[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 16th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 1818)
---------------------------------------
Vector Time (GMT): 2013/319/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3487489
42 A = 6789767
88 meter
Y = 2777427
27 meter E =
0006080
Z = 5117583
49 I = 51
98271
XDOT = -2903
649744 Wp = 125
05417
YDOT = -6874
952601 meter/sec RA = 77
65141 deg
ZDOT = 1747
572867 TA = 308
09629
MA = 308
15110
Ha = 227
539 n
mi
Hp = 220
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11441894
41 X = -3543148
49
Y = 9112294
20 feet Y = 2738116
78 meter
Z = 16789972
07 Z = 5100505
92
XDOT = -9526
409921 XDOT = -2835
046150
YDOT = -22555
618770 feet/sec YDOT = -6907
039460 meter/sec
ZDOT = 5733
506781 ZDOT = 1733
633540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5565266
71 X = -1696293
29
Y = -13616165
71 feet Y = -4150207
31 meter
Z = 16717710
76 Z = 5095558
24
XDOT = 23326
903751 XDOT = 7110
040263
YDOT = -2545
778693 feet/sec YDOT = -775
953346 meter/sec
ZDOT = 5675
948032 ZDOT = 1730
028960
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 13319
60684744
00016717 00000-0 10270-3 0 9003
2 25544 51
6499 78
1446 0000838 127
5953 232
5274 15
50210790 18191
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
60684744 = yrday
fracday
Element set: 900
Inclination: 51
6499 deg
RA of node: 78
1446 deg
Eccentricity:
0000838
Arg of perigee: 127
5953 deg
Mean anomaly: 232
5274 deg
Mean motion: 15
50210790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1819
Checksum: 318
Coasting Arc #2 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2013/320/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3470005
46 A = 6789394
04 meter
Y = -2614330
11 meter E =
0014516
Z = -5230076
62 I = 51
97389
XDOT = 3190
054228 Wp = 82
17313
YDOT = 6831
845791 meter/sec RA = 72
71714 deg
ZDOT = -1299
653086 TA = 175
38063
MA = 175
36722
Ha = 227
428 n
mi
Hp = 220
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11384532
36 X = 3524388
54
Y = -8577198
54 feet Y = -2575222
19 meter
Z = -17159044
04 Z = -5213087
13
XDOT = 10466
057177 XDOT = 3119
735451
YDOT = 22414
192228 feet/sec YDOT = 6867
125844 meter/sec
ZDOT = -4263
953693 ZDOT = -1284
326435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5296309
49 X = 1614315
13
Y = 13326154
71 feet Y = 4061811
96 meter
Z = -17087170
93 Z = -5208169
70
XDOT = -23399
129711 XDOT = -7132
054736
YDOT = 3918
516351 feet/sec YDOT = 1194
363784 meter/sec
ZDOT = -4200
568775 ZDOT = -1280
333363
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 13320
57383155
00016717 00000-0 10270-3 0 9014
2 25544 51
6501 73
3539 0000736 126
3252 233
7967 15
50188448 18344
Satellite: ISS
Catalog Number: 25544
Epoch time: 13320
57383155 = yrday
fracday
Element set: 901
Inclination: 51
6501 deg
RA of node: 73
3539 deg
Eccentricity:
0000736
Arg of perigee: 126
3252 deg
Mean anomaly: 233
7967 deg
Mean motion: 15
50188448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 302
Coasting Arc #3 (Orbit 1849)
---------------------------------------
Vector Time (GMT): 2013/321/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3472603
79 A = 6788866
87 meter
Y = 2447706
13 meter E =
0004014
Z = 5292395
15 I = 51
96326
XDOT = -3482
595304 Wp = 120
25402
YDOT = -6775
439407 meter/sec RA = 67
78106 deg
ZDOT = 846
057042 TA = 321
67548
MA = 321
70399
Ha = 227
449 n
mi
Hp = 220
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11393057
04 X = -3525426
15
Y = 8030531
93 feet Y = 2408577
79 meter
Z = 17363501
16 Z = 5275396
89
XDOT = -11425
837611 XDOT = -3410
682025
YDOT = -22229
131913 feet/sec YDOT = -6813
981936 meter/sec
ZDOT = 2775
777697 ZDOT = 829
312987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4992152
04 X = -1521607
94
Y = -13109576
84 feet Y = -3995799
02 meter
Z = 17291610
03 Z = 5270482
74
XDOT = 23389
165248 XDOT = 7129
017567
YDOT = -5326
205963 feet/sec YDOT = -1623
427577 meter/sec
ZDOT = 2706
436692 ZDOT = 824
921904
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 13321
60526399
00016717 00000-0 10270-3 0 9029
2 25544 51
6506 68
2428 0000743 125
0413 235
0808 15
50256132 18505
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
60526399 = yrday
fracday
Element set: 902
Inclination: 51
6506 deg
RA of node: 68
2428 deg
Eccentricity:
0000743
Arg of perigee: 125
0413 deg
Mean anomaly: 235
0808 deg
Mean motion: 15
50256132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1850
Checksum: 278
Coasting Arc #4 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2013/322/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3530285
00 A = 6788764
98 meter
Y = -2282115
64 meter E =
0015354
Z = -5343961
01 I = 51
94972
XDOT = 3744
176546 Wp = 88
39146
YDOT = 6661
656627 meter/sec RA = 62
84482 deg
ZDOT = -371
887240 TA = 178
07260
MA = 178
06667
Ha = 227
350 n
mi
Hp = 220
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11582299
88 X = 3581501
86
Y = -7487256
05 feet Y = -2242351
16 meter
Z = -17532680
49 Z = -5326686
50
XDOT = 12284
043785 XDOT = 3671
212719
YDOT = 21855
828830 feet/sec YDOT = 6703
118443 meter/sec
ZDOT = -1220
102495 ZDOT = -353
874908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4644667
24 X = 1415694
57
Y = 13084011
29 feet Y = 3988006
64 meter
Z = -17459647
01 Z = -5321700
41
XDOT = -23118
351211 XDOT = -7046
473449
YDOT = 6680
470858 feet/sec YDOT = 2036
207517 meter/sec
ZDOT = -1145
421312 ZDOT = -349
124416
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 13322
57221990
00016717 00000-0 10270-3 0 9036
2 25544 51
6502 63
4521 0000665 119
0593 241
0624 15
50232043 18651
Satellite: ISS
Catalog Number: 25544
Epoch time: 13322
57221990 = yrday
fracday
Element set: 903
Inclination: 51
6502 deg
RA of node: 63
4521 deg
Eccentricity:
0000665
Arg of perigee: 119
0593 deg
Mean anomaly: 241
0624 deg
Mean motion: 15
50232043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 271
Coasting Arc #5 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2013/323/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3609722
26 A = 6788516
37 meter
Y = 2118295
05 meter E =
0002973
Z = 5342217
29 I = 51
93512
XDOT = -3999
037551 Wp = 90
78257
YDOT = -6538
158009 meter/sec RA = 57
90638 deg
ZDOT = -109
616926 TA =
25830
MA =
25815
Ha = 227
361 n
mi
Hp = 220
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11842920
81 X = -3659092
79
Y = 6949786
90 feet Y = 2077652
52 meter
Z = 17526959
63 Z = 5324561
42
XDOT = -13120
201940 XDOT = -3925
096703
YDOT = -21450
649636 feet/sec YDOT = -6582
464359 meter/sec
ZDOT = -359
635583 ZDOT = -128
865010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4288864
53 X = -1307245
91
Y = -13144200
47 feet Y = -4006352
30 meter
Z = 17452342
54 Z = 5319474
01
XDOT = 22766
998313 XDOT = 6939
381086
YDOT = -8012
358756 feet/sec YDOT = -2442
166949 meter/sec
ZDOT = -439
524253 ZDOT = -133
966992
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 13323
60362230
00016717 00000-0 10270-3 0 9045
2 25544 51
6506 58
3408 0000641 120
3796 239
7418 15
50300658 18817
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
60362230 = yrday
fracday
Element set: 904
Inclination: 51
6506 deg
RA of node: 58
3408 deg
Eccentricity:
0000641
Arg of perigee: 120
3796 deg
Mean anomaly: 239
7418 deg
Mean motion: 15
50300658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1881
Checksum: 286
Coasting Arc #6 (Orbit 1895)
---------------------------------------
Vector Time (GMT): 2013/324/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3738154
81 A = 6788726
19 meter
Y = -1973800
49 meter E =
0015279
Z = -5325227
03 I = 51
91740
XDOT = 4210
629699 Wp = 95
10716
YDOT = 6359
892468 meter/sec RA = 52
96730 deg
ZDOT = 598
595219 TA = 180
59646
MA = 180
59828
Ha = 227
292 n
mi
Hp = 220
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12264287
42 X = 3785817
40
Y = -6475723
38 feet Y = -1931731
27 meter
Z = -17471217
29 Z = -5306951
44
XDOT = 13814
401899 XDOT = 4136
291166
YDOT = 20865
788937 feet/sec YDOT = 6406
562726 meter/sec
ZDOT = 1963
895076 ZDOT = 618
870202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3967930
03 X = 1209425
07
Y = 13390110
08 feet Y = 4081305
55 meter
Z = -17394012
08 Z = -5301694
88
XDOT = -22160
639604 XDOT = -6754
562951
YDOT = 9226
813274 feet/sec YDOT = 2812
332686 meter/sec
ZDOT = 2048
124216 ZDOT = 624
268261
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 13324
57055041
00016717 00000-0 10270-3 0 9052
2 25544 51
6496 53
5497 0000649 107
7403 252
3819 15
50275703 18966
Satellite: ISS
Catalog Number: 25544
Epoch time: 13324
57055041 = yrday
fracday
Element set: 905
Inclination: 51
6496 deg
RA of node: 53
5497 deg
Eccentricity:
0000649
Arg of perigee: 107
7403 deg
Mean anomaly: 252
3819 deg
Mean motion: 15
50275703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1896
Checksum: 312
Coasting Arc #7 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2013/325/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3887065
93 A = 6788801
38 meter
Y = 1835921
29 meter E =
0004242
Z = 5251382
39 I = 51
89946
XDOT = -4402
187788 Wp = 62
74346
YDOT = -6178
481445 meter/sec RA = 48
02623 deg
ZDOT = -1095
880655 TA = 37
73910
MA = 37
70936
Ha = 227
295 n
mi
Hp = 220
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12752840
96 X = -3932816
85
Y = 6023363
80 feet Y = 1792197
56 meter
Z = 17228944
84 Z = 5232388
07
XDOT = -14442
873320 XDOT = -4327
447893
YDOT = -20270
608415 feet/sec YDOT = -6227
291560 meter/sec
ZDOT = -3595
408973 ZDOT = -1117
085162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3666611
01 X = -1117583
04
Y = -13719666
28 feet Y = -4181754
28 meter
Z = 17148735
38 Z = 5226934
54
XDOT = 21492
599110 XDOT = 6550
944209
YDOT = -10358
773014 feet/sec YDOT = -3157
354015 meter/sec
ZDOT = -3683
571533 ZDOT = -1122
752603
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 13325
60192309
00016717 00000-0 10270-3 0 9067
2 25544 51
6501 48
4382 0000594 110
1685 249
9530 15
50344314 19124
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
60192309 = yrday
fracday
Element set: 906
Inclination: 51
6501 deg
RA of node: 48
4382 deg
Eccentricity:
0000594
Arg of perigee: 110
1685 deg
Mean anomaly: 249
9530 deg
Mean motion: 15
50344314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 285
Coasting Arc #8 (Orbit 1926)
---------------------------------------
Vector Time (GMT): 2013/326/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4073575
14 A = 6789324
17 meter
Y = -1734038
54 meter E =
0014216
Z = -5159931
94 I = 51
87877
XDOT = 4540
737499 Wp = 101
59129
YDOT = 5950
646559 meter/sec RA = 43
08383 deg
ZDOT = 1585
900254 TA = 183
67927
MA = 183
68973
Ha = 227
258 n
mi
Hp = 220
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13364747
85 X = 4117728
63
Y = -5689102
82 feet Y = -1688238
13 meter
Z = -16928910
58 Z = -5140035
48
XDOT = 14897
432739 XDOT = 4466
154607
YDOT = 19523
118633 feet/sec YDOT = 6001
006890 meter/sec
ZDOT = 5203
084824 ZDOT = 1607
778111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3474982
08 X = 1059174
54
Y = 14203645
08 feet Y = 4329271
02 meter
Z = -16844920
76 Z = -5134331
85
XDOT = -20604
082561 XDOT = -6280
124365
YDOT = 11315
867481 feet/sec YDOT = 3449
076408 meter/sec
ZDOT = 5294
112322 ZDOT = 1613
645436
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 13326
56882382
00016717 00000-0 10270-3 0 9071
2 25544 51
6492 43
6461 0000724 96
7817 263
3417 15
50321644 19270
Satellite: ISS
Catalog Number: 25544
Epoch time: 13326
56882382 = yrday
fracday
Element set: 907
Inclination: 51
6492 deg
RA of node: 43
6461 deg
Eccentricity:
0000724
Arg of perigee: 96
7817 deg
Mean anomaly: 263
3417 deg
Mean motion: 15
50321644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1927
Checksum: 315
Coasting Arc #9 (Orbit 1942)
---------------------------------------
Vector Time (GMT): 2013/327/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4276234
85 A = 6789739
57 meter
Y = 1642187
10 meter E =
0006698
Z = 5007764
79 I = 51
85793
XDOT = -4646
624602 Wp = 60
46593
YDOT = -5729
219474 meter/sec RA = 38
14012 deg
ZDOT = -2083
765770 TA = 49
78452
MA = 49
72592
Ha = 227
265 n
mi
Hp = 220
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14029641
90 X = -4318606
95
Y = 5387752
97 feet Y = 1594130
44 meter
Z = 16429674
52 Z = 4986888
14
XDOT = -15244
831371 XDOT = -4572
091375
YDOT = -18796
651817 feet/sec YDOT = -5780
764179 meter/sec
ZDOT = -6836
501870 ZDOT = -2106
158048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3326422
50 X = -1013893
58
Y = -14754007
82 feet Y = -4497021
58 meter
Z = 16341575
98 Z = 4980912
36
XDOT = 19690
694835 XDOT = 6001
723786
YDOT = -12134
229054 feet/sec YDOT = -3698
513016 meter/sec
ZDOT = -6929
725280 ZDOT = -2112
180265
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 13327
60016740
00016717 00000-0 10270-3 0 9085
2 25544 51
6495 38
5345 0000670 98
0130 262
1097 15
50386923 19430
Satellite: ISS
Catalog Number: 25544
Epoch time: 13327
60016740 = yrday
fracday
Element set: 908
Inclination: 51
6495 deg
RA of node: 38
5345 deg
Eccentricity:
0000670
Arg of perigee: 98
0130 deg
Mean anomaly: 262
1097 deg
Mean motion: 15
50386923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1943
Checksum: 299
Coasting Arc #10 (Orbit 1957)
---------------------------------------
Vector Time (GMT): 2013/328/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4500682
73 A = 6790533
37 meter
Y = -1599395
94 meter E =
0012201
Z = -4838232
56 I = 51
83556
XDOT = 4694
392419 Wp = 106
69504
YDOT = 5474
670569 meter/sec RA = 33
19461 deg
ZDOT = 2559
025837 TA = 188
46623
MA = 188
48683
Ha = 227
238 n
mi
Hp = 220
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14766019
45 X = 4541736
09
Y = -5247362
02 feet Y = -1548836
79 meter
Z = -15873466
40 Z = -4816268
74
XDOT = 15401
549931 XDOT = 4620
393357
YDOT = 17961
517614 feet/sec YDOT = 5526
752444 meter/sec
ZDOT = 8395
754059 ZDOT = 2581
651392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3348738
04 X = 1020695
35
Y = 15404197
62 feet Y = 4695199
43 meter
Z = -15780802
36 Z = -4809988
56
XDOT = -18617
242326 XDOT = -5674
535461
YDOT = 12738
248774 feet/sec YDOT = 3882
618226 meter/sec
ZDOT = 8489
996275 ZDOT = 2587
750865
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 13328
56704110
00016717 00000-0 10270-3 0 9097
2 25544 51
6495 33
7417 0000863 91
0247 269
1003 15
50370864 19580
Satellite: ISS
Catalog Number: 25544
Epoch time: 13328
56704110 = yrday
fracday
Element set: 909
Inclination: 51
6495 deg
RA of node: 33
7417 deg
Eccentricity:
0000863
Arg of perigee: 91
0247 deg
Mean anomaly: 269
1003 deg
Mean motion: 15
50370864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1958
Checksum: 301
Coasting Arc #11 (Orbit 1973)
---------------------------------------
Vector Time (GMT): 2013/329/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4734099
18 A = 6791262
99 meter
Y = 1567674
99 meter E =
0009378
Z = 4604213
76 I = 51
81205
XDOT = -4698
905754 Wp = 68
23206
YDOT = -5238
612076 meter/sec RA = 28
24830 deg
ZDOT = -3039
424586 TA = 52
10623
MA = 52
02146
Ha = 227
258 n
mi
Hp = 220
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15531821
45 X = -4773643
69
Y = 5143290
64 feet Y = 1514514
12 meter
Z = 15105688
20 Z = 4581119
64
XDOT = -15416
357461 XDOT = -4625
212330
YDOT = -17187
047492 feet/sec YDOT = -5290
746153 meter/sec
ZDOT = -9971
865440 ZDOT = -3062
072766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3427530
46 X = -1044711
29
Y = -16089636
12 feet Y = -4904121
09 meter
Z = 15008276
93 Z = 4574522
81
XDOT = 17571
747412 XDOT = 5355
868611
YDOT = -13158
707036 feet/sec YDOT = -4010
773905 meter/sec
ZDOT = -10066
236670 ZDOT = -3068
188937
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 13329
59835640
00016717 00000-0 10270-3 0 9106
2 25544 51
6493 28
6300 0000844 91
4138 268
7110 15
50428041 19747
Satellite: ISS
Catalog Number: 25544
Epoch time: 13329
59835640 = yrday
fracday
Element set: 910
Inclination: 51
6493 deg
RA of node: 28
6300 deg
Eccentricity:
0000844
Arg of perigee: 91
4138 deg
Mean anomaly: 268
7110 deg
Mean motion: 15
50428041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1974
Checksum: 297
Coasting Arc #12 (Orbit 1988)
---------------------------------------
Vector Time (GMT): 2013/330/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4970754
52 A = 6792245
69 meter
Y = -1592762
54 meter E =
0009465
Z = -4355756
62 I = 51
78858
XDOT = 4646
390538 Wp = 107
85019
YDOT = 4986
153260 meter/sec RA = 23
30031 deg
ZDOT = 3482
551683 TA = 197
52057
MA = 197
55324
Ha = 227
218 n
mi
Hp = 220
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16308249
73 X = 5009355
07
Y = -5225598
88 feet Y = -1536960
56 meter
Z = -14290540
09 Z = -4331515
07
XDOT = 15244
063446 XDOT = 4573
371418
YDOT = 16358
770537 feet/sec YDOT = 5037
703875 meter/sec
ZDOT = 11425
694499 ZDOT = 3504
946380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3715616
89 X = 1132520
03
Y = 16803920
04 feet Y = 5121834
83 meter
Z = -14188301
21 Z = -4324594
21
XDOT = -16445
034083 XDOT = -5012
446389
YDOT = 13352
792980 feet/sec YDOT = 4069
931300 meter/sec
ZDOT = 11519
035398 ZDOT = 3511
001989
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 13330
56520342
00016717 00000-0 10270-3 0 9116
2 25544 51
6502 23
8372 0001004 90
0899 270
0367 15
50421888 19890
Satellite: ISS
Catalog Number: 25544
Epoch time: 13330
56520342 = yrday
fracday
Element set: 911
Inclination: 51
6502 deg
RA of node: 23
8372 deg
Eccentricity:
0001004
Arg of perigee: 90
0899 deg
Mean anomaly: 270
0367 deg
Mean motion: 15
50421888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1989
Checksum: 290
Coasting Arc #13 (Orbit 2004)
---------------------------------------
Vector Time (GMT): 2013/331/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5207003
38 A = 6793208
66 meter
Y = 1626656
41 meter E =
0011847
Z = 4039866
66 I = 51
76269
XDOT = -4543
455012 Wp = 79
33787
YDOT = -4765
820840 meter/sec RA = 18
35138 deg
ZDOT = -3925
201532 TA = 51
40097
MA = 51
29494
Ha = 227
242 n
mi
Hp = 220
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17083344
43 X = -5244430
91
Y = 5336799
25 feet Y = 1568219
12 meter
Z = 13254155
70 Z = 4014480
19
XDOT = -14906
348464 XDOT = -4470
756994
YDOT = -15635
895144 feet/sec YDOT = -4816
222174 meter/sec
ZDOT = -12877
957782 ZDOT = -3947
096992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4058283
29 X = -1236964
75
Y = -17512248
38 feet Y = -5337733
31 meter
Z = 13147099
30 Z = 4007235
87
XDOT = 15410
076022 XDOT = 4696
991171
YDOT = -13337
201377 feet/sec YDOT = -4065
178980 meter/sec
ZDOT = -12969
228524 ZDOT = -3953
020854
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 13331
59649120
00016717 00000-0 10270-3 0 9127
2 25544 51
6494 18
7252 0001014 89
9057 270
2210 15
50467319 20052
Satellite: ISS
Catalog Number: 25544
Epoch time: 13331
59649120 = yrday
fracday
Element set: 912
Inclination: 51
6494 deg
RA of node: 18
7252 deg
Eccentricity:
0001014
Arg of perigee: 89
9057 deg
Mean anomaly: 270
2210 deg
Mean motion: 15
50467319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2005
Checksum: 283
Coasting Arc #14 (Orbit 2019)
---------------------------------------
Vector Time (GMT): 2013/332/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5427361
52 A = 6794264
74 meter
Y = -1718769
83 meter E =
0006692
Z = -3714905
72 I = 51
73789
XDOT = 4391
538798 Wp = 98
24408
YDOT = 4547
043926 meter/sec RA = 13
40130 deg
ZDOT = 4317
856593 TA = 217
64979
MA = 217
69665
Ha = 227
185 n
mi
Hp = 220
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17806304
20 X = 5464224
16
Y = -5639008
62 feet Y = -1657871
49 meter
Z = -12188010
88 Z = -3688450
05
XDOT = 14407
935689 XDOT = 4319
390977
YDOT = 14918
123118 feet/sec YDOT = 4595
749493 meter/sec
ZDOT = 14166
196172 ZDOT = 4339
015467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4620061
10 X = 1408194
62
Y = 18172093
70 feet Y = 5538854
16 meter
Z = -12076445
79 Z = -3680900
68
XDOT = -14379
835688 XDOT = -4382
973918
YDOT = 13116
215201 feet/sec YDOT = 3997
822393 meter/sec
ZDOT = 14254
397976 ZDOT = 4344
740503
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 13332
56331194
00016717 00000-0 10270-3 0 9135
2 25544 51
6505 13
9329 0001106 91
8653 268
2624 15
50472043 20206
Satellite: ISS
Catalog Number: 25544
Epoch time: 13332
56331194 = yrday
fracday
Element set: 913
Inclination: 51
6505 deg
RA of node: 13
9329 deg
Eccentricity:
0001106
Arg of perigee: 91
8653 deg
Mean anomaly: 268
2624 deg
Mean motion: 15
50472043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2020
Checksum: 275
Coasting Arc #15 (Orbit 2035)
---------------------------------------
Vector Time (GMT): 2013/333/13:19:53
789
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5636993
28 A = 6795323
50 meter
Y = 1813370
46 meter E =
0013753
Z = 3321205
42 I = 51
71012
XDOT = -4186
667029 Wp = 91
62274
YDOT = -4374
106280 meter/sec RA = 8
44954 deg
ZDOT = -4701
213883 TA = 49
82311
MA = 49
70277
Ha = 227
189 n
mi
Hp = 219
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18494072
45 X = -5672985
70
Y = 5949378
16 feet Y = 1750132
71 meter
Z = 10896343
23 Z = 3293733
43
XDOT = -13735
784215 XDOT = -4114
605920
YDOT = -14350
742389 feet/sec YDOT = -4420
521255 meter/sec
ZDOT = -15423
930061 ZDOT = -4721
377816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5215238
75 X = -1589604
77
Y = -18781331
47 feet Y = -5724549
83 meter
Z = 10780490
95 Z = 3285893
64
XDOT = 13508
081604 XDOT = 4117
263273
YDOT = -12683
847668 feet/sec YDOT = -3866
036769 meter/sec
ZDOT = -15507
968839 ZDOT = -4726
828902
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 13333
59457266
00016717 00000-0 10270-3 0 9149
2 25544 51
6491 8
8204 0001105 90
4042 269
7235 15
50505309 20364
Satellite: ISS
Catalog Number: 25544
Epoch time: 13333
59457266 = yrday
fracday
Element set: 914
Inclination: 51
6491 deg
RA of node: 8
8204 deg
Eccentricity:
0001105
Arg of perigee: 90
4042 deg
Mean anomaly: 269
7235 deg
Mean motion: 15
50505309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2036
Checksum: 287
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