[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 27th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 ET - UTC (sec) : 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 2482)
---------------------------------------
Vector Time (GMT): 2015/147/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4982053
41 A = 6779808
06 meter
Y = -2532227
06 meter E =
0012032
Z = 3834127
93 I = 51
59690
XDOT = 5168
565263 Wp = 60
66713
YDOT = 3854
744684 meter/sec RA = 186
00133 deg
ZDOT = -4154
568751 TA = 73
12172
MA = 72
98982
Ha = 219
597 n
mi
Hp = 213
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16345319
60 X = 4991374
17
Y = -8307831
55 feet Y = -2476462
50 meter
Z = 12579159
86 Z = 3858352
55
XDOT = 16957
235116 XDOT = 5145
257980
YDOT = 12646
800144 feet/sec YDOT = 3912
412796 meter/sec
ZDOT = -13630
474906 ZDOT = -4129
517091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4436301
68 X = -1352184
75
Y = -17716411
60 feet Y = -5399962
26 meter
Z = 12683563
70 Z = 3865950
22
XDOT = 14862
427726 XDOT = 4530
067971
YDOT = -13439
831685 feet/sec YDOT = -4096
460698 meter/sec
ZDOT = -13523
593332 ZDOT = -4121
991247
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 15147
57683008
00016717 00000-0 10270-3 0 9002
2 25544 51
6424 186
9489 0004374 350
6069 9
5002 15
55221704 24831
Satellite: ISS
Catalog Number: 25544
Epoch time: 15147
57683008 = yrday
fracday
Element set: 900
Inclination: 51
6424 deg
RA of node: 186
9489 deg
Eccentricity:
0004374
Arg of perigee: 350
6069 deg
Mean anomaly: 9
5002 deg
Mean motion: 15
55221704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2483
Checksum: 307
Coasting Arc #2 (Orbit 2497)
---------------------------------------
Vector Time (GMT): 2015/148/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6224446
77 A = 6784028
14 meter
Y = 1599083
98 meter E =
0009554
Z = -2159451
76 I = 51
64377
XDOT = -3033
141746 Wp = 23
92140
YDOT = -4405
047646 meter/sec RA = 181
01298 deg
ZDOT = 5497
885681 TA = 312
11310
MA = 312
19427
Ha = 219
640 n
mi
Hp = 212
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20421413
30 X = -6231375
56
Y = 5246338
53 feet Y = 1529439
49 meter
Z = -7084815
47 Z = -2189706
05
XDOT = -9951
252447 XDOT = -3010
365019
YDOT = -14452
256057 feet/sec YDOT = -4438
839091 meter/sec
ZDOT = 18037
682681 ZDOT = 5483
206229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 890997
30 X = 271575
98
Y = 21021496
59 feet Y = 6407352
16 meter
Z = -7214957
01 Z = -2199118
90
XDOT = -14695
858398 XDOT = -4479
297640
YDOT = 6773
510368 feet/sec YDOT = 2064
565960 meter/sec
ZDOT = 17975
408152 ZDOT = 5478
904405
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 15148
54069510
00016717 00000-0 10270-3 0 9017
2 25544 51
6433 182
1364 0004268 355
1473 4
9638 15
55244980 24983
Satellite: ISS
Catalog Number: 25544
Epoch time: 15148
54069510 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 182
1364 deg
Eccentricity:
0004268
Arg of perigee: 355
1473 deg
Mean anomaly: 4
9638 deg
Mean motion: 15
55244980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2498
Checksum: 314
Coasting Arc #3 (Orbit 2513)
---------------------------------------
Vector Time (GMT): 2015/149/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6758862
43 A = 6786143
90 meter
Y = -561675
95 meter E =
0009877
Z = 117981
88 I = 51
68077
XDOT = 504
811229 Wp = 114
85909
YDOT = 4729
253782 meter/sec RA = 176
03724 deg
ZDOT = -6013
981040 TA = 63
87061
MA = 63
76902
Ha = 219
866 n
mi
Hp = 212
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22174745
51 X = 6764067
77
Y = -1842768
87 feet Y = -486064
83 meter
Z = 387079
66 Z = 150828
23
XDOT = 1656
204819 XDOT = 481
104166
YDOT = 15515
924482 feet/sec YDOT = 4734
766656 meter/sec
ZDOT = -19730
908924 ZDOT = -6011
586077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2431104
57 X = 741000
67
Y = -22115056
26 feet Y = -6740669
15 meter
Z = 528188
78 Z = 160991
94
XDOT = 13955
827285 XDOT = 4253
736157
YDOT = 1040
703501 feet/sec YDOT = 317
206427 meter/sec
ZDOT = -19721
423898 ZDOT = -6011
090004
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 15149
56880858
00016717 00000-0 10270-3 0 9027
2 25544 51
6419 177
0021 0004384 358
9280 1
1863 15
55220195 25146
Satellite: ISS
Catalog Number: 25544
Epoch time: 15149
56880858 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 177
0021 deg
Eccentricity:
0004384
Arg of perigee: 358
9280 deg
Mean anomaly: 1
1863 deg
Mean motion: 15
55220195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2514
Checksum: 307
Coasting Arc #4 (Orbit 2529)
---------------------------------------
Vector Time (GMT): 2015/150/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6479342
77 A = 6784603
47 meter
Y = -510444
24 meter E =
0016336
Z = 1913201
11 I = 51
70691
XDOT = 2045
123100 Wp = 52
69063
YDOT = -4812
478225 meter/sec RA = 171
06501 deg
ZDOT = 5618
904777 TA = 328
39692
MA = 328
49492
Ha = 219
945 n
mi
Hp = 212
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21257686
27 X = -6482447
07
Y = -1674685
81 feet Y = -582917
97 meter
Z = 6276906
52 Z = 1881717
62
XDOT = 6709
721458 XDOT = 2071
490395
YDOT = -15788
970555 feet/sec YDOT = -4789
461257 meter/sec
ZDOT = 18434
726959 ZDOT = 5628
903488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5360860
18 X = -1633990
18
Y = 20679280
59 feet Y = 6303044
73 meter
Z = 6141814
54 Z = 1872025
07
XDOT = -12888
451615 XDOT = -3928
400052
YDOT = -8852
487338 feet/sec YDOT = -2698
238141 meter/sec
ZDOT = 18478
472627 ZDOT = 5632
238457
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 15150
59691233
00016717 00000-0 10270-3 0 9030
2 25544 51
6415 171
8686 0004461 1
4931 358
6234 15
55244718 25307
Satellite: ISS
Catalog Number: 25544
Epoch time: 15150
59691233 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 171
8686 deg
Eccentricity:
0004461
Arg of perigee: 1
4931 deg
Mean anomaly: 358
6234 deg
Mean motion: 15
55244718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2530
Checksum: 301
Coasting Arc #5 (Orbit 2544)
---------------------------------------
Vector Time (GMT): 2015/151/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5454625
90 A = 6780451
70 meter
Y = 1645177
49 meter E =
0007946
Z = -3686174
31 I = 51
72320
XDOT = -4321
377207 Wp = 47
87536
YDOT = 4600
637035 meter/sec RA = 166
08377 deg
ZDOT = -4342
057152 TA = 175
91105
MA = 175
90455
Ha = 219
998 n
mi
Hp = 212
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17895754
26 X = 5453730
09
Y = 5397563
96 feet Y = 1706169
99 meter
Z = -12093747
75 Z = -3659678
38
XDOT = -14177
746743 XDOT = -4351
409005
YDOT = 15093
953528 feet/sec YDOT = 4552
145015 meter/sec
ZDOT = -14245
594330 ZDOT = -4363
122487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8157149
96 X = 2486299
31
Y = -16899258
77 feet Y = -5150894
07 meter
Z = -11980250
81 Z = -3651580
45
XDOT = 11455
727140 XDOT = 3491
705632
YDOT = 15691
412587 feet/sec YDOT = 4782
742557 meter/sec
ZDOT = -14336
835886 ZDOT = -4369
867578
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 15151
56075227
00016717 00000-0 10270-3 0 9048
2 25544 51
6405 167
0548 0004499 5
2460 354
8739 15
55238494 25458
Satellite: ISS
Catalog Number: 25544
Epoch time: 15151
56075227 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 167
0548 deg
Eccentricity:
0004499
Arg of perigee: 5
2460 deg
Mean anomaly: 354
8739 deg
Mean motion: 15
55238494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2545
Checksum: 320
Coasting Arc #6 (Orbit 2560)
---------------------------------------
Vector Time (GMT): 2015/152/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3811508
64 A = 6776057
81 meter
Y = -2755619
83 meter E =
0006799
Z = 4871730
30 I = 51
73848
XDOT = 6036
228916 Wp = 81
83705
YDOT = -4079
569918 meter/sec RA = 161
08975 deg
ZDOT = 2413
102745 TA = 344
54705
MA = 344
56780
Ha = 220
167 n
mi
Hp = 212
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12504949
62 X = -3804076
79
Y = -9040747
46 feet Y = -2798201
55 meter
Z = 15983367
12 Z = 4853232
19
XDOT = 19803
900642 XDOT = 6069
676874
YDOT = -13384
415743 feet/sec YDOT = -4011
882089 meter/sec
ZDOT = 7917
003758 ZDOT = 2442
506878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10718961
45 X = -3267139
45
Y = 11212981
18 feet Y = 3417716
66 meter
Z = 15904396
32 Z = 4847660
00
XDOT = -9661
405948 XDOT = -2944
796533
YDOT = -20654
298282 feet/sec YDOT = -6295
430116 meter/sec
ZDOT = 8043
985938 ZDOT = 2451
806914
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 15152
58883910
00016717 00000-0 10270-3 0 9058
2 25544 51
6397 161
9203 0004613 8
3024 351
8205 15
55254357 25616
Satellite: ISS
Catalog Number: 25544
Epoch time: 15152
58883910 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 161
9203 deg
Eccentricity:
0004613
Arg of perigee: 8
3024 deg
Mean anomaly: 351
8205 deg
Mean motion: 15
55254357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2561
Checksum: 298
Coasting Arc #7 (Orbit 2575)
---------------------------------------
Vector Time (GMT): 2015/153/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1808599
55 A = 6774080
51 meter
Y = 3791084
53 meter E =
0016541
Z = -5328337
40 I = 51
76156
XDOT = -6968
071345 Wp = 73
48806
YDOT = 3176
574547 meter/sec RA = 156
08682 deg
ZDOT = -100
733571 TA = 195
52701
MA = 195
57781
Ha = 220
147 n
mi
Hp = 212
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5933725
57 X = 1791955
74
Y = 12437941
36 feet Y = 3811217
04 meter
Z = -17481421
92 Z = -5319591
43
XDOT = -22861
126461 XDOT = -7002
585343
YDOT = 10421
832504 feet/sec YDOT = 3098
460051 meter/sec
ZDOT = -330
490720 ZDOT = -134
667042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13086671
10 X = 3988817
35
Y = -4465386
30 feet Y = -1361049
74 meter
Z = -17444510
93 Z = -5317086
93
XDOT = 7198
489386 XDOT = 2194
099565
YDOT = 23014
754673 feet/sec YDOT = 7014
897224 meter/sec
ZDOT = -476
794444 ZDOT = -145
326947
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 15153
55266191
00016717 00000-0 10270-3 0 9063
2 25544 51
6396 157
1070 0004621 11
9540 348
1722 15
55257516 25765
Satellite: ISS
Catalog Number: 25544
Epoch time: 15153
55266191 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 157
1070 deg
Eccentricity:
0004621
Arg of perigee: 11
9540 deg
Mean anomaly: 348
1722 deg
Mean motion: 15
55257516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2576
Checksum: 302
Coasting Arc #8 (Orbit 2591)
---------------------------------------
Vector Time (GMT): 2015/154/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 330300
58 A = 6775571
77 meter
Y = -4623389
01 meter E =
0010325
Z = 4939057
00 I = 51
79536
XDOT = 7087
564052 Wp = 39
81099
YDOT = -1899
437572 meter/sec RA = 151
08452 deg
ZDOT = -2241
688918 TA = 72
07278
MA = 71
96024
Ha = 220
138 n
mi
Hp = 212
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1083663
33 X = 357983
54
Y = -15168599
13 feet Y = -4619541
22 meter
Z = 16204255
26 Z = 4940728
21
XDOT = 23253
162900 XDOT = 7119
166648
YDOT = -6231
750565 feet/sec YDOT = -1820
002812 meter/sec
ZDOT = -7354
622433 ZDOT = -2207
182025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14977166
96 X = -4565040
49
Y = -2585801
46 feet Y = -788152
29 meter
Z = 16212239
66 Z = 4941490
65
XDOT = -3911
364267 XDOT = -1192
183829
YDOT = -22737
415574 feet/sec YDOT = -6930
364267 meter/sec
ZDOT = -7206
052558 ZDOT = -2196
404820
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 15154
58073046
00016717 00000-0 10270-3 0 9073
2 25544 51
6393 151
9721 0004695 14
3027 345
8258 15
55290241 25923
Satellite: ISS
Catalog Number: 25544
Epoch time: 15154
58073046 = yrday
fracday
Element set: 907
Inclination: 51
6393 deg
RA of node: 151
9721 deg
Eccentricity:
0004695
Arg of perigee: 14
3027 deg
Mean anomaly: 345
8258 deg
Mean motion: 15
55290241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2592
Checksum: 310
Coasting Arc #9 (Orbit 2606)
---------------------------------------
Vector Time (GMT): 2015/155/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2272866
98 A = 6779785
27 meter
Y = 5132089
82 meter E =
0008089
Z = -3806745
05 I = 51
83706
XDOT = -6389
770339 Wp = 68
35550
YDOT = 295
412779 meter/sec RA = 146
09531 deg
ZDOT = 4223
460132 TA = 246
09218
MA = 246
17694
Ha = 220
263 n
mi
Hp = 212
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7456912
65 X = -2311594
45
Y = 16837565
03 feet Y = 5106457
09 meter
Z = -12489321
04 Z = -3817879
67
XDOT = -20963
813447 XDOT = -6413
114926
YDOT = 969
202031 feet/sec YDOT = 223
827116 meter/sec
ZDOT = 13856
496497 ZDOT = 4192
363003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16112288
13 X = 4911025
42
Y = 8847795
73 feet Y = 2696808
14 meter
Z = -12538060
62 Z = -3821600
88
XDOT = -263
426194 XDOT = -80
292304
YDOT = 19879
326255 feet/sec YDOT = 6059
218642 meter/sec
ZDOT = 13722
833984 ZDOT = 4182
719798
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 15155
54453681
00016717 00000-0 10270-3 0 9088
2 25544 51
6396 147
1589 0004791 18
5885 341
5443 15
55279268 26072
Satellite: ISS
Catalog Number: 25544
Epoch time: 15155
54453681 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 147
1589 deg
Eccentricity:
0004791
Arg of perigee: 18
5885 deg
Mean anomaly: 341
5443 deg
Mean motion: 15
55279268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2607
Checksum: 344
Coasting Arc #10 (Orbit 2622)
---------------------------------------
Vector Time (GMT): 2015/156/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3871418
97 A = 6784037
09 meter
Y = -5178297
90 meter E =
0014747
Z = 2040623
60 I = 51
87795
XDOT = 5036
107182 Wp = 91
96930
YDOT = 1555
975295 meter/sec RA = 141
12245 deg
ZDOT = -5571
737054 TA = 65
53653
MA = 65
38278
Ha = 220
249 n
mi
Hp = 211
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12701505
81 X = 3919123
59
Y = -16989166
34 feet Y = -5134738
69 meter
Z = 6694959
32 Z = 2059545
48
XDOT = 16522
661357 XDOT = 5045
399071
YDOT = 5104
905824 feet/sec YDOT = 1612
344986 meter/sec
ZDOT = -18279
977210 ZDOT = -5547
249798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16033944
24 X = -4887146
21
Y = -13847922
06 feet Y = -4220846
64 meter
Z = 6777181
55 Z = 2065684
94
XDOT = 5277
036739 XDOT = 1608
440798
YDOT = -15059
157503 feet/sec YDOT = -4590
031207 meter/sec
ZDOT = -18175
025186 ZDOT = -5539
747677
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 15156
57258729
00016717 00000-0 10270-3 0 9099
2 25544 51
6401 142
0240 0004850 20
8064 339
3286 15
55327583 26230
Satellite: ISS
Catalog Number: 25544
Epoch time: 15156
57258729 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 142
0240 deg
Eccentricity:
0004850
Arg of perigee: 20
8064 deg
Mean anomaly: 339
3286 deg
Mean motion: 15
55327583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2623
Checksum: 303
Coasting Arc #11 (Orbit 2637)
---------------------------------------
Vector Time (GMT): 2015/157/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4893896
63 A = 6785785
51 meter
Y = 4688243
78 meter E =
0016618
Z = 10032
74 I = 51
90827
XDOT = -3262
628137 Wp = 40
30523
YDOT = -3430
553348 meter/sec RA = 136
16301 deg
ZDOT = 6039
581167 TA = 319
80254
MA = 319
92533
Ha = 220
280 n
mi
Hp = 211
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16056091
32 X = -4946006
71
Y = 15381377
23 feet Y = 4633225
66 meter
Z = 32915
81 Z = -13866
89
XDOT = -10704
160556 XDOT = -3253
362387
YDOT = -11255
096287 feet/sec YDOT = -3466
987063 meter/sec
ZDOT = 19814
898841 ZDOT = 6023
754078
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14478971
50 X = 4413190
51
Y = 16874250
02 feet Y = 5143271
41 meter
Z = -70627
29 Z = -21527
20
XDOT = -10598
976251 XDOT = -3230
567961
YDOT = 9141
580068 feet/sec YDOT = 2786
353605 meter/sec
ZDOT = 19747
484932 ZDOT = 6019
033407
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 15157
53637657
00016717 00000-0 10270-3 0 9109
2 25544 51
6403 137
2111 0004730 26
0625 334
0765 15
55349110 26383
Satellite: ISS
Catalog Number: 25544
Epoch time: 15157
53637657 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 137
2111 deg
Eccentricity:
0004730
Arg of perigee: 26
0625 deg
Mean anomaly: 334
0765 deg
Mean motion: 15
55349110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2638
Checksum: 286
Coasting Arc #12 (Orbit 2653)
---------------------------------------
Vector Time (GMT): 2015/158/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5349117
82 A = 6783951
88 meter
Y = -3604073
33 meter E =
0006564
Z = -2106632
58 I = 51
92547
XDOT = 1280
228823 Wp = 95
55893
YDOT = 5132
461720 meter/sec RA = 131
20452 deg
ZDOT = -5545
439272 TA = 107
66921
MA = 107
59753
Ha = 220
369 n
mi
Hp = 211
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17549599
14 X = 5399255
08
Y = -11824387
57 feet Y = -3543975
46 meter
Z = -6911524
20 Z = -2080526
21
XDOT = 4200
225798 XDOT = 1249
678875
YDOT = 16838
785171 feet/sec YDOT = 5146
607794 meter/sec
ZDOT = -18193
698399 ZDOT = -5539
293890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11155482
66 X = -3400191
11
Y = -18025176
34 feet Y = -5494073
75 meter
Z = -6798673
62 Z = -2072235
72
XDOT = 15672
971498 XDOT = 4777
121712
YDOT = -2866
550184 feet/sec YDOT = -873
724496 meter/sec
ZDOT = -18168
195731 ZDOT = -5537
666059
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 15158
56440877
00016717 00000-0 10270-3 0 9110
2 25544 51
6414 132
0763 0004890 27
7292 332
4121 15
55350348 26547
Satellite: ISS
Catalog Number: 25544
Epoch time: 15158
56440877 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 132
0763 deg
Eccentricity:
0004890
Arg of perigee: 27
7292 deg
Mean anomaly: 332
4121 deg
Mean motion: 15
55350348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2654
Checksum: 301
Coasting Arc #13 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2015/159/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5202890
25 A = 6779513
38 meter
Y = 2015291
83 meter E =
0014034
Z = 3837054
76 I = 51
93153
XDOT = 620
236527 Wp = 79
71701
YDOT = -6400
922719 meter/sec RA = 126
23725 deg
ZDOT = 4192
365305 TA = 326
31676
MA = 326
40587
Ha = 220
425 n
mi
Hp = 211
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17069849
89 X = -5243677
99
Y = 6611849
85 feet Y = 1956881
35 meter
Z = 12588762
34 Z = 3811681
24
XDOT = 2034
896742 XDOT = 671
402158
YDOT = -21000
402622 feet/sec YDOT = -6393
701074 meter/sec
ZDOT = 13754
479346 ZDOT = 4195
502064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6262009
46 X = 1908660
48
Y = 17280821
19 feet Y = 5267194
30 meter
Z = 12479332
01 Z = 3803700
40
XDOT = -19694
911874 XDOT = -6003
009139
YDOT = -2831
724997 feet/sec YDOT = -863
109779 meter/sec
ZDOT = 13769
105476 ZDOT = 4196
823349
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 15159
59243012
00016717 00000-0 10270-3 0 9127
2 25544 51
6418 126
9426 0004713 31
2793 328
8640 15
55388900 26707
Satellite: ISS
Catalog Number: 25544
Epoch time: 15159
59243012 = yrday
fracday
Element set: 912
Inclination: 51
6418 deg
RA of node: 126
9426 deg
Eccentricity:
0004713
Arg of perigee: 31
2793 deg
Mean anomaly: 328
8640 deg
Mean motion: 15
55388900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 308
Coasting Arc #14 (Orbit 2684)
---------------------------------------
Vector Time (GMT): 2015/160/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597400
46 A = 6775286
60 meter
Y = -40754
29 meter E =
0016484
Z = -4991740
37 I = 51
93536
XDOT = -2273
327034 Wp = 63
41603
YDOT = 6989
437486 meter/sec RA = 121
25422 deg
ZDOT = -2149
097127 TA = 185
69146
MA = 185
71022
Ha = 220
416 n
mi
Hp = 211
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15083334
83 X = 4621762
54
Y = -133708
31 feet Y = 10793
40 meter
Z = -16377100
95 Z = -4969347
88
XDOT = -7458
422028 XDOT = -2340
876110
YDOT = 22931
225349 feet/sec YDOT = 6963
638111 meter/sec
ZDOT = -7050
843594 ZDOT = -2160
304133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -86834
84 X = -26467
26
Y = -15187538
76 feet Y = -4629161
81 meter
Z = -16280830
11 Z = -4962397
02
XDOT = 21799
330147 XDOT = 6644
435829
YDOT = 7492
791526 feet/sec YDOT = 2283
802857 meter/sec
ZDOT = -7100
277288 ZDOT = -2164
164517
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 15160
55619327
00016717 00000-0 10270-3 0 9132
2 25544 51
6418 122
1285 0004875 34
2905 325
8562 15
55374647 26854
Satellite: ISS
Catalog Number: 25544
Epoch time: 15160
55619327 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 122
1285 deg
Eccentricity:
0004875
Arg of perigee: 34
2905 deg
Mean anomaly: 325
8562 deg
Mean motion: 15
55374647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2685
Checksum: 320
Coasting Arc #15 (Orbit 2700)
---------------------------------------
Vector Time (GMT): 2015/161/12:52:19
110
Vector Time (MET): N/A
Weight (LBS) : 892082
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3623329
02 A = 6773646
77 meter
Y = -2080649
83 meter E =
0006867
Z = 5327012
97 I = 51
94625
XDOT = 3556
304274 Wp = 51
28397
YDOT = -6797
493972 meter/sec RA = 116
26298 deg
ZDOT = -231
682668 TA = 40
93877
MA = 40
88723
Ha = 220
525 n
mi
Hp = 211
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11887562
40 X = -3625670
17
Y = -6826278
98 feet Y = -2121181
71 meter
Z = 17477076
69 Z = 5309405
63
XDOT = 11667
664940 XDOT = 3633
176598
YDOT = -22301
489408 feet/sec YDOT = -6757
295217 meter/sec
ZDOT = -760
113741 ZDOT = -214
220465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6655821
48 X = -2028694
39
Y = 12092946
20 feet Y = 3685930
00 meter
Z = 17401756
42 Z = 5304055
36
XDOT = -21581
120882 XDOT = -6577
925645
YDOT = -10873
205236 feet/sec YDOT = -3314
152956 meter/sec
ZDOT = -683
808842 ZDOT = -208
424935
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 15161
58419588
00016717 00000-0 10270-3 0 9144
2 25544 51
6421 116
9946 0004861 36
9705 323
1782 15
55403608 27019
Satellite: ISS
Catalog Number: 25544
Epoch time: 15161
58419588 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 116
9946 deg
Eccentricity:
0004861
Arg of perigee: 36
9705 deg
Mean anomaly: 323
1782 deg
Mean motion: 15
55403608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2701
Checksum: 317
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