Date:
May 20th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 1854)
---------------------------------------
Vector Time (GMT): 2010/136/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4772523
40 A = 6730774
89 meter
Y = 4409693
39 meter E =
0014856
Z = 1716806
23 I = 51
83606
XDOT = -4455
743108 Wp = 25
87146
YDOT = 2589
270476 meter/sec RA = 30
75285 deg
ZDOT = 5730
409067 TA = 353
08756
MA = 353
10803
Ha = 190
661 n
mi
Hp = 185
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15657885
18 X = 4714518
69
Y = 14467497
99 feet Y = 4462738
02 meter
Z = 5632566
38 Z = 1739851
11
XDOT = -14618
579751 XDOT = -4512
203199
YDOT = 8494
981875 feet/sec YDOT = 2539
127212 meter/sec
ZDOT = 18800
554681 ZDOT = 5708
626070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17502428
53 X = -5334740
22
Y = -12128499
29 feet Y = -3696766
58 meter
Z = 5724348
95 Z = 1744781
56
XDOT = 12504
756811 XDOT = 3811
449876
YDOT = -9204
750827 feet/sec YDOT = -2805
608052 meter/sec
ZDOT = 18713
789363 ZDOT = 5703
962998
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 10136
93339497
00016717 00000-0 10270-3 0 9005
2 25544 51
6465 30
9730 0009637 319
9852 40
0600 15
74029215 18558
Satellite: ISS
Catalog Number: 25544
Epoch time: 10136
93339497 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 30
9730 deg
Eccentricity:
0009637
Arg of perigee: 319
9852 deg
Mean anomaly: 40
0600 deg
Mean motion: 15
74029215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1855
Checksum: 307
Coasting Arc #2 (Orbit 1869)
---------------------------------------
Vector Time (GMT): 2010/137/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3691284
11 A = 6721246
92 meter
Y = -2588574
13 meter E =
0008078
Z = -4989255
21 I = 51
77748
XDOT = 5876
774485 Wp = 56
09790
YDOT = 4554
593959 meter/sec RA = 25
59796 deg
ZDOT = 1991
557929 TA = 233
09406
MA = 233
16811
Ha = 190
873 n
mi
Hp = 184
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12110512
16 X = 3744192
68
Y = -8492697
29 feet Y = -2546999
50 meter
Z = -16368947
53 Z = -4971194
69
XDOT = 19280
756183 XDOT = 5815
732742
YDOT = 14942
893567 feet/sec YDOT = 4619
969977 meter/sec
ZDOT = 6533
982707 ZDOT = 2019
959788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10716427
02 X = -3266366
96
Y = 10310125
41 feet Y = 3142526
23 meter
Z = -16297004
66 Z = -4967327
02
XDOT = -20603
855121 XDOT = -6280
055041
YDOT = -10943
793883 feet/sec YDOT = -3335
668375 meter/sec
ZDOT = 6647
103820 ZDOT = 2026
037244
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 10137
88572043
00016717 00000-0 10270-3 0 9017
2 25544 51
6464 26
0838 0009693 323
6842 36
3663 15
74069677 18705
Satellite: ISS
Catalog Number: 25544
Epoch time: 10137
88572043 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 26
0838 deg
Eccentricity:
0009693
Arg of perigee: 323
6842 deg
Mean anomaly: 36
3663 deg
Mean motion: 15
74069677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1870
Checksum: 326
Coasting Arc #3 (Orbit 1885)
---------------------------------------
Vector Time (GMT): 2010/138/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5445081
54 A = 6730521
98 meter
Y = -3534602
63 meter E =
0002537
Z = -1782154
40 I = 51
78136
XDOT = 3999
110087 Wp = 343
19434
YDOT = -3288
995084 meter/sec RA = 20
50452 deg
ZDOT = -5691
074018 TA = 216
49731
MA = 216
51460
Ha = 190
975 n
mi
Hp = 184
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17864440
75 X = -5396494
89
Y = -11596465
32 feet Y = -3595220
90 meter
Z = -5846963
25 Z = -1808489
04
XDOT = 13120
439919 XDOT = 4063
237243
YDOT = -10790
666285 feet/sec YDOT = -3243
915429 meter/sec
ZDOT = -18671
502684 ZDOT = -5671
490935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19579688
97 X = 5967889
20
Y = 8307493
04 feet Y = 2532123
88 meter
Z = -5951854
30 Z = -1814125
19
XDOT = -10538
491872 XDOT = -3212
132323
YDOT = 11506
539623 feet/sec YDOT = 3507
193277 meter/sec
ZDOT = -18593
491277 ZDOT = -5667
296141
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 10138
90151730
00016717 00000-0 10270-3 0 9028
2 25544 51
6465 20
8669 0009747 327
4264 32
6297 15
74077316 18868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10138
90151730 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 20
8669 deg
Eccentricity:
0009747
Arg of perigee: 327
4264 deg
Mean anomaly: 32
6297 deg
Mean motion: 15
74077316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1886
Checksum: 320
Coasting Arc #4 (Orbit 1901)
---------------------------------------
Vector Time (GMT): 2010/139/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3285418
77 A = 6721299
26 meter
Y = 3148914
36 meter E =
0012118
Z = 4949759
61 I = 51
72209
XDOT = -6527
714635 Wp = 2
22565
YDOT = -3503
042110 meter/sec RA = 15
34278 deg
ZDOT = -2092
193405 TA = 108
09627
MA = 107
96424
Ha = 191
194 n
mi
Hp = 184
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10778932
97 X = -3344431
36
Y = 10331083
87 feet Y = 3111844
43 meter
Z = 16239368
81 Z = 4933656
00
XDOT = -21416
386597 XDOT = -6477
894331
YDOT = -11492
920308 feet/sec YDOT = -3575
760143 meter/sec
ZDOT = -6864
151590 ZDOT = -2123
784370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8695886
27 X = 2650506
13
Y = -12222016
80 feet Y = -3725270
72 meter
Z = 16175217
36 Z = 4930206
25
XDOT = 22288
956366 XDOT = 6793
673900
YDOT = 6555
037961 feet/sec YDOT = 1997
975570 meter/sec
ZDOT = -6989
981049 ZDOT = -2130
546224
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 10139
91729707
00016717 00000-0 10270-3 0 9036
2 25544 51
6470 15
6501 0009855 331
8208 28
2421 15
74108936 19020
Satellite: ISS
Catalog Number: 25544
Epoch time: 10139
91729707 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 15
6501 deg
Eccentricity:
0009855
Arg of perigee: 331
8208 deg
Mean anomaly: 28
2421 deg
Mean motion: 15
74108936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1902
Checksum: 300
Coasting Arc #5 (Orbit 1917)
---------------------------------------
Vector Time (GMT): 2010/140/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5918295
53 A = 6730247
65 meter
Y = 2571461
10 meter E =
0016978
Z = 1872557
97 I = 51
72328
XDOT = -3489
260451 Wp = 31
27672
YDOT = 3905
203770 meter/sec RA = 10
24706 deg
ZDOT = 5656
659377 TA = 349
51755
MA = 349
55290
Ha = 191
215 n
mi
Hp = 183
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19416980
10 X = 5880004
57
Y = 8436552
18 feet Y = 2637428
78 meter
Z = 6143562
91 Z = 1901216
28
XDOT = -11447
704893 XDOT = -3560
148887
YDOT = 12812
348327 feet/sec YDOT = 3865
788015 meter/sec
ZDOT = 18558
593758 ZDOT = 5639
536614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20712520
75 X = -6313176
33
Y = -4215498
81 feet Y = -1284884
04 meter
Z = 6257711
08 Z = 1907350
34
XDOT = 8327
670628 XDOT = 2538
274008
YDOT = -13428
458968 feet/sec YDOT = -4092
994293 meter/sec
ZDOT = 18490
382792 ZDOT = 5635
868675
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 10140
93306002
00016717 00000-0 10270-3 0 9040
2 25544 51
6472 10
4335 0009857 335
6985 24
3712 15
74123761 19186
Satellite: ISS
Catalog Number: 25544
Epoch time: 10140
93306002 = yrday
fracday
Element set: 904
Inclination: 51
6472 deg
RA of node: 10
4335 deg
Eccentricity:
0009857
Arg of perigee: 335
6985 deg
Mean anomaly: 24
3712 deg
Mean motion: 15
74123761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1918
Checksum: 290
Coasting Arc #6 (Orbit 1932)
---------------------------------------
Vector Time (GMT): 2010/141/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2788607
87 A = 6721263
91 meter
Y = -3651132
34 meter E =
0010209
Z = -4911166
39 I = 51
66316
XDOT = 6980
557184 Wp = 55
20922
YDOT = 2373
561823 meter/sec RA = 5
08053 deg
ZDOT = 2207
984999 TA = 236
19535
MA = 236
29260
Ha = 191
393 n
mi
Hp = 183
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9148975
96 X = 2853085
92
Y = -11978780
63 feet Y = -3619587
66 meter
Z = -16112750
62 Z = -4897462
85
XDOT = 22902
090498 XDOT = 6942
770724
YDOT = 7787
276321 feet/sec YDOT = 2451
411167 meter/sec
ZDOT = 7244
045271 ZDOT = 2241
805085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6310672
92 X = -1923493
11
Y = 13752328
38 feet Y = 4191709
69 meter
Z = -16058161
49 Z = -4894527
62
XDOT = -23022
334107 XDOT = -7017
207436
YDOT = -1982
948463 feet/sec YDOT = -604
402692 meter/sec
ZDOT = 7378
749821 ZDOT = 2249
042946
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 10141
88532237
00016717 00000-0 10270-3 0 9057
2 25544 51
6470 5
5440 0009910 339
3975 20
6787 15
74173682 19331
Satellite: ISS
Catalog Number: 25544
Epoch time: 10141
88532237 = yrday
fracday
Element set: 905
Inclination: 51
6470 deg
RA of node: 5
5440 deg
Eccentricity:
0009910
Arg of perigee: 339
3975 deg
Mean anomaly: 20
6787 deg
Mean motion: 15
74173682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1933
Checksum: 312
Coasting Arc #7 (Orbit 1948)
---------------------------------------
Vector Time (GMT): 2010/142/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6228747
86 A = 6729881
14 meter
Y = -1584621
50 meter E =
0004634
Z = -2006176
15 I = 51
66144
XDOT = 2921
161516 Wp = 16
49798
YDOT = -4414
810893 meter/sec RA = 359
98202 deg
ZDOT = -5581
232722 TA = 185
82828
MA = 185
83368
Ha = 191
509 n
mi
Hp = 183
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20435524
47 X = -6200819
65
Y = -5198889
43 feet Y = -1654118
80 meter
Z = -6581942
74 Z = -2036367
97
XDOT = 9583
863240 XDOT = 2997
424518
YDOT = -14484
287708 feet/sec YDOT = -4381
717993 meter/sec
ZDOT = -18311
130978 ZDOT = -5566
856582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21048251
02 X = 6415506
91
Y = 113317
38 feet Y = 34539
14 meter
Z = -6702191
42 Z = -2042827
94
XDOT = -5893
668718 XDOT = -1796
390225
YDOT = 14863
498438 feet/sec YDOT = 4530
394324 meter/sec
ZDOT = -18253
862437 ZDOT = -5563
777271
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 10142
90105323
00016717 00000-0 10270-3 0 9064
2 25544 51
6464
3272 0009930 342
9511 17
1317 15
74167707 19496
Satellite: ISS
Catalog Number: 25544
Epoch time: 10142
90105323 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node:
3272 deg
Eccentricity:
0009930
Arg of perigee: 342
9511 deg
Mean anomaly: 17
1317 deg
Mean motion: 15
74167707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1949
Checksum: 284
Coasting Arc #8 (Orbit 1964)
---------------------------------------
Vector Time (GMT): 2010/143/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2306890
20 A = 6721391
35 meter
Y = 4058936
70 meter E =
0013902
Z = 4837285
19 I = 51
60366
XDOT = -7214
743886 Wp = 14
60418
YDOT = -1241
547871 meter/sec RA = 354
80707 deg
ZDOT = -2384
213361 TA = 98
74799
MA = 98
59051
Ha = 191
633 n
mi
Hp = 183
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7568537
41 X = -2375605
52
Y = 13316721
47 feet Y = 4032755
13 meter
Z = 15870358
25 Z = 4825911
53
XDOT = -23670
419575 XDOT = -7188
742202
YDOT = -4073
319788 feet/sec YDOT = -1322
081882 meter/sec
ZDOT = -7822
222314 ZDOT = -2419
200046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3960018
34 X = 1207013
59
Y = -14844938
29 feet Y = -4524737
19 meter
Z = 15825048
56 Z = 4823474
80
XDOT = 22791
570935 XDOT = 6946
870821
YDOT = -2458
939045 feet/sec YDOT = -749
484621 meter/sec
ZDOT = -7961
562730 ZDOT = -2426
684320
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 10143
91676546
00016717 00000-0 10270-3 0 9077
2 25544 51
6471 355
1098 0010125 346
3395 13
7493 15
74234337 19656
Satellite: ISS
Catalog Number: 25544
Epoch time: 10143
91676546 = yrday
fracday
Element set: 907
Inclination: 51
6471 deg
RA of node: 355
1098 deg
Eccentricity:
0010125
Arg of perigee: 346
3395 deg
Mean anomaly: 13
7493 deg
Mean motion: 15
74234337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1965
Checksum: 317
Coasting Arc #9 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2010/144/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6335118
81 A = 6729460
95 meter
Y = 585686
08 meter E =
0018629
Z = 2155329
06 I = 51
60030
XDOT = -2328
463955 Wp = 38
36522
YDOT = 4862
766453 meter/sec RA = 349
70661 deg
ZDOT = 5511
650938 TA = 345
80326
MA = 345
85555
Ha = 191
687 n
mi
Hp = 182
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20784510
53 X = 6317628
33
Y = 1921542
26 feet Y = 656431
15 meter
Z = 7071289
56 Z = 2186063
20
XDOT = -7639
317439 XDOT = -2409
442319
YDOT = 15953
958179 feet/sec YDOT = 4836
274891 meter/sec
ZDOT = 18082
844284 ZDOT = 5500
142809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20471114
68 X = -6239595
75
Y = 3856892
27 feet Y = 1175580
76 meter
Z = 7193690
62 Z = 2192636
90
XDOT = 3340
619298 XDOT = 1018
220762
YDOT = -15976
747878 feet/sec YDOT = -4869
712753 meter/sec
ZDOT = 18036
994071 ZDOT = 5497
675793
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 10144
93246354
00016717 00000-0 10270-3 0 9081
2 25544 51
6465 349
8931 0010112 351
0100 9
0881 15
74220932 19811
Satellite: ISS
Catalog Number: 25544
Epoch time: 10144
93246354 = yrday
fracday
Element set: 908
Inclination: 51
6465 deg
RA of node: 349
8931 deg
Eccentricity:
0010112
Arg of perigee: 351
0100 deg
Mean anomaly: 9
0881 deg
Mean motion: 15
74220932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1981
Checksum: 286
Coasting Arc #10 (Orbit 1995)
---------------------------------------
Vector Time (GMT): 2010/145/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1745056
86 A = 6721605
20 meter
Y = -4411720
84 meter E =
0011953
Z = -4767319
02 I = 51
54350
XDOT = 7254
361356 Wp = 56
34439
YDOT = 107
265262 meter/sec RA = 344
52541 deg
ZDOT = 2567
273273 TA = 238
81046
MA = 238
92770
Ha = 191
895 n
mi
Hp = 182
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5725252
17 X = 1817419
04
Y = -14474149
74 feet Y = -4391801
41 meter
Z = -15640810
45 Z = -4758666
13
XDOT = 23800
398148 XDOT = 7240
151143
YDOT = 351
920151 feet/sec YDOT = 188
308090 meter/sec
ZDOT = 8422
812576 ZDOT = 2602
481136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1345154
10 X = -410002
97
Y = 15541798
76 feet Y = 4737140
26 meter
Z = -15606329
68 Z = -4756809
29
XDOT = -21688
079114 XDOT = -6610
526514
YDOT = 6684
785448 feet/sec YDOT = 2037
522605 meter/sec
ZDOT = 8563
030535 ZDOT = 2610
011707
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 10145
88466407
00016717 00000-0 10270-3 0 9090
2 25544 51
6455 345
0023 0010236 354
8470 5
2586 15
74256979 19964
Satellite: ISS
Catalog Number: 25544
Epoch time: 10145
88466407 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 345
0023 deg
Eccentricity:
0010236
Arg of perigee: 354
8470 deg
Mean anomaly: 5
2586 deg
Mean motion: 15
74256979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1996
Checksum: 328
Coasting Arc #11 (Orbit 2011)
---------------------------------------
Vector Time (GMT): 2010/146/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6298886
50 A = 6728891
04 meter
Y = 369037
40 meter E =
0007493
Z = -2352344
42 I = 51
53972
XDOT = 1706
962952 Wp = 30
57633
YDOT = -5213
852900 meter/sec RA = 339
42179 deg
ZDOT = -5389
872612 TA = 175
91853
MA = 175
91241
Ha = 192
001 n
mi
Hp = 182
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20665638
13 X = -6291117
53
Y = 1210752
62 feet Y = 298643
28 meter
Z = -7717665
43 Z = -2382926
04
XDOT = 5600
272151 XDOT = 1791
321819
YDOT = -17105
816600 feet/sec YDOT = -5194
292176 meter/sec
ZDOT = -17683
309094 ZDOT = -5381
375873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19245097
82 X = 5865905
82
Y = -7501061
56 feet Y = -2286323
56 meter
Z = -7839462
13 Z = -2389468
06
XDOT = -706
782785 XDOT = -215
427393
YDOT = 16628
349835 feet/sec YDOT = 5068
321030 meter/sec
ZDOT = -17649
442081 ZDOT = -5379
549946
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 10146
90032882
00016717 00000-0 10270-3 0 9102
2 25544 51
6456 339
7845 0010285 359
0411 1
0731 15
74281332 20120
Satellite: ISS
Catalog Number: 25544
Epoch time: 10146
90032882 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 339
7845 deg
Eccentricity:
0010285
Arg of perigee: 359
0411 deg
Mean anomaly: 1
0731 deg
Mean motion: 15
74281332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2012
Checksum: 276
Coasting Arc #12 (Orbit 2027)
---------------------------------------
Vector Time (GMT): 2010/147/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1226275
26 A = 6721858
98 meter
Y = 4698754
96 meter E =
0015911
Z = 4647668
91 I = 51
48841
XDOT = -7106
082893 Wp = 28
02894
YDOT = 944
966802 meter/sec RA = 334
23265 deg
ZDOT = -2812
554688 TA = 89
88683
MA = 89
70451
Ha = 192
064 n
mi
Hp = 182
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4023212
79 X = -1301304
31
Y = 15415862
72 feet Y = 4684621
75 meter
Z = 15248257
57 Z = 4641530
08
XDOT = -23313
920253 XDOT = -7102
458459
YDOT = 3100
284783 feet/sec YDOT = 865
523073 meter/sec
ZDOT = -9227
541626 ZDOT = -2847
067591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1107821
86 X = -337664
10
Y = -15917086
66 feet Y = -4851528
01 meter
Z = 15223780
94 Z = 4640208
43
XDOT = 19836
602284 XDOT = 6046
196376
YDOT = -10393
400301 feet/sec YDOT = -3167
908412 meter/sec
ZDOT = -9365
001821 ZDOT = -2854
452555
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 10147
91597463
00016717 00000-0 10270-3 0 9116
2 25544 51
6456 334
5667 0010388 1
7977 358
3222 15
74334044 20286
Satellite: ISS
Catalog Number: 25544
Epoch time: 10147
91597463 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 334
5667 deg
Eccentricity:
0010388
Arg of perigee: 1
7977 deg
Mean anomaly: 358
3222 deg
Mean motion: 15
74334044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2028
Checksum: 316
Coasting Arc #13 (Orbit 2043)
---------------------------------------
Vector Time (GMT): 2010/148/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6080508
40 A = 6728393
00 meter
Y = -1267205
54 meter E =
0019993
Z = 2553585
25 I = 51
48324
XDOT = -1067
337200 Wp = 47
02903
YDOT = 5526
311410 meter/sec RA = 329
12747 deg
ZDOT = 5271
440429 TA = 342
04798
MA = 342
11850
Ha = 192
189 n
mi
Hp = 181
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19949174
54 X = 6081821
62
Y = -4157498
48 feet Y = -1199202
77 meter
Z = 8377904
37 Z = 2583127
64
XDOT = -3501
762468 XDOT = -1154
662047
YDOT = 18130
942947 feet/sec YDOT = 5513
886640 meter/sec
ZDOT = 17294
752063 ZDOT = 5266
044092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17295103
25 X = -5271547
47
Y = 10684018
63 feet Y = 3256488
88 meter
Z = 8495574
71 Z = 2589451
17
XDOT = -2005
718840 XDOT = -611
343102
YDOT = -17014
005923 feet/sec YDOT = -5185
869005 meter/sec
ZDOT = 17273
226035 ZDOT = 5264
879296
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 10148
93160737
00016717 00000-0 10270-3 0 9120
2 25544 51
6452 329
3486 0010518 7
3496 352
7819 15
74304910 20443
Satellite: ISS
Catalog Number: 25544
Epoch time: 10148
93160737 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 329
3486 deg
Eccentricity:
0010518
Arg of perigee: 7
3496 deg
Mean anomaly: 352
7819 deg
Mean motion: 15
74304910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2044
Checksum: 307
Coasting Arc #14 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2010/149/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626717
49 A = 6722262
36 meter
Y = -4928558
17 meter E =
0013271
Z = -4534463
48 I = 51
43833
XDOT = 6793
028985 Wp = 58
33976
YDOT = -1934
709741 meter/sec RA = 323
93168 deg
ZDOT = 3055
133378 TA = 242
10442
MA = 242
23889
Ha = 192
318 n
mi
Hp = 181
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2056159
76 X = 703810
67
Y = -16169810
28 feet Y = -4921118
00 meter
Z = -14876848
68 Z = -4531232
47
XDOT = 22286
840503 XDOT = 6799
317016
YDOT = -6347
472902 feet/sec YDOT = -1858
711425 meter/sec
ZDOT = 10023
403471 ZDOT = 3088
149039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3763265
29 X = 1147043
26
Y = 15871734
90 feet Y = 4837704
80 meter
Z = -14863951
35 Z = -4530532
37
XDOT = -17345
342528 XDOT = -5286
860403
YDOT = 13581
589219 feet/sec YDOT = 4139
668394 meter/sec
ZDOT = 10154
916018 ZDOT = 3095
218402
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 10149
88374473
00016717 00000-0 10270-3 0 9130
2 25544 51
6461 324
4569 0010572 10
2923 349
8455 15
74346884 20594
Satellite: ISS
Catalog Number: 25544
Epoch time: 10149
88374473 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 324
4569 deg
Eccentricity:
0010572
Arg of perigee: 10
2923 deg
Mean anomaly: 349
8455 deg
Mean motion: 15
74346884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 328
Coasting Arc #15 (Orbit 2074)
---------------------------------------
Vector Time (GMT): 2010/150/20:57:33
838
Vector Time (MET): N/A
Weight (LBS) : 794797
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5762413
21 A = 6727554
32 meter
Y = 2067652
45 meter E =
0010557
Z = -2806110
88 I = 51
43351
XDOT = 412
969339 Wp = 39
36029
YDOT = -5750
596751 meter/sec RA = 318
82519 deg
ZDOT = -5087
737238 TA = 172
84167
MA = 172
82658
Ha = 192
382 n
mi
Hp = 181
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18905555
16 X = -5771474
20
Y = 6783636
65 feet Y = 2003163
53 meter
Z = -9206400
53 Z = -2834126
39
XDOT = 1354
886283 XDOT = 501
958201
YDOT = -18866
787241 feet/sec YDOT = -5745
480257 meter/sec
ZDOT = -16692
051305 ZDOT = -5085
515849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14965852
18 X = 4561591
74
Y = -13318921
69 feet Y = -4059607
33 meter
Z = -9318001
21 Z = -2840126
77
XDOT = 4710
254445 XDOT = 1435
685555
YDOT = 16958
835696 feet/sec YDOT = 5169
053120 meter/sec
ZDOT = -16683
174061 ZDOT = -5085
031454
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 10150
89934214
00016717 00000-0 10270-3 0 9149
2 25544 51
6466 319
2388 0010608 14
4065 345
7399 15
74392199 20753
Satellite: ISS
Catalog Number: 25544
Epoch time: 10150
89934214 = yrday
fracday
Element set: 914
Inclination: 51
6466 deg
RA of node: 319
2388 deg
Eccentricity:
0010608
Arg of perigee: 14
4065 deg
Mean anomaly: 345
7399 deg
Mean motion: 15
74392199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2075
Checksum: 326
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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