[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 17th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 119 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3420)
---------------------------------------
Vector Time (GMT): 2012/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5844834
40 A = 6774456
67 meter
Y = -2872952
46 meter E =
0008334
Z = 1873593
00 I = 51
72788
XDOT = 3629
759431 Wp = 275
00412
YDOT = 3722
686018 meter/sec RA = 166
94288 deg
ZDOT = -5635
857451 TA = 244
37680
MA = 244
46293
Ha = 215
928 n
mi
Hp = 205
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19175965
90 X = 5867424
48
Y = -9425697
04 feet Y = -2807465
70 meter
Z = 6146958
65 Z = 1902041
57
XDOT = 11908
659552 XDOT = 3615
239453
YDOT = 12213
536804 feet/sec YDOT = 3763
195271 meter/sec
ZDOT = -18490
345969 ZDOT = -5618
259426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16523315
87 X = 5036306
68
Y = 13494212
72 feet Y = 4113036
04 meter
Z = 6263608
32 Z = 1909147
82
XDOT = -5132
106492 XDOT = -1564
266059
YDOT = 14802
302142 feet/sec YDOT = 4511
741693 meter/sec
ZDOT = -18418
526762 ZDOT = -5613
966957
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 12016
53576473
00016717 00000-0 10270-3 0 9007
2 25544 51
6385 167
8435 0022051 286
2306 73
6423 15
58719617 34216
Satellite: ISS
Catalog Number: 25544
Epoch time: 12016
53576473 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 167
8435 deg
Eccentricity:
0022051
Arg of perigee: 286
2306 deg
Mean anomaly: 73
6423 deg
Mean motion: 15
58719617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 307
Coasting Arc #2 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2012/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6552287
64 A = 6775143
88 meter
Y = 1008884
00 meter E =
0016841
Z = 1357884
25 I = 51
76113
XDOT = 433
251244 Wp = 329
28412
YDOT = -4975
609663 meter/sec RA = 161
95815 deg
ZDOT = 5833
316621 TA = 45
51754
MA = 45
37997
Ha = 216
063 n
mi
Hp = 205
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21497006
71 X = -6569678
47
Y = 3309986
87 feet Y = 935514
96 meter
Z = 4455000
81 Z = 1326011
48
XDOT = 1421
427965 XDOT = 460
520482
YDOT = -16324
178683 feet/sec YDOT = -4970
612688 meter/sec
ZDOT = 19138
177890 ZDOT = 5835
487242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12262836
08 X = -3737712
44
Y = -17995735
27 feet Y = -5485100
11 meter
Z = 4324431
29 Z = 1318086
66
XDOT = 13979
794875 XDOT = 4261
041478
YDOT = -4962
383992 feet/sec YDOT = -1512
534641 meter/sec
ZDOT = 19147
377579 ZDOT = 5836
120686
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 12017
56155488
00016717 00000-0 10270-3 0 9011
2 25544 51
6398 162
6934 0021919 289
9769 69
9026 15
58765582 34378
Satellite: ISS
Catalog Number: 25544
Epoch time: 12017
56155488 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 162
6934 deg
Eccentricity:
0021919
Arg of perigee: 289
9769 deg
Mean anomaly: 69
9026 deg
Mean motion: 15
58765582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 363
Coasting Arc #3 (Orbit 3451)
---------------------------------------
Vector Time (GMT): 2012/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5275073
80 A = 6768955
94 meter
Y = 1229183
51 meter E =
0017382
Z = -4056450
41 I = 51
76895
XDOT = -4199
226959 Wp = 310
19469
YDOT = 5115
121273 meter/sec RA = 156
95982 deg
ZDOT = -3888
818129 TA = 279
54534
MA = 279
74172
Ha = 216
336 n
mi
Hp = 205
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17306672
56 X = 5280641
96
Y = 4032754
31 feet Y = 1288204
11 meter
Z = -13308564
34 Z = -4030810
87
XDOT = -13776
991335 XDOT = -4237
222291
YDOT = 16781
893939 feet/sec YDOT = 5067
950824 meter/sec
ZDOT = -12758
589662 ZDOT = -3909
309508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4153917
93 X = 1266114
19
Y = 17358301
13 feet Y = 5290810
19 meter
Z = -13203645
52 Z = -4024471
15
XDOT = -19866
052113 XDOT = -6055
172684
YDOT = -5070
101296 feet/sec YDOT = -1545
366875 meter/sec
ZDOT = -12842
830686 ZDOT = -3914
494793
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 12018
52321867
00016717 00000-0 10270-3 0 9025
2 25544 51
6397 157
8665 0021995 294
0008 65
8845 15
58772886 34527
Satellite: ISS
Catalog Number: 25544
Epoch time: 12018
52321867 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 157
8665 deg
Eccentricity:
0021995
Arg of perigee: 294
0008 deg
Mean anomaly: 65
8845 deg
Mean motion: 15
58772886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3452
Checksum: 346
Coasting Arc #4 (Orbit 3467)
---------------------------------------
Vector Time (GMT): 2012/019/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2446475
92 A = 6763863
57 meter
Y = -3430038
40 meter E =
0019271
Z = 5305299
99 I = 51
78049
XDOT = 6558
475867 Wp = 299
05845
YDOT = -3935
505669 meter/sec RA = 151
92769 deg
ZDOT = 490
411625 TA = 146
33130
MA = 146
20872
Ha = 216
488 n
mi
Hp = 205
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8026495
80 X = -2433710
39
Y = -11253406
82 feet Y = -3457325
54 meter
Z = 17405839
86 Z = 5293445
92
XDOT = 21517
309275 XDOT = 6599
613753
YDOT = -12911
764006 feet/sec YDOT = -3861
934794 meter/sec
ZDOT = 1608
962024 ZDOT = 522
371600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6226217
93 X = 1897751
22
Y = -12408790
43 feet Y = -3782199
32 meter
Z = 17357511
09 Z = 5290569
38
XDOT = 20478
730926 XDOT = 6241
917186
YDOT = 12661
269734 feet/sec YDOT = 3859
155015 meter/sec
ZDOT = 1740
115673 ZDOT = 530
387257
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 12019
54897611
00016717 00000-0 10270-3 0 9034
2 25544 51
6403 152
7157 0022047 298
0251 61
8674 15
58806133 34684
Satellite: ISS
Catalog Number: 25544
Epoch time: 12019
54897611 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 152
7157 deg
Eccentricity:
0022047
Arg of perigee: 298
0251 deg
Mean anomaly: 61
8674 deg
Mean motion: 15
58806133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3468
Checksum: 312
Coasting Arc #5 (Orbit 3482)
---------------------------------------
Vector Time (GMT): 2012/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -923749
01 A = 6766750
61 meter
Y = 4892887
82 meter E =
0012240
Z = -4570033
55 I = 51
81738
XDOT = -6859
819892 Wp = 311
45716
YDOT = 1580
272941 meter/sec RA = 146
89359 deg
ZDOT = 3081
103577 TA = 349
20042
MA = 349
22668
Ha = 216
696 n
mi
Hp = 205
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3030672
61 X = -956193
78
Y = 16052781
55 feet Y = 4882376
93 meter
Z = -14993548
39 Z = -4574599
33
XDOT = -22505
970773 XDOT = -6891
948044
YDOT = 5184
622511 feet/sec YDOT = 1503
382274 meter/sec
ZDOT = 10108
607535 ZDOT = 3047
701538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15510720
73 X = -4727667
68
Y = 5071834
08 feet Y = 1545895
03 meter
Z = -15012571
62 Z = -4575831
83
XDOT = -14950
479878 XDOT = -4556
906267
YDOT = -16230
860752 feet/sec YDOT = -4947
166357 meter/sec
ZDOT = 9971
678661 ZDOT = 3039
367656
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 12020
51060832
00016717 00000-0 10270-3 0 9041
2 25544 51
6408 147
8889 0022020 301
6123 58
2883 15
58824115 34835
Satellite: ISS
Catalog Number: 25544
Epoch time: 12020
51060832 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 147
8889 deg
Eccentricity:
0022020
Arg of perigee: 301
6123 deg
Mean anomaly: 58
2883 deg
Mean motion: 15
58824115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3483
Checksum: 290
Coasting Arc #6 (Orbit 3498)
---------------------------------------
Vector Time (GMT): 2012/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3838619
23 A = 6773644
28 meter
Y = -5157849
33 meter E =
0009438
Z = 2151739
55 I = 51
86611
XDOT = 5105
070693 Wp = 329
94795
YDOT = 1499
232413 meter/sec RA = 141
88993 deg
ZDOT = -5515
982159 TA = 186
25610
MA = 186
26790
Ha = 216
910 n
mi
Hp = 205
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12593895
12 X = 3885557
60
Y = -16922077
85 feet Y = -5114661
28 meter
Z = 7059512
96 Z = 2170500
54
XDOT = 16748
919595 XDOT = 5114
721378
YDOT = 4918
741511 feet/sec YDOT = 1556
374909 meter/sec
ZDOT = -18097
054327 ZDOT = -5491
158907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20906886
78 X = 6372419
09
Y = 2601734
25 feet Y = 793008
60 meter
Z = 7136714
97 Z = 2175270
72
XDOT = 4202
303066 XDOT = 1280
861974
YDOT = 15571
834508 feet/sec YDOT = 4746
295158 meter/sec
ZDOT = -17995
454453 ZDOT = -5485
014517
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 12021
53633283
00016717 00000-0 10270-3 0 9051
2 25544 51
6414 142
7388 0021991 305
5528 54
3577 15
58840952 34999
Satellite: ISS
Catalog Number: 25544
Epoch time: 12021
53633283 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 142
7388 deg
Eccentricity:
0021991
Arg of perigee: 305
5528 deg
Mean anomaly: 54
3577 deg
Mean motion: 15
58840952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3499
Checksum: 324
Coasting Arc #7 (Orbit 3514)
---------------------------------------
Vector Time (GMT): 2012/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5421972
36 A = 6775100
64 meter
Y = 3886137
43 meter E =
0022291
Z = 1103809
01 I = 51
89559
XDOT = -2010
871006 Wp = 345
91620
YDOT = -4473
278952 meter/sec RA = 136
91340 deg
ZDOT = 5917
394785 TA = 26
05741
MA = 25
94537
Ha = 217
223 n
mi
Hp = 205
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17788623
24 X = -5470386
88
Y = 12749794
71 feet Y = 3825234
82 meter
Z = 3621420
63 Z = 1077352
66
XDOT = -6597
345821 XDOT = -1989
445097
YDOT = -14676
112048 feet/sec YDOT = -4495
646382 meter/sec
ZDOT = 19414
024884 ZDOT = 5907
678024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20018401
90 X = -6101608
90
Y = -8889947
70 feet Y = -2709656
06 meter
Z = 3512760
20 Z = 1070689
31
XDOT = 8598
112790 XDOT = 2620
704778
YDOT = -11767
123815 feet/sec YDOT = -3586
619339 meter/sec
ZDOT = 19374
506627 ZDOT = 5905
349620
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 12022
56203995
00016717 00000-0 10270-3 0 9069
2 25544 51
6426 137
5885 0022031 309
9470 49
9749 15
58869862 35157
Satellite: ISS
Catalog Number: 25544
Epoch time: 12022
56203995 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 137
5885 deg
Eccentricity:
0022031
Arg of perigee: 309
9470 deg
Mean anomaly: 49
9749 deg
Mean motion: 15
58869862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3515
Checksum: 340
Coasting Arc #8 (Orbit 3529)
---------------------------------------
Vector Time (GMT): 2012/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5352062
35 A = 6769078
67 meter
Y = -1358610
86 meter E =
0019535
Z = -3920313
92 I = 51
89738
XDOT = -1396
694925 Wp = 329
99767
YDOT = 6343
455321 meter/sec RA = 131
92584 deg
ZDOT = -4079
884330 TA = 257
36634
MA = 257
58485
Ha = 217
430 n
mi
Hp = 205
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17559259
69 X = 5385900
32
Y = -4457384
71 feet Y = -1298571
41 meter
Z = -12861922
32 Z = -3894232
43
XDOT = -4582
332432 XDOT = -1447
706287
YDOT = 20811
861290 feet/sec YDOT = 6327
551609 meter/sec
ZDOT = -13385
447278 ZDOT = -4086
792804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13003575
96 X = 3963489
95
Y = 12721757
60 feet Y = 3877591
72 meter
Z = -12754952
81 Z = -3887709
62
XDOT = -19175
604475 XDOT = -5844
724244
YDOT = 6067
398543 feet/sec YDOT = 1849
343076 meter/sec
ZDOT = -13414
177543 ZDOT = -4088
641315
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 12023
52362469
00016717 00000-0 10270-3 0 9079
2 25544 51
6429 132
7616 0022064 313
3147 46
6168 15
58893631 35302
Satellite: ISS
Catalog Number: 25544
Epoch time: 12023
52362469 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 132
7616 deg
Eccentricity:
0022064
Arg of perigee: 313
3147 deg
Mean anomaly: 46
6168 deg
Mean motion: 15
58893631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3530
Checksum: 305
Coasting Arc #9 (Orbit 3545)
---------------------------------------
Vector Time (GMT): 2012/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3776169
03 A = 6763489
87 meter
Y = -1884679
71 meter E =
0019293
Z = 5294244
60 I = 51
89942
XDOT = 4143
819728 Wp = 320
64694
YDOT = -6416
169869 meter/sec RA = 126
90295 deg
ZDOT = 687
450610 TA = 122
90498
MA = 122
71922
Ha = 217
632 n
mi
Hp = 204
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12389006
00 X = -3780531
06
Y = -6183332
38 feet Y = -1926931
69 meter
Z = 17369568
91 Z = 5275889
99
XDOT = 13595
209083 XDOT = 4211
919257
YDOT = -21050
426078 feet/sec YDOT = -6369
450380 meter/sec
ZDOT = 2255
415388 ZDOT = 707
745785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1481441
14 X = -451543
26
Y = -13861081
31 feet Y = -4224857
58 meter
Z = 17294471
66 Z = 5271354
96
XDOT = 24039
886571 XDOT = 7327
357427
YDOT = 283
681296 feet/sec YDOT = 86
466059 meter/sec
ZDOT = 2339
016465 ZDOT = 712
932218
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 12024
54929722
00016717 00000-0 10270-3 0 9084
2 25544 51
6434 127
6110 0022141 317
4350 42
5088 15
58958124 35469
Satellite: ISS
Catalog Number: 25544
Epoch time: 12024
54929722 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 127
6110 deg
Eccentricity:
0022141
Arg of perigee: 317
4350 deg
Mean anomaly: 42
5088 deg
Mean motion: 15
58958124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3546
Checksum: 297
Coasting Arc #10 (Orbit 3560)
---------------------------------------
Vector Time (GMT): 2012/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1355608
93 A = 6766038
94 meter
Y = 4716041
21 meter E =
0014218
Z = -4648544
45 I = 51
92549
XDOT = -5503
890667 Wp = 344
42575
YDOT = 4477
103524 meter/sec RA = 121
87517 deg
ZDOT = 2948
346327 TA = 314
69110
MA = 314
80684
Ha = 217
854 n
mi
Hp = 204
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4447535
85 X = 1325353
47
Y = 15472576
14 feet Y = 4731031
32 meter
Z = -15251130
07 Z = -4642032
59
XDOT = -18057
384079 XDOT = -5567
867513
YDOT = 14688
659857 feet/sec YDOT = 4415
197901 meter/sec
ZDOT = 9673
052253 ZDOT = 2921
453982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10414524
62 X = -3174347
10
Y = 12309454
06 feet Y = 3751921
60 meter
Z = -15224755
29 Z = -4640505
41
XDOT = -21339
610069 XDOT = -6504
313149
YDOT = -6273
153477 feet/sec YDOT = -1912
057180 meter/sec
ZDOT = 9562
533532 ZDOT = 2914
660221
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 12025
51085167
00016717 00000-0 10270-3 0 9099
2 25544 51
6431 122
7842 0022079 321
3430 38
6144 15
58981724 35615
Satellite: ISS
Catalog Number: 25544
Epoch time: 12025
51085167 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 122
7842 deg
Eccentricity:
0022079
Arg of perigee: 321
3430 deg
Mean anomaly: 38
6144 deg
Mean motion: 15
58981724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3561
Checksum: 298
Coasting Arc #11 (Orbit 3576)
---------------------------------------
Vector Time (GMT): 2012/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1226865
63 A = 6773140
44 meter
Y = -6284661
70 meter E =
0013800
Z = 2232875
10 I = 51
96370
XDOT = 5274
338676 Wp = 2
66492
YDOT = -922
786955 meter/sec RA = 116
87683 deg
ZDOT = -5480
510425 TA = 152
62370
MA = 152
55092
Ha = 218
066 n
mi
Hp = 204
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4025149
70 X = 1286204
23
Y = -20618968
83 feet Y = -6270610
33 meter
Z = 7325705
71 Z = 2238979
22
XDOT = 17304
260749 XDOT = 5310
887951
YDOT = -3027
516255 feet/sec YDOT = -863
601756 meter/sec
ZDOT = -17980
677247 ZDOT = -5454
799715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19261744
86 X = 5870979
83
Y = -8363939
01 feet Y = -2549328
61 meter
Z = 7351148
15 Z = 2240629
96
XDOT = 11726
486934 XDOT = 3574
233218
YDOT = 11252
325663 feet/sec YDOT = 3429
708862 meter/sec
ZDOT = -17875
232263 ZDOT = -5448
370794
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 12026
53649241
00016717 00000-0 10270-3 0 9103
2 25544 51
6425 117
6341 0022115 325
3979 34
5736 15
58973371 35776
Satellite: ISS
Catalog Number: 25544
Epoch time: 12026
53649241 = yrday
fracday
Element set: 910
Inclination: 51
6425 deg
RA of node: 117
6341 deg
Eccentricity:
0022115
Arg of perigee: 325
3979 deg
Mean anomaly: 34
5736 deg
Mean motion: 15
58973371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3577
Checksum: 313
Coasting Arc #12 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2012/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3233071
35 A = 6774799
16 meter
Y = 5839697
03 meter E =
0026725
Z = 1050162
29 I = 51
98239
XDOT = -3744
220245 Wp =
04730
YDOT = -3136
543036 meter/sec RA = 111
90544 deg
ZDOT = 5940
360914 TA = 11
33035
MA = 11
27030
Ha = 218
374 n
mi
Hp = 204
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10607189
48 X = -3303233
08
Y = 19159110
99 feet Y = 5803150
56 meter
Z = 3445414
34 Z = 1034285
94
XDOT = -12284
187154 XDOT = -3737
724897
YDOT = -10290
495525 feet/sec YDOT = -3178
376780 meter/sec
ZDOT = 19489
373076 ZDOT = 5922
187845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21774474
42 X = -6636859
80
Y = 2429641
23 feet Y = 740554
65 meter
Z = 3379939
33 Z = 1030205
51
XDOT = 1384
359723 XDOT = 421
952844
YDOT = -14481
653044 feet/sec YDOT = -4414
007848 meter/sec
ZDOT = 19415
096128 ZDOT = 5917
721300
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 12027
56211545
00016717 00000-0 10270-3 0 9110
2 25544 51
6428 112
4831 0022260 329
5196 30
4664 15
58988338 35936
Satellite: ISS
Catalog Number: 25544
Epoch time: 12027
56211545 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 112
4831 deg
Eccentricity:
0022260
Arg of perigee: 329
5196 deg
Mean anomaly: 30
4664 deg
Mean motion: 15
58988338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 310
Coasting Arc #13 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2012/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4272583
48 A = 6768696
98 meter
Y = -3505244
00 meter E =
0021911
Z = -3921930
29 I = 51
97144
XDOT = 1416
440027 Wp = 349
90455
YDOT = 6327
378632 meter/sec RA = 106
92227 deg
ZDOT = -4087
573166 TA = 237
37885
MA = 237
59051
Ha = 218
515 n
mi
Hp = 204
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14017662
32 X = 4330513
82
Y = -11500144
34 feet Y = -3457141
50 meter
Z = -12867225
37 Z = -3901033
83
XDOT = 4647
112948 XDOT = 1365
436933
YDOT = 20759
116247 feet/sec YDOT = 6342
932889 meter/sec
ZDOT = -13410
673118 ZDOT = -4080
816272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17619116
23 X = 5370306
63
Y = 4529696
07 feet Y = 1380651
36 meter
Z = -12781324
75 Z = -3895747
78
XDOT = -13580
477566 XDOT = -4139
329562
YDOT = 14832
168951 feet/sec YDOT = 4520
845096 meter/sec
ZDOT = -13383
415158 ZDOT = -4079
264940
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 12028
52362090
00016717 00000-0 10270-3 0 9120
2 25544 51
6416 107
6551 0022231 332
9838 27
0158 15
59019471 36088
Satellite: ISS
Catalog Number: 25544
Epoch time: 12028
52362090 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 107
6551 deg
Eccentricity:
0022231
Arg of perigee: 332
9838 deg
Mean anomaly: 27
0158 deg
Mean motion: 15
59019471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 292
Coasting Arc #14 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2012/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203533
69 A = 6763115
16 meter
Y = -158811
06 meter E =
0020175
Z = 5299237
91 I = 51
96177
XDOT = 1077
884282 Wp = 342
25220
YDOT = -7570
240380 meter/sec RA = 101
90217 deg
ZDOT = 647
507994 TA = 101
71101
MA = 101
48456
Ha = 218
730 n
mi
Hp = 203
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13791121
03 X = -4227187
58
Y = -521033
65 feet Y = -205949
76 meter
Z = 17385951
15 Z = 5278760
15
XDOT = 3536
365756 XDOT = 1159
310709
YDOT = -24836
746655 feet/sec YDOT = -7557
731528 meter/sec
ZDOT = 2124
370058 ZDOT = 652
942094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8018365
90 X = -2443997
93
Y = -11361503
40 feet Y = -3462986
24 meter
Z = 17302018
43 Z = 5273655
22
XDOT = 21051
611606 XDOT = 6416
531217
YDOT = -11684
497014 feet/sec YDOT = -3561
434690 meter/sec
ZDOT = 2147
182946 ZDOT = 654
461362
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 12029
54920905
00016717 00000-0 10270-3 0 9139
2 25544 51
6422 102
5034 0022319 336
8183 23
1963 15
59076444 36240
Satellite: ISS
Catalog Number: 25544
Epoch time: 12029
54920905 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 102
5034 deg
Eccentricity:
0022319
Arg of perigee: 336
8183 deg
Mean anomaly: 23
1963 deg
Mean motion: 15
59076444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 293
Coasting Arc #15 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2012/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 885127
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3182389
63 A = 6765872
13 meter
Y = 3775831
82 meter E =
0017792
Z = -4618556
09 I = 51
97559
XDOT = -3142
948100 Wp = 7
79429
YDOT = 6323
035334 meter/sec RA = 96
87658 deg
ZDOT = 3022
199283 TA = 292
07834
MA = 292
26718
Ha = 218
955 n
mi
Hp = 203
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10440910
86 X = 3162366
64
Y = 12387899
66 feet Y = 3811307
31 meter
Z = -15152743
07 Z = -4603144
99
XDOT = -10311
509513 XDOT = -3228
100945
YDOT = 20744
866583 feet/sec YDOT = 6287
412834 meter/sec
ZDOT = 9915
351979 ZDOT = 3006
724339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3181660
99 X = -969770
27
Y = 15945283
10 feet Y = 4860122
29 meter
Z = -15089840
30 Z = -4599383
32
XDOT = -21542
373140 XDOT = -6566
115333
YDOT = 4966
693715 feet/sec YDOT = 1513
848244 meter/sec
ZDOT = 9851
454323 ZDOT = 3002
723278
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 12030
51068443
00016717 00000-0 10270-3 0 9149
2 25544 51
6412 97
6753 0022360 341
0624 18
9698 15
59097082 36399
Satellite: ISS
Catalog Number: 25544
Epoch time: 12030
51068443 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 97
6753 deg
Eccentricity:
0022360
Arg of perigee: 341
0624 deg
Mean anomaly: 18
9698 deg
Mean motion: 15
59097082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 312
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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