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

 
Date: May 2nd 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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


132/22:41:26 692 -1 1 1 1 1 1
N/A -0 1 -0 1 222 0
000/00:02:49 384 -0 0 -0 0 213 9

134/06:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 213 9

Coasting Arc #1 (Orbit 3140)
---------------------------------------

Vector Time (GMT): 2018/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4422324
43                 A    =         6777892
10  meter
 Y    =        -214547
33  meter          E    =           
0007413
 Z    =        5128165
55                 I    =           51
27620
 XDOT =       2036
764769                 Wp   =           48
67787
 YDOT =       7253
759472  meter/sec      RA   =          245
45874  deg
 ZDOT =      -1446
770461                 TA   =           55
34489
                                          MA   =           55
27504
                                          Ha   =            221
586  n
mi
                                          Hp   =            213
875

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14508938
43                 X    =         4399484
51
 Y    =        -703895
45  feet           Y    =         -165221
72  meter
 Z    =       16824690
12                 Z    =         5149592
57
 XDOT =       6682
299112                 XDOT =        1962
527649
 YDOT =      23798
423466  feet/sec       YDOT =        7276
120938  meter/sec
 ZDOT =      -4746
622246                 ZDOT =       -1437
056468

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10665933
08                 X    =         3250976
40
 Y    =       -9696226
22  feet           Y    =        -2955409
75  meter
 Z    =       16920284
55                 Z    =         5157302
73
 XDOT =      19605
714579                 XDOT =        5975
821804
 YDOT =      13322
224614  feet/sec       YDOT =        4060
614062  meter/sec
 ZDOT =      -4704
230580                 ZDOT =       -1433
849481


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   18122
54579039  
00016717  00000-0  10270-3 0  9003
2 25544  51
6406 246
2395 0002936  38
5583 321
5779 15
54175366 31413


Satellite: ISS
Catalog Number: 25544
Epoch time:      18122
54579039   =   yrday
fracday
Element set:     900
Inclination:       51
6406  deg
RA of node:       246
2395  deg
Eccentricity:     
0002936     
Arg of perigee:    38
5583  deg
Mean anomaly:     321
5779  deg
Mean motion:   15
54175366  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3141
Checksum:              320


Coasting Arc #2 (Orbit 3155)
---------------------------------------

Vector Time (GMT): 2018/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4915550
68                 A    =         6780591
16  meter
 Y    =       -1430667
20  meter          E    =           
0010897
 Z    =       -4456062
94                 I    =           51
30053
 XDOT =       -924
025287                 Wp   =           96
01766
 YDOT =      -6881
561766  meter/sec      RA   =          240
43951  deg
 ZDOT =       3234
425912                 TA   =          206
71023
                                          MA   =          206
76639
                                          Ha   =            221
692  n
mi
                                          Hp   =            213
658

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16127134
79                 X    =        -4877541
70
 Y    =       -4693790
03  feet           Y    =        -1485423
55  meter
 Z    =      -14619629
06                 Z    =        -4479849
10
 XDOT =      -3031
579026                 XDOT =        -862
716489
 YDOT =     -22577
302382  feet/sec       YDOT =       -6891
552198  meter/sec
 ZDOT =      10611
633569                 ZDOT =        3230
085853

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15242672
32                 X    =        -4645966
52
 Y    =        6831466
77  feet           Y    =         2082231
07  meter
 Z    =      -14725545
74                 Z    =        -4488346
34
 XDOT =     -16513
450175                 XDOT =       -5033
299613
 YDOT =     -14051
670327  feet/sec       YDOT =       -4282
949116  meter/sec
 ZDOT =      10593
151511                 ZDOT =        3228
792581


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   18123
51028194  
00016717  00000-0  10270-3 0  9013
2 25544  51
6410 241
4322 0002956  41
2838 318
8538 15
54200628 31569


Satellite: ISS
Catalog Number: 25544
Epoch time:      18123
51028194   =   yrday
fracday
Element set:     901
Inclination:       51
6410  deg
RA of node:       241
4322  deg
Eccentricity:     
0002956     
Arg of perigee:    41
2838  deg
Mean anomaly:     318
8538  deg
Mean motion:   15
54200628  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3156
Checksum:              286


Coasting Arc #3 (Orbit 3171)
---------------------------------------

Vector Time (GMT): 2018/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5179956
48                 A    =         6784543
32  meter
 Y    =        2898617
50  meter          E    =           
0014892
 Z    =        3274594
24                 I    =           51
32983
 XDOT =       -400
528152                 Wp   =           83
95770
 YDOT =       6048
779762  meter/sec      RA   =          235
43010  deg
 ZDOT =      -4700
699480                 TA   =           57
82240
                                          MA   =           57
67805
                                          Ha   =            221
751  n
mi
                                          Hp   =            213
717

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       16994607
87                 X    =         5131251
91
 Y    =        9509899
93  feet           Y    =         2956270
85  meter
 Z    =       10743419
44                 Z    =         3299638
85
 XDOT =      -1314
068741                 XDOT =        -445
303681
 YDOT =      19845
077960  feet/sec       YDOT =        6044
050660  meter/sec
 ZDOT =     -15422
242387                 ZDOT =       -4702
753582

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18980248
93                 X    =         5785179
87
 Y    =       -4074296
12  feet           Y    =        -1241845
46  meter
 Z    =       10854778
51                 Z    =         3308536
49
 XDOT =      11930
636814                 XDOT =        3636
458101
 YDOT =      14291
717311  feet/sec       YDOT =        4356
115436  meter/sec
 ZDOT =     -15432
167898                 ZDOT =       -4703
724775


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   18124
53907165  
00016717  00000-0  10270-3 0  9021
2 25544  51
6402 236
3033 0002980  47
3100 312
8303 15
54178171 31727


Satellite: ISS
Catalog Number: 25544
Epoch time:      18124
53907165   =   yrday
fracday
Element set:     902
Inclination:       51
6402  deg
RA of node:       236
3033  deg
Eccentricity:     
0002980     
Arg of perigee:    47
3100  deg
Mean anomaly:     312
8303  deg
Mean motion:   15
54178171  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3172
Checksum:              272


Coasting Arc #4 (Orbit 3186)
---------------------------------------

Vector Time (GMT): 2018/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 928423
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5166420
53                 A    =         6787798
08  meter
 Y    =       -4022047
61  meter          E    =           
0010373
 Z    =       -1777194
72                 I    =           51
36101
 XDOT =       1844
153221                 Wp   =           40
98579
 YDOT =      -4850
906772  meter/sec      RA   =          230
43273  deg
 ZDOT =       5643
658624                 TA   =          299
41921
                                          MA   =          299
52270
                                          Ha   =            221
790  n
mi
                                          Hp   =            213
718

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16950198
58                 X    =        -5112428
15
 Y    =      -13195694
26  feet           Y    =        -4079520
10  meter
 Z    =       -5830691
35                 Z    =        -1802160
72
 XDOT =       6050
371460                 XDOT =        1870
846131
 YDOT =     -15915
048466  feet/sec       YDOT =       -4830
135212  meter/sec
 ZDOT =      18515
940366                 ZDOT =        5652
681564

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21385366
90                 X    =        -6518259
83
 Y    =        1672209
30  feet           Y    =          509689
40  meter
 Z    =       -5941577
14                 Z    =        -1810992
71
 XDOT =      -6241
253676                 XDOT =       -1902
334121
 YDOT =     -14185
101322  feet/sec       YDOT =       -4323
618883  meter/sec
 ZDOT =      18556
800007                 ZDOT =        5656
112642


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   18125
50355811  
00016717  00000-0  10270-3 0  9035
2 25544  51
6410 231
4956 0003062  45
6720 314
4684 15
54175207 31870


Satellite: ISS
Catalog Number: 25544
Epoch time:      18125
50355811   =   yrday
fracday
Element set:     903
Inclination:       51
6410  deg
RA of node:       231
4956  deg
Eccentricity:     
0003062     
Arg of perigee:    45
6720  deg
Mean anomaly:     314
4684  deg
Mean motion:   15
54175207  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3187
Checksum:              289


Coasting Arc #5 (Orbit 3202)
---------------------------------------

Vector Time (GMT): 2018/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4784579
35                 A    =         6789114
30  meter
 Y    =        4809950
44  meter          E    =           
0013027
 Z    =          43251
87                 I    =           51
38697
 XDOT =      -3359
545496                 Wp   =          120
77626
 YDOT =       3407
734223  meter/sec      RA   =          225
44324  deg
 ZDOT =      -5990
999077                 TA   =           58
75628
                                          MA   =           58
62871
                                          Ha   =            221
848  n
mi
                                          Hp   =            213
628

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       15697438
81                 X    =         4730227
47
 Y    =       15780677
29  feet           Y    =         4863151
00  meter
 Z    =         141902
47                 Z    =           66362
09
 XDOT =     -11022
130894                 XDOT =       -3368
300678
 YDOT =      11180
230391  feet/sec       YDOT =        3370
116787  meter/sec
 ZDOT =     -19655
508782                 ZDOT =       -6007
339827

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       22247412
91                 X    =         6781011
45
 Y    =         672584
55  feet           Y    =          205003
77  meter
 Z    =         244430
61                 Z    =           74502
45
 XDOT =       -177
981312                 XDOT =         -54
248704
 YDOT =      13983
629976  feet/sec       YDOT =        4262
210417  meter/sec
 ZDOT =     -19728
840246                 ZDOT =       -6013
350507


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   18126
53234098  
00016717  00000-0  10270-3 0  9043
2 25544  51
6406 226
3664 0003029  51
9213 308
2212 15
54201269 32039


Satellite: ISS
Catalog Number: 25544
Epoch time:      18126
53234098   =   yrday
fracday
Element set:     904
Inclination:       51
6406  deg
RA of node:       226
3664  deg
Eccentricity:     
0003029     
Arg of perigee:    51
9213  deg
Mean anomaly:     308
2212  deg
Mean motion:   15
54201269  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3203
Checksum:              276


Coasting Arc #6 (Orbit 3218)
---------------------------------------

Vector Time (GMT): 2018/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4044858
16                 A    =         6787968
96  meter
 Y    =       -5183450
45  meter          E    =           
0017058
 Z    =        1653438
81                 I    =           51
40724
 XDOT =       4777
402364                 Wp   =           61
92314
 YDOT =      -1899
511175  meter/sec      RA   =          220
45571  deg
 ZDOT =       5695
173212                 TA   =          316
25864
                                          MA   =          316
39367
                                          Ha   =            221
890  n
mi
                                          Hp   =            213
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13270532
03                 X    =        -3994626
37
 Y    =      -17006071
03  feet           Y    =        -5228402
03  meter
 Z    =        5424668
01                 Z    =         1633911
98
 XDOT =      15673
892271                 XDOT =        4770
623820
 YDOT =      -6231
992043  feet/sec       YDOT =       -1846
125079  meter/sec
 ZDOT =      18684
951484                 ZDOT =        5718
363798

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21405468
65                 X    =        -6524386
84
 Y    =       -2837339
68  feet           Y    =         -864821
13  meter
 Z    =        5338156
09                 Z    =         1627069
98
 XDOT =       6541
798608                 XDOT =        1993
940216
 YDOT =     -13771
307090  feet/sec       YDOT =       -4197
494401  meter/sec
 ZDOT =      18788
670796                 ZDOT =        5726
786859


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   18127
56112021  
00016717  00000-0  10270-3 0  9059
2 25544  51
6408 221
2378 0003169  53
6338 306
5107 15
54212189 32193


Satellite: ISS
Catalog Number: 25544
Epoch time:      18127
56112021   =   yrday
fracday
Element set:     905
Inclination:       51
6408  deg
RA of node:       221
2378  deg
Eccentricity:     
0003169     
Arg of perigee:    53
6338  deg
Mean anomaly:     306
5107  deg
Mean motion:   15
54212189  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3219
Checksum:              286


Coasting Arc #7 (Orbit 3233)
---------------------------------------

Vector Time (GMT): 2018/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2910835
38                 A    =         6784779
25  meter
 Y    =        5222046
42  meter          E    =           
0007107
 Z    =       -3214858
72                 I    =           51
42132
 XDOT =      -5983
735852                 Wp   =           84
03569
 YDOT =        405
987520  meter/sec      RA   =          215
46381  deg
 ZDOT =      -4766
777150                 TA   =          133
25238
                                          MA   =          133
19304
                                          Ha   =            221
897  n
mi
                                          Hp   =            213
608

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9549984
84                 X    =         2867840
88
 Y    =       17132698
22  feet           Y    =         5254357
07  meter
 Z    =      -10547436
75                 Z    =        -3200823
10
 XDOT =     -19631
679304                 XDOT =       -5964
676356
 YDOT =       1331
980052  feet/sec       YDOT =         339
179952  meter/sec
 ZDOT =     -15639
032643                 ZDOT =       -4795
797945

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       18952117
86                 X    =         5776605
52
 Y    =        5182007
68  feet           Y    =         1579475
94  meter
 Z    =      -10485418
72                 Z    =        -3195955
63
 XDOT =     -12387
834400                 XDOT =       -3775
811925
 YDOT =      13455
243590  feet/sec       YDOT =        4101
158246  meter/sec
 ZDOT =     -15768
602703                 ZDOT =       -4806
270104


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   18128
52559947  
00016717  00000-0  10270-3 0  9069
2 25544  51
6399 216
4298 0003050  57
9396 302
2053 15
54204334 32342


Satellite: ISS
Catalog Number: 25544
Epoch time:      18128
52559947   =   yrday
fracday
Element set:     906
Inclination:       51
6399  deg
RA of node:       216
4298  deg
Eccentricity:     
0003050     
Arg of perigee:    57
9396  deg
Mean anomaly:     302
2053  deg
Mean motion:   15
54204334  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3234
Checksum:              315


Coasting Arc #8 (Orbit 3249)
---------------------------------------

Vector Time (GMT): 2018/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1484328
70                 A    =         6780826
67  meter
 Y    =       -4937850
79  meter          E    =           
0011655
 Z    =        4394823
58                 I    =           51
43687
 XDOT =       6842
746018                 Wp   =           98
16994
 YDOT =        929
608058  meter/sec      RA   =          210
46259  deg
 ZDOT =       3346
334860                 TA   =          317
88825
                                          MA   =          317
97776
                                          Ha   =            221
868  n
mi
                                          Hp   =            213
501

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4869844
82                 X    =        -1450349
88
 Y    =      -16200297
87  feet           Y    =        -4954259
65  meter
 Z    =       14418712
54                 Z    =         4387695
64
 XDOT =      22449
954126                 XDOT =        6815
587471
 YDOT =       3049
895204  feet/sec       YDOT =        1005
976460  meter/sec
 ZDOT =      10978
788912                 ZDOT =        3379
508838

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15152223
19                 X    =        -4618397
63
 Y    =       -7581219
36  feet           Y    =        -2310755
66  meter
 Z    =       14387479
15                 Z    =         4385303
65
 XDOT =      17093
128569                 XDOT =        5209
985588
 YDOT =     -12989
463654  feet/sec       YDOT =       -3959
188522  meter/sec
 ZDOT =      11126
752777                 ZDOT =        3391
434247


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   18129
55437272  
00016717  00000-0  10270-3 0  9070
2 25544  51
6408 211
3003 0003071  59
5486 300
5970 15
54242781 32507


Satellite: ISS
Catalog Number: 25544
Epoch time:      18129
55437272   =   yrday
fracday
Element set:     907
Inclination:       51
6408  deg
RA of node:       211
3003  deg
Eccentricity:     
0003071     
Arg of perigee:    59
5486  deg
Mean anomaly:     300
5970  deg
Mean motion:   15
54242781  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3250
Checksum:              291


Coasting Arc #9 (Orbit 3264)
---------------------------------------

Vector Time (GMT): 2018/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -177176
57                 A    =         6777990
93  meter
 Y    =        4442797
83  meter          E    =           
0016591
 Z    =       -5130680
81                 I    =           51
45522
 XDOT =      -7207
657521                 Wp   =           75
24501
 YDOT =      -2069
305848  meter/sec      RA   =          205
45424  deg
 ZDOT =      -1543
020880                 TA   =          179
82217
                                          MA   =          179
82158
                                          Ha   =            221
949  n
mi
                                          Hp   =            213
493

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -581287
95                 X    =         -201921
60
 Y    =       14576108
36  feet           Y    =         4440678
18  meter
 Z    =      -16832942
28                 Z    =        -5131601
56
 XDOT =     -23647
170345                 XDOT =       -7176
487037
 YDOT =      -6789
061182  feet/sec       YDOT =       -2149
732547  meter/sec
 ZDOT =      -5062
404463                 ZDOT =       -1577
957813

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10404045
07                 X    =         3171152
94
 Y    =       10217672
00  feet           Y    =         3114346
43  meter
 Z    =      -16837571
12                 Z    =        -5132091
68
 XDOT =     -20243
696321                 XDOT =       -6170
278639
 YDOT =      12014
353092  feet/sec       YDOT =        3661
974822  meter/sec
 ZDOT =      -5218
121717                 ZDOT =       -1590
483499


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   18130
51884776  
00016717  00000-0  10270-3 0  9084
2 25544  51
6401 206
4925 0003143  61
1927 298
9541 15
54199507 32654


Satellite: ISS
Catalog Number: 25544
Epoch time:      18130
51884776   =   yrday
fracday
Element set:     908
Inclination:       51
6401  deg
RA of node:       206
4925  deg
Eccentricity:     
0003143     
Arg of perigee:    61
1927  deg
Mean anomaly:     298
9541  deg
Mean motion:   15
54199507  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3265
Checksum:              322


Coasting Arc #10 (Orbit 3280)
---------------------------------------

Vector Time (GMT): 2018/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1913777
43                 A    =         6777033
77  meter
 Y    =       -3777301
53  meter          E    =           
0005737
 Z    =        5286763
86                 I    =           51
48304
 XDOT =       7056
062667                 Wp   =           69
03505
 YDOT =       2985
684353  meter/sec      RA   =          200
44243  deg
 ZDOT =       -418
652844                 TA   =           24
97747
                                          MA   =           24
94972
                                          Ha   =            221
819  n
mi
                                          Hp   =            213
416

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6278797
34                 X    =         1930193
38
 Y    =      -12392721
55  feet           Y    =        -3755808
58  meter
 Z    =       17345025
78                 Z    =         5296100
31
 XDOT =      23149
811900                 XDOT =        7024
185127
 YDOT =       9795
552340  feet/sec       YDOT =        3064
411869  meter/sec
 ZDOT =      -1373
532954                 ZDOT =        -384
453926

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5162670
81                 X    =        -1573582
06
 Y    =      -12840824
02  feet           Y    =        -3913883
16  meter
 Z    =       17387145
58                 Z    =         5299601
97
 XDOT =      21773
488012                 XDOT =        6636
559146
 YDOT =     -10418
176936  feet/sec       YDOT =       -3175
460330  meter/sec
 ZDOT =      -1221
199022                 ZDOT =        -372
221462


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   18131
54761755  
00016717  00000-0  10270-3 0  9090
2 25544  51
6403 201
3639 0003149  64
8181 295
3298 15
54250602 32812


Satellite: ISS
Catalog Number: 25544
Epoch time:      18131
54761755   =   yrday
fracday
Element set:     909
Inclination:       51
6403  deg
RA of node:       201
3639  deg
Eccentricity:     
0003149     
Arg of perigee:    64
8181  deg
Mean anomaly:     295
3298  deg
Mean motion:   15
54250602  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3281
Checksum:              306


Coasting Arc #11 (Orbit 3295)
---------------------------------------

Vector Time (GMT): 2018/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905676
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3579012
93                 A    =         6778803
03  meter
 Y    =        3049614
88  meter          E    =           
0014860
 Z    =       -4896460
18                 I    =           51
51945
 XDOT =      -6306
506379                 Wp   =           98
93918
 YDOT =      -3663
785961  meter/sec      RA   =          195
43384  deg
 ZDOT =       2331
593659                 TA   =          193
93122
                                          MA   =          193
97226
                                          Ha   =            221
988  n
mi
                                          Hp   =            213
257

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11742168
40                 X    =        -3589063
75
 Y    =       10005298
16  feet           Y    =         3009535
74  meter
 Z    =      -16064501
89                 Z    =        -4913870
45
 XDOT =     -20690
637728                 XDOT =       -6276
394047
 YDOT =     -12020
295148  feet/sec       YDOT =       -3734
141311  meter/sec
 ZDOT =       7649
585494                 ZDOT =        2301
031445

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =           6399
72                 X    =            1950
63
 Y    =       15345015
52  feet           Y    =         4677160
73  meter
 Z    =      -16142589
28                 Z    =        -4920261
21
 XDOT =     -21513
645938                 XDOT =       -6557
359282
 YDOT =       7899
983850  feet/sec       YDOT =        2407
915077  meter/sec
 ZDOT =       7513
550419                 ZDOT =        2290
130168


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   18132
51208937  
00016717  00000-0  10270-3 0  9108
2 25544  51
6397 196
5556 0003317  67
1504 292
9998 15
54227654 32966


Satellite: ISS
Catalog Number: 25544
Epoch time:      18132
51208937   =   yrday
fracday
Element set:     910
Inclination:       51
6397  deg
RA of node:       196
5556  deg
Eccentricity:     
0003317     
Arg of perigee:    67
1504  deg
Mean anomaly:     292
9998  deg
Mean motion:   15
54227654  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3296
Checksum:              338


Coasting Arc #12 (Orbit 3302)
---------------------------------------

Vector Time (GMT): 2018/132/22:42:51
384
Vector Time (MET): N/A
Weight (LBS)     : 905563
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1245260
97                 A    =         6777629
71  meter
 Y    =        4042183
10  meter          E    =           
0017156
 Z    =       -5310687
23                 I    =           51
52945
 XDOT =      -7399
713192                 Wp   =           87
05358
 YDOT =      -1946
772898  meter/sec      RA   =          193
22291  deg
 ZDOT =        254
906383                 TA   =          185
37458
                                          MA   =          185
39302
                                          Ha   =            222
022  n
mi
                                          Hp   =            213
886

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4085501
88                 X    =        -1264572
24
 Y    =       13261755
56  feet           Y    =         4028149
83  meter
 Z    =      -17423514
52                 Z    =        -5316783
23
 XDOT =     -24277
274253                 XDOT =       -7378
632105
 YDOT =      -6387
050190  feet/sec       YDOT =       -2029
403719  meter/sec
 ZDOT =        836
307032                 ZDOT =         219
011672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3306969
85                 X    =        -1007964
41
 Y    =      -13441127
36  feet           Y    =        -4096855
62  meter
 Z    =      -17451200
25                 Z    =        -5319125
84
 XDOT =      23185
006110                 XDOT =        7066
789862
 YDOT =      -6575
605913  feet/sec       YDOT =       -2004
244682  meter/sec
 ZDOT =        676
257032                 ZDOT =         206
123143


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   18132
96217624  
00016717  00000-0  10270-3 0  9111
2 25544  51
6414 194
3132 0002692  57
8350 302
3063 15
54040346 33031


Satellite: ISS
Catalog Number: 25544
Epoch time:      18132
96217624   =   yrday
fracday
Element set:     911
Inclination:       51
6414  deg
RA of node:       194
3132  deg
Eccentricity:     
0002692     
Arg of perigee:    57
8350  deg
Mean anomaly:     302
3063  deg
Mean motion:   15
54040346  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3303
Checksum:              276


Coasting Arc #13 (Orbit 3318)
---------------------------------------

Vector Time (GMT): 2018/133/22:42:51
384
Vector Time (MET): N/A
Weight (LBS)     : 905563
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2936228
29                 A    =         6778950
11  meter
 Y    =       -3555863
07  meter          E    =           
0008779
 Z    =        4963849
14                 I    =           51
56595
 XDOT =       6863
023400                 Wp   =           57
88326
 YDOT =       2693
428015  meter/sec      RA   =          188
21921  deg
 ZDOT =      -2122
867094                 TA   =           52
84208
                                          MA   =           52
76193
                                          Ha   =            221
891  n
mi
                                          Hp   =            213
897

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9633294
91                 X    =         2951660
42
 Y    =      -11666217
41  feet           Y    =        -3522942
01  meter
 Z    =       16285594
29                 Z    =         4978149
99
 XDOT =      22516
480970                 XDOT =        6842
706661
 YDOT =       8836
706087  feet/sec       YDOT =        2770
061540  meter/sec
 ZDOT =      -6964
787054                 ZDOT =       -2089
577464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2033173
43                 X    =         -619711
26
 Y    =       14922118
26  feet           Y    =         4548261
65  meter
 Z    =       16349867
69                 Z    =         4983439
67
 XDOT =     -22767
858905                 XDOT =       -6939
643394
 YDOT =       4392
683319  feet/sec       YDOT =        1338
889876  meter/sec
 ZDOT =      -6816
438958                 ZDOT =       -2077
650594


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   18133
99107675  
00016717  00000-0  10270-3 0  9120
2 25544  51
6408 189
1852 0002682  58
9203 301
2213 15
54069635 33197


Satellite: ISS
Catalog Number: 25544
Epoch time:      18133
99107675   =   yrday
fracday
Element set:     912
Inclination:       51
6408  deg
RA of node:       189
1852  deg
Eccentricity:     
0002682     
Arg of perigee:    58
9203  deg
Mean anomaly:     301
2213  deg
Mean motion:   15
54069635  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3319
Checksum:              311


Coasting Arc #14 (Orbit 3323)
---------------------------------------

Vector Time (GMT): 2018/134/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905563
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2471259
12                 A    =         6778748
95  meter
 Y    =       -3759306
43  meter          E    =           
0007853
 Z    =        5065689
62                 I    =           51
57249
 XDOT =       7111
748733                 Wp   =           61
99384
 YDOT =       2254
770801  meter/sec      RA   =          186
61547  deg
 ZDOT =      -1790
391100                 TA   =           45
36814
                                          MA   =           45
30413
                                          Ha   =            222
087  n
mi
                                          Hp   =            213
931

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8107805
50                 X    =         2488506
06
 Y    =      -12333682
52  feet           Y    =        -3731574
88  meter
 Z    =       16619716
60                 Z    =         5077736
14
 XDOT =      23332
508968                 XDOT =        7094
703673
 YDOT =       7397
541998  feet/sec       YDOT =        2334
204038  meter/sec
 ZDOT =      -5873
986550                 ZDOT =       -1755
885250

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13389662
15                 X    =         4081169
02
 Y    =       -6063627
47  feet           Y    =        -1848193
65  meter
 Z    =       16673949
25                 Z    =         5082219
73
 XDOT =      15237
604938                 XDOT =        4644
421985
 YDOT =      17866
592021  feet/sec       YDOT =        5445
737248  meter/sec
 ZDOT =      -5720
150885                 ZDOT =       -1743
501990


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   18134
31261120  
00016717  00000-0  10270-3 0  9134
2 25544  51
6382 187
5773 0002670  74
2178 285
9269 15
53993007 33244


Satellite: ISS
Catalog Number: 25544
Epoch time:      18134
31261120   =   yrday
fracday
Element set:     913
Inclination:       51
6382  deg
RA of node:       187
5773  deg
Eccentricity:     
0002670     
Arg of perigee:    74
2178  deg
Mean anomaly:     285
9269  deg
Mean motion:   15
53993007  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3324
Checksum:              312


Coasting Arc #15 (Orbit 3338)
---------------------------------------

Vector Time (GMT): 2018/135/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905563
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4033471
73                 A    =         6781591
32  meter
 Y    =        3320771
20  meter          E    =           
0010902
 Z    =       -4334353
89                 I    =           51
61532
 XDOT =      -6156
146871                 Wp   =          103
54317
 YDOT =      -2935
565324  meter/sec      RA   =          181
62012  deg
 ZDOT =       3484
597479                 TA   =          201
91434
                                          MA   =          201
96100
                                          Ha   =            222
040  n
mi
                                          Hp   =            213
847

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13233174
95                 X    =        -4049251
24
 Y    =       10894918
64  feet           Y    =         3275578
19  meter
 Z    =      -14220321
17                 Z    =        -4353985
66
 XDOT =     -20197
332254                 XDOT =       -6139
789756
 YDOT =      -9631
119830  feet/sec       YDOT =       -3004
316358  meter/sec
 ZDOT =      11432
406427                 ZDOT =        3454
731920

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16902490
67                 X    =        -5151879
16
 Y    =        2368427
97  feet           Y    =          721896
84  meter
 Z    =      -14308391
38                 Z    =        -4361197
69
 XDOT =     -12019
375168                 XDOT =       -3663
505551
 YDOT =     -17610
705792  feet/sec       YDOT =       -5367
743125  meter/sec
 ZDOT =      11299
356521                 ZDOT =        3444
043867


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   18135
27720372  
00016717  00000-0  10270-3 0  9140
2 25544  51
6384 182
7703 0002486  75
9102 284
2327 15
54021510 33391


Satellite: ISS
Catalog Number: 25544
Epoch time:      18135
27720372   =   yrday
fracday
Element set:     914
Inclination:       51
6384  deg
RA of node:       182
7703  deg
Eccentricity:     
0002486     
Arg of perigee:    75
9102  deg
Mean anomaly:     284
2327  deg
Mean motion:   15
54021510  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3339
Checksum:              295


Coasting Arc #16 (Orbit 3354)
---------------------------------------

Vector Time (GMT): 2018/136/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905563
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5319937
74                 A    =         6785391
90  meter
 Y    =       -2796665
11  meter          E    =           
0015373
 Z    =        3135331
35                 I    =           51
66132
 XDOT =       4748
888721                 Wp   =           92
34103
 YDOT =       3567
506239  meter/sec      RA   =          176
63493  deg
 ZDOT =      -4855
671589                 TA   =           51
52523
                                          MA   =           51
38741
                                          Ha   =            222
034  n
mi
                                          Hp   =            213
883

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       17453863
97                 X    =         5335585
32
 Y    =       -9175410
45  feet           Y    =        -2737086
68  meter
 Z    =       10286520
19                 Z    =         3161212
07
 XDOT =      15580
343573                 XDOT =        4732
229726
 YDOT =      11704
416794  feet/sec       YDOT =        3620
518859  meter/sec
 ZDOT =     -15930
681066                 ZDOT =       -4832
642801

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19632921
07                 X    =         5984114
34
 Y    =         987555
04  feet           Y    =          301006
78  meter
 Z    =       10402459
69                 Z    =         3170669
71
 XDOT =       7583
852779                 XDOT =        2311
558327
 YDOT =      16639
497046  feet/sec       YDOT =        5071
718700  meter/sec
 ZDOT =     -15828
228156                 ZDOT =       -4824
443942


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   18136
30610185  
00016717  00000-0  10270-3 0  9156
2 25544  51
6388 177
6411 0002562  80
6464 279
4978 15
54016732 33559


Satellite: ISS
Catalog Number: 25544
Epoch time:      18136
30610185   =   yrday
fracday
Element set:     915
Inclination:       51
6388  deg
RA of node:       177
6411  deg
Eccentricity:     
0002562     
Arg of perigee:    80
6464  deg
Mean anomaly:     279
4978  deg
Mean motion:   15
54016732  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3355
Checksum:              319


Coasting Arc #17 (Orbit 3369)
---------------------------------------

Vector Time (GMT): 2018/137/06:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 905563
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6190718
40                 A    =         6788408
68  meter
 Y    =        2230258
02  meter          E    =           
0009808
 Z    =       -1657747
52                 I    =           51
70440
 XDOT =      -3009
239601                 Wp   =           48
91191
 YDOT =      -4123
121784  meter/sec      RA   =          171
66245  deg
 ZDOT =       5719
021469                 TA   =          292
95199
                                          MA   =          293
05546
                                          Ha   =            222
085  n
mi
                                          Hp   =            213
852

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -20310755
90                 X    =        -6207145
05
 Y    =        7317119
48  feet           Y    =         2160937
47  meter
 Z    =       -5438804
21                 Z    =        -1687860
06
 XDOT =      -9872
833338                 XDOT =       -2990
690533
 YDOT =     -13527
302442  feet/sec       YDOT =       -4156
670071  meter/sec
 ZDOT =      18763
193795                 ZDOT =        5704
447988

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21235052
48                 X    =        -6472443
99
 Y    =       -3695281
03  feet           Y    =        -1126321
66  meter
 Z    =       -5573605
51                 Z    =        -1698834
96
 XDOT =      -2246
985342                 XDOT =        -684
881132
 YDOT =     -15153
943564  feet/sec       YDOT =       -4618
921998  meter/sec
 ZDOT =      18698
569418                 ZDOT =        5699
323959


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   18137
27069132  
00016717  00000-0  10270-3 0  9164
2 25544  51
6390 172
8337 0002647  79
8967 280
2484 15
54022516 33704


Satellite: ISS
Catalog Number: 25544
Epoch time:      18137
27069132   =   yrday
fracday
Element set:     916
Inclination:       51
6390  deg
RA of node:       172
8337  deg
Eccentricity:     
0002647     
Arg of perigee:    79
8967  deg
Mean anomaly:     280
2484  deg
Mean motion:   15
54022516  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            3370
Checksum:              322
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