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

 
Date: June 2nd 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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


160/04:50:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 0
000/00:00:00 000 0 0 0 0 221 6

Coasting Arc #1 (Orbit 2949)
---------------------------------------

Vector Time (GMT): 2020/152/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3777061
90                 A    =         6791031
55  meter
 Y    =        1804090
68  meter          E    =           
0002870
 Z    =        5345318
24                 I    =           51
98684
 XDOT =      -3041
173565                 Wp   =           67
04333
 YDOT =      -7030
457846  meter/sec      RA   =           67
92314  deg
 ZDOT =        224
905434                 TA   =           20
82775
                                          MA   =           20
81605
                                          Ha   =            228
681  n
mi
                                          Hp   =            221
952

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12391935
37                 X    =        -3822919
69
 Y    =        5918932
67  feet           Y    =         1761595
98  meter
 Z    =       17537133
33                 Z    =         5326859
44
 XDOT =      -9977
603559                 XDOT =       -2963
423338
 YDOT =     -23065
806583  feet/sec       YDOT =       -7064
031707  meter/sec
 ZDOT =        737
878722                 ZDOT =         210
320713

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1033983
52                 X    =          315158
18
 Y    =      -13802221
26  feet           Y    =        -4206917
04  meter
 Z    =       17452061
14                 Z    =         5319388
24
 XDOT =      23979
507490                 XDOT =        7308
953883
 YDOT =       2640
973625  feet/sec       YDOT =         804
968761  meter/sec
 ZDOT =        671
211636                 ZDOT =         204
585307


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   20153
02479753  
00016717  00000-0  10270-3 0  9005
2 25544  51
6442  68
4689 0001535   7
9546 352
1628 15
49444327 29506


Satellite: ISS
Catalog Number: 25544
Epoch time:      20153
02479753   =   yrday
fracday
Element set:     900
Inclination:       51
6442  deg
RA of node:        68
4689  deg
Eccentricity:     
0001535     
Arg of perigee:     7
9546  deg
Mean anomaly:     352
1628  deg
Mean motion:   15
49444327  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2950
Checksum:              315


Coasting Arc #2 (Orbit 2964)
---------------------------------------

Vector Time (GMT): 2020/153/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3698360
42                 A    =         6791125
07  meter
 Y    =       -1970054
77  meter          E    =           
0015306
 Z    =       -5357323
79                 I    =           51
97310
 XDOT =       3519
234333                 Wp   =           83
40917
 YDOT =       6791
647900  meter/sec      RA   =           62
99766  deg
 ZDOT =        -66
498628                 TA   =          185
94941
                                          MA   =          185
96761
                                          Ha   =            228
651  n
mi
                                          Hp   =            222
067

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12133728
40                 X    =         3746138
35
 Y    =       -6463434
27  feet           Y    =        -1928429
38  meter
 Z    =      -17576521
61                 Z    =        -5339242
58
 XDOT =      11546
044400                 XDOT =        3443
349567
 YDOT =      22282
309382  feet/sec       YDOT =        6830
578192  meter/sec
 ZDOT =       -218
171352                 ZDOT =         -49
587023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -194891
33                 X    =          -59402
88
 Y    =       13852376
73  feet           Y    =         4222204
43  meter
 Z    =      -17493173
98                 Z    =        -5331919
43
 XDOT =     -24080
735728                 XDOT =       -7339
808250
 YDOT =       -523
022975  feet/sec       YDOT =        -159
417403  meter/sec
 ZDOT =       -140
797946                 ZDOT =         -42
915214


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   20153
99227081  
00016717  00000-0  10270-3 0  9017
2 25544  51
6442  63
6817 0001653  13
2274 346
8920 15
49412384 29654


Satellite: ISS
Catalog Number: 25544
Epoch time:      20153
99227081   =   yrday
fracday
Element set:     901
Inclination:       51
6442  deg
RA of node:        63
6817  deg
Eccentricity:     
0001653     
Arg of perigee:    13
2274  deg
Mean anomaly:     346
8920  deg
Mean motion:   15
49412384  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2965
Checksum:              305


Coasting Arc #3 (Orbit 2980)
---------------------------------------

Vector Time (GMT): 2020/154/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3608146
61                 A    =         6791007
99  meter
 Y    =        2119668
32  meter          E    =           
0003345
 Z    =        5346058
36                 I    =           51
95695
 XDOT =      -3988
736392                 Wp   =           57
45596
 YDOT =      -6542
848952  meter/sec      RA   =           58
06995  deg
 ZDOT =        -96
086275                 TA   =           33
46683
                                          MA   =           33
44570
                                          Ha   =            228
738  n
mi
                                          Hp   =            221
871

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11837751
34                 X    =        -3657549
63
 Y    =        6954292
39  feet           Y    =         2079042
58  meter
 Z    =       17539561
56                 Z    =         5328411
43
 XDOT =     -13086
405484                 XDOT =       -3914
809121
 YDOT =     -21466
039869  feet/sec       YDOT =       -6587
040477  meter/sec
 ZDOT =       -315
243683                 ZDOT =        -115
283480

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        -615676
16                 X    =         -187658
09
 Y    =      -13818936
02  feet           Y    =        -4212011
70  meter
 Z    =       17458198
91                 Z    =         5321259
03
 XDOT =      24078
366512                 XDOT =        7339
086113
 YDOT =      -1589
536964  feet/sec       YDOT =        -484
490867  meter/sec
 ZDOT =       -403
132820                 ZDOT =        -122
874884


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   20155
02423861  
00016717  00000-0  10270-3 0  9028
2 25544  51
6444  58
5739 0001591  14
9565 345
1632 15
49449369 29817


Satellite: ISS
Catalog Number: 25544
Epoch time:      20155
02423861   =   yrday
fracday
Element set:     902
Inclination:       51
6444  deg
RA of node:        58
5739  deg
Eccentricity:     
0001591     
Arg of perigee:    14
9565  deg
Mean anomaly:     345
1632  deg
Mean motion:   15
49449369  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2981
Checksum:              319


Coasting Arc #4 (Orbit 2995)
---------------------------------------

Vector Time (GMT): 2020/155/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3524622
88                 A    =         6791150
62  meter
 Y    =       -2282821
09  meter          E    =           
0015313
 Z    =       -5350320
81                 I    =           51
93806
 XDOT =       4424
081324                 Wp   =           85
93439
 YDOT =       6235
213735  meter/sec      RA   =           53
14211  deg
 ZDOT =        255
752687                 TA   =          186
48941
                                          MA   =          186
50927
                                          Ha   =            228
691  n
mi
                                          Hp   =            222
016

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11563723
36                 X    =         3575877
26
 Y    =       -7489570
50  feet           Y    =        -2243118
88  meter
 Z    =      -17553545
97                 Z    =        -5333075
18
 XDOT =      14514
702505                 XDOT =        4352
786186
 YDOT =      20456
737975  feet/sec       YDOT =        6284
288288  meter/sec
 ZDOT =        839
083620                 ZDOT =         277
071198

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1454569
75                 X    =          443352
86
 Y    =       13801572
89  feet           Y    =         4206719
42  meter
 Z    =      -17474013
64                 Z    =        -5326079
36
 XDOT =     -23784
781070                 XDOT =       -7249
601270
 YDOT =       3685
675350  feet/sec       YDOT =        1123
393847  meter/sec
 ZDOT =        936
737490                 ZDOT =         285
517587


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   20155
99170809  
00016717  00000-0  10270-3 0  9036
2 25544  51
6442  53
7865 0001654  17
5320 342
5887 15
49412562 29964


Satellite: ISS
Catalog Number: 25544
Epoch time:      20155
99170809   =   yrday
fracday
Element set:     903
Inclination:       51
6442  deg
RA of node:        53
7865  deg
Eccentricity:     
0001654     
Arg of perigee:    17
5320  deg
Mean anomaly:     342
5887  deg
Mean motion:   15
49412562  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2996
Checksum:              324


Coasting Arc #5 (Orbit 3011)
---------------------------------------

Vector Time (GMT): 2020/156/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3432973
91                 A    =         6791053
07  meter
 Y    =        2427096
59  meter          E    =           
0004001
 Z    =        5330609
97                 I    =           51
91794
 XDOT =      -4847
051180                 Wp   =           50
80885
 YDOT =      -5920
838898  meter/sec      RA   =           48
21179  deg
 ZDOT =       -423
047200                 TA   =           43
22841
                                          MA   =           43
19702
                                          Ha   =            228
784  n
mi
                                          Hp   =            221
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11263037
76                 X    =        -3485752
64
 Y    =        7962915
33  feet           Y    =         2388410
60  meter
 Z    =       17488877
85                 Z    =         5313805
95
 XDOT =     -15902
398884                 XDOT =       -4778
427411
 YDOT =     -19425
324467  feet/sec       YDOT =       -5974
658300  meter/sec
 ZDOT =      -1387
950130                 ZDOT =        -446
426923

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2248819
04                 X    =         -685440
04
 Y    =      -13708107
19  feet           Y    =        -4178231
07  meter
 Z    =       17411361
20                 Z    =         5306982
89
 XDOT =      23392
442532                 XDOT =        7130
016484
 YDOT =      -5747
725721  feet/sec       YDOT =       -1751
906800  meter/sec
 ZDOT =      -1495
095929                 ZDOT =        -455
705239


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   20157
02366984  
00016717  00000-0  10270-3 0  9044
2 25544  51
6451  48
6787 0001700  19
6875 340
4341 15
49455807 30121


Satellite: ISS
Catalog Number: 25544
Epoch time:      20157
02366984   =   yrday
fracday
Element set:     904
Inclination:       51
6451  deg
RA of node:        48
6787  deg
Eccentricity:     
0001700     
Arg of perigee:    19
6875  deg
Mean anomaly:     340
4341  deg
Mean motion:   15
49455807  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3012
Checksum:              309


Coasting Arc #6 (Orbit 3026)
---------------------------------------

Vector Time (GMT): 2020/157/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3343994
99                 A    =         6791248
30  meter
 Y    =       -2589415
19  meter          E    =           
0015354
 Z    =       -5326739
61                 I    =           51
89359
 XDOT =       5228
199001                 Wp   =           87
93537
 YDOT =       5553
298522  meter/sec      RA   =           43
28097  deg
 ZDOT =        584
577704                 TA   =          187
62628
                                          MA   =          187
64966
                                          Ha   =            228
795  n
mi
                                          Hp   =            221
906

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10971112
16                 X    =         3398576
52
 Y    =       -8495456
65  feet           Y    =        -2551714
03  meter
 Z    =      -17476179
83                 Z    =        -5310363
60
 XDOT =      17152
883861                 XDOT =        5162
872230
 YDOT =      18219
483341  feet/sec       YDOT =        5611
398585  meter/sec
 ZDOT =       1917
905852                 ZDOT =         609
816873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3090104
15                 X    =          941863
74
 Y    =       13624420
31  feet           Y    =         4152723
31  meter
 Z    =      -17400614
21                 Z    =        -5303707
21
 XDOT =     -22718
160344                 XDOT =       -6924
495273
 YDOT =       7741
503553  feet/sec       YDOT =        2359
610283  meter/sec
 ZDOT =       2033
623753                 ZDOT =         619
848520


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   20157
99113387  
00016717  00000-0  10270-3 0  9058
2 25544  51
6439  43
8912 0001844  24
4215 335
7023 15
49413357 30279


Satellite: ISS
Catalog Number: 25544
Epoch time:      20157
99113387   =   yrday
fracday
Element set:     905
Inclination:       51
6439  deg
RA of node:        43
8912  deg
Eccentricity:     
0001844     
Arg of perigee:    24
4215  deg
Mean anomaly:     335
7023  deg
Mean motion:   15
49413357  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3027
Checksum:              301


Coasting Arc #7 (Orbit 3042)
---------------------------------------

Vector Time (GMT): 2020/158/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3248972
24                 A    =         6791195
52  meter
 Y    =        2732576
52  meter          E    =           
0004789
 Z    =        5297930
06                 I    =           51
86845
 XDOT =      -5595
253398                 Wp   =           49
05904
 YDOT =      -5182
127984  meter/sec      RA   =           38
34791  deg
 ZDOT =       -754
955995                 TA   =           48
15589
                                          MA   =           48
11501
                                          Ha   =            228
860  n
mi
                                          Hp   =            221
711

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10659357
75                 X    =        -3305021
63
 Y    =        8965146
05  feet           Y    =         2695929
72  meter
 Z    =       17381660
29                 Z    =         5282012
21
 XDOT =     -18357
130571                 XDOT =       -5533
222300
 YDOT =     -17001
732231  feet/sec       YDOT =       -5244
351096  meter/sec
 ZDOT =      -2476
889747                 ZDOT =        -781
986023

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3879627
66                 X    =        -1182510
51
 Y    =      -13471935
07  feet           Y    =        -4106245
81  meter
 Z    =       17308186
52                 Z    =         5275535
25
 XDOT =      21956
017123                 XDOT =        6692
194019
 YDOT =      -9679
177608  feet/sec       YDOT =       -2950
213335  meter/sec
 ZDOT =      -2600
869109                 ZDOT =        -792
744905


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   20159
02309173  
00016717  00000-0  10270-3 0  9065
2 25544  51
6438  38
7837 0001767  27
7262 332
3982 15
49455070 30432


Satellite: ISS
Catalog Number: 25544
Epoch time:      20159
02309173   =   yrday
fracday
Element set:     906
Inclination:       51
6438  deg
RA of node:        38
7837  deg
Eccentricity:     
0001767     
Arg of perigee:    27
7262  deg
Mean anomaly:     332
3982  deg
Mean motion:   15
49455070  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3043
Checksum:              311


Coasting Arc #8 (Orbit 3057)
---------------------------------------

Vector Time (GMT): 2020/159/23:25:30
983
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3151325
63                 A    =         6791420
52  meter
 Y    =       -2896862
24  meter          E    =           
0015206
 Z    =       -5285797
02                 I    =           51
84084
 XDOT =       5913
941375                 Wp   =           90
50750
 YDOT =       4764
468001  meter/sec      RA   =           33
41279  deg
 ZDOT =        916
818036                 TA   =          188
24757
                                          MA   =          188
27260
                                          Ha   =            228
857  n
mi
                                          Hp   =            221
822

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10338994
85                 X    =         3209160
29
 Y    =       -9504141
22  feet           Y    =        -2861297
43  meter
 Z    =      -17341853
76                 Z    =        -5270349
28
 XDOT =      19402
694799                 XDOT =        5855
770779
 YDOT =      15631
456696  feet/sec       YDOT =        4830
276463  meter/sec
 ZDOT =       3007
933188                 ZDOT =         945
405255

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4731769
40                 X    =         1442243
31
 Y    =       13315505
06  feet           Y    =         4058565
94  meter
 Z    =      -17270526
62                 Z    =        -5264056
51
 XDOT =     -20930
839106                 XDOT =       -6379
719759
 YDOT =      11500
244740  feet/sec       YDOT =        3505
274597  meter/sec
 ZDOT =       3139
105839                 ZDOT =         956
799460


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   20159
99055179  
00016717  00000-0  10270-3 0  9076
2 25544  51
6430  33
9953 0001864  31
1190 329
0071 15
49414565 30589


Satellite: ISS
Catalog Number: 25544
Epoch time:      20159
99055179   =   yrday
fracday
Element set:     907
Inclination:       51
6430  deg
RA of node:        33
9953  deg
Eccentricity:     
0001864     
Arg of perigee:    31
1190  deg
Mean anomaly:     329
0071  deg
Mean motion:   15
49414565  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3058
Checksum:              309


Coasting Arc #9 (Orbit 3061)
---------------------------------------

Vector Time (GMT): 2020/160/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2883071
08                 A    =         6791244
06  meter
 Y    =        3108160
67  meter          E    =           
0005078
 Z    =        5302433
60                 I    =           51
83188
 XDOT =      -6147
233969                 Wp   =           50
37641
 YDOT =      -4524
926979  meter/sec      RA   =           32
30319  deg
 ZDOT =       -686
412437                 TA   =           46
18598
                                          MA   =           46
14400
                                          Ha   =            229
040  n
mi
                                          Hp   =            221
618

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9458894
62                 X    =        -2943369
26
 Y    =       10197377
53  feet           Y    =         3075581
90  meter
 Z    =       17396435
71                 Z    =         5288283
00
 XDOT =     -20168
090451                 XDOT =       -6092
843833
 YDOT =     -14845
560955  feet/sec       YDOT =       -4593
365472  meter/sec
 ZDOT =      -2252
009307                 ZDOT =        -716
141989

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13485680
19                 X    =        -4110435
32
 Y    =        3723432
26  feet           Y    =         1134902
15  meter
 Z    =       17331060
36                 Z    =         5282507
20
 XDOT =      -9209
177419                 XDOT =       -2806
957277
 YDOT =     -22181
793848  feet/sec       YDOT =       -6761
010765  meter/sec
 ZDOT =      -2388
457279                 ZDOT =        -728
001779


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   20160
24854082  
00016717  00000-0  10270-3 0  9087
2 25544  51
6408  32
7188 0002134  33
5837 326
5448 15
49427567 30627


Satellite: ISS
Catalog Number: 25544
Epoch time:      20160
24854082   =   yrday
fracday
Element set:     908
Inclination:       51
6408  deg
RA of node:        32
7188  deg
Eccentricity:     
0002134     
Arg of perigee:    33
5837  deg
Mean anomaly:     326
5448  deg
Mean motion:   15
49427567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3062
Checksum:              308


Coasting Arc #10 (Orbit 3076)
---------------------------------------

Vector Time (GMT): 2020/161/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2767647
68                 A    =         6791372
71  meter
 Y    =       -3255956
96  meter          E    =           
0015649
 Z    =       -5291914
10                 I    =           51
80364
 XDOT =       6417
032730                 Wp   =           89
26635
 YDOT =       4075
346843  meter/sec      RA   =           27
36553  deg
 ZDOT =        851
013318                 TA   =          188
85817
                                          MA   =          188
88582
                                          Ha   =            229
003  n
mi
                                          Hp   =            221
660

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9080208
92                 X    =         2829555
95
 Y    =      -10682273
48  feet           Y    =        -3224660
02  meter
 Z    =      -17361922
90                 Z    =        -5278320
29
 XDOT =      21053
256987                 XDOT =        6366
850362
 YDOT =      13370
560510  feet/sec       YDOT =        4146
825926  meter/sec
 ZDOT =       2792
038444                 ZDOT =         882
063392

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13337972
07                 X    =         4065413
89
 Y    =       -4564786
58  feet           Y    =        -1391346
95  meter
 Z    =      -17299096
86                 Z    =        -5272764
72
 XDOT =      11051
249278                 XDOT =        3368
420780
 YDOT =      21199
366322  feet/sec       YDOT =        6461
566855  meter/sec
 ZDOT =       2934
594797                 ZDOT =         894
464494


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   20161
21599611  
00016717  00000-0  10270-3 0  9090
2 25544  51
6414  27
9302 0002249  36
4288 323
7015 15
49418123 30770


Satellite: ISS
Catalog Number: 25544
Epoch time:      20161
21599611   =   yrday
fracday
Element set:     909
Inclination:       51
6414  deg
RA of node:        27
9302  deg
Eccentricity:     
0002249     
Arg of perigee:    36
4288  deg
Mean anomaly:     323
7015  deg
Mean motion:   15
49418123  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3077
Checksum:              294


Coasting Arc #11 (Orbit 3092)
---------------------------------------

Vector Time (GMT): 2020/162/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2652102
43                 A    =         6791441
50  meter
 Y    =        3383014
78  meter          E    =           
0005952
 Z    =        5254531
87                 I    =           51
77304
 XDOT =      -6672
005214                 Wp   =           49
61951
 YDOT =      -3628
532861  meter/sec      RA   =           22
42580  deg
 ZDOT =      -1026
860265                 TA   =           50
22702
                                          MA   =           50
17462
                                          Ha   =            229
105  n
mi
                                          Hp   =            221
529

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8701123
47                 X    =        -2715258
46
 Y    =       11099129
85  feet           Y    =         3353003
08  meter
 Z    =       17239277
80                 Z    =         5241496
28
 XDOT =     -21889
780887                 XDOT =       -6625
946155
 YDOT =     -11904
635372  feet/sec       YDOT =       -3702
886272  meter/sec
 ZDOT =      -3368
964124                 ZDOT =       -1059
158685

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13131064
90                 X    =        -4002348
58
 Y    =        5343186
03  feet           Y    =         1628603
10  meter
 Z    =       17179011
31                 Z    =         5236162
65
 XDOT =     -12819
048707                 XDOT =       -3907
246046
 YDOT =     -20146
784118  feet/sec       YDOT =       -6140
739799  meter/sec
 ZDOT =      -3517
295609                 ZDOT =       -1072
071702


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   20162
24794709  
00016717  00000-0  10270-3 0  9101
2 25544  51
6408  22
8222 0002268  38
4780 321
6531 15
49430453 30936


Satellite: ISS
Catalog Number: 25544
Epoch time:      20162
24794709   =   yrday
fracday
Element set:     910
Inclination:       51
6408  deg
RA of node:        22
8222  deg
Eccentricity:     
0002268     
Arg of perigee:    38
4780  deg
Mean anomaly:     321
6531  deg
Mean motion:   15
49430453  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3093
Checksum:              291


Coasting Arc #12 (Orbit 3107)
---------------------------------------

Vector Time (GMT): 2020/163/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2524514
69                 A    =         6791591
93  meter
 Y    =       -3533146
92  meter          E    =           
0015309
 Z    =       -5235337
70                 I    =           51
74204
 XDOT =       6869
229838                 Wp   =           91
79193
 YDOT =       3147
998832  meter/sec      RA   =           17
48418  deg
 ZDOT =       1190
461349                 TA   =          189
62474
                                          MA   =          189
65410
                                          Ha   =            229
022  n
mi
                                          Hp   =            221
597

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8282528
52                 X    =         2589265
80
 Y    =      -11591689
36  feet           Y    =        -3504553
19  meter
 Z    =      -17176304
78                 Z    =        -5222917
96
 XDOT =      22536
843301                 XDOT =        6827
734922
 YDOT =      10328
080157  feet/sec       YDOT =        3224
583265  meter/sec
 ZDOT =       3905
713088                 ZDOT =        1223
728744

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12902984
20                 X    =         3932829
58
 Y    =       -6200848
81  feet           Y    =        -1890018
72  meter
 Z    =      -17118862
69                 Z    =        -5217829
35
 XDOT =      14433
507385                 XDOT =        4399
333051
 YDOT =      18852
481102  feet/sec       YDOT =        5746
236240  meter/sec
 ZDOT =       4058
534834                 ZDOT =        1237
041417


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   20163
21539974  
00016717  00000-0  10270-3 0  9111
2 25544  51
6410  18
0337 0002235  40
4197 319
7119 15
49425663 31086


Satellite: ISS
Catalog Number: 25544
Epoch time:      20163
21539974   =   yrday
fracday
Element set:     911
Inclination:       51
6410  deg
RA of node:        18
0337  deg
Eccentricity:     
0002235     
Arg of perigee:    40
4197  deg
Mean anomaly:     319
7119  deg
Mean motion:   15
49425663  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3108
Checksum:              291


Coasting Arc #13 (Orbit 3123)
---------------------------------------

Vector Time (GMT): 2020/164/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2399899
18                 A    =         6791699
77  meter
 Y    =        3662124
35  meter          E    =           
0006727
 Z    =        5188336
74                 I    =           51
71130
 XDOT =      -7050
656372                 Wp   =           50
53407
 YDOT =      -2674
692556  meter/sec      RA   =           12
54033  deg
 ZDOT =      -1368
068036                 TA   =           52
64204
                                          MA   =           52
58078
                                          Ha   =            229
110  n
mi
                                          Hp   =            221
473

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7873684
98                 X    =        -2465873
55
 Y    =       12014843
67  feet           Y    =         3634917
40  meter
 Z    =       17022102
17                 Z    =         5176519
30
 XDOT =     -23132
074711                 XDOT =       -7013
577909
 YDOT =      -8775
238045  feet/sec       YDOT =       -2753
330520  meter/sec
 ZDOT =      -4488
412190                 ZDOT =       -1402
227394

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12625459
91                 X    =        -3848240
18
 Y    =        6986243
92  feet           Y    =         2129407
15  meter
 Z    =       16967424
78                 Z    =         5171671
07
 XDOT =     -15954
449536                 XDOT =       -4862
916219
 YDOT =     -17507
692071  feet/sec       YDOT =       -5336
344543  meter/sec
 ZDOT =      -4645
366734                 ZDOT =       -1415
907780


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   20164
24734700  
00016717  00000-0  10270-3 0  9120
2 25544  51
6422  12
9258 0002253  42
9545 317
1781 15
49439180 31242


Satellite: ISS
Catalog Number: 25544
Epoch time:      20164
24734700   =   yrday
fracday
Element set:     912
Inclination:       51
6422  deg
RA of node:        12
9258  deg
Eccentricity:     
0002253     
Arg of perigee:    42
9545  deg
Mean anomaly:     317
1781  deg
Mean motion:   15
49439180  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3124
Checksum:              286


Coasting Arc #14 (Orbit 3138)
---------------------------------------

Vector Time (GMT): 2020/165/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2258076
44                 A    =         6791866
16  meter
 Y    =       -3813219
41  meter          E    =           
0014917
 Z    =       -5159958
31                 I    =           51
67882
 XDOT =       7171
319583                 Wp   =           93
97885
 YDOT =       2177
546195  meter/sec      RA   =            7
59405  deg
 ZDOT =       1531
888811                 TA   =          190
79367
                                          MA   =          190
82572
                                          Ha   =            229
055  n
mi
                                          Hp   =            221
495

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7408387
28                 X    =         2325613
16
 Y    =      -12510562
36  feet           Y    =        -3787589
74  meter
 Z    =      -16928997
07                 Z    =        -5148825
94
 XDOT =      23527
951388                 XDOT =        7138
995628
 YDOT =       7144
180431  feet/sec       YDOT =        2257
560078  meter/sec
 ZDOT =       5025
881925                 ZDOT =        1566
645857

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12306913
76                 X    =         3751147
31
 Y    =       -7853687
54  feet           Y    =        -2393803
96  meter
 Z    =      -16877463
68                 Z    =        -5144250
93
 XDOT =      17283
080386                 XDOT =        5267
882902
 YDOT =      15959
131344  feet/sec       YDOT =        4864
343234  meter/sec
 ZDOT =       5185
614968                 ZDOT =        1580
575442


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   20165
21479439  
00016717  00000-0  10270-3 0  9134
2 25544  51
6423   8
1370 0002310  44
7645 315
3691 15
49441086 31394


Satellite: ISS
Catalog Number: 25544
Epoch time:      20165
21479439   =   yrday
fracday
Element set:     913
Inclination:       51
6423  deg
RA of node:         8
1370  deg
Eccentricity:     
0002310     
Arg of perigee:    44
7645  deg
Mean anomaly:     315
3691  deg
Mean motion:   15
49441086  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3139
Checksum:              292


Coasting Arc #15 (Orbit 3154)
---------------------------------------

Vector Time (GMT): 2020/166/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2121016
15                 A    =         6792050
47  meter
 Y    =        3943937
43  meter          E    =           
0007686
 Z    =        5102630
89                 I    =           51
64578
 XDOT =      -7276
726816                 Wp   =           52
62442
 YDOT =      -1691
607671  meter/sec      RA   =            2
64637  deg
 ZDOT =      -1710
910226                 TA   =           53
95026
                                          MA   =           53
87908
                                          Ha   =            229
170  n
mi
                                          Hp   =            221
379

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6958714
40                 X    =        -2189746
40
 Y    =       12939427
25  feet           Y    =         3919833
81  meter
 Z    =       16740915
00                 Z    =         5092161
38
 XDOT =     -23873
775644                 XDOT =       -7248
959329
 YDOT =      -5549
893934  feet/sec       YDOT =       -1772
825753  meter/sec
 ZDOT =      -5613
222526                 ZDOT =       -1746
190415

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11947111
93                 X    =        -3641479
72
 Y    =        8645241
00  feet           Y    =         2635069
46  meter
 Z    =       16692424
73                 Z    =         5087851
06
 XDOT =     -18506
420658                 XDOT =       -5640
757016
 YDOT =     -14383
078739  feet/sec       YDOT =       -4383
962400  meter/sec
 ZDOT =      -5775
388669                 ZDOT =       -1760
338466


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   20166
24673770  
00016717  00000-0  10270-3 0  9143
2 25544  51
6421   3
0298 0002382  48
2819 311
8535 15
49443526 31553


Satellite: ISS
Catalog Number: 25544
Epoch time:      20166
24673770   =   yrday
fracday
Element set:     914
Inclination:       51
6421  deg
RA of node:         3
0298  deg
Eccentricity:     
0002382     
Arg of perigee:    48
2819  deg
Mean anomaly:     311
8535  deg
Mean motion:   15
49443526  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3155
Checksum:              300


Coasting Arc #16 (Orbit 3169)
---------------------------------------

Vector Time (GMT): 2020/167/04:50:00
000
Vector Time (MET): N/A
Weight (LBS)     : 980095
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1959049
30                 A    =         6792233
57  meter
 Y    =       -4094992
56  meter          E    =           
0014409
 Z    =       -5065357
82                 I    =           51
61275
 XDOT =       7321
022468                 Wp   =           96
43246
 YDOT =       1190
004349  meter/sec      RA   =          357
69581  deg
 ZDOT =       1872
418637                 TA   =          191
74678
                                          MA   =          191
78043
                                          Ha   =            229
082  n
mi
                                          Hp   =            221
411

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6427327
11                 X    =         2029299
77
 Y    =      -13435014
95  feet           Y    =        -4072691
65  meter
 Z    =      -16618628
02                 Z    =        -5055671
39
 XDOT =      24019
102586                 XDOT =        7298
076222
 YDOT =       3904
213742  feet/sec       YDOT =        1271
744707  meter/sec
 ZDOT =       6143
105765                 ZDOT =        1907
925768

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11517452
49                 X    =         3510519
52
 Y    =       -9520959
44  feet           Y    =        -2901988
44  meter
 Z    =      -16573731
54                 Z    =        -5051673
37
 XDOT =      19512
640051                 XDOT =        5947
452688
 YDOT =      12643
767440  feet/sec       YDOT =        3853
820316  meter/sec
 ZDOT =       6306
343137                 ZDOT =        1922
173388


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   20167
21418279  
00016717  00000-0  10270-3 0  9153
2 25544  51
6422 358
2412 0002304  50
8950 309
2405 15
49450717 31700


Satellite: ISS
Catalog Number: 25544
Epoch time:      20167
21418279   =   yrday
fracday
Element set:     915
Inclination:       51
6422  deg
RA of node:       358
2412  deg
Eccentricity:     
0002304     
Arg of perigee:    50
8950  deg
Mean anomaly:     309
2405  deg
Mean motion:   15
49450717  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3170
Checksum:              287
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