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

 
Date: March 16th 2020

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 14255 723 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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


073/05:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 1
000/00:00:00 000 0 0 0 0 221 5

079/17:18:26 637 1 0 1 9 1 9
N/A 1 5 0 0 230 7
000/00:08:53 274 -0 6 -0 0 221 9

081/01:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 7
000/00:00:00 000 0 0 0 0 221 7

085/12:40:00 000 0 0 0 0 0 0
N/A 0 0 0 0 230 9
000/00:00:00 000 0 0 0 0 221 4

Coasting Arc #1 (Orbit 1686)
---------------------------------------

Vector Time (GMT): 2020/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4063546
67                 A    =         6791669
46  meter
 Y    =       -1049794
44  meter          E    =           
0006298
 Z    =        5336016
37                 I    =           51
98361
 XDOT =       2413
941241                 Wp   =           38
54121
 YDOT =      -7262
301576  meter/sec      RA   =          110
81054  deg
 ZDOT =        414
055797                 TA   =           47
55333
                                          MA   =           47
50009
                                          Ha   =            230
180  n
mi
                                          Hp   =            221
559

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13331846
02                 X    =        -4077424
62
 Y    =       -3444207
48  feet           Y    =        -1095312
84  meter
 Z    =       17506615
38                 Z    =         5316243
87
 XDOT =       7919
754729                 XDOT =        2492
959804
 YDOT =     -23826
448741  feet/sec       YDOT =       -7234
865296  meter/sec
 ZDOT =       1358
450776                 ZDOT =         425
974491

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12516021
58                 X    =        -3814883
38
 Y    =       -6009778
37  feet           Y    =        -1831780
45  meter
 Z    =       17415913
22                 Z    =         5308370
35
 XDOT =      11983
442490                 XDOT =        3652
553271
 YDOT =     -20904
090065  feet/sec       YDOT =       -6371
566652  meter/sec
 ZDOT =       1413
433450                 ZDOT =         430
814515


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   20071
54914440  
00016717  00000-0  10270-3 0  9008
2 25544  51
6410 111
5742 0005954  13
5438 346
5870 15
49242261 16878


Satellite: ISS
Catalog Number: 25544
Epoch time:      20071
54914440   =   yrday
fracday
Element set:     900
Inclination:       51
6410  deg
RA of node:       111
5742  deg
Eccentricity:     
0005954     
Arg of perigee:    13
5438  deg
Mean anomaly:     346
5870  deg
Mean motion:   15
49242261  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1687
Checksum:              290


Coasting Arc #2 (Orbit 1701)
---------------------------------------

Vector Time (GMT): 2020/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4124558
43                 A    =         6791727
88  meter
 Y    =         787724
23  meter          E    =           
0017620
 Z    =       -5352562
14                 I    =           51
99487
 XDOT =      -1845
627695                 Wp   =           69
03257
 YDOT =       7414
862519  meter/sec      RA   =          105
88626  deg
 ZDOT =       -325
713328                 TA   =          197
83820
                                          MA   =          197
90013
                                          Ha   =            230
146  n
mi
                                          Hp   =            221
636

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13532015
84                 X    =         4141442
87
 Y    =        2584397
08  feet           Y    =          833941
80  meter
 Z    =      -17560899
42                 Z    =        -5332485
84
 XDOT =      -6055
208972                 XDOT =       -1926
823583
 YDOT =      24326
976768  feet/sec       YDOT =        7393
769367  meter/sec
 ZDOT =      -1068
613282                 ZDOT =        -334
876632

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12968639
99                 X    =         3952841
47
 Y    =        4983518
06  feet           Y    =         1518976
30  meter
 Z    =      -17468791
43                 Z    =        -5324487
63
 XDOT =      -9938
196003                 XDOT =       -3029
162142
 YDOT =      21907
146664  feet/sec       YDOT =        6677
298303  meter/sec
 ZDOT =      -1110
976646                 ZDOT =        -338
625682


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   20072
51672563  
00016717  00000-0  10270-3 0  9014
2 25544  51
6415 106
7862 0005908  16
6137 343
5205 15
49220277 17021


Satellite: ISS
Catalog Number: 25544
Epoch time:      20072
51672563   =   yrday
fracday
Element set:     901
Inclination:       51
6415  deg
RA of node:       106
7862  deg
Eccentricity:     
0005908     
Arg of perigee:    16
6137  deg
Mean anomaly:     343
5205  deg
Mean motion:   15
49220277  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1702
Checksum:              289


Coasting Arc #3 (Orbit 1712)
---------------------------------------

Vector Time (GMT): 2020/073/05:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3799039
49                 A    =         6791903
57  meter
 Y    =        1966313
08  meter          E    =           
0016497
 Z    =       -5288926
24                 I    =           52
00082
 XDOT =      -2367
631346                 Wp   =           78
06020
 YDOT =       7206
437345  meter/sec      RA   =          102
36825  deg
 ZDOT =        984
438420                 TA   =          201
30519
                                          MA   =          201
37396
                                          Ha   =            230
085  n
mi
                                          Hp   =            221
527

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12464040
31                 X    =         3802459
74
 Y    =        6451158
39  feet           Y    =         2008815
27  meter
 Z    =      -17352120
22                 Z    =        -5270463
94
 XDOT =      -7767
819378                 XDOT =       -2452
821710
 YDOT =      23643
167142  feet/sec       YDOT =        7179
484569  meter/sec
 ZDOT =       3229
784844                 ZDOT =         972
729863

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10908976
50                 X    =        -3325056
04
 Y    =        8994138
42  feet           Y    =         2741413
39  meter
 Z    =      -17267470
21                 Z    =        -5263124
92
 XDOT =     -17963
076369                 XDOT =       -5475
145677
 YDOT =     -15727
812747  feet/sec       YDOT =       -4793
837325  meter/sec
 ZDOT =       3175
732481                 ZDOT =         967
963260


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   20073
22628431  
00016717  00000-0  10270-3 0  9029
2 25544  51
6405 103
2720 0005634  19
8214 340
3154 15
49251689 17133


Satellite: ISS
Catalog Number: 25544
Epoch time:      20073
22628431   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:       103
2720  deg
Eccentricity:     
0005634     
Arg of perigee:    19
8214  deg
Mean anomaly:     340
3154  deg
Mean motion:   15
49251689  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1713
Checksum:              276


Coasting Arc #4 (Orbit 1728)
---------------------------------------

Vector Time (GMT): 2020/074/05:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3915983
49                 A    =         6792031
33  meter
 Y    =       -1752067
68  meter          E    =           
0009139
 Z    =        5262094
62                 I    =           52
00834
 XDOT =       1820
240286                 Wp   =           36
71392
 YDOT =      -7364
383650  meter/sec      RA   =           97
44366  deg
 ZDOT =      -1089
347048                 TA   =           63
72373
                                          MA   =           63
62985
                                          Ha   =            230
329  n
mi
                                          Hp   =            221
311

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12847714
88                 X    =        -3921660
48
 Y    =       -5748253
54  feet           Y    =        -1795890
38  meter
 Z    =       17264089
95                 Z    =         5243058
70
 XDOT =       5971
916949                 XDOT =        1907
747120
 YDOT =     -24161
363681  feet/sec       YDOT =       -7343
539221  meter/sec
 ZDOT =      -3573
973255                 ZDOT =       -1080
292031

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10248400
90                 X    =         3123712
60
 Y    =       -9802186
29  feet           Y    =        -2987706
38  meter
 Z    =       17176798
91                 Z    =         5235488
31
 XDOT =      19347
344564                 XDOT =        5897
070623
 YDOT =      13991
872490  feet/sec       YDOT =        4264
722735  meter/sec
 ZDOT =      -3532
069095                 ZDOT =       -1076
574660


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   20074
25836746  
00016717  00000-0  10270-3 0  9034
2 25544  51
6417  98
1636 0005757  23
5809 336
5604 15
49230577 17299


Satellite: ISS
Catalog Number: 25544
Epoch time:      20074
25836746   =   yrday
fracday
Element set:     903
Inclination:       51
6417  deg
RA of node:        98
1636  deg
Eccentricity:     
0005757     
Arg of perigee:    23
5809  deg
Mean anomaly:     336
5604  deg
Mean motion:   15
49230577  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1729
Checksum:              327


Coasting Arc #5 (Orbit 1743)
---------------------------------------

Vector Time (GMT): 2020/075/05:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4045267
44                 A    =         6792009
01  meter
 Y    =        1500177
57  meter          E    =           
0016889
 Z    =       -5259467
65                 I    =           52
01207
 XDOT =      -1246
052440                 Wp   =           79
97579
 YDOT =       7454
621579  meter/sec      RA   =           92
52205  deg
 ZDOT =       1173
977305                 TA   =          201
21905
                                          MA   =          201
28918
                                          Ha   =            230
260  n
mi
                                          Hp   =            221
258

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13271874
82                 X    =         4053738
72
 Y    =        4921842
43  feet           Y    =         1545461
74  meter
 Z    =      -17255471
30                 Z    =        -5239796
93
 XDOT =      -4088
098558                 XDOT =       -1335
022089
 YDOT =      24457
419879  feet/sec       YDOT =        7440
189931  meter/sec
 ZDOT =       3851
631577                 ZDOT =        1167
708053

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9463350
31                 X    =        -2884429
17
 Y    =       10673215
43  feet           Y    =         3253196
06  meter
 Z    =      -17165254
35                 Z    =        -5231969
53
 XDOT =     -20496
167740                 XDOT =       -6247
231927
 YDOT =     -12057
411066  feet/sec       YDOT =       -3675
098893  meter/sec
 ZDOT =       3822
486494                 ZDOT =        1165
093884


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   20075
22594236  
00016717  00000-0  10270-3 0  9048
2 25544  51
6421  93
3769 0005790  27
4958 332
6497 15
49262971 17440


Satellite: ISS
Catalog Number: 25544
Epoch time:      20075
22594236   =   yrday
fracday
Element set:     904
Inclination:       51
6421  deg
RA of node:        93
3769  deg
Eccentricity:     
0005790     
Arg of perigee:    27
4958  deg
Mean anomaly:     332
6497  deg
Mean motion:   15
49262971  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1744
Checksum:              332


Coasting Arc #6 (Orbit 1759)
---------------------------------------

Vector Time (GMT): 2020/076/05:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4139736
00                 A    =         6792131
13  meter
 Y    =       -1272330
43  meter          E    =           
0009795
 Z    =        5228115
23                 I    =           52
01267
 XDOT =        685
153215                 Wp   =           41
10296
 YDOT =      -7525
451284  meter/sec      RA   =           87
59858  deg
 ZDOT =      -1280
361097                 TA   =           61
18343
                                          MA   =           61
08512
                                          Ha   =            230
462  n
mi
                                          Hp   =            221
059

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13581811
02                 X    =        -4150595
73
 Y    =       -4174312
44  feet           Y    =        -1318684
42  meter
 Z    =       17152609
03                 Z    =         5207979
86
 XDOT =       2247
878003                 XDOT =         775
473318
 YDOT =     -24689
800801  feet/sec       YDOT =       -7517
284451  meter/sec
 ZDOT =      -4200
659767                 ZDOT =       -1276
813266

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8685461
90                 X    =         2647328
79
 Y    =      -11384780
02  feet           Y    =        -3470080
95  meter
 Z    =       17060246
39                 Z    =         5199963
10
 XDOT =      21518
708719                 XDOT =        6558
902418
 YDOT =      10104
696462  feet/sec       YDOT =        3079
911482  meter/sec
 ZDOT =      -4183
982041                 ZDOT =       -1275
277726


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   20076
25802236  
00016717  00000-0  10270-3 0  9055
2 25544  51
6421  88
2692 0005827  30
8953 329
2539 15
49249459 17605


Satellite: ISS
Catalog Number: 25544
Epoch time:      20076
25802236   =   yrday
fracday
Element set:     905
Inclination:       51
6421  deg
RA of node:        88
2692  deg
Eccentricity:     
0005827     
Arg of perigee:    30
8953  deg
Mean anomaly:     329
2539  deg
Mean motion:   15
49249459  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1760
Checksum:              324


Coasting Arc #7 (Orbit 1774)
---------------------------------------

Vector Time (GMT): 2020/077/05:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4241677
82                 A    =         6792152
21  meter
 Y    =        1003785
26  meter          E    =           
0017075
 Z    =       -5223150
36                 I    =           52
01112
 XDOT =       -107
617180                 Wp   =           82
27332
 YDOT =       7524
906112  meter/sec      RA   =           82
67718  deg
 ZDOT =       1364
785542                 TA   =          200
77768
                                          MA   =          200
84718
                                          Ha   =            230
365  n
mi
                                          Hp   =            221
063

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13916265
81                 X    =         4255508
72
 Y    =        3293258
72  feet           Y    =         1051295
86  meter
 Z    =      -17136320
08                 Z    =        -5202512
65
 XDOT =       -353
074737                 XDOT =        -198
384168
 YDOT =      24688
012179  feet/sec       YDOT =        7523
195200  meter/sec
 ZDOT =       4477
642853                 ZDOT =        1364
042057

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7768474
77                 X    =        -2367831
11
 Y    =       12140631
75  feet           Y    =         3700464
56  meter
 Z    =      -17041635
30                 Z    =        -5194290
44
 XDOT =     -22272
367983                 XDOT =       -6788
617761
 YDOT =      -7999
658088  feet/sec       YDOT =       -2438
295785  meter/sec
 ZDOT =       4473
820494                 ZDOT =        1363
620487


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   20077
22559558  
00016717  00000-0  10270-3 0  9060
2 25544  51
6428  83
4827 0005795  34
4953 325
6572 15
49270671 17756


Satellite: ISS
Catalog Number: 25544
Epoch time:      20077
22559558   =   yrday
fracday
Element set:     906
Inclination:       51
6428  deg
RA of node:        83
4827  deg
Eccentricity:     
0005795     
Arg of perigee:    34
4953  deg
Mean anomaly:     325
6572  deg
Mean motion:   15
49270671  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1775
Checksum:              340


Coasting Arc #8 (Orbit 1790)
---------------------------------------

Vector Time (GMT): 2020/078/05:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4312036
61                 A    =         6792240
16  meter
 Y    =        -764407
91  meter          E    =           
0010413
 Z    =        5187240
63                 I    =           52
00662
 XDOT =       -452
165396                 Wp   =           44
84785
 YDOT =      -7508
133686  meter/sec      RA   =           77
75293  deg
 ZDOT =      -1473
318725                 TA   =           59
32094
                                          MA   =           59
21836
                                          Ha   =            230
551  n
mi
                                          Hp   =            220
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14147101
75                 X    =        -4328364
56
 Y    =       -2507899
98  feet           Y    =         -812719
24  meter
 Z    =       17018505
99                 Z    =         5166255
14
 XDOT =      -1483
482269                 XDOT =        -361
017194
 YDOT =     -24632
984533  feet/sec       YDOT =       -7512
680543  meter/sec
 ZDOT =      -4833
722851                 ZDOT =       -1475
293428

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6886097
82                 X    =         2098882
61
 Y    =      -12738919
46  feet           Y    =        -3882822
65  meter
 Z    =       16922209
80                 Z    =         5157889
55
 XDOT =      22900
140645                 XDOT =        6979
962869
 YDOT =       5906
921720  feet/sec       YDOT =        1800
429740  meter/sec
 ZDOT =      -4842
364837                 ZDOT =       -1475
952802


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   20078
25767087  
00016717  00000-0  10270-3 0  9073
2 25544  51
6434  78
3746 0005892  37
1745 322
9812 15
49274697 17910


Satellite: ISS
Catalog Number: 25544
Epoch time:      20078
25767087   =   yrday
fracday
Element set:     907
Inclination:       51
6434  deg
RA of node:        78
3746  deg
Eccentricity:     
0005892     
Arg of perigee:    37
1745  deg
Mean anomaly:     322
9812  deg
Mean motion:   15
49274697  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1791
Checksum:              347


Coasting Arc #9 (Orbit 1805)
---------------------------------------

Vector Time (GMT): 2020/079/05:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939740
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4384752
56                 A    =         6792334
12  meter
 Y    =         482966
53  meter          E    =           
0017280
 Z    =       -5179343
61                 I    =           51
99837
 XDOT =       1017
082829                 Wp   =           84
12951
 YDOT =       7418
211240  meter/sec      RA   =           72
83070  deg
 ZDOT =       1558
966504                 TA   =          200
82675
                                          MA   =          200
89724
                                          Ha   =            230
515  n
mi
                                          Hp   =            220
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14385671
13                 X    =         4404183
86
 Y    =        1584535
87  feet           Y    =          532108
31  meter
 Z    =      -16992597
14                 Z    =        -5157997
40
 XDOT =       3336
885923                 XDOT =         926
482175
 YDOT =      24337
963385  feet/sec       YDOT =        7429
078491  meter/sec
 ZDOT =       5114
719501                 ZDOT =        1563
686539

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5856474
06                 X    =        -1785053
29
 Y    =       13359636
89  feet           Y    =         4072017
32  meter
 Z    =      -16894628
11                 Z    =        -5149482
65
 XDOT =     -23234
998897                 XDOT =       -7082
027664
 YDOT =      -3716
397862  feet/sec       YDOT =       -1132
758068  meter/sec
 ZDOT =       5135
957426                 ZDOT =        1565
439823


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   20079
22524012  
00016717  00000-0  10270-3 0  9081
2 25544  51
6432  73
5880 0005972  41
0302 319
1296 15
49275255 18068


Satellite: ISS
Catalog Number: 25544
Epoch time:      20079
22524012   =   yrday
fracday
Element set:     908
Inclination:       51
6432  deg
RA of node:        73
5880  deg
Eccentricity:     
0005972     
Arg of perigee:    41
0302  deg
Mean anomaly:     319
1296  deg
Mean motion:   15
49275255  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1806
Checksum:              293


Coasting Arc #10 (Orbit 1813)
---------------------------------------

Vector Time (GMT): 2020/079/17:22:53
274
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3721878
01                 A    =         6792702
78  meter
 Y    =       -1985675
00  meter          E    =           
0018187
 Z    =       -5339464
28                 I    =           51
99030
 XDOT =       2963
955264                 Wp   =           72
88371
 YDOT =       7027
902145  meter/sec      RA   =           70
32766  deg
 ZDOT =       -543
889009                 TA   =          191
91539
                                          MA   =          191
95847
                                          Ha   =            230
655  n
mi
                                          Hp   =            221
867

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12210885
87                 X    =         3769741
40
 Y    =       -6514681
75  feet           Y    =        -1943787
04  meter
 Z    =      -17517927
44                 Z    =        -5321268
80
 XDOT =       9724
262678                 XDOT =        2887
788758
 YDOT =      23057
421735  feet/sec       YDOT =        7060
621290  meter/sec
 ZDOT =      -1784
412760                 ZDOT =        -529
676981

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3701578
61                 X    =        -1128241
16
 Y    =      -13445031
37  feet           Y    =        -4098045
56  meter
 Z    =      -17434277
76                 Z    =        -5313967
86
 XDOT =      23634
609224                 XDOT =        7203
828892
 YDOT =      -4261
426777  feet/sec       YDOT =       -1298
882882  meter/sec
 ZDOT =      -1719
581274                 ZDOT =        -524
128372


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   20079
74127953  
00016717  00000-0  10270-3 0  9092
2 25544  51
6427  71
0371 0005069  32
9001 327
2464 15
48905567 18143


Satellite: ISS
Catalog Number: 25544
Epoch time:      20079
74127953   =   yrday
fracday
Element set:     909
Inclination:       51
6427  deg
RA of node:        71
0371  deg
Eccentricity:     
0005069     
Arg of perigee:    32
9001  deg
Mean anomaly:     327
2464  deg
Mean motion:   15
48905567  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1814
Checksum:              309


Coasting Arc #11 (Orbit 1829)
---------------------------------------

Vector Time (GMT): 2020/080/17:22:53
274
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3515498
32                 A    =         6792636
04  meter
 Y    =        2321201
51  meter          E    =           
0006156
 Z    =        5323614
96                 I    =           51
97763
 XDOT =      -3585
748042                 Wp   =           61
62877
 YDOT =      -6749
585103  meter/sec      RA   =           65
40689  deg
 ZDOT =        577
410731                 TA   =           22
89743
                                          MA   =           22
87000
                                          Ha   =            230
741  n
mi
                                          Hp   =            221
699

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11533787
13                 X    =        -3567052
02
 Y    =        7615490
51  feet           Y    =         2281600
89  meter
 Z    =       17465928
34                 Z    =         5306412
94
 XDOT =     -11764
265229                 XDOT =       -3512
810373
 YDOT =     -22144
308082  feet/sec       YDOT =       -6789
275620  meter/sec
 ZDOT =       1894
392163                 ZDOT =         560
170584

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5145879
10                 X    =         1568463
95
 Y    =       12934492
79  feet           Y    =         3942433
40  meter
 Z    =       17386817
38                 Z    =         5299501
94
 XDOT =     -23101
399792                 XDOT =       -7041
306657
 YDOT =       6760
424269  feet/sec       YDOT =        2060
577317  meter/sec
 ZDOT =       1815
653279                 ZDOT =         553
411119


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   20080
77359311  
00016717  00000-0  10270-3 0  9104
2 25544  51
6424  65
9318 0004892  35
3310 324
8163 15
48925309 18309


Satellite: ISS
Catalog Number: 25544
Epoch time:      20080
77359311   =   yrday
fracday
Element set:     910
Inclination:       51
6424  deg
RA of node:        65
9318  deg
Eccentricity:     
0004892     
Arg of perigee:    35
3310  deg
Mean anomaly:     324
8163  deg
Mean motion:   15
48925309  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1830
Checksum:              297


Coasting Arc #12 (Orbit 1834)
---------------------------------------

Vector Time (GMT): 2020/081/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2855423
54                 A    =         6793358
04  meter
 Y    =        3351703
92  meter          E    =           
0006867
 Z    =        5167165
12                 I    =           51
97309
 XDOT =      -4357
929099                 Wp   =           83
01547
 YDOT =      -6111
129233  meter/sec      RA   =           63
82977  deg
 ZDOT =       1554
823109                 TA   =          352
05701
                                          MA   =          352
06788
                                          Ha   =            230
709  n
mi
                                          Hp   =            221
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9368187
47                 X    =        -2917789
77
 Y    =       10996403
95  feet           Y    =         3319424
29  meter
 Z    =       16952641
48                 Z    =         5153143
07
 XDOT =     -14297
667647                 XDOT =       -4296
821072
 YDOT =     -20049
636592  feet/sec       YDOT =       -6159
520882  meter/sec
 ZDOT =       5101
125687                 ZDOT =        1533
803316

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6457409
20                 X    =         1968218
32
 Y    =      -13006574
66  feet           Y    =        -3964403
96  meter
 Z    =       16888065
95                 Z    =         5147482
50
 XDOT =      17910
563441                 XDOT =        5459
139737
 YDOT =      15394
808625  feet/sec       YDOT =        4692
337669  meter/sec
 ZDOT =       5005
000199                 ZDOT =        1525
524061


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   20081
09619149  
00016717  00000-0  10270-3 0  9119
2 25544  51
6402  64
3308 0004590  39
7669 320
3817 15
48907608 18351


Satellite: ISS
Catalog Number: 25544
Epoch time:      20081
09619149   =   yrday
fracday
Element set:     911
Inclination:       51
6402  deg
RA of node:        64
3308  deg
Eccentricity:     
0004590     
Arg of perigee:    39
7669  deg
Mean anomaly:     320
3817  deg
Mean motion:   15
48907608  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1835
Checksum:              314


Coasting Arc #13 (Orbit 1849)
---------------------------------------

Vector Time (GMT): 2020/082/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2539816
86                 A    =         6793395
12  meter
 Y    =       -3622886
70  meter          E    =           
0017672
 Z    =       -5170761
39                 I    =           51
95865
 XDOT =       4870
928042                 Wp   =           69
36286
 YDOT =       5677
538247  meter/sec      RA   =           58
90794  deg
 ZDOT =      -1583
746459                 TA   =          185
38015
                                          MA   =          185
39916
                                          Ha   =            230
673  n
mi
                                          Hp   =            221
683

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8332732
48                 X    =         2605256
51
 Y    =      -11886111
21  feet           Y    =        -3594119
29  meter
 Z    =      -16964440
24                 Z    =        -5158264
83
 XDOT =      15980
735045                 XDOT =        4814
770937
 YDOT =      18627
093986  feet/sec       YDOT =        5731
694273  meter/sec
 ZDOT =      -5196
018565                 ZDOT =       -1560
222729

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4998750
05                 X    =        -1523619
01
 Y    =       13699535
38  feet           Y    =         4175618
39  meter
 Z    =      -16906848
65                 Z    =        -5153207
47
 XDOT =     -19377
069731                 XDOT =       -5906
130854
 YDOT =     -13356
849758  feet/sec       YDOT =       -4071
167806  meter/sec
 ZDOT =      -5088
383720                 ZDOT =       -1550
939358


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   20082
06398353  
00016717  00000-0  10270-3 0  9129
2 25544  51
6415  59
5449 0004711  44
0967 316
0558 15
48910536 18507


Satellite: ISS
Catalog Number: 25544
Epoch time:      20082
06398353   =   yrday
fracday
Element set:     912
Inclination:       51
6415  deg
RA of node:        59
5449  deg
Eccentricity:     
0004711     
Arg of perigee:    44
0967  deg
Mean anomaly:     316
0558  deg
Mean motion:   15
48910536  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1850
Checksum:              310


Coasting Arc #14 (Orbit 1865)
---------------------------------------

Vector Time (GMT): 2020/083/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2189774
73                 A    =         6793347
63  meter
 Y    =        3843856
61  meter          E    =           
0007400
 Z    =        5149030
02                 I    =           51
94072
 XDOT =      -5367
372004                 Wp   =           86
72238
 YDOT =      -5227
966067  meter/sec      RA   =           53
98359  deg
 ZDOT =       1618
562685                 TA   =          347
71330
                                          MA   =          347
73133
                                          Ha   =            230
756  n
mi
                                          Hp   =            221
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7184300
28                 X    =        -2257605
87
 Y    =       12611078
13  feet           Y    =         3818990
30  meter
 Z    =       16893143
12                 Z    =         5138227
91
 XDOT =     -17609
488203                 XDOT =       -5316
374392
 YDOT =     -17152
119642  feet/sec       YDOT =       -5287
702513  meter/sec
 ZDOT =       5310
245029                 ZDOT =        1592
614848

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3455920
49                 X    =         1053364
56
 Y    =      -14155958
09  feet           Y    =        -4314736
03  meter
 Z    =       16843313
53                 Z    =         5133841
97
 XDOT =      20725
521093                 XDOT =        6317
138829
 YDOT =      11242
998910  feet/sec       YDOT =        3426
866068  meter/sec
 ZDOT =       5191
468271                 ZDOT =        1582
359529


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   20083
09629145  
00016717  00000-0  10270-3 0  9130
2 25544  51
6418  54
4383 0004652  46
8991 313
2548 15
48931002 18668


Satellite: ISS
Catalog Number: 25544
Epoch time:      20083
09629145   =   yrday
fracday
Element set:     913
Inclination:       51
6418  deg
RA of node:        54
4383  deg
Eccentricity:     
0004652     
Arg of perigee:    46
8991  deg
Mean anomaly:     313
2548  deg
Mean motion:   15
48931002  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1866
Checksum:              312


Coasting Arc #15 (Orbit 1880)
---------------------------------------

Vector Time (GMT): 2020/084/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1831436
84                 A    =         6793462
47  meter
 Y    =       -4050522
74  meter          E    =           
0017837
 Z    =       -5153128
14                 I    =           51
92013
 XDOT =       5792
913234                 Wp   =           70
71648
 YDOT =       4712
202629  meter/sec      RA   =           49
05981  deg
 ZDOT =      -1644
044753                 TA   =          183
42546
                                          MA   =          183
43769
                                          Ha   =            230
762  n
mi
                                          Hp   =            221
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6008651
07                 X    =         1901625
63
 Y    =      -13289116
59  feet           Y    =        -4029650
45  meter
 Z    =      -16906588
40                 Z    =        -5144060
87
 XDOT =      19005
620848                 XDOT =        5747
775222
 YDOT =      15459
982379  feet/sec       YDOT =        4776
730535  meter/sec
 ZDOT =      -5393
847615                 ZDOT =       -1616
015440

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1887795
02                 X    =         -575399
92
 Y    =       14510519
13  feet           Y    =         4422806
23  meter
 Z    =      -16864705
84                 Z    =        -5140362
34
 XDOT =     -21723
567678                 XDOT =       -6621
343428
 YDOT =      -8950
096472  feet/sec       YDOT =       -2727
989405  meter/sec
 ZDOT =      -5265
499509                 ZDOT =       -1604
924250


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   20084
06408101  
00016717  00000-0  10270-3 0  9146
2 25544  51
6418  49
6529 0004724  51
3042 308
8530 15
48906699 18816


Satellite: ISS
Catalog Number: 25544
Epoch time:      20084
06408101   =   yrday
fracday
Element set:     914
Inclination:       51
6418  deg
RA of node:        49
6529  deg
Eccentricity:     
0004724     
Arg of perigee:    51
3042  deg
Mean anomaly:     308
8530  deg
Mean motion:   15
48906699  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1881
Checksum:              306


Coasting Arc #16 (Orbit 1896)
---------------------------------------

Vector Time (GMT): 2020/085/01:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1445325
80                 A    =         6793376
74  meter
 Y    =        4203301
53  meter          E    =           
0007838
 Z    =        5130710
86                 I    =           51
89832
 XDOT =      -6200
860743                 Wp   =           91
09549
 YDOT =      -4182
980609  meter/sec      RA   =           44
13301  deg
 ZDOT =       1677
735291                 TA   =          342
74274
                                          MA   =          342
76937
                                          Ha   =            230
768  n
mi
                                          Hp   =            221
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4741882
54                 X    =        -1517142
92
 Y    =       13790359
36  feet           Y    =         4186737
89  meter
 Z    =       16833040
87                 Z    =         5123515
16
 XDOT =     -20344
031308                 XDOT =       -6161
774011
 YDOT =     -13723
689661  feet/sec       YDOT =       -4252
104309  meter/sec
 ZDOT =       5504
380877                 ZDOT =        1647
709444

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         277366
82                 X    =           84541
41
 Y    =      -14618574
31  feet           Y    =        -4455741
45  meter
 Z    =       16799734
49                 Z    =         5120559
07
 XDOT =      22594
469105                 XDOT =        6886
794183
 YDOT =       6605
211788  feet/sec       YDOT =        2013
268553  meter/sec
 ZDOT =       5366
851856                 ZDOT =        1635
816446


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   20085
09638581  
00016717  00000-0  10270-3 0  9158
2 25544  51
6428  44
5467 0004586  54
5155 305
6423 15
48940548 18972


Satellite: ISS
Catalog Number: 25544
Epoch time:      20085
09638581   =   yrday
fracday
Element set:     915
Inclination:       51
6428  deg
RA of node:        44
5467  deg
Eccentricity:     
0004586     
Arg of perigee:    54
5155  deg
Mean anomaly:     305
6423  deg
Mean motion:   15
48940548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1897
Checksum:              334


Coasting Arc #17 (Orbit 1903)
---------------------------------------

Vector Time (GMT): 2020/085/12:40:00
000
Vector Time (MET): N/A
Weight (LBS)     : 939545
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         577565
06                 A    =         6794372
46  meter
 Y    =       -4662526
12  meter          E    =           
0016828
 Z    =       -4924049
77                 I    =           51
88889
 XDOT =       6479
975353                 Wp   =           66
52295
 YDOT =       3299
814629  meter/sec      RA   =           41
76311  deg
 ZDOT =      -2364
385209                 TA   =          180
33578
                                          MA   =          180
33692
                                          Ha   =            230
869  n
mi
                                          Hp   =            221
378

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1894898
50                 X    =          653578
07
 Y    =      -15297001
71  feet           Y    =        -4655642
90  meter
 Z    =      -16155018
92                 Z    =        -4921059
06
 XDOT =      21259
761657                 XDOT =        6454
079065
 YDOT =      10826
163482  feet/sec       YDOT =        3372
133271  meter/sec
 ZDOT =      -7757
169321                 ZDOT =       -2332
971326

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1363825
92                 X    =         -415694
14
 Y    =      -15368225
25  feet           Y    =        -4684235
06  meter
 Z    =      -16140977
96                 Z    =        -4919770
08
 XDOT =      22033
003534                 XDOT =        6715
659477
 YDOT =       6041
111008  feet/sec       YDOT =        1841
330635  meter/sec
 ZDOT =      -7613
219136                 ZDOT =       -2320
509193


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   20085
54802033  
00016717  00000-0  10270-3 0  9164
2 25544  51
6421  42
3167 0005046  51
8450 308
3154 15
48913423 19040


Satellite: ISS
Catalog Number: 25544
Epoch time:      20085
54802033   =   yrday
fracday
Element set:     916
Inclination:       51
6421  deg
RA of node:        42
3167  deg
Eccentricity:     
0005046     
Arg of perigee:    51
8450  deg
Mean anomaly:     308
3154  deg
Mean motion:   15
48913423  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1904
Checksum:              278
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