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

 
Date: June 10th 2016

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 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


164/08:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 4
000/00:00:00 000 0 0 0 0 214 2

166/13:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 2

170/05:52:30 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 0

171/22:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 220 2
000/00:00:00 000 0 0 0 0 214 0

Coasting Arc #1 (Orbit 395)
---------------------------------------

Vector Time (GMT): 2016/162/14:03:15
360
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1042492
70                 A    =         6787531
32  meter
 Y    =        6569210
73  meter          E    =           
0013744
 Z    =        1318067
81                 I    =           52
03101
 XDOT =      -4568
580510                 Wp   =           57
73515
 YDOT =      -1908
089765  meter/sec      RA   =           90
12081  deg
 ZDOT =       5859
187706                 TA   =          316
53961
                                          MA   =          316
64786
                                          Ha   =            220
344  n
mi
                                          Hp   =            214
194

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -3420251
63                 X    =        -1122276
36
 Y    =       21552528
64  feet           Y    =         6557106
67  meter
 Z    =        4324369
47                 Z    =         1312810
46
 XDOT =     -14988
781201                 XDOT =       -4575
365519
 YDOT =      -6260
137023  feet/sec       YDOT =       -1959
217128  meter/sec
 ZDOT =      19223
056778                 ZDOT =        5836
978124

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21479954
97                 X    =         6547090
27
 Y    =       -3876797
90  feet           Y    =        -1181648
00  meter
 Z    =        4300204
19                 Z    =         1310702
24
 XDOT =      -1188
744629                 XDOT =        -362
329363
 YDOT =      14765
532222  feet/sec       YDOT =        4500
534221  meter/sec
 ZDOT =      19126
623424                 ZDOT =        5829
794820


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   16162
64733618  
00016717  00000-0  10270-3 0  9001
2 25544  51
6440  90
6567 0000425 322
0926  38
0197 15
54497751  3964


Satellite: ISS
Catalog Number: 25544
Epoch time:      16162
64733618   =   yrday
fracday
Element set:     900
Inclination:       51
6440  deg
RA of node:        90
6567  deg
Eccentricity:     
0000425     
Arg of perigee:   322
0926  deg
Mean anomaly:      38
0197  deg
Mean motion:   15
54497751  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             396
Checksum:              309


Coasting Arc #2 (Orbit 410)
---------------------------------------

Vector Time (GMT): 2016/163/14:03:15
360
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1876769
45                 A    =         6784416
01  meter
 Y    =       -5779637
43  meter          E    =           
0004056
 Z    =       -3018519
60                 I    =           52
01955
 XDOT =       4244
639306                 Wp   =          109
38858
 YDOT =       3980
004105  meter/sec      RA   =           85
17082  deg
 ZDOT =      -4988
256118                 TA   =          104
97216
                                          MA   =          104
92726
                                          Ha   =            220
275  n
mi
                                          Hp   =            214
278

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6157380
09                 X    =         1955921
95
 Y    =      -18962065
05  feet           Y    =        -5758207
34  meter
 Z    =       -9903279
51                 Z    =        -3009210
93
 XDOT =      13925
981975                 XDOT =        4224
049174
 YDOT =      13057
756249  feet/sec       YDOT =        4027
355747  meter/sec
 ZDOT =     -16365
669678                 ZDOT =       -4967
686471

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19943425
72                 X    =        -6078756
16
 Y    =         746218
89  feet           Y    =          227447
52  meter
 Z    =       -9861597
93                 Z    =        -3005815
05
 XDOT =       7430
031133                 XDOT =        2264
673489
 YDOT =     -16235
806110  feet/sec       YDOT =       -4948
673702  meter/sec
 ZDOT =     -16276
782140                 ZDOT =       -4961
163196


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   16163
61162744  
00016717  00000-0  10270-3 0  9016
2 25544  51
6437  85
8481 0000474 297
4479  62
6625 15
54500064  4112


Satellite: ISS
Catalog Number: 25544
Epoch time:      16163
61162744   =   yrday
fracday
Element set:     901
Inclination:       51
6437  deg
RA of node:        85
8481  deg
Eccentricity:     
0000474     
Arg of perigee:   297
4479  deg
Mean anomaly:      62
6625  deg
Mean motion:   15
54500064  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             411
Checksum:              302


Coasting Arc #3 (Orbit 422)
---------------------------------------

Vector Time (GMT): 2016/164/08:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4243016
39                 A    =         6776647
77  meter
 Y    =        -674382
30  meter          E    =           
0003850
 Z    =        5238533
15                 I    =           51
98742
 XDOT =       -229
361497                 Wp   =           51
09794
 YDOT =      -7579
830422  meter/sec      RA   =           81
40785  deg
 ZDOT =      -1158
639578                 TA   =           49
97094
                                          MA   =           49
93717
                                          Ha   =            220
431  n
mi
                                          Hp   =            214
151

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13920657
44                 X    =        -4260606
45
 Y    =       -2212540
37  feet           Y    =         -721929
28  meter
 Z    =       17186788
57                 Z    =         5217878
88
 XDOT =       -752
498350                 XDOT =        -138
956716
 YDOT =     -24868
210046  feet/sec       YDOT =       -7581
889727  meter/sec
 ZDOT =      -3801
310950                 ZDOT =       -1159
534733

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13866117
65                 X    =        -4226392
66
 Y    =        3081010
76  feet           Y    =          939092
08  meter
 Z    =       17096897
19                 Z    =         5211134
26
 XDOT =      -9559
858505                 XDOT =       -2913
844872
 YDOT =     -21863
275649  feet/sec       YDOT =       -6663
926418  meter/sec
 ZDOT =      -3803
747057                 ZDOT =       -1159
382103


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   16164
38305654  
00016717  00000-0  10270-3 0  9021
2 25544  51
6399  81
9987 0000356 308
9387  51
1734 15
54521494  4239


Satellite: ISS
Catalog Number: 25544
Epoch time:      16164
38305654   =   yrday
fracday
Element set:     902
Inclination:       51
6399  deg
RA of node:        81
9987  deg
Eccentricity:     
0000356     
Arg of perigee:   308
9387  deg
Mean anomaly:      51
1734  deg
Mean motion:   15
54521494  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             423
Checksum:              324


Coasting Arc #4 (Orbit 437)
---------------------------------------

Vector Time (GMT): 2016/165/08:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4301657
79                 A    =         6779400
95  meter
 Y    =        2556665
65  meter          E    =           
0009575
 Z    =       -4583176
13                 I    =           51
99186
 XDOT =       -821
894418                 Wp   =          108
69134
 YDOT =       6952
824373  meter/sec      RA   =           76
43204  deg
 ZDOT =       3109
449621                 TA   =          192
30435
                                          MA   =          192
32774
                                          Ha   =            220
321  n
mi
                                          Hp   =            214
245

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14113050
50                 X    =         4295011
95
 Y    =        8388010
65  feet           Y    =         2604732
83  meter
 Z    =      -15036667
10                 Z    =        -4562295
66
 XDOT =      -2696
503996                 XDOT =        -914
685960
 YDOT =      22811
103586  feet/sec       YDOT =        6943
114343  meter/sec
 ZDOT =      10201
606367                 ZDOT =        3105
232189

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16336157
55                 X    =         4979260
82
 Y    =        2319610
84  feet           Y    =          707017
38  meter
 Z    =      -14946157
92                 Z    =        -4555588
93
 XDOT =       6334
510394                 XDOT =        1930
758768
 YDOT =      20944
878287  feet/sec       YDOT =        6383
998902  meter/sec
 ZDOT =      10181
867699                 ZDOT =        3103
433275


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   16165
34733599  
00016717  00000-0  10270-3 0  9032
2 25544  51
6409  77
1891 0000404 327
4384  32
6743 15
54520372  4383


Satellite: ISS
Catalog Number: 25544
Epoch time:      16165
34733599   =   yrday
fracday
Element set:     903
Inclination:       51
6409  deg
RA of node:        77
1891  deg
Eccentricity:     
0000404     
Arg of perigee:   327
4384  deg
Mean anomaly:      32
6743  deg
Mean motion:   15
54520372  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             438
Checksum:              309


Coasting Arc #5 (Orbit 453)
---------------------------------------

Vector Time (GMT): 2016/166/08:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 923955
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4159525
43                 A    =         6783405
90  meter
 Y    =       -4174508
50  meter          E    =           
0012349
 Z    =        3349060
59                 I    =           51
99694
 XDOT =       1955
004271                 Wp   =           89
28784
 YDOT =      -5734
935611  meter/sec      RA   =           71
46609  deg
 ZDOT =      -4705
249973                 TA   =           51
88035
                                          MA   =           51
76908
                                          Ha   =            220
320  n
mi
                                          Hp   =            214
110

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13646736
99                 X    =        -4128804
26
 Y    =      -13695894
03  feet           Y    =        -4220851
58  meter
 Z    =       10987731
61                 Z    =         3328928
85
 XDOT =       6414
056006                 XDOT =        2041
844645
 YDOT =     -18815
405549  feet/sec       YDOT =       -5712
587522  meter/sec
 ZDOT =     -15437
171828                 ZDOT =       -4695
542538

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18034613
07                 X    =        -5496950
06
 Y    =       -7103961
21  feet           Y    =        -2165287
38  meter
 Z    =       10900809
88                 Z    =         3322566
85
 XDOT =      -2031
829312                 XDOT =        -619
301574
 YDOT =     -18539
550223  feet/sec       YDOT =       -5650
854908  meter/sec
 ZDOT =     -15393
731160                 ZDOT =       -4692
009258


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   16166
37589243  
00016717  00000-0  10270-3 0  9042
2 25544  51
6407  72
0587 0000517 331
8838  28
2287 15
54554867  4543


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
37589243   =   yrday
fracday
Element set:     904
Inclination:       51
6407  deg
RA of node:        72
0587  deg
Eccentricity:     
0000517     
Arg of perigee:   331
8838  deg
Mean anomaly:      28
2287  deg
Mean motion:   15
54554867  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             454
Checksum:              329


Coasting Arc #6 (Orbit 456)
---------------------------------------

Vector Time (GMT): 2016/166/13:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 912263
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4128185
57                 A    =         6784146
13  meter
 Y    =        4420942
39  meter          E    =           
0004364
 Z    =       -3073155
54                 I    =           52
00059
 XDOT =      -2156
755337                 Wp   =           63
95144
 YDOT =       5445
505208  meter/sec      RA   =           70
34824  deg
 ZDOT =       4943
841662                 TA   =          260
96226
                                          MA   =          261
01165
                                          Ha   =            220
234  n
mi
                                          Hp   =            214
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13543915
92                 X    =         4093370
81
 Y    =       14504404
17  feet           Y    =         4466912
10  meter
 Z    =      -10082531
28                 Z    =        -3053185
93
 XDOT =      -7075
968952                 XDOT =       -2241
503226
 YDOT =      17865
830735  feet/sec       YDOT =        5420
912675  meter/sec
 ZDOT =      16219
952960                 ZDOT =        4933
159230

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10508986
23                 X    =         3203139
00
 Y    =      -16885102
65  feet           Y    =        -5146579
29  meter
 Z    =       -9996366
98                 Z    =        -3046892
66
 XDOT =      17882
665858                 XDOT =        5450
636553
 YDOT =       1569
759632  feet/sec       YDOT =         478
462736  meter/sec
 ZDOT =      16172
317292                 ZDOT =        4929
322311


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   16166
56874547  
00016717  00000-0  10270-3 0  9058
2 25544  51
6441  71
0984 0000618 323
7901  36
3210 15
54556187  4570


Satellite: ISS
Catalog Number: 25544
Epoch time:      16166
56874547   =   yrday
fracday
Element set:     905
Inclination:       51
6441  deg
RA of node:        71
0984  deg
Eccentricity:     
0000618     
Arg of perigee:   323
7901  deg
Mean anomaly:      36
3210  deg
Mean motion:   15
54556187  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             457
Checksum:              312


Coasting Arc #7 (Orbit 472)
---------------------------------------

Vector Time (GMT): 2016/167/13:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 912263
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3700460
44                 A    =         6787370
48  meter
 Y    =       -5515426
07  meter          E    =           
0013399
 Z    =        1367170
70                 I    =           51
99978
 XDOT =       3329
644325                 Wp   =          119
24460
 YDOT =      -3691
082629  meter/sec      RA   =           65
39592  deg
 ZDOT =      -5841
734376                 TA   =           45
93108
                                          MA   =           45
82084
                                          Ha   =            220
274  n
mi
                                          Hp   =            214
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12140618
25                 X    =        -3645151
71
 Y    =      -18095229
90  feet           Y    =        -5556497
96  meter
 Z    =        4485468
17                 Z    =         1349328
49
 XDOT =      10924
029937                 XDOT =        3399
048297
 YDOT =     -12109
851144  feet/sec       YDOT =       -3653
459727  meter/sec
 ZDOT =     -19165
795197                 ZDOT =       -5825
391447

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14065338
42                 X    =        -4287115
15
 Y    =       16663735
48  feet           Y    =         5079106
57  meter
 Z    =        4408804
44                 Z    =         1343803
59
 XDOT =     -13461
111217                 XDOT =       -4102
946699
 YDOT =      -6278
042249  feet/sec       YDOT =       -1913
547277  meter/sec
 ZDOT =     -19093
827276                 ZDOT =       -5819
798554


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   16167
59729360  
00016717  00000-0  10270-3 0  9065
2 25544  51
6443  65
9687 0000445 321
2893  38
8228 15
54539776  4734


Satellite: ISS
Catalog Number: 25544
Epoch time:      16167
59729360   =   yrday
fracday
Element set:     906
Inclination:       51
6443  deg
RA of node:        65
9687  deg
Eccentricity:     
0000445     
Arg of perigee:   321
2893  deg
Mean anomaly:      38
8228  deg
Mean motion:   15
54539776  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             473
Checksum:              343


Coasting Arc #8 (Orbit 488)
---------------------------------------

Vector Time (GMT): 2016/168/13:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 912263
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3006566
73                 A    =         6787849
28  meter
 Y    =        6059571
35  meter          E    =           
0012960
 Z    =         477635
24                 I    =           51
98828
 XDOT =      -4433
806697                 Wp   =           47
02931
 YDOT =       1718
071487  meter/sec      RA   =           60
44712  deg
 ZDOT =       6018
782686                 TA   =          318
09958
                                          MA   =          318
19869
                                          Ha   =            220
111  n
mi
                                          Hp   =            214
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9864064
08                 X    =         2936263
47
 Y    =       19880483
43  feet           Y    =         6092799
64  meter
 Z    =        1567044
74                 Z    =          492070
39
 XDOT =     -14546
609898                 XDOT =       -4481
925954
 YDOT =       5636
717476  feet/sec       YDOT =        1668
220018  meter/sec
 ZDOT =      19746
662356                 ZDOT =        5997
127496

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16158357
60                 X    =         4925067
40
 Y    =      -15206699
41  feet           Y    =        -4635001
98  meter
 Z    =        1628736
82                 Z    =          496438
98
 XDOT =       8551
170304                 XDOT =        2606
396709
 YDOT =      11223
001651  feet/sec       YDOT =        3420
770903  meter/sec
 ZDOT =      19651
931598                 ZDOT =        5989
908751


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   16168
62582894  
00016717  00000-0  10270-3 0  9070
2 25544  51
6448  60
8378 0000701 319
4561  40
6539 15
54602795  4891


Satellite: ISS
Catalog Number: 25544
Epoch time:      16168
62582894   =   yrday
fracday
Element set:     907
Inclination:       51
6448  deg
RA of node:        60
8378  deg
Eccentricity:     
0000701     
Arg of perigee:   319
4561  deg
Mean anomaly:      40
6539  deg
Mean motion:   15
54602795  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             489
Checksum:              335


Coasting Arc #9 (Orbit 503)
---------------------------------------

Vector Time (GMT): 2016/169/13:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 912263
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1986585
90                 A    =         6785785
91  meter
 Y    =       -6066012
14  meter          E    =           
0005113
 Z    =       -2299668
92                 I    =           51
96343
 XDOT =       5381
066781                 Wp   =          134
53466
 YDOT =        300
127867  meter/sec      RA   =           55
49595  deg
 ZDOT =      -5451
073608                 TA   =           70
95514
                                          MA   =           70
89976
                                          Ha   =            220
142  n
mi
                                          Hp   =            214
148

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -6517670
27                 X    =        -1907435
70
 Y    =      -19901614
62  feet           Y    =        -6087784
63  meter
 Z    =       -7544845
53                 Z    =        -2309127
82
 XDOT =      17654
418573                 XDOT =        5403
789907
 YDOT =        984
671481  feet/sec       YDOT =         360
430254  meter/sec
 ZDOT =     -17884
099765                 ZDOT =       -5424
878303

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -16954419
81                 X    =        -5167707
16
 Y    =       12267718
51  feet           Y    =         3739200
60  meter
 Z    =       -7584834
57                 Z    =        -2311857
58
 XDOT =      -3626
313479                 XDOT =       -1105
300349
 YDOT =     -15976
396113  feet/sec       YDOT =       -4869
605535  meter/sec
 ZDOT =     -17769
989137                 ZDOT =       -5416
292689


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   16169
59007635  
00016717  00000-0  10270-3 0  9083
2 25544  51
6437  56
0282 0000705 318
5733  41
5366 15
54566515  5040


Satellite: ISS
Catalog Number: 25544
Epoch time:      16169
59007635   =   yrday
fracday
Element set:     908
Inclination:       51
6437  deg
RA of node:        56
0282  deg
Eccentricity:     
0000705     
Arg of perigee:   318
5733  deg
Mean anomaly:      41
5366  deg
Mean motion:   15
54566515  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             504
Checksum:              307


Coasting Arc #10 (Orbit 514)
---------------------------------------

Vector Time (GMT): 2016/170/05:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1352027
12                 A    =         6777819
75  meter
 Y    =        4495029
74  meter          E    =           
0006323
 Z    =        4885643
67                 I    =           51
92159
 XDOT =      -5813
138884                 Wp   =          118
01356
 YDOT =      -4383
215041  meter/sec      RA   =           52
10488  deg
 ZDOT =       2418
800257                 TA   =          308
34653
                                          MA   =          308
40334
                                          Ha   =            220
192  n
mi
                                          Hp   =            214
024

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4435784
53                 X    =        -1425923
69
 Y    =       14747472
89  feet           Y    =         4479496
65  meter
 Z    =       16029014
65                 Z    =         4878896
92
 XDOT =     -19071
977967                 XDOT =       -5775
442194
 YDOT =     -14380
626774  feet/sec       YDOT =       -4448
010974  meter/sec
 ZDOT =       7935
696380                 ZDOT =        2390
652277

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6011234
24                 X    =        -1832224
20
 Y    =       14212690
15  feet           Y    =         4332027
96  meter
 Z    =       15998685
98                 Z    =         4876399
49
 XDOT =     -16529
620696                 XDOT =       -5038
228388
 YDOT =     -15806
515019  feet/sec       YDOT =       -4817
825778  meter/sec
 ZDOT =       7813
913813                 ZDOT =        2381
680930


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   16170
29718635  
00016717  00000-0  10270-3 0  9092
2 25544  51
6408  52
5004 0000615 328
7691  31
3425 15
54612096  5158


Satellite: ISS
Catalog Number: 25544
Epoch time:      16170
29718635   =   yrday
fracday
Element set:     909
Inclination:       51
6408  deg
RA of node:        52
5004  deg
Eccentricity:     
0000615     
Arg of perigee:   328
7691  deg
Mean anomaly:      31
3425  deg
Mean motion:   15
54612096  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             515
Checksum:              294


Coasting Arc #11 (Orbit 529)
---------------------------------------

Vector Time (GMT): 2016/171/05:52:30
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2794734
44                 A    =         6776010
33  meter
 Y    =       -3133993
61  meter          E    =           
0014662
 Z    =       -5330716
39                 I    =           51
89544
 XDOT =       5403
896295                 Wp   =           85
00959
 YDOT =       5415
556678  meter/sec      RA   =           47
11992  deg
 ZDOT =       -350
358343                 TA   =          181
65507
                                          MA   =          181
65993
                                          Ha   =            220
188  n
mi
                                          Hp   =            214
084

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        9169076
25                 X    =         2855466
26
 Y    =      -10282131
28  feet           Y    =        -3102400
70  meter
 Z    =      -17489227
01                 Z    =        -5316993
15
 XDOT =      17729
318552                 XDOT =        5344
638448
 YDOT =      17767
574404  feet/sec       YDOT =        5475
655365  meter/sec
 ZDOT =      -1149
469630                 ZDOT =        -324
250607

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10115307
38                 X    =         3083145
69
 Y    =       -9464985
72  feet           Y    =        -2884927
65  meter
 Z    =      -17428764
92                 Z    =        -5312287
55
 XDOT =      15485
718046                 XDOT =        4720
046860
 YDOT =      18461
377830  feet/sec       YDOT =        5627
027963  meter/sec
 ZDOT =      -1036
800721                 ZDOT =        -316
016860


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   16171
26142121  
00016717  00000-0  10270-3 0  9103
2 25544  51
6414  47
6901 0000595 340
0872  20
0257 15
54602519  5305


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
26142121   =   yrday
fracday
Element set:     910
Inclination:       51
6414  deg
RA of node:        47
6901  deg
Eccentricity:     
0000595     
Arg of perigee:   340
0872  deg
Mean anomaly:      20
0257  deg
Mean motion:   15
54602519  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             530
Checksum:              262


Coasting Arc #12 (Orbit 540)
---------------------------------------

Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5685252
89                 A    =         6784422
07  meter
 Y    =       -2302054
78  meter          E    =           
0012976
 Z    =        2886051
50                 I    =           51
91141
 XDOT =       -258
195014                 Wp   =           97
68580
 YDOT =      -5747
096892  meter/sec      RA   =           43
68487  deg
 ZDOT =      -5075
001376                 TA   =           49
56642
                                          MA   =           49
45330
                                          Ha   =            220
165  n
mi
                                          Hp   =            214
030

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -18652404
50                 X    =        -5673107
42
 Y    =       -7552673
17  feet           Y    =        -2365563
58  meter
 Z    =        9468672
90                 Z    =         2858463
06
 XDOT =       -847
096503                 XDOT =        -169
258126
 YDOT =     -18855
304765  feet/sec       YDOT =       -5749
486173  meter/sec
 ZDOT =     -16650
266983                 ZDOT =       -5076
040460

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15289584
98                 X    =         4660265
50
 Y    =      -13169561
70  feet           Y    =        -4014082
41  meter
 Z    =        9348907
30                 Z    =         2849546
95
 XDOT =      16137
786712                 XDOT =        4918
797390
 YDOT =       6871
504221  feet/sec       YDOT =        2094
434487  meter/sec
 ZDOT =     -16653
598999                 ZDOT =       -5076
016975


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   16171
96852018  
00016717  00000-0  10270-3 0  9114
2 25544  51
6443  44
1620 0000476 316
9543  43
1573 15
54631968  5411


Satellite: ISS
Catalog Number: 25544
Epoch time:      16171
96852018   =   yrday
fracday
Element set:     911
Inclination:       51
6443  deg
RA of node:        44
1620  deg
Eccentricity:     
0000476     
Arg of perigee:   316
9543  deg
Mean anomaly:      43
1573  deg
Mean motion:   15
54631968  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             541
Checksum:              299


Coasting Arc #13 (Orbit 555)
---------------------------------------

Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5735084
41                 A    =         6787447
30  meter
 Y    =        3429991
26  meter          E    =           
0009627
 Z    =       -1162933
59                 I    =           51
89648
 XDOT =      -1590
306156                 Wp   =           33
99610
 YDOT =       4645
513297  meter/sec      RA   =           38
72615  deg
 ZDOT =       5890
170491                 TA   =          313
41933
                                          MA   =          313
49942
                                          Ha   =            220
188  n
mi
                                          Hp   =            214
092

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       18815893
72                 X    =         5701952
16
 Y    =       11253252
16  feet           Y    =         3493939
71  meter
 Z    =       -3815398
91                 Z    =        -1135153
98
 XDOT =      -5217
539881                 XDOT =       -1670
747124
 YDOT =      15241
185359  feet/sec       YDOT =        4627
278780  meter/sec
 ZDOT =      19324
706336                 ZDOT =        5882
250506

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18435129
44                 X    =        -5619027
45
 Y    =       11904768
00  feet           Y    =         3628573
29  meter
 Z    =       -3695038
69                 Z    =        -1126247
79
 XDOT =     -10430
571288                 XDOT =       -3179
238128
 YDOT =     -10198
080281  feet/sec       YDOT =       -3108
374870  meter/sec
 ZDOT =      19289
213309                 ZDOT =        5879
352216


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   16172
93274175  
00016717  00000-0  10270-3 0  9125
2 25544  51
6435  39
3524 0000673 326
6566  33
4544 15
54589745  5564


Satellite: ISS
Catalog Number: 25544
Epoch time:      16172
93274175   =   yrday
fracday
Element set:     912
Inclination:       51
6435  deg
RA of node:        39
3524  deg
Eccentricity:     
0000673     
Arg of perigee:   326
6566  deg
Mean anomaly:      33
4544  deg
Mean motion:   15
54589745  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             556
Checksum:              323


Coasting Arc #14 (Orbit 571)
---------------------------------------

Vector Time (GMT): 2016/173/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5261218
36                 A    =         6787578
62  meter
 Y    =       -4216987
44  meter          E    =           
0009877
 Z    =        -739998
87                 I    =           51
87106
 XDOT =       3486
066107                 Wp   =          139
37917
 YDOT =      -3310
054130  meter/sec      RA   =           33
77118  deg
 ZDOT =      -5974
339886                 TA   =           48
59267
                                          MA   =           48
50782
                                          Ha   =            220
089  n
mi
                                          Hp   =            213
954

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -17261215
08                 X    =        -5210077
34
 Y    =      -13835260
62  feet           Y    =        -4275535
83  meter
 Z    =       -2427817
83                 Z    =         -765432
84
 XDOT =      11437
224760                 XDOT =        3551
841498
 YDOT =     -10859
757644  feet/sec       YDOT =       -3270
701979  meter/sec
 ZDOT =     -19600
852643                 ZDOT =       -5957
246247

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19880366
28                 X    =         6059535
64
 Y    =       -9674138
80  feet           Y    =        -2948677
51  meter
 Z    =       -2537785
83                 Z    =         -773517
12
 XDOT =       4169
411425                 XDOT =        1270
836602
 YDOT =      13647
402952  feet/sec       YDOT =        4159
728420  meter/sec
 ZDOT =     -19525
652607                 ZDOT =       -5951
418915


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   16173
96123968  
00016717  00000-0  10270-3 0  9133
2 25544  51
6427  34
2220 0000485 329
8418  30
2707 15
54642818  5729


Satellite: ISS
Catalog Number: 25544
Epoch time:      16173
96123968   =   yrday
fracday
Element set:     913
Inclination:       51
6427  deg
RA of node:        34
2220  deg
Eccentricity:     
0000485     
Arg of perigee:   329
8418  deg
Mean anomaly:      30
2707  deg
Mean motion:   15
54642818  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             572
Checksum:              306


Coasting Arc #15 (Orbit 587)
---------------------------------------

Vector Time (GMT): 2016/174/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4279772
90                 A    =         6785079
34  meter
 Y    =        4613519
86  meter          E    =           
0013631
 Z    =        2519437
66                 I    =           51
83592
 XDOT =      -5195
689583                 Wp   =           73
25899
 YDOT =       1907
660720  meter/sec      RA   =           28
80975  deg
 ZDOT =       5312
782037                 TA   =          314
95243
                                          MA   =          315
06289
                                          Ha   =            220
099  n
mi
                                          Hp   =            213
899

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       14041249
67                 X    =         4215627
03
 Y    =       15136220
02  feet           Y    =         4661020
13  meter
 Z    =        8265871
58                 Z    =         2540072
39
 XDOT =     -17046
225667                 XDOT =       -5242
442376
 YDOT =       6258
729395  feet/sec       YDOT =        1849
296933  meter/sec
 ZDOT =      17430
387260                 ZDOT =        5287
429567

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -19555059
20                 X    =        -5960382
04
 Y    =        6510212
68  feet           Y    =         1984312
82  meter
 Z    =        8354835
26                 Z    =         2546553
79
 XDOT =       1838
352472                 XDOT =         560
329834
 YDOT =     -16787
749737  feet/sec       YDOT =       -5116
906120  meter/sec
 ZDOT =      17319
485716                 ZDOT =        5278
979246


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   16174
98972962  
00016717  00000-0  10270-3 0  9143
2 25544  51
6430  29
0907 0000573 341
3122  18
8010 15
54645032  5883


Satellite: ISS
Catalog Number: 25544
Epoch time:      16174
98972962   =   yrday
fracday
Element set:     914
Inclination:       51
6430  deg
RA of node:        29
0907  deg
Eccentricity:     
0000573     
Arg of perigee:   341
3122  deg
Mean anomaly:      18
8010  deg
Mean motion:   15
54645032  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             588
Checksum:              300


Coasting Arc #16 (Orbit 602)
---------------------------------------

Vector Time (GMT): 2016/175/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2811506
67                 A    =         6780921
17  meter
 Y    =       -4694779
22  meter          E    =           
0007196
 Z    =       -4012273
47                 I    =           51
79334
 XDOT =       6534
183317                 Wp   =           66
76997
 YDOT =       -525
970390  meter/sec      RA   =           23
83667  deg
 ZDOT =      -3966
113338                 TA   =          162
03660
                                          MA   =          162
01115
                                          Ha   =            220
145  n
mi
                                          Hp   =            213
822

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9224103
25                 X    =        -2739309
81
 Y    =      -15402818
95  feet           Y    =        -4725815
20  meter
 Z    =      -13163626
85                 Z    =        -4025756
14
 XDOT =      21437
609307                 XDOT =        6558
844702
 YDOT =      -1725
624640  feet/sec       YDOT =        -452
762434  meter/sec
 ZDOT =     -13012
182868                 ZDOT =       -3934
312371

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17764340
47                 X    =         5414570
97
 Y    =       -2287969
79  feet           Y    =         -697373
19  meter
 Z    =      -13221398
81                 Z    =        -4029882
36
 XDOT =      -7108
028469                 XDOT =       -2166
527077
 YDOT =      19148
661032  feet/sec       YDOT =        5836
511883  meter/sec
 ZDOT =     -12873
469758                 ZDOT =       -3923
833582


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   16175
95393341  
00016717  00000-0  10270-3 0  9150
2 25544  51
6428  24
2807 0000609 351
9110   8
2033 15
54653718  6036


Satellite: ISS
Catalog Number: 25544
Epoch time:      16175
95393341   =   yrday
fracday
Element set:     915
Inclination:       51
6428  deg
RA of node:        24
2807  deg
Eccentricity:     
0000609     
Arg of perigee:   351
9110  deg
Mean anomaly:       8
2033  deg
Mean motion:   15
54653718  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             603
Checksum:              290


Coasting Arc #17 (Orbit 618)
---------------------------------------

Vector Time (GMT): 2016/176/22:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 897031
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1008035
47                 A    =         6777195
99  meter
 Y    =        4487515
53  meter          E    =           
0005702
 Z    =        4974116
45                 I    =           51
75070
 XDOT =      -7333
091504                 Wp   =          117
86444
 YDOT =       -724
672119  meter/sec      RA   =           18
84937  deg
 ZDOT =       2135
405106                 TA   =          311
35288
                                          MA   =          311
40192
                                          Ha   =            220
098  n
mi
                                          Hp   =            213
840

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3307202
97                 X    =          933618
14
 Y    =       14722819
98  feet           Y    =         4498371
45  meter
 Z    =       16319279
70                 Z    =         4978832
90
 XDOT =     -24058
699161                 XDOT =       -7334
815806
 YDOT =      -2377
533200  feet/sec       YDOT =        -806
685495  meter/sec
 ZDOT =       7005
922264                 ZDOT =        2099
778860

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14835543
11                 X    =        -4521873
54
 Y    =       -2639188
85  feet           Y    =         -804424
76  meter
 Z    =       16338887
74                 Z    =         4980092
98
 XDOT =      11173
520028                 XDOT =        3405
688905
 YDOT =     -20305
969019  feet/sec       YDOT =       -6189
259357  meter/sec
 ZDOT =       6850
806686                 ZDOT =        2088
125878


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   16176
98241091  
00016717  00000-0  10270-3 0  9169
2 25544  51
6422  19
1501 0000653 350
8776   9
2365 15
54676574  6190


Satellite: ISS
Catalog Number: 25544
Epoch time:      16176
98241091   =   yrday
fracday
Element set:     916
Inclination:       51
6422  deg
RA of node:        19
1501  deg
Eccentricity:     
0000653     
Arg of perigee:   350
8776  deg
Mean anomaly:       9
2365  deg
Mean motion:   15
54676574  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             619
Checksum:              313
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