
Mean anomaly:      66
2259  deg
Mean motion:   15
48922532  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              312


Coasting Arc #18 (Orbit 2659)
---------------------------------------

Vector Time (GMT): 2021/026/07:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 956872
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6003625
35                 A    =         6803257
40  meter
 Y    =        2691978
92  meter          E    =           
0005731
 Z    =       -1720290
21                 I    =           51
42794
 XDOT =       -670
533163                 Wp   =          149
62985
 YDOT =      -5107
493748  meter/sec      RA   =          323
81370  deg
 ZDOT =      -5665
461004                 TA   =           49
24776
                                          MA   =           49
19802
                                          Ha   =            228
591  n
mi
                                          Hp   =            223
518

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19696933
57                 X    =        -6024925
70
 Y    =        8831951
85  feet           Y    =         2624723
14  meter
 Z    =       -5643996
74                 Z    =        -1749504
22
 XDOT =      -2199
911953                 XDOT =        -585
850886
 YDOT =     -16756
869253  feet/sec       YDOT =       -5114
518078  meter/sec
 ZDOT =     -18587
470485                 ZDOT =       -5668
512950

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3147991
43                 X    =          959507
79
 Y    =      -21319303
92  feet           Y    =        -6498123
83  meter
 Z    =       -5779679
49                 Z    =        -1761646
31
 XDOT =      13680
248352                 XDOT =        4169
739698
 YDOT =       7051
454718  feet/sec       YDOT =        2149
283398  meter/sec
 ZDOT =     -18601
391633                 ZDOT =       -5669
704170


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   21026
34133177  
00016717  00000-0  10270-3 0  9175
2 25544  51
6434 324
3120 0001989 296
5738  63
5208 15
48900898 26607


Satellite: ISS
Catalog Number: 25544
Epoch time:      21026
34133177   =   yrday
fracday
Element set:     917
Inclination:       51
6434  deg
RA of node:       324
3120  deg
Eccentricity:     
0001989     
Arg of perigee:   296
5738  deg
Mean anomaly:      63
5208  deg
Mean motion:   15
48900898  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2660
Checksum:              316
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list