[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 8th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 966)
---------------------------------------
Vector Time (GMT): 2014/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4007988
68 A = 6789294
25 meter
Y = 2294929
51 meter E =
0016625
Z = -4991665
31 I = 51
79532
XDOT = -5473
934613 Wp = 73
74439
YDOT = 4893
082345 meter/sec RA = 151
51313 deg
ZDOT = -2147
025413 TA = 175
33639
MA = 175
32088
Ha = 228
108 n
mi
Hp = 218
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13149569
16 X = 4006276
44
Y = 7529296
29 feet Y = 2339740
15 meter
Z = -16376854
68 Z = -4972198
94
XDOT = -17959
103062 XDOT = -5517
813705
YDOT = 16053
419766 feet/sec YDOT = 4831
624080 meter/sec
ZDOT = -7044
046631 ZDOT = -2173
723482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10889627
04 X = 3319158
32
Y = -10663081
07 feet Y = -3250107
11 meter
Z = -16294709
75 Z = -4966627
53
XDOT = 9714
189571 XDOT = 2960
884981
YDOT = 20851
859691 feet/sec YDOT = 6355
646834 meter/sec
ZDOT = -7157
966283 ZDOT = -2181
748123
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 14157
51996451
00016717 00000-0 10270-3 0 9005
2 25544 51
6437 152
4740 0004257 71
4731 288
6882 15
50577585 9674
Satellite: ISS
Catalog Number: 25544
Epoch time: 14157
51996451 = yrday
fracday
Element set: 900
Inclination: 51
6437 deg
RA of node: 152
4740 deg
Eccentricity:
0004257
Arg of perigee: 71
4731 deg
Mean anomaly: 288
6882 deg
Mean motion: 15
50577585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 967
Checksum: 333
Coasting Arc #2 (Orbit 982)
---------------------------------------
Vector Time (GMT): 2014/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3711880
99 A = 6788530
96 meter
Y = -2398644
14 meter E =
0008248
Z = 5146344
00 I = 51
81922
XDOT = 5493
786301 Wp = 101
79413
YDOT = -5112
567771 meter/sec RA = 146
56271 deg
ZDOT = 1575
799405 TA = 333
02998
MA = 333
07283
Ha = 228
200 n
mi
Hp = 218
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12178087
23 X = -3709782
46
Y = -7869567
38 feet Y = -2440141
36 meter
Z = 16884330
71 Z = 5128316
97
XDOT = 18024
233270 XDOT = 5542
893082
YDOT = -16773
516309 feet/sec YDOT = -5050
858248 meter/sec
ZDOT = 5169
945556 ZDOT = 1602
606668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10782303
68 X = -3286446
16
Y = 9825454
95 feet Y = 2994798
67 meter
Z = 16808298
10 Z = 5123169
26
XDOT = -10821
795484 XDOT = -3298
483264
YDOT = -20936
901118 feet/sec YDOT = -6381
567461 meter/sec
ZDOT = 5284
377700 ZDOT = 1610
678323
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 14158
55114605
00016717 00000-0 10270-3 0 9014
2 25544 51
6431 147
3606 0004204 73
4171 286
7441 15
50588079 9832
Satellite: ISS
Catalog Number: 25544
Epoch time: 14158
55114605 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 147
3606 deg
Eccentricity:
0004204
Arg of perigee: 73
4171 deg
Mean anomaly: 286
7441 deg
Mean motion: 15
50588079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 983
Checksum: 300
Coasting Arc #3 (Orbit 997)
---------------------------------------
Vector Time (GMT): 2014/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3436035
87 A = 6788015
19 meter
Y = 2567738
85 meter E =
0018562
Z = -5277189
36 I = 51
84283
XDOT = -5442
386323 Wp = 81
39860
YDOT = 5285
782860 meter/sec RA = 141
61311 deg
ZDOT = -971
900153 TA = 179
30314
MA = 179
30055
Ha = 228
107 n
mi
Hp = 218
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11273083
58 X = 3432702
67
Y = 8424340
04 feet Y = 2606144
55 meter
Z = -17313613
39 Z = -5260505
29
XDOT = -17855
598172 XDOT = -5496
367419
YDOT = 17341
807284 feet/sec YDOT = 5224
620842 meter/sec
ZDOT = -3188
648797 ZDOT = -998
469574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10931102
23 X = 3331799
96
Y = -8999601
99 feet Y = -2743078
69 meter
Z = -17243297
12 Z = -5255756
96
XDOT = 11843
353314 XDOT = 3609
854090
YDOT = 20710
652868 feet/sec YDOT = 6312
606994 meter/sec
ZDOT = -3302
117341 ZDOT = -1006
485365
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 14159
51787281
00016717 00000-0 10270-3 0 9028
2 25544 51
6430 142
5666 0004258 77
0241 283
1385 15
50591268 9989
Satellite: ISS
Catalog Number: 25544
Epoch time: 14159
51787281 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 142
5666 deg
Eccentricity:
0004258
Arg of perigee: 77
0241 deg
Mean anomaly: 283
1385 deg
Mean motion: 15
50591268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 998
Checksum: 321
Coasting Arc #4 (Orbit 1013)
---------------------------------------
Vector Time (GMT): 2014/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3165738
48 A = 6787671
74 meter
Y = -2761509
09 meter E =
0006622
Z = 5325765
84 I = 51
86545
XDOT = 5372
388157 Wp = 90
24012
YDOT = -5459
689841 meter/sec RA = 136
66506 deg
ZDOT = 362
085189 TA = 356
31580
MA = 356
32067
Ha = 228
178 n
mi
Hp = 218
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10386281
10 X = -3160494
60
Y = -9060069
18 feet Y = -2796881
56 meter
Z = 17472985
03 Z = 5310399
40
XDOT = 17625
945398 XDOT = 5431
281442
YDOT = -17912
368245 feet/sec YDOT = -5399
283085 meter/sec
ZDOT = 1187
943535 ZDOT = 388
326443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11194023
91 X = -3411938
49
Y = 8179876
41 feet Y = 2493226
33 meter
Z = 17408283
80 Z = 5306044
90
XDOT = -12876
253814 XDOT = -3924
682162
YDOT = -20390
632893 feet/sec YDOT = -6215
064906 meter/sec
ZDOT = 1300
068162 ZDOT = 396
260776
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 14160
54904203
00016717 00000-0 10270-3 0 9039
2 25544 51
6427 137
4532 0004188 79
1309 281
0313 15
50605282 10140
Satellite: ISS
Catalog Number: 25544
Epoch time: 14160
54904203 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 137
4532 deg
Eccentricity:
0004188
Arg of perigee: 79
1309 deg
Mean anomaly: 281
0313 deg
Mean motion: 15
50605282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1014
Checksum: 273
Coasting Arc #5 (Orbit 1028)
---------------------------------------
Vector Time (GMT): 2014/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2937049
29 A = 6787644
65 meter
Y = 3007217
92 meter E =
0018992
Z = -5345793
31 I = 51
88766
XDOT = -5235
894516 Wp = 89
99440
YDOT = 5569
670233 meter/sec RA = 131
71786 deg
ZDOT = 257
279834 TA = 182
45119
MA = 182
46051
Ha = 228
077 n
mi
Hp = 218
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9635988
49 X = 2929172
14
Y = 9866200
54 feet Y = 3040018
44 meter
Z = -17538691
95 Z = -5331544
12
XDOT = -17178
131613 XDOT = -5299
036490
YDOT = 18273
196302 feet/sec YDOT = 5510
766021 meter/sec
ZDOT = 844
093942 ZDOT = 231
691456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11683305
95 X = 3561071
65
Y = -7469470
19 feet Y = -2276694
51 meter
Z = -17478766
54 Z = -5327528
04
XDOT = 13734
795450 XDOT = 4186
365653
YDOT = 19770
045982 feet/sec YDOT = 6025
910015 meter/sec
ZDOT = 734
697794 ZDOT = 223
935888
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 14161
51575695
00016717 00000-0 10270-3 0 9047
2 25544 51
6430 132
6590 0004216 82
5116 277
6513 15
50608921 10293
Satellite: ISS
Catalog Number: 25544
Epoch time: 14161
51575695 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 132
6590 deg
Eccentricity:
0004216
Arg of perigee: 82
5116 deg
Mean anomaly: 277
6513 deg
Mean motion: 15
50608921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1029
Checksum: 294
Coasting Arc #6 (Orbit 1044)
---------------------------------------
Vector Time (GMT): 2014/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2721795
59 A = 6787799
90 meter
Y = -3273179
35 meter E =
0007308
Z = 5281183
52 I = 51
90881
XDOT = 5094
623775 Wp = 74
29691
YDOT = -5663
013242 meter/sec RA = 126
77267 deg
ZDOT = -881
244042 TA = 24
11650
MA = 24
08230
Ha = 228
137 n
mi
Hp = 218
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8929775
56 X = -2710646
49
Y = -10738777
39 feet Y = -3303554
57 meter
Z = 17326717
60 Z = 5267987
90
XDOT = 16714
644930 XDOT = 5161
851087
YDOT = -18579
439769 feet/sec YDOT = -5605
665880 meter/sec
ZDOT = -2891
220611 ZDOT = -856
332196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12273518
56 X = -3740968
46
Y = 6807364
79 feet Y = 2074884
79 meter
Z = 17271302
82 Z = 5264293
10
XDOT = -14522
974308 XDOT = -4426
602569
YDOT = -19094
952427 feet/sec YDOT = -5820
141500 meter/sec
ZDOT = -2784
654490 ZDOT = -848
762689
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 14162
54691367
00016717 00000-0 10270-3 0 9057
2 25544 51
6434 127
5457 0004164 85
1786 274
9840 15
50625520 10451
Satellite: ISS
Catalog Number: 25544
Epoch time: 14162
54691367 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 127
5457 deg
Eccentricity:
0004164
Arg of perigee: 85
1786 deg
Mean anomaly: 274
9840 deg
Mean motion: 15
50625520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1045
Checksum: 312
Coasting Arc #7 (Orbit 1059)
---------------------------------------
Vector Time (GMT): 2014/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2565318
79 A = 6788268
86 meter
Y = 3571471
35 meter E =
0017794
Z = -5187251
14 I = 51
92895
XDOT = -4900
305429 Wp = 98
35216
YDOT = 5681
380961 meter/sec RA = 121
82862 deg
ZDOT = 1490
129967 TA = 185
96407
MA = 185
98528
Ha = 228
022 n
mi
Hp = 218
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8416400
23 X = 2550389
36
Y = 11717425
69 feet Y = 3600075
69 meter
Z = -17018540
48 Z = -5174824
79
XDOT = -16077
117549 XDOT = -4970
710361
YDOT = 18639
701316 feet/sec YDOT = 5626
188721 meter/sec
ZDOT = 4888
877845 ZDOT = 1466
154569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13027870
51 X = 3970894
93
Y = -6338703
93 feet Y = -1932036
96 meter
Z = -16966437
46 Z = -5171370
14
XDOT = 15067
775567 XDOT = 4592
657993
YDOT = 18173
907449 feet/sec YDOT = 5539
406990 meter/sec
ZDOT = 4786
256206 ZDOT = 1458
850892
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 14163
51361664
00016717 00000-0 10270-3 0 9060
2 25544 51
6440 122
7516 0004135 88
1864 271
9761 15
50630106 10601
Satellite: ISS
Catalog Number: 25544
Epoch time: 14163
51361664 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 122
7516 deg
Eccentricity:
0004135
Arg of perigee: 88
1864 deg
Mean anomaly: 271
9761 deg
Mean motion: 15
50630106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1060
Checksum: 285
Coasting Arc #8 (Orbit 1075)
---------------------------------------
Vector Time (GMT): 2014/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2426308
56 A = 6788917
19 meter
Y = -3881169
89 meter E =
0009747
Z = 5006960
90 I = 51
94787
XDOT = 4717
928650 Wp = 70
84489
YDOT = -5668
205484 meter/sec RA = 116
88682 deg
ZDOT = -2101
045741 TA = 39
55263
MA = 39
48155
Ha = 228
073 n
mi
Hp = 218
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7960329
93 X = -2407050
42
Y = -12733497
01 feet Y = -3908195
53 meter
Z = 16427037
09 Z = 4995220
36
XDOT = 15478
768536 XDOT = 4791
167415
YDOT = -18596
474685 feet/sec YDOT = -5615
036747 meter/sec
ZDOT = -6893
194687 ZDOT = -2077
949587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13847482
81 X = -4220712
76
Y = 5947111
66 feet Y = 1812679
63 meter
Z = 16377894
52 Z = 4991982
25
XDOT = -15473
167563 XDOT = -4716
221473
YDOT = -17258
983733 feet/sec YDOT = -5260
538242 meter/sec
ZDOT = -6794
281942 ZDOT = -2070
897136
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 14164
54476076
00016717 00000-0 10270-3 0 9079
2 25544 51
6449 117
6386 0004113 91
4447 268
7175 15
50648601 10767
Satellite: ISS
Catalog Number: 25544
Epoch time: 14164
54476076 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 117
6386 deg
Eccentricity:
0004113
Arg of perigee: 91
4447 deg
Mean anomaly: 268
7175 deg
Mean motion: 15
50648601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1076
Checksum: 320
Coasting Arc #9 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2014/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2356744
44 A = 6789806
97 meter
Y = 4199676
27 meter E =
0015182
Z = -4800758
79 I = 51
96463
XDOT = -4502
097126 Wp = 104
94645
YDOT = 5578
305946 meter/sec RA = 111
94631 deg
ZDOT = 2672
989997 TA = 191
36948
MA = 191
40381
Ha = 227
956 n
mi
Hp = 218
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7732101
18 X = 2332928
07
Y = 13778465
44 feet Y = 4225898
46 meter
Z = -15750520
96 Z = -4789367
27
XDOT = -14770
659862 XDOT = -4577
124920
YDOT = 18301
528694 feet/sec YDOT = 5527
540693 meter/sec
ZDOT = 8769
652221 ZDOT = 2650
938067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14744863
06 X = 4494234
26
Y = -5806716
82 feet Y = -1769887
29 meter
Z = -15702912
53 Z = -4786247
74
XDOT = 15601
807476 XDOT = 4755
430919
YDOT = 16186
257832 feet/sec YDOT = 4933
571387 meter/sec
ZDOT = 8675
164293 ZDOT = 2644
190076
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 14165
51145195
00016717 00000-0 10270-3 0 9083
2 25544 51
6454 112
8448 0004055 94
2792 265
8822 15
50653700 10918
Satellite: ISS
Catalog Number: 25544
Epoch time: 14165
51145195 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 112
8448 deg
Eccentricity:
0004055
Arg of perigee: 94
2792 deg
Mean anomaly: 265
8822 deg
Mean motion: 15
50653700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 305
Coasting Arc #10 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2014/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2303454
35 A = 6790855
05 meter
Y = -4517730
90 meter E =
0012672
Z = 4507467
89 I = 51
97991
XDOT = 4316
571819 Wp = 77
49073
YDOT = -5445
924720 meter/sec RA = 107
00793 deg
ZDOT = -3242
087581 TA = 45
01850
MA = 44
91586
Ha = 227
996 n
mi
Hp = 218
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7557264
93 X = -2274660
57
Y = -14821951
76 feet Y = -4543329
24 meter
Z = 14788280
47 Z = 4496347
39
XDOT = 14161
981033 XDOT = 4392
897510
YDOT = -17867
207088 feet/sec YDOT = -5397
226829 meter/sec
ZDOT = -10636
770280 ZDOT = -3220
933753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15655837
08 X = -4771899
14
Y = 5750444
23 feet Y = 1752735
40 meter
Z = 14741875
83 Z = 4493323
75
XDOT = -15543
786278 XDOT = -4737
746057
YDOT = -15195
384755 feet/sec YDOT = -4631
553273 meter/sec
ZDOT = -10546
098603 ZDOT = -3214
450854
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 14166
54258331
00016717 00000-0 10270-3 0 9095
2 25544 51
6462 107
7319 0004056 97
8643 262
2969 15
50671833 11070
Satellite: ISS
Catalog Number: 25544
Epoch time: 14166
54258331 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 107
7319 deg
Eccentricity:
0004056
Arg of perigee: 97
8643 deg
Mean anomaly: 262
2969 deg
Mean motion: 15
50671833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 319
Coasting Arc #11 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2014/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2322388
99 A = 6792009
85 meter
Y = 4820175
05 meter E =
0011736
Z = -4195762
53 I = 51
99207
XDOT = -4119
659900 Wp = 106
69112
YDOT = 5245
501794 meter/sec RA = 102
07063 deg
ZDOT = 3751
271420 TA = 201
75741
MA = 201
80730
Ha = 227
891 n
mi
Hp = 218
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7619386
46 X = 2288697
61
Y = 15814222
62 feet Y = 4845957
62 meter
Z = -13765625
09 Z = -4184562
02
XDOT = -13515
944553 XDOT = -4196
232452
YDOT = 17209
651555 feet/sec YDOT = 5199
004518 meter/sec
ZDOT = 12307
320932 ZDOT = 3731
073473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16547228
29 X = 5043595
18
Y = -5968016
60 feet Y = -1819051
46 meter
Z = -13718933
45 Z = -4181530
91
XDOT = 15221
003909 XDOT = 4639
361991
YDOT = 14151
101447 feet/sec YDOT = 4313
255721 meter/sec
ZDOT = 12220
726107 ZDOT = 3724
877317
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 14167
50926267
00016717 00000-0 10270-3 0 9104
2 25544 51
6462 102
9381 0004007 100
8525 259
3077 15
50678483 11228
Satellite: ISS
Catalog Number: 25544
Epoch time: 14167
50926267 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 102
9381 deg
Eccentricity:
0004007
Arg of perigee: 100
8525 deg
Mean anomaly: 259
3077 deg
Mean motion: 15
50678483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 296
Coasting Arc #12 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2014/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2350454
92 A = 6793288
14 meter
Y = -5109123
53 meter E =
0015324
Z = 3797733
39 I = 52
00245
XDOT = 3971
290477 Wp = 88
69240
YDOT = -4997
047792 meter/sec RA = 97
13509 deg
ZDOT = -4249
597789 TA = 46
05911
MA = 45
93277
Ha = 227
921 n
mi
Hp = 218
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7711466
28 X = -2311596
89
Y = -16762216
30 feet Y = -5135190
94 meter
Z = 12459755
23 Z = 3786409
16
XDOT = 13029
168233 XDOT = 4047
516484
YDOT = -16394
513753 feet/sec YDOT = -4952
211641 meter/sec
ZDOT = -13942
249963 ZDOT = -4230
121303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17393935
51 X = -5301671
54
Y = 6250016
85 feet Y = 1905005
14 meter
Z = 12412590
56 Z = 3783357
60
XDOT = -14693
475915 XDOT = -4478
571459
YDOT = -13269
888705 feet/sec YDOT = -4044
662077 meter/sec
ZDOT = -13858
748617 ZDOT = -4224
146578
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 14168
54038107
00016717 00000-0 10270-3 0 9117
2 25544 51
6466 97
8249 0004016 104
4501 255
7096 15
50691488 11389
Satellite: ISS
Catalog Number: 25544
Epoch time: 14168
54038107 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 97
8249 deg
Eccentricity:
0004016
Arg of perigee: 104
4501 deg
Mean anomaly: 255
7096 deg
Mean motion: 15
50691488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 310
Coasting Arc #13 (Orbit 1152)
---------------------------------------
Vector Time (GMT): 2014/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2445505
48 A = 6794491
36 meter
Y = 5360410
54 meter E =
0008638
Z = -3392381
49 I = 52
00951
XDOT = -3832
049398 Wp = 97
00808
YDOT = 4699
068079 meter/sec RA = 92
20038 deg
ZDOT = 4671
856874 TA = 223
71098
MA = 223
77941
Ha = 227
821 n
mi
Hp = 218
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8023311
94 X = 2401861
41
Y = 17586648
74 feet Y = 5387514
01 meter
Z = -11129860
53 Z = -3380607
18
XDOT = -12572
340546 XDOT = -3907
004910
YDOT = 15416
890023 feet/sec YDOT = 4655
796144 meter/sec
ZDOT = 15327
614416 ZDOT = 4653
059741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18128316
12 X = 5525510
75
Y = -6790936
20 feet Y = -2069877
35 meter
Z = -11080834
09 Z = -3377438
23
XDOT = 13959
592519 XDOT = 4254
883800
YDOT = 12435
486604 feet/sec YDOT = 3790
336317 meter/sec
ZDOT = 15247
038242 ZDOT = 4647
297256
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 14169
50704832
00016717 00000-0 10270-3 0 9120
2 25544 51
6465 93
0307 0003977 107
7024 252
4561 15
50703207 11533
Satellite: ISS
Catalog Number: 25544
Epoch time: 14169
50704832 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 93
0307 deg
Eccentricity:
0003977
Arg of perigee: 107
7024 deg
Mean anomaly: 252
4561 deg
Mean motion: 15
50703207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1153
Checksum: 287
Coasting Arc #14 (Orbit 1168)
---------------------------------------
Vector Time (GMT): 2014/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2536726
13 A = 6795777
82 meter
Y = -5586097
58 meter E =
0017198
Z = 2903755
64 I = 52
01430
XDOT = 3757
125892 Wp = 101
58653
YDOT = -4353
978012 meter/sec RA = 87
26710 deg
ZDOT = -5071
754727 TA = 45
54001
MA = 45
39947
Ha = 227
849 n
mi
Hp = 218
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8322592
30 X = -2488178
07
Y = -18327091
80 feet Y = -5614193
66 meter
Z = 9526757
36 Z = 2891550
09
XDOT = 12326
528516 XDOT = 3830
170743
YDOT = -14284
704765 feet/sec YDOT = -4311
554602 meter/sec
ZDOT = -16639
615245 ZDOT = -5053
326082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18764353
85 X = -5719375
05
Y = 7349311
98 feet Y = 2240070
29 meter
Z = 9475947
44 Z = 2888268
78
XDOT = -13036
288908 XDOT = -3973
460859
YDOT = -11838
223872 feet/sec YDOT = -3608
290636 meter/sec
ZDOT = -16560
654352 ZDOT = -5047
687446
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 14170
53815375
00016717 00000-0 10270-3 0 9131
2 25544 51
6467 87
9170 0003994 111
2779 248
8791 15
50704961 11690
Satellite: ISS
Catalog Number: 25544
Epoch time: 14170
53815375 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 87
9170 deg
Eccentricity:
0003994
Arg of perigee: 111
2779 deg
Mean anomaly: 248
8791 deg
Mean motion: 15
50704961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1169
Checksum: 335
Coasting Arc #15 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2014/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900140
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2682826
01 A = 6796789
76 meter
Y = 5757480
06 meter E =
0007939
Z = -2421579
72 I = 52
01596
XDOT = -3706
779484 Wp = 74
04125
YDOT = 3985
368448 meter/sec RA = 82
33446 deg
ZDOT = 5385
582556 TA = 259
08902
MA = 259
17837
Ha = 227
736 n
mi
Hp = 218
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8801922
59 X = 2630008
44
Y = 18889370
26 feet Y = 5787186
02 meter
Z = -7944815
35 Z = -2408674
72
XDOT = -12161
350013 XDOT = -3777
230764
YDOT = 13075
355802 feet/sec YDOT = 3943
522504 meter/sec
ZDOT = 17669
234109 ZDOT = 5367
404708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19215219
13 X = 5856798
79
Y = -8118404
83 feet Y = -2474489
79 meter
Z = -7891077
11 Z = -2405200
30
XDOT = 12003
111628 XDOT = 3658
548424
YDOT = 11364
819078 feet/sec YDOT = 3463
996855 meter/sec
ZDOT = 17591
393796 ZDOT = 5361
856829
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 14171
50480890
00016717 00000-0 10270-3 0 9140
2 25544 51
6471 83
1228 0003929 114
5698 245
5863 15
50726404 11848
Satellite: ISS
Catalog Number: 25544
Epoch time: 14171
50480890 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 83
1228 deg
Eccentricity:
0003929
Arg of perigee: 114
5698 deg
Mean anomaly: 245
5863 deg
Mean motion: 15
50726404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1184
Checksum: 312
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