[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 4th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 109 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 101 ET - UTC (sec) : 66 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 2252)
---------------------------------------
Vector Time (GMT): 2011/306/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6444096
75 A = 6772499
47 meter
Y = 1067998
88 meter E =
0028660
Z = -1730490
89 I = 51
63260
XDOT = -2283
309759 Wp = 19
66989
YDOT = -4626
102729 meter/sec RA = 182
69637 deg
ZDOT = 5701
365002 TA = 321
26595
MA = 321
47110
Ha = 219
319 n
mi
Hp = 201
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21142049
72 X = -6447153
91
Y = 3503933
32 feet Y = 995919
92 meter
Z = -5677463
54 Z = -1761803
99
XDOT = -7491
173751 XDOT = -2259
106481
YDOT = -15177
502393 feet/sec YDOT = -4651
500698 meter/sec
ZDOT = 18705
265755 ZDOT = 5690
331446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6118077
55 X = -1864790
04
Y = -20502834
87 feet Y = -6249264
07 meter
Z = -5805195
67 Z = -1769423
64
XDOT = 12610
301702 XDOT = 3843
619959
YDOT = -8997
677148 feet/sec YDOT = -2742
491995 meter/sec
ZDOT = 18660
480036 ZDOT = 5687
714315
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 11306
66016952
00016717 00000-0 10270-3 0 9003
2 25544 51
6371 183
7608 0021745 12
8034 347
3669 15
59473463 22532
Satellite: ISS
Catalog Number: 25544
Epoch time: 11306
66016952 = yrday
fracday
Element set: 900
Inclination: 51
6371 deg
RA of node: 183
7608 deg
Eccentricity:
0021745
Arg of perigee: 12
8034 deg
Mean anomaly: 347
3669 deg
Mean motion: 15
59473463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2253
Checksum: 309
Coasting Arc #2 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2011/307/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6458024
40 A = 6772352
00 meter
Y = 1124501
61 meter E =
0018562
Z = -1748320
47 I = 51
66325
XDOT = -2330
022183 Wp = 36
73686
YDOT = 4584
597448 meter/sec RA = 177
70184 deg
ZDOT = -5674
644196 TA = 162
44331
MA = 162
37906
Ha = 219
467 n
mi
Hp = 200
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21187744
08 X = 6453463
12
Y = 3689309
74 feet Y = 1196693
65 meter
Z = -5735959
54 Z = -1716958
23
XDOT = -7644
429734 XDOT = -2353
548245
YDOT = 15041
330210 feet/sec YDOT = 4558
410010 meter/sec
ZDOT = -18617
599069 ZDOT = -5686
020816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -633394
65 X = -193058
69
Y = 21530922
67 feet Y = 6562625
23 meter
Z = -5608111
75 Z = -1709352
46
XDOT = -14388
587093 XDOT = -4385
641346
YDOT = -5270
134251 feet/sec YDOT = -1606
336920 meter/sec
ZDOT = -18664
196422 ZDOT = -5688
847069
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 11307
68545717
00016717 00000-0 10270-3 0 9013
2 25544 51
6373 178
6075 0021916 16
7428 343
4446 15
59551650 22697
Satellite: ISS
Catalog Number: 25544
Epoch time: 11307
68545717 = yrday
fracday
Element set: 901
Inclination: 51
6373 deg
RA of node: 178
6075 deg
Eccentricity:
0021916
Arg of perigee: 16
7428 deg
Mean anomaly: 343
4446 deg
Mean motion: 15
59551650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 324
Coasting Arc #3 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2011/308/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4068693
25 A = 6765135
50 meter
Y = -3027882
49 meter E =
0023410
Z = 4453823
69 I = 51
66897
XDOT = 6087
744079 Wp = 43
79824
YDOT = -3385
192335 meter/sec RA = 172
68415 deg
ZDOT = 3266
281660 TA = 13
46618
MA = 13
40382
Ha = 219
529 n
mi
Hp = 200
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13348731
12 X = -4056168
58
Y = -9933997
68 feet Y = -3073310
91 meter
Z = 14612282
46 Z = 4434088
31
XDOT = 19972
913645 XDOT = 6109
278326
YDOT = -11106
274064 feet/sec YDOT = -3316
994914 meter/sec
ZDOT = 10716
147179 ZDOT = 3295
908687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7667097
00 X = 2336931
17
Y = -14846900
20 feet Y = -4525335
18 meter
Z = 14531927
23 Z = 4429331
42
XDOT = 13051
156530 XDOT = 3977
992510
YDOT = 17326
500850 feet/sec YDOT = 5281
117459 meter/sec
ZDOT = 10837
128457 ZDOT = 3303
156754
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 11308
71071979
00016717 00000-0 10270-3 0 9023
2 25544 51
6368 173
4532 0021627 20
4232 339
7784 15
59568723 22856
Satellite: ISS
Catalog Number: 25544
Epoch time: 11308
71071979 = yrday
fracday
Element set: 902
Inclination: 51
6368 deg
RA of node: 173
4532 deg
Eccentricity:
0021627
Arg of perigee: 20
4232 deg
Mean anomaly: 339
7784 deg
Mean motion: 15
59568723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 323
Coasting Arc #4 (Orbit 2299)
---------------------------------------
Vector Time (GMT): 2011/309/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 301504
47 A = 6761571
79 meter
Y = 4217340
02 meter E =
0030203
Z = -5295667
45 I = 51
68799
XDOT = -7545
078580 Wp = 52
24101
YDOT = 1207
468892 meter/sec RA = 167
63440 deg
ZDOT = 552
230400 TA = 222
91193
MA = 223
14797
Ha = 219
523 n
mi
Hp = 200
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 989187
90 X = 280048
70
Y = 13836417
38 feet Y = 4220591
42 meter
Z = -17374237
05 Z = -5294255
03
XDOT = -24754
194815 XDOT = -7560
702636
YDOT = 3961
512113 feet/sec YDOT = 1123
007862 meter/sec
ZDOT = 1811
779528 ZDOT = 515
537877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13426343
60 X = -4092349
53
Y = 3514519
84 feet Y = 1071225
65 meter
Z = -17368664
30 Z = -5293968
88
XDOT = -8006
408283 XDOT = -2440
353245
YDOT = -22700
288479 feet/sec YDOT = -6919
047928 meter/sec
ZDOT = 1662
066572 ZDOT = 506
597891
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 11309
67188131
00016717 00000-0 10270-3 0 9039
2 25544 51
6375 168
6226 0021625 24
5877 335
6305 15
59595217 23008
Satellite: ISS
Catalog Number: 25544
Epoch time: 11309
67188131 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 168
6226 deg
Eccentricity:
0021625
Arg of perigee: 24
5877 deg
Mean anomaly: 335
6305 deg
Mean motion: 15
59595217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2300
Checksum: 311
Coasting Arc #5 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2011/310/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3588616
00 A = 6767143
24 meter
Y = -4281098
36 meter E =
0029734
Z = 3817863
18 I = 51
73559
XDOT = 6264
542542 Wp = 46
45082
YDOT = 1489
290070 meter/sec RA = 162
59103 deg
ZDOT = -4177
982992 TA = 87
60653
MA = 87
26613
Ha = 219
520 n
mi
Hp = 199
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11773674
55 X = 3617674
55
Y = -14045598
29 feet Y = -4240805
62 meter
Z = 12525797
84 Z = 3835367
76
XDOT = 20552
961097 XDOT = 6267
719662
YDOT = 4886
122276 feet/sec YDOT = 1559
361610 meter/sec
ZDOT = -13707
293281 ZDOT = -4147
541642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16039338
43 X = 4888790
35
Y = 8765794
41 feet Y = 2671814
14 meter
Z = 12597393
63 Z = 3839685
58
XDOT = -169
851000 XDOT = -51
770585
YDOT = 20020
736756 feet/sec YDOT = 6102
320563 meter/sec
ZDOT = -13583
189520 ZDOT = -4140
156166
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 11310
69709443
00016717 00000-0 10270-3 0 9049
2 25544 51
6367 163
4676 0021574 28
1748 332
0570 15
59615120 23169
Satellite: ISS
Catalog Number: 25544
Epoch time: 11310
69709443 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 163
4676 deg
Eccentricity:
0021574
Arg of perigee: 28
1748 deg
Mean anomaly: 332
0570 deg
Mean motion: 15
59615120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 302
Coasting Arc #6 (Orbit 2330)
---------------------------------------
Vector Time (GMT): 2011/311/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5962522
12 A = 6773034
88 meter
Y = 3091269
26 meter E =
0031902
Z = -742756
16 I = 51
78545
XDOT = -2775
369169 Wp = 34
82699
YDOT = -3951
794381 meter/sec RA = 157
59072 deg
ZDOT = 5983
992391 TA = 317
13081
MA = 317
37909
Ha = 219
537 n
mi
Hp = 199
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19562080
46 X = -5993037
90
Y = 10141959
53 feet Y = 3024422
04 meter
Z = -2436864
06 Z = -771796
95
XDOT = -9105
541893 XDOT = -2760
042932
YDOT = -12965
204663 feet/sec YDOT = -3982
744358 meter/sec
ZDOT = 19632
520968 ZDOT = 5970
546724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14019438
27 X = -4273124
78
Y = -16982271
42 feet Y = -5176196
33 meter
Z = -2555474
37 Z = -778908
59
XDOT = 9500
477381 XDOT = 2895
745506
YDOT = -10717
708813 feet/sec YDOT = -3266
757646 meter/sec
ZDOT = 19577
854959 ZDOT = 5967
330192
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 11311
65820893
00016717 00000-0 10270-3 0 9050
2 25544 51
6378 158
6365 0021593 31
9110 328
3348 15
59663818 23313
Satellite: ISS
Catalog Number: 25544
Epoch time: 11311
65820893 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 158
6365 deg
Eccentricity:
0021593
Arg of perigee: 31
9110 deg
Mean anomaly: 328
3348 deg
Mean motion: 15
59663818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2331
Checksum: 317
Coasting Arc #7 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2011/312/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6159461
41 A = 6770004
34 meter
Y = -764571
71 meter E =
0022329
Z = -2739475
86 I = 51
80291
XDOT = -1618
962804 Wp = 48
47810
YDOT = 5416
113720 meter/sec RA = 152
60251 deg
ZDOT = -5164
497878 TA = 162
43920
MA = 162
36188
Ha = 219
599 n
mi
Hp = 199
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20208206
72 X = 6180861
41
Y = -2508437
37 feet Y = -695573
24 meter
Z = -8987781
70 Z = -2709500
48
XDOT = -5311
557756 XDOT = -1654
317722
YDOT = 17769
401967 feet/sec YDOT = 5397
811692 meter/sec
ZDOT = -16943
890675 ZDOT = -5172
448987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7037454
30 X = 2145016
07
Y = 19165646
81 feet Y = 5841689
15 meter
Z = -8865456
36 Z = -2702191
10
XDOT = -17089
259348 XDOT = -5208
806249
YDOT = -1558
142477 feet/sec YDOT = -474
921827 meter/sec
ZDOT = -16976
587050 ZDOT = -5174
463733
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 11312
68337286
00016717 00000-0 10270-3 0 9064
2 25544 51
6373 153
4820 0021667 35
5592 324
7002 15
59721485 23472
Satellite: ISS
Catalog Number: 25544
Epoch time: 11312
68337286 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 153
4820 deg
Eccentricity:
0021667
Arg of perigee: 35
5592 deg
Mean anomaly: 324
7002 deg
Mean motion: 15
59721485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 310
Coasting Arc #8 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2011/313/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4078763
69 A = 6762452
79 meter
Y = -2043337
56 meter E =
0022972
Z = 4971540
32 I = 51
80470
XDOT = 5199
300957 Wp = 54
91807
YDOT = -5266
154747 meter/sec RA = 147
58053 deg
ZDOT = 2107
280246 TA = 14
72137
MA = 14
65459
Ha = 219
643 n
mi
Hp = 199
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13381770
63 X = -4079763
01
Y = -6703863
40 feet Y = -2088954
37 meter
Z = 16310827
82 Z = 4951722
75
XDOT = 17058
074006 XDOT = 5247
564658
YDOT = -17277
410587 feet/sec YDOT = -5207
743109 meter/sec
ZDOT = 6913
649101 ZDOT = 2132
656363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3219735
23 X = 981375
30
Y = -14706280
82 feet Y = -4482474
40 meter
Z = 16230073
42 Z = 4946926
38
XDOT = 19827
292757 XDOT = 6043
358832
YDOT = 12063
331957 feet/sec YDOT = 3676
903581 meter/sec
ZDOT = 7017
443382 ZDOT = 2138
916743
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 11313
70851106
00016717 00000-0 10270-3 0 9071
2 25544 51
6374 148
3274 0021484 39
0902 321
1801 15
59772161 23633
Satellite: ISS
Catalog Number: 25544
Epoch time: 11313
70851106 = yrday
fracday
Element set: 907
Inclination: 51
6374 deg
RA of node: 148
3274 deg
Eccentricity:
0021484
Arg of perigee: 39
0902 deg
Mean anomaly: 321
1801 deg
Mean motion: 15
59772161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 288
Coasting Arc #9 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2011/314/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 742089
93 A = 6762054
61 meter
Y = 4444600
08 meter E =
0030232
Z = -5061958
01 I = 51
82907
XDOT = -6677
175647 Wp = 65
53504
YDOT = 3244
333571 meter/sec RA = 142
53566 deg
ZDOT = 1890
822944 TA = 222
64513
MA = 222
88021
Ha = 219
615 n
mi
Hp = 199
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2434678
24 X = 716925
10
Y = 14582021
26 feet Y = 4452757
96 meter
Z = -16607473
80 Z = -5058413
91
XDOT = -21906
744249 XDOT = -6722
143672
YDOT = 10644
139013 feet/sec YDOT = 3169
413841 meter/sec
ZDOT = 6203
487349 ZDOT = 1858
275195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13420010
21 X = -4090419
11
Y = 6240104
24 feet Y = 1901983
77 meter
Z = -16593239
99 Z = -5057619
55
XDOT = -15530
466226 XDOT = -4733
686106
YDOT = -17441
467380 feet/sec YDOT = -5316
159257 meter/sec
ZDOT = 6070
514646 ZDOT = 1850
292864
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 11314
66955699
00016717 00000-0 10270-3 0 9080
2 25544 51
6379 143
4967 0021578 42
8540 317
4293 15
59786435 23785
Satellite: ISS
Catalog Number: 25544
Epoch time: 11314
66955699 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 143
4967 deg
Eccentricity:
0021578
Arg of perigee: 42
8540 deg
Mean anomaly: 317
4293 deg
Mean motion: 15
59786435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 359
Coasting Arc #10 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2011/315/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2715890
78 A = 6769400
02 meter
Y = -5508585
12 meter E =
0031513
Z = 2838908
52 I = 51
87729
XDOT = 5736
960047 Wp = 66
51599
YDOT = 171
384476 meter/sec RA = 137
51282 deg
ZDOT = -5098
847037 TA = 81
25213
MA = 80
89535
Ha = 219
613 n
mi
Hp = 198
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8910402
81 X = 2763495
76
Y = -18072785
83 feet Y = -5477948
29 meter
Z = 9314004
33 Z = 2852218
09
XDOT = 18822
047398 XDOT = 5759
387095
YDOT = 562
285027 feet/sec YDOT = 235
664251 meter/sec
ZDOT = -16728
500776 ZDOT = -5070
921708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19816437
45 X = 6040050
13
Y = 3508490
12 feet Y = 1069387
79 meter
Z = 9368609
64 Z = 2855552
22
XDOT = 4951
547003 XDOT = 1509
231527
YDOT = 16894
411224 feet/sec YDOT = 5149
416541 meter/sec
ZDOT = -16614
552626 ZDOT = -5064
115640
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 11315
69464706
00016717 00000-0 10270-3 0 9099
2 25544 51
6378 138
3405 0021551 46
5880 313
7065 15
59807250 23946
Satellite: ISS
Catalog Number: 25544
Epoch time: 11315
69464706 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 138
3405 deg
Eccentricity:
0021551
Arg of perigee: 46
5880 deg
Mean anomaly: 313
7065 deg
Mean motion: 15
59807250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 319
Coasting Arc #11 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2011/316/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4875914
22 A = 6772634
26 meter
Y = 4639574
03 meter E =
0034764
Z = 582948
84 I = 51
91125
XDOT = -2891
694231 Wp = 50
57818
YDOT = -3821
879605 meter/sec RA = 132
53025 deg
ZDOT = 6015
006413 TA = 315
71614
MA = 315
99376
Ha = 219
663 n
mi
Hp = 198
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15997093
91 X = -4930264
39
Y = 15221699
59 feet Y = 4584744
65 meter
Z = 1912561
82 Z = 559129
34
XDOT = -9487
185798 XDOT = -2877
962765
YDOT = -12538
975081 feet/sec YDOT = -3854
139828 meter/sec
ZDOT = 19734
273009 ZDOT = 6000
991410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19245903
41 X = -5866151
36
Y = -10842770
70 feet Y = -3304876
51 meter
Z = 1815095
04 Z = 553240
97
XDOT = 8380
355700 XDOT = 2554
332417
YDOT = -11456
230824 feet/sec YDOT = -3491
859155 meter/sec
ZDOT = 19677
283689 ZDOT = 5997
636069
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 11316
71971157
00016717 00000-0 10270-3 0 9108
2 25544 51
6390 133
1865 0021676 50
1259 310
1799 15
59850131 24102
Satellite: ISS
Catalog Number: 25544
Epoch time: 11316
71971157 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 133
1865 deg
Eccentricity:
0021676
Arg of perigee: 50
1259 deg
Mean anomaly: 310
1799 deg
Mean motion: 15
59850131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 294
Coasting Arc #12 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2011/317/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5259673
96 A = 6766497
48 meter
Y = -1909798
14 meter E =
0027271
Z = -3836377
94 I = 51
91098
XDOT = -742
915776 Wp = 58
72697
YDOT = 6360
840893 meter/sec RA = 127
53948 deg
ZDOT = -4193
246279 TA = 167
20017
MA = 167
13080
Ha = 219
615 n
mi
Hp = 198
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17256148
15 X = 5299275
57
Y = -6265741
92 feet Y = -1850759
59 meter
Z = -12586541
80 Z = -3810729
88
XDOT = -2437
387716 XDOT = -793
618320
YDOT = 20868
900568 feet/sec YDOT = 6352
249912 meter/sec
ZDOT = -13757
369681 ZDOT = -4196
978210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11323743
35 X = 3451476
97
Y = 14540771
63 feet Y = 4432027
19 meter
Z = -12481746
77 Z = -3804436
42
XDOT = -19511
598908 XDOT = -5947
135347
YDOT = 3395
443704 feet/sec YDOT = 1034
931241 meter/sec
ZDOT = -13772
960606 ZDOT = -4197
998393
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 11317
68068609
00016717 00000-0 10270-3 0 9115
2 25544 51
6392 128
3537 0021553 53
6042 306
7098 15
59884602 24257
Satellite: ISS
Catalog Number: 25544
Epoch time: 11317
68068609 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 128
3537 deg
Eccentricity:
0021553
Arg of perigee: 53
6042 deg
Mean anomaly: 306
7098 deg
Mean motion: 15
59884602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 316
Coasting Arc #13 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2011/318/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3792095
26 A = 6760453
53 meter
Y = -1767524
44 meter E =
0023259
Z = 5291847
43 I = 51
91012
XDOT = 3793
174397 Wp = 62
61106
YDOT = -6676
766043 meter/sec RA = 122
50860 deg
ZDOT = 496
857392 TA = 22
73456
MA = 22
63172
Ha = 219
661 n
mi
Hp = 198
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12441257
40 X = -3797755
84
Y = -5798964
71 feet Y = -1809961
95 meter
Z = 17361704
17 Z = 5273411
29
XDOT = 12444
797889 XDOT = 3865
139713
YDOT = -21905
400405 feet/sec YDOT = -6633
946093 meter/sec
ZDOT = 1630
109555 ZDOT = 515
459314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1393309
91 X = 424680
86
Y = -13750477
11 feet Y = -4191145
42 meter
Z = 17286547
25 Z = 5268939
60
XDOT = 23758
968829 XDOT = 7241
733699
YDOT = 4516
258987 feet/sec YDOT = 1376
555739 meter/sec
ZDOT = 1706
430947 ZDOT = 520
120153
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 11318
70569941
00016717 00000-0 10270-3 0 9125
2 25544 51
6400 123
1988 0021571 56
9639 303
3585 15
59972353 24411
Satellite: ISS
Catalog Number: 25544
Epoch time: 11318
70569941 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 123
1988 deg
Eccentricity:
0021571
Arg of perigee: 56
9639 deg
Mean anomaly: 303
3585 deg
Mean motion: 15
59972353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 320
Coasting Arc #14 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2011/319/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1283231
03 A = 6764167
79 meter
Y = 4994422
27 meter E =
0028257
Z = -4396594
74 I = 51
93842
XDOT = -5290
567909 Wp = 74
82199
YDOT = 4355
176779 meter/sec RA = 117
47320 deg
ZDOT = 3428
712394 TA = 229
68759
MA = 229
93485
Ha = 219
593 n
mi
Hp = 198
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4210075
56 X = 1248645
16
Y = 16385899
85 feet Y = 5008579
01 meter
Z = -14424523
44 Z = -4390444
47
XDOT = -17357
506264 XDOT = -5355
531409
YDOT = 14288
637726 feet/sec YDOT = 4295
650986 meter/sec
ZDOT = 11249
056412 ZDOT = 3402
852948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13926684
60 X = -4244853
47
Y = 9642881
48 feet Y = 2939150
28 meter
Z = -14399709
00 Z = -4389031
30
XDOT = -18684
773227 XDOT = -5695
118880
YDOT = -10470
338118 feet/sec YDOT = -3191
359058 meter/sec
ZDOT = 11143
226441 ZDOT = 3396
455419
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 11319
66662867
00016717 00000-0 10270-3 0 9133
2 25544 51
6403 118
3675 0021642 60
5167 299
8144 15
59979974 24561
Satellite: ISS
Catalog Number: 25544
Epoch time: 11319
66662867 = yrday
fracday
Element set: 913
Inclination: 51
6403 deg
RA of node: 118
3675 deg
Eccentricity:
0021642
Arg of perigee: 60
5167 deg
Mean anomaly: 299
8144 deg
Mean motion: 15
59979974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 348
Coasting Arc #15 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2011/320/15:45:39
421
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1486674
66 A = 6771479
34 meter
Y = -6452472
85 meter E =
0031759
Z = 1397718
03 I = 51
97592
XDOT = 4991
554449 Wp = 85
45175
YDOT = -138
132550 meter/sec RA = 112
47558 deg
ZDOT = -5830
971858 TA = 79
34857
MA = 78
99107
Ha = 219
611 n
mi
Hp = 197
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4877541
55 X = 1551927
07
Y = -21169530
34 feet Y = -6435483
15 meter
Z = 4585689
07 Z = 1405098
59
XDOT = 16376
490975 XDOT = 5021
054162
YDOT = -453
190781 feet/sec YDOT = -82
148740 meter/sec
ZDOT = -19130
485098 ZDOT = -5806
651006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21501802
76 X = 6553749
48
Y = -3054676
23 feet Y = -931065
32 meter
Z = 4616210
78 Z = 1407021
05
XDOT = 6108
520813 XDOT = 1861
877144
YDOT = 13666
880724 feet/sec YDOT = 4165
665245 meter/sec
ZDOT = -19031
175868 ZDOT = -5800
702404
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 11320
69159357
00016717 00000-0 10270-3 0 9144
2 25544 51
6402 113
2119 0021688 64
3709 295
9684 15
59998641 24727
Satellite: ISS
Catalog Number: 25544
Epoch time: 11320
69159357 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 113
2119 deg
Eccentricity:
0021688
Arg of perigee: 64
3709 deg
Mean anomaly: 295
9684 deg
Mean motion: 15
59998641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 335
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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