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

 
Date: December 17th 2018

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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


348/03:56:00 000 0 0 0 0 0 0
N/A 0 0 0 0 222 4
000/00:00:00 000 0 0 0 0 213 6

354/01:40:30 000 0 0 0 0 0 0
N/A 0 0 0 0 222 1
000/00:00:00 000 0 0 0 0 214 1

358/04:25:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 8
000/00:00:00 000 0 0 0 0 214 6

361/02:52:50 495 -1 8 2 2 2 2
N/A 1 0 -0 0 221 4
000/00:05:40 991 0 7 -0 0 216 2

361/09:04:00 000 0 0 0 0 0 0
N/A 0 0 0 0 221 4
000/00:00:00 000 0 0 0 0 216 2

Coasting Arc #1 (Orbit 2625)
---------------------------------------

Vector Time (GMT): 2018/346/14:51:13
974
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3956599
57                 A    =         6778987
94  meter
 Y    =       -2362622
92  meter          E    =           
0008313
 Z    =        4964352
13                 I    =           51
43409
 XDOT =       5539
948359                 Wp   =           93
83935
 YDOT =       4882
321895  meter/sec      RA   =          208
35198  deg
 ZDOT =      -2089
289943                 TA   =           16
55101
                                          MA   =           16
52389
                                          Ha   =            222
525  n
mi
                                          Hp   =            213
488

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12980969
71                 X    =         3958610
87
 Y    =       -7751387
53  feet           Y    =        -2318366
71  meter
 Z    =       16287244
53                 Z    =         4983576
53
 XDOT =      18175
683594                 XDOT =        5495
089772
 YDOT =      16018
116452  feet/sec       YDOT =        4944
022829  meter/sec
 ZDOT =      -6854
625797                 ZDOT =       -2062
487342

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13531326
90                 X    =         4124348
44
 Y    =        6531358
21  feet           Y    =         1990757
98  meter
 Z    =       16374018
13                 Z    =         4990800
73
 XDOT =      -2956
940289                 XDOT =        -901
275400
 YDOT =      23029
550156  feet/sec       YDOT =        7019
406888  meter/sec
 ZDOT =      -6734
480890                 ZDOT =       -2052
669775


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   18346
66360442  
00016717  00000-0  10270-3 0  9000
2 25544  51
6355 209
2941 0005017 139
5923 220
5603 15
54043037 26265


Satellite: ISS
Catalog Number: 25544
Epoch time:      18346
66360442   =   yrday
fracday
Element set:     900
Inclination:       51
6355  deg
RA of node:       209
2941  deg
Eccentricity:     
0005017     
Arg of perigee:   139
5923  deg
Mean anomaly:     220
5603  deg
Mean motion:   15
54043037  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2626
Checksum:              289


Coasting Arc #2 (Orbit 2640)
---------------------------------------

Vector Time (GMT): 2018/347/14:51:13
974
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5207125
09                 A    =         6782112
97  meter
 Y    =        1347022
69  meter          E    =           
0012439
 Z    =       -4145169
65                 I    =           51
47424
 XDOT =      -4302
585707                 Wp   =          123
31917
 YDOT =      -5106
365688  meter/sec      RA   =          203
34637  deg
 ZDOT =       3746
963558                 TA   =          185
39455
                                          MA   =          185
40797
                                          Ha   =            222
604  n
mi
                                          Hp   =            213
353

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17083743
75                 X    =        -5201665
88
 Y    =        4419365
78  feet           Y    =         1288823
86  meter
 Z    =      -13599637
94                 Z    =        -4170450
62
 XDOT =     -14116
094840                 XDOT =       -4263
365845
 YDOT =     -16753
168268  feet/sec       YDOT =       -5154
261209  meter/sec
 ZDOT =      12293
187525                 ZDOT =        3726
157978

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13199158
59                 X    =        -4023103
54
 Y    =      -11578217
12  feet           Y    =        -3529040
58  meter
 Z    =      -13713582
58                 Z    =        -4179899
97
 XDOT =       5042
670135                 XDOT =        1537
005857
 YDOT =     -20193
066740  feet/sec       YDOT =       -6154
846742  meter/sec
 ZDOT =      12200
038775                 ZDOT =        3718
571819


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   18347
62817295  
00016717  00000-0  10270-3 0  9011
2 25544  51
6351 204
4853 0005177 143
0885 217
0625 15
54069006 26410


Satellite: ISS
Catalog Number: 25544
Epoch time:      18347
62817295   =   yrday
fracday
Element set:     901
Inclination:       51
6351  deg
RA of node:       204
4853  deg
Eccentricity:     
0005177     
Arg of perigee:   143
0885  deg
Mean anomaly:     217
0625  deg
Mean motion:   15
54069006  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2641
Checksum:              305


Coasting Arc #3 (Orbit 2649)
---------------------------------------

Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4438073
59                 A    =         6780379
00  meter
 Y    =       -2241507
11  meter          E    =           
0010444
 Z    =        4600768
37                 I    =           51
48578
 XDOT =       5400
530765                 Wp   =           92
87330
 YDOT =       4566
736337  meter/sec      RA   =          200
63062  deg
 ZDOT =      -2979
293677                 TA   =           26
89899
                                          MA   =           26
84488
                                          Ha   =            222
390  n
mi
                                          Hp   =            213
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14560608
89                 X    =         4440460
84
 Y    =       -7354025
94  feet           Y    =        -2191864
48  meter
 Z    =       15094384
41                 Z    =         4622332
58
 XDOT =      17718
276787                 XDOT =        5363
534669
 YDOT =      14982
730763  feet/sec       YDOT =        4626
922190  meter/sec
 ZDOT =      -9774
585555                 ZDOT =       -2953
149340

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15858450
95                 X    =        -4833655
85
 Y    =       -3414014
70  feet           Y    =        -1040591
68  meter
 Z    =       15191692
01                 Z    =         4630427
73
 XDOT =      -4599
406397                 XDOT =       -1401
899070
 YDOT =     -21685
901237  feet/sec       YDOT =       -6609
862697  meter/sec
 ZDOT =      -9657
337072                 ZDOT =       -2943
556340


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   18348
20691317  
00016717  00000-0  10270-3 0  9022
2 25544  51
6357 201
6036 0004920 143
6572 216
4916 15
54072253 26506


Satellite: ISS
Catalog Number: 25544
Epoch time:      18348
20691317   =   yrday
fracday
Element set:     902
Inclination:       51
6357  deg
RA of node:       201
6036  deg
Eccentricity:     
0004920     
Arg of perigee:   143
6572  deg
Mean anomaly:     216
4916  deg
Mean motion:   15
54072253  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2650
Checksum:              292


Coasting Arc #4 (Orbit 2664)
---------------------------------------

Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5625484
36                 A    =         6784094
70  meter
 Y    =        1356719
34  meter          E    =           
0009291
 Z    =       -3552297
87                 I    =           51
53042
 XDOT =      -3971
004577                 Wp   =          120
67203
 YDOT =      -4792
914255  meter/sec      RA   =          195
63404  deg
 ZDOT =       4462
082455                 TA   =          197
39986
                                          MA   =          197
43172
                                          Ha   =            222
489  n
mi
                                          Hp   =            213
542

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18456313
53                 X    =        -5622982
30
 Y    =        4451178
95  feet           Y    =         1293825
48  meter
 Z    =      -11654520
57                 Z    =        -3579618
35
 XDOT =     -13028
230241                 XDOT =       -3938
788170
 YDOT =     -15724
784301  feet/sec       YDOT =       -4837
140935  meter/sec
 ZDOT =      14639
378133                 ZDOT =        4442
870645

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17206038
93                 X    =         5244400
67
 Y    =        7843155
87  feet           Y    =         2390593
91  meter
 Z    =      -11777668
83                 Z    =        -3589833
46
 XDOT =       1192
560007                 XDOT =         363
492290
 YDOT =      19217
978939  feet/sec       YDOT =        5857
639981  meter/sec
 ZDOT =      14553
346785                 ZDOT =        4435
860100


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   18349
17147849  
00016717  00000-0  10270-3 0  9036
2 25544  51
6367 196
7957 0004871 145
5805 214
5664 15
54052381 26653


Satellite: ISS
Catalog Number: 25544
Epoch time:      18349
17147849   =   yrday
fracday
Element set:     903
Inclination:       51
6367  deg
RA of node:       196
7957  deg
Eccentricity:     
0004871     
Arg of perigee:   145
5805  deg
Mean anomaly:     214
5664  deg
Mean motion:   15
54052381  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2665
Checksum:              343


Coasting Arc #5 (Orbit 2680)
---------------------------------------

Vector Time (GMT): 2018/350/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6423096
30                 A    =         6787525
41  meter
 Y    =        -493015
89  meter          E    =           
0017841
 Z    =        2106981
53                 I    =           51
57410
 XDOT =       2191
428701                 Wp   =          119
97103
 YDOT =       4864
737157  meter/sec      RA   =          190
64958  deg
 ZDOT =      -5515
971154                 TA   =           36
65014
                                          MA   =           36
52823
                                          Ha   =            222
307  n
mi
                                          Hp   =            213
687

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21073150
59                 X    =         6417897
34
 Y    =       -1617506
21  feet           Y    =         -421217
55  meter
 Z    =        6912669
06                 Z    =         2138170
12
 XDOT =       7189
726710                 XDOT =        2163
660714
 YDOT =      15960
423743  feet/sec       YDOT =        4889
088284  meter/sec
 ZDOT =     -18097
018222                 ZDOT =       -5505
393101

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -17739498
40                 X    =        -5406999
11
 Y    =      -11403598
08  feet           Y    =        -3475816
69  meter
 Z    =        7053165
46                 Z    =         2149804
83
 XDOT =       2974
078476                 XDOT =         906
499119
 YDOT =     -15842
606274  feet/sec       YDOT =       -4828
826392  meter/sec
 ZDOT =     -18049
859127                 ZDOT =       -5501
597062


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   18350
20034679  
00016717  00000-0  10270-3 0  9049
2 25544  51
6365 191
6668 0004780 149
4773 210
6659 15
54076199 26812


Satellite: ISS
Catalog Number: 25544
Epoch time:      18350
20034679   =   yrday
fracday
Element set:     904
Inclination:       51
6365  deg
RA of node:       191
6668  deg
Eccentricity:     
0004780     
Arg of perigee:   149
4773  deg
Mean anomaly:     210
6659  deg
Mean motion:   15
54076199  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2681
Checksum:              335


Coasting Arc #6 (Orbit 2695)
---------------------------------------

Vector Time (GMT): 2018/351/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6764029
14                 A    =         6789323
66  meter
 Y    =        -287785
74  meter          E    =           
0010149
 Z    =        -482859
02                 I    =           51
61289
 XDOT =       -216
069756                 Wp   =           68
16842
 YDOT =      -4785
016224  meter/sec      RA   =          185
67536  deg
 ZDOT =       5983
399368                 TA   =          286
62422
                                          MA   =          286
73564
                                          Ha   =            222
299  n
mi
                                          Hp   =            213
795

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22191696
67                 X    =        -6757962
84
 Y    =        -944178
94  feet           Y    =         -363391
87  meter
 Z    =       -1584183
12                 Z    =         -515701
78
 XDOT =       -708
890274                 XDOT =        -191
610653
 YDOT =     -15698
872127  feet/sec       YDOT =       -4787
296052  meter/sec
 ZDOT =      19630
575354                 ZDOT =        5982
408902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17354173
31                 X    =         5289552
03
 Y    =       13845761
54  feet           Y    =         4220188
12  meter
 Z    =       -1732070
20                 Z    =         -527935
00
 XDOT =      -7571
307211                 XDOT =       -2307
734438
 YDOT =      11905
736588  feet/sec       YDOT =        3628
868512  meter/sec
 ZDOT =      19626
580968                 ZDOT =        5982
181879


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   18351
16490984  
00016717  00000-0  10270-3 0  9051
2 25544  51
6363 186
8593 0004877 153
9098 206
2301 15
54087695 26964


Satellite: ISS
Catalog Number: 25544
Epoch time:      18351
16490984   =   yrday
fracday
Element set:     905
Inclination:       51
6363  deg
RA of node:       186
8593  deg
Eccentricity:     
0004877     
Arg of perigee:   153
9098  deg
Mean anomaly:     206
2301  deg
Mean motion:   15
54087695  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2696
Checksum:              349


Coasting Arc #7 (Orbit 2711)
---------------------------------------

Vector Time (GMT): 2018/352/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6584248
93                 A    =         6788857
27  meter
 Y    =        1058733
96  meter          E    =           
0013762
 Z    =       -1235551
21                 I    =           51
64575
 XDOT =      -1831
241535                 Wp   =          147
79834
 YDOT =       4608
041119  meter/sec      RA   =          180
70465  deg
 ZDOT =      -5851
468373                 TA   =           45
63457
                                          MA   =           45
52191
                                          Ha   =            222
241  n
mi
                                          Hp   =            213
943

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21601866
57                 X    =         6577922
22
 Y    =        3473536
60  feet           Y    =         1132328
32  meter
 Z    =       -4053645
71                 Z    =        -1203582
26
 XDOT =      -6008
010287                 XDOT =       -1854
210273
 YDOT =      15118
245142  feet/sec       YDOT =        4587
434881  meter/sec
 ZDOT =     -19197
730881                 ZDOT =       -5860
419449

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15681968
53                 X    =        -4779864
01
 Y    =      -15294700
00  feet           Y    =        -4661824
56  meter
 Z    =       -3909751
19                 Z    =        -1191692
16
 XDOT =      12397
039547                 XDOT =        3778
617654
 YDOT =      -7829
024503  feet/sec       YDOT =       -2386
286669  meter/sec
 ZDOT =     -19238
498873                 ZDOT =       -5863
894456


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   18352
19377451  
00016717  00000-0  10270-3 0  9069
2 25544  51
6377 181
7301 0004676 157
8540 202
2816 15
54083425 27125


Satellite: ISS
Catalog Number: 25544
Epoch time:      18352
19377451   =   yrday
fracday
Element set:     906
Inclination:       51
6377  deg
RA of node:       181
7301  deg
Eccentricity:     
0004676     
Arg of perigee:   157
8540  deg
Mean anomaly:     202
2816  deg
Mean motion:   15
54083425  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2712
Checksum:              308


Coasting Arc #8 (Orbit 2727)
---------------------------------------

Vector Time (GMT): 2018/353/03:56:00
000
Vector Time (MET): N/A
Weight (LBS)     : 966149
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5925402
58                 A    =         6786214
45  meter
 Y    =       -1767035
57  meter          E    =           
0014875
 Z    =        2786527
54                 I    =           51
66947
 XDOT =       3712
992128                 Wp   =           97
91375
 YDOT =      -4336
434988  meter/sec      RA   =          175
73235  deg
 ZDOT =       5120
181140                 TA   =          293
67110
                                          MA   =          293
82714
                                          Ha   =            222
166  n
mi
                                          Hp   =            214
035

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19440297
16                 X    =        -5918738
31
 Y    =       -5797360
78  feet           Y    =        -1833260
52  meter
 Z    =        9142150
72                 Z    =         2757759
74
 XDOT =      12181
732703                 XDOT =        3736
336028
 YDOT =     -14227
148910  feet/sec       YDOT =       -4294
783658  meter/sec
 ZDOT =      16798
494554                 ZDOT =        5138
274056

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12877402
36                 X    =         3925032
24
 Y    =       15749816
28  feet           Y    =         4800544
00  meter
 Z    =        9012727
74                 Z    =         2747079
42
 XDOT =     -16827
858277                 XDOT =       -5129
131203
 YDOT =       4050
725980  feet/sec       YDOT =        1234
661279  meter/sec
 ZDOT =      16880
426967                 ZDOT =        5145
154139


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   18353
22263660  
00016717  00000-0  10270-3 0  9071
2 25544  51
6370 176
6019 0004727 161
4172 198
7154 15
54100796 27288


Satellite: ISS
Catalog Number: 25544
Epoch time:      18353
22263660   =   yrday
fracday
Element set:     907
Inclination:       51
6370  deg
RA of node:       176
6019  deg
Eccentricity:     
0004727     
Arg of perigee:   161
4172  deg
Mean anomaly:     198
7154  deg
Mean motion:   15
54100796  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2728
Checksum:              313


Coasting Arc #9 (Orbit 2741)
---------------------------------------

Vector Time (GMT): 2018/354/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3589711
22                 A    =         6779934
24  meter
 Y    =       -3242259
78  meter          E    =           
0011467
 Z    =        4747330
40                 I    =           51
67675
 XDOT =       6445
256166                 Wp   =          135
57033
 YDOT =      -3158
699612  meter/sec      RA   =          171
21735  deg
 ZDOT =       2704
362220                 TA   =          287
66075
                                          MA   =          287
78593
                                          Ha   =            222
113  n
mi
                                          Hp   =            214
123

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11777267
78                 X    =        -3576248
81
 Y    =      -10637335
24  feet           Y    =        -3282327
68  meter
 Z    =       15575230
97                 Z    =         4729925
00
 XDOT =      21145
853564                 XDOT =        6466
962115
 YDOT =     -10363
187703  feet/sec       YDOT =       -3086
503209  meter/sec
 ZDOT =       8872
579461                 ZDOT =        2735
723715

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -5189801
32                 X    =        -1581851
44
 Y    =       15078117
93  feet           Y    =         4595810
34  meter
 Z    =       15497131
32                 Z    =         4723525
63
 XDOT =     -16636
061714                 XDOT =       -5070
671610
 YDOT =     -15031
263785  feet/sec       YDOT =       -4581
529202  meter/sec
 ZDOT =       9014
191481                 ZDOT =        2747
525563


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   18354
12289046  
00016717  00000-0  10270-3 0  9088
2 25544  51
6353 172
1145 0004697 165
9155 194
2129 15
54102937 27424


Satellite: ISS
Catalog Number: 25544
Epoch time:      18354
12289046   =   yrday
fracday
Element set:     908
Inclination:       51
6353  deg
RA of node:       172
1145  deg
Eccentricity:     
0004697     
Arg of perigee:   165
9155  deg
Mean anomaly:     194
2129  deg
Mean motion:   15
54102937  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2742
Checksum:              316


Coasting Arc #10 (Orbit 2756)
---------------------------------------

Vector Time (GMT): 2018/355/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1929409
89                 A    =         6777775
65  meter
 Y    =        3814144
61  meter          E    =           
0015579
 Z    =       -5272883
97                 I    =           51
70258
 XDOT =      -7199
663363                 Wp   =          100
85930
 YDOT =       2462
889703  meter/sec      RA   =          166
22305  deg
 ZDOT =       -857
924604                 TA   =          160
96236
                                          MA   =          160
90407
                                          Ha   =            222
013  n
mi
                                          Hp   =            214
266

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6330084
93                 X    =         1912228
73
 Y    =       12513597
80  feet           Y    =         3835625
25  meter
 Z    =      -17299488
08                 Z    =        -5263552
71
 XDOT =     -23620
942792                 XDOT =       -7222
501615
 YDOT =       8080
346795  feet/sec       YDOT =        2382
250480  meter/sec
 ZDOT =      -2814
713269                 ZDOT =        -892
953483

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8841835
76                 X    =         2694991
54
 Y    =      -10950889
29  feet           Y    =        -3337831
05  meter
 Z    =      -17257820
18                 Z    =        -5260183
59
 XDOT =      16127
865399                 XDOT =        4915
773374
 YDOT =      17680
700247  feet/sec       YDOT =        5389
077435  meter/sec
 ZDOT =      -2972
808151                 ZDOT =        -906
111924


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   18355
08744753  
00016717  00000-0  10270-3 0  9096
2 25544  51
6358 167
3053 0004668 167
9105 192
2161 15
54078082 27571


Satellite: ISS
Catalog Number: 25544
Epoch time:      18355
08744753   =   yrday
fracday
Element set:     909
Inclination:       51
6358  deg
RA of node:       167
3053  deg
Eccentricity:     
0004668     
Arg of perigee:   167
9105  deg
Mean anomaly:     192
2161  deg
Mean motion:   15
54078082  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2757
Checksum:              331


Coasting Arc #11 (Orbit 2772)
---------------------------------------

Vector Time (GMT): 2018/356/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -197986
55                 A    =         6777818
49  meter
 Y    =       -4294725
38  meter          E    =           
0004530
 Z    =        5236138
74                 I    =           51
73530
 XDOT =       7419
665430                 Wp   =          124
85698
 YDOT =      -1635
941181  meter/sec      RA   =          161
22948  deg
 ZDOT =      -1063
142291                 TA   =          335
29782
                                          MA   =          335
31951
                                          Ha   =            221
928  n
mi
                                          Hp   =            214
323

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -649562
16                 X    =         -175381
48
 Y    =      -14090306
38  feet           Y    =        -4296813
80  meter
 Z    =       17178932
87                 Z    =         5235231
25
 XDOT =      24342
734352                 XDOT =        7442
571738
 YDOT =      -5367
261094  feet/sec       YDOT =       -1552
841090  meter/sec
 ZDOT =      -3487
999644                 ZDOT =       -1027
044621

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12467552
13                 X    =        -3800109
89
 Y    =        6606393
38  feet           Y    =         2013628
70  meter
 Z    =       17175276
11                 Z    =         5235024
16
 XDOT =     -14615
773397                 XDOT =       -4454
887731
 YDOT =     -18954
152126  feet/sec       YDOT =       -5777
225568  meter/sec
 ZDOT =      -3325
140678                 ZDOT =       -1013
502879


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   18356
11630530  
00016717  00000-0  10270-3 0  9100
2 25544  51
6362 162
1766 0004550 171
7375 188
3854 15
54082365 27734


Satellite: ISS
Catalog Number: 25544
Epoch time:      18356
11630530   =   yrday
fracday
Element set:     910
Inclination:       51
6362  deg
RA of node:       162
1766  deg
Eccentricity:     
0004550     
Arg of perigee:   171
7375  deg
Mean anomaly:     188
3854  deg
Mean motion:   15
54082365  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2773
Checksum:              308


Coasting Arc #12 (Orbit 2787)
---------------------------------------

Vector Time (GMT): 2018/357/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1490702
58                 A    =         6780178
15  meter
 Y    =        4685136
53  meter          E    =           
0013137
 Z    =       -4681596
42                 I    =           51
77409
 XDOT =      -7066
904960                 Wp   =          128
03686
 YDOT =        632
021328  meter/sec      RA   =          156
24118  deg
 ZDOT =       2880
336215                 TA   =          170
58358
                                          MA   =          170
55892
                                          Ha   =            221
792  n
mi
                                          Hp   =            214
434

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4890756
49                 X    =        -1520241
64
 Y    =       15371182
83  feet           Y    =         4668302
02  meter
 Z    =      -15359568
32                 Z    =        -4688908
74
 XDOT =     -23185
383728                 XDOT =       -7087
438284
 YDOT =       2073
560787  feet/sec       YDOT =         552
879030  meter/sec
 ZDOT =       9449
921965                 ZDOT =        2845
957965

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15921903
41                 X    =         4852996
16
 Y    =       -2378528
38  feet           Y    =         -724975
45  meter
 Z    =      -15393007
97                 Z    =        -4691788
83
 XDOT =      11812
144012                 XDOT =        3600
341495
 YDOT =      18866
773967  feet/sec       YDOT =        5750
592705  meter/sec
 ZDOT =       9294
884602                 ZDOT =        2833
080827


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   18357
08085791  
00016717  00000-0  10270-3 0  9111
2 25544  51
6360 157
3685 0004471 175
9601 184
1588 15
54074441 27888


Satellite: ISS
Catalog Number: 25544
Epoch time:      18357
08085791   =   yrday
fracday
Element set:     911
Inclination:       51
6360  deg
RA of node:       157
3685  deg
Eccentricity:     
0004471     
Arg of perigee:   175
9601  deg
Mean anomaly:     184
1588  deg
Mean motion:   15
54074441  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2788
Checksum:              333


Coasting Arc #13 (Orbit 2803)
---------------------------------------

Vector Time (GMT): 2018/358/01:40:30
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2981232
56                 A    =         6783760
01  meter
 Y    =       -4887016
08  meter          E    =           
0012353
 Z    =        3626332
18                 I    =           51
81766
 XDOT =       6253
284746                 Wp   =          107
09235
 YDOT =        531
584339  meter/sec      RA   =          151
26378  deg
 ZDOT =      -4415
632422                 TA   =           30
00222
                                          MA   =           29
93150
                                          Ha   =            221
615  n
mi
                                          Hp   =            214
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9780946
70                 X    =         3018044
33
 Y    =      -16033517
33  feet           Y    =        -4853472
57  meter
 Z    =       11897415
30                 Z    =         3640902
54
 XDOT =      20516
026071                 XDOT =        6268
324277
 YDOT =       1744
043108  feet/sec       YDOT =         601
597658  meter/sec
 ZDOT =     -14486
983012                 ZDOT =       -4385
219804

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18684243
13                 X    =        -5694957
31
 Y    =       -1435344
96  feet           Y    =         -437493
14  meter
 Z    =       11963608
61                 Z    =         3646507
90
 XDOT =      -7837
576726                 XDOT =       -2388
893386
 YDOT =     -17823
552551  feet/sec       YDOT =       -5432
618818  meter/sec
 ZDOT =     -14349
915837                 ZDOT =       -4373
854347


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   18358
10971308  
00016717  00000-0  10270-3 0  9124
2 25544  51
6373 152
2398 0004432 180
2127 179
9024 15
54102147 28047


Satellite: ISS
Catalog Number: 25544
Epoch time:      18358
10971308   =   yrday
fracday
Element set:     912
Inclination:       51
6373  deg
RA of node:       152
2398  deg
Eccentricity:     
0004432     
Arg of perigee:   180
2127  deg
Mean anomaly:     179
9024  deg
Mean motion:   15
54102147  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2804
Checksum:              295


Coasting Arc #14 (Orbit 2805)
---------------------------------------

Vector Time (GMT): 2018/358/04:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4973630
07                 A    =         6781188
02  meter
 Y    =       -1218922
43  meter          E    =           
0011675
 Z    =        4442291
56                 I    =           51
81372
 XDOT =       4305
111656                 Wp   =          131
54366
 YDOT =      -5407
278215  meter/sec      RA   =          150
74556  deg
 ZDOT =       3323
138334                 TA   =          284
93654
                                          MA   =          285
06578
                                          Ha   =            221
787  n
mi
                                          Hp   =            214
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -16317683
97                 X    =        -4981208
18
 Y    =       -3999089
35  feet           Y    =        -1274584
04  meter
 Z    =       14574447
38                 Z    =         4418113
04
 XDOT =      14124
382072                 XDOT =        4349
115502
 YDOT =     -17740
414091  feet/sec       YDOT =       -5358
889907  meter/sec
 ZDOT =      10902
684822                 ZDOT =        3344
156958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       13725566
04                 X    =         4183552
53
 Y    =        9850409
27  feet           Y    =         3002404
75  meter
 Z    =       14465556
20                 Z    =         4409101
53
 XDOT =     -18950
763428                 XDOT =       -5776
192693
 YDOT =      10191
106940  feet/sec       YDOT =        3106
249395  meter/sec
 ZDOT =      10998
006769                 ZDOT =        3352
192463


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   18358
23832037  
00016717  00000-0  10270-3 0  9134
2 25544  51
6390 151
5996 0004497 180
2116 179
9035 15
54092545 28065


Satellite: ISS
Catalog Number: 25544
Epoch time:      18358
23832037   =   yrday
fracday
Element set:     913
Inclination:       51
6390  deg
RA of node:       151
5996  deg
Eccentricity:     
0004497     
Arg of perigee:   180
2116  deg
Mean anomaly:     179
9035  deg
Mean motion:   15
54092545  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2806
Checksum:              323


Coasting Arc #15 (Orbit 2820)
---------------------------------------

Vector Time (GMT): 2018/359/04:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3722328
78                 A    =         6778210
78  meter
 Y    =        2368958
19  meter          E    =           
0013093
 Z    =       -5156356
46                 I    =           51
83409
 XDOT =      -5432
691717                 Wp   =           97
14611
 YDOT =       5171
491883  meter/sec      RA   =          145
76360  deg
 ZDOT =      -1550
860387                 TA   =          157
95804
                                          MA   =          157
90169
                                          Ha   =            221
557  n
mi
                                          Hp   =            214
736

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       12212364
78                 X    =         3720608
27
 Y    =        7772172
54  feet           Y    =         2410574
89  meter
 Z    =      -16917179
98                 Z    =        -5138278
82
 XDOT =     -17823
791723                 XDOT =       -5482
583871
 YDOT =      16966
836888  feet/sec       YDOT =        5110
460977  meter/sec
 ZDOT =      -5088
124628                 ZDOT =       -1577
370670

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8723229
88                 X    =        -2658840
47
 Y    =      -11670355
09  feet           Y    =        -3557124
23  meter
 Z    =      -16835901
24                 Z    =        -5131582
70
 XDOT =      21835
692893                 XDOT =        6655
519194
 YDOT =      -8831
625140  feet/sec       YDOT =       -2691
879343  meter/sec
 ZDOT =      -5208
204988                 ZDOT =       -1587
460880


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   18359
20286868  
00016717  00000-0  10270-3 0  9148
2 25544  51
6406 146
7915 0004367 183
6239 176
4883 15
54120201 28210


Satellite: ISS
Catalog Number: 25544
Epoch time:      18359
20286868   =   yrday
fracday
Element set:     914
Inclination:       51
6406  deg
RA of node:       146
7915  deg
Eccentricity:     
0004367     
Arg of perigee:   183
6239  deg
Mean anomaly:     176
4883  deg
Mean motion:   15
54120201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2821
Checksum:              322


Coasting Arc #16 (Orbit 2836)
---------------------------------------

Vector Time (GMT): 2018/360/04:25:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950917
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2326146
65                 A    =         6777351
24  meter
 Y    =       -3493593
84  meter          E    =           
0004106
 Z    =        5319594
81                 I    =           51
85806
 XDOT =       6112
590861                 Wp   =          154
53403
 YDOT =      -4619
567162  meter/sec      RA   =          140
77922  deg
 ZDOT =       -364
461397                 TA   =          298
90895
                                          MA   =          298
95013
                                          Ha   =            221
482  n
mi
                                          Hp   =            214
745

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7631714
74                 X    =        -2312746
78
 Y    =      -11461922
06  feet           Y    =        -3519532
04  meter
 Z    =       17452738
87                 Z    =         5308327
58
 XDOT =      20054
431959                 XDOT =        6165
564191
 YDOT =     -15156
060243  feet/sec       YDOT =       -4550
915692  meter/sec
 ZDOT =      -1195
739491                 ZDOT =        -334
640832

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3359590
53                 X    =         1024003
20
 Y    =       13419783
33  feet           Y    =         4090349
96  meter
 Z    =       17402281
11                 Z    =         5304215
28
 XDOT =     -23057
959716                 XDOT =       -7028
066121
 YDOT =       7133
052281  feet/sec       YDOT =        2174
154335  meter/sec
 ZDOT =      -1060
766947                 ZDOT =        -323
321765


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   18360
23171854  
00016717  00000-0  10270-3 0  9152
2 25544  51
6403 141
6635 0004394 189
1246 170
9828 15
54138221 28375


Satellite: ISS
Catalog Number: 25544
Epoch time:      18360
23171854   =   yrday
fracday
Element set:     915
Inclination:       51
6403  deg
RA of node:       141
6635  deg
Eccentricity:     
0004394     
Arg of perigee:   189
1246  deg
Mean anomaly:     170
9828  deg
Mean motion:   15
54138221  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2837
Checksum:              311


Coasting Arc #17 (Orbit 2850)
---------------------------------------

Vector Time (GMT): 2018/361/02:55:40
991
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -395458
29                 A    =         6782404
11  meter
 Y    =        5160984
56  meter          E    =           
0008931
 Z    =       -4391866
94                 I    =           51
89389
 XDOT =      -6403
424809                 Wp   =          139
03923
 YDOT =       2429
837267  meter/sec      RA   =          136
09820  deg
 ZDOT =       3429
321335                 TA   =          165
65325
                                          MA   =          165
62787
                                          Ha   =            221
376  n
mi
                                          Hp   =            216
179

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1297435
35                 X    =         -431807
45
 Y    =       16932364
05  feet           Y    =         5156359
36  meter
 Z    =      -14409012
27                 Z    =        -4393875
81
 XDOT =     -21008
611578                 XDOT =       -6446
777586
 YDOT =       7971
907045  feet/sec       YDOT =        2357
987059  meter/sec
 ZDOT =      11251
054249                 ZDOT =        3398
111099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12100149
78                 X    =         3688125
65
 Y    =      -11903699
55  feet           Y    =        -3628247
62  meter
 Z    =      -14418607
34                 Z    =        -4394791
52
 XDOT =      20217
710799                 XDOT =        6162
358252
 YDOT =       7083
706350  feet/sec       YDOT =        2159
113696  meter/sec
 ZDOT =      11110
022219                 ZDOT =        3386
334772


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   18361
13196358  
00016717  00000-0  10270-3 0  9169
2 25544  51
6398 137
1754 0004348 214
8936 145
1932 15
53700139 28519


Satellite: ISS
Catalog Number: 25544
Epoch time:      18361
13196358   =   yrday
fracday
Element set:     916
Inclination:       51
6398  deg
RA of node:       137
1754  deg
Eccentricity:     
0004348     
Arg of perigee:   214
8936  deg
Mean anomaly:     145
1932  deg
Mean motion:   15
53700139  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2851
Checksum:              322


Coasting Arc #18 (Orbit 2854)
---------------------------------------

Vector Time (GMT): 2018/361/09:04:00
000
Vector Time (MET): N/A
Weight (LBS)     : 950680
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         545187
69                 A    =         6780907
34  meter
 Y    =        4779634
12  meter          E    =           
0010950
 Z    =       -4789081
53                 I    =           51
89164
 XDOT =      -6325
442284                 Wp   =          132
51207
 YDOT =       3396
687452  meter/sec      RA   =          134
82868  deg
 ZDOT =       2666
573848                 TA   =          163
76785
                                          MA   =          163
73275
                                          Ha   =            221
424  n
mi
                                          Hp   =            216
238

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1788673
51                 X    =          514962
43
 Y    =       15681214
31  feet           Y    =         4785562
12  meter
 Z    =      -15712209
73                 Z    =        -4786506
31
 XDOT =     -20752
763400                 XDOT =       -6375
907487
 YDOT =      11143
987703  feet/sec       YDOT =        3325
669602  meter/sec
 ZDOT =       8748
601863                 ZDOT =        2635
725182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13365654
11                 X    =        -4073851
37
 Y    =       -8414777
77  feet           Y    =        -2564824
27  meter
 Z    =      -15701088
34                 Z    =        -4785691
73
 XDOT =       3854
069564                 XDOT =        1174
720403
 YDOT =     -22205
674668  feet/sec       YDOT =       -6768
289639  meter/sec
 ZDOT =       8609
096395                 ZDOT =        2624
052581


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   18361
38924299  
00016717  00000-0  10270-3 0  9170
2 25544  51
6365 135
8901 0004578 214
4828 145
6028 15
53693734 28550


Satellite: ISS
Catalog Number: 25544
Epoch time:      18361
38924299   =   yrday
fracday
Element set:     917
Inclination:       51
6365  deg
RA of node:       135
8901  deg
Eccentricity:     
0004578     
Arg of perigee:   214
4828  deg
Mean anomaly:     145
6028  deg
Mean motion:   15
53693734  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            2855
Checksum:              344
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