[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 8th 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) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
There are no maneuvers
Coasting Arc #1 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2016/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5543685
02 A = 6780847
38 meter
Y = 820471
74 meter E =
0007750
Z = -3825092
23 I = 51
78653
XDOT = -3668
711858 Wp = 82
66406
YDOT = 5258
220109 meter/sec RA = 155
91338 deg
ZDOT = -4195
486353 TA = 143
18489
MA = 143
13165
Ha = 220
401 n
mi
Hp = 212
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18187942
97 X = 5552678
72
Y = 2691836
42 feet Y = 882515
12 meter
Z = -12549515
18 Z = -3798140
88
XDOT = -12036
456228 XDOT = -3706
858303
YDOT = 17251
378310 feet/sec YDOT = 5216
980717 meter/sec
ZDOT = -13764
719005 ZDOT = -4213
400630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11417918
80 X = -3480181
65
Y = -14512588
50 feet Y = -4423436
98 meter
Z = -12431954
36 Z = -3789259
69
XDOT = 19476
683238 XDOT = 5936
493051
YDOT = -3482
349471 feet/sec YDOT = -1061
420119 meter/sec
ZDOT = -13843
788109 ZDOT = -4219
586616
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 16221
52406418
00016717 00000-0 10270-3 0 9009
2 25544 51
6412 156
8898 0001851 100
7293 259
4068 15
54952217 13125
Satellite: ISS
Catalog Number: 25544
Epoch time: 16221
52406418 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 156
8898 deg
Eccentricity:
0001851
Arg of perigee: 100
7293 deg
Mean anomaly: 259
4068 deg
Mean motion: 15
54952217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 298
Coasting Arc #2 (Orbit 1327)
---------------------------------------
Vector Time (GMT): 2016/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4169209
62 A = 6776723
30 meter
Y = -2100222
63 meter E =
0008466
Z = 4907472
38 I = 51
80221
XDOT = 5293
199134 Wp = 119
63402
YDOT = -5042
235381 meter/sec RA = 150
92746 deg
ZDOT = 2331
910586 TA = 307
57838
MA = 307
65523
Ha = 220
359 n
mi
Hp = 212
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13678509
24 X = -4169252
70
Y = -6890494
19 feet Y = -2146845
66 meter
Z = 16100631
17 Z = 4887219
53
XDOT = 17366
138892 XDOT = 5337
861972
YDOT = -16542
766999 feet/sec YDOT = -4982
793517 meter/sec
ZDOT = 7650
625282 ZDOT = 2357
731968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5521870
12 X = 1683066
01
Y = 14384680
08 feet Y = 4384450
49 meter
Z = 16012519
43 Z = 4880615
92
XDOT = -22893
126079 XDOT = -6977
824829
YDOT = 119
101933 feet/sec YDOT = 36
302269 meter/sec
ZDOT = 7764
204168 ZDOT = 2366
529431
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 16222
55235530
00016717 00000-0 10270-3 0 9019
2 25544 51
6413 151
7586 0001659 111
9653 248
1677 15
54980985 13285
Satellite: ISS
Catalog Number: 25544
Epoch time: 16222
55235530 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 151
7586 deg
Eccentricity:
0001659
Arg of perigee: 111
9653 deg
Mean anomaly: 248
1677 deg
Mean motion: 15
54980985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1328
Checksum: 318
Coasting Arc #3 (Orbit 1342)
---------------------------------------
Vector Time (GMT): 2016/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2465269
18 A = 6774937
83 meter
Y = 3395120
16 meter E =
0016516
Z = -5333573
13 I = 51
82452
XDOT = -6287
076683 Wp = 91
19968
YDOT = 4370
103494 meter/sec RA = 145
93166 deg
ZDOT = -124
848039 TA = 177
61591
MA = 177
60803
Ha = 220
297 n
mi
Hp = 212
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8088153
48 X = 2453028
86
Y = 11138845
68 feet Y = 3422619
95 meter
Z = -17498599
50 Z = -5321627
33
XDOT = -20626
892005 XDOT = -6334
870565
YDOT = 14337
609888 feet/sec YDOT = 4299
529966 meter/sec
ZDOT = -409
606426 ZDOT = -155
504974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1226934
88 X = 373969
75
Y = -13776459
77 feet Y = -4199064
94 meter
Z = -17446973
41 Z = -5317837
50
XDOT = 23944
326576 XDOT = 7298
230741
YDOT = 2818
904034 feet/sec YDOT = 859
201950 meter/sec
ZDOT = -544
213754 ZDOT = -165
876352
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 16223
51637445
00016717 00000-0 10270-3 0 9028
2 25544 51
6420 146
9465 0001743 109
0304 251
1038 15
54963261 13430
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
51637445 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 146
9465 deg
Eccentricity:
0001743
Arg of perigee: 109
0304 deg
Mean anomaly: 251
1038 deg
Mean motion: 15
54963261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1343
Checksum: 282
Coasting Arc #4 (Orbit 1358)
---------------------------------------
Vector Time (GMT): 2016/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -636158
05 A = 6776276
69 meter
Y = -4532747
12 meter E =
0007193
Z = 4991851
97 I = 51
85509
XDOT = 6625
634446 Wp = 68
08669
YDOT = -3250
674158 meter/sec RA = 140
93885 deg
ZDOT = -2102
300639 TA = 42
32761
MA = 42
27213
Ha = 220
294 n
mi
Hp = 212
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2087132
72 X = -609672
52
Y = -14871217
57 feet Y = -4539712
96 meter
Z = 16377467
10 Z = 4988826
03
XDOT = 21737
645820 XDOT = 6671
703866
YDOT = -10664
941462 feet/sec YDOT = -3176
324297 meter/sec
ZDOT = -6897
311808 ZDOT = -2070
003320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7982998
63 X = -2433217
98
Y = 12735365
81 feet Y = 3881739
50 meter
Z = 16364988
67 Z = 4988048
55
XDOT = -22564
157434 XDOT = -6877
555186
YDOT = -5441
684060 feet/sec YDOT = -1658
625301 meter/sec
ZDOT = -6755
701893 ZDOT = -2059
137937
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 16224
54465331
00016717 00000-0 10270-3 0 9036
2 25544 51
6416 141
8153 0001710 110
6256 249
5081 15
54978522 13593
Satellite: ISS
Catalog Number: 25544
Epoch time: 16224
54465331 = yrday
fracday
Element set: 903
Inclination: 51
6416 deg
RA of node: 141
8153 deg
Eccentricity:
0001710
Arg of perigee: 110
6256 deg
Mean anomaly: 249
5081 deg
Mean motion: 15
54978522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1359
Checksum: 293
Coasting Arc #5 (Orbit 1373)
---------------------------------------
Vector Time (GMT): 2016/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1091509
95 A = 6780110
67 meter
Y = 5391087
05 meter E =
0008531
Z = -3973319
33 I = 51
89316
XDOT = -6293
462560 Wp = 109
59006
YDOT = 1691
631356 meter/sec RA = 135
95511 deg
ZDOT = 4028
361643 TA = 202
32153
MA = 202
35869
Ha = 220
216 n
mi
Hp = 212
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3581069
40 X = -1132412
83
Y = 17687293
48 feet Y = 5378652
40 meter
Z = -13035824
56 Z = -3978720
86
XDOT = -20647
843043 XDOT = -6331
478937
YDOT = 5549
971639 feet/sec YDOT = 1621
041049 meter/sec
ZDOT = 13216
409591 ZDOT = 3997
697530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13944868
63 X = 4250395
96
Y = -11426553
02 feet Y = -3482813
36 meter
Z = -13060308
41 Z = -3980782
00
XDOT = 18698
075432 XDOT = 5699
173392
YDOT = 7882
208884 feet/sec YDOT = 2402
497268 meter/sec
ZDOT = 13082
171048 ZDOT = 3987
445735
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 16225
50865923
00016717 00000-0 10270-3 0 9045
2 25544 51
6423 137
0035 0001713 117
1570 242
9758 15
54989332 13747
Satellite: ISS
Catalog Number: 25544
Epoch time: 16225
50865923 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 137
0035 deg
Eccentricity:
0001713
Arg of perigee: 117
1570 deg
Mean anomaly: 242
9758 deg
Mean motion: 15
54989332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1374
Checksum: 306
Coasting Arc #6 (Orbit 1389)
---------------------------------------
Vector Time (GMT): 2016/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2588554
53 A = 6784463
95 meter
Y = -5800513
55 meter E =
0015437
Z = 2362696
33 I = 51
93059
XDOT = 5434
243896 Wp = 108
43086
YDOT = 210
271888 meter/sec RA = 130
98757 deg
ZDOT = -5413
377786 TA = 45
28408
MA = 45
15848
Ha = 220
207 n
mi
Hp = 212
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8492632
98 X = 2641748
12
Y = -19030556
27 feet Y = -5771269
22 meter
Z = 7751628
40 Z = 2375399
84
XDOT = 17828
884173 XDOT = 5457
784264
YDOT = 689
868399 feet/sec YDOT = 271
172953 meter/sec
ZDOT = -17760
425806 ZDOT = -5386
922702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18453260
40 X = -5624553
77
Y = 9637711
97 feet Y = 2937574
61 meter
Z = 7808093
10 Z = 2379906
78
XDOT = -12911
517121 XDOT = -3935
430419
YDOT = -10362
769899 feet/sec YDOT = -3158
572265 meter/sec
ZDOT = -17644
875011 ZDOT = -5378
157903
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 16226
53692488
00016717 00000-0 10270-3 0 9054
2 25544 51
6428 131
8716 0001702 122
5224 237
6094 15
54976476 13901
Satellite: ISS
Catalog Number: 25544
Epoch time: 16226
53692488 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 131
8716 deg
Eccentricity:
0001702
Arg of perigee: 122
5224 deg
Mean anomaly: 237
6094 deg
Mean motion: 15
54976476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1390
Checksum: 319
Coasting Arc #7 (Orbit 1404)
---------------------------------------
Vector Time (GMT): 2016/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3690898
88 A = 6786692
35 meter
Y = 5672142
95 meter E =
0011468
Z = -449547
22 I = 51
95942
XDOT = -4183
809116 Wp = 49
83689
YDOT = -2253
981440 meter/sec RA = 126
03167 deg
ZDOT = 6018
808600 TA = 305
33529
MA = 305
44244
Ha = 220
129 n
mi
Hp = 212
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12109248
28 X = -3751868
22
Y = 18609392
89 feet Y = 5630527
96 meter
Z = -1474892
46 Z = -467624
41
XDOT = -13726
407861 XDOT = -4187
529945
YDOT = -7394
952232 feet/sec YDOT = -2300
788507 meter/sec
ZDOT = 19746
747376 ZDOT = 5998
475909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20929485
08 X = 6379307
05
Y = -7393095
69 feet Y = -2253415
56 meter
Z = -1554829
87 Z = -473912
14
XDOT = 5947
776725 XDOT = 1812
882346
YDOT = 12774
357357 feet/sec YDOT = 3893
624122 meter/sec
ZDOT = 19658
277697 ZDOT = 5991
843042
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 16227
50091589
00016717 00000-0 10270-3 0 9068
2 25544 51
6436 127
0600 0001586 122
2838 237
8469 15
55002172 14056
Satellite: ISS
Catalog Number: 25544
Epoch time: 16227
50091589 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 127
0600 deg
Eccentricity:
0001586
Arg of perigee: 122
2838 deg
Mean anomaly: 237
8469 deg
Mean motion: 15
55002172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1405
Checksum: 298
Coasting Arc #8 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2016/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4398356
22 A = 6785835
69 meter
Y = -4917870
81 meter E =
0009759
Z = -1570436
64 I = 51
97468
XDOT = 2707
251910 Wp = 141
09569
YDOT = 4256
939422 meter/sec RA = 121
08096 deg
ZDOT = -5775
255175 TA = 55
99884
MA = 55
90618
Ha = 220
162 n
mi
Hp = 212
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14430302
57 X = 4460650
58
Y = -16134746
74 feet Y = -4868337
12 meter
Z = -5152351
18 Z = -1548919
64
XDOT = 8882
060073 XDOT = 2687
501747
YDOT = 13966
336686 feet/sec YDOT = 4287
103354 meter/sec
ZDOT = -18947
687581 ZDOT = -5762
152173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21226140
99 X = -6469727
77
Y = 4356960
13 feet Y = 1328001
45 meter
Z = -5057493
90 Z = -1541524
14
XDOT = 1394
042079 XDOT = 424
904026
YDOT = -15033
199605 feet/sec YDOT = -4582
119239 meter/sec
ZDOT = -18891
141802 ZDOT = -5758
020021
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 16228
52916794
00016717 00000-0 10270-3 0 9076
2 25544 51
6438 121
9286 0001614 133
3979 226
7309 15
54982634 14219
Satellite: ISS
Catalog Number: 25544
Epoch time: 16228
52916794 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 121
9286 deg
Eccentricity:
0001614
Arg of perigee: 133
3979 deg
Mean anomaly: 226
7309 deg
Mean motion: 15
54982634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 329
Coasting Arc #9 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2016/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4670410
09 A = 6782136
76 meter
Y = 3606045
11 meter E =
0013778
Z = 3332584
28 I = 51
97892
XDOT = -1200
205485 Wp = 92
41145
YDOT = -5930
460286 meter/sec RA = 116
12209 deg
ZDOT = 4717
752391 TA = 306
21603
MA = 306
34332
Ha = 220
132 n
mi
Hp = 212
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15322867
75 X = -4726574
62
Y = 11830856
68 feet Y = 3553503
45 meter
Z = 10933675
47 Z = 3309760
62
XDOT = -3937
682039 XDOT = -1156
716731
YDOT = -19456
890701 feet/sec YDOT = -5943
638600 meter/sec
ZDOT = 15478
190259 ZDOT = 4712
027868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19403158
69 X = 5914082
77
Y = -679272
05 feet Y = -207042
12 meter
Z = 10833315
63 Z = 3301994
60
XDOT = -8073
684104 XDOT = -2460
858915
YDOT = 16762
883585 feet/sec YDOT = 5109
326917 meter/sec
ZDOT = 15454
173307 ZDOT = 4710
432024
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 16229
55741219
00016717 00000-0 10270-3 0 9089
2 25544 51
6443 116
7961 0001471 129
7532 230
3751 15
55011131 14377
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
55741219 = yrday
fracday
Element set: 908
Inclination: 51
6443 deg
RA of node: 116
7961 deg
Eccentricity:
0001471
Arg of perigee: 129
7532 deg
Mean anomaly: 230
3751 deg
Mean motion: 15
55011131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 290
Coasting Arc #10 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2016/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4597620
31 A = 6777601
28 meter
Y = -1795624
31 meter E =
0010983
Z = -4655157
25 I = 51
97729
XDOT = -243
617600 Wp = 76
66934
YDOT = 7058
778797 meter/sec RA = 111
15103 deg
ZDOT = -2966
778727 TA = 163
90211
MA = 163
86719
Ha = 219
961 n
mi
Hp = 212
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15084056
13 X = 4639970
00
Y = -5891155
88 feet Y = -1743973
98 meter
Z = -15272825
62 Z = -4632720
73
XDOT = -799
270341 XDOT = -308
121517
YDOT = 23158
723088 feet/sec YDOT = 7055
693762 meter/sec
ZDOT = -9733
526008 ZDOT = -2968
118987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15846134
55 X = -4829901
81
Y = -3758938
67 feet Y = -1145724
51 meter
Z = -15174454
50 Z = -4625173
73
XDOT = 13467
920604 XDOT = 4105
022200
YDOT = -17498
826140 feet/sec YDOT = -5333
642208 meter/sec
ZDOT = -9740
582548 ZDOT = -2968
929561
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 16230
52138312
00016717 00000-0 10270-3 0 9093
2 25544 51
6441 111
9848 0001360 134
1394 225
9871 15
55045546 14526
Satellite: ISS
Catalog Number: 25544
Epoch time: 16230
52138312 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 111
9848 deg
Eccentricity:
0001360
Arg of perigee: 134
1394 deg
Mean anomaly: 225
9871 deg
Mean motion: 15
55045546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 293
Coasting Arc #11 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2016/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223293
90 A = 6774901
07 meter
Y = -279203
01 meter E =
0004674
Z = 5287138
07 I = 51
97826
XDOT = 1510
397579 Wp = 125
47836
YDOT = -7479
322175 meter/sec RA = 106
16855 deg
ZDOT = 808
374650 TA = 316
81787
MA = 316
85451
Ha = 220
104 n
mi
Hp = 212
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13855951
13 X = -4245540
01
Y = -916020
36 feet Y = -326554
84 meter
Z = 17346253
50 Z = 5266568
77
XDOT = 4955
372635 XDOT = 1589
994344
YDOT = -24538
458578 feet/sec YDOT = -7461
986809 meter/sec
ZDOT = 2652
147802 ZDOT = 815
905304
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11132316
99 X = 3393130
22
Y = 8485721
90 feet Y = 2586448
04 meter
Z = 17256390
93 Z = 5259747
95
XDOT = -17064
571479 XDOT = -5201
281387
YDOT = 16902
842606 feet/sec YDOT = 5151
986426 meter/sec
ZDOT = 2686
341092 ZDOT = 818
796765
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 16231
54961509
00016717 00000-0 10270-3 0 9100
2 25544 51
6433 106
8525 0001469 138
7704 221
3561 15
55044385 14680
Satellite: ISS
Catalog Number: 25544
Epoch time: 16231
54961509 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 106
8525 deg
Eccentricity:
0001469
Arg of perigee: 138
7704 deg
Mean anomaly: 221
3561 deg
Mean motion: 15
55044385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 304
Coasting Arc #12 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2016/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3653020
87 A = 6775335
41 meter
Y = 2413571
72 meter E =
0014740
Z = -5183695
62 I = 51
98773
XDOT = -2571
646104 Wp = 104
67978
YDOT = 7061
678351 meter/sec RA = 101
18226 deg
ZDOT = 1475
566501 TA = 179
47518
MA = 179
47363
Ha = 219
833 n
mi
Hp = 213
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11984976
62 X = 3650939
90
Y = 7918542
39 feet Y = 2454410
28 meter
Z = -17006875
40 Z = -5165955
70
XDOT = -8437
159133 XDOT = -2657
587985
YDOT = 23168
236059 feet/sec YDOT = 7032
440048 meter/sec
ZDOT = 4841
097445 ZDOT = 1462
865132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5927085
64 X = -1806575
70
Y = -13184468
90 feet Y = -4018626
12 meter
Z = -16929743
79 Z = -5160185
91
XDOT = 18651
496673 XDOT = 5684
976186
YDOT = -14528
810553 feet/sec YDOT = -4428
381456 meter/sec
ZDOT = 4784
364752 ZDOT = 1458
274376
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 16232
51357708
00016717 00000-0 10270-3 0 9119
2 25544 51
6431 102
0405 0001295 145
0026 215
1213 15
55065122 14832
Satellite: ISS
Catalog Number: 25544
Epoch time: 16232
51357708 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 102
0405 deg
Eccentricity:
0001295
Arg of perigee: 145
0026 deg
Mean anomaly: 215
1213 deg
Mean motion: 15
55065122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 255
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